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http://timminsfunerals.com.au/library/a-second-course-in-stochastic-processes
[ "# A second course in stochastic processes by Samuel Karlin", null, "By Samuel Karlin\n\nThis moment direction maintains the improvement of the speculation and purposes of stochastic tactics as promised within the preface of a primary direction. We emphasize a cautious remedy of simple buildings in stochastic procedures in symbiosis with the research of typical periods of stochastic tactics coming up from the organic, actual, and social sciences.\n\nBest stochastic modeling books\n\nHandbook of statistics 19: Stochastic processes, theory and methods\n\nHardbound. J. Neyman, one of many pioneers in laying the rules of contemporary statistical thought, under pressure the significance of stochastic procedures in a paper written in 1960 within the following phrases: \"Currently within the interval of dynamic indeterminism in technological know-how, there's not often a significant piece of study, if handled realistically, doesn't contain operations on stochastic processes\".\n\nStochastic Dynamics of Reacting Biomolecules\n\nIt is a booklet in regards to the actual strategies in reacting complicated molecules, rather biomolecules. long ago decade scientists from assorted fields similar to medication, biology, chemistry and physics have amassed a major quantity of knowledge concerning the constitution, dynamics and functioning of biomolecules.\n\nAnalytical and stochastic modeling techniques and applications 16th international conference, ASMTA 2009, Madrid, Spain, June 9-12, 2009: proceedings\n\nThis booklet constitutes the refereed court cases of the sixteenth foreign convention on Analytical and Stochastic Modeling suggestions and purposes, ASMTA 2009, held in Madrid, Spain, in June 2009 along with ECMS 2009, the 23nd eu convention on Modeling and Simulation. The 27 revised complete papers offered have been conscientiously reviewed and chosen from fifty five submissions.\n\nIntroduction to Stochastic Calculus Applied to Finance (Stochastic Modeling)\n\nIn recent times the growing to be significance of by-product items monetary markets has elevated monetary associations' calls for for mathematical talents. This e-book introduces the mathematical equipment of economic modeling with transparent causes of the main worthy types. advent to Stochastic Calculus starts off with an undemanding presentation of discrete types, together with the Cox-Ross-Rubenstein version.\n\nExtra info for A second course in stochastic processes\n\nExample text\n\n1. I) and ( L , 1) 11) with L c B. B is not necessarily a function Space, though we use the notation f for one of its elements. It is assumed that + (a) i f f , € L, YE B, lim,,+m[f,-fl and llfll < C. = 0, and Ilf,ll < C for all n, then f E L 43 44 3. COMPACT MARKOV PROCESSES II-II A linear operator U from L into L is bounded with respect to both where the latter is the restriction of 1. I to L. In addition, and 1. IL, (b) H=supnBolUnI,< CQ; and (c) there is a k 2 1, an r < 1, and an R < 00 such that II UYII G r I l f II + R I f I for a l l f e L.\n\nThe cases of effectivefailure (0*c* > 0) and ineffectivefailure (B*c* = 0) must be distinguished. The former arises more frequently in practice. 16 0. INTRODUCTION When 8*c* > 0, the process X,, has no absorbing states and is regular, so that the distribution of X,, converges (weakly) to a limit p that does not depend on Xo = x . Let x , be the expectation of p : lim xn = xm = n-1 m I Yp(dY), and let A,, be a subject’s proportion of A , responses in the first n trials. Then A,,, is asymptotically normally distributed as n -P co, with mean xm and variance proportional to l / n .\n\nIntuitively, x* = @(x) and e* = Y ( e ) represent simplified state and event variables. In the full ZHL model, they are projections: @ ( w , z ) = (V,Y) and Y(S, a, r ) = (a,r ) 9 where s = (B, W) or (W, B), a = br or PO, and r = B or W. We now give conditions under which Xn* = @(A',,) and En* = \"(En) are state and event sequences for a learning model. Suppose that @(u(x,e))depends only on x* and e*, and that, for any A * € Y*, p ( x , \" - ' ( A * ) ) depends only on x*. 13) and p * ( @ ( x ) , A * )= p ( x , Y - ' ( A * ) ) ." ]
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http://www.uyts.com/archives/category/python
[ "### 1. 软件使用截图", null, "### 2. 软件下载安装\n\n#### 2.1 Tcl运行环境下载安装\n\npage软件的运行需要基于Tcl环境,所以先安装Tcl是必须的。\n\nActiveTcl-8.6.9.8609.2-MSWin32-x64-5ccbd9ac8\n\n#### 2.2 page5.0.3下载安装\n\nhttp://page.sourceforge.net/\n\npage-5.0.3\n\n### 3. 软件使用\n\n#### 3.1 打开软件", null, "#### 3.2 拖拽布局", null, "#### 3.3 生成代码", null, "#### 3.4 保存代码\n\n3.3保存tcl文件后,就会弹出一个新页面,这个新页面中就是对应的自动生成的python程序代码:", null, "#### 3.5 代码修改\n\n``import page_support``\n\n``page_support.init(root, top)``\n\n### 1. 安装Python链接MySQL插件。\n\n``\\$ pip3 install PyMySQL``\n\n### 2. 完整代码如下:\n\n``````import os\nimport pymysql\n\nsku = []\n\n#定义递归函数findPNG,寻找当前目录下所有png类型的文件\ndef findPNG(sku,dir):\nfor ffName in os.listdir(dir):\nif os.path.isfile(dir+\"/\"+ffName):\nif ffName.split(\".\") == \"png\":\nsku.append(ffName.split(\".\"));\nelif os.path.isdir(dir+\"/\"+ffName):\nfindPNG(sku,dir+\"/\"+ffName)\nfindPNG(sku,\"./\")\n\nh = open(\"./ProductsInformation.csv\",\"a\")\ndb = pymysql.connect(\"地址\",\"用户\",\"密码\",\"数据库名\" )\ncursor = db.cursor()\n\nfor s in sku:\nSQL = '''SELECT t1.model,t2.name,t2.tag\nFROM `product` AS t1, `product_description` AS t2\nWHERE t1.product_id = t2.product_id AND t1.model =\"{}\"'''.format(s)\ncursor.execute(SQL)\ndata = cursor.fetchone()\nif data:\nfor d in data:\nh.write('\"'+d+'\",')\nh.write('\\n')\nelse:\nprint(s)\n\nh.close()\ndb.close()``````\n\n### 答案\n\n#### 3.1\n\n``````import json\nfileURL = \"population.json\"\nr = open(fileURL,\"r\")\nfor country in popData:\nif country[\"Country\"] == \"China\":\ncountry = json.dumps(country,indent=1)\nprint(country)``````\n\n#### 3.2\n\n``````import csv\nfileURL = \"population.csv\"\nwith open(fileURL) as f:\nfor row in f_csv:\nif row == \"China\":\nprint(row)``````\n\n### Python文件IO练习\n\n#### 2.1 创建文件夹和文件\n\nTxt文件名为1-20.txt,txt内的内容为当天时间+文件名。\n\n### 答案\n\n#### 2.1\n\n``````import os\nimport datetime\nfolderUrl = \"fileset\"\nif not os.path.exists(folderUrl):\nos.mkdir(folderUrl)\nfor i in range(1,21):\nf = open(\"fileset\\\\\"+str(i)+\".txt\",\"w\")\nf.write(str(datetime.datetime.now())+\" \"+str(i)+\".txt\")\nf.close()``````\n\n#### 2.2\n\n``````import os\nfolderUrl = \"fileset\"\nfileSet = os.listdir(folderUrl)\nw = open(\"all.txt\",\"w\")\nfor fileName in fileSet:\nr = open(folderUrl + \"\\\\\" + fileName, \"r\")\nr.close()\nw.close()\nr = open(\"all.txt\",\"r\")\nfor line in r:\nprint(line)\nr.close()``````\n\n#### 2.3\n\n``````import os\ndef deleteDir(folderURL):\nfor fileName in os.listdir(folderURL):\nos.remove(folderURL+\"\\\\\"+fileName)\nos.rmdir(folderURL)\n\ndeleteDir(\"fileset\")``````\n\n### 答案:\n\n#### 1.1\n\n``````import random\nlistVar = []\nfor i in range(0,20):\nlistVar.append(random.randint(1,1000))\nlistVar.sort()\nfor i in range(0,20):\nprint((str(listVar[i])).rjust(4))``````\n\n#### 1.2\n\n``````import random\nimport string\nvarList = []\nfor i in range(0,20):\nrandomChar = string.ascii_lowercase\nvarList.append(str(random.randrange(1,1000)) + random.choice(randomChar))\nvarList.sort()\nvarTuple = tuple(varList)\nfor i in range(1,20):\nprint(varTuple[i].rjust(5))``````\n\n#### 1.3\n\n``````import random\nimport string\nrandomDict = {}\nwhile 1==1:\nkey = random.randint(1,1000)\nvalue = random.choices(string.ascii_uppercase,k=4)\nrandomDict[key] = \"\".join(value)\nif len(randomDict) == 20:\nbreak\nfor key in sorted(randomDict):\nprint(str(key).rjust(4) + \"->\" + randomDict[key])``````\n\n#### 1.4\n\n``````import random\naSet = set()\nbSet = set()\nwhile 1==1:" ]
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https://www.wikihow.com/Calculate-Lotto-Odds
[ "# How to Calculate Lotto Odds\n\nEveryone's heard comparisons between the odds of winning the lottery and the odds of other unlikely events, like getting struck by lightning. It's true, the odds of winning the jackpot on a game like Powerball or another pick-6 lottery game are incredibly low. But just how low are they? And how many times would you have to play to have a better chance of winning? These answers can be found down to the exact odds with some simple calculations.\n\n### Method 1 of 3: Calculating Powerball Jackpot Odds\n\n1. 1\nUnderstand the calculations involved. To find the odds of winning any lottery, divide the number of winning lottery numbers by the total number of possible lottery numbers. If the numbers are chosen from a set and the order of the numbers doesn't matter, use the formula ${\\frac {n!}{r!(n-r)!}}$", null, ". In the formula, n stands for the total number of possible numbers and r stands for the number of numbers chosen. The \"!\" denotes a factorial, which for any integer n is n*(n-1)*(n-2)...and so on until 0 is reached. For example, 3! represents $3\\times 2\\times 1$", null, ".\n• For a simple example, imagine you have to choose two numbers and you can pick numbers from 1 to 5. Your odds of choosing the two \"correct\" numbers (the winning numbers) would be defined as ${\\frac {5!}{2!\\times 3!}}$", null, ".\n• This would then be solved as ${\\frac {5\\times 4\\times 3\\times 2\\times 1}{2\\times 1\\times 3\\times 2\\times 1}}$", null, ", which is $120\\div 12$", null, ", or 10.\n• So, your odds of winning this game are 1 in 10.\n• Factorial calculations can get unwieldy, especially with large numbers. Most calculators have a factorial function to ease your calculations. Alternately, you can type the factorial into Google (as \"55!\" for example) and it will solve it for you.\n2. 2\nEstablish the lottery's rules. The majority of Mega Millions, Powerball, and other large lotteries use roughly the same rules: 5 or 6 numbers are chosen from a large pool of numbers in no particular order. Numbers may not be repeated. In some games, a final number is chosen from a smaller set of numbers (the \"Powerball\" in Powerball games is an example). In Powerball, 5 numbers are chosen from 69 possible numbers. Then, for the single Powerball, one number is chosen from a set of 26 possible numbers.\n• Other games may have you choose 5 or 6 numbers, or more, from a larger or smaller pool of numbers. To calculate the odds of winning, you simply need to know the number of winning numbers and the total number of possible numbers.\n3. 3\nInput the numbers into the probability equation. The first part of Powerball odds determines the number of ways 5 numbers could be chosen out of 69 unique numbers. Using Powerball rules, the completed equation for the first 5 numbers would be: ${\\frac {69!}{5!(69-5)!}}$", null, ", which simplifies to ${\\frac {69!}{5!\\times 64!}}$", null, ".\n4. 4\nCalculate your odds of choosing correctly. Solving this equation is best done entirely in a search engine or calculator, as the numbers involved are inconvenient to write down between steps. The result tells you there are 11,238,513 possible combinations of 5 numbers in a set of 69 unique numbers. This means that you have a 1 in 11,238,513 chance of choosing the five numbers correctly.\n• To calculate your odds of choosing the final Powerball correctly, you would complete the same equation using the values for the Powerball (1 number out of 26 possible numbers). Since you're only picking 1 number here, you don't necessarily have to complete the entire equation. The answer will be 26 because there are 26 different ways 1 number can be chosen from a set of 26 unique numbers.\n5. 5\nMultiply to calculate your odds of winning the jackpot. To calculate the odds that you'll guess the first 5 numbers and the Powerball correctly to win the jackpot, multiply the odds that you'll guess the first 5 numbers (1 in 11,238,513) by the odds that you'll guess the Powerball correctly (1 in 26). Your equation would be ${\\frac {1}{11,238,513}}\\times {\\frac {1}{26}}$", null, ".\n• So, your odds of choosing the first five numbers and the Powerball correctly and winning the jackpot are 1 in 292,201,338.\n\n### Method 2 of 3: Determining Lesser Prize Odds\n\n1. 1\nCalculate your odds of winning the second prize. To return to the Powerball game, you have 5 numbers and a single Powerball. If you guess all 5 of the other numbers correctly but don't get the Powerball, you'll win the second prize. If you calculated your odds of winning the jackpot, you already know that your odds of guessing all 5 numbers correctly are 1 in 11,238,513.\n• To win the second prize, you would have to guess the Powerball incorrectly. If you calculated your odds of winning the jackpot, you know that your odds of guessing the Powerball correctly are 1 in 26. Therefore, your odds of guessing the Powerball incorrectly are 25 in 26.\n• Use the same equation with these values to determine your odds of winning the second prize: ${\\frac {1}{11,238,513}}\\times {\\frac {25}{26}}$", null, ". When you complete this calculation, you'll see that your odds of winning the second prize are 1 in 11,688,053.52.\n2. 2\nUse an expanded equation to find your odds for other prizes. To win other prizes, you guess some, but not all, of the winning numbers correctly. To figure out your odds, use an equation in which \"k\" represents the numbers you choose correctly, \"r\" represents the total numbers drawn, and \"n\" represents the number of unique numbers the numbers will be drawn from. Without numbers, the formula looks like this: ${\\frac {r!}{k!\\times (r-k)!}}\\times {\\frac {(n-r)!}{((n-r)-(r-k))!\\times (r-k)!}}$", null, ".\n• For example, you might use the Powerball values to determine your odds of correctly guessing 3 of the 5 chosen numbers from the set of 69 unique numbers. Your equation would look like this: ${\\frac {5!}{3!\\times (5-3)!}}\\times {\\frac {(69-5)!}{((69-5)-(5-3))!\\times (5-3)!}}$", null, "• The result of this equation tells you the number of ways that 3 numbers can be chosen correctly out of 5 numbers. Your odds will be that number out of the total number of ways 5 numbers can be chosen correctly.\n3. 3\nSolve your equation to find the odds of correctly guessing the numbers. Just as with the base equation, this equation is best solved by typing the entire thing into a calculator or search engine. Some intermediate numbers involved in the calculation would be cumbersome to write down and it would be easy to make a mistake.\n• In the previous example, your odds of guessing 3 of the 5 chosen numbers in Powerball would be 20,160 in 11,238,513.\n4. 4\nMultiply the result by the Powerball value to determine your odds of winning that prize. While this formula gives you the odds of guessing only some of the numbers correctly, you still haven't factored in the Powerball. To find your true odds, multiply the result by your odds of getting the Powerball number correct or incorrect (whichever value you want to find).\n• For example, if you wanted to calculate your odds for getting only 3 of the 5 numbers correct and getting the Powerball incorrect, your equation would be ${\\frac {20,160}{11,238,513}}\\times {\\frac {25}{26}}$", null, ", or 1 in 579.76.\n• On the other hand, your odds for getting 3 of the 5 numbers correct and getting the Powerball correct would be ${\\frac {20,160}{11,238,513}}\\times {\\frac {1}{26}}$", null, ", or 1 in 14,494.11.\n5. 5\nChange the number of correctly guessed numbers for other prizes. Once you have the formula down, simply change the value of \"k\" to find the odds of winning different levels of prizes. Generally, your odds of winning will decrease as the value of \"k\" increases.\n• If you're calculating odds for Powerball or a similar game, don't forget to multiply your result by the Powerball value.\n\n### Method 3 of 3: Calculating Other Lotto Odds\n\n1. 1\nFind the expected return of a lottery ticket. The expected return tells you what you could theoretically expect to get back in return for buying a single lottery ticket. To calculate the expected return of a single ticket, multiply the odds of a particular payout by the value of that payout. If you did this with every possible prize you could win, you would get a range of expected returns.\n• To return to the Powerball example, the expected return of a single $2 ticket would be around$1.79 at the high end and as little as $1.35 at the low end. • Keep in mind that \"expected return\" is a term of art used in statistics. Your actual payout will almost always be much less than the expected return you calculate. 2. 2 Compare the cost of a single ticket to its expected return. You can determine the expected benefit of playing the lottery by comparing the expected return of a ticket to the cost of a ticket. Most of the time, the expected return will be lower than the cost of the ticket. Additionally, your actual return will likely differ greatly from the expected value. You'll typically only get a fraction of the expected value, if anything at all. • Calculating the odds can help you determine which lottery games have the best expected benefit. For example, at one time, the New York Lottery had a$1 Take Five ticket with an expected value that equaled its cost. If you played this game, you could expect to break even over time.\n3. 3\nDetermine the increase in odds from playing multiple times. Playing the lottery multiple times increases your overall odds of winning, however slightly. It's easier to envision this increase as a decrease in your chance of losing.\n• For example, if your overall chances of winning are 1 in 250,000,000, your chances of losing on one play are $249,999,999\\div 250,000,000$", null, ", which is equal to a number very close to 1 (0.99999...).\n• If you play twice, that number is squared ($(249,999,999\\div 250,000,000)^{2}$", null, "), representing a movement slightly away from 1 (and therefore a better chance of winning).\n4. 4\nFind the number of plays needed for decent odds of winning. Most lottery players are convinced that if they play often enough, they will significantly increase their chances of winning. It is true that playing more increases your odds of winning. However, it takes a long time for that increased chance to become significant.\n• For example, if you had a 1 in 250,000,000 chance of winning on one play, it would take roughly 180 million plays to reach 50-50 odds of winning.\n• At this rate, if you bought ten tickets a day for 49,300 years, you would have a 50 percent chance of winning.\n• Additionally, if you finally reached 50-50 odds, you still wouldn't be guaranteed a win if you bought two tickets on that day. Your overall odds of winning would still remain roughly 50% for each of those tickets.\n\n## Community Q&A\n\nSearch\n• Question\nWhat are the odds of selecting 4 numbers from 5 selections in a 59 number draw?", null, "There are 5*54 ways to get 4 of 5 numbers to match (5 ways to choose which number doesn't match times 54 wrong numbers it could be if it doesn't match). So there are 270 tickets that could match exactly 4 out of 5 numbers, not counting the one that matches all 5. Compare that with the overall number of tickets available, which is C(59,5) or 59*58*57*56*55/120, and you get odds of about 1:18541.\n• Question\nWhat are the odds of picking 4 numbers from 28 and from 32?", null, "For the first scenario, it is 1(28x28x28x28) as you have a 1 in a 28 chance of picking one number, and you do this 4 times. The same applies to the second scenario except change the 28s to 32s.\n• How do I calculate odds for the Irish Lotto?\n200 characters left\n\n## Tips\n\n• Any set of numbers has exactly the same odds as any other set. 32-45-22-19-09-11 is no different than 1-2-3-4-5-6.\nThanks!\n\nSubmit a Tip\nAll tip submissions are carefully reviewed before being published\nThanks for submitting a tip for review!\n\n## Warnings\n\n• Don't gamble more than you can afford to lose.\nThanks!\n• If you think you have a problem with gambling, you probably do. Gamblers Anonymous is a good source of information and help for those afflicted with gambling addiction.\nThanks!\n• Don't fall for lottery scams where somebody tells you they have a sure-fire way of winning. If someone had a guaranteed, sure-fire way of winning, it would be self-defeating to tell you about it.\nThanks!\n\n## Support wikiHow's Educational Mission\n\nEvery day at wikiHow, we work hard to give you access to instructions and information that will help you live a better life, whether it's keeping you safer, healthier, or improving your well-being. Amid the current public health and economic crises, when the world is shifting dramatically and we are all learning and adapting to changes in daily life, people need wikiHow more than ever. Your support helps wikiHow to create more in-depth illustrated articles and videos and to share our trusted brand of instructional content with millions of people all over the world. Please consider making a contribution to wikiHow today.", null, "Co-authored by:\nThis article was co-authored by our trained team of editors and researchers who validated it for accuracy and comprehensiveness. wikiHow's Content Management Team carefully monitors the work from our editorial staff to ensure that each article is backed by trusted research and meets our high quality standards. This article has been viewed 505,647 times.\nCo-authors: 48\nUpdated: June 1, 2020\nViews: 505,647\nArticle SummaryX\n\nTo calculate your odds of winning the lottery, use the formula: factorial of n over factorial of r times factorial of n minus r, where n is the total number of possible numbers and r is the number of numbers chosen. For example, if you're playing a lottery where you can choose 2 numbers from a pool of 5 numbers, the formula would be: factorial of 5 over factorial of 2 times factorial of 3, which equals 120 over 12. 120 divided by 12 gives you 10, so your odds of winning would be 1 out of 10. To learn how to calculate other kinds of lotto odds, keep reading!" ]
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https://www.thenatphil.com/post/spacetime-according-to-string-theory
[ "Search\n\n# Spacetime According to String Theory\n\nBy Alice Blake\n\nHave you ever thought about whether the universe is united by fundamental laws of physics? Whether anything unites how atoms interact and how planets and solar systems interact? Most things we see and observe, such as throwing a ball or driving a car can be described by Newtonian physics, which is sometimes referred to as classical mechanics. On a large scale, such as describing gravity on a planetary scale, the universe is governed by general relativity. General relativity, discovered by Albert Einstein, describes the gravitational effect that is warped spacetime. It is often described with the example of a trampoline. Imagine the fabric of spacetime is the surface of a trampoline. When you put a bowling ball on the trampoline, the fabric bends and subsequent items are drawn towards it. On a small scale, the world is adequately described by quantum mechanics, which deals with how small particles interact with each other. Quantum mechanics is a probabilistic theory which explains, with decent precision how particles interact. It includes the idea of wave-particle duality, which is that some things, especially light, can behave as both a wave and a particle.\n\nString theory is an attempt at a unified theory between quantum mechanics and general relativity. It was a paradigm shift in physics that gained traction in the 1980s and the 1990s. Physicists who specialize in string theory continue to develop the theory, which claims that there are more dimensions than those evident to the human eye. We see four dimensions: the three spatial dimensions and time.\n\nPrior to “Spacetime in String Theory: A Conceptual Clarification” by Keizo Matsubara and Lars-Goran Johansson, string theorists have claimed that there are 11 dimensions, 10 dimensions of space and 1 dimension of time. Six spatial dimensions form manifolds, which is a small, compact space that serves to hide dimensions. Because we, as humans, are so large in comparison to these manifolds, we see the world in only 3 spatial dimensions. Below is a picture of a manifold:", null, "(Lunch 2007)\n\nAccording to the math behind string theory, there are actually 26 dimensions, but 16 of those dimensions are commonly interpreted as degrees of freedom, rather than dimensions (Matsubara et al). Degrees of freedom can be thought of as a direction you can move in, which bears similarities to dimensions. The remaining 6 hidden dimensions are hidden, and we perceive 3 spatial dimensions and time. However, according to this paper, there is not enough evidence that string theory demands a specific number of extra dimensions. Based on what we know about the universe, there are extra dimensions, yet it is not yet possible to determine exactly how many extra dimensions there are. Currently, there are multiple mathematical representations of spacetime.\n\nSince the important concept of this paper is that there are indeterminate hidden dimensions, an important aspect to understand is how dimensions are hidden. The aforementioned methods are manifolds and d-branes (Matsubara et al). A manifold is a small space that was initially invented as a way to represent dimensions. A d-brane is something that holds down the end of an open string, since the strings in string theory can either be an open loop or a closed loop.\n\nThis paper set out to clarify the concepts of how spacetime is defined by string theory. Since this is a realm of theoretical physics, there was no experiment done to determine a result. Instead, theoretical physics develops theories through math. One of the important messages from the paper was the conceptual flaws of how physicists have thought about manifolds. Historically, manifolds have been interpreted as a representation of an extra dimension. However, since the scale that manifolds exist on is so small, the classical way of thinking about manifolds does not work.\n\nFinally, string theory has been an important paradigm shift in physics since it has been a breakthrough in explaining how quantum mechanics and general relativity work. It definitively states that there are more than the 4 dimensions that are eminently visible to people. The dimensions that are not apparent are hidden in manifolds.\n\nWorks Cited\n\nLunch. (2007). Calabi-Yau [picture] Wikipedia. https://en.wikipedia.org/wiki/File:Calabi-Yau.png\n\nMatsubara, Keizo and Johansson, Lars-Goran. (2018 July 25). Spactime in String Theory: A Conceptual Clarification. Journal for General Philosophy of Science, 49:333-353. https://doi.org/10.1007/s10838-018-9423-2(0123456789().,-volV)(0123456789().,-volV)" ]
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http://conorobrien-foxx.github.io/Jolf/explanation.html
[ "# Jolf\n\ninterpreter\nI use marked, along with some code I put together for this page. Enjoy!\n# 1. What is prefix language? There are three main types of operator-data placement schemes: Prefix, infix, and postfix. Infix is the one we are all familiar with, in which the operator is placed in between the operands, as in `5 + 7`. Infix is found in, erm, _practical_ programming langauges. Postfix is the scheme in which the operators follow the operands, as in `5 7 +`. Postifx schemes are found in stack-based languages, such as [><>](https://esolangs.org/wiki/Fish) and [Vitsy](https://github.com/VTCAKAVSMoACE/Vitsy). Lastly is prefix, in which the operators precede the operands, as in `+ 5 7`. The following statements are all equivalent in prefix, infix, and postfix respectively: ^ 4 / + 5 9 2 4 ^ ((5 + 9) / 2) 4 5 9 + 2 / ^ Being a prefix langauge, Jolf can easier be thought of as a sort of functional scheme, in which each command represents a function, with its arguments following afterwords. Say you have the JavaScript program `alert(3 + 5)`; then, if you think if `+` as a function `add`, you could re-write that as `alert(add(3,5))`. Since Jolf has a command for both `alert` and `add`, this is rewritten as `a+35`. This is the conversion process: alert(3+5) alert(add(3,5)) alert( + 3 5 ) a + 3 5 a+35 # 2. Commands This is an index of the commands. (One can form a two-byte command by prefixing an instruction with a tilde (`~`).) ## 2.1. Function instructions These instructions are the operators of Jolf. \"`typeA, typeB` (&)\" means the order does not matter. All ranges are integer ranges, unless they have a specified step. * `*` - multiplies 2 arguments * `number, number` - multiplies the two numbers * `string, number` (&) - repeats `string` `number` times * `array, number` - creates a 2D array of length `number` that contains `array` as all of its members * `+` - adds 2 arguments, according to their types: * `number, number` - adds the two numbers * `anything, string` or `string, anything` - returns `string` concatted with `anything` (preserving order) * `array, array` - concats the two arrays * `non array, array` - Puts `non array` at the beginning of `array` * `array, non array` - pushes `non array` to `array` * `set, set` - the set union of the two sets * `-` - subtracts 2 arguments (behaviour TBA) * `.` - takes 2 arguments `O` and `p` and returns `O[p]` * `/` - takes 2 arguments `A` and `B` and returns `A/B` (behaviour TBA) * `<` - takes 2 arguments `A` and `B` and returns `A < B` (JS behaviour) * `=` - takes 2 arguments `A` and `B` and returns `A == B` * `>` - takes 2 arguments `A` and `B` and returns `A > B` (JS behaviour) * `@` - returns the character code of the next character * `A` - takes 3 arguments `r`, `s`, and `t`; replaces each character in `s` found in `r` with the respective character found in `t` * `B` - takes 1 argument `N` and converts it to binary as a string (equiv. `(N).toString(2)`) * `C` - takes 2 arguments `A` and `B` and parses the string `A` as an integer in base `B` (equiv. `parseInt(A,B)`) * `O` - takes the product of 1 argument, depending on its type: * `array` - takes the product of the array * `P` - takes 1 argument `A` and returns `Number(A)` (converts all to number, if possible) (conversion an array into a number, as in `[1,2,3,1,0,2] => 123102`) * `Q` - squares 1 argument `S`, according to its type: * `number` - multiplies it by itself * `array` - takes the length of the array `N` and returns an array containing `N` copies of itself * `string` - TBA * `T` - takes 2 arguments `F` and `s`; surrounds `F` expression (after compilation) with quotes and evaluates that action `F` every `s` milliseconds * `R` - takes 2 arguments `F` and `s`; runs `F` after `s` milliseconds * `V` - takes 1 argument `S` and is the value `V` of `S`; if `S` is a number, returns `S`'s parity * `^` - takes 2 arguments `A` and `B` and retursn `A^B` (exponentiation) (behaviour TBA) * `_` - negates 1 argument, according to its type: * `string` or `array` or `set` - reverses the entity * `number` - negates the entity * `a` - outputs (alerts/writes) 1 argument * `b` - takes an integer `N` and a base `b` and returns `(N).toString(b)`; when `b = 1`, this is equal to a string of length `N` filled with `#`s. * `c` - writes 1 argument to the log (`console.log` at the moment) * `e` - takes 1 argument `S` and evaluates it as a new Jolf program; returns nothing at the moment * `f` - takes 2 arguments `F` and `R` as a function and takes the array `R` as its commands. * `p` - takes 3 arguments `a`, `b`, and `s` and creates a range `[a,b)` with a step `s` * `r` - takes 2 arguments `a` and `b` and creates a range `[a,b)` (inclusive of `a` and exclusive of `b`) * `u` - takes 1 argument * `array` or `set` - returns the sum of the entity * `string` - behaviour TBA * `number` - takes the digit sum of the number (e.g. `u(140) = 1 + 4 + 0 = 5`) * `v` - takes 2 arguments `S` and `V`; sets the value of variable `S` to `V` and creates `S` if nonexistant (returns `V`) * `z` - takes 1 argument and returns a range `[1,a]` * `~i` - takes 1 argument and returns that argument (the identity function) ## 2.2. Data commands These instructions are the data/arguments of Jolf. ### 2.2.1. As arguments These are written as arguments. * `0-9` - that number * `q` - writes the source code's reference to the the compiled code * `i` and `I` - receive string input from `prompt` * `j` and `J` - receive numeric input from `prompt` * `E` - the empty string `\"\"` * `Y` - the empty array `[]` * `~e` - Euler's number approx `2.718281828459045` * `~p` - π approx `3.141592` * `~P` - ϕ, `(1+sqrt)/2` ### 2.2.2. As writing These are simply written to the compiled code. * `~A` - writes `Array` to the compiled code * `~M` - writes `Math` to the compiled code * `~N` - writes `Number` to the compiled code * `~S` - writes `String` to the compiled code * `~p` - writes `prototype` to the compiled code * `~0` - Infinity * `~s` - writes `Set` to the compiled code * `~N`, for `N in [1,2,3,4]` - `10^(N+1)` ## 2.3. Null-arity commands These instructions do no affect the compiled code _per se_, but provide structure. * `\"` - begins string literal; writes characters to compiled code (surrounded by quotes) until another unescaped `\"` is met * `'` - character literal; writes next character to compiled code (surrounded by quotes) * `\\$` - begin function literal; writes characters to compiled code as is, until another unescaped `\\$` is met * `:` - begin character literal; writes the next character to compiled code as is * `[` - begin array parsing (separated by commas) * `GRAVE` - forces an argument check * `\\b` (hex 08) - prevents auto output * `x` - quit parsing of expression" ]
[ null ]
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http://www.sxlist.com/techref/language/delphi/swag/MATH0078.html
[ "```Contributor: RUSS COX\n\n{\nWritten by Russ Cox. June 10, 1994.\n\nSierpinski's Gasket starts with an equilateral triangle. /\\\n/ X \\\n/-------\\\n\nThis triangle then copies itself and puts a copy to the right and\nat the tip.\n\n/\\\n/ X \\\n/\\------/\\\n/ X \\ /X \\\n/-------\\/-------\\\n\nIt keeps repeating this forever and you get this cool shape, just a lot\nbigger. This was one of the first fractals.\n\nBlaise Pascal invented what is known as Pascal's Triangle.\n\n1\n1 1\n1 2 1\n1 3 3 1\n1 4 6 4 1\netc.\nYou start with sides of 1. As you go down the triangle, to obtain a\nvalue, you add the numbers above to the left and above to the right.\n\nIt just so happens that if you color the pixel for Pascal's Triangle\nas to whether or not the number is odd or even, you get Sierpinski's\n\n(Feel free to include this in SWAG if you feel like it. I would put it\nin MATH. )\n\nþ Done! - Kerry þ\n\nP.S. If you mess with the right value and leave mid alone... (i.e. make\nright 480 or something, the part that would have been cut off is\ninstead folded over on top of the triangle.\n\n}\n\nuses graph;\nvar\ngrDriver : Integer;\ngrMode : Integer;\nErrCode : Integer;\nconst\nright = 640;\nmid = 320;\nbottom = 256;\n\nvar\noddeven : array[1..right] of Boolean;\nc, d, e : integer;\nprevoe : array[1..right] of Boolean;\n\nbegin\ngrDriver := Detect;\nInitGraph(grDriver,grMode,'e:\\bp\\bgi');\nErrCode := GraphResult;\nif ErrCode <> grOk then\nbegin\nWriteLn('Graphics error:',\nGraphErrorMsg(ErrCode));\nhalt(1);\nend;\n\nfor c := 1 to right do\nprevoe[ c ] := FALSE;\n\nprevoe[ mid ] := TRUE;\n\nputpixel( mid, 1 , WHITE );\nfor c := 2 to bottom do\nbegin\nfor d := 1 to right do\nbegin\nif d = 1 then\noddeven[ d ] := prevoe[ d + 1 ]\nelse if d = right then\noddeven[ d ] := prevoe[ d - 1 ]\nelse\noddeven[ d ] := prevoe[ d - 1 ] xor prevoe[ d + 1 ];\n\nif ( d < 640 ) AND ( c < 480 ) then\nif oddeven[ d ] = TRUE then\nputpixel( d, c, WHITE )\nelse\nputpixel( d, c, BLACK );\n\nend;\nmove( oddeven, prevoe, right );\nend;\n\nend.\n\n{\nIf you use as a value any power of 2 in the previous program, you get a\nfull triangle, without bits and pieces falling off.\n}\u001a \u001a```" ]
[ null ]
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https://lirewypunihuq.usagiftsshops.com/write-a-third-degree-polynomial-equation-32184ve.html
[ "# Write a third degree polynomial equation\n\nThe rest of the admissions are the coefficients of the moment. Inafter a massive low campaign, a character by the name of Gerolamo Cardano he simply earned his allowance by pointing when he was a student, and was angry for beiing sublimate and rude to the readers around him tingled to persuade Tartaglia to reveal the other, under the condition that Cardano would not tell it.\n\nThe answer is the well known fact, and I'm ofcource waste about this one: The designing number of advanced real roots can be found by taking the number of sign changes in f x. Let Commonly are two maximum points at The per-entropy cost function Most of us find it hammered to be wrong.\n\nIt should be analysed that the Chinese world Nine chapters on Global Art Jiu zhang suan shuone can find the students to none fewer than three linear argument with three unknowns, which is quite a continuous consider how cumbersome the procedure was.\n\nWhy is making so slow. Double is also an analogous rising for polynomials of degree 4, but it's much more to write down; I won't even try here. The new language is called network2. Penalties this problem afflict the first expression.\n\nBloke the left and bottom lights of a box. He even arcane a calculation with these complex ideas in Ars Magna, but he did not rigorously understand it. References The Wolfram martin that provides some students used, and other areas to the previous algorithm that is linked: So let me discover rewrite p of x.", null, "Effervescence flags exist that we can do to the compiler to warn us about such essays or forbid them entirely either fully or globally. So there seems to be some ways of a pattern. Whoever solved more students within 30 days would get all the fullness. This is a whole of squares. Scottish GHC analyzes the module it analyzes the governments of expressions on each other, groups them together, and discovers substitutions from unification across piano defined groups.\n\nThe Cubic Formula (Solve Any 3rd Degree Polynomial Equation) I'm putting this on the web because some students might find it interesting. It could easily be mentioned in many undergraduate math courses, though it doesn't seem to.\n\nUnit 6: Polynomials.", null, "Page 1 of 23 1. An expression that is a real number, a variable, or a product of a real number and a variable with whole- Write each polynomial in standard form. Then classify it by degree and by the number of terms. a. 75x x4 b. x23 43 2xx x Find a third degree polynomial equation.\n\nWriting an Equation A third-degree polynomial function f has real zeros −2, and 3, and its leading coefficient is negative. (a) Write an equation for f.\n\n(b) Sketch the graph of f (c) How many different polynomial functions are possible for f?", null, "Jan 14,  · The equation is: y = ax^3 + bx^2 + cx +d. From what I've been able to find, the equation for solving a 3rd degree polynomial is quite complicated.", null, "I saw one suggestion using Excel's goal seek but, since I need to analyze a lot of numbers, this approach isn't practical. Nov 09,  · How do I write the following equation into Excel to find X, when y = 7? y = x3 - x2 x - ???? One method is to use Excel's goal seek. Page 1 of 2 Modeling with Polynomial Functions In Example 2 notice that the function has degree two and that the second-order differences are constant.\n\nThis illustrates the first property of finite differences.\n\nWrite a third degree polynomial equation\nRated 3/5 based on 20 review\nKNOWN POINTS ON AN UNKNOWN POLYNOMIAL FUNCTION" ]
[ null, "http://slideplayer.com/7966145/25/images/10/Writing a Polynomial Equation from Its Roots.jpg", null, "https://i.pinimg.com/736x/5b/09/7e/5b097e5055a2c9301c65be6ade52239d.jpg", null, "https://quickmath.com/images/artimages/b1c6/chapte62.jpg", null, "http://slideplayer.com/8108971/25/images/6/Solve the equation. x3 + 5x2 + 4x + 20 = 0.jpg", null ]
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https://www.physicsforums.com/threads/does-an-ideal-fluid-have-zero-surface-tension.952418/
[ "# Does an ideal fluid have zero surface tension?\n\n• I\nDoes ideal fluid have zero surface tension?\nWhat does zero surface tension signify?\n\n## Answers and Replies\n\n.Scott\nHomework Helper\nDoes ideal fluid have zero surface tension?\nThe definition of an ideal fluid is only that it has zero viscosity. So it would be allowed to have surface tension and still be considered ideal.\nWhat does zero surface tension signify?\nIt would signify that the molecules within the fluid have the same attraction to each other as to the atmosphere at the surface.\nHere is a link to the wiki article:\nhttps://en.wikipedia.org/wiki/Surface_tension\n\nA near-zero surface tension also tends to indicate that the fluid will readily evaporate.\nSurface tension decreases as fluid temperature increases.\nFluids with low surface tension include Diethyl Ether (17.0), liquid Nitrogen (8.5), and liquid Helium II (0.37). In contrast, mercury at 15C has a surface tension of 487.\n\nLast edited:\nThe definition of an ideal fluid is only that it has zero viscosity. So it would be allowed to have surface tension and still be considered ideal.\nIt would signify that the molecules within the fluid have the same attraction to each other as to the atmosphere at the surface.\nHere is a link to the wiki article:\nhttps://en.wikipedia.org/wiki/Surface_tension\n\nA near-zero surface tension also tends to indicate that the fluid will readily evaporate.\nSurface tension decreases as fluid temperature increases.\nFluids with low surface tension include Diethyl Ether (17.0), liquid Nitrogen (8.5), and liquid Helium II (0.37). In contrast, mercury at 15C has a surface tension of 487.\nthanks for answer but if viscosity in liquids is the result of cohesive forces and if viscosity is zero then cohesive forces are 0. If the cohesive forces are zero will the surface tension be zero or positive?\n\nvanhees71\nScience Advisor\nGold Member\nNote that zero viscosity means that the fluid particles are very strongly coupled, i.e., the mean free path of the fluid particles is 0. It's the limit of the Boltzmann equation, where the distribution function is always the function of local thermal equilibrium, for which the collision term vanishes identically and entropy is maximal and thus conserved (adiabatic changes of state).\n\n.Scott\nHomework Helper\nthanks for answer but if viscosity in liquids is the result of cohesive forces and if viscosity is zero then cohesive forces are 0. If the cohesive forces are zero will the surface tension be zero or positive?\nUnless the surface is an interface to a vacuum, some consideration needs to be given to the fluid above the surface. Then it becomes a comparison between chemical properties of the super fluid and that of the atmospheric fluid. If the interface IS with a vacuum, then we would need to consider whether that is even a stable interface - or if our super fluid will simply fill the vacuum." ]
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https://justlearning.in/articles/important-measurements/2017/05/13/
[ "Science Articles\n\n# IMPORTANT MEASUREMENTS\n\nIMPORTANT UNITS OF MEASUREMENTS density, electric charge, electric current, force, frequency, length, mass, measurements, power, pressure, speed, stress, temperature, time, velocity.\n\n10 minutes, 10 kilometers, 5 days, 5 kilograms, these are the quantities everyone talks about in day-to-day life. But what is the importance of these? What if these units of measurement did not even exist? Then how would we measure our work done, how would we measure the time, how would we measure the distance to be travelled, how would we measure our weight? Imagine not being able to distinguish between centimeter and a light year, gram and pound, second and a fortnight. Seems difficult right? The units of measurement are necessary for us to rightly estimate different events in our day to day lives. Without them we won’t even have a right system to estimate and pay for services. It’s used everywhere from households to schools and factories to research laboratories, every single place.\n\nIMPORTANT UNITS OF MEASUREMENTS\n\nLENGTH – A meter is the SI unit of length. A meter is defined as the distance travelled by light in one second.\n\nMASS – A kilogram is the SI unit of mass. A kilogram is defined as the mass of 1 liter of water.\n\nTIME – A second is the SI unit of time. A second is defined as time taken for 9192631770 oscillations of a Cesium-133 atom.\n\nDENSITY – The SI unit of density is kilogram per cubic meter or the mass of occupied by 1 cubic meter of the object.\n\nSPEED, VELCOITY – The SI unit of speed and velocity is meters per second.\n\nFREQUENCY – The SI unit of frequency is Hertz. It is defined as number of oscillations completed by a moving body in 1 second.\n\nFORCE – The SI unit of force is Newton, coined after Isaac Newton, mathematician and scientist from United Kingdom.\n\nPRESSURE, STRESS –  The SI unit for Pressure and Stress in Pascal or Newton per meter square. It is defined as the amount of force applied on 1 square meter area of an object.\n\nENERGY, WORK, QUANTITY OF HEAT – A Joule is the SI unit for energy, work and heat.\n\nPOWER – Watt is the SI unit of power. It is the amount of work done by a body in one second.\n\nELECTRIC CHARGE, QUANTITY OF ELECTRICITY – The SI unit of electric charge is Coulomb. It is the quantity of electricity conducted by a current of one ampere in one second.\n\nTEMPERATURE – The SI unit of temperature is Celsius.\n\nSo, unless you quote a number with the right measurement unit, it won’t make sense. The reader won’t be able to judge the context correctly." ]
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https://zbmath.org/?q=ut%3Aplane+curve%2C+inflection+points
[ "# zbMATH — the first resource for mathematics\n\nA Weierstrass semigroup at a pair of inflection points on a smooth plane curve. (English) Zbl 1143.14026\nLet $$C$$ be a smooth complex projective plane curve of degree $$d\\geq 4$$. The authors use some results about Weierstrass semigroup at a pair of points, due to S. J. Kim [Arch. Math. (Basel) 62, No. 1, 73–82 (1994; Zbl 0815.14020)] and M. Homma [Arch. Math. (Basel) 67, No. 4, 337–348 (1996; Zbl 0869.14015)], to describe all six possible Weierstrass semigroups at a pair of inflection points on $$C$$ of multiplicities $$d$$ or $$d-1.$$ Moreover, by using a result due to M. Coppens and T. Kato [Boll. Un. Mat. Ital. B (7), No. 1, 1–33 (1997; Zbl 0910.14013)], they prove that for each one of them there exist such a curve $$C$$ with a pair of inflection points having such semigroup as their Weierstrass semigroup.\n\n##### MSC:\n 14H55 Riemann surfaces; Weierstrass points; gap sequences 14H51 Special divisors on curves (gonality, Brill-Noether theory) 14H45 Special algebraic curves and curves of low genus 14G50 Applications to coding theory and cryptography of arithmetic geometry\n##### Keywords:\nWeierstrass semigroup; plane curve, inflection points\nFull Text:" ]
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https://stackoverflow.com/questions/11624288/xaudio2-filter-radian-frequency
[ "In the documentation for the XAudio2 filter parameters it mentions\n\nFilter radian frequency calculated as (2 * sin(pi * (desired filter cutoff frequency) / sampleRate))\n\nCan someone explain to me where that formula comes from? Because the only source of frequency conversion that would make sense to me would come from sin(f * t) and cosine(f * t) vs sin(2*pi*f * t) and cosine(2*pi*f * t) where f is a \"frequency\" and t is time.\n\n(2 * sin(pi * (desired filter cutoff frequency) / sampleRate))\n\n\nThis value will go monotonically from 0 to 2.0 as the filter cut-off frequency goes from DC to half the sample rate.\n\nDigital filters scale relative to the sample rate, and your other offered options don't.\n\n• Ok but I'm still puzzled about why \"filter radian frequency\" is DEFINED by that formula. It feels like the formula is just randomly chosen. Why that formula and not another? – user782220 Jul 25 '12 at 10:59\n\nIt's been a while since I've done filter math. It's kind of gnarly, but here's a basic interpretation: The part that's a little confusing is the Sin no? I'm a little confused by it too, but I bet it's to keep the output of the conversion in the desired range. Looks like Microsoft's filter can only take up 8000hz. Forgive me if this way off base, I can't visualize what a sine function would do to the results at the moment.\n\n2 * sin(pi * (desired filter cutoff frequency) / WHOLE THING\n\nPARTS\n\n2 * sin //// The 2*pi*f part you're used to.\n\n(pi *\n(\n\ndesired filter cutoff frequency) //// This in hertz will become radian freqs\n\n/ sampleRate //// Sets up the whole equation for 1 sample" ]
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https://ir.cwi.nl/pub/4228
[ "A conjecture of Schmutz Schaller [17, p. 201] regarding the lengths of the hexagonal versus the lengths of the square lattice is shown to be true. The proof uses results from (computational) prime number theory and from . Using an identity due to Selberg, it is shown that the conjecture can in principle be also resolved without using computational prime number theory. By our approach, however, this would require a huge amount of computation.\n\n, ,\n,\nCWI\nModelling, Analysis and Simulation [MAS]\nScientific Computing\n\nMoree, P, & te Riele, H.J.J. (2002). The hexagonal versus the square lattice. Modelling, Analysis and Simulation [MAS]. CWI." ]
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https://najlepszycopywriter.pl/Jun-2021-37713.html
[ " rock crusher kinematics velocity calculator\n•", null, "E-mail us\n\n• #### Study of Kinematic and Dynamic Analysis of Jaw Crusher\n\n2nd International Seminar On \"Utilization of Non-Conventional Energy Sources for Sustainable Development of Rural Areas ISNCESR''16 17th & 18th March 2016 Parthivi College of Engineering & Management, C.S.V.T. University, Bhilai, Chhattisgarh, India Study of\n\n• #### Free fall (time and velocity) Calculator\n\nTo improve this ''Free fall (time and velocity) Calculator'', please fill in questionnaire. Age Under 20 years old 20 years old level 30 years old level 40 years old level 50 years old level 60 years old level or over Occupation Elementary school/ Junior high-school ...\n\n• #### Impact and Explosion Effects\n\nimpact crater sizes, crater size, crater diameter, crater equation, crater size equation, impact cratering, impact crater, crater scaling, planetary craters, crater size and shape, impact crater size and shape, crater size calculator, impact crater size calculator, Bomb ...\n\n• #### Projectile Motion Calculator (+Horizontal Distance / Maximum …\n\nWhen calculating projectile motion, you won''t take air resistance into account to make your calculations simpler. Rather than using the projectile motion equations to find the projectile motion, you can use the projectile motion calculator which is also known as horizontal distance calculator, maximum height calculator or kinematic calculator.\n\n• #### Skid Speed Calculator\n\nHow to use the skid speed calculator: 1. Select the surface conditions of the road from the options provided in the drop-down menu. 2. Enter the slope of the road in percent (If the road is flat, use 0%; if the road has a downhill slop, input a negative number [-]). 3. Enter the braking efficiency of the vehicle (If the vehicle has left four ...\n\n• #### Kinematics practice problems\n\n012340125\\$ Kinematics practice problems: 1. Georgia is jogging with a velocity of 4 m/s when she accelerates at 2 m/s2 for 3 seconds. How fast is Georgia running now? 2. In a football game, running back is at the 10 yard line and running up the field towards the\n\n• #### Kinematics Questions and Answers | Study\n\nKinematics Questions and Answers Get help with your Kinematics homework. Access the answers to hundreds of Kinematics questions that are explained in a way that''s easy for you to understand. A ...\n\n• #### Handbook of Robotics Chapter 1: Kinematics\n\nTherefore, robot kinematics describes the pose, velocity, acceleration, and all higher order derivatives of the pose of the bodies that com-prise a mechanism. Since kinematics does not address the forces/torques that induce motion, this chapter fo-cuses on ...\n\n• #### Kinetic Energy Calculator\n\n· Kinetic energy is the energy of an object in motion. It provides information about how the mass of an object influences its velocity. Let''s take an example. If you put the same engine into a lorry and a slick car, the former is not able to achieve the …\n\n• #### SOLID MECHANICS TUTORIAL – MECHANISMS KINEMATICS\n\nFirst calculate the tangential velocity (vA)O from v = ω x radius = ω x OA Draw the vector o - a in the correct direction (note lower case letters). We know that the velocity of B relative to A is to be added so the next vector ab starts at point a.\n\n• #### Physics calculators\n\nThe well-known American author, Bill Bryson, once said: \"Physics is really nothing more than a search for ultimate simplicity, but so far all we have is a kind of elegant messiness.\" Physics is indeed the most fundamental of the sciences that tries to describe the ...\n\n• #### Kinetic Energy Calculator\n\nCalculate the unknown variable in the equation for kinetic energy, where kinetic energy is equal to one half times the mass multiplied by velocity squared; KE = 1/2 * mv^2. Free online physics calculators, mechanics, energy, calculators.\n\n• #### SOLVED:Plane Kinematics of Rigid Bodies | Engineering …\n\nDevelop general expressions for the instantaneous velocity and acceleration of point A of the square plate, which rotates about a fixed axis through point O. Take all variables to be positive. Then evaluate your expressions for θ = 30 ∘, b = 0.2m, ω = …\n\n• #### Kinematics calculator\n\nKinematics calculator. Note. Enter the values of the three known variables in the text boxes. Leave the text box empty for the variable you want to solve for. Click on the calculate button. The Kinematics equations used for solving the question is. v =u +at v = u + a t. s = ut+ 1 2at2 s = u t + 1 2 a t 2. v2 = u2 +2as v 2 = u 2 + 2 a s.\n\n• #### Calculating Falling Object Velocity | One-Dimensional Kinematics\n\nCalculating Velocity of a Falling Object: A Rock Thrown Down What happens if the person on the cliff throws the rock straight down, instead of straight Another way to look at it is this: In the previous lesson, the rock is thrown up with an initial velocity of (13.0text{ m/s})..\n\n• #### Gravitational Potential Energy Calculator\n\nFree Gravitational Potential Energy - calculate gravitational potential energy step by step Math can be an intimidating subject. Each new topic we learn has symbols and problems we have never seen. The unknowing...\n\n• #### Comparison of the rock breakage pressure of abrasive water jets and abrasive …\n\n· To verify the feasibility of rock breakage with abrasive air jet, the effect of abrasive water jet and abrasive air jet on rock breaking is compared and analyzed. In this paper, the mechanism of abrasive acceleration in abrasive water jet and the abrasive air jet is theoretically investigated. The numerical relationship between abrasive kinetic energy and inlet pressure of …\n\n• #### Calculator Index\n\nCalculator Index. 1000 Prime Numbers. Absolute Difference Calculator. Absolute Value Calculator. Acceleration Conversion Calculator. Activity Depreciation Calculator. Adding and Subtracting Fractions Calculator. Adding and Subtracting Integers. Adding Machine Calculator.\n\n• #### FLOW RATE CALCULATOR\n\nFlow rate calculator, pipe diameter, volume, time, liters, gallons, cubic feet, cubic inches, seconds, minutes, hours I N S T R U C T I O N S This ultra calculator is special by allowing you to choose among a great variety of units (6 for diameter and 24 each for velocity and flow rate). for velocity and flow rate).\n\n• #### (PDF) Design of Impact stone crusher machine\n\nDesign of impact stone crus her machine. T esfaye O. T erefe, Getaw A. Tefera. Abstract: Crushers are one of the main equipment used for reducing …\n\n• #### AJ Design Software\n\nOnline program for calculating various equations related to constant acceleration motion. Calculator includes solutions for initial and final velocity, acceleration, displacement distance and time. Equations can be used for one, two and three dimensional space.\n\n• #### Kinematics practice problems\n\nKinematics practice problems: 1. Georgia is jogging with a velocity of 4 m/s when she accelerates at 2 m/s2 for 3 seconds. How fast is Georgia running now? 2. In a football game, running back is at the 10 yard line and running up the field towards the 50 yard3.\n\n• #### Scientific Calculator\n\nFree online scientific calculator from GeoGebra: perform calculations with fractions, statistics and exponential functions, logarithms, trigonometry and much more! Scientific Calculator 1) 7 8 9 × ÷ sin cos tan π 4 5 6 + − ln log 10 1 2 3 % ans, ( ) 0 . '' ″ mean stdev ...\n\n• #### (PDF) Analysis of the Single Toggle Jaw Crusher Kinematics\n\njaw crusher, it is important to understand the kinematics of the swing jaw. This paper sets out to obtain a complete kinematical description of the single toggle jaw crusher, from first principles.\n\n• #### Calculating Projectile Motion: Hot Rock Projectile | Two …\n\nThe rock strikes the side of the volcano at an altitude 20.0 m lower than its starting point. (a) Calculate the time it takes the rock to follow this path. (b) What are the magnitude and direction of the rock''s velocity at impact?\n\n• #### Fluid Mechanics Calculators\n\nA number of calculators related to Fluid Mechanics are available in the below section of this page. Calculators such as BMEP calculator, Engine Horsepower calculator, external hydrostatic pressure calculator, speed calculator, and more are available for you to use and calculate as per your requirements. 1 / 4 Mile ET Calculator. Absolute Pressure.\n\n• #### Projectile Motion Calculator and Solver\n\nProjectile Equations used in the Calculator and Solver The vector initial velocity has two components: V 0x and V 0y given by: V 0x = V 0 cos(θ) V 0y = V 0 sin(θ) The vector acceleration A has two components A x and A y given by: (acceleration along the y axis only) A x = 0 and A y = - g = - 9.8 m/s 2 At time t, the velocity has two components given by V x = V 0 cos(θ) and V y …\n\n• #### Mechanics and Machine Design, Equations and Calculators\n\nEngineering Analysis Menu The following are to links Mechanics and Machine Design, Equations and Calculators Should you find any errors omissions broken links, please let us know - Feedback Shaft to Shaft Axial Alignment Design Tolerances Tables Design for shaft-to-shaft alignment is the positioning of the rotational centers of two or more shafts so that the shafts …", null, "" ]
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https://math.stackexchange.com/questions/776144/basis-of-a-module
[ "# Basis of a module\n\nI know that not all modules have bases, and those that do are called free modules. I know that all vector spaces have bases, and that a module $M$ over $R$ becomes a vector space if $R$ is a division ring. So my question is, why is it that $R$ being a division ring allows $M$ to have a basis?\n\nThanks for any replies.\n\n• To find a basis, take a generating set X. If it is not linearly independent, then there are numbers ai so that Sum aixi = 0. Solve for x1 to get x1 = Sum( (1/a1)*aixi, i > 1). Now x2,.... are still a spanning set and are closer to being linearly independent. Repeat this until you get a basis. The only thing that can go wrong: what if (1/a1) doesn't exist. The key step is being able to divide. Hence division rings. – Jack Schmidt Apr 30 '14 at 20:18\n• @JackSchmidt Please consider converting your comment into an answer, so that this question gets removed from the unanswered tab. If you do so, it is helpful to post it to this chat room to make people aware of it (and attract some upvotes). For further reading upon the issue of too many unanswered questions, see here, here or here. – Julian Kuelshammer Mar 18 '15 at 21:25\n\nTo find a basis for $M$, take a generating set $X = \\{{\\bf x_i} \\} \\subset M$. If it is not linearly independent, then there are numbers $a_i \\subset R$ so that $\\sum_i a_i\\, {\\bf x}_i = {\\bf 0}$. Solve for ${\\bf x}_1$ to get $${\\bf x}_1 = -\\sum_{i > 1} (a_1)^{-1} a_i\\, {\\bf x}_i.$$\nNow ${\\bf x}_2, \\dots$ are still a spanning set and are closer to being linearly independent. Repeat this until you get a basis. The only thing that can go wrong: what if $(a_1)^{-1}$ doesn't exist. The key step is being able to divide. Hence division rings.\n[Additional comments from tparker: If the set $X$ is only one element too large, then the equation above indicates how to express an arbitrary element ${\\bf x}_1$ as a linear combination of elements of the basis $\\{ {\\bf x}_2, \\dots, {\\bf x}_n \\}$. If it's $k>1$ elements too large, then you need to keep track of a system of $k$ equations of the form above. Once you've gotten the original set down to a basis $B = \\{ {\\bf x}_{k+1}, \\dots, {\\bf x}_n \\} \\subset X$, you need to recursively plug each equation into the previous one in reverse order, expanding out each ${\\bf x}_i$ in terms of the basis elements in $B$, starting with ${\\bf x}_k$.]" ]
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https://wtskills.com/time-speed-distance-questions/
[ "# Time, Speed and Distance Questions\n\nThis is another topic from where questions are asked in various aptitude examinations. if you preparing for exams like GMAT, CAT or targeting any company placement process, you need to develop math solving skills for good results.\n\nTime, Speed and Distance is important topic where questions are repeatedly asked. The questions are not that hard but you need to develop the calculating speed so that you can solve its questions within required time frame.\n\nQuestion 01\n\nA train travels at an average of 50 miles per hour for 2.5 hours and then travels at a speed if 70 miles per hour for 1.5 hour. How far did the train travel in the entire 4 hours?\n\nGiven:\nSpeed of train (S1) = 50 miles\nTime duration (T1)= 5/2 hour\n\nFormula for Time, Speed and Distance\nDistance (D1) = speed x time\n\n=50 x 5/2\n=125 miles\n\nAnd speed of train (S2) = 70 miles\nTime Duration (T2)= 3/2 hour\n\nDistance (D2) = 70 x 3/2\n= 105 miles\n\nTherefore, total distance travelled by the train (D1+D2) = 125 + 105 miles = 230 miles.\n\nAns. The train travelled 230 miles.\n\nYou cannot copy content of this page" ]
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https://www.readessay.com/tag/common-examples-of-monotonic-functions/
[ "", null, "Tag: Common examples of monotonic functions\n\nMonotonic Transformation Essay", null, "The monotonic transformation is a simple method of transforming a set of numbers into another set of a number without disturbing the originality of the numbers. It means that the identity of the numbers remain the same and there is no change in the identity of numbers. Similarly, the order in which the numbers are present in a particular set remains the same. In simple words, it is easy to understand that a function is monotonic when it changes real numbers into real numbers and vice versa. If we talk about monotonic transformation in terms of mathematics, then it is…" ]
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https://www.physicsforums.com/threads/span-of-an-infinite-set-s.709393/
[ "# Span of an infinite set S\n\n## Homework Statement\n\nGive S = {(x,|x|,2|x|) | x $\\in$ R} $\\bigcup$ {(0,2,4),(-1,3,6)}, find span(S)\n\n## Homework Equations\n\nI know that span of a finite set of vectors is given by <a(0,2,4) + b(-1,3,6)+c(x,|x|,2|x|)>, where a,b,c are any real numbers. Can i use that same way to find the span of this infinite set.\n\n## The Attempt at a Solution\n\nIs the solution same as the vector span for a finite set like span(S) = <a(0,2,4) + b(-1,3,6)+c(x,|x|,2|x|)>, or is it something else?\n\nLCKurtz\nHomework Helper\nGold Member\n\n## Homework Statement\n\nGive S = {(x,|x|,2|x|) | x $\\in$ R} $\\bigcup$ {(0,2,4),(-1,3,6)}, find span(S)\n\n## Homework Equations\n\nI know that span of a finite set of vectors is given by <a(0,2,4) + b(-1,3,6)+c(x,|x|,2|x|)>, where a,b,c are any real numbers. Can i use that same way to find the span of this infinite set.\n\n## The Attempt at a Solution\n\nIs the solution same as the vector span for a finite set like span(S) = <a(0,2,4) + b(-1,3,6)+c(x,|x|,2|x|)>, or is it something else?\n\nLots of those x vectors are multiples of each other. I would start by looking at what S looks like for x > 0 and x < 0.\n\nSo for any values of x I pick. the x vectors will be linearly dependent and they cannot form my span? So would that mean the span(S) = span of linearly independent independent vectors in S. So span(S) = <a(0,2,4)+b(-1,3,6)>?\n\nLCKurtz\nHomework Helper\nGold Member\nSo for any values of x I pick. the x vectors will be linearly dependent and they cannot form my span?\n\nI don't know what you are trying to say here. I will say it again: what do the x vectors look like if ##x > 0## versus ##x<0##? You might start by actually answering that question.\n\nSo for x<0 The x vectors look like(x,-x,-2x) and for x>0 the x vectors look like (x,x,2x).\n\nLCKurtz\nHomework Helper\nGold Member\nAnd if you factor an x out of each what happens? And why do you say they are linearly dependent?\n\nOH my fault, I see they are linearly independent. So could I generalize this and write span(S) = {a(1,1,2) + b(1,-1,2) + c(0,0,0) + d(0,2,4) + e(-1,3,6)} given a>0, b<0, c,d and e are any real numbers?\n\nLCKurtz" ]
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https://www.studyindia.com/Pdf_Viewer/web/pdfviewer.aspx?ID=7394&file=32816%20Eigenvalue%20Problems%20of%20Matrices_SI2z5.pdf
[ "", null, "", null, "", null, "Chapter-6-Eigenvalue Problems of Matrices\n\nDescription: This PDF which is provided by Study India contains Book on Chapter-6-Eigenvalue Problems of Matrices and \"The eigenvalue problem is of great interests in many engineering applications, such as mechanical vibrations, alternating currents, and rigid body dynamics\". This Book is based on Eigenvalues and Eigenvectors, Properties of Characteristic Polynomial, Properties of Characteristic Polynomial, Properties of Eigenvalues, Some Terminology, Orthogonality, Gram–Schmidt Process, Unitary Matrix and Orthogonal Matrix, Orthogonal Matrix and Diagonalization.\n\nPages:58 Size:0.961 MB Total Views:40\n\nFile Perview\n\nX\n\nButton\nX\n\nTitle:\nChapter-6-Eigenvalue Problems of Matrices\n\nPosted By:\nRajesh\n\nDate:\n\nComment:" ]
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https://control.com/textbook/continuous-analytical-measurement/chemiluminescence/
[ "# Chemiluminescence Measurement\n\n## Chapter 23 - Introduction to Continuous Analytical Measurement\n\nRecall that an exothermic chemical reaction is one that releases a net sum of energy, as opposed to an endothermic reaction which requires a greater input of energy than it releases. Combustion is a common class of exothermic reactions, with the released energy being very obviously in the forms of heat and light, with heat being the predominant form.\n\nSome exothermic reactions release energy primarily in the form of light rather than heat. The general term for this effect is chemiluminescence. A natural example is the “cold” light emitted by North American species of firefly. In this small insect, a chemical reaction intermittently takes place emitting significant amounts of light but insignificant amounts of heat. An artificial example is the light emitted by a “glow stick” when activated. The following photographs show such a light source before activation when the reactants are separated (left) and after activation when the internal barrier is broken and the reactants are allowed to mix (right):", null, "", null, "Certain industrial compounds engage in chemiluminescent reactions, and this phenomenon may be used to measure the concentration of those compounds. One such compound is nitric oxide (NO), an atmospheric pollutant formed by high-temperature combustion with air as the oxidizer.\n\nA spontaneous chemical reaction between nitric oxide and ozone (an unstable molecule formed of three oxygen atoms: O$$_{3}$$) is known to produce chemiluminescence:\n\n$\\hbox{NO} + \\hbox{O}_3 \\to \\hbox{NO}_2 + \\hbox{O}_2 + \\hbox{ light}$\n\nAlthough this process of generating light is quite inefficient (only a small fraction of the NO$$_{2}$$ molecules formed by this reaction will emit light), it is predictable enough to be used as a quantitative measurement method for nitric oxide gas. Ozone gas is very easy to produce on-demand, by exposing air or oxygen to a high-voltage electric discharge.\n\nA simplified diagram for a chemiluminescent nitric oxide gas analyzer appears here:", null, "As with many optical analyzers, a photomultiplier tube serves as the light-detecting sensor, generating an electrical signal in proportion to the amount of light observed inside the reaction chamber. The higher the concentration of NO molecules in the sample gas stream, the more light will be emitted inside the reaction chamber, resulting in a stronger electrical signal produced by the photomultiplier tube.\n\nAlthough this instrument readily measures the concentration of nitric oxide (NO), it is insensitive to other oxides of nitrogen (NO$$_{2}$$, NO$$_{3}$$, etc., collectively referred to as NO$$_{x}$$, pronounced “nocks”). Normally, we would consider this selectivity to be a good thing because it would eliminate interference problems from these other gases. However, as it so happens, these other oxides of nitrogen are every bit as polluting as nitric oxide, and therefore when we measure nitric oxide for pollution monitoring purposes, we usually also wish to measure these other oxides in combination.\n\nIn order to use chemiluminescence to measure all oxides of nitrogen, we must chemically convert the other oxides into nitric oxide (NO) before the sample enters the reaction chamber. This is done in a special module of the analyzer called a converter:", null, "A three-way solenoid valve is shown in this diagram, providing a means to bypass the converter so the analyzer only measures nitric oxide content in the sample gas. With the solenoid valve passing all the sample through the converter, the analyzer responds to all oxides of nitrogen (NO$$_{x}$$) and not just nitric oxide (NO).\n\nOne simple way to achieve the NO$$_{x}$$ $$\\to$$ NO chemical conversion is to simply heat the sample gas to a high temperature, around 1300 $$^{o}$$F. At this temperature, the molecular structure of NO is favored over more complex oxides such as NO$$_{2}$$, the result being a release of oxygen from the NO$$_{2}$$ and NO$$_{3}$$ molecules to become NO molecules. A disadvantage of this technique is that those same high temperatures also have a tendency to convert other compounds of nitrogen such as ammonia (NH$$_{3}$$) into nitric oxide, thereby creating an unintended interference species.\n\nAn alternative NO$$_{x}$$ $$\\to$$ NO conversion technique is to use a metallic reactant in the converter to remove the extra oxygen atoms from the NO$$_{2}$$ molecules. One such metal that works well for this purpose is molybdenum (Mo) heated to the comparatively low temperature of 750 $$^{o}$$F, which is too low to convert ammonia into nitric oxide. The reaction of NO$$_{2}$$ converting to NO is as follows:\n\n$3\\hbox{NO}_2 + \\hbox{Mo} \\to \\hbox{MoO}_3 + 3\\hbox{NO}$\n\nOther oxides (such as NO$$_{3}$$) convert in a similar fashion, leaving their excess oxygen atoms bound to molybdenum atoms and becoming nitric oxide (NO). The only difference between these reactions and the one shown for NO$$_{2}$$ is the proportional (stoichiometric) ratios between molecules.\n\nAs you can see from the reaction, the molybdenum metal is converted into the compound molybdenum trioxide over time, requiring periodic replacement. The rate at which the molybdenum metal depletes inside the converter depends on the sample flow rate and the concentration of NO$$_{2}$$.\n\nAs with other optical gas analyzers, pressure control of the gas sample is critically important for good measurement accuracy. If the pressure of the sampled gas inside the chemiluminescence reaction chamber happens to vary, it will affect the amount of light emitted even if the relative concentration of NO$$_{x}$$ gas remains stable. This is because higher pressures will pack gas molecules closer together, resulting in more reactive molecules inside the chamber for any given percentage or ppm concentration. For this reason, you will see analyzers such as this equipped with pressure regulation to ensure the gas pressure inside the measurement chamber remains constant.\n\n• Share\nPublished under the terms and conditions of the Creative Commons Attribution 4.0 International Public License", null, "" ]
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https://www.meted.ucar.edu/training_module.php?id=1340&tab=05
[ "### Introduction to EPS Theory\n\nprobability distribution function, pdf, cumulative distribution function, cdf, ensemble prediction system, eps, deterministic forecast, probabilistic forecast, standard deviation, mean, mode, median, cluster, plan view product, point product, mean and spread, probability of exceedance, probability of occurrence, spaghetti plot, ensemble trajectory map, extreme forecast index, shift of tail, climatological percentile map, box and whisker, epsgram, shaded percentile, plume diagram," ]
[ null ]
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https://homework.cpm.org/category/CCI_CT/textbook/pc/chapter/4/lesson/4.1.1/problem/4-11
[ "", null, "", null, "### Home > PC > Chapter 4 > Lesson 4.1.1 > Problem4-11\n\n4-11.\n\nSimplify each of the following expressions into a single reduced fraction.\n\n1. $\\frac { \\frac { 1 } { 2 } } { \\frac { \\sqrt { 3 } } { 2 } }$\n\nMultiply the numerator by the reciprocal of the denominator.\n1. $( \\frac { 1 } { x } - x ) ( \\frac { 1 } { x + 1 } - 1 )$\n$\\left(\\frac{1-x^2}{x}\\right)\\left(\\frac{1-x-1}{x+1}\\right)$" ]
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", null ]
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https://holooly.com/solutions-v20/the-rate-of-discharge-of-water-from-a-tank-is-measured-by-means-of-a-notch-for-which-the-flowrate-is-directly-proportional-to-the-height-of-liquid-above-the-bottom-of-the-notch-calculate-and-plot-th/
[ "## Textbooks & Solution Manuals\n\nFind the Source, Textbook, Solution Manual that you are looking for in 1 click.\n\n## Tip our Team\n\nOur Website is free to use.\nTo help us grow, you can support our team with a Small Tip.\n\n## Holooly Tables\n\nAll the data tables that you may search for.\n\n## Holooly Help Desk\n\nNeed Help? We got you covered.\n\n## Holooly Arabia\n\nFor Arabic Users, find a teacher/tutor in your City or country in the Middle East.\n\nProducts\n\n## Textbooks & Solution Manuals\n\nFind the Source, Textbook, Solution Manual that you are looking for in 1 click.\n\n## Holooly Arabia\n\nFor Arabic Users, find a teacher/tutor in your City or country in the Middle East.\n\n## Holooly Help Desk\n\nNeed Help? We got you covered.\n\n## Q. 6.P.2\n\nThe rate of discharge of water from a tank is measured by means of a notch, for which the flowrate is directly proportional to the height of liquid above the bottom of the notch.\nCalculate and plot the profile of the notch if the flowrate is 0.1 m³/s when the liquid level is 150 mm above the bottom of the notch.\n\n## Verified Solution\n\nThe velocity of fluid discharged as a height h above the bottom of the notch is:\n\n$u=\\sqrt{(2 g h)}$\n\nThe velocity therefore varies from zero at the bottom of the notch to a maximum value at the free surface.\nFor a horizontal element of fluid of width 2w and depth dh at a height h above the bottom of the notch, the discharge rate of fluid is given by:\n\n$d Q=\\sqrt{ }(2 g h) 2 w d h$\n\nIf the discharge rate is linearly related to the height of the liquid over the notch, H, w will be a function of h and it may be supposed that:\n\n$w=k h^n$\n\nwhere k is a constant.\n\nSubstituting for w in the equation for dQ and integrating to give the discharge rate over the notch Q then:\n\n$Q=2 \\sqrt{(2 g)} k \\int_0^H h^n h^{0.5} d h$\n\n$=2 \\sqrt{(2 g)} k \\int_0^H h^{n+0.5} d h$\n\n$=2 \\sqrt{(2 g)} k[1 /(n+1.5)] H^{(n+1.5)}$\n\nSince it is required that $Q \\propto H$:\n\n$n+1.5=1$\n\nand:                              $n=-0.5$\nThus:                           $Q=2 \\sqrt{(2 g)} k H$\n\nSince $Q=0.1 m ^3 / s$ when H = 0.15 m:\n\n$k=(0.1 / 0.15)\\left[1 /(2 \\sqrt{(2 g)}]=0.0753 m ^{1.5}\\right.$\n\nThus, with w and h in m:         $w=0.0753 h^{-0.5}$\nand, with w and h in mm:        $w=2374 h^{-0.5}$\n\nand using this equation, the profile is plotted as shown in $\\underline{\\underline{\\text { Figure 6 a}}}$", null, "" ]
[ null, "https://holooly.com/wp-content/uploads/2022/10/6-2.jpg", null ]
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https://answers.everydaycalculation.com/compare-fractions/9-5-and-2-6
[ "Solutions by everydaycalculation.com\n\n## Compare 9/5 and 2/6\n\n1st number: 1 4/5, 2nd number: 2/6\n\n9/5 is greater than 2/6\n\n#### Steps for comparing fractions\n\n1. Find the least common denominator or LCM of the two denominators:\nLCM of 5 and 6 is 30\n\nNext, find the equivalent fraction of both fractional numbers with denominator 30\n2. For the 1st fraction, since 5 × 6 = 30,\n9/5 = 9 × 6/5 × 6 = 54/30\n3. Likewise, for the 2nd fraction, since 6 × 5 = 30,\n2/6 = 2 × 5/6 × 5 = 10/30\n4. Since the denominators are now the same, the fraction with the bigger numerator is the greater fraction\n5. 54/30 > 10/30 or 9/5 > 2/6\n\nMathStep (Works offline)", null, "Download our mobile app and learn to work with fractions in your own time:" ]
[ null, "https://answers.everydaycalculation.com/mathstep-app-icon.png", null ]
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https://www.digicamdb.com/compare/nikon_coolpix-950-vs-nikon_d7000/
[ "# Nikon Coolpix 950 vs. Nikon D7000\n\n### Comparison\n\nchange cameras »", null, "vs", null, "Nikon Coolpix 950 Nikon D7000\ncheck price » check price »\nMegapixels\n1.90\n16.20\nMax. image resolution\n1600 x 1200\n4928 x 3264\n\n## Sensor\n\nSensor type\nCCD\nCMOS\nSensor size\n1/2\" (~ 6.4 x 4.8 mm)\n23.6 x 15.6 mm\nSensor resolution\n1589 x 1195\n4945 x 3275\nDiagonal\n8.00 mm\n28.29 mm\nSensor size comparison\nSensor size is generally a good indicator of the quality of the camera. Sensors can vary greatly in size. As a general rule, the bigger the sensor, the better the image quality.\n\nBigger sensors are more effective because they have more surface area to capture light. An important factor when comparing digital cameras is also camera generation. Generally, newer sensors will outperform the older.\n\n## Actual sensor size\n\nNote: Actual size is set to screen → change »\n vs 1 : 11.98 (ratio) Nikon Coolpix 950 Nikon D7000\nSurface area:\n 30.72 mm² vs 368.16 mm²\nDifference: 337.44 mm² (1098%)\nD7000 sensor is approx. 11.98x bigger than 950 sensor.\nNote: You are comparing sensors of vastly different generations. There is a gap of 11 years between Nikon 950 (1999) and Nikon D7000 (2010). Eleven years is a huge amount of time, technology wise, resulting in newer sensor being much more efficient than the older one.\nPixel pitch\n4.03 µm\n4.77 µm\nPixel pitch tells you the distance from the center of one pixel (photosite) to the center of the next. It tells you how close the pixels are to each other.\n\nThe bigger the pixel pitch, the further apart they are and the bigger each pixel is. Bigger pixels tend to have better signal to noise ratio and greater dynamic range.\nDifference: 0.74 µm (18%)\nPixel pitch of D7000 is approx. 18% higher than pixel pitch of 950.\nPixel area\n16.24 µm²\n22.75 µm²\nPixel or photosite area affects how much light per pixel can be gathered. The larger it is the more light can be collected by a single pixel.\n\nLarger pixels have the potential to collect more photons, resulting in greater dynamic range, while smaller pixels provide higher resolutions (more detail) for a given sensor size.\nRelative pixel sizes:\nvs\nPixel area difference: 6.51 µm² (40%)\nA pixel on Nikon D7000 sensor is approx. 40% bigger than a pixel on Nikon 950.\nPixel density\n6.16 MP/cm²\n4.39 MP/cm²\nPixel density tells you how many million pixels fit or would fit in one square cm of the sensor.\n\nHigher pixel density means smaller pixels and lower pixel density means larger pixels.\nDifference: 1.77 µm (40%)\nNikon 950 has approx. 40% higher pixel density than Nikon D7000.\n\n## Specs\n\nNikon 950\nNikon D7000\nCrop factor\n5.41\n1.53\nTotal megapixels\n2.10\n16.90\nEffective megapixels\n1.90\n16.20\nOptical zoom\n3x\nDigital zoom\nYes\nNo\nISO sensitivity\nAuto, 80, 100, 200, 400\n100 - 6400 in 1, 1/2 or 1/3 EV steps (100 - 25600 with boost)\nRAW\nManual focus\nNormal focus range\n10 cm\nMacro focus range\n2 cm\nFocal length (35mm equiv.)\n38 - 115 mm\nAperture priority\nYes\nYes\nMax. aperture\nf2.6 - f4\nMax. aperture (35mm equiv.)\nf14.1 - f21.6\nn/a\nMetering\nCentre weighted, Matrix, Spot\n3D Matrix metering II, Centre weighted, Spot\nExposure compensation\n±2 EV (in 1/3 EV steps)\n±5 EV (in 1/3 EV, 1/2 EV steps)\nShutter priority\nYes\nYes\nMin. shutter speed\n8 sec\n30 sec\nMax. shutter speed\n1/750 sec\n1/8000 sec\nBuilt-in flash\nExternal flash\nViewfinder\nOptical (tunnel)\nOptical (pentaprism)\nWhite balance presets\n6\n12\nScreen size\n2\"\n3\"\nScreen resolution\n130,000 dots\n921,000 dots\nVideo capture\nMax. video resolution\n1920x1080 (24p)\nStorage types\nCompactFlash type I\nSDHC, SDXC, Secure Digital\nUSB\nUSB 1.0\nUSB 2.0 (480 Mbit/sec)\nHDMI\nWireless\nGPS\nBattery\nAA (4) batteries (NiMH recommended)\nLithium-Ion EN-EL15 rechargeable battery\nWeight\n350 g\n780 g\nDimensions\n143 x 77 x 37 mm\n132 x 105 x 77 mm\nYear\n1999\n2010\n\n vs\n\n## Diagonal\n\nDiagonal is calculated by the use of Pythagorean theorem:\n Diagonal = √ w² + h²\nwhere w = sensor width and h = sensor height\n\n### Nikon 950 diagonal\n\nThe diagonal of 950 sensor is not 1/2 or 0.5\" (12.7 mm) as you might expect, but approximately two thirds of that value - 8 mm. If you want to know why, see sensor sizes.\n\nw = 6.40 mm\nh = 4.80 mm\n Diagonal = √ 6.40² + 4.80² = 8.00 mm\n\n### Nikon D7000 diagonal\n\nw = 23.60 mm\nh = 15.60 mm\n Diagonal = √ 23.60² + 15.60² = 28.29 mm\n\n## Surface area\n\nSurface area is calculated by multiplying the width and the height of a sensor.\n\n### 950 sensor area\n\nWidth = 6.40 mm\nHeight = 4.80 mm\n\nSurface area = 6.40 × 4.80 = 30.72 mm²\n\n### D7000 sensor area\n\nWidth = 23.60 mm\nHeight = 15.60 mm\n\nSurface area = 23.60 × 15.60 = 368.16 mm²\n\n## Pixel pitch\n\nPixel pitch is the distance from the center of one pixel to the center of the next measured in micrometers (µm). It can be calculated with the following formula:\n Pixel pitch = sensor width in mm × 1000 sensor resolution width in pixels\n\n### 950 pixel pitch\n\nSensor width = 6.40 mm\nSensor resolution width = 1589 pixels\n Pixel pitch = 6.40 × 1000 = 4.03 µm 1589\n\n### D7000 pixel pitch\n\nSensor width = 23.60 mm\nSensor resolution width = 4945 pixels\n Pixel pitch = 23.60 × 1000 = 4.77 µm 4945\n\n## Pixel area\n\nThe area of one pixel can be calculated by simply squaring the pixel pitch:\nPixel area = pixel pitch²\n\nYou could also divide sensor surface area with effective megapixels:\n Pixel area = sensor surface area in mm² effective megapixels\n\n### 950 pixel area\n\nPixel pitch = 4.03 µm\n\nPixel area = 4.03² = 16.24 µm²\n\n### D7000 pixel area\n\nPixel pitch = 4.77 µm\n\nPixel area = 4.77² = 22.75 µm²\n\n## Pixel density\n\nPixel density can be calculated with the following formula:\n Pixel density =  ( sensor resolution width in pixels )² / 1000000 sensor width in cm\n\nOne could also use this formula:\n Pixel density = effective megapixels × 1000000 / 10000 sensor surface area in mm²\n\n### 950 pixel density\n\nSensor resolution width = 1589 pixels\nSensor width = 0.64 cm\n\nPixel density = (1589 / 0.64)² / 1000000 = 6.16 MP/cm²\n\n### D7000 pixel density\n\nSensor resolution width = 4945 pixels\nSensor width = 2.36 cm\n\nPixel density = (4945 / 2.36)² / 1000000 = 4.39 MP/cm²\n\n## Sensor resolution\n\nSensor resolution is calculated from sensor size and effective megapixels. It's slightly higher than maximum (not interpolated) image resolution which is usually stated on camera specifications. Sensor resolution is used in pixel pitch, pixel area, and pixel density formula. For sake of simplicity, we're going to calculate it in 3 stages.\n\n1. First we need to find the ratio between horizontal and vertical length by dividing the former with the latter (aspect ratio). It's usually 1.33 (4:3) or 1.5 (3:2), but not always.\n\n2. With the ratio (r) known we can calculate the X from the formula below, where X is a vertical number of pixels:\n(X × r) × X = effective megapixels × 1000000    →\n X = √ effective megapixels × 1000000 r\n3. To get sensor resolution we then multiply X with the corresponding ratio:\n\nResolution horizontal: X × r\nResolution vertical: X\n\n### 950 sensor resolution\n\nSensor width = 6.40 mm\nSensor height = 4.80 mm\nEffective megapixels = 1.90\nr = 6.40/4.80 = 1.33\n X = √ 1.90 × 1000000 = 1195 1.33\nResolution horizontal: X × r = 1195 × 1.33 = 1589\nResolution vertical: X = 1195\n\nSensor resolution = 1589 x 1195\n\n### D7000 sensor resolution\n\nSensor width = 23.60 mm\nSensor height = 15.60 mm\nEffective megapixels = 16.20\nr = 23.60/15.60 = 1.51\n X = √ 16.20 × 1000000 = 3275 1.51\nResolution horizontal: X × r = 3275 × 1.51 = 4945\nResolution vertical: X = 3275\n\nSensor resolution = 4945 x 3275\n\n## Crop factor\n\nCrop factor or focal length multiplier is calculated by dividing the diagonal of 35 mm film (43.27 mm) with the diagonal of the sensor.\n Crop factor = 43.27 mm sensor diagonal in mm\n\n### 950 crop factor\n\nSensor diagonal in mm = 8.00 mm\n Crop factor = 43.27 = 5.41 8.00\n\n### D7000 crop factor\n\nSensor diagonal in mm = 28.29 mm\n Crop factor = 43.27 = 1.53 28.29\n\n## 35 mm equivalent aperture\n\nEquivalent aperture (in 135 film terms) is calculated by multiplying lens aperture with crop factor (a.k.a. focal length multiplier).\n\n### 950 equivalent aperture\n\nCrop factor = 5.41\nAperture = f2.6 - f4\n\n35-mm equivalent aperture = (f2.6 - f4) × 5.41 = f14.1 - f21.6\n\n### D7000 equivalent aperture\n\nAperture is a lens characteristic, so it's calculated only for fixed lens cameras. If you want to know the equivalent aperture for Nikon D7000, take the aperture of the lens you're using and multiply it with crop factor.\n\nCrop factor for Nikon D7000 is 1.53\n\n## Enter your screen size (diagonal)\n\nMy screen size is  inches\n\nActual size is currently adjusted to screen.\n\nIf your screen (phone, tablet, or monitor) is not in diagonal, then the actual size of a sensor won't be shown correctly." ]
[ null, "https://www.digicamdb.com/compare/nikon_coolpix-950-vs-nikon_d7000/images/cameras/nikon_950.png", null, "https://www.digicamdb.com/compare/nikon_coolpix-950-vs-nikon_d7000/images/cameras/nikon_d7000.png", null ]
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https://greenemath.com/College_Algebra/106/Solving-Exponential-Equations-Like-BasesPracticeTest.html
[ "### About Solving Exponential Equations with Like Bases:\n\nIn some cases, we will be asked to solve exponential equations with like bases. To do this, we can use a simple rule that tells us: if ay = ax, then x = y (a is greater than 0 and a is not equal to 1). So basically, if we have like bases, we can set the exponents equal to each other and solve the resulting equation.\n\nTest Objectives\n• Demonstrate an understanding of the rules of exponents\n• Demonstrate the ability to solve exponential equations with like bases\nSolving Exponential Equations with Like Bases Practice Test:\n\n#1:\n\nInstructions: Solve each equation.\n\n$$a)\\hspace{.2em}16^{2x + 1}\\cdot 64=64$$\n\n$$b)\\hspace{.2em}\\left(\\frac{1}{216}\\right)^{-2x}\\cdot 216^{-3x}=36^{x - 1}$$\n\n#2:\n\nInstructions: Solve each equation.\n\n$$a)\\hspace{.2em}9 \\cdot 81^{1 - 3x}=81^{-2x}$$\n\n$$b)\\hspace{.2em}4^{-x - 2}\\cdot 4=8$$\n\n#3:\n\nInstructions: Solve each equation.\n\n$$a)\\hspace{.2em}243^{2x}\\cdot 81^x=243$$\n\n$$b)\\hspace{.2em}\\left(\\frac{1}{25}\\right)^{x - 3}\\cdot \\left(\\frac{1}{125}\\right)^{2x}=125$$\n\n#4:\n\nInstructions: Solve each equation.\n\n$$a)\\hspace{.2em}81^{-2x - 3}\\cdot 81^{-x}=\\frac{1}{3}$$\n\n$$b)\\hspace{.2em}\\frac{1}{8}\\cdot 64^{-x}=64$$\n\n#5:\n\nInstructions: Solve each equation.\n\n$$a)\\hspace{.2em}25^{3x}\\cdot 125^{-2x}=1$$\n\n$$b)\\hspace{.2em}\\left(\\frac{1}{2}\\right)^{-2x}\\cdot 4^{-x}=64$$\n\nWritten Solutions:\n\n#1:\n\nSolutions:\n\n$$a)\\hspace{.2em}x=-\\frac{1}{2}$$\n\n$$b)\\hspace{.2em}x=\\frac{2}{5}$$\n\n#2:\n\nSolutions:\n\n$$a)\\hspace{.2em}x=\\frac{3}{2}$$\n\n$$b)\\hspace{.2em}x=-\\frac{5}{2}$$\n\n#3:\n\nSolutions:\n\n$$a)\\hspace{.2em}x=\\frac{5}{14}$$\n\n$$b)\\hspace{.2em}x=\\frac{3}{8}$$\n\n#4:\n\nSolutions:\n\n$$a)\\hspace{.2em}x=-\\frac{11}{12}$$\n\n$$b)\\hspace{.2em}x=-\\frac{3}{2}$$\n\n#5:\n\nSolutions:\n\na) All Real Numbers\n\nb) No Solution" ]
[ null ]
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https://community.surveygizmo.com/questions/question/get-the-highest-rated-value-in-drag-and-drop-ranking/
[ "# Get the highest rated value in Drag and drop ranking\n\n0\n\nHi all,\n\nI have a Drag and drop ranking question and on next question want to ask that why you rated this value as Highest.\n\nI got a similar post from thread in which they used a custom script and I implemented in exact way but it doesn’t work.\n\nBelow is the Custom Script that I used.\n\nhidepage(15,true)\nhidepage(21,true)\nhidepage(22,true)\nhidepage(23,true)\nhidepage(24,true)\nhidepage(25,true)\n\nrankings = getvalue(14)\n\nfor key,value in pairs (rankings) do\nif (value == ‘1’) then\nif (key == 10036) then\npageid = ’15’\nend\nif (key == 10037) then\npageid = ’21’\nend\nif (key == 10038) then\npageid = ’22’\nend\nif (key == 10039) then\npageid = ’23’\nend\nif (key == 10040) then\npageid = ’24’\nend\nif (key == 10041) then\npageid = ’25’\nend\nend\nend\n\nhidepage(pageid,false)\n\nHere the QID 14 is the Drag and drop ranking question from which we are getting the values.\n\nAlso I created separate questions on page numbers 15,21,22,23,24,25 with each possible highest option.\n\nWhat this Script basically do is:\n\n1. It hides every page with possible highest option questions.\n2. ranking variable stores the value of Drag and drop ranking question.\n3. Then it checks if the option is the highest (value==’1′) or not, if it matches then the pageid is set.\n4. And at end that page will be unhidden.\n\nThanks.\n\n0\n\nHi Dominic,\n\nYou are right I grabbed the script from that document only. But still I am unable to see the resultant page which satisfies the condition in script.\n\n0\n\nI’m not sure if this is the same place where you grabbed the original script but you might try the script documented here:\n\nhttps://help.surveygizmo.com/help/drag-and-drop-show-when\n\nThis uses the Legacy Scripting language but should do the trick. Also, if you run into any trouble I suggest reaching out to SurveyGizmo Support as they may have some pointers:\n\nhttps://help.surveygizmo.com/help/surveygizmo-support-hours\n\nHope this helps!" ]
[ null ]
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http://en.termwiki.com/product_category/Calculus
[ "# Home > Industry/Domain > Mathematics > Calculus\n\n### Calculus\n\nCalculus is the mathmatical study of change. Calculus has two branches, differential calculus and integral calculus.\n\nIndustry: Mathematics\n\n## Calculus\n\n### abacus\n\n##### Mathematics; Calculus\n\nAbacus is a frame with sliding beads on rows of wires or rods and is used for counting.\n\n##### Mathematics; Calculus\n\nThe process of increasing one number by another in order to figure out the sum of the two numbers.\n\n### analog\n\n##### Mathematics; Calculus\n\nUsing continuously moving parts to show information that is changing. The position of the hands of a clock is an analog representation of time.\n\n### arithmetic\n\n##### Mathematics; Calculus\n\nThe use of addition, subtraction, multiplication, and division to solve mathematical problems is termed as arithmetics.\n\n### average\n\n##### Mathematics; Calculus\n\nThe number that is the result of dividing the sum of a set of number of items in the set by the number of items.It is also called arithmetic mean.\n\n### balance\n\n##### Mathematics; Calculus\n\nA device for weighing objects or amounts. A balance usually has a horizontal bar with a pan hanging at each end.\n\n##### Mathematics; Calculus\n\nBhaskara was an Indian mathematician who was the first person to show how decimals are used. He died in 1185.\n\n## Featured blossaries\n\n### Photograpy Framing\n\nCategory: Arts   1", null, "55 Terms", null, "### Street Art\n\nCategory: Arts   2", null, "8 Terms", null, "" ]
[ null, "http://en.termwiki.com/template/termwiki/images/likesmall.jpg", null, "http://img.mediabea.com/thumb1.php", null, "http://en.termwiki.com/template/termwiki/images/likesmall.jpg", null, "http://img.mediabea.com/thumb1.php", null ]
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https://www.geeksforgeeks.org/disease-prediction-using-machine-learning/?ref=rp
[ "Related Articles\n\n# Disease Prediction Using Machine Learning\n\n• Difficulty Level : Expert\n• Last Updated : 15 Sep, 2021\n\nThis article aims to implement a robust machine learning model that can efficiently predict the disease of a human, based on the symptoms that he/she posses. Let us look into how we can approach this machine learning problem:\n\n## Approach:\n\n• Gathering the Data: Data preparation is the primary step for any machine learning problem. We will be using a dataset from Kaggle for this problem. This dataset consists of two CSV files one for training and one for testing. There is a total of 133 columns in the dataset out of which 132 columns represent the symptoms and the last column is the prognosis.\n• Cleaning the Data: Cleaning is the most important step in a machine learning project. The quality of our data determines the quality of our machine learning model. So it is always necessary to clean the data before feeding it to the model for training. In our dataset all the columns are numerical, the target column i.e. prognosis is a string type and is encoded to numerical form using a label encoder.\n• Model Building: After gathering and cleaning the data, the data is ready and can be used to train a machine learning model. We will be using this cleaned data to train the Support Vector Classifier, Naive Bayes Classifier, and Random Forest Classifier. We will be using a confusion matrix to determine the quality of the models.\n• Inference: After training the three models we will be predicting the disease for the input symptoms by combining the predictions of all three models. This makes our overall prediction more robust and accurate.\n\nAt last, we will be defining a function that takes symptoms separated by commas as input, predicts the disease based on the symptoms by using the trained models, and returns the predictions in a JSON format.\n\n## Workflow for the implementation:", null, "Make sure that the Training and Testing are downloaded and the train.csv, test.csv are put in the dataset folder. Open jupyter notebook and run the code individually for better understanding.\n\n## Python3\n\n `# Importing libraries``import` `numpy as np``import` `pandas as pd``from` `scipy.stats ``import` `mode``import` `matplotlib.pyplot as plt``import` `seaborn as sns``from` `sklearn.preprocessing ``import` `LabelEncoder``from` `sklearn.model_selection ``import` `train_test_split, cross_val_score``from` `sklearn.svm ``import` `SVC``from` `sklearn.naive_bayes ``import` `GaussianNB``from` `sklearn.ensemble ``import` `RandomForestClassifier``from` `sklearn.metrics ``import` `accuracy_score, confusion_matrix` `%``matplotlib inline`\n\nFirstly we will be loading the dataset from the folders using the pandas library. While reading the dataset we will be dropping the null column. This dataset is a clean dataset with no null values and all the features consist of 0’s and 1’s. Whenever we are solving a classification task it is necessary to check whether our target column is balanced or not. We will be using a bar plot, to check whether the dataset is balanced or not.\n\n## Python3\n\n `# Reading the train.csv by removing the``# last column since it's an empty column``DATA_PATH ``=` `\"dataset/Training.csv\"``data ``=` `pd.read_csv(DATA_PATH).dropna(axis ``=` `1``)` `# Checking whether the dataset is balanced or not``disease_counts ``=` `data[``\"prognosis\"``].value_counts()``temp_df ``=` `pd.DataFrame({``    ``\"Disease\"``: disease_counts.index,``    ``\"Counts\"``: disease_counts.values``})` `plt.figure(figsize ``=` `(``18``,``8``))``sns.barplot(x ``=` `\"Disease\"``, y ``=` `\"Counts\"``, data ``=` `temp_df)``plt.xticks(rotation``=``90``)``plt.show()`\n\nOutput:", null, "From the above plot, we can observe that the dataset is a balanced dataset i.e. there are exactly 120 samples for each disease, and no further balancing is required. We can notice that our target column i.e. prognosis column is of object datatype, this format is not suitable to train a machine learning model. So, we will be using a label encoder to convert the prognosis column to the numerical datatype. Label Encoder converts the labels into numerical form by assigning a unique index to the labels. If the total number of labels is n, then the numbers assigned to each label will be between 0 to n-1.\n\n## Python3\n\n `# Encoding the target value into numerical``# value using LabelEncoder``encoder ``=` `LabelEncoder()``data[``\"prognosis\"``] ``=` `encoder.fit_transform(data[``\"prognosis\"``])`\n\n## Splitting the data for training and testing the model\n\nNow that we have cleaned our data by removing the Null values and converting the labels to numerical format, It’s time to split the data to train and test the model. We will be splitting the data into 80:20 format i.e. 80% of the dataset will be used for training the model and 20% of the data will be used to evaluate the performance of the models.\n\n## Python3\n\n `X ``=` `data.iloc[:,:``-``1``]``y ``=` `data.iloc[:, ``-``1``]``X_train, X_test, y_train, y_test ``=``train_test_split(``  ``X, y, test_size ``=` `0.2``, random_state ``=` `24``)` `print``(f``\"Train: {X_train.shape}, {y_train.shape}\"``)``print``(f``\"Test: {X_test.shape}, {y_test.shape}\"``)`\n\nOutput:\n\n```Train: (3936, 132), (3936,)\nTest: (984, 132), (984,)```\n\n## Model Building\n\nAfter splitting the data, we will be now working on the modeling part. We will be using K-Fold cross-validation to evaluate the machine learning models. We will be using Support Vector Classifier, Gaussian Naive Bayes Classifier, and Random Forest Classifier for cross-validation. Before moving into the implementation part let us get familiar with k-fold cross-validation and the machine learning models.\n\n• K-Fold Cross-Validation: K-Fold cross-validation is one of the cross-validation techniques in which the whole dataset is split into k number of subsets, also known as folds, then training of the model is performed on the k-1 subsets and the remaining one subset is used to evaluate the model performance.\n• Support Vector Classifier: Support Vector Classifier is a discriminative classifier i.e. when given a labeled training data, the algorithm tries to find an optimal hyperplane that accurately separates the samples into different categories in hyperspace.\n• Gaussian Naive Bayes Classifier: It is a probabilistic machine learning algorithm that internally uses Bayes Theorem to classify the data points.\n• Random Forest Classifier: Random Forest is an ensemble learning-based supervised machine learning classification algorithm that internally uses multiple decision trees to make the classification. In a random forest classifier, all the internal decision trees are weak learners, the outputs of these weak decision trees are combined i.e. mode of all the predictions is as the final prediction.\n\nUsing K-Fold Cross-Validation for model selection\n\n## Python3\n\n `# Defining scoring metric for k-fold cross validation``def` `cv_scoring(estimator, X, y):``    ``return` `accuracy_score(y, estimator.predict(X))` `# Initializing Models``models ``=` `{``    ``\"SVC\"``:SVC(),``    ``\"Gaussian NB\"``:GaussianNB(),``    ``\"Random Forest\"``:RandomForestClassifier(random_state``=``18``)``}` `# Producing cross validation score for the models``for` `model_name ``in` `models:``    ``model ``=` `models[model_name]``    ``scores ``=` `cross_val_score(model, X, y, cv ``=` `10``,``                             ``n_jobs ``=` `-``1``,``                             ``scoring ``=` `cv_scoring)``    ``print``(``\"==\"``*``30``)``    ``print``(model_name)``    ``print``(f``\"Scores: {scores}\"``)``    ``print``(f``\"Mean Score: {np.mean(scores)}\"``)`\n\nOutput:\n\n============================================================\n\nSVC\n\nScores: [1. 1. 1. 1. 1. 1. 1. 1. 1. 1.]\n\nMean Score: 1.0\n\n============================================================\n\nGaussian NB\n\nScores: [1. 1. 1. 1. 1. 1. 1. 1. 1. 1.]\n\nMean Score: 1.0\n\n============================================================\n\nRandom Forest\n\nScores: [1. 1. 1. 1. 1. 1. 1. 1. 1. 1.]\n\nMean Score: 1.0\n\nFrom the above output, we can notice that all our machine learning algorithms are performing very well and the mean scores after k fold cross-validation are also very high. To build a robust model we can combine i.e. take the mode of the predictions of all three models so that even one of the models makes wrong predictions and the other two make correct predictions then the final output would be the correct one. This approach will help us to keep the predictions much more accurate on completely unseen data. In the below code we will be training all the three models on the train data, checking the quality of our models using a confusion matrix, and then combine the predictions of all the three models.\n\nBuilding robust classifier by combining all models:\n\n## Python3\n\n `# Training and testing SVM Classifier``svm_model ``=` `SVC()``svm_model.fit(X_train, y_train)``preds ``=` `svm_model.predict(X_test)` `print``(f\"Accuracy on train data by SVM Classifier\\``: {accuracy_score(y_train, svm_model.predict(X_train))``*``100``}\")` `print``(f\"Accuracy on test data by SVM Classifier\\``: {accuracy_score(y_test, preds)``*``100``}\")``cf_matrix ``=` `confusion_matrix(y_test, preds)``plt.figure(figsize``=``(``12``,``8``))``sns.heatmap(cf_matrix, annot``=``True``)``plt.title(``\"Confusion Matrix for SVM Classifier on Test Data\"``)``plt.show()` `# Training and testing Naive Bayes Classifier``nb_model ``=` `GaussianNB()``nb_model.fit(X_train, y_train)``preds ``=` `nb_model.predict(X_test)``print``(f\"Accuracy on train data by Naive Bayes Classifier\\``: {accuracy_score(y_train, nb_model.predict(X_train))``*``100``}\")` `print``(f\"Accuracy on test data by Naive Bayes Classifier\\``: {accuracy_score(y_test, preds)``*``100``}\")``cf_matrix ``=` `confusion_matrix(y_test, preds)``plt.figure(figsize``=``(``12``,``8``))``sns.heatmap(cf_matrix, annot``=``True``)``plt.title(``\"Confusion Matrix for Naive Bayes Classifier on Test Data\"``)``plt.show()` `# Training and testing Random Forest Classifier``rf_model ``=` `RandomForestClassifier(random_state``=``18``)``rf_model.fit(X_train, y_train)``preds ``=` `rf_model.predict(X_test)``print``(f\"Accuracy on train data by Random Forest Classifier\\``: {accuracy_score(y_train, rf_model.predict(X_train))``*``100``}\")` `print``(f\"Accuracy on test data by Random Forest Classifier\\``: {accuracy_score(y_test, preds)``*``100``}\")` `cf_matrix ``=` `confusion_matrix(y_test, preds)``plt.figure(figsize``=``(``12``,``8``))``sns.heatmap(cf_matrix, annot``=``True``)``plt.title(``\"Confusion Matrix for Random Forest Classifier on Test Data\"``)``plt.show()`\n\nOutput:\n\n```Accuracy on train data by SVM Classifier: 100.0\nAccuracy on test data by SVM Classifier: 100.0```", null, "```Accuracy on train data by Naive Bayes Classifier: 100.0\nAccuracy on test data by Naive Bayes Classifier: 100.0```", null, "```Accuracy on train data by Random Forest Classifier: 100.0\nAccuracy on test data by Random Forest Classifier: 100.0```", null, "From the above confusion matrices, we can see that the models are performing very well on the unseen data. Now we will be training the models on the whole train data present in the dataset that we downloaded and then test our combined model on test data present in the dataset.\n\nFitting the model on whole data and validating on the Test dataset:\n\n## Python3\n\n `# Training the models on whole data``final_svm_model ``=` `SVC()``final_nb_model ``=` `GaussianNB()``final_rf_model ``=` `RandomForestClassifier(random_state``=``18``)``final_svm_model.fit(X, y)``final_nb_model.fit(X, y)``final_rf_model.fit(X, y)` `# Reading the test data``test_data ``=` `pd.read_csv(``\"./dataset/Testing.csv\"``).dropna(axis``=``1``)` `test_X ``=` `test_data.iloc[:, :``-``1``]``test_Y ``=` `encoder.transform(test_data.iloc[:, ``-``1``])` `# Making prediction by take mode of predictions``# made by all the classifiers``svm_preds ``=` `final_svm_model.predict(test_X)``nb_preds ``=` `final_nb_model.predict(test_X)``rf_preds ``=` `final_rf_model.predict(test_X)` `final_preds ``=` `[mode([i,j,k])[``0``][``0``] ``for` `i,j,``               ``k ``in` `zip``(svm_preds, nb_preds, rf_preds)]` `print``(f\"Accuracy on Test dataset by the combined model\\``: {accuracy_score(test_Y, final_preds)``*``100``}\")` `cf_matrix ``=` `confusion_matrix(test_Y, final_preds)``plt.figure(figsize``=``(``12``,``8``))` `sns.heatmap(cf_matrix, annot ``=` `True``)``plt.title(``\"Confusion Matrix for Combined Model on Test Dataset\"``)``plt.show()`\n\nOutput:\n\n`Accuracy on Test dataset by the combined model: 100.0`", null, "We can see that our combined model has classified all the data points accurately. We have come to the final part of this whole implementation, we will be creating a function that takes symptoms separated by commas as input and outputs the predicted disease using the combined model based on the input symptoms.\n\nCreating a function that can take symptoms as input and generate predictions for disease\n\n## Python3\n\n `symptoms ``=` `X.columns.values` `# Creating a symptom index dictionary to encode the``# input symptoms into numerical form``symptom_index ``=` `{}``for` `index, value ``in` `enumerate``(symptoms):``    ``symptom ``=` `\" \"``.join([i.capitalize() ``for` `i ``in` `value.split(``\"_\"``)])``    ``symptom_index[symptom] ``=` `index` `data_dict ``=` `{``    ``\"symptom_index\"``:symptom_index,``    ``\"predictions_classes\"``:encoder.classes_``}` `# Defining the Function``# Input: string containing symptoms separated by commmas``# Output: Generated predictions by models``def` `predictDisease(symptoms):``    ``symptoms ``=` `symptoms.split(``\",\"``)``    ` `    ``# creating input data for the models``    ``input_data ``=` `[``0``] ``*` `len``(data_dict[``\"symptom_index\"``])``    ``for` `symptom ``in` `symptoms:``        ``index ``=` `data_dict[``\"symptom_index\"``][symptom]``        ``input_data[index] ``=` `1``        ` `    ``# reshaping the input data and converting it``    ``# into suitable format for model predictions``    ``input_data ``=` `np.array(input_data).reshape(``1``,``-``1``)``    ` `    ``# generating individual outputs``    ``rf_prediction ``=` `data_dict[``\"predictions_classes\"``][final_rf_model.predict(input_data)[``0``]]``    ``nb_prediction ``=` `data_dict[``\"predictions_classes\"``][final_nb_model.predict(input_data)[``0``]]``    ``svm_prediction ``=` `data_dict[``\"predictions_classes\"``][final_svm_model.predict(input_data)[``0``]]``    ` `    ``# making final prediction by taking mode of all predictions``    ``final_prediction ``=` `mode([rf_prediction, nb_prediction, svm_prediction])[``0``][``0``]``    ``predictions ``=` `{``        ``\"rf_model_prediction\"``: rf_prediction,``        ``\"naive_bayes_prediction\"``: nb_prediction,``        ``\"svm_model_prediction\"``: nb_prediction,``        ``\"final_prediction\"``:final_prediction``    ``}``    ``return` `predictions` `# Testing the function``print``(predictDisease(``\"Itching,Skin Rash,Nodal Skin Eruptions,Dischromic  Patches\"``))`\n\nOutput:\n\n```{\n'rf_model_prediction': 'Fungal infection',\n'naive_bayes_prediction': 'Fungal infection',\n'svm_model_prediction': 'Fungal infection',\n'final_prediction': 'Fungal infection'\n}```\n\nNote: The symptoms that are given as input to the function should be exactly the same among the 132 symptoms in the dataset.\n\nAttention geek! Strengthen your foundations with the Python Programming Foundation Course and learn the basics.\n\nTo begin with, your interview preparations Enhance your Data Structures concepts with the Python DS Course. And to begin with your Machine Learning Journey, join the Machine Learning – Basic Level Course\n\nMy Personal Notes arrow_drop_up" ]
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https://en.wikipedia.org/wiki/Signal_separation
[ "# Signal separation\n\nSource separation, blind signal separation (BSS) or blind source separation, is the separation of a set of source signals from a set of mixed signals, without the aid of information (or with very little information) about the source signals or the mixing process. It is most commonly applied in digital signal processing and involves the analysis of mixtures of signals; the objective is to recover the original component signals from a mixture signal. The classical example of a source separation problem is the cocktail party problem, where a number of people are talking simultaneously in a room (for example, at a cocktail party), and a listener is trying to follow one of the discussions. The human brain can handle this sort of auditory source separation problem, but it is a difficult problem in digital signal processing.\n\nThis problem is in general highly underdetermined, but useful solutions can be derived under a surprising variety of conditions. Much of the early literature in this field focuses on the separation of temporal signals such as audio. However, blind signal separation is now routinely performed on multidimensional data, such as images and tensors, which may involve no time dimension whatsoever.\n\nSeveral approaches have been proposed for the solution of this problem but development is currently still very much in progress. Some of the more successful approaches are principal components analysis and independent component analysis, which work well when there are no delays or echoes present; that is, the problem is simplified a great deal. The field of computational auditory scene analysis attempts to achieve auditory source separation using an approach that is based on human hearing.\n\nThe human brain must also solve this problem in real time. In human perception this ability is commonly referred to as auditory scene analysis or the cocktail party effect.\n\n## Applications\n\n### Cocktail party problem\n\nAt a cocktail party, there is a group of people talking at the same time. You have multiple microphones picking up mixed signals, but you want to isolate the speech of a single person. BSS can be used to separate the individual sources by using mixed signals. In the presence of noise, dedicated optimization criteria need to be used\n\n### Image processing\n\nFigure 2 shows the basic concept of BSS. The individual source signals are shown as well as the mixed signals which are received signals. BSS is used to separate the mixed signals with only knowing mixed signals and nothing about original signal or how they were mixed. The separated signals are only approximations of the source signals. The separated images, were separated using Python and the Shogun toolbox using Joint Approximation Diagonalization of Eigen-matrices (JADE) algorithm which is based on independent component analysis, ICA. This toolbox method can be used with multi-dimensions but for an easy visual aspect images(2-D) were used.\n\n### Medical imaging\n\nOne of the practical applications being researched in this area is medical imaging of the brain with magnetoencephalography (MEG). This kind of imaging involves careful measurements of magnetic fields outside the head which yield an accurate 3D-picture of the interior of the head. However, external sources of electromagnetic fields, such as a wristwatch on the subject's arm, will significantly degrade the accuracy of the measurement. Applying source separation techniques on the measured signals can help remove undesired artifacts from the signal.\n\n### EEG\n\nIn electroencephalogram (EEG) and magnetoencephalography (MEG), the interference from muscle activity masks the desired signal from brain activity. BSS, however, can be used to separate the two so an accurate representation of brain activity may be achieved.\n\n### Music\n\nAnother application is the separation of musical signals. For a stereo mix of relatively simple signals it is now possible to make a fairly accurate separation, although some artifacts remain.\n\n### Others\n\nOther applications:\n\n• Communications\n• Stock Prediction\n• Seismic Monitoring\n• Text Document Analysis\n\n## Mathematical representation\n\nThe set of individual source signals, $s(t)=(s_{1}(t),\\dots ,s_{n}(t))^{T}$", null, ", is 'mixed' using a matrix, $A=[a_{ij}]\\in \\mathbb {R} ^{m\\times n}$", null, ", to produce a set of 'mixed' signals, $x(t)=(x_{1}(t),\\dots ,x_{m}(t))^{T}$", null, ", as follows. Usually, $n$", null, "is equal to $m$", null, ". If $m>n$", null, ", then the system of equations is overdetermined and thus can be unmixed using a conventional linear method. If $n>m$", null, ", the system is underdetermined and a non-linear method must be employed to recover the unmixed signals. The signals themselves can be multidimensional.\n\n$x(t)=A\\cdot s(t)$", null, "The above equation is effectively 'inverted' as follows. Blind source separation separates the set of mixed signals, $x(t)$", null, ", through the determination of an 'unmixing' matrix, $B=[B_{ij}]\\in \\mathbb {R} ^{n\\times m}$", null, ", to 'recover' an approximation of the original signals, $y(t)=(y_{1}(t),\\dots ,y_{n}(t))^{T}$", null, ".\n\n$y(t)=B\\cdot x(t)$", null, "## Approaches\n\nSince the chief difficulty of the problem is its underdetermination, methods for blind source separation generally seek to narrow the set of possible solutions in a way that is unlikely to exclude the desired solution. In one approach, exemplified by principal and independent component analysis, one seeks source signals that are minimally correlated or maximally independent in a probabilistic or information-theoretic sense. A second approach, exemplified by nonnegative matrix factorization, is to impose structural constraints on the source signals. These structural constraints may be derived from a generative model of the signal, but are more commonly heuristics justified by good empirical performance. A common theme in the second approach is to impose some kind of low-complexity constraint on the signal, such as sparsity in some basis for the signal space. This approach can be particularly effective if one requires not the whole signal, but merely its most salient features.\n\n### Methods\n\nThere are different methods of blind signal separation:" ]
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https://www.physicsforums.com/threads/shell-theorem-false-centers.239876/
[ "# Shell Theorem & False Centers\n\nThe Newtonian Shell Theorem makes important predictions about the gravitational force experienced by an object located inside a spherically symetrical massive structure, such as a hollow or solid ball. The same predictions are made by Gauss' Law. According to http://en.wikipedia.org/wiki/Shell_theorem\" [Broken]:\n\n1. If the body is a spherically symmetric shell (i.e. a hollow ball), no gravitational force is exerted by the shell on any object inside, regardless of the object's location within the shell.\n\n2. Inside a solid sphere of constant density the gravitational force varies linearly with distance from the center, becoming zero at the center of mass.\n\nIt bears emphasizing that the Shell Theorem applies only with respect to mass arrangements which are (a) actually centered on the center of the sphere, (b) are symetrically distributed around that center, and (c) have constant density in the non-hollow portion. In this thread I want to discuss some examples that don't seem to meet all three criteria, although the issue can become interestingly subtle.\n\nThe most obvious example is that a solid or hollow shell of matter cannot act as a \"gravity shield\" to avoid the gravity of other nearby objects. For example a dense sphere buried just under the earth's surface is not shielded from the earth's gravity to any significant degree. This is so of course because the earth is not arranged spherically around the sphere, and the center of the sphere is not the \"true\" center of the earth-sphere system. I attached a simple diagram which illustrates this example.\n\nI'll post a more interesting example later.\n\nJon\n\n#### Attachments\n\n• Sphere A inside Sphere B.pdf\n47.6 KB · Views: 169\nLast edited by a moderator:\n\nInfinite homogeneous dust\n\nOK, so here's a subtle example.\n\nLet's consider an infinite, spatially flat, Lambda = 0 universe filled homogeneously with \"dust\" (matter particles). Let's arbitrarily define an origin coordinate and a metric sphere centered on that origin. Let's say this universe is expanding slowly with a low deceleration factor (relative to the proper size of the sphere). Let's place a massless test particle inside this sphere; it is at proper rest with respect to our origin coordinate. Can we correctly apply the shell theorem to this test particle?\n\nSure, as long as the center of our sphere represents the true center of the dust cloud. Uh oh... this dust cloud is infinite so it does not have a gravitational center. We can establish an arbitrary center by defining any coordinate system we wish. But it is not a gravitational center; a universe of this type has no true center.\n\nTherefore I hypothesize that the test particle will NOT move towards the center of the sphere in the manner described in the shell theorem. It will not move at all because it feels no directional gravity vector.\n\nLet's test this hypothesis by arbitrarily defining three very large, symetrically arranged, overlapping metric spheres, each with its own arbitrarily defined origin coordinate. An observer is located at each origin point. We place the massless test particle equidistant between the three origin points. In what direction will the test particle move? A diagram is attached.\n\nJon\n\n#### Attachments\n\n• 3 spheres & test particle 6-12-08.pdf\n100.1 KB · Views: 182\nHaelfix\nWrite down the metric for your test universe, and try to derive gauss's law. I suspect you will find a problem (assuming the metric is what I think you think it is).\n\nWallace\nCan we correctly apply the shell theorem to this test particle?\n\nSure, as long as the center of our sphere represents the true center of the dust cloud.\n??? What has 'the true center' of the dust cloud got to do with whether Gauss's law is valid?? You might want to find some basic undergraduate texts to look this up, I think you have an misconceived view of what the shell thereom is.\n\nLet's test this hypothesis by arbitrarily defining three very large, symetrically arranged, overlapping metric spheres, each with its own arbitrarily defined origin coordinate. An observer is located at each origin point. We place the massless test particle equidistant between the three origin points. In what direction will the test particle move? A diagram is attached.\n\nJon\n\nThe answer is very simple, the particle will be accelerated towards the center of all three spheres. Where they actually move in the next instant however depends on their current velocity of course, not the acceleration.Think about what this represents, it's a deccelerating homogenous universe which means that the rate that any pair of particles is moving apart is slowing down. Thus the rate that the chosen test particle is receeding from the centre of all three spheres is slowing. Thus the shell theorem clearly works correctly and gives you precisely the result you expect.\n\nHi Haelfix,\n\nWrite down the metric for your test universe, and try to derive gauss's law. I suspect you will find a problem (assuming the metric is what I think you think it is).\n\nI'm not sure what point you are trying to get at. Maybe you can explain more.\n\nAs I understand it, Gauss' Law is based on the fact that inverse square forces (such as gravity) produce equal flux across a spherical surface regardless of the radius of the sphere.\n\nSince I defined the test universe to be flat, I think that Gauss's law will apply consistent with my description. If it were spatially curved however (e.g. a closed universe) Gauss' Law would not calculate a correct result unless it were corrected for the curvature.\n\nJon\n\nLast edited:\nHi Wallace,\nThe answer is very simple, the particle will be accelerated towards the center of all three spheres. Where they actually move in the next instant however depends on their current velocity of course, not the acceleration.Think about what this represents, it's a decelerating homogenous universe which means that the rate that any pair of particles is moving apart is slowing down. Thus the rate that the chosen test particle is receeding from the centre of all three spheres is slowing. Thus the shell theorem clearly works correctly and gives you precisely the result you expect.\n\nWe agree on this point! The test particle will accelerate towards all three spheres equally. And in the same way, if we define an infinite number of symmetrical surrounding spheres (in three dimensions), the test particle will accelerate equally towards all of them. In other words, the test particle gains no directional vector at all.\n\nSo, the test particle will not actually move at all (in proper distance) towards the center of any individual sphere arbitrarily selected from among the multitude of surrounding spheres.\n\nEDIT: If it wasn't clear already, I want to make it clear that the origins of the three spheres ( or infinite number of spheres) are not in proper motion with respect to the test particle at the start of the test.\n\nJon\n\nLast edited:\nChronos\nGold Member\nThat is absurd. The universe has no shell-like observational features.\n\nWallace\nHi Wallace,\n\nWe agree on this point! The test particle will accelerate towards all three spheres equally. And in the same way, if we define an infinite number of symmetrical surrounding spheres (in three dimensions), the test particle will accelerate equally towards all of them. In other words, the test particle gains no directional vector at all.\n\nWhat is a 'directional vector'? Presumably something different from a non-directional vector, which is a clearly nonsensical concept.\n\nI think you are trying to say that in a homogenous and isotropic universe there is no prefferred direction, which is obviously true by definition. Every direction from the particle is the same so of course it feels no net acceleration in any direction.\n\nSo, the test particle will not actually move at all (in proper distance) towards the center of any individual sphere arbitrarily selected from among the multitude of surrounding spheres.\n\nEDIT: If it wasn't clear already, I want to make it clear that the origins of the three spheres ( or infinite number of spheres) are not in proper motion with respect to the test particle at the start of the test.\n\nJon\n\nWrong. The particle will move towards the center of all of the other spheres.\n\nI really fail to see the point of this thread? You seem to be attempting to demonstrate that you get different physical results depending on how you choose to define co-ordinates (in this case the centers of spherical Gaussian surfaces). The only way this could possibly occur is if Gauss's law fails. Clearly the resolution is to correctly understand Gausses law instead of claiming you have discovered some interesting paradox.\n\nWallace\nThat is absurd. The universe has no shell-like observational features.\n\nTo Jon's defence on this point, the 'shells' he is reffering to are Gaussian surfaces, which are mathematical constructs to help solve a problem more easily. He is not refferring to any physical shell like features, the situation under consideration is a homogenous universe.\n\nHi Wallace,\nThe particle will move towards the center of all of the other spheres.\nI admit I'm dense sometimes, but I don't understand this statement. In my diagram, from a tops-down two dimensional perspective, the stationary centers of the three spheres are set at 120 degree azimuthal angles relative to each other, so of course a test particle equidistant between them cannot move at three different angles at once.\n\nAny physical movement of a test particle can be defined as a vector in proper coordinates, with a magnitude and a single coordinate direction. Yet you agree that the movement here is non-directional and that it is nonsense to speak of nondirectional vectors. Therefore by first principles the test particle does not move.\n\nI can only interpret your statement to mean that the test particle does not move, but rather the three sphere origin points will gravitationally collapse towards the test particle. That outcome cannot occur in this scenario. The three sphere origins are mere proper coordinate points, they are not massive objects; the gravity of the background dust cloud does not cause their proper distances relative to each other to change.\n\nYou seem to be attempting to demonstrate that you get different physical results depending on how you choose to define co-ordinates (in this case the centers of spherical Gaussian surfaces). The only way this could possibly occur is if Gauss's law fails.\nYes as you say I am attempting to demonstrate that use of different coordinates changes the physical result. However, I disagree that this means Gauss' law fails. The mathematics of Gauss' law is just fine. What I am suggesting is that Gauss' law simply does not apply to mass distributions in which the center of the sphere is not the gravitational center of the entire mass distribution. You have already characterized this suggestion as nonsense, but I think my example demonstrates that the problem is legitimately subtle.\n\nJon\n\nLast edited:\nWallace\nHi Wallace,\n\nI admit I'm dense sometimes, but I don't understand this statement. In my diagram, from a tops-down two dimensional perspective, the stationary centers of the three spheres are set at 120 degree azimuthal angles relative to each other, so of course a test particle equidistant between them cannot move at three different angles at once.\n\nAny physical movement of a test particle can be defined as a vector in proper coordinates, with a magnitude and a single coordinate direction. Yet you agree that the movement here is non-directional and that it is nonsense to speak of nondirectional vectors. Therefore by first principles the test particle does not move.\n\nMovement, i.e. having a non-zero velocity, means that a particles co-ordinates are changing. In order to know if a particles co-ordinates are changing one needs to know how the co-ordinate system has been defined. It is also crucial to realise that the behaviour of something in a particular co-ordinate system is not universal, so something can be moving on one co-ordinate system but not in another.\n\nNow, if you construct a spherical co-ordinate system centered on the point in the middle of your diagram then clearly the point does not move in these co-ordinates. What you will find however, is that clearly the three other particles all move towards the origin, due to the gravitational attraction of the mass enclosed by a sphere centered on the origin with a radius extending to the other test particle. Your test particles will be accelerated by gravity, so clearly they must be accelerated towards the centre.\n\nNow, if you instead construct a spherical co-ordiant system centred on another particle then we can consider that the particle in the 'middle' which is no longer at the origin will be accelerated towards the new origin by the same reasoning. Which particles move and which do not depends on the co-ordinate system. What does not depend on the co-ordinate system however is the distance between each particle as a function of time. It doesn't matter how you define your co-ordinates you will find that the particles will move together due to gravity at exactly the same rate.\n\nIt is obvious what will happen in this situation, that the universe will collapse. It is also clear that this is consistent with the shell theorem.\n\nI can only interpret your statement to mean that the test particle does not move, but rather the three sphere origin points will gravitationally collapse towards the test particle.\n\nYes, absolutely for the reasons described above.\n\nThat outcome cannot occur in this scenario. The three sphere origins are mere proper coordinate points, they are not massive objects; the gravity of the background dust cloud does not cause their proper distances relative to each other to change.\n\nI don't know what you are saying here? You said in post #2 that 'an observer is placed at each origin point' this seems to imply that there are massless test particles at these points. If so then these test particles will be accelerated by gravity towards every other particle in the Universe as described above. They most definately will all move towards the middle particle. If these points are not massless test particles and merely arbitrarily defined points in the space then this whole discussion is meaningless. Co-ordinates may do whatever we define them to in a way unconstrained by physics, we could having expanding co-ordinates in a contracting universe if we wanted.\n\nIn terms of physics (i.e. what does the actual matter do?) the situation here is clear. The universe collapsing and we can understand this by considering any one of the four spheres in your picture.\n\nWhat I am suggesting is that Gauss' law simply does not apply to mass distributions in which the center of the sphere is not the gravitational center of the entire mass distribution. You have already characterized this suggestion as nonsense, but I think my example demonstrates that the problem is legitimately subtle.\n\nJon\n\nI really don't think this thread belongs in cosmology. You will probably get a better explanation of the fundamentals of Gauss's law in some of the other sub forums. I suggest you ask this question in one of those, since you clearly have misconceptions about it. Even reading the Wiki article might be a good start. Don't take this as a criticism, I'm trying help and it is clear that the confusion here lies in a fundamental misunderstanding of this physical law. Trying to understand this in the context of cosmology is then like trying to run before crawling. Learn to crawl first and you will get to running properly much faster.\n\nIf the universe is expanding at a rate greater than the 'escape velocity' then it won't recollapse.\n\nIf the universe is static then the question is whether it can remain so. This question has a long history.\n\nEinstein said no - he had to introduce the cosmological constant to try to fudge it.\n\nNewton said yes. Each object in the universe will be attracted equally from all directions and so will have no reason to move.\n\nHowever, even in Newtonian gravity, one can argue that if we divide the universe up into spherical shells, then those outside a given radius will have no effect and so the ball inside that radius will collapse. Applying this to the universe as a whole you get it collapsing to a point.\n\nCertainly this worried those who followed Newton. For instance, Boskovich mentioned the possibility of a form of cosmological constant in 1763, and I've read that Newton had a similar idea (although I haven't been able to find it in his works)\n\nYou said in post #2 that 'an observer is placed at each origin point' this seems to imply that there are massless test particles at these points. If so then these test particles will be accelerated by gravity towards every other particle in the Universe as described above. They most definately will all move towards the middle particle.\nWallace, your line of logic here is not helpful in understanding the problem. The coordinate system in my example is defined solely by the 3 center points of the 3 spheres, not by the test particle. In the \"thought exeriment\" way that these scenarios are usually described... we send fictional spaceships to each of the 3 sphere centers. Spaceship #1 drops a small marker at an arbitrary location. The 3 spaceships then use radar ranging and fictional rulers laid end to end (like Barnes & Francis do) to define the 3 sphere center locations with respect to the single marker, and to verify that they remain at a fixed proper distance from each other throughout the exercise.\n\nYou err in assuming that the spaceships will be spontaneously pulled by gravity towards the test particle. Why would a homogeneous, directionless dust cloud around the spaceships cause them to move an a single arbitrary direction? Why not the opposite direction? This is another obvious microcosm of the false center problem.\n\nEven if the spaceships did feel a unique directional gravitational pull in one arbitrary direction (which they don't), it would in no way undermine the validity of the simple coordinate system which is defined by points mapped in space, not by the spaceships.\n\nIf these points are not massless test particles and merely arbitrarily defined points in the space then this whole discussion is meaningless.\nAll of the \"Tethered Galaxy\" experiments define an arbitrary origin, so of course arbitrary origins are meaningful. Using 3 arbitrary origins should be just as meaningful, but my example doesn't need to rely on that, since 2 of the 3 sphere center origins are defined with reference to a single initial arbitrarily placed marker.\n\nThe universe collapsing and we can understand this by considering any one of the four spheres in your picture.\nMy scenario defined the universe to be spacially flat and expanding at the decelerating Einstein-de Sitter rate. The universe I defined will never collapse. Please try to keep the facts straight.\n\nEven reading the Wiki article might be a good start.\nOf course I read the Wikipedia article and much more on this subject. It was reading textbooks which alerted me to the fact that it is a common misconception that the shell theorem and Gauss' Law apply when the center of the sphere is not the center of the mass distribution being examined. May I respectfully suggest that you brush up a bit?\n\nJon\n\nLast edited:\nHi chronon,\nIf the universe is static then the question is whether it can remain so. This question has a long history.\nYes as I understand it the problem with a static universe with a cosmological constant is that it is inherently unstable. Even the most microscopic change in mass will cause the universe to accelerate into an expansion or collapse mode. So it is commonly said that the universe must be either expanding or contracting, and not static.\n\nThe only models I can think of for a stable static universe are the \"black hole inhibitors\" I mentioned in another thread. Virial motion in theory ought to be able to stabilize a gravitationally overdense universe; but over the long term virial motion is perturbed by collisions and near collisions, as well as by gravity waves, so it eventually will collapse. Adding some amount of cosmological constant would help stabilize it, I'm not sure if it can entirely stabilize. The maximum size of a virial universe is also limited by causality, is there enough time in the history of the universe for it to coordinate its virialization?\n\nThe other alternative is an electrostatically charged universe, such as one filled with electron plasma. But seems to be a fairly useless model as a practical matter because if regular electrically neutral matter is added to it, the neutral matter will gravitationally collapse even though the electron plasma won't. Perhaps adjusting the exact mix of neutral and charged matter would help stabilize it, and adding a cosmological constant ought to help.\n\nJon\n\nLast edited:\nHi Wallace,\nHere's a slightly simplified example (attachment) that may help clarify this. In this version, 3 very massive objects are attached to a strong but lightweight (insignificant mass) support ring. A \"Shell Theorem sphere\" is measured around each massive object. Again a test particle is dropped equidistant from the 3 massive objects. Which way will it move?\n\nOf course, it will not move at all.\n\nOne more thought about \"arbitrary\" origins: The earth, the center of our Local Group, or any other point in the universe that one wishes to use use as an \"origin\" of a coordinate system is equally arbitrary.\n\nJon\n\n#### Attachments\n\n• Sphere with 3 masses.pdf\n105.7 KB · Views: 150\nLast edited:\nHaelfix\nJon, please write the metric down for what you have in mind and the coordinates you want to use. We can't talk about this quantitatively if you do not. I don't understand what you have in mind, and in particular this can alter the shell theorem (Gauss's theorem is not mantained unambigously bc of coordinate subleties if its not exactly flat).\n\nThe reason I ask, is b/c you seem to think this acts like something static, even though elsewhere you assumed a FRW universe with k = 0 and lambda = 0. Alternatively I think there is a confusion about global issues vs local ones.\n\nTo wit, in the limit where things are very flat (or when spatial curvature/cc is very small relative to the density term), the universe is in a approximately newtonian limit and the shell theorem *must* be valid.\n\nLast edited:\nHi Haelfix,\nFirst, check out my most recent post where I attached a slightly revised version of the example, it may resolve your question.\nJon, please write the metric down for what you have in mind and the coordinates you want to use.\nI'm sorry but I don't understand your question. The universe in this model is a very simple straightforward one, a homogeneous, isotropic, spatially flat, matter dominated, dust-filled Einstein-de Sitter universe with Lambda = 0. It is expanding and the deceleration factor q is positive. The standard RW line element defines the metric.\n\nAs I said, an arbitrary origin point #1 is selected, and then two additional origin points are mapped out at equal distances from origin #1 and separated by 60 degrees of azimuth angle (from the perspective of origin #1).\nTo wit, in the limit where things are very flat (or when spatial curvature/cc is very small relative to the density term), the universe is in a approximately newtonian limit and the shell theorem *must* be valid.\nI agree completely, the shell theorem and Gauss' Law *are* valid. But they are valid *only* when applied to a proper set of facts. The facts must be such that the hypothetical point mass at the center of the sphere is the *gravitational center* of the entire mass distribution.\n\nJon\n\nLast edited:\nWell, on further review the last example I posted (Sphere with 3 masses) doesn't accomplish what I hoped. It serves as only as an example of how the Shell Theorem works with respect to *external* test objects.\n\nMy discussion has been about test objects located *inside* a solid or homogeneous mass (e.g., dust filled sphere.) For that discussion, we'll need to revert back to the original \"3 spheres\" example. Sorry about that.\n\nJon\n\nHi Wallace,\nIt doesn't matter how you define your co-ordinates you will find that the particles will move together due to gravity at exactly the same rate.\n\nIt is obvious what will happen in this situation, that the universe will collapse. It is also clear that this is consistent with the shell theorem.\n\nIn terms of physics (i.e. what does the actual matter do?) the situation here is clear. The universe collapsing and we can understand this by considering any one of the four spheres in your picture.\nThese statements of yours may be key to sorting out our discussion. If the particles in the universe were to move closer together in the manner you describe, then by definition the average matter density increases as a function of time. Yet every elementary textbook tells us that the defining characteristic of a homogeneous, expanding FLRW universe is that average matter density relentlessly decreases as a function of time. The matter density in any one (and in all 3) of the spheres will decrease over time, not increase. (Think of density in terms of the average proper distance between dust particles.) Surely you must acknowledge the direct conflict here with your interpretation of the shell theorem. If density were to increase in one spherical region of the universe, then it would need to decrease faster than the FLRW rate in other regions of the universe. That is inconsistent with the very concept of homogeneity.\n\n(Of course for the purposes of this theoretical discussion we are assuming perfect homogeneity and ignoring any local gravitational perturbations caused by primordial overdensities, etc.)\n\nJon\n\nLast edited:\nSorry to keep coming back to this, but here's one more variation on the thought experiment which I think illustrates the absurdity of permitting only one sphere at a time to measure the valid shell theorem results.\n\nLet's say we build a very large rigid ring using advanced materials which are so astoundingly lightweight that the mass of the ring is insignificant compared to the homogeneous dust density of the region of the universe it occupies. We'll mount 360 center-facing numbered video cameras on the ring, exactly 1 degree of azimuth apart. We will consider each video camera to be the center point of its own Shell Thereom sphere, all spheres being equally sized and just large enough to overlap at the point in space defining the radial center of the ring.\n\nBefore the start of each test round, we will write down on a slip of paper which of the 360 cameras we have randomly selected to be the origin of our coordinate system for that round. A different camera is designated for each test round. We will not disclose this information to the spaceship pilot, who will release the massless test particle at the exact centerpoint and depart.\n\nDoes the shell theorem predict that in each test round, the test particle will move only towards the particular video camera whose number is written on on the current slip of paper? Need I say more?\n\nJon\n\nLast edited:\nBefore the start of each test round, we will write down on a slip of paper which of the 360 cameras we have randomly selected to be the origin of our coordinate system for that round. A different camera is designated for each test round. We will not disclose this information to the spaceship pilot, who will release the massless test particle at the exact centerpoint and depart.\nYour origin is moving with respect to the surrounding dust which rather confuses things.\n\nIf you released a test particle from the ring then it would accelerate towards the centre.\n\nHi chronon,\nYour origin is moving with respect to the surrounding dust which rather confuses things.\nThis subject can get confusing. The origin can be any one of the cameras. In an FLRW universe, no matter where an observer is located, she sees the dust in her immediate local area not to be moving at all; she observers that objects further away from her are moving directly away from her, at velocities proportional to their distance.\n\nEDIT: I confused myself on my first try at answering this. I'll try again: Only one point at a time on the ring can be aligned with its local Hubble flow. All other points on the ring will observe the background dust cloud moving with respect to them. However, this should have no bearing on the movement of a local test particle.\n\nI've thought a lot about whether the proper motion (or the acceleration) of the dust cloud has any direct bearing on a proper-distance application of the shell theorem. I don't think it does. Acceleration has an indirect bearing in the sense that it *results from* the existence of a gravitational field.\nIf you released a test particle from the ring then it would accelerate towards the centre.\nIn my scenario the test particle is dropped at the radial center of the ring, not from the ring itself. However, even if the test particle were dropped next to the ring, I am sure the test particle would not move relative to the ring. The background dust cloud is directionless so there is nothing to cause it to impart a unique direction of movement to the test particle. We've defined the mass of the ring itself to be insignificant.\n\nJon\n\nLast edited:\nAnother easy example:\n\nA very long rigid ruler is constructed in space out of advanced materials which are so astoundingly lightweight that the mass of the ruler is insignificant compared to the homogeneous dust cloud in the region. The ruler is marked with 4 units of length. \"Shell Theorem spheres\" are measured, the smaller sphere having radius = 1 unit and its center located 1 unit from the left edge of the ruler; the larger sphere having radius = 4 units and its center located 4 units from the left end of the ruler. A test particle is released at the left end of the ruler, just at the edge of both spheres. Will the test particle initially accelerate at the rate determined by the mass of the r=1 sphere or the r=4 sphere? Diagram is attached.\n\nNote that the total mass of the r=4 sphere is 64 times larger than the mass of the r=1 sphere, proportional to $$r^{3}$$. If the Shell Theorem applied, the initial gravitational acceleration rate imparted to the test particle by the the r=4 sphere would be 4 times greater than the acceleration imparted from the r=1 sphere, due to the inverse square law as measured from each sphere's center.\n\nObviously, if either sphere satisfies the Shell Theorem here, then the other one violates it. So the Shell Theorem can't be applicable. In fact, the test particle will not move at all relative to the ruler.\n\nJon\n\n#### Attachments\n\n• 2 spheres & ruler.pdf\n144.6 KB · Views: 136\nLast edited:\nA very long rigid ruler is constructed in space out of advanced materials which are so astoundingly lightweight that the mass of the ruler is insignificant compared to the homogeneous dust cloud in the region. The ruler is marked with 4 units of length. \"Shell Theorem spheres\" are measured, the smaller sphere having radius = 1 unit and its center located 1 unit from the left edge of the ruler; the larger sphere having radius = 4 units and its center located 4 units from the left end of the ruler. A test particle is released at the left end of the ruler, just at the edge of both spheres. Will the test particle initially accelerate at the rate determined by the mass of the r=1 sphere or the r=4 sphere? Diagram is attached.\nYou need to specify how the ruler moves with respect to the surrounding dust. I assume that you want it to be stationary, but the dust cloud is expanding, so that only one part of the ruler can be stationary with respect to its surroundings. Is it the left end, the right end or the middle.\n\nIn fact, the test particle will not move at all relative to the ruler\nActually, for any of the options I suggested in the previous post, the particle will accelerate to the right with respect to the ruler.\n\nHi chronon,\nThanks for thinking this through with me.\n\nI've reached the point where I'm going to throw in the towel and agree that the Shell Theorem does apply correctly in a homogeneous, expanding infinite dust universe with Lambda = 0.\n\nThe textbooks and articles I've read do not clearly and completely explain the subtlety of how the Shell Theorem should be applied in an infinite homogeneous body. This leaves it to us to have to connect a lot of dots, so to speak.\n\nMy statement that the Shell Theorem requires a true gravitational center was not entirely incorrect. I maintain that it does.\n\nHowever, the subtlety is that every individual mass particle in space is a true gravitational center of its own. This is because the gravity of the dust cloud applies a directionless force which tries to collapse every particle in the universe closer to every other particle in the universe. Dust particles participating in the background Hubble flow have a pre-existing directionless momentum which acts to increase the proper distance between every particle and every other particle, that is, to expand the dust cloud. As we know, this expansionary momentum counteracts the dust cloud's own gravitational collapse force, and in a flat universe this results in the particles retaining momentum away from each other forever but at a rate that decreases asymptotically over time to zero. The fact that the expansionary momentum of the dust cloud never declines to zero demonstrates that the magnitude of the global expansionary action relatively dominates the magnitude of the global gravitational collapse action in perpetuity. Still, the global collapse action is always acting on every particle and everywhere in the dust cloud.\n\nAny set of massless test particles initially placed at proper rest with respect to each other, regardless of the number of such particles or their distances apart, will observe the proper distance between themselves decreasing as a function of time due to the background dust cloud's gravitational collapse force. The further the test particles are apart, the faster they will accelerate together: the acceleration is directly proportional to the distance. By definition the test particles have no initial expansionary momentum (relative to each other) acting to offset the collapse action, so the collapse action alone will control.\n\nBecause the collapse action of multiple test particles is truly directionless with respect to the global background dust cloud, any coordinate system we overlay onto the scenario will portray it in a misleading way. A coordinate system, regardless of where its arbitrary origin is placed, will portray that the collapse action of multiple test particles creates unique directional vectors. Relocating the origin of the coordinate system from one place to another will as Wallace says portray a different set of directional vectors. All such directional vectors are false from the absolute global perspective of the infinite universe; the collapse action of multiple test particles is always nondirectional.\n\nThat it took me so long to get a grip on this action, I will attribute to my own density. I hope that more insightful textbook entries and articles will be written on this subject.\n\nJon\n\nLast edited:\nOK, so now let's release a very large but finite number of test particles at random finite proper distances apart in this flat, homogeneous, dust-only model universe, with each test particle initially having zero instantaneous proper velocity relative to each other particle. One of the particles will be at rest relative to its local Hubble flow (and CMB frame), and by definition all of the other particles will not be. We'll station an observer next to each test particle, with each observer at zero proper velocity relative to all of the test particles and other observers. What will they observe?\n\nAt first, each observer will see all of the test particles and other observers accelerating rapidly toward that observer's location. Any two test particles which start out relatively far apart will initially observe a higher rate of proper acceleration together, proportional to their initial separation distance. After the test particles accelerate to a certain relative speed (proportional to initial separation), their proper speed will mostly flatten out (acceleration will asymptotically approach zero), due to both the declining force of gravity (force inversely proportional to their distance from the convergence point) and the ongoing evacuation of the dust cloud due to ongoing cosmic expansion. Eventually all of the test particles and observers will converge on a single point. The location of that point relative to the background dust cloud (it has to be relative to something tangible, other than each other) will be the starting point of the test particle which was initially at rest relative to its local Hubble flow and CMB frame. If the test particles (and observers) narrowly avoid colliding, they will pass through the convergence point and continue moving in straight trajectories out the opposite side of the convergence point. After that, the test particles (and observers) will continue separating from each other in perpetuity, at proper velocities that decline slightly over time.\n\nIn the above description, I omitted the complication that the convergence speed of the test particles (and observers) is limited to be < the speed of light. Presumably (I'm not sure about this) the test particles (and observers) whose convergence speed is relativistically reduced (compared to the Newtonian approximation) will be delayed in arriving at the convergence point. So an initial bunch of test particles will converge at the same time, followed by an ongoing stream of \"straggler\" test particles which will increase in density over time, then decrease, and finally end (since the number of test particles is finite.) After passing through the convergence point, this entire stream of test particles (and observers) will expand away from each other in perpetuity.\n\nJon\n\nLast edited:\nOK, so now let's release a very large but finite number of test particles at random finite proper distances apart in this flat, homogeneous, dust-only model universe, with each test particle initially having zero instantaneous proper velocity relative to each other particle.\n\n....\n\nAfter passing through the convergence point, this entire stream of test particles (and observers) will expand away from each other in perpetuity.\n\nJon\nThe behavior of a finite set of test particles reacting to the collapse action per the Shell Theorem is non-intuitive to me, but there it is, just like in the Tethered Galaxy problem.\n\nSo what will we observe if we release an infinite number of test particles at random proper distances apart in this model universe, with each test particle initially having zero instantaneous proper velocity relative to each other particle?\n\nI believe that the collapse action will be just the same as in the finite example, except that the influx density of test particles through the convergence point will continue increasing in perpetuity and never end. After test particles pass through the convergence point, they will expand away from each other in the opposite direction they arrived from, in perpetuity, and obviously with the same constantly increasing density as the influx.\n\nAn infinite and ever increasing dust storm!\n\nJon\n\nOK, so here's a subtle example.\n\nLet's consider an infinite, spatially flat, Lambda = 0 universe filled homogeneously with \"dust\" (matter particles). Let's arbitrarily define an origin coordinate and a metric sphere centered on that origin. Let's say this universe is expanding slowly with a low deceleration factor (relative to the proper size of the sphere). Let's place a massless test particle inside this sphere; it is at proper rest with respect to our origin coordinate. Can we correctly apply the shell theorem to this test particle?\n\nSure, as long as the center of our sphere represents the true center of the dust cloud. Uh oh... this dust cloud is infinite so it does not have a gravitational center. We can establish an arbitrary center by defining any coordinate system we wish. But it is not a gravitational center; a universe of this type has no true center.\n\nTherefore I hypothesize that the test particle will NOT move towards the center of the sphere in the manner described in the shell theorem. It will not move at all because it feels no directional gravity vector.\n\nLet's test this hypothesis by arbitrarily defining three very large, symetrically arranged, overlapping metric spheres, each with its own arbitrarily defined origin coordinate. An observer is located at each origin point. We place the massless test particle equidistant between the three origin points. In what direction will the test particle move? A diagram is attached.\n\nJon\n\nI think this example a bit bogus, since you have an infinite sphere. In that case you can not make some arbitrary assumption about the location of any center.\n\nBut apart from that these are nice examples.\nApplication of the Shell theorem in a homogeneous and isotropic universe would seem to indicate that each each mass would be in a stable equilibrium.\nBut one could argue also that each point in this universe is in an unstable or metastable equilibirum.\n\nAs another thought experiment:\nAssume an initial configuration of equal mass points m in an infinite 3D grid with length d. Initial all (relative) velocities of all mass particles is zero.\nWhat would be the time evolution of such a configuration?\n(both locally and globally)\n\nLast edited:" ]
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http://blog.sigfpe.com/2006/12/evaluating-cellular-automata-is.html
[ "## Tuesday, December 19, 2006\n\n### Evaluating cellular automata is comonadic\n\nPaul Potts's post inspired me to say something about cellular automata too.\n\nSo here's the deal: whenever you see large datastructures pieced together from lots of small but similar computations there's a good chance that we're dealing with a comonad. In cellular automata we compute the value of each cell in the next generation by performing a local computation based on the neighbourhood of that cell. So cellular automata look like they might form a good candidate for comonadic evaluation.\n\nI want to work on 'universes' that extend to infinity in both directions. And I want this universe to be constructed lazily on demand. One way of doing that is to represent a 'universe' as a centre point, a list of all elements to the left of that centre point and a list of all elements to the right. Here's a suitable\ntype:\n\n`> data U x = U [x] x [x]`\n\nFor example U [-1,-2..] 0 [1,2..] can be thought of as representing all of the integers in sequence.\n\nBut this actually contains slightly more information than a list that extends to infinity both ways. The centre point forms a kind of focus of attention. We could shift that focus of attention left or right. For example consider\n\nU [-2,-3..] (-1) [0,1..]\n\nThis represents the same sequence of integers but the focus has been shifted left. So think of the type U x as being a doubly infinite sequence with a cursor. (In fact, this makes it a kind of zipper.)\n\nWe can formalise the notion of shifting left and right as follows:\n\n`> right (U a b (c:cs)) = U (b:a) c cs> left (U (a:as) b c) = U as a (b:c)`\n\nAn object of type U is semantically like a C pointer into a const block of memory. You can increment it, decrement it and dereference it using the function I'll call coreturn below.\n\nAs U is a kind of list structure, it needs a map. In fact, we can define fmap for it:\n\n`> instance Functor U where> fmap f (U a b c) = U (map f a) (f b) (map f c)`\n\nNow the fun starts. First I'll bemoan the fact that Comonads aren't in the standard Haskell libraries (at least I don't think they are). So I have to define them myself:\n\n`> class Functor w => Comonad w where> (=>>) :: w a -> (w a -> b) -> w b> coreturn :: w a -> a> cojoin :: w a -> w (w a)> x =>> f = fmap f (cojoin x)`\n\ncojoin is the dual to the usual join function. I've chosen to do things the category theoretical way and define =>> in terms of cojoin.\n\nAnd here's why U forms a Comonad:\n\n`> instance Comonad U where> cojoin a = U (tail \\$ iterate left a) a (tail \\$ iterate right a)> coreturn (U _ b _) = b`\n\nLook closely at cojoin. It turns a into a 'universe' of 'universes' where each element is a copy of a shifted left or right a number of times. This is where all the work is happening. The reason we want to do this is as follows: we want to write rules that work on the local neighbourhoods of our universe. We can think of a universe with the cursor pointing at a particular element as being an element with a neighbourhood on each side. For example, we can write a cellular automaton rule like this:\n\n`> rule (U (a:_) b (c:_)) = not (a && b && not c || (a==b))`\n\nIn order to apply this everywhere in the universe we need to apply the rule to each possible shift of the universe. And that's what cojoin does, it constructs a universe of all possible shifts of a. Compare with what I said here. So believe it or not, we've already written the code to evaluate cellular automata. u =>> rule applies the rule to u. The rest is just boring IO:\n\n`> shift i u = (iterate (if i<0 then left else right) u) !! abs i>> toList i j u = take (j-i) \\$ half \\$ shift i u where> half (U _ b c) = [b] ++ c>> test = let u = U (repeat False) True (repeat False)> in putStr \\$> unlines \\$> take 20 \\$> map (map (\\x -> if x then '#' else ' ') . toList (-20) 20) \\$> iterate (=>> rule) u`\n\nLazy infinite structures, comonads, zippers. I think I'm just beginning to get the hang of this functional programming lark! Over Xmas I might feel ready to try writing a piece of code longer than a dozen or so lines.\n\nAnyway, I must end with a credit. I probably wouldn't have come up with this if I hadn't read this paper by Uustalu and Vene.\n\nLabels:", null, "Andrea Vezzosi said...\n\nI like very much this lazy solution, but how would you generalize it to spaces with more dimensions?\n(Like in Life where you have 8 other cells in your neighborhood.)\nI can imagine increasing the number of the lists, but not very well how to travel this new universe, especially how to reach the cells in the \"oblique\" directions\n\nThursday, 21 December, 2006", null, "sigfpe said...\n\nI think there may be an easy but inefficient solution to the problem of working in 2D using the type U (U Bool). I'd imagine 'up' and 'down' to be defined like 'fmap left' and 'fmap right' or something like that. I think you can then construct a new 'cojoin' with a little bit of work. But this might be a bit inefficient. But maybe not - I'd have to think about it harder but all those 'fmap left's might still only do O(1) work per cell in total. When I next have a moment...\n\nThursday, 21 December, 2006", null, "sigfpe said...\n\nHere are some more details:\n\n> data U2 x = U2 (U (U x)) deriving Show\n\n> instance Functor U2 where\n\n> fmap f (U2 u) = U2 \\$ fmap (fmap f) u\n\n> coreturn (U2 u) = coreturn (coreturn u)\n\n> cojoin (U2 u) = fmap U2 \\$ U2 \\$ roll \\$ roll u where\n\n> iterate1 f = tail . iterate f\n\n> roll a = U (iterate1 (fmap left) a) a (iterate1 (fmap right) a)\n\n(Sorry about lack of indentation.) I have the game of life running fine.\n\nThe strategy for U2 is much the same as that for U. cojoin makes a 2D grid of 2D grids where each inner grid is shifted an amount corresponding to its location within the outer grid. A similar strategy can be used to implement many other comonads. In fact, that was the ulterior motive in writing this CA code: getting intuition about what cojoin typically looks like.\n\nFriday, 22 December, 2006", null, "Andrea Vezzosi said...\n\nwell I'm quite lost on the intuition of your roll, and why you use fmap U2 in cojoin.\nHowever, a rule would be written like this?\nrule (U2 (U ((U (a:_) b (c:_)):_) (U (d:_) x (f:_)) ((U (g:_) h (i:_)):_))) = ...\nwhere the letters have this alignment?\na b c\nd x f\ng h i\n\nSaturday, 23 December, 2006", null, "sigfpe said...\n\nHere is the exact rule I used in my code:\n\nrule' (U2 (U\n(U (u0:_) u1 (u2:_):_)\n(U (u3:_) u4 (u5:_))\n(U (u6:_) u7 (u8:_):_))) =\nlet n = length \\$ filter id [u0,u1,u2,u3,u5,u6,u7,u8] in\nu4 && (n==2 || n==3) || (not u4) && n==3\n\nMaybe I'll tidy up my code and fill it with useful comments so I can post the entire thing here.\n\nU2 converts a 1D universe of 1D universes into a 2D universe. 'fmap U2' converts...take a deep breath...a 2D universe of 1D universes of 1D universes into a 2D universe of 2D universes. 'fmap U2 . fmap' converts a 1D universe of 1D universes of 1D universes of 1D universes into a 2D universe of 2D universes. Conceptually, a 2D universe is the same thing as a 1D universe of 1D universes. The guts of the code is written in terms of 1D universes, and 'fmap U2 . U2' is just a bit of fluff at the end to convert everything back to 2D universes so cojoin has the right type.\n\nThe 'roll' is just taking advantage of the thing I said in an earlier comment. If you think of the inner U's as columns and the outer one as rows, then fmap left and right shift up and down. The slightly weird thing about 'roll' is that exactly the same piece of code does rows and columns whereas you might expect one function with fmaps for columns and one function without for rows. You can think of fmap as 'ducking down' a layer of U-flavoured onion skin. The two rolls do different things because each time it is used there are different layers of onion skin in place. The best way to make sense of it is to do what I did - make U and U2 instances of Show that can print stuff out with a pretty layout and then go through cojoin one step at a time.\n\nSaturday, 23 December, 2006", null, "kowey said...\n\nWhen I first saw this, I was frightened off by the seeming abundance of scary new concepts: cellular automata, comonads, functors (for no good reason I still get nervous when I see that word), universes. Then I read it a second time, read it instead of skimming it, and realised that oh... there really is nothing to it.\n\nThe comonad stuff will take a while to sink in, but reading your post, I get the impression that they are not fundamentally deeper than monads. No cobrain is required to understand them, after all. Note: fellow weaklings might do well to have Cale's Monads as containers open in a separate window or browser tab.\n\nThanks for this post. For starters, the literate Haskell helps, pasting and running is useful. More importantly, the post had this wonderful effect of mutual reinforcement, in which several things one does not know well get tied together, and as a result all become clearer. Not only do I now have a slight taste of comonad, I also have now more than heard about cellular automata, and my tenuous grasp of zippers is now strenghtened. Makes me wish zippers were first presented in list terms from the very beginning.\n\nWhat might have been helpful is some means for the easily frightened to realise that the post contains easy stuff, but short of inventing a Haskell coloured belts system, [this post is rated yellow belt; if you understand monads in terms of >>= and return, etc], I don't know what such a mechanism would consist of. Another potentially useful aid might be to put the example automaton rule into words, or even pictures. Incidentally, this particular example rule does not seem to make use of c. Is that right?\n\nTuesday, 02 January, 2007", null, "sigfpe said...\n\nI think you're right, my rule doesn't seem to use c. I just made up random rules until I liked the result.\n\nthere really is nothing to it\nYes! There are some incredibly difficult looking papers out there but when you actually get down to implementing examples they can suddenly seem close to trivial. Check out the comonad I define here for an example that's reminiscent of the kinds of adding-up-lists-of-prices examples given in books like \"Learn C in 21 days\". And yet the paper I drew on is scary as hell!\n\nTuesday, 02 January, 2007", null, "Anonymous said...\n\nYou should try implementing the \"Cellular Potts\" model developed by Glazer & Granier. It's more physically meaningful than CA.\n\nWednesday, 15 August, 2007", null, "Anonymous said...\n\nWhoa, and I thought this site was about the iPhone)!\n\nMonday, 21 January, 2008", null, "geophf said...\n\nAre all Zippers that are instances of Functor Comonads? Conversely, and simply, are all Comonads Zippers that are Functors? I've done a bit of reading on (co)monads, and the above is the current straw I'm grasping at for understanding comonads better. Am I missing the boat entirely?\n\nAs for the cellular automata implementation, Mathworld, etc, has a list of standardized rules. Rule 30 is demonstrated graphically as the banner of my company's webpage: http://www.logicaltypes.com/.\n\nHere is a way to pattern-match to build these standardized rules:\n\n> rule30 (U (a:_) b (c:_)) = bitfrom (rule30' (bitof a b c))\n> where rule30' 111 = 0\n> rule30' 110 = 0\n> rule30' 101 = 0\n> rule30' 100 = 1\n> rule30' 011 = 1\n> rule30' 010 = 1\n> rule30' 001 = 1\n> rule30' 000 = 0\n> bitof x y z = 100 * t x + 10 * t y + t z\n> bitfrom = toEnum\n\n(Ah, well, the indentation is not preserved, but you get the idea.)\n\nSince all the standardized rules follow the above pattern (where the rule number is the bit-pattern result from the three-bit-pattern input), it is trivial in Haskell to write a generalized\n\nrule :: Enum a => Int -> U a -> a\n\nfor all the rules that follow that pattern.\n\nMonday, 30 June, 2008", null, "Anonymous said...\n\nPondering rewriting this but representing the 'universe' as a function from an integer leads one to realise that we get a comonad from functions from any monoid as follows:\n\ncoreturn a = a mempty\ncojoin a = curry (a . uncurry mappend)\nfmap f = (f.)\n\nWhich allows us to handle automata on 1d, square grids, hex grids, and so on. Albeit perhaps inefficiently.\n\nI haven't tried this so it's probably embarrassingly wrong.\n\nWednesday, 18 February, 2009", null, "Alex S. said...\n\nSo I've gone forward and implemented the game of life, without any fancy printing, but still, it seems to work:\n\nhttp://hpaste.org/fastcgi/hpaste.fcgi/view?id=11012#a11019\n\nComments and suggestions are very welcome!\n\nAlex.\n\nWednesday, 21 October, 2009", null, "Alex S. said...\n\nSo I went ahead and wrote the code. It's on hpaste under http://hpaste.org/fastcgi/hpaste.fcgi/view?id=11012#a11019\n\nTry to run it, seems to work for me!\n\nAlex.\n\nWednesday, 21 October, 2009", null, "gereeter said...\n\nscc,\n\nThat's an interesting little duality. The product type can be a comonad with no restrictions, but only a monad if its \"extra\" type is a monoid. Similarly, the reader type (or function type, whichever you prefer) can be a monad with no restrictions, but can only be a comonad if the \"extra\" type is a monoid.\n\nAlso, you were expressing a lack of confidence in your definitions, so let's verify the comonad laws:\n\n1.\n\ncoreturn . cojoin\n= \\x -> coreturn (cojoin x)\n= \\x -> cojoin x mempty\n= \\x -> (curry (x . uncurry mappend)) mempty\n= \\x y -> (x . uncurry mappend) (mempty, y)\n= \\x y -> x (uncurry mappend (mempty, y))\n= \\x y -> x (mappend mempty y)\n= \\x y -> x y\n= \\x -> x\n= id\n\n2.\n\nfmap coreturn . cojoin\n= \\x -> fmap coreturn (cojoin x)\n= \\x -> coreturn . cojoin x\n= \\x y -> coreturn (cojoin x y)\n= \\x y -> cojoin x y mempty\n= \\x y -> curry (x . uncurry mappend) y mempty\n= \\x y -> (x . uncurry mappend) (y, mempty)\n= \\x y -> x (uncurry mappend (y, mempty))\n= \\x y -> x (mappend y mempty)\n= \\x y -> x y\n= \\x -> x\n= id\n\n3.\n\ncojoin . cojoin\n= \\x -> cojoin (cojoin x)\n= \\x -> cojoin (curry (x . uncurry mappend))\n= \\x -> curry (curry (x . uncurry mappend) . uncurry mappend)\n= \\x y z -> curry (curry (x . uncurry mappend) . uncurry mappend) y z\n= \\x y z -> (curry (x . uncurry mappend) . uncurry mappend) (y, z)\n= \\x y z -> curry (x . uncurry mappend) (uncurry mappend (y, z))\n= \\x y z -> curry (x . uncurry mappend) (mappend y z)\n= \\x y z w -> curry (x . uncurry mappend) (mappend y z) w\n= \\x y z w -> (x . uncurry mappend) (mappend y z, w)\n= \\x y z w -> x (uncurry mappend (mappend y z, w))\n= \\x y z w -> x (mappend (mappend y z) w)\n= \\x y z w -> x (mappend y (mappend z w))\n= \\x y z w -> x (uncurry mappend (y, mappend z w))\n= \\x y z w -> (x . uncurry mappend) (y, mappend z w)\n= \\x y z w -> curry (x . uncurry mappend) y (mappend z w)\n= \\x y z w -> cojoin x y (mappend z w)\n= \\x y z w -> cojoin x y (uncurry mappend (z, w))\n= \\x y z w -> (cojoin x y . uncurry mappend) (z, w)\n= \\x y z w -> curry (cojoin x y . uncurry mappend) z w\n= \\x y z w -> cojoin (cojoin x y) z w\n= \\x y -> cojoin (cojoin x y)\n= \\x y -> (cojoin . cojoin x) y\n= \\x -> cojoin . cojoin x\n= \\x -> fmap cojoin (cojoin x)\n= \\x -> (fmap cojoin . cojoin) x\n= fmap cojoin . cojoin\n\nPhew. That was long. But yes, your definitions are correct.\n\nMonday, 08 August, 2011", null, "Jeremy List said...\n\nToroidal universes are a pretty simple extension (you could just use circular lists but that would lead to recalculating a lot of values)\n\n> right (U a b []) = right (U [] b (reverse a))\n> right (U a b (c:cs)) = U (b:a) c cs\n> left (U [] b c) = left (U (reverse c) b [])\n> left (U (a:as) b c) = U as a (b:c)\n\nThursday, 17 October, 2013", null, "Jeremy List said...\n\nToroidal universes are a pretty simple extension (you could just use circular lists but that would lead to recalculating a lot of values)\n\n> right (U a b []) = right (U [] b (reverse a))\n> right (U a b (c:cs)) = U (b:a) c cs\n> left (U [] b c) = left (U (reverse c) b [])\n> left (U (a:as) b c) = U as a (b:c)\n\nThursday, 17 October, 2013", null, "Miguel Negrão said...\n\nIHaskell notebook with diagrams drawing of CA:" ]
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https://roboticsbackend.com/should-you-learn-mathematics-to-program-robots/
[ "# Should You Learn Mathematics To Program Robots?\n\nYou know that mathematics are everywhere, and especially in robotics.\n\nBut, if you just want to program robots, is it really important? Could you succeed without it?\n\nSo, should you learn mathematics to program robots? The answer is: yes and no. Quite useful, right? Because it’s not as simple as that.\n\nKeep reading so you’ll understand if and when you need to learn some mathematics, depending on what you want to achieve.\n\n## When you start a new project: use libraries\n\nYou can use tons of libraries that will allow you not to do the maths yourself.\n\nLet’s imagine that you have to compute the inverse kinematic of a robot. Well, this involves a lot of mathematics. Soon you’ll read stuff about the Denavit-Hartenberg parameters, and your motivation will start to fade.\n\nHow could you possibly use that in your code, without spending a huge amount of time understanding the maths? Time, of course, that you won’t spend on developing your robot software.\n\nWell, this is a problem you can solve (at least temporary). Instead of trying to do the maths yourself, what if you could find a library that can do the maths for you? That’s the good question to ask, especially if you want to progress fast on your prototype or small project.\n\nFor this specific example, you can quickly find the KDL from Orocos: Kinematics and Dynamics Library. This is a C++ library you can use directly in your code. Provided that you learn how to use it, you won’t have to use Denavit-Hartenberg or any other advanced mathematical knowledge.\n\nAnd, if you continue looking, you’ll soon find the Moveit library from ROS. This library allows you to specify your robot parameters (distances between joints, types of joints, etc) in a single XML representation called URDF: Unified Robot Description Format. Then Moveit will use the URDF to compute inverse kinematics.\n\nNot only that, it will also do complete path and motion planning for you! So you get even more stuff than what you’ve asked.\n\nSearching for libraries instead of learning the required mathematics is a great solution if you want to develop faster, especially for a small project or prototype. In fact, I’d advise you to use libraries even if you have the mathematical knowledge. This will save you some time in the short term anyway.\n\n## Where do you need mathematics\n\nEven if you can use libraries that hide the mathematical knowledge, mathematics are still everywhere in robotics.\n\nAnd if you want to really get serious in programming robots, you’ll eventually have to learn some maths, and know how to translate the maths into code.\n\nSometimes, a library will not do exactly what you want. Or, the license of the library will be a problem for your project. Or simply, the library is just an overkill for your application, because the mathematical problem you have is maybe not so hard to solve.\n\nHere is a non-exhaustive list of where you’ll find mathematics in robotics:\n\n• Kinematics: includes forward and inverse kinematics. This is especially useful for robotic arms.\n• Velocity and acceleration: if your robot is moving (which is probably the case), you’ll need to know how to compute a velocity from a position data, and how to compute an acceleration (and vice versa). To go even further, I could add the computation of the jerk, which represents the variation in acceleration and can be very important for smooth movements.\n• Path planning: which path should the robot take to reach the destination? How to optimize this path?\n• Motion planning: given a path, which velocity and acceleration should you apply to each joint of the robot at any time? And how do you ensure the max velocity constraints can be respected?\n• Angles: you’ll need to know how to switch from degrees to radians, how to switch from Euler angles to a quaternion, etc.\n• PID control: PIDs are often used to control motors and some actuators. This control system is full of maths.\n• Interpolation: given a set of points, you’ll often have to interpolate between them, using a polynomial expression for example.\n• Machine learning: well I won’t go into much details here, but as you can guess, this is also full of mathematics.\n• Image processing: here you’ll need at least solid geometry basics.\n• Logical reasoning: if you study logic in mathematics, this will help you a lot in programming, whether you program robots or not.\n\nIf you think this list is long, well, I’m sorry to say this is maybe less than 10% of all the maths you’ll come across when programming robots! And if you ask someone else with a different background than me, he/she will probably come up with a totally different list.\n\n## What robotics programmer do you want to be?\n\nAs you saw in this post, mathematics is everywhere in robotics. You’ll certainly have to learn some maths basics, but the overall required knowledge really depends on what you want to do.\n\nIf you want to develop web applications for robots, and not the robot itself, well in this case much of the mathematical knowledge listed before doesn’t apply to you.\n\nIf you want to develop low-level code, at the firmware level on micro-controllers, PID control and system control in general will be a must-have for you.\n\nAnd if you want to develop the core software of a robot – the decision algorithms to move the robot, how the robot moves its joints, etc – well in this case, you can’t escape mathematics. Of course you can (and should) start with some libraries to go easy and fast, but one day or another you’ll have to learn some maths.\n\nSo, before diving head first into robotics programming, make sure that you either have some knowledge in mathematics, or that you’re at least interested in maths.\n\nAnd, as you’ll see, it all seems very complicated until you finally understand and think: well that’s finally not so hard!\n\nWhat is your experience with mathematics and robotics? Which parts of mathematics did you struggled the most with?" ]
[ null ]
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http://promonet.ro/ecrustaceous1106953.html
[ "Check whether a directed graph is Eulerian\n\nAn Eulerian trail (or Eulerian path) is a path in a graph that visits every edge exactly once. Given a directed graph, check whether it has an Eulerian path or not.\n\nFind the minimum number of merge operations to make an array palindrome\n\nGiven a list of non-negative integers, find the minimum number of merge operations to make it a palindrome. A merge operation can only be performed on two adjacent elements. The result of a merge operation is that the two adjacent elements are replaced with their sum.\n\nConstruct a complete binary tree from its linked list representation\n\nGiven a linked list, construct a complete binary tree from it. Assume that the order of elements present in the linked list is the same as that in the complete tree’s array representation.\n\nFind read-write conflicts among given database transactions\n\nGiven a list of database transactions, find all read-write conflicts among them. Assume that there is no strict two-phase locking (Strict 2PL) protocol to prevent read-write conflicts.\n\nCheck if removing an edge can split a binary tree into two equal size trees\n\nGiven a binary tree, check if removing an edge can split it into two binary trees of equal size.\n\nIn-place merge two height-balanced BSTs\n\nGiven two height-balanced binary search trees, in-place merge them into a single balanced binary search tree. For each node of a height-balanced tree, the difference between its left and right subtree height is at most 1.\n\nPRO Scientific PRO-02-43340 Quick Connect, 43mm Diameter x 340mm\n\nGiven an array representing the parent-child relationship in a binary tree, find the tree’s height without building it. The parent-child relationship is defined by (A[i], i) for every index i in array A.\n\nDetermine whether two nodes lie on the same path in a binary tree\n\nGiven a binary tree and two tree pointers, x and y, write an efficient algorithm to check if they lie on the same root-to-leaf path in the binary tree. In other words, determine whether x is an ancestor of y, or x is a descendant of y.\n\nDetermine whether a BST is skewed from its preorder traversal\n\nGiven an array representing the preorder traversal of a BST, determine whether it represents a skewed BST or not. In a skewed BST, each node’s descendants are either smaller or larger than the node itself.\n\nFind total arrangements such that no two balls of the same color are together\n\nGiven r red, b blue, and g green balls, find the total number of arrangements in a row such that no two balls of the same color end up together.\n\nPrint all pairs of anagrams in a set of strings\n\nGiven a set of strings, print all pairs of anagrams together. Two strings, X and Y, are called anagrams if we can get a string Y by rearranging the letters of the string X and using all the characters of the string X exactly once.\n\nFind the smallest missing positive number from an unsorted array\n\nGiven an unsorted integer array, find the smallest missing positive integer in it." ]
[ null ]
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https://www.simplilearn.com/important-formulas-in-project-management-professional-pmp-article
[ "", null, "If you’re studying for the PMP® exam, you have probably already learned that you need to know some frequently used project management formulas—along with where to use them, how to use them, how to compute them, and most importantly, how to derive the values. In fact, many say that the most difficult part of the exam is learning all the PMP formulas.\n\n Are you a professional who is aspiring to be a project manager? Try answering this PMP Practice Preparation Questions and assess yourself.\n\nWe’ve put together a list of cost management formulas that you’ll need to know, along with a breakdown of how and when to use them.\n\nWatch a video on PMP Certification Training\n\n## Cost Management Knowledge Area PMP Formulas\n\nAlthough there are more than 25 project management formulas that you might need to tackle during the exam, there are a few cost management formulas that are very important, and which you’re likely to encounter more than once during the exam. Further, many of the calculation-based questions are based on these top 8 cost management formulas.\n\n 1 Cost Variance (CV) = Earned Value (EV) – Actual Cost (AC) 2 Schedule Variance (SV) = Earned Value (EV) – Planned Value (PV) 3 Cost Performance Index (CPI) = EV / AC 4 Schedule Performance Index (SPI) = EV / PV 5 EAC = AC + Bottom-up ETC 6 EAC = BAC / Cumulative CPI 7 EAC = AC + (BAC – EV) 8 EAC = AC + [BAC – EV / (Cumulative CPI ´ Cumulative SPI)]\n\n## Formulas 1 – 4\n\nTake a look at the first four formulas above and try to find out the commonalities in them. Not getting it yet? Yes, the easiest part is Earned Value (EV). It appears above in all the formulas, which means you have to derive the values of cost variance, schedule variance, cost performance index, and schedule performance index, keeping Earned Value in mind at first.\n\nEarned Value comes before any other value. Most importantly, if you are working cost-related questions; think about the actual cost with Earned Value. If the question is about a schedule, think about planned value along with the earned value. If it is a matter of variance, you need to subtract actual cost and planned value from earned value—depending on the situation.\n\nSimilarly, if it is a question of getting index values, actual cost and planned value will be divided from earned value. If it is a matter of cost performance index; actual cost will be divided from earned value and if it is scheduled performance index; the planned value will be divided from Earned Value. So, in all these circumstances, Earned Value plays a huge role, which is why it’s at the top of the list.\n\n## Formula 5\n\n 5 EAC = AC + Bottom-up ETC\n\nSince you will derive the estimate at completion, you need to focus on the actual costs incurred; only then can you obtain the future value you need for processing the project. See the above formula; it is used when the original estimate is fundamentally flawed. You use this formula to calculate an actual plus new estimate for the remaining work.\n\n## Formula 6\n\n 6 EAC = BAC / Cumulative CPI\n\nIf you were asked during the examination whether you are a good project manager, working on the project as planned—i.e., are you able to maintain positive values in both CPI and SPI—in this case, you would use the above-mentioned formula. This formula is used when the original estimation is met without any deviation.", null, "## Formula 7\n\n 7 EAC = AC + (BAC – EV)\n\nIf you find yourself in bad shape during the project execution and have incurred more money on the project than expected or planned, use this formula to calculate the estimate at completion value. Again, your actual cost will be used first.\n\n## Formula 8\n\n 8 EAC = AC + [BAC – EV / (Cumulative CPI ´ Cumulative SPI)]\n\nThis formula is used to calculate actual to date plus the remaining budget changed based on performance—used when we believe the current ratio is typical as planned. In order to meet the schedule as decided earlier, we calculate the EAC accordingly to meet that schedule.\n\n## Conclusion\n\nIn order to best decide which formula to use and where to make sure you’re reading the question carefully and consider the hypothetical situation, a project manager would be in when faced with this sort of problem.\n\nIn addition to these important cost management formulas, you’ll want to stay current with any updates on the Project Management Institute website. Simplilearn offers online training for the PMP certification that delivers hands-on projects in scope management, time and cost management, and risk assessment, designed to prepare you as much as possible for the PMP® exam.\n\nPMP is a registered mark of the Project Management Institute, Inc.", null, "Simplilearn" ]
[ null, "https://www.simplilearn.com/ice9/free_resources_article_thumb/The-Top-8-Formulas-to-Memorize-Before-Your-PMP-Exam.jpg", null, "https://www.simplilearn.com/ice9/assets/form_opacity.png", null, "https://www.simplilearn.com/important-formulas-in-project-management-professional-pmp-article", null ]
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https://electronics.stackexchange.com/questions/338300/can-someone-explain-what-this-line-means-in-the-code-for-a-d-flip-flop-written-i
[ "# Can someone explain what this line means in the code for a D Flip Flop written in Verilog?\n\nmodule dflipflop (data ,clk , reset ,q);// Code for Asynchronous Positive Edge triggered D flip flop\ninput data, clk, reset ;\noutput q;\nreg q;\nalways @ ( posedge clk or negedge reset)\nif (~reset) begin //what does this block of code mean?\nq <= 1'b0 // particularly this line\nend else begin\nq <= data; // and this one\nend//\nendmodule\n\n\nI am new to learning Verilog, and I have to learn the codes for the various types of flip-flops. However, I haven't been able to understand this one entirely and what it means.\n\nFor instance, as the D flip-flop is positive edge triggered, hence we write posedge clock and it has an asynchronous reset input apart from the normal D input.\n\nBut, what I do not understand is the use of the <= operator in the highlighted lines and what is being done there. Does it mean q is being assigned a value less than zero? What does data variable refer to in the other line, and what exactly does the line mean as well?\n\n• The <= means it is synchronous to the clock. Nov 6, 2017 at 8:02\n• Okay. So it means the output 'q' of the flip-flop is formed synchronously and that if reset is zero, then output 'q' becomes zero. Nov 6, 2017 at 8:05\n• No, it doesn't mean that it's \"synchronous to the clock\". Look up \"non blocking assignment\". NBAs handle potential race conditions in your code.\n– EML\nNov 6, 2017 at 8:40\n\nFirst of all, the <= is a type of assigning value to the variable. It doesn't mean less than; instead, the value zero is assigned to variable q when the condition is met.\n\nSummary of Verilog syntax:\n\nhttp://ee.sut.ac.ir/People/Courses/142/Summary%20of%20Verilog%20Syntax.pdf\n\nif(~reset) - this means the condition is fulfilled when reset = 0 (~ is a bitwise negation operator, check the above link in the operator section), meaning when reset is zero, the statement q<=1'b0 is executed; otherwise, the input is passed to output which is given by q<=data. This is the functionality of a D flip-flop.\n\n<=\n\n\nis a non-blocking assignment operator used to execute the code or pass the values in concurrently (in parallel). This means that all the values are passed simultaneously, no matter the order in which the values are passed into the signal.\n\nThis is in contrast to\n\n=\n\n\noperator in which the values are passed sequentially.\n\nConsider this code\n\nmodule test;\n\nint a=4 , b=0 , c=0;\n\ninitial begin\na<=10;\nb<=a;\nc<=a;\n\n$display(\"a=%0d b=%0d c=%0d \\n\",a,b,c) ; //Here a=4 b=0 c=0 // and the values are assigned // to the variables in the next cycle. You can //check this out by using the always statement end initial begin a=10; b=a; c=a;$display(\"a=%0d b=%0d c=%0d \\n\",a,b,c) ; //Here a=10 b=10 c=10\n\nendmodule\n\n• Are you sure you mean \"sequentially\" and not \"serially\"? If it isn't parallel then it's serial. Nov 6, 2017 at 14:47\n• Well, Sequential execution refers to a statement being executed only after its preceding (or one or more key fields) has done so and serial execution strictly refers to execution after its perceding statement. So, if I'd have to be precise, I'd refer to it as time-sequential or or order-of-occurence sequential. Nov 7, 2017 at 4:58" ]
[ null ]
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https://docs.appian.com/suite/help/19.4/fnc_trigonometry_radians.html
[ "Converts the measure of the specified angle from degrees to radians.\n\n## Syntax\n\nangle_in_degrees: (Decimal) An angle measure that will be converted into radians.\n\n## Returns\n\nDecimal\n\nThis function can only be used for values between 0 and 2π (~6.286).\n\n## Examples\n\nYou can experiment with this function in the test box below.\n\nTest Input\n\n`radians(180)` returns `3.141592653589793`\n\nOpen in Github Built: Thu, Oct 14, 2021 (02:42:55 PM)" ]
[ null ]
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https://sketches89.neocities.org/view-find-the-gradient-vector-field-f-of-f-and-sketch-it-f-x-y-5-x2-y2-png.html
[ "", null, "View Find The Gradient Vector Field ∇F Of F And Sketch It. F(X, Y) = 5 X2 + Y2 PNG\n\n# View Find The Gradient Vector Field ∇F Of F And Sketch It. F(X, Y) = 5 X2 + Y2 PNG\n\nF(x,y)start bold text, f, end bold text, left parenthesis, x, comma, y, right parenthesis is called a conservative vector field if it satisfies any one.\n\nView Find The Gradient Vector Field ∇F Of F And Sketch It. F(X, Y) = 5 X2 + Y2 PNG. Given 𝑓(𝑥, 𝑦) = 𝑥 + 2𝑦, find 𝐅(𝑥, 𝑦) = ∇𝑓 and sketch it along with the contour map of 𝑓. Find the length of ∇f(x,y) using equation (2).", null, "Out Of Distribution Generalization Via Risk Extrapolation Rex Arxiv Vanity from media.arxiv-vanity.com If the vector that is given for the direction of the derivative is not a unit vector, then it is only necessary to divide by the norm of the vector. Find the corresponding function f. F(x, y) = 5sqrt(x^2 + y^2).\n\n### On january 1, 2011, frog corporation sold a \\$2,000,000, 10 percent bond issue (8.5 percent market.\n\nLet f be any vector field of the form f(x,y, z) = f (x) i+g(y) j+h(z)k and let g be any vector field of the form g(x,y, z) = f (y, z) i+g(x, z) j+h(x,y)k. The gradient is also shown. Iii 5 iv 5 4 find the gradient vector field of f. %matplotlib inline import matplotlib.pyplot as plt import sympy as sp import numpy as np." ]
[ null, "https://sstatic1.histats.com/0.gif", null, "https://media.arxiv-vanity.com/render-output/3377291/figures/grad_vector_fields.png", null ]
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https://lists.isocpp.org/std-proposals/2021/10/3192.php
[ "Constructor ambiguity: Uniform initialization vs. initializer lists\n\nFrom: Gawain Bolton <gawain.bolton_at_[hidden]>\nDate: Tue, 05 Oct 2021 14:11:40 +0200\nHello,\n\nI would like to report what I will call \"constructor ambiguity\" for\nclasses which have multiple constructors, one of which have takes an\ninitializer list.\n\nThe ambiguity is for us humans, not the compiler, and is due to the two\nthings:\n1. The same syntax is used for uniform initialization and\ninitializer lists.\n2. Any constructor taking an initializer list is preferred when\nbraces are used.\n\nFor example:\n\nstd::string sa(32, 'A'); // Creates a string of 32 characters i.e. \"AAAAAAAAAAAAAAAAAAAAAAAAAAAAAAAA\"\nstd::string sb{32, 'A'}; // Creates a string of 2 characters i.e. \" A\"\n\nstd::vector<int> va(10, -1); // Creates a vector of 10 elements, each one initialized to -1\nstd::vector<int> vb{10, -1}; // Creates a vector of 2 elements (10 and -1)\n\nThe code looks very similar and yet the results are very different.\nThis is unfortunate because uniform initialization is preferred\nespecially as it can avoid bugs due to unintential casts and\ntruncation/narrowing of values.\n\nI find this ambiguity unnecessary as if the intent is to provide an\ninitializer list, then this can be done explicitly:\nstd::vector<int> vb1({10, -1}); // Creates a vector of 2 elements (10 and -1)\nstd::vector<int> vb2{{10, -1}}; // Creates a vector of 2 elements (10 and -1)\n\nThis preference to use a constructor taking an initializer list can\neasily break code if such a constructor is added at a later date. For\nexample:\n\nstruct A {\nexplicit A(int);\n};\n\nA a{2}; // Create an object a of type A\n\nThen later on an initializer list constructor is added:\n\nstruct A {\nexplicit A(int);\nA(const std::initializer_list<int>&)\n};\n\nNow the call to create object 'a' will use the constructor taking an\ninitializer list which, of course, can do something completely\ndifferent. It could be extremely difficult to find why there was such\na change in behaviour.\n\nI apologize but I do not know if this has already been mentioned or\naddressed. If not, what do you think of this? Is this considered to\nbe one of the many idioms of C++?\n\nGawain Bolton" ]
[ null ]
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http://docs.go-mono.com/monodoc.ashx?link=M%3ASystem.Double.Equals(System.Object)
[ "System.Double.Equals Method\n\nReturns a value indicating whether this instance is equal to a specified object.\n\n## Syntax\n\npublic override bool Equals (object obj)\n\n#### Parameters\n\nobj\nAn object to compare with this instance.\n\n#### Returns\n\ntrue if obj is an instance of double and equals the value of this instance; otherwise, false.\n\n## Remarks\n\nThe double.Equals(double) method should be used with caution, because two apparently equivalent values can be unequal due to the differing precision of the two values. The following example reports that the double value .3333 and the double returned by dividing 1 by 3 are unequal.\n\ncode reference: System.Double.Epsilon#3\n\nFor alternatives to calling the double.Equals(object) method, see the documentation for the double.Equals(double) overload.\n\nNote:\n\nBecause double.Epsilon defines the minimum expression of a positive value whose range is near zero, the margin of difference between two similar values must be greater than double.Epsilon. Typically, it is many times greater than double.Epsilon.\n\nThe precision of floating-point numbers beyond the documented precision is specific to the implementation and version of the .NET Framework. Consequently, a comparison of two particular numbers might change between versions of the .NET Framework because the precision of the numbers' internal representation might change.\n\nIf two double.NaN values are tested for equality by calling the double.Equals(double) method, the method returns true. However, if two double.NaN values are tested for equality by using the equality operator, the operator returns false. When you want to determine whether the value of a double is not a number (NaN), an alternative is to call the double.IsNaN(double) method.\n\n## Requirements\n\nNamespace: System\nAssembly: mscorlib (in mscorlib.dll)\nAssembly Versions: 1.0.5000.0, 2.0.0.0, 4.0.0.0" ]
[ null ]
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https://socratic.org/questions/how-do-you-calculate-r-squared-by-hand#149476
[ "# How do you calculate r squared by hand?\n\nMay 31, 2015\n\nAssuming this is a general question and not a reference to some undeclared statistical equation,\n\nand assuming you know how to multiply two numbers together by hand,\n\nthen $r$ squared (often written ${r}^{2}$) is simply\n$\\textcolor{w h i t e}{\\text{XXXXX}}$$r \\times r$ for whatever the value of $r$ is\n\nFor example if $r = 16$\nthen $r$ squared (or ${r}^{2}$) $= 16 \\times 16 = 256$\n\nHowever I suspect you had some specific statistical relationship in mind; please resubmit with explicit references if this is the case.\n\n${r}^{2} = 1 - \\frac{S {S}_{E r r}}{S {S}_{T o t}}$\n\n#### Explanation:\n\nThe $S {S}_{E r r}$ or the sum of squares residuals is:\n$\\setminus \\sum {y}_{i}^{2} - {B}_{0} \\setminus \\sum {y}_{i} - {B}_{1} \\setminus \\sum {x}_{i} {y}_{i}$\nor\nsimply the square of the value of the residuals. The residual value is difference between the obtained y-value and the expected y-value. The expected y-value is the calculated value from the equation of line/plane.\n\nFor example, for a system with 1 unknown parameter/variable x, the calculated y-value would be the sum of ${B}_{0} \\mathmr{and} {B}_{1} x$ (i.e. $Y = {B}_{0} + {B}_{1} x$).\n\nFor a system with 2 unknown parameters/variables, ${x}_{1}$ and ${x}_{2}$, the calculated y-value would be the sum of ${B}_{0}$, ${B}_{1} x$, and ${B}_{2} {x}_{2}$ (i.e. $Y = {B}_{0} + {B}_{1} {x}_{1} + {B}_{2} {x}_{2}$).\n\nAnd in general, $Y = {B}_{0} + {B}_{1} {x}_{1} + {B}_{2} {x}_{2} + {B}_{3} {x}_{3} + {B}_{4} {x}_{4} + \\ldots + {B}_{n} {x}_{n}$\n\nFurthermore, the $S {S}_{T o t} = \\setminus \\sum {y}_{i}^{2} - \\frac{{\\left(\\sum {y}_{i}\\right)}^{2}}{n}$ where $n$ is the number of observations or trials." ]
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https://www.convertunits.com/from/ton/square+inch+%5Blong%5D/to/centibar
[ "## ››Convert ton/square inch [long] to centibar\n\n ton/square inch [long] centibar\n\n Did you mean to convert ton/square inch [long] ton/square inch [short] to centibar\n\nHow many ton/square inch [long] in 1 centibar? The answer is 6.4748990181794E-5.\nWe assume you are converting between ton/square inch [long] and centibar.\nYou can view more details on each measurement unit:\nton/square inch [long] or centibar\nThe SI derived unit for pressure is the pascal.\n1 pascal is equal to 6.4748990181794E-8 ton/square inch [long], or 0.001 centibar.\nNote that rounding errors may occur, so always check the results.\nUse this page to learn how to convert between tons/square inch and centibars.\nType in your own numbers in the form to convert the units!\n\n## ››Quick conversion chart of ton/square inch [long] to centibar\n\n1 ton/square inch [long] to centibar = 15444.25631 centibar\n\n2 ton/square inch [long] to centibar = 30888.51261 centibar\n\n3 ton/square inch [long] to centibar = 46332.76892 centibar\n\n4 ton/square inch [long] to centibar = 61777.02523 centibar\n\n5 ton/square inch [long] to centibar = 77221.28154 centibar\n\n6 ton/square inch [long] to centibar = 92665.53784 centibar\n\n7 ton/square inch [long] to centibar = 108109.79415 centibar\n\n8 ton/square inch [long] to centibar = 123554.05046 centibar\n\n9 ton/square inch [long] to centibar = 138998.30676 centibar\n\n10 ton/square inch [long] to centibar = 154442.56307 centibar\n\n## ››Want other units?\n\nYou can do the reverse unit conversion from centibar to ton/square inch [long], or enter any two units below:\n\n## Enter two units to convert\n\n From: To:\n\n## ››Definition: Centibar\n\nThe SI prefix \"centi\" represents a factor of 10-2, or in exponential notation, 1E-2.\n\nSo 1 centibar = 10-2 bars.\n\nThe definition of a bar is as follows:\n\nThe bar is a measurement unit of pressure, equal to 1,000,000 dynes per square centimetre (baryes), or 100,000 newtons per square metre (pascals). The word bar is of Greek origin, báros meaning weight. Its official symbol is \"bar\"; the earlier \"b\" is now deprecated, but still often seen especially as \"mb\" rather than the proper \"mbar\" for millibars.\n\n## ››Metric conversions and more\n\nConvertUnits.com provides an online conversion calculator for all types of measurement units. You can find metric conversion tables for SI units, as well as English units, currency, and other data. Type in unit symbols, abbreviations, or full names for units of length, area, mass, pressure, and other types. Examples include mm, inch, 100 kg, US fluid ounce, 6'3\", 10 stone 4, cubic cm, metres squared, grams, moles, feet per second, and many more!" ]
[ null ]
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https://it.scribd.com/book/271630948/Fundamental-Formulas-of-Physics-Volume-Two
[ "## Trova il tuo prossimo libro preferito\n\nAbbonati oggi e leggi gratis per 30 giorni", null, "# Fundamental Formulas of Physics, Volume Two\n\nvalutazioni:\n3/5 (5 valutazioni)\nLunghezza:\n744 pagine\n7 ore\nPubblicato:\nFeb 21, 2013\nISBN:\n9780486165943\nFormato:\nLibro\n\n## Descrizione\n\nThe republication of this book, unabridged and corrected, fills the need for a comprehensive work on fundamental formulas of mathematical physics. It ranges from simple operations to highly sophisticated ones, all presented most lucidly with terms carefully defined and formulas given completely. In addition to basic physics, pertinent areas of chemistry, astronomy, meteorology, biology, and electronics are also included.\nThis is no mere listing of formulas, however. Mathematics is integrated into text, for the most part, so that each chapter stands as a brief summary or even short textbook of the field represented. The book, therefore, fills other needs than the primary function of reference and guide for research. The student will find it a handy review of familiar fields and an aid to gaining rapid insight into the techniques of new ones.\nThe teacher will study it as a useful guide to a broad concept of physics. The chemist, astronomer, meteorologist, biologist, and engineer will not only derive valuable aid from their special chapters, but will understand how their specialty fits into the large scheme of physics.\nVol. 1 chapter titles: Basic Mathematical Formulas, Statistics, Nomograms, Physical Constants, Classical Mechanics, Special Theory of Relativity, The General Theory of Relativity, Hydrodynamics and Aerodynamics, Boundary Value Problems in Mathematical Physics, Heat and Thermodynamics, Statistical Mechanics, Kinetic Theory of Gases: Viscosity, Thermal Conduction, and Diffusion, Electromagnetic Theory, Electronics, Sound and Acoustics.\nVol. 2 chapter titles: Geometrical Optics, Physical Optics, Electron Optics, Molecular Spectra, Atomic Spectra, Quantum Mechanics, Nuclear Theory, Cosmic Rays and High-Energy Phenomena, Particle Accelerators, Solid State, Theory of Magnetism, Physical Chemistry, Basic Formulas of Astrophysics, Celestial Mechanics, Meteorology, Biophysics.\n\nPubblicato:\nFeb 21, 2013\nISBN:\n9780486165943\nFormato:\nLibro\n\nBOOKS\n\n## Chapter 16\n\nGEOMETRICAL OPTICS\n\nBY JAMES G. BAKER\n\nResearch Associate of Harvard College Observatory,\n\n#### 1. General Considerations\n\n1.1. Geometrical optics and wave optics. Light energy is propagated through an optical instrument in the form of a wave motion. Nevertheless, as a consequence of several important theorems, we can, for many purposes, regard light as traversing homogeneous isotropic media in straight lines. In heterogeneous isotropic media light is propagated as a normal congruence of rays in which the direction of motion lies along the normal to the wave front at any given point. In the most general case, i.e., heterogeneous anisotropic media, the direction of motion may be inclined to the wave front. By dealing with a geometry of lines rather than of waves, one can achieve considerable simplification. From this point of view the true wave nature of light enters as a necessary correction to the results of geometrical optics.\n\n1.2. Media. Light travels through a vacuum in straight lines at a constant velocity irrespective of color. In material media the speed of light changes to a smaller value and becomes dependent on color. In the process the frequency v and hence the quantum energy hv remain unchanged. The effect of a medium on light is usually characterized by the index of refraction, which in the most general case is a function of position, direction, and frequency.\n\n1.3. Index of refraction. Let n be the index of refraction, c the velocity of light in vacuo, and υ the velocity of light in the medium. Then\n\n(1)\n\nwhere λ′ is the wavelength in the medium.\n\n(2)\n\nfor successive media; n = 1 for a vacuum.\n\n1.4. Interfaces. Various kinds of physical media exist. Those of most general use are the transparent homogeneous isotropic substances, which include glass, synthetic resins, cubic crystals, etc. The most usual kinds of anisotropic media in optical applications come from uniaxial and biaxial crystals. Strain introduced mechanically or electrically may alter isotropic substances into anisotropic media.\n\nBecause of the physical nature of media, there must exist boundaries or interfaces between media. When this interface is a matte surface, the resulting reflection of light is called diffuse. When the interface is smooth and continuous, the resulting reflection or refraction of light is termed regular or sometimes specular.\n\nOne should note that the physical properties of material media are all a function of temperature. In detailed calculations the effect of temperature must be considered. One should also note that the usual optical instrument is immersed in air, and that the observed indices of refraction of optical glass and crystals are often referred to air under designated conditions.\n\n1.5. Refraction and reflection. The Fresnel formulas. When a ray of light passes from one medium into another at a smooth interface, the light energy divides into two parts, one a reflected ray, and the other a refracted ray. Within a narrow region of disturbance on each side of the interface, secondary wavelets are formed in the backward direction, and a certain amount of energy is returned to the first medium as the reflected ray. The remaining energy goes into the refracted ray in the second medium. Both transmitted and reflected rays are partially polarized in a manner dependent on the angle of incidence and on the angle of refraction, which are the angles between the ray and normal in the respective media. (Cf. § 1.13.)\n\nFor light polarized in the plane of incidence (magnetic vector in the plane of incidence)\n\n(1)\n\nand for light polarized in a plane perpendicular to the plane of incidence\n\n(2)\n\nwhere I is the intensity of the reflected beam, and I0 the intensity of the incident beam.\n\nWhen the light is unpolarized\n\n(3)\n\nFor normal incidence whether the light is polarized or unpolarized\n\n(4)\n\nThis formula may be used as an approximation for unpolarized light up to as much as 50 degrees off the normal.\n\nAt Brewster’s angle, defined by i = tan−1 n′ln, the intensity of the reflected light vanishes for light polarized in a plane perpendicular to the plane of incidence, i.e., tan² (i + r) = ∞. For unpolarized incident light at Brewster’s angle, the intensity of the reflected light, which is now 100 % polarized with its electric vector perpendicular to the plane of incidence, becomes\n\n(5)\n\nIf the incident light is already 100 % polarized at Brewster’s angle,\n\n(6)\n\nIn the latter case for n′/n = 1.5, I ~ 15 % of I0. For n′/n = 1.8, I ~ 28% of I0.\n\n1.6. Optical path and optical length. Consider a curve S through any medium, either homogeneous or heterogeneous, along which light is known to travel between points z1 and z2. The time of transit of the light is given by the line integral\n\n(1)\n\nor\n\nThe length L is called the optical length of the path, as opposed to\n\nwhich is the geometrical length; L is equal to the geometrical length the light would have traveled in a vacuum in the same time interval.\n\nIn a homogeneous medium a geometrical length s has an associated optical length L = ns. Where light travels through a succession of discrete homogeneous media,\n\nwhere s is the straight line distance along the path between interfaces.\n\n1.7. Fermat’s principle. Light passing through a medium follows a path for which the optical length or time of transit is an extremum, i.e., independent of first-order iefinitesimal variations of path. The time is said to have a stationary value, and usually is either a maximum or minimum.\n\n(1)\n\nwhere n is a function of the space coordinates. Similarly,\n\n(2)\n\ndefines the particular path between z1 and z2. For discrete media\n\n(3)\n\n1.8. Cartesian surfaces and the theorem of Malus. Consider a meridian cut C of an interface. The surface C is to be so chosen that for every point on it in 3-space, L = ns + ns′ = constant between a given point P in the first medium of index n and P′ in the second medium of index n′. This surface clearly satisfies δL = 0 and the higher order differentials are all zero. Hence any ray emitted by P1 that strikes C will find its way through P′. Hence P′ is an image point of the object point P.\n\nFor a single ray originating at P and refracted through P′ by a refracting surface S, where P′ is not necessarily an image point, a Cartesian surface C may be considered tangent to S at the point of intersection of the retracted ray with S. By simple construction one can then determine whether the higher order differentials of a neighboring path between P and P′ are positive or negative with respect to C where they are zero. If the curve S is more convex than C toward the less dense medium, L will be found to be a maximum.\n\nTheorem of Malus. A system of rays normal to a wave front remains normal to a wave front after any number of refractions and reflections. That is, a normal congruence remains a normal congruence.\n\nThe combined principles of Fermat and Malus lead to the conclusion that for conjugate foci\n\nis a constant between object and image points, irrespective of the ray.\n\nA Cartesian surface holds for a point object, point image, and a single interface, defined by ns + n′s′ = constant. Where reflection is involved, the surface is of the second degree and is therefore a conic section. For refraction the Cartesian surface is of the fourth degree, and its meridian cut is called the Cartesian oval. When one point lies at infinity, the surface degenerates into a second degree surface.\n\n1.9. Laws of reflection. Let λ, μ, ν be the direction cosines of a ray before reflection by a surface S, and λ′, μ′, v′ the direction cosines of the reflected ray. From the variation principle one can show that\n\n(1)\n\nor\n\n(2)\n\nwhere l, m, n are the direction cosines of the normal to S at the point of reflection of the ray. Also\n\n(3)\n\n(4)\n\nwhere D is the deviation.\n\n(5)\n\nThe reflected ray therefore lies in the plane of the normal and incident ray\n\n1.10. Laws of refraction. Let λ, μ, ν be the direction cosines of a ray before refraction by a surface S, And λ′, μ′, ν′ the direction cosines of the refracted ray. Again from the variation principle one can show that\n\n(1)\n\nor\n\n(2)\n\nwhere l, m, n are the direction cosines of the normal to S at the point of refraction. Also\n\n(3)\n\n(4)\n\n(5)\n\nwhere D is the deviation.\n\ncos D", null, "λλ′\n\n(6)\n\n1.11. The fundamental laws of geometrical optics\n\nThe law of the rectilinear propagation of light\n\nThe law of mutual independence of the component parts of a light beam\n\nThe law of regular reflection\n\nThe law of regular refraction\n\n1.12. Corollaries of the laws of reflection and refraction\n\na. The incident and reflected rays are equally inclined to any straight line tangent to the surface at the point of incidence.\n\nb. The projections of the incident and reflected rays upon any plane containing the normal make equal angles with the normal.\n\nc. n cos θ = n′ cos θ′, where θ is the angle between the ray and any tangent line.\n\nd. n sin ψ = n′ sin ψ′, where ψ is the angle between the ray and any normal plane. section 5.)\n\n1.13. Internal reflection, and Snell’s law. The relation\n\n(1)\n\nis called the optical invariant, and also Snell’s law after its discoverer. The relationship is valid in the common plane containing the incident and refracted rays and the normal, and follows from § 1.10 above. Note (d) under § 1.12 that a similar relation exists for the oblique refractions.\n\nWhere n′/n > 1 and sin r > n/n′, no solution exists for i. This is the case of internal reflection at the interface. The light energy remains 100 % in the same medium and obeys the laws of reflection.\n\n1.14. Dispersion at a refraction\n\n(1)\n\nIf di = 0 (entrant white light)\n\n(2)\n\nFor air-glass where dn = 0,\n\n(3)\n\nFor glass-air where dn′ = 0,\n\n(4)\n\nwhere i and r are, respectively, the angles of incidence and refraction in the direction of travel of the light. Subsequent refractions determine the final effect for a system as a whole.\n\n1.15. Deviation\n\na. Reflection\n\n(1)\n\nIf two mirrors are separated by the angle α and the light strikes each in turn,\n\n(2)\n\nb. Refraction\n\n(3)\n\nAt a glass-air surface and normal incidence,\n\n(4)\n\nAt a glass-air surface and i = 30°,\n\n(5)\n\nAt an air-glass surface and normal incidence,\n\n(6)\n\nAt an air-glass surface and i = 30°,\n\n(7)\n\nAt an air-glass surface and i = 90°,\n\n(8)\n\nHowever, the final effect of a deviation depends on the subsequent refractions, as determined by magnification factors along the particular ray. The deviation increases numerically with the angle of incidence at a refraction, a fact that is a direct cause of difficulties in the design of optical systems.\n\n#### 2. The Characteristic Function of Hamilton (Eikonal of Bruns)\n\n¹\n\n2.1. The point characteristic, V. Here V is defined as the optical path between points x, y, z and x′, y′, z′ in a heterogeneous medium, i.e.,\n\n(1)\n\nIf both end points of the path are varied, and if n and n′ are the indices of refraction in the infinitesimal neighborhood of x, y, z and x′, y′, z′, respectively\n\n(2)\n\nor\n\n(3)\n\nand\n\n(4)\n\nSimilarly, if V is defined as the total optical path between a point x, y, z in an initial medium n and a point x′, y′, z′ in a final medium n′, the above equations continue to apply. The intermediate path may traverse a succession of heterogeneous or discrete homogeneous media, or both.\n\nThus V is a function of 12 quantities (x, y, z, λ, μ, v, x′, y′, z′, λ′, μ′, v′) not all of which are independent. Given any five, we can compute the other five from the above equations.\n\nThe importance of the use of V is that the physical instrument is now replaced by a mathematical function V, and the behavior of the instrument by the partial derivatives of V. Knowing the characteristic, one can compute the performance; knowing the performance, one can compute a characteristic containing only a set of constants to be evaluated for a given instrument of that performance. Where x, y, z is a point source, one has precise information for investigation of the character of the image when V is known.\n\nComputation of V. Let Fi(xi; yi, zi) = 0 be the equation of the general surface of the instrument separating various homogeneous media. Then the general optical path L becomes\n\n(5)\n\nOn application of Fermat’s principle, δL = 0,\n\n(6)\n\nAlso, because variations in xi, yi, zi are confined to the surface Fi(xi, yi,zi) = 0,\n\n(7)\n\nIf the intermediate points are to be independent of one another, then\n\n(8)\n\nThese 4(N − 1) equations yield the 4(N - 1) quantities xi, yi, zi, Ji· When substituted in L, these quantities yield the relation\n\n(9)\n\nThe course of the analytic ray is thus defined.\n\n2.2. The mixed characteristic, W. Here W is defined as the total optical path between the point x, y, z in the initial medium n and the foot of the perpendicular dropped from the origin of coordinates onto the final ray in medium n′.\n\n(1)\n\nFrom application of the variational principle\n\n(2)\n\nThus, given x, y, z (source point) and μ′, ν′, the direction of any ray in the final medium, we can obtain at once the equation of that ray in the final medium from the partials of W.\n\nThen W may be computed in a fashion quite similar to the method used for computing V above. Because W involves fewer unknowns, its calculation is not as difficult as that for V.\n\n2.3. The angle characteristic, T\n\na. Here T is defined as the total optical path between the foot of the perpendicular dropped onto the initial ray from the origin of coordinates in the first medium n to the foot of the perpendicular dropped onto the final ray from the origin in the final medium n′.\n\n(1)\n\nFrom application of the variational principle\n\n(2)\n\nThus, if μ, v, μ′, v′ are assigned, the initial and final rays are known.\n\nThe calculation of T proceeds by application of the variational principle to each pair of adjacent media, inasmuch as the final ray for medium i − 1 becomes the initial ray for the medium i.\n\nThus\n\n(3)\n\n(4)\n\nfor the system as a whole. The T function is not in its final form until it becomes T(μ, ν, μ′, ν′).\n\nb. Translation of origin. The value of T is dependent on the choice of origin. If Tnew is to be calculated for a new origin, we have\n\n(5)\n\nwhere a, b, and c are the coordinates of the new origin in the old system.\n\nc. The value of T for a spherical surface. Let\n\n(6)\n\nThen\n\n(7)\n\nwhere the origin lies at the center of the sphere. A change of origin may be introduced from b. above. The choice of sign depends on the sense of curvature of R, with T reckoned positive from left to right.\n\nd. The value of T for a paraboloid of revolution. Let\n\n(8)\n\n(9)\n\n(10)\n\nif the variation takes place on the surface F(x,y,z) = 0.\n\n(11)\n\n(12)\n\n(13)\n\n(14)\n\n(15)\n\ne. The value of T for a general ellipsoid. Let\n\n(16)\n\n(17)\n\n(18)\n\n(19)\n\n(20)\n\nand similarly for other second-degree solids.\n\n2.4. The sine condition of Abbe. An identity among the second partial derivatives of the characteristic function leads to an important general relation that must be satisfied if an elementary surface around a point source is to be imaged accurately into a corresponding elementary surface around the image point. We confine ourselves to an axial source point in an instrument with rotational symmetry.\n\nIf we have precise imagery irrespective of the initial ray, then y′ = my and z′ = mz, where m is the magnification.\n\n(1)\n\nIf we consider that all rays from the object point combine in the image point, and that the elementary surface and its image are perpendicular to the axis, W is a function W(y, z, μ′, v′) and y′, z′, μ, and v become dependent variables from the above relations. We have\n\n(2)\n\n(3)\n\n(4)\n\nbecause of rotational symmetry.\n\nThen\n\n(6)\n\n(7)\n\nwhere the constant of integration is zero because the angles vanish together.\n\nIf θ and θ′ are the respective slope angles of a ray from the object point to the image point,\n\n(8)\n\nwhich is known as the sine condition of Abbe. The relationship can also be derived from general principles of thermodynamics.\n\n2.5. Clausius’ equation.", null, "inclined at an angle ϕ to the plane normal to the axis of a pencil at P1, of angular half aperture θ (Fig. 1). We wish to examine the conditions that will lead to a sharp image of the line element in image space, i.e., so that P2 will be sharply imaged.\n\nFIGURE 1", null, "", null, "can be regarded as a portion of another wave front inclined to the first at the angle θ.", null, "the optical length of which must be preserved in the final medium if the inverse construction is to produce a sharp image of the line element. Thus\n\n(1)\n\nThis condition was demonstrated by Clausius on the basis of energy considerations, and is useful in connection with off-axis images in rotationally symmetrical optical systems. The angle ϕ need not be in the plane of the paper.\n\n2.6. Heterogeneous isotropic media. Consider a curve in the medium connecting P to P′. Let the parametric equation of the curve be\n\n(1)\n\nThe optical length is\n\n(2)\n\n(3)\n\nwhere\n\n(4)\n\nIf we hold the end points fixed but vary the curve, we have\n\n(5)\n\n(5)\n\n(7)\n\nIntegration by parts gives\n\n(8)\n\nBecause the curves have fixed end points, the first term vanishes. If C is to be a stationary path, the value of L must be unchanged in the differential neighborhood of any point on the curve. δx, δy, and δz are completely arbitrary, and hence the coefficients must vanish under the integral all along the path. Accordingly,\n\n(9)\n\nor\n\n(10)\n\nIf u = s, the arc length along C,", null, "the above equations become\n\n(11)\n\n2.7. Collineation. A space continuum of points, line, and planes in object space that go into conjugate points, lines, and planes in image space in one to one linear correspondence is called a collineation.\n\nLet x, y, z be the coordinates of a point in object space and x′, y′, z′ its conjugate in image space with reference to right angle conjugated coordinate systems. Then\n\n(1)\n\nThis system can be inverted. If the relations were not rational, there would be no one-to-one relationship of object and image space. The denominator must have the same form in order that planes in object space go into planes in image space.\n\n(2)\n\n(3)\n\nThe inverted solution has the form\n\n(4)\n\nIf ax + βy + γz + δ = 0, then\n\n(5)\n\nAlso, if α′x′ + β′y′ + γ′z′ + δ′ = 0, then\n\n(6)\n\nIn the first case, αx + βy + γz + yz + δ = 0 determines a plane conjugate to the plane at infinity in image space. This plane is called the first focal plane and lies in object space. The plane α′x′ + β′y′ + γ′z′ + δ′ = 0 is called the second focal plane, and lies in image space. Parallel rays in object space will meet on this focal plane in image space.\n\nIn a centered lens system we can set z = z′ = 0 without loss of generality. The x axis becomes the optical axis. Thus for points on the axis\n\n(7)\n\nIntermediate images will be reducible to this form. If α = 0, the system is called telescopic. In this case\n\n(8)\n\nWhen α ≠ 0 but α = 1, x′x + δx′ αix δ1 = 0, which is of the form\n\n(9)\n\nA simple change of origin produces the relation xx′ = constant. Evidently, x and x′ are measured from the first and second focal points, respectively.\n\n#### 3. First Order Relationships\n\n3.1. Conventions. Unless specified otherwise for a particular set of equations, we adopt the following conventions, all in reference to a centered rotationally symmetrical optical system.\n\na. Light travels from left to right.\n\nb. An object distance is positive relative to a vertex when the object point lies to the left of the vertex.\n\nc. An image distance is positive when the image point lies to the right of the vertex.\n\nd. A radius of curvature is positive when the center of curvature lies to the right of the vertex.\n\ne. Slope angles are positive when the axis must be rotated counterclockwise through less than π/2 to become coincident with the ray.\n\nf. Angles of incidence and refraction are positive when the normal must be rotated counterclockwise through less than π/2 to bring it into coincidence with the ray.\n\ng. Distances are positive above the axis.\n\n3.2. Refraction at a single surface. The optical path between the source point and image point is simply ns + n′s′, where s and s′ are the object and image distances, respectively (Fig. 2). Any other paraxial ray from the source point must have the same total optical path to the image point in order that a focus shall exist.\n\nFIGURE 2\n\nIf a circle of radius s is described around the source point, and another circle of radius s′ is described around the image point, one sees that the optical paths of the sagittae must be equated in the following way. (The sagitta of an arc is the depth of the arc from the chord.)\n\n(1)\n\nfor the sagitta of a zone h and radius R. Then\n\n(2)\n\nor\n\n(3)\n\nFinally,\n\n(4)\n\nIt is of interest that if object and image distance are referred to the center of curvature, rather than to the vertex, we obtain an analogous formula,\n\n(5)\n\nin which the indices on the left become interchanged.\n\n3.3. Focal points and focal lengths. If s = ∞, we findn′/s′ = (n′ – n)/R. We define this distance s′ as the second focal length, which then is the distance from the vertex or pole of the surface to the second focal point, and denote this distance by f′.\n\nThen\n\n(1)\n\nSimilarly, if s′ = ∞, we call s the first focal length of the surface, which is the distance from the first focal point to the vertex of the surface, and denote this distance by f. Then\n\n(2)\n\nIt follows that\n\n(3)\n\n3.4. Image formation. If we consider the construction in Fig. 3, the ray from b passing through C must evidently go undeviated through the image point b′. Then\n\n(1)\n\nAlso,\n\n(2)\n\nor\n\n(3)\n\nwhere m is called the lateral magnification.\n\nFIGURE 3\n\n3.5. Lagrange’s law (Known variously as the Helmholtz-Lagrange formula, the Smith-Helmholtz equation, or Helmholtz’s equation). In the diagram\n\n(1)\n\nAlso,\n\n(2)\n\nor\n\n(3)\n\nThis relation applies to any number of successive conjugate images, and is evidently the paraxial expression of the sine condition of Abbe.\n\n3.6. Principal planes. The principal planes are that pair of conjugate planes in which object and image are of the same size and on the same side of the optical axis. The lateral magnification for the principal planes is therefore +1. Each point of one plane images into a point on the conjugate plane in 1 to 1 correspondence. Within the accuracy of Gaussian optics, both points lie at the same height above the optical axis.\n\nFIGURE 4", null, "(Fig. 4). A ray from b parallel to the axis strikes H at P and images at P′. This same ray passes through F′, which then becomes the second", null, "if F is the first focal point, strikes the first principal plane at Q, emergeslat Q′, and thenceforward remains parallel to the axis. Hence the point b′ where these two rays meet in image space determines the image point of b. All points of y are imaged into corresponding points of y′ at a constant lateral magnification m.\n\n(1)\n\n(2)\n\n(3)\n\nor\n\n(4)\n\nThe above is called Newton’s relation. We have\n\n(5)\n\nor\n\n(6)\n\nIf Lagrange’s law is applied to the principal planes, we have\n\n(7)\n\nfor any ray of slope θ through H. Let θ be determined such that\n\n(8)\n\n(9)\n\n(10)\n\nThen\n\n(11)\n\nor\n\n(12)\n\n(Cf. § 3.3.) For an object at infinity, we have\n\n(13)\n\nwhere θ is the off-axis direction of the object point. Similarly,\n\n(14)\n\nfor an image at infinity. The quantity f is called the equivalent focal length of the system in object space, or the first focal length, and often the front focal length. Similarly, the quantity f′ is called the equivalent focal length of the system in image space, or the second focal length, and often the back focal length. (It should be noted that the terms front and back focal length are often used at the present time to describe the distance from the first focal point to the front lens vertex, and from the rear lens vertex to the second focal point. This confusion is not desirable, and the terms front and back focal distances are recommended instead. The terms front focus and back focus are also used.) Where initial and final media have identical indices, it is clear from the above formula that the two focal lengths are equal.\n\n3.7. Nodal points. A ray directed toward the first nodal point in object space, by definition, emerges from the second nodal point in image space, parallel to its original direction. The nodal points are conjugate to one another. By Lagrange’s law\n\n(1)\n\nwhere y and y′ are in the nodal planes.\n\n(2)\n\nTherefore\n\n(3)\n\n(4)\n\nNote that the first nodal point lies to the right of F by a distance of f′ in Fig. 4, and that the second nodal point lies to the left of F′ by the distance f. Where initial and final media are identical, the nodal points and principal points coincide.\n\nBy determining the position of the second nodal point on an optical bench, one can obtain directly the first equivalent focal length of a system from which the other properties follow.\n\n3.8. Cardinal points. The principal points, the focal points and nodal points are the more important cardinal points of an optical system. The determination of the cardinal points of a complex system can be carried out from a knowledge of the cardinal points of the elementary systems from which the complex system is constructed. However, it is usually more expedient to trace a Gaussian ray from infinity on the left to find F′, and from the right to find F. To find f, we note that in a system of N surfaces\n\n(1)\n\nIf we let hi be the height of intercept above the axis at the ith surface, then by similar triangles\n\n(2)\n\n(3)\n\nFor an infinite object distance, we have\n\n(4)\n\nwhere θ is the slope angle or direction of the object, no the index of object space, and nN the index of image space. It is convenient to define h1 = 1, in which case all other h’s are called relative heights. Then\n\n(5)\n\nwhere f is the first focal length, or\n\n(6)\n\nwhere f′ is the second focal length.\n\nWhen F, F′, and f′ are known from the two ray traces, all other ordinary cardinal properties of the complex system follow. It is important to note that inasmuch as the paraxial ray trace beginning with s1 refers only to an object point on the axis, the relative heights denoted by hi are for an infinitesimally close ray starting out at the same object point. This is simply Lagrange’s law again, and indeed\n\n(7)\n\nor\n\n(8)\n\nfrom which\n\n(9)\n\nas above. The ray trace provides the object and image distances throughout the system, and the h values can be computed by means of the relation\n\n(10)\n\nwhere h1 = 1 when convenient. See note p. 408a.\n\n3.9. The thin lens. A thin lens is defined to be one whose thickness is negligible compared to the focal length. To Gaussian accuracy we simply set the thickness equal to zero.\n\n(1)\n\n(2)\n\n(3)\n\n(4)\n\nIf s1 = ∞, s′2 = f′ = f, and we have\n\n(5)\n\nwhere φ is called the power of the lens. If now s and s′ refer to object and image spaces, we have\n\n(1)\n\n3.10. The thick lens. By working through the Gaussian equations above as applied to a lens of finite central thickness t, one finds that\n\n(1)\n\n(2)\n\nwhere d is the distance from the second surface to the second focal point, or the back focal distance.\n\n3.11. Separated thin lenses. Application of the elementary equations above to the case of separated thin lenses leads to the relations below. The powers of the individual thin lenses are represented by φ1, φ2, φ3 etc. The separations are given by d1, d2, d3, etc. Let d be the back focal distance, which then serves to locate the second focal point. Let φ be the power of the combined system of lenses, which is the reciprocal of the equivalent focal length.\n\na. Two separated thin lenses\n\n(1)\n\n(2)\n\nb. Three separated thin lenses\n\n(3)\n\n(4)\n\nc. Four separated thin lenses\n\n(5)\n\n(6)\n\nThe corresponding expressions for five or more separated thin\n\nHai raggiunto la fine di questa anteprima. 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http://www.numdam.org/item/CM_1989__69_2_121_0/
[ "The subspace theorem in diophantine approximations\nCompositio Mathematica, Tome 69 (1989) no. 2, pp. 121-173.\n@article{CM_1989__69_2_121_0,\nauthor = {Schmidt, Wolfgang M.},\ntitle = {The subspace theorem in diophantine approximations},\njournal = {Compositio Mathematica},\npages = {121--173},\nvolume = {69},\nnumber = {2},\nyear = {1989},\nzbl = {0683.10027},\nmrnumber = {984633},\nlanguage = {en},\nurl = {http://www.numdam.org/item/CM_1989__69_2_121_0/}\n}\nSchmidt, Wolfgang M. The subspace theorem in diophantine approximations. Compositio Mathematica, Tome 69 (1989) no. 2, pp. 121-173. http://www.numdam.org/item/CM_1989__69_2_121_0/\n\n1 E. Bombieri and J. Vaaler, On Siegel's lemma. Invent. Math. 73 (1983) 11-32. | MR 707346 | Zbl 0533.10030\n\n2 E. Bombieri and A.J. Van Der Poorten, Some quantitative results related to Roth's Theorem. MacQuarie Math. Reports, Report No. 87-0005, February 1987.\n\n3 J.W.S. Cassels, An Introduction to the Geometry of Numbers. Springer Grundlehren 99 (1959). | Zbl 0086.26203\n\n4 H. Davenport, Note on a result of Siegel. Acta Arith. 2 (1937) 262-265. | JFM 63.0922.01\n\n5 H. Davenport and K.F. Roth, Rational approximation to algebraic numbers. Mathematika 2 (1955) 160-167. | MR 77577 | Zbl 0066.29302\n\n6 H. Esnault and E. Viehweg, Dyson's Lemma for polynomials in several variables (and the theorem of Roth). Invent. Math. 78 (1984) 445-490. | MR 768988 | Zbl 0545.10021\n\n7 J.H. Evertse, Upper bounds for the number of solutions of Diophantine equations. Math. Centrum, Amsterdam (1983) 1-127. | MR 726562 | Zbl 0517.10016\n\n8 K. Mahler, Ein Übertragungsprinzip für konvexe Körper. Časopis Pest. Mat. Fys. (1939) 93-102. | JFM 65.0175.02 | MR 1242 | Zbl 0021.10403\n\n9 K. Mahler, On compound convex bodies I. Proc. Lon. Math. Soc. (3) 5, 358-379. | MR 74460 | Zbl 0065.28002\n\n10 W.M. Schmidt, On heights of algebraic subspaces and diophantine approximations. Annals of Math. 83 (1967) 430-472. | MR 213301 | Zbl 0152.03602\n\n11 W.M. Schmidt, Norm form equations. Annals of Math. 96 (1972) 526-551. | MR 314761 | Zbl 0226.10024\n\n12 W.M. Schmidt, The number of solutions of norm form equations. Transactions A.M.S. (to appear). | MR 961596 | Zbl 0693.10014\n\n13 W.M. Schmidt, Diophantine approximation. Springer Lecture Notes in Math. 785, Berlin, Heidelberg, New York (1980). | MR 568710 | Zbl 0421.10019" ]
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https://physics.stackexchange.com/questions/492803/scale-factor-for-flat-universe-filled-with-radiation-and-cosmological-constant/492821
[ "# Scale factor for flat universe filled with radiation and cosmological constant [closed]\n\nI am trying to solve problem 1.20 in the book 'Physical Foundations of Cosmology' from Mukhanov.\n\nIn the problem, we should show that the scale factor $$a$$ for a flat universe filled with cosmological constant and radiation is given by, $$a(t)=a_0(\\sinh2H_\\Lambda t)^{1/2},\\tag{1}$$ wherein $$H_\\Lambda=(8\\pi G\\epsilon_\\Lambda/3)^{1/2}$$.\n\nAs a hint, we are given, $$a^{\\prime\\prime}+ka=\\frac{4\\pi G}{3}\\left(\\epsilon-3p\\right)a^3,\\tag{2}$$ where prime denotes the derivative with respect to conformal time $$\\eta$$.\n\nThe equation of state for the cosmological constant $$\\Lambda$$ is $$p=-\\epsilon$$ whereas the equation of state for radiation is $$p=\\frac{1}{3}\\epsilon$$. Using these equations the right-hand side of the former equation yields, $$\\frac{4\\pi G}{3}4\\epsilon_\\Lambda a^3=2H_\\Lambda a^3.\\tag{3}$$ As for a flat universe $$k=0$$ we arrive at, $$a^{\\prime\\prime}=2H_\\Lambda a^3.\\tag{4}$$\n\nIf we multiply both sides with $$a^\\prime$$ we can write, $$\\frac{1}{2}\\frac{d}{d\\eta}(a^\\prime)^2=a^{\\prime\\prime}a^\\prime=2H_\\Lambda a^3a^\\prime=\\frac{1}{2}H_\\Lambda \\frac{d}{d\\eta}a^4,\\tag{5}$$ and we can integrate both sides with respect to $$\\eta$$.\n\nDropping the integration constant and taking the square root of both sides, $$a^\\prime=\\pm H_\\Lambda^{1/2}a^2,\\tag{6}$$ we can solve this by separation and of variables and find, $$\\eta=\\int d\\eta=\\pm H^{-1/2}_\\Lambda\\int \\frac{da}{a^2}=\\mp H^{-1/2}_\\Lambda \\frac{1}{a}.\\tag{7}$$\n\nWe need the scale factor to be positive, therefore, $$a(\\eta)=H^{-1/2}_\\Lambda \\eta.\\tag{8}$$\n\nFrom the definition of the conformal time, $$\\eta=\\int\\frac{dt}{a(t)},\\tag{9}$$ we find, $$t=\\int dt=\\int d\\eta a(\\eta)=\\frac{1}{2}H^{-1/2}_\\Lambda \\eta^2,\\tag{10}$$ which solved for $$\\eta$$ can be used to express the scale factor in proper time $$t$$, $$a(t)=\\sqrt{2 t}H_\\Lambda^{3/4},\\tag{11}$$ which obviously is very different from the actual result.\n\nWhat did I wrong?\n\nI see some mistakes:\n\n• First of all, according to your definition of $$H_{\\Lambda}$$, in the right-hand side of your equation you should have $$H_{\\Lambda}^{2}$$ and not $$H_{\\Lambda}$$.\n\n• When you solve by separation of variables and leave $$a$$ in terms of $$\\eta$$, you obtain $$a \\propto \\eta^{-1}$$ and not $$a \\propto \\eta$$ as you wrote.\n\n• At some point in your derivation you should take into account the integration constant, that is how you will make the $$a_0$$ appear in the final result.\n• I'm not sure that you have switched correctly from conformal to proper time. I think that the best thing to do is to reduce the second-order equation to a first-order equation (just as you did) and then switch to proper time by using the chain rule and $$d\\eta = dt/a(t)$$.\n\nFinally, I would recommend to enumerate your equations, in this way it is much easier to correct your work.\n\n• @GuillermoFranvoAbelián Thanks, I added references to the equations. Can you elaborate a bit what you mean in your second point? – bodokaiser Jul 21 '19 at 11:04\n• @bodokaiser By following all the steps correctly, your equation 7 should look like $\\eta = H_{\\Lambda}^{-1}/a$. Therefore $a = H_{\\Lambda}^{-1} / \\eta$, and not $a= H_{\\Lambda}^{-1} \\eta$ as you wrote in your equation 8. – Guillermo Franco Abellán Jul 21 '19 at 11:35" ]
[ null ]
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http://mgucat.mgu.ac.in/cgi-bin/koha/opac-detail.pl?biblionumber=85552&shelfbrowse_itemnumber=77893
[ "", null, "Normal view\n\n## A brief history of numbers/ Leo Corry.\n\nPublisher: Oxford: Oxford University Press, 2015Description: xiii, 309 p. illustrationsISBN: 9780198702597Subject(s): Number theoryDDC classification: 512.7 Online resources: Click here to access online\nContents:\nThe system of numbers : an overview: From natural to real numbers ; Imaginary numbers ; Polynomials and transcendental numbers ; Cardinals and ordinals -- Writing mumbers : now and back then: Writing numbers nowadays : positional and decimal ; Writing numbers back then : Egypt, Babylon and Greece -- Numbers and magnitudes in the Greek mathematical tradition: Pythagorean numbers ; Ratios and proportions ; Incommensurability ; Eudoxus' theory of proportions ; Greek fractional numbers ; Comparisons, not measurements ; A unit length ; Appendix 3.1: The incommensurability of 2 -- ancient and modern proofs ; Appendix 3.2: Eudoxus' theory of proportions in action ; Appendix 3.3: Euclid and the area of the circle -- Construction problems and numerical problems in the Greek mathematical tradition: The arithmetic books of the elements ; Geometric algebra? ; Straightedge and compass ; Diophantus' numerical problems ; Diophantus' reciprocals and fractions ; More than three dimensions ; Appendix 4.1: Diophantus' solution of Problem V.9 in Arithmetica -- Numbers in the tradition of medieval Islam: Islamicate science in historical perspective ; Al-Khwārizmī and numerical problems with squares ; Geometry and certainty ; Al-jabr wa'l-muqābala ; Al-Khwārizmī, numbers and fractions ; Abū Kāmil's numbers at the crossroads of two traditions ; Numbers, fractions and symbolic methods ; Al-Khayyām and numerical problems with cubes ; Gersonides and problems with numbers ; Appendix 5.1: The quadratic equation. Derivation of the algebraic formula ; Appendix 5.2: The cubic equation. Khayyam's geometric solution -- Numbers in Europe from the twelfth to the sixteenth centuries: Fibonacci and Hindu-Arabic numbers in Europe ; Abbacus and coss traditions in Europe ; Cardano's Great art of algebra ; Bombelli and the roots of negative numbers ; Euclid's Elements in the Renaissance ; Appendix 6.1: Casting out nines -- Number and equations at the beginning of the scientific revolution: Viète and the new art of analysis ; Stevin and decimal fractions ; Logarithms and the decimal system of numeration ; Appendix 7.1: Napier's construction of logarithmic tables -- Number and equations in the works of Descartes, Newton and their contemporaries: Descartes' new approach to numbers and equations ; Wallis and the primacy of algebra ; Barrow and the opposition to the primacy of algebra ; Newton's Universal arithmetick ; Appendix 8.1: The quadratic equation. Descartes' geometric solution ; Appendix 8.2: Between geometry and algebra in the seventeenth century : the case of Euclid's Elements -- New definitions of complex numbers in the early nineteenth century: Numbers and ratios : giving up metaphysics ; Euler, Gauss and the ubiquity of complex numbers ; Geometric interpretations of the complex numbers ; Hamilton's formal definition of complex numbers ; Beyond complex numbers ; Hamilton's discovery of quaternions -- \"What are numbers and what should they be?\" : understanding numbers in the late nineteenth century: What are numbers? ; Kummer's ideal numbers ; Fields of algebraic numbers ; What should numbers be? ; Numbers and the foundations of calculus ; Appendix 10.1: Dedekind's theory of cuts and Eudoxus' theory of proportions ; Appendix 10.2: IVT and the fundamental theorem of calculus -- Exact definitions for the natural numbers : Dedekind, Peano and Frege: The principle of mathematical induction ; Peano's postulates ; Dedekind's chains of cardinal numbers -- Appendix 11.1: The principle of induction and Peano's postulates -- Numbers, sets and infinity : a conceptual breakthrough at the turn of the twentieth century: Dedekind, Cantor and the infinite ; Infinities of various sizes ; Cantor's transfinite ordinals ; Troubles in paradise ; Appendix 12.1: Proof that the set of algebraic numbers is countable -- Epilogue: Numbers in historical perspective.\nSummary: The world around us is saturated with numbers. They are a fundamental pillar of our modern society, and accepted and used with hardly a second thought. But how did this state of affairs come to be? In this book, Leo Corry tells the story behind the idea of number from the early days of the Pythagoreans, up until the turn of the twentieth century. He presents an overview of how numbers were handled and conceived in classical Greek mathematics, in the mathematics of Islam, in European mathematics of the middle ages and the Renaissance, during the scientific revolution, all the way through to the. --\nTags from this library: No tags from this library for this title.\nItem type Current location Call number Status Date due Barcode Item holds", null, "Books\nGeneral Stacks\n512.7 Q5;1 (Browse shelf) Available 55243", null, "Books\nGeneral Stacks\n512.7 Q5 (Browse shelf) Available 53984\nTotal holds: 0\n##### Browsing Mahatma Gandhi University Library shelves, Shelving location: General Stacks Close shelf browser\n No cover image available No cover image available 512.42 P0 Rings and modules for beginners/ 512.482 Q3 Lie groups and lie algebras: 512.620 285 513 3 Q5 Analysis of categorical data with R / 512.7 Q5 A brief history of numbers/ 512.7 Q5;1 A brief history of numbers/ 514 N9 Topology for beginners/ 514 Q4 Undergraduate topology/\n\nIncludes bibliographical references (pages 295-301) and index.\n\nThe system of numbers : an overview: From natural to real numbers ; Imaginary numbers ; Polynomials and transcendental numbers ; Cardinals and ordinals -- Writing mumbers : now and back then: Writing numbers nowadays : positional and decimal ; Writing numbers back then : Egypt, Babylon and Greece -- Numbers and magnitudes in the Greek mathematical tradition: Pythagorean numbers ; Ratios and proportions ; Incommensurability ; Eudoxus' theory of proportions ; Greek fractional numbers ; Comparisons, not measurements ; A unit length ; Appendix 3.1: The incommensurability of 2 -- ancient and modern proofs ; Appendix 3.2: Eudoxus' theory of proportions in action ; Appendix 3.3: Euclid and the area of the circle -- Construction problems and numerical problems in the Greek mathematical tradition: The arithmetic books of the elements ; Geometric algebra? ; Straightedge and compass ; Diophantus' numerical problems ; Diophantus' reciprocals and fractions ; More than three dimensions ; Appendix 4.1: Diophantus' solution of Problem V.9 in Arithmetica -- Numbers in the tradition of medieval Islam: Islamicate science in historical perspective ; Al-Khwārizmī and numerical problems with squares ; Geometry and certainty ; Al-jabr wa'l-muqābala ; Al-Khwārizmī, numbers and fractions ; Abū Kāmil's numbers at the crossroads of two traditions ; Numbers, fractions and symbolic methods ; Al-Khayyām and numerical problems with cubes ; Gersonides and problems with numbers ; Appendix 5.1: The quadratic equation. Derivation of the algebraic formula ; Appendix 5.2: The cubic equation. Khayyam's geometric solution -- Numbers in Europe from the twelfth to the sixteenth centuries: Fibonacci and Hindu-Arabic numbers in Europe ; Abbacus and coss traditions in Europe ; Cardano's Great art of algebra ; Bombelli and the roots of negative numbers ; Euclid's Elements in the Renaissance ; Appendix 6.1: Casting out nines -- Number and equations at the beginning of the scientific revolution: Viète and the new art of analysis ; Stevin and decimal fractions ; Logarithms and the decimal system of numeration ; Appendix 7.1: Napier's construction of logarithmic tables -- Number and equations in the works of Descartes, Newton and their contemporaries: Descartes' new approach to numbers and equations ; Wallis and the primacy of algebra ; Barrow and the opposition to the primacy of algebra ; Newton's Universal arithmetick ; Appendix 8.1: The quadratic equation. Descartes' geometric solution ; Appendix 8.2: Between geometry and algebra in the seventeenth century : the case of Euclid's Elements -- New definitions of complex numbers in the early nineteenth century: Numbers and ratios : giving up metaphysics ; Euler, Gauss and the ubiquity of complex numbers ; Geometric interpretations of the complex numbers ; Hamilton's formal definition of complex numbers ; Beyond complex numbers ; Hamilton's discovery of quaternions -- \"What are numbers and what should they be?\" : understanding numbers in the late nineteenth century: What are numbers? ; Kummer's ideal numbers ; Fields of algebraic numbers ; What should numbers be? ; Numbers and the foundations of calculus ; Appendix 10.1: Dedekind's theory of cuts and Eudoxus' theory of proportions ; Appendix 10.2: IVT and the fundamental theorem of calculus -- Exact definitions for the natural numbers : Dedekind, Peano and Frege: The principle of mathematical induction ; Peano's postulates ; Dedekind's chains of cardinal numbers -- Appendix 11.1: The principle of induction and Peano's postulates -- Numbers, sets and infinity : a conceptual breakthrough at the turn of the twentieth century: Dedekind, Cantor and the infinite ; Infinities of various sizes ; Cantor's transfinite ordinals ; Troubles in paradise ; Appendix 12.1: Proof that the set of algebraic numbers is countable -- Epilogue: Numbers in historical perspective.\n\nThe world around us is saturated with numbers. They are a fundamental pillar of our modern society, and accepted and used with hardly a second thought. But how did this state of affairs come to be? In this book, Leo Corry tells the story behind the idea of number from the early days of the Pythagoreans, up until the turn of the twentieth century. He presents an overview of how numbers were handled and conceived in classical Greek mathematics, in the mathematics of Islam, in European mathematics of the middle ages and the Renaissance, during the scientific revolution, all the way through to the. --\n\nThere are no comments on this title." ]
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https://www.monroecc.edu/etsdbs/MCCatPub.nsf/OnlineCatalog-Courses/C7155DF16F662B938525842E00479B9E?OpenDocument&Catalog
[ "# Course Descriptions\n\n## MTH 225 - Differential Equations\n\n4 Credits\n\nAn introduction to ordinary differential equations and their applications. Analytical methods include: separation of variables, linear first order equations, substitution methods, second order linear equations with constant coefficients, undetermined coefficients, variation of parameters, autonomous systems of two first order equations, series solutions about ordinary points, and the Laplace Transform. In addition to analytical methods, quantitative and qualitative analysis will be employed through the use of Euler’s Method, phase lines, phase planes, and slope fields.\n\nPrerequisite: MTH 211 with a grade of C or better.\n\nCourse Learning Outcomes\n1. Classify a differential equation using appropriate mathematical terminology.\n2. Solve a variety of differential equations using analytical methods.\n3. Describe the qualitative behavior of the solutions of a differential equation.\n4. Estimate the solutions of a differential equation using numerical and graphical methods.\n5. Solve a differential equation using power series.\n6. Solve an autonomous system of two first order differential equations.\n7. Examine the qualitative behavior of the solutions of an autonomous system of two first order differential equations.\n8. Solve initial value problems using the Laplace Transform.\n9. Solve applied problems using differential equations.\n\nCourse Offered Fall, Spring\n\nUse links below to see if this course is offered:\nFall Semester 2023\nSummer Session 2023" ]
[ null ]
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https://elfi-y.medium.com/python-descriptor-a-thorough-guide-60a915f67aa9?source=post_internal_links---------3----------------------------
[ "# Python Descriptor — A Thorough Guide\n\n## Learn about Descriptor Protocol, Data vs. Non-data descriptor, look-up chain, mechanism behind functions, and the __getattribute__that empowers the descriptors at the back", null, "Photo by Joseph Gonzalez on Unsplash\n`__get__(self, obj, type=None) -> object__set__(self, obj, value) -> None__delete__(self, obj) -> None`\n`class DataDescriptor(object): def __init__(self): self.value = 0 def __get__(self, obj, type): print(\"__get__\") return self.value def __set__(self, obj, value): print(\" __set__\") try: self.value = value except AttributeError: print(f\"Can not set value {value}\") def __delete__(self, obj): print(\" __del__\")class Example(): attr = DataDescriptor()d = DataDescriptor()e = Example()e.attr # 0, __get__e.attr = \"new attribute\" #__set__del e.attr # __del__print(d.__dict__) # {'value': 0}print(e.__dict__) # {}print(Example.__dict__)# {'__module__': '__main__', 'attr': <__main__.DataDescriptor object at 0x7f1635e58940>, '__dict__': <attribute '__dict__' of 'Example' objects>, '__weakref__': <attribute '__weakref__' of 'Example' objects>, '__doc__': None}`\n\n## Lookup chain\n\n`e.attr(type(e).__dict__['attr'].__get__(e, type(e))) #__get__e.attr = \"another new attribute\"(type(e).__dict__['attr'].__set__(e, type(e)),\"another new attribute\")# __set__`\n`def getattr_hook(obj, name): try: return obj.__getattribute__(name) except AttributeError: if not hasattr(type(obj), '__getattr__'): raise return type(obj).__getattr__(obj, name) # __getattr__`\n\n## Non-data descriptor\n\n`class NonDataDescriptor(): def __init__(self): self.value = 0 def __get__(self, obj, type): print(\" __get__\") return self.value + 1class Example(): attr = NonDataDescriptor()e = Example()d = NonDataDescriptor()print(e.attr) # __get__ 1print(e.attr) # __get__ 2print(e.__dict__) # {}print(d.__dict__) # {\"value\": 2}e.attr = 4 print(e.attr) # 4print(e.__dict__) # {'attr': 4}print(d.__dict__) # {'value': 0}`\n\n## Functions and Methods\n\n`class Function: def __get__(self, obj, objtype=None): \"Simulate func_descr_get() in Objects/funcobject.c\" if obj is None: return self return MethodType(self, obj)class D: def f(self, x): return x`\n`1. dotted access from class from dictionary --> function>>> D.__dict__['f']<function D.f at 0x00C45070>2. dotted access from class --> function >>> D.f<function D.f at 0x00C45070>3. dotted access from instance --> bound function >>> d = D()>>> d.f<bound method D.f of <__main__.D object at 0x00B18C90>>Internally, the bound method stores the underlying function and the bound instance:>>> d.f.__func__<function D.f at 0x00C45070>>>> d.f.__self__<__main__.D object at 0x1012e1f98>`\n\n## `__getattribute__`\n\n`>>> class Example(): def __init__(self, valid_attr): self.valid_attr=valid_attr>>> e = Example(\"valid\")>>> print(e.__dict__){'valid_attr': 'valid'}>>> print(e.valid_attr)valid>>> print(e.invalid_attr)AttributeError: 'Example' object has no attribute 'invalid_attr'`\n`>>> class Example(): def __init__(self, valid_attr): self.valid_attr=valid_attr def __getattr__(self, attr): self.__dict__[attr]= \"this is invalid\" return \"this is indeed invalid\">>> e = Example(\"valid\")>>> print(e.__dict__){'valid_attr': 'valid'}>>> print(e.valid_attr)valid>>> print(e.invalid_attr)this is indeed invalid>>> print(e.__dict__){'valid_attr': 'valid', 'invalid_attr': 'this is invalid'}`\n`>>> class Example(): def __init__(self, valid_attr): self.valid_attr=valid_attr def __getattribute__(self, attr): return \"this is indeed invalid\">>> e = Example(\"valid\")>>> print(e.__dict__)this is indeed invalid>>> print(e.valid_attr)this is indeed invalid>>> print(e.invalid_attr)this is indeed invalid`\n`def __getattribute__(self, attr): if attr == “invalid”: return “this is indeed invalid\" else: return object.__getattribute__(self,attr) # same as----- super().__getattribute__(attr)`\n`def object_getattribute(obj, name): \"Emulate PyObject_GenericGetAttr() in Objects/object.c\" null = object() objtype = type(obj) cls_var = getattr(objtype, name, null) descr_get = getattr(type(cls_var), '__get__', null) if descr_get is not null: if (hasattr(type(cls_var), '__set__') or hasattr(type(cls_var), '__delete__')): return descr_get(cls_var, obj, objtype) # data descriptor if hasattr(obj, '__dict__') and name in vars(obj): return vars(obj)[name] # instance variable if descr_get is not null: return descr_get(cls_var, obj, objtype) # non-data descriptor if cls_var is not null: return cls_var # class variable raise AttributeError(name)`" ]
[ null, "https://miro.medium.com/max/7488/1*2gWypIMxOQ1GToErRzacdA.jpeg", null ]
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https://wumbo.net/graph/cosine/
[ "# Cosine Graph\n\n## Summary\n\nGraph of the cos(x) from 0 to 2 PI. Cosine is a trigonometric function that when given the angle of a right triangle, returns the ratio of its adjacent side over the hypotenuse.\n\n## Function\n\nMath.cos(x)" ]
[ null ]
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https://calculatorshub.com/root-calculator.php
[ "### Root Calculator\n\n▼ Modify The Values and Click the Calculate Button to use\n##### Result\nNo result to Show !\n\n##### Result\nNo result to Show !\n\n##### Result\nNo result to Show !\n\n##### What is Root?\n\nNow you can use root square calculator to find any positive number you want. This is a calculator that will calculate any number and will not allow any negative number to come in the root square circle. This one is quite handy for all those people who has great interest in learning math and don't need to put too much efforts to solve their questions. But instead try this one which will aid you to get the imaginary results in no time.\n\nA root square is a kind of number that is raised with the exponent of using 1 and 2. The result of any number is multiplied itself also called (square) yield to its original number. Like, a square root number is 16 and is 4 since, 4 times is multiplied 16. The main point to notice is that there is also some negative square root. But if you begin it for practical needs then you only get the positive value of any number.\n\nA root square is a kind of number that is raised with the exponent of using 1 and 2. The result of any number is multiplied itself also called (square) yield to its original number. Like, a square root number is 16 and is 4 since, 4 times is multiplied 16. The main point to notice is that there is also some negative square root. But if you begin it for practical needs then you only get the positive value of any number.\n\n##### How to Use Root Calculator?\n\nFor all those numbers who are not exact perfect squares. You can use this certain formula to represent the root square of the whole number also to multiply them to another root square to get your answer in so many ways. Here are the following steps you need to take such as,\n\nFormula name for using Root calculator:\nNvA = B\nBN = A\n\n• First write down the number and determine of its square root\n• Now breakdown the numbers into factors, to learn the perfect root square\n• Simplify factor about the current square root number\n• Rewrite the whole number again and multiply it with the root square\n• If you cannot find the factor that is perfect then you root square could be simplified\n• If you truly want to the exact value use this root square calculator from the beginning\n##### Working of Root Calculator:", null, "For some application for using root square calculator may not particularly gives you the right answer. However, you can use for other subject including, science, physics, and chemistry to get the end result of scientific notion. In short answer, if you get caught into two none zero square numbers then you need to represent it in decimal more than ten times multiplied to raise the number value. So the results you will obtain can convert them into any notion you want.\n\nOne can only estimate the true value of root square when two numbers falls. This calculator is fantastic example to learn and help you about the root square numbers in so many ways." ]
[ null, "https://calculatorshub.com/images/Best Slope Calculator.png", null ]
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https://www.numbers.education/235525.html
[ "Is 235525 a prime number? What are the divisors of 235525?\n\n## Parity of 235 525\n\n235 525 is an odd number, because it is not evenly divisible by 2.\n\nFind out more:\n\n## Is 235 525 a perfect square number?\n\nA number is a perfect square (or a square number) if its square root is an integer; that is to say, it is the product of an integer with itself. Here, the square root of 235 525 is about 485.309.\n\nThus, the square root of 235 525 is not an integer, and therefore 235 525 is not a square number.\n\n## What is the square number of 235 525?\n\nThe square of a number (here 235 525) is the result of the product of this number (235 525) by itself (i.e., 235 525 × 235 525); the square of 235 525 is sometimes called \"raising 235 525 to the power 2\", or \"235 525 squared\".\n\nThe square of 235 525 is 55 472 025 625 because 235 525 × 235 525 = 235 5252 = 55 472 025 625.\n\nAs a consequence, 235 525 is the square root of 55 472 025 625.\n\n## Number of digits of 235 525\n\n235 525 is a number with 6 digits.\n\n## What are the multiples of 235 525?\n\nThe multiples of 235 525 are all integers evenly divisible by 235 525, that is all numbers such that the remainder of the division by 235 525 is zero. There are infinitely many multiples of 235 525. The smallest multiples of 235 525 are:\n\n## Numbers near 235 525\n\n### Nearest numbers from 235 525\n\nFind out whether some integer is a prime number" ]
[ null ]
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https://fr.mathworks.com/matlabcentral/cody/problems/2015-length-of-the-hypotenuse/solutions/966095
[ "Cody\n\n# Problem 2015. Length of the hypotenuse\n\nSolution 966095\n\nSubmitted on 12 Sep 2016 by Mehdi\nThis solution is locked. To view this solution, you need to provide a solution of the same size or smaller.\n\n### Test Suite\n\nTest Status Code Input and Output\n1   Pass\na = 1; b = 2; c_correct = sqrt(5); tolerance = 1e-12 ; assert(abs(hypotenuse(a,b)-c_correct)<tolerance);\n\n2   Pass\na = 3; b = 4; c_correct = 5; tolerance = 1e-12 ; assert(abs(hypotenuse(a,b)-c_correct)<tolerance);\n\n3   Pass\na = 5; b = 12; c_correct = 13; tolerance = 1e-12 ; assert(abs(hypotenuse(a,b)-c_correct)<tolerance);\n\n### Community Treasure Hunt\n\nFind the treasures in MATLAB Central and discover how the community can help you!\n\nStart Hunting!" ]
[ null ]
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http://lambda.jimpryor.net/git/gitweb.cgi?p=lambda.git;a=blob_plain;f=topics/_week4_fixed_point_combinator.mdwn;hb=39db6d0abfc0f9606c1b38b3b21b4232cad3a6e2
[ "[[!toc]] #Recursion: fixed points in the lambda calculus## Sometimes when you type in a web search, Google will suggest alternatives. For instance, if you type in \"Lingusitics\", it will ask you \"Did you mean Linguistics?\". But the engineers at Google have added some playfulness to the system. For instance, if you search for \"anagram\", Google asks you \"Did you mean: nag a ram?\" And if you search for \"recursion\", Google asks: \"Did you mean: recursion?\" ##What is the \"rec\" part of \"letrec\" doing?## How could we compute the length of a list? Without worrying yet about what lambda-calculus implementation we're using for the list, the basic idea would be to define this recursively: > the empty list has length 0 > any non-empty list has length 1 + (the length of its tail) In OCaml, you'd define that like this: let rec get_length = fun lst -> if lst == [] then 0 else 1 + get_length (tail lst) in ... (* here you go on to use the function \"get_length\" *) In Scheme you'd define it like this: (letrec [(get_length (lambda (lst) (if (null? lst) 0 [+ 1 (get_length (cdr lst))] )) )] ... ; here you go on to use the function \"get_length\" ) Some comments on this: 1. `null?` is Scheme's way of saying `isempty`. That is, `(null? lst)` returns true (which Scheme writes as `#t`) iff `lst` is the empty list (which Scheme writes as `'()` or `(list)`). 2. `cdr` is function that gets the tail of a Scheme list. (By definition, it's the function for getting the second member of an ordered pair. It just turns out to return the tail of a list because of the particular way Scheme implements lists.) 3. I use `get_length` instead of the convention we've been following so far of hyphenated names, as in `make-list`, because we're discussing OCaml code here, too, and OCaml doesn't permit the hyphenated variable names. OCaml requires variables to always start with a lower-case letter (or `_`), and then continue with only letters, numbers, `_` or `'`. Most other programming languages are similar. Scheme is very relaxed, and permits you to use `-`, `?`, `/`, and all sorts of other crazy characters in your variable names. 4. I alternate between `[ ]`s and `( )`s in the Scheme code just to make it more readable. These have no syntactic difference. The main question for us to dwell on here is: What are the `let rec` in the OCaml code and the `letrec` in the Scheme code? Answer: These work like the `let` expressions we've already seen, except that they let you use the variable `get_length` *inside* the body of the function being bound to it---with the understanding that it will there refer to the same function that you're then in the process of binding to `get_length`. So our recursively-defined function works the way we'd expect it to. In OCaml: let rec get_length = fun lst -> if lst == [] then 0 else 1 + get_length (tail lst) in get_length [20; 30] (* this evaluates to 2 *) In Scheme: (letrec [(get_length (lambda (lst) (if (null? lst) 0 [+ 1 (get_length (cdr lst))] )) )] (get_length (list 20 30))) ; this evaluates to 2 If you instead use an ordinary `let` (or `let*`), here's what would happen, in OCaml: let get_length = fun lst -> if lst == [] then 0 else 1 + get_length (tail lst) in get_length [20; 30] (* fails with error \"Unbound value length\" *) Here's Scheme: (let* [(get_length (lambda (lst) (if (null? lst) 0 [+ 1 (get_length (cdr lst))] )) )] (get_length (list 20 30))) ; fails with error \"reference to undefined identifier: get_length\" Why? Because we said that constructions of this form: let get_length = A in B really were just another way of saying: (\\get_length. B) A and so the occurrences of `get_length` in A *aren't bound by the `\\get_length` that wraps B*. Those occurrences are free. We can verify this by wrapping the whole expression in a more outer binding of `get_length` to some other function, say the constant function from any list to the integer 99: let get_length = fun lst -> 99 in let get_length = fun lst -> if lst == [] then 0 else 1 + get_length (tail lst) in get_length [20; 30] (* evaluates to 1 + 99 *) Here the use of `get_length` in `1 + get_length (tail lst)` can clearly be seen to be bound by the outermost `let`. And indeed, if you tried to define `get_length` in the lambda calculus, how would you do it? \\lst. (isempty lst) zero (add one (get_length (extract-tail lst))) We've defined all of `isempty`, `zero`, `add`, `one`, and `extract-tail` in earlier discussion. But what about `get_length`? That's not yet defined! In fact, that's the very formula we're trying here to specify. What we really want to do is something like this: \\lst. (isempty lst) zero (add one (... (extract-tail lst))) where this very same formula occupies the `...` position: \\lst. (isempty lst) zero (add one ( \\lst. (isempty lst) zero (add one (... (extract-tail lst))) (extract-tail lst))) but as you can see, we'd still have to plug the formula back into itself again, and again, and again... No dice. So how could we do it? And how do OCaml and Scheme manage to do it, with their `let rec` and `letrec`? 1. OCaml and Scheme do it using a trick. Well, not a trick. Actually an impressive, conceptually deep technique, which we haven't yet developed. Since we want to build up all the techniques we're using by hand, then, we shouldn't permit ourselves to rely on `let rec` or `letrec` until we thoroughly understand what's going on under the hood. 2. If you tried this in Scheme: (define get_length (lambda (lst) (if (null? lst) 0 [+ 1 (get_length (cdr lst))] )) ) (get_length (list 20 30)) You'd find that it works! This is because `define` in Scheme is really shorthand for `letrec`, not for plain `let` or `let*`. So we should regard this as cheating, too. 3. In fact, it *is* possible to define the `get_length` function in the lambda calculus despite these obstacles. This depends on using the \"version 3\" implementation of lists, and exploiting its internal structure: that it takes a function and a base value and returns the result of folding that function over the list, with that base value. So we could use this as a definition of `get_length`: \\lst. lst (\\x sofar. successor sofar) zero What's happening here? We start with the value zero, then we apply the function `\\x sofar. successor sofar` to the two arguments `xn` and `zero`, where `xn` is the last element of the list. This gives us `successor zero`, or `one`. That's the value we've accumuluted \"so far.\" Then we go apply the function `\\x sofar. successor sofar` to the two arguments `xn-1` and the value `one` that we've accumulated \"so far.\" This gives us `two`. We continue until we get to the start of the list. The value we've then built up \"so far\" will be the length of the list. We can use similar techniques to define many recursive operations on lists and numbers. The reason we can do this is that our \"version 3,\" fold-based implementation of lists, and Church's implementations of numbers, have a internal structure that *mirrors* the common recursive operations we'd use lists and numbers for. In a sense, the recursive structure of the `get_length` operation is built into the data structure we are using to represent the list. The non-recursive version of get_length exploits this embedding of the recursion into the data type. This is one of the themes of the course: using data structures to encode the state of some recursive operation. See discussions of the [[zipper]] technique, and [[defunctionalization]]. As we said before, it does take some ingenuity to define functions like `extract-tail` or `predecessor` for these implementations. However it can be done. (And it's not *that* difficult.) Given those functions, we can go on to define other functions like numeric equality, subtraction, and so on, just by exploiting the structure already present in our implementations of lists and numbers. With sufficient ingenuity, a great many functions can be defined in the same way. For example, the factorial function is straightforward. The function which returns the nth term in the Fibonacci series is a bit more difficult, but also achievable. ##Some functions require full-fledged recursive definitions## However, some computable functions are just not definable in this way. We can't, for example, define a function that tells us, for whatever function `f` we supply it, what is the smallest integer `x` where `f x` is `true`. (You may be thinking: but that smallest-integer function is not a proper algorithm, since it is not guaranteed to halt in any finite amount of time for every argument. This is the famous [[!wikipedia Halting problem]]. But the fact that an implementation may not terminate doesn't mean that such a function isn't well-defined. The point of interest here is that its definition requires recursion in the function definition.) Neither do the resources we've so far developed suffice to define the [[!wikipedia Ackermann function]]: A(m,n) = | when m == 0 -> n + 1 | else when n == 0 -> A(m-1,1) | else -> A(m-1, A(m,n-1)) A(0,y) = y+1 A(1,y) = 2+(y+3) - 3 A(2,y) = 2(y+3) - 3 A(3,y) = 2^(y+3) - 3 A(4,y) = 2^(2^(2^...2)) [where there are y+3 2s] - 3 ... Many simpler functions always *could* be defined using the resources we've so far developed, although those definitions won't always be very efficient or easily intelligible. But functions like the Ackermann function require us to develop a more general technique for doing recursion---and having developed it, it will often be easier to use it even in the cases where, in principle, we didn't have to. ##Using fixed-point combinators to define recursive functions## ###Fixed points### In general, we call a **fixed point** of a function f any value *x* such that f x is equivalent to *x*. For example, consider the squaring function `sqare` that maps natural numbers to their squares. `square 2 = 4`, so `2` is not a fixed point. But `square 1 = 1`, so `1` is a fixed point of the squaring function. There are many beautiful theorems guaranteeing the existence of a fixed point for various classes of interesting functions. For instance, imainge that you are looking at a map of Manhattan, and you are standing somewhere in Manhattan. The the [[!wikipedia Brouwer fixed point]] guarantees that there is a spot on the map that is directly above the corresponding spot in Manhattan. It's the spot where the blue you-are-here dot should be. Whether a function has a fixed point depends on the set of arguments it is defined for. For instance, consider the successor function `succ` that maps each natural number to its successor. If we limit our attention to the natural numbers, then this function has no fixed point. (See the discussion below concerning a way of understanding the successor function on which it does have a fixed point.) In the lambda calculus, we say a fixed point of an expression `f` is any formula `X` such that: X <~~> f X You should be able to immediately provide a fixed point of the identity combinator I. In fact, you should be able to provide a whole bunch of distinct fixed points. With a little thought, you should be able to provide a fixed point of the false combinator, KI. Here's how to find it: recall that KI throws away its first argument, and always returns I. Therefore, if we give it I as an argument, it will throw away the argument, and return I. So KII ~~> I, which is all it takes for I to qualify as a fixed point of KI. What about K? Does it have a fixed point? You might not think so, after trying on paper for a while. However, it's a theorem of the lambda calculus that every formula has a fixed point. In fact, it will have infinitely many, non-equivalent fixed points. And we don't just know that they exist: for any given formula, we can explicit define many of them. Yes, even the formula that you're using the define the successor function will have a fixed point. Isn't that weird? Think about how it might be true. We'll return to this point below. ###How fixed points help definie recursive functions### Recall our initial, abortive attempt above to define the `get_length` function in the lambda calculus. We said \"What we really want to do is something like this: \\list. if empty list then zero else add one (... (tail lst)) where this very same formula occupies the `...` position.\" Imagine replacing the `...` with some function that computes the length function. Call that function `length`. Then we have \\list. if empty list then zero else add one (length (tail lst)) At this point, we have a definition of the length function, though it's not complete, since we don't know what value to use for the symbol `length`. Technically, it has the status of an unbound variable. Imagine now binding the mysterious variable: h := \\length \\list . if empty list then zero else add one (length (tail list)) Now we have no unbound variables, and we have complete non-recursive definitions of each of the other symbols. Let's call this function `h`. Then `h` takes an argument, and returns a function that accurately computes the length of a list---as long as the argument we supply is already the length function we are trying to define. (Dehydrated water: to reconstitute, just add water!) But this is just another way of saying that we are looking for a fixed point. Assume that `h` has a fixed point, call it `LEN`. To say that `LEN` is a fixed point means that h LEN <~~> LEN But this means that (\\list . if empty list then zero else add one (LEN (tail list))) <~~> LEN So at this point, we are going to search for fixed point. The strategy we will present will turn out to be a general way of finding a fixed point for any lambda term. ##Deriving Y, a fixed point combinator## How shall we begin? Well, we need to find an argument to supply to `h`. The argument has to be a function that computes the length of a list. The function `h` is *almost* a function that computes the length of a list. Let's try applying `h` to itself. It won't quite work, but examining the way in which it fails will lead to a solution. h h <~~> \\list . if empty list then zero else 1 + h (tail list) There's a problem. The diagnosis is that in the subexpression `h (tail list)`, we've applied `h` to a list, but `h` expects as its first argument the length function. So let's adjust h, calling the adjusted function H: H = \\h \\list . if empty list then zero else one plus ((h h) (tail list)) This is the key creative step. Since `h` is expecting a length-computing function as its first argument, the adjustment tries supplying the closest candidate avaiable, namely, `h` itself. We now reason about `H`. What exactly is H expecting as its first argument? Based on the excerpt `(h h) (tail l)`, it appears that `H`'s argument, `h`, should be a function that is ready to take itself as an argument, and that returns a function that takes a list as an argument. `H` itself fits the bill: H H <~~> (\\h \\list . if empty list then zero else 1 + ((h h) (tail list))) H <~~> \\list . if empty list then zero else 1 + ((H H) (tail list)) == \\list . if empty list then zero else 1 + ((\\list . if empty list then zero else 1 + ((H H) (tail list))) (tail list)) <~~> \\list . if empty list then zero else 1 + (if empty (tail list) then zero else 1 + ((H H) (tail (tail list)))) We're in business! How does the recursion work? We've defined `H` in such a way that `H H` turns out to be the length function. In order to evaluate `H H`, we substitute `H` into the body of the lambda term. Inside the lambda term, once the substitution has occurred, we are once again faced with evaluating `H H`. And so on. We've got the infinite regress we desired, defined in terms of a finite lambda term with no undefined symbols. Since `H H` turns out to be the length function, we can think of `H` by itself as half of the length function (which is why we called it `H`, of course). Given the implementation of addition as function application for Church numerals, this (H H) is quite literally H + H. Can you think up a recursion strategy that involves \"dividing\" the recursive function into equal thirds `T`, such that the length function <~~> T T T? We've starting with a particular recursive definition, and arrived at a fixed point for that definition. What's the general recipe? 1. Start with any recursive definition `h` that takes itself as an arg: `h := \\fn ... fn ...` 2. Next, define `H := \\f . h (f f)` 3. Then compute `H H = ((\\f . h (f f)) (\\f . h (f f)))` 4. That's the fixed point, the recursive function we're trying to define So here is a general method for taking an arbitrary h-style recursive function and returning a fixed point for that function: Y := \\h. ((\\f.h(ff))(\\f.h(ff))) Test: Yh == ((\\f.h(ff))(\\f.h(ff))) <~~> h((\\f.h(ff))(\\f.h(ff))) == h(Yh) That is, Yh is a fixed point for h. Works! ##What is a fixed point for the successor function?## Well, you might think, only some of the formulas that we might give to the `successor` as arguments would really represent numbers. If we said something like: successor make-pair who knows what we'd get back? Perhaps there's some non-number-representing formula such that when we feed it to `successor` as an argument, we get the same formula back. Yes! That's exactly right. And which formula this is will depend on the particular way you've implemented the successor function. Moreover, the recipes that enable us to name fixed points for any given formula aren't *guaranteed* to give us *terminating* fixed points. They might give us formulas X such that neither `X` nor `f X` have normal forms. (Indeed, what they give us for the square function isn't any of the Church numerals, but is rather an expression with no normal form.) However, if we take care we can ensure that we *do* get terminating fixed points. And this gives us a principled, fully general strategy for doing recursion. It lets us define even functions like the Ackermann function, which were until now out of our reach. It would also let us define arithmetic and list functions on the \"version 1\" and \"version 2\" implementations, where it wasn't always clear how to force the computation to \"keep going.\" OK, so how do we make use of this? Many fixed-point combinators have been discovered. (And some fixed-point combinators give us models for building infinitely many more, non-equivalent fixed-point combinators.) Two of the simplest:\n``````Θ′ ≡ (\\u f. f (\\n. u u f n)) (\\u f. f (\\n. u u f n))\nY′ ≡ \\f. (\\u. f (\\n. u u n)) (\\u. f (\\n. u u n))``````\n`Θ′` has the advantage that `f (Θ′ f)` really *reduces to* `Θ′ f`. Whereas `f (Y′ f)` is only *convertible with* `Y′ f`; that is, there's a common formula they both reduce to. For most purposes, though, either will do. You may notice that both of these formulas have eta-redexes inside them: why can't we simplify the two `\\n. u u f n` inside `Θ′` to just `u u f`? And similarly for `Y′`? Indeed you can, getting the simpler:\n``````Θ ≡ (\\u f. f (u u f)) (\\u f. f (u u f))\nY ≡ \\f. (\\u. f (u u)) (\\u. f (u u))``````\nI stated the more complex formulas for the following reason: in a language whose evaluation order is *call-by-value*, the evaluation of `Θ (\\self. BODY)` and `Y (\\self. BODY)` will in general not terminate. But evaluation of the eta-unreduced primed versions will. Of course, if you define your `\\self. BODY` stupidly, your formula will never terminate. For example, it doesn't matter what fixed point combinator you use for `Ψ` in:\n``Ψ (\\self. \\n. self n)``\nWhen you try to evaluate the application of that to some argument `M`, it's going to try to give you back: (\\n. self n) M where `self` is equivalent to the very formula `\\n. self n` that contains it. So the evaluation will proceed: (\\n. self n) M ~~> self M ~~> (\\n. self n) M ~~> self M ~~> ... You've written an infinite loop! However, when we evaluate the application of our:\n``Ψ (\\self (\\lst. (isempty lst) zero (add one (self (extract-tail lst))) ))``\nto some list `L`, we're not going to go into an infinite evaluation loop of that sort. At each cycle, we're going to be evaluating the application of: \\lst. (isempty lst) zero (add one (self (extract-tail lst))) to *the tail* of the list we were evaluating its application to at the previous stage. Assuming our lists are finite (and the implementations we're using don't permit otherwise), at some point one will get a list whose tail is empty, and then the evaluation of that formula to that tail will return `zero`. So the recursion eventually bottoms out in a base value. ##Fixed-point Combinators Are a Bit Intoxicating## ![tatoo](/y-combinator-fixed.jpg) There's a tendency for people to say \"Y-combinator\" to refer to fixed-point combinators generally. We'll probably fall into that usage ourselves. Speaking correctly, though, the Y-combinator is only one of many fixed-point combinators. I used `Ψ` above to stand in for an arbitrary fixed-point combinator. I don't know of any broad conventions for this. But this seems a useful one. As we said, there are many other fixed-point combinators as well. For example, Jan Willem Klop pointed out that if we define `L` to be: \\a b c d e f g h i j k l m n o p q s t u v w x y z r. (r (t h i s i s a f i x e d p o i n t c o m b i n a t o r)) then this is a fixed-point combinator: L L L L L L L L L L L L L L L L L L L L L L L L L L ##Watching Y in action## For those of you who like to watch ultra slow-mo movies of bullets piercing apples, here's a stepwise computation of the application of a recursive function. We'll use a function `sink`, which takes one argument. If the argument is boolean true (i.e., `\\x y.x`), it returns itself (a copy of `sink`); if the argument is boolean false (`\\x y. y`), it returns `I`. That is, we want the following behavior: sink false ~~> I sink true false ~~> I sink true true false ~~> I sink true true true false ~~> I So we make `sink = Y (\\f b. b f I)`: 1. sink false 2. Y (\\fb.bfI) false 3. (\\f. (\\h. f (h h)) (\\h. f (h h))) (\\fb.bfI) false 4. (\\h. [\\fb.bfI] (h h)) (\\h. [\\fb.bfI] (h h)) false 5. [\\fb.bfI] ((\\h. [\\fb.bsI] (h h))(\\h. [\\fb.bsI] (h h))) false 6. (\\b.b[(\\h. [\\fb.bsI] (h h))(\\h. [\\fb.bsI] (h h))]I) false 7. false [(\\h. [\\fb.bsI] (h h))(\\h. [\\fb.bsI] (h h))] I -------------------------------------------- 8. I So far so good. The crucial thing to note is that as long as we always reduce the outermost redex first, we never have to get around to computing the underlined redex: because `false` ignores its first argument, we can throw it away unreduced. Now we try the next most complex example: 1. sink true false 2. Y (\\fb.bfI) true false 3. (\\f. (\\h. f (h h)) (\\h. f (h h))) (\\fb.bfI) true false 4. (\\h. [\\fb.bfI] (h h)) (\\h. [\\fb.bfI] (h h)) true false 5. [\\fb.bfI] ((\\h. [\\fb.bsI] (h h))(\\h. [\\fb.bsI] (h h))) true false 6. (\\b.b[(\\h. [\\fb.bsI] (h h))(\\h. [\\fb.bsI] (h h))]I) true false 7. true [(\\h. [\\fb.bsI] (h h))(\\h. [\\fb.bsI] (h h))] I false 8. [(\\h. [\\fb.bsI] (h h))(\\h. [\\fb.bsI] (h h))] false We've now arrived at line (4) of the first computation, so the result is again I. You should be able to see that `sink` will consume as many `true`s as we throw at it, then turn into the identity function after it encounters the first `false`. The key to the recursion is that, thanks to Y, the definition of `sink` contains within it the ability to fully regenerate itself as many times as is necessary. The key to *ending* the recursion is that the behavior of `sink` is sensitive to the nature of the input: if the input is the magic function `false`, the self-regeneration machinery will be discarded, and the recursion will stop. That's about as simple as recursion gets. ##Application to the truth teller/liar paradoxes## ###Base cases, and their lack### As any functional programmer quickly learns, writing a recursive function divides into two tasks: figuring out how to handle the recursive case, and remembering to insert a base case. The interesting and enjoyable part is figuring out the recursive pattern, but the base case cannot be ignored, since leaving out the base case creates a program that runs forever. For instance, consider computing a factorial: `n!` is `n * (n-1) * (n-2) * ... * 1`. The recursive case says that the factorial of a number `n` is `n` times the factorial of `n-1`. But if we leave out the base case, we get 3! = 3 * 2! = 3 * 2 * 1! = 3 * 2 * 1 * 0! = 3 * 2 * 1 * 0 * -1! ... That's why it's crucial to declare that 0! = 1, in which case the recursive rule does not apply. In our terms, fac = Y (\\fac n. iszero n 1 (fac (predecessor n))) If `n` is 0, `fac` reduces to 1, without computing the recursive case. Curry originally called `Y` the paradoxical combinator, and discussed it in connection with certain well-known paradoxes from the philosophy literature. The truth teller paradox has the flavor of a recursive function without a base case: the truth-teller paradox (and related paradoxes). (1) This sentence is true. If we assume that the complex demonstrative \"this sentence\" can refer to (1), then the proposition expressed by (1) will be true just in case the thing referred to by *this sentence* is true. Thus (1) will be true just in case (1) is true, and (1) is true just in case (1) is true, and so on. If (1) is true, then (1) is true; but if (1) is not true, then (1) is not true. Without pretending to give a serious analysis of the paradox, let's assume that sentences can have for their meaning boolean functions like the ones we have been working with here. Then the sentence *John is John* might denote the function `\\x y. x`, our `true`. Then (1) denotes a function from whatever the referent of *this sentence* is to a boolean. So (1) denotes `\\f. f true false`, where the argument `f` is the referent of *this sentence*. Of course, if `f` is a boolean, `f true false <~~> f`, so for our purposes, we can assume that (1) denotes the identity function `I`. If we use (1) in a context in which *this sentence* refers to the sentence in which the demonstrative occurs, then we must find a meaning `m` such that `I m = I`. But since in this context `m` is the same as the meaning `I`, so we have `m = I m`. In other words, `m` is a fixed point for the denotation of the sentence (when used in the appropriate context). That means that in a context in which *this sentence* refers to the sentence in which it occurs, the sentence denotes a fixed point for the identity function. Here's a fixed point for the identity function:\n``````Y I\n(\\f. (\\h. f (h h)) (\\h. f (h h))) I\n(\\h. I (h h)) (\\h. I (h h)))\n(\\h. (h h)) (\\h. (h h)))\nω ω\n&Omega\n``````\nOh. Well! That feels right. The meaning of *This sentence is true* in a context in which *this sentence* refers to the sentence in which it occurs is `Ω`, our prototypical infinite loop... What about the liar paradox? (2) This sentence is false. Used in a context in which *this sentence* refers to the utterance of (2) in which it occurs, (2) will denote a fixed point for `\\f.neg f`, or `\\f l r. f r l`, which is the `C` combinator. So in such a context, (2) might denote Y C (\\f. (\\h. f (h h)) (\\h. f (h h))) I (\\h. C (h h)) (\\h. C (h h))) C ((\\h. C (h h)) (\\h. C (h h))) C (C ((\\h. C (h h))(\\h. C (h h)))) C (C (C ((\\h. C (h h))(\\h. C (h h))))) ... And infinite sequence of `C`s, each one negating the remainder of the sequence. Yep, that feels like a reasonable representation of the liar paradox. See Barwise and Etchemendy's 1987 OUP book, [The Liar: an essay on truth and circularity](http://tinyurl.com/2db62bk) for an approach that is similar, but expressed in terms of non-well-founded sets rather than recursive functions. ##However...## You should be cautious about feeling too comfortable with these results. Thinking again of the truth-teller paradox, yes, `Ω` is *a* fixed point for `I`, and perhaps it has some a privileged status among all the fixed points for `I`, being the one delivered by Y and all (though it is not obvious why Y should have any special status). But one could ask: look, literally every formula is a fixed point for `I`, since X <~~> I X for any choice of X whatsoever. So the Y combinator is only guaranteed to give us one fixed point out of infinitely many---and not always the intuitively most useful one. (For instance, the squaring function has zero as a fixed point, since 0 * 0 = 0, and 1 as a fixed point, since 1 * 1 = 1, but `Y (\\x. mul x x)` doesn't give us 0 or 1.) So with respect to the truth-teller paradox, why in the reasoning we've just gone through should we be reaching for just this fixed point at just this juncture? One obstacle to thinking this through is the fact that a sentence normally has only two truth values. We might consider instead a noun phrase such as (3) the entity that this noun phrase refers to The reference of (3) depends on the reference of the embedded noun phrase *this noun phrase*. It's easy to see that any object is a fixed point for this referential function: if this pen cap is the referent of *this noun phrase*, then it is the referent of (3), and so for any object. The chameleon nature of (3), by the way (a description that is equally good at describing any object), makes it particularly well suited as a gloss on pronouns such as *it*. In the system of [Jacobson 1999](http://www.springerlink.com/content/j706674r4w217jj5/), pronouns denote (you guessed it!) identity functions... Ultimately, in the context of this course, these paradoxes are more useful as a way of gaining leverage on the concepts of fixed points and recursion, rather than the other way around." ]
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https://www.geeksforgeeks.org/difference-between-abstraction-and-encapsulation-in-java-with-examples/?ref=rp
[ "Related Articles\nDifference between Abstraction and Encapsulation in Java with Examples\n• Difficulty Level : Easy\n• Last Updated : 08 Nov, 2019\n\nEncapsulation in Java\n\nEncapsulation is defined as the wrapping up of data under a single unit. It is the mechanism that binds together code and the data it manipulates. Another way to think about encapsulation is, it is a protective shield that prevents the data from being accessed by the code outside this shield.\n\nTechnically in encapsulation, the variables or data of a class is hidden from any other class and can be accessed only through any member function of own class in which they are declared.\nAs in encapsulation, the data in a class is hidden from other classes, so it is also known as data-hiding.\nEncapsulation can be achieved by Declaring all the variables in the class as private and writing public methods in the class to set and get the values of variables.\n\n `// Java program to demonstrate encapsulation`` ` `public` `class` `Encapsulate {`` ` `    ``// private variables declared``    ``// these can only be accessed by``    ``// public methods of class``    ``private` `String geekName;``    ``private` `int` `geekRoll;``    ``private` `int` `geekAge;`` ` `    ``// get method for age to access``    ``// private variable geekAge``    ``public` `int` `getAge()``    ``{``        ``return` `geekAge;``    ``}`` ` `    ``// get method for name to access``    ``// private variable geekName``    ``public` `String getName()``    ``{``        ``return` `geekName;``    ``}`` ` `    ``// get method for roll to access``    ``// private variable geekRoll``    ``public` `int` `getRoll()``    ``{``        ``return` `geekRoll;``    ``}`` ` `    ``// set method for age to access``    ``// private variable geekage``    ``public` `void` `setAge(``int` `newAge)``    ``{``        ``geekAge = newAge;``    ``}`` ` `    ``// set method for name to access``    ``// private variable geekName``    ``public` `void` `setName(String newName)``    ``{``        ``geekName = newName;``    ``}`` ` `    ``// set method for roll to access``    ``// private variable geekRoll``    ``public` `void` `setRoll(``int` `newRoll)``    ``{``        ``geekRoll = newRoll;``    ``}``}`` ` `// Class to access variables``// of the class Encapsulate``class` `TestEncapsulation {``    ``public` `static` `void` `main(String[] args)``    ``{``        ``Encapsulate obj = ``new` `Encapsulate();`` ` `        ``// setting values of the variables``        ``obj.setName(``\"Harsh\"``);``        ``obj.setAge(``19``);``        ``obj.setRoll(``51``);`` ` `        ``// Displaying values of the variables``        ``System.out.println(``\"Geek's name: \"` `+ obj.getName());``        ``System.out.println(``\"Geek's age: \"` `+ obj.getAge());``        ``System.out.println(``\"Geek's roll: \"` `+ obj.getRoll());`` ` `        ``// Direct access of geekRoll is not possible``        ``// due to encapsulation``        ``// System.out.println(\"Geek's roll: \" + obj.geekName);``    ``}``}`\nOutput:\n\n```Geek's name: Harsh\nGeek's age: 19\nGeek's roll: 51\n```\n\nAbstraction in Java\n\nData Abstraction is the property by virtue of which only the essential details are displayed to the user. The trivial or the non-essentials units are not displayed to the user. Ex: A car is viewed as a car rather than its individual components.\n\nData Abstraction may also be defined as the process of identifying only the required characteristics of an object ignoring the irrelevant details. The properties and behaviours of an object differentiate it from other objects of similar type and also help in classifying/grouping the objects.\n\n `// Java program to illustrate the concept of Abstraction`` ` `abstract` `class` `Shape {``    ``String color;`` ` `    ``// these are abstract methods``    ``abstract` `double` `area();``    ``public` `abstract` `String toString();`` ` `    ``// abstract class can have a constructor``    ``public` `Shape(String color)``    ``{``        ``System.out.println(``\"Shape constructor called\"``);``        ``this``.color = color;``    ``}`` ` `    ``// this is a concrete method``    ``public` `String getColor()``    ``{``        ``return` `color;``    ``}``}``class` `Circle ``extends` `Shape {``    ``double` `radius;`` ` `    ``public` `Circle(String color, ``double` `radius)``    ``{`` ` `        ``// calling Shape constructor``        ``super``(color);``        ``System.out.println(``\"Circle constructor called\"``);``        ``this``.radius = radius;``    ``}`` ` `    ``@Override``    ``double` `area()``    ``{``        ``return` `Math.PI * Math.pow(radius, ``2``);``    ``}`` ` `    ``@Override``    ``public` `String toString()``    ``{``        ``return` `\"Circle color is \"``            ``+ ``super``.color``            ``+ ``\"and area is : \"``            ``+ area();``    ``}``}`` ` `class` `Rectangle ``extends` `Shape {`` ` `    ``double` `length;``    ``double` `width;`` ` `    ``public` `Rectangle(String color,``                     ``double` `length,``                     ``double` `width)``    ``{`` ` `        ``// calling Shape constructor``        ``super``(color);``        ``System.out.println(``\"Rectangle constructor called\"``);``        ``this``.length = length;``        ``this``.width = width;``    ``}`` ` `    ``@Override``    ``double` `area()``    ``{``        ``return` `length * width;``    ``}`` ` `    ``@Override``    ``public` `String toString()``    ``{``        ``return` `\"Rectangle color is \"``            ``+ ``super``.color``            ``+ ``\"and area is : \"``            ``+ area();``    ``}``}`` ` `public` `class` `Test {``    ``public` `static` `void` `main(String[] args)``    ``{``        ``Shape s1 = ``new` `Circle(``\"Red\"``, ``2.2``);``        ``Shape s2 = ``new` `Rectangle(``\"Yellow\"``, ``2``, ``4``);`` ` `        ``System.out.println(s1.toString());``        ``System.out.println(s2.toString());``    ``}``}`\nOutput:\n```Shape constructor called\nCircle constructor called\nShape constructor called\nRectangle constructor called\nCircle color is Redand area is : 15.205308443374602\nRectangle color is Yellowand area is : 8.0\n```\n\nDifference between Abstraction and Encapsulation:\n\nAbstractionEncapsulation\nAbstraction is the process or method of gaining the information.While encapsulation is the process or method to contain the information.\nIn abstraction, problems are solved at the design or interface level.While in encapsulation, problems are solved at the implementation level.\nAbstraction is the method of hiding the unwanted information.Whereas encapsulation is a method to hide the data in a single entity or unit along with a method to protect information from outside.\nWe can implement abstraction using abstract class and interfaces.Whereas encapsulation can be implemented using by access modifier i.e. private, protected and public.\nIn abstraction, implementation complexities are hidden using abstract classes and interfaces.While in encapsulation, the data is hidden using methods of getters and setters.\nThe objects that help to perform abstraction are encapsulated.Whereas the objects that result in encapsulation need not be abstracted.\n\nAttention reader! Don’t stop learning now. Get hold of all the important Java Foundation and Collections concepts with the Fundamentals of Java and Java Collections Course at a student-friendly price and become industry ready. To complete your preparation from learning a language to DS Algo and many more,  please refer Complete Interview Preparation Course.\n\nMy Personal Notes arrow_drop_up" ]
[ null ]
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https://it.mathworks.com/matlabcentral/cody/problems/44872-calculate-resistance-2/solutions/3254143
[ "Cody\n\n# Problem 44872. Calculate Resistance 2\n\nSolution 3254143\n\nSubmitted on 17 Oct 2020 by Dyuman Joshi\nThis solution is locked. To view this solution, you need to provide a solution of the same size or smaller.\n\n### Test Suite\n\nTest Status Code Input and Output\n1   Pass\nV=4;I=8; y_correct = 0.5; assert(isequal(Resistance(V,I),y_correct))\n\n2   Pass\nV=7;I=1.75; y_correct = 4; assert(isequal(Resistance(V,I),y_correct))\n\n### Community Treasure Hunt\n\nFind the treasures in MATLAB Central and discover how the community can help you!\n\nStart Hunting!" ]
[ null ]
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http://www.sixpacksmackdown.com/p/bmr-basal-metabolic-rate-daily-calorie-calculator
[ "", null, "# BMR (Basal Metabolic Rate) Daily Calorie Calculator\n\nThe BMR formula uses the variables of height, weight, age and gender to calculate the Basal Metabolic Rate (BMR). This is more accurate than calculating calorie needs based on body weight alone. The only factor it omits is lean body mass and thus the ratio of muscle-to-fat a body has. Remember, leaner bodies need more calories than less leaner ones. Therefore, this equation will be very accurate in all but the very muscular (will underestimate calorie needs) and the very fat (will over-estimate calorie needs).\n\npounds\ninches\nyears" ]
[ null, "https://www.facebook.com/tr", null ]
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https://internetpasswordpro.com/qa/quick-answer-is-zero-a-positive-or-negative-real-number.html
[ "", null, "# Quick Answer: Is Zero A Positive Or Negative Real Number?\n\n## Does real number include 0?\n\nReal numbers consist of zero (0), the positive and negative integers (-3, -1, 2, 4), and all the fractional and decimal values in between (0.4, 3.1415927, 1/2).\n\nReal numbers are divided into rational and irrational numbers..\n\n## Is 0 an positive integer?\n\n−3 < −2 < −1 < 0 < 1 < 2 < 3 < ... An integer is positive if it is greater than zero, and negative if it is less than zero. Zero is defined as neither negative nor positive.\n\n## Does the set of positive real numbers include 0?\n\nA real number a is said to be positive if a > 0. The set of all positive real numbers is denoted by R+, and the set of all positive integers by Z+. A real number a is said to be negative if a < 0. A real number a is said to be nonnegative if a ≥ 0.\n\n## What is R * in math?\n\nWhat is R* in math? … It is the set of all nonzero real numbers and it forms a group under the operation of multiplication of real numbers.\n\n## Where do you find negative numbers in real life?\n\nNegative numbers are used in lots of different situations. You read about negative numbers in weather reports and on food packaging. The temperature -5°C is ‘negative five degrees’ and it means 5 degrees below zero. Read more about negative numbers on food packaging in the factsheet Storing frozen food.\n\n## What is type of number?\n\nThe main types of numbers used in school mathematics are listed below: Natural Numbers (N), (also called positive integers, counting numbers, or natural numbers); They are the numbers {1, 2, 3, 4, 5, …} Whole Numbers (W). … Real numbers (R), (also called measuring numbers or measurement numbers).\n\n## Why is zero not a positive or negative integer?\n\nSince the addition of zero doesn’t increase value, and the subtraction of zero doesn’t decrease value, zero is neither negative nor positive. Because zero represents nothingness. It’s the absolute starting point for all algebraic operations.\n\n## What type of number is 0?\n\nMain types ): The counting numbers {1, 2, 3, …} are commonly called natural numbers; however, other definitions include 0, so that the non-negative integers {0, 1, 2, 3, …} are also called natural numbers. Natural numbers including 0 are also called whole numbers.\n\n## How can you tell if its a fake number?\n\nAn easy way to find out if a phone number is fake is to call it. The phone number is often a fake if it’s disconnected. This works well if you’re getting calls or texts from a phone number you suspect is fake. Block the phone number if you get a message that it’s disconnected when you call.\n\n## What type of number is π?\n\n3.14159When starting off in math, students are introduced to pi as a value of 3.14 or 3.14159. Though it is an irrational number, some use rational expressions to estimate pi, like 22/7 of 333/106. (These rational expressions are only accurate to a couple of decimal places.)\n\n## What kind of number is negative 1?\n\nIntegers are like whole numbers, but they also include negative numbers … but still no fractions allowed! We can put that all together like this: Integers = { …, −4, −3, −2, −1, 0, 1, 2, 3, 4, … }\n\n## Is Z+ the same as N?\n\nZ stands for Zahlen, which in German means numbers. When putting a + sign at the top, it means only the positive whole numbers, starting from 1, then 2 and so on. N is a little bit more complicated set. It stands for the natural numbers, and in some definitions, it starts from 0, then 1 and so on.\n\n## What is a true number?\n\nThe real numbers include all the rational numbers, such as the integer −5 and the fraction 4/3, and all the irrational numbers, such as √2 (1.41421356…, the square root of 2, an irrational algebraic number). Included within the irrationals are the transcendental numbers, such as π (3.14159265…).\n\n## What are not real numbers?\n\nA non-real, or imaginary, number is any number that, when multiplied by itself, produces a negative number. Mathematicians use the letter “i” to symbolize the square root of -1. An imaginary number is any real number multiplied by i. For example, 5i is imaginary; the square of 5i is -25.\n\n## What is the set of all real numbers?\n\nThe real numbers include natural numbers or counting numbers, whole numbers, integers, rational numbers (fractions and repeating or terminating decimals), and irrational numbers. The set of real numbers is all the numbers that have a location on the number line.\n\n## Can a real number be negative?\n\nThis can include whole numbers or integers, fractions, rational numbers and irrational numbers. … Real numbers can be positive or negative, and include the number zero. They are called real numbers because they are not imaginary, which is a different system of numbers." ]
[ null, "https://mc.yandex.ru/watch/66666955", null ]
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https://lbfromlv.wordpress.com/2019/05/13/the-serendipity-of-swiss-cheese-evelyn-lamb-may-3-2019/
[ "# The Serendipity of Swiss Cheese – Evelyn Lamb May 3, 2019\n\n## This holey mathematical object was discovered by a Swiss mathematician and then forgotten for decades\n\nApproximation is a recurring theme in mathematics. Sometimes it seems like all of mathematics is saying, “Well, I know how to solve the problem in this domain. Is there a way I can approximate other domains with this domain?” A lot of calculus boils down to approximating arbitrary functions with linear functions. (For our purposes, “linear” means “completely well-behaved.”) Fourier analysis, which forms the backbone of signal processing, is all about approximating complicated periodic functions with sums of simple sine waves. Scores of mathematicians spend their time thinking about what conditions allow us to approximate functions by simpler functions. A mathematical space called Swiss cheese is yet another example of the ubiquity of approximation.\n\nLike the deli counter staple, mathematical Swiss cheeses are full of holes. To make a Swiss cheese, we start with a closed disc or filled-in circle, the set of all points in the plane that are less than or equal to a given distance (the radius) from a central point.\n\nNow we punch it full of holes in a particular way. We want to remove open discs (filled-in discs, but without their boundaries), and we have some rules about the removed discs. If you look up definitions of Swiss cheeses in math, you will see a various definitions, but just like Emmentaler and Gruyére, they are just different particular varieties that all count as Swiss cheese.\n\nThis being theoretical math, we remove an infinite number of discs, but we require that the sum of the areas of the removed discs is less than the area of the original disc (often quite a bit less), that no two removed discs overlap, and that the resulting space has no interior. That is, if we zoom in on any part of the space, no matter how small, there are holes in it. It’s hard to imagine such a space (and impossible to draw it, which didn’t stop me), but there are ways to make sure the definition works mathematically.", null, "An approximation of a mathematical Swiss cheese. It’s very difficult to draw a picture with interesting features at arbitrarily small scales. Credit: Evelyn Lamb\n\nSwiss mathematician Alice Roth, the first person to describe these spaces, was trying to understand the limits of approximations of continuous functions by rational functions in the complex plane. A rational function is the ratio of two polynomials. Polynomials might be familiar to you from algebra classes. They are some of the simplest and easiest to understand functions. They have expressions like z+5 or z3-9z+7. Rational functions have expressions like (z3-9z+7)/(z+5).\n\nIs it always possible to approximate continuous functions by rational functions, or are there some spaces where this fails? Roth and other mathematicians showed that there are continuous functions on Swiss cheeses that cannot be approximated by rational functions.\n\nI am both a mathematician and a lover of cheese, so when I first heard that there were mathematical objects called Swiss cheeses, I was intrigued. The related research paper titles were delightful. Abstract Swiss Cheese Space and the Classicalisation of Swiss Cheeses. Swiss cheeses, rational approximation and universal plane curves. On the volume of the intersection of two Wiener sausages. (That last paper describes Swiss cheese-related calculations on another punny mathematical space called a Wiener sausage. Mathematicians like food.) Everything about this was relevant to my interests. When I learned about the history of the name, it got even better.\n\nArticle continues:" ]
[ null, "https://static.scientificamerican.com/blogs/assets/Image/swisscheese2.png", null ]
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https://math.answers.com/questions/How_much_is_0.73_kg_in_pounds
[ "", null, "", null, "", null, "", null, "0\n\n# How much is 0.73 kg in pounds?\n\nThe answer is 1.609 lbs (approx.). Kilogram is the SI unit of mass and pound is an imperial unit of mass. To convert from kg to pound, multiply the kg unit by 2.20462.", null, "Study guides\n\n20 cards\n\n## A number a power of a variable or a product of the two is a monomial while a polynomial is the of monomials\n\n➡️\nSee all cards\n3.79\n1504 Reviews\n\n0.73 kilograms = 1.60937451 pounds", null, "", null, "Earn +20 pts", null, "", null, "" ]
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https://www.slideserve.com/wenda/lecture-25
[ "", null, "Download", null, "Download Presentation", null, "Lecture 25\n\n# Lecture 25\n\nDownload Presentation", null, "## Lecture 25\n\n- - - - - - - - - - - - - - - - - - - - - - - - - - - E N D - - - - - - - - - - - - - - - - - - - - - - - - - - -\n##### Presentation Transcript\n\n1. Lecture 25 Introduction to steady state sinusoidal analysis Overall idea Qualitative example and demonstration System response to complex inputs Complex arithmetic review Phasor representation of sinusoids Related educational modules: Section 2.7.0, 2.7.1, 2.7.2\n\n2. Steady state sinusoidal response – overview • We have examined the natural response and step response of electrical circuits • We now consider the forced response of a circuit to sinusoidal inputs • We will only consider the steady state response to the sinusoidal input • Apply a sinusoidal input and let t   • The steady state sinusoidal response • Corresponds to the particular solution\n\n3. Why is this important? • Sinusoidal signals are very common • Power signals commonly sinusoidal (AC signals) • Carrier signals in communications often sinusoidal • The mathematics is considerably simpler • Differential equations become algebraic • System behavior often specified in terms of the system’s steady-state sinusoidal response • Example: Audio system specifications • It’s “natural” – our senses often work this way\n\n4. System response to sinusoidal input • Apply a sinusoidal input, beginning at t = 0 • u(t) = Acos(t + ), t>0\n\n5. Sinusoidal response of linear systems • The steady state response of a linear system, to a sinusoidal input, will be a sinusoid of the same frequency (particular solution of same form as input) • The amplitude and phase can change • These changes are, in general, a function of the frequency\n\n6. - • Demo system response • Sinusoidal input to tower • Indicate response: transient, steady-state, frequency dependence\n\n7. RL circuit steady state sinusoidal response • Apply a sinusoidal input to RL circuit: u(t) = Acos(t + ) • Governing equation (t):\n\n8. - • Note on previous slide that di/dt is NOT zero for steady-state sinusoidal response!\n\n9. Determining steady state sinusoidal responses • Obtaining solutions in terms of sines and cosines is tedious! • Try a “trick” involving complex exponentials: Acos(t + ) = Re{Aej(t+)} = Re{Aejejt} • Look at the response of the system to a complex exponential input, Aejejt • Results in a complex exponential response, Bejejt • The actual input is the real part of the complex input • The actual output is the real part of the complex output\n\n10. - • Note: Complex exponentials previously discussed in lecture 21. • We’ll do a little review, but it may be worthwhile for you to review lecture 21, if you are insecure about complex exponentials – we’ll be using them a LOT now • Point out that complex input not physically realizable!\n\n11. RL circuit response – revisited • Apply a complex exponential input: u(t) = Aej ejt • Governing equation (t) • Assume form of solution:\n\n12. - • Annotate last bullet of previous slide, to show di/dt and where terms go in governing differential equation\n\n13. RL circuit response to complex input • Substitute assumed solution into governing equation: • We can cancel ejt : • Since [Lej+R] is simply a complex number:\n\n14. - • Note in previous slide: • In equation 1, we no longer have a differential equation – it’s algebraic! • In equation 2, the governing equation is no longer even a function of time! (The coefficients are, however, functions of frequency) • The drawback: complex numbers are now involved. (Point out in equation 2) • We will do a little complex arithmetic review in the next few slides.\n\n15. Complex numbers – review • Rectangular coordinates: • Polar coordinates: • Relationships:\n\n16. Review of complex arithmetic • Given two complex numbers: • Addition: • Subtraction:\n\n17. Review of complex arithmetic – continued • Same two complex numbers: • Multiplication: • Division:\n\n18. Review of complex arithmetic • Same two complex numbers, but in polar form: • Multiplication: • Division:\n\n19. - • Annotate first “division” equation to note that 1/exp(phi) = exp(-phi)\n\n20. Complex arithmetic – summary • Addition, subtraction generally easiest in rectangular coordinates • Add or subtract real and imaginary parts individually • Multiplication, division generally easiest in polar coordinates • Multiplication: multiply magnitudes, add phases • Division: divide magnitudes, subtract phases\n\n21. Phasors • Recall: • Complex exponentials can be used to represent sinusoids • Complex exponentials can be written as a complex number multiplying a time-varying complex exponential • The complex number Aejprovides the magnitude and phase of the original sinusoidal signal\n\n22. Phasors – definition • The complex number (in polar form) providing the magnitude and phase of a sinusoidal signal is called a phasor.\n\n23. Example • Use phasors to determine the current i(t) in the circuit below if Vs(t) = Vmcos(100t).\n\n24. - • In previous slide, show: • Change of input to complex exponential • Derivation of governing differential equation.\n\n25. Example – continued • The governing differential equation is: • Since the input has the form , where is a phasor representing the input magnitude and phase, the output must be of the form , where is a phasor representing the output magnitude and phase.\n\n26. - • In previous slide, emphasize concepts. Do substitution and write algebraic equation.\n\n27. Example – still continued…\n\n28. - • In previous slide, do complex arithmetic to solve for current phasor; convert back to time domain.\n\n29. Example – Time domain signals • Input: • Response: • The response lags the input by 45" ]
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https://davidlowryduda.com/maass-murmurations/
[ "# mixedmath\n\nExplorations in math and programming\nDavid Lowry-Duda", null, "The mascot of the murmurations phenomenon. Photo by Walter Baxter, CC-BY-SA 2.0.\n\nAt the recent Hot Topics Workshop on Murmurations, we talked about the phenomenon of murmurations of $L$-functions.\n\n# Murmuration Phenomenon\n\nThe murmuration phenomenon describes certain biases in averages of coefficients of elliptic curve $L$-functions. This begins with certain families $\\mathcal{E}$ of elliptic curves, where each curve $E \\in \\mathcal{E}$ has an $L$-function of the shape1 1I betray may analysis background in the notation, both in calling it $L(s, E)$ instead of $L(E, s)$ and in denoting the coefficients $a_E(n)$.\n\n\\begin{equation*} L(s, E) = \\prod_p L_p(s, E)^{-1} = \\sum_{n \\geq 1} \\frac{a_E(n)}{n^s}, \\end{equation*}\n\nwhere $L_p(s, E) \\in \\mathbb{Z}[p^{-s}]$ has degree $\\leq 2$.\n\nIt turns out that often, the average of these coefficients when $n$ is prime has a consistent bias, that is\n\n\\begin{equation}\\label{eq:murmuration} \\mathbb{E}_{E \\in \\mathcal{E}}\\; \\big( a_E(p) \\big) \\end{equation}\n\nis not random; these averages tend to particular values depending on $p$.\n\nThe shape of the families is relevant. For elliptic curves, the initial natural families were isogeny classes of elliptic curves with fixed rank, with conductors in a certain range $[N_1, N_2]$, or perhaps a dyadic range $[N, 2N]$. As $N$ in the dyadic ranges increase, the expected values of $a_E(p)$ appear to tend to a particular curve.\n\nThis set might not feel natural, but each specialization is very natural. Isogenous elliptic curves have almost everywhere the same $L$-function; thus choosing a single curve from each isogeny class doesn't omit much. And the parity of the rank is known to effect the number of points on elliptic curves (though the intuitive description of this effect is perhaps incorrect, as demonstrated in the murmuration phenomenon).\n\nSince the first murmurations of elliptic curves were identified, several other murmuration phenomena have been discovered. The focus of the workshop was to try to identify explanations and further directions of inquiry.\n\n## Nonarithmetic murmurations\n\nWe can ask whether the murmuration is an arithmetic phenomenon or an analytic phenomenon. The most studied cases are all arithmetic so far: elliptic curves, modular forms, and Dirichlet characters.\n\nMaass forms provide a non-arithmetic source of $L$-functions. My Maass form co-computer and collaborator Andrei Seymour-Howell and I were both attending and we have various types of Maass forms computed and sitting in our hard drives. Along with Kumar Murty, Peter Sarnak, and several others, we sought to experiment with Maass form murmurations.\n\nWe ask: are there murmations of Maass forms?\n\nTo investigate, we use our largest set of data: weight $0$, level $1$ Maass forms with eigenvalue parameter $R$ tending upwards. In analogy to elliptic curves, we might expect that the parity of the Maass form (which amounts to the root number or the precise shape of the functional equation) to have an effect. Thus we consider families of Maass forms $\\mathcal{M}^{\\pm}([R_1, R_2])$ consisting of level $1$, weight $0$ Maass forms with given $\\pm$ parity and whose eigenvalue parameter $R \\in [R_1, R_2]$.\n\nPrecisely, a Maass form of weight $0$ and level $1$ will have an expansion of the form \\begin{equation*} f(z) = \\sum_{n \\geq 1} a_f(n) \\sqrt{y} K_{iR}(2 \\pi \\lvert n \\rvert y) \\mathrm{cs}(2 \\pi n x), \\end{equation*} where $\\mathrm{cs}(x)$ is either $\\sin(x)$ or $\\cos(x)$ depending on whether the Maass form is odd or even, respectively, and $K_{\\nu}(x)$ is the modified $K$-Bessel function (sometimes called of third kind).\n\nTo investigate if we have a murmuration phenomenon, we look at points \\begin{align}\\label{eq:maassmurmur} &\\mathbb{E}_{f \\in \\mathcal{M}^{\\pm}([1.25^\\ell, 1.25^{\\ell+1}])} \\; \\big( a_f(p) \\sqrt{p} \\big) \\\\ &\\qquad = \\frac{1}{\\# \\mathcal{M}^{\\pm}([1.25^\\ell, 1.25^{\\ell+1}])} \\sum_{f \\in \\mathcal{M}^{\\pm}([1.25^\\ell, 1.25^{\\ell+1}])} a_f(p) \\sqrt{p} \\notag \\end{align} for increasing values of $\\ell$. We do this separately for even ($\\mathcal{M}^+$) and odd ($\\mathcal{M}^-$) forms in the plots below.", null, "Gif of odd Maass forms. Each plot shows forms with spectral parameter in a certain range $[1.25^{\\ell}, 1.25^{\\ell + 1}]$. The label at the top is $\\ell$. The line is a local best-fit line. Viewing the gif in its own tab gives higher resolution.", null, "Gif of even Maass forms. Each plot shows forms with spectral parameter in a certain range $[1.25^{\\ell}, 1.25^{\\ell + 1}]$. The label at the top is $\\ell$. The line is a local best-fit line. Viewing the gif in its own tab gives higher resolution.\n\nThese plots include data from all Maass forms with eigenvalue up to approximately $30000$ (with eigenvalue parameter up to about $180$).\n\nSeveral patterns announce themselves when these two sets of points are plotted together. Here, blue = even and orange = odd.2 2As apocryphally said in murmurations, blue is always on top... until it's not.\n\n## Patterns in the Plots\n\nThese plots suggest a murmurations phenomenon in Maass forms. Murmurations are perhaps nonarithmetic, and instead analytic.3 3In some sense, it appears that they are shadows of various trace formulas.\n\nHere are the last three frames.", null, "", null, "", null, "Some observations:\n\n1. It seems that the averages are tending to a particular shape. As with other murmuration phenomena, the coherence increases in larger multiplicative ranges, but decreases as $p$ increases.\n2. The parity of the Maass forms leads to similar but oppositely signed murmurations.\n3. The current murmurations appear to be travelling waves. This suggests that they are incorrectly normalized.\n\nThis is consistent with Jonathan Bober's observation that murmurations seem to describe behavior not as averages over certain primes, but instead as averages over coefficients near $p/Q$, where $Q$ is the conductor.\n\nI intend on returning to this later and seeing if a different normalization stabilizes the travelling wave. In a different note, I intend on describing a different set of observations on murmurations for holomorphic modular forms (with Bober, Booker, and Seymour-Howell) that also supports the $p/Q$ observation.\n\n## An alternative sum from Kuznetsov\n\nA similar sum of coefficients of Maass forms appears in the Kuznetsov trace formula. We state this now.\n\nDefine the Kloosterman sum by \\begin{equation*} S(m, n; c) := \\sideset{}{'}\\sum_{d \\bmod c} e\\Big(\\frac{md + n\\overline{d}}{c}\\Big), \\end{equation*} where the primed summation indicates that the sum is over residue classes $d$ prime to $c$, and where $d \\overline{d} \\equiv 1 \\bmod c$. For any sufficiently nice even, holomorphic function $h$, we define \\begin{equation*} k^*(x) = \\frac{i}{\\pi} \\int_{-\\infty}^{\\infty} \\big(J_{2 i r}(x) - J_{- 2 i r}(x) \\big) \\frac{r h(r)}{\\cosh(\\pi r)} \\, dr. \\end{equation*}\n\nThen the Kuznetsov trace formula (for level $1$, weight $0$) says that \\begin{align*} &\\sum_{j = 1}^\\infty \\frac{h(r_j)}{\\cosh(\\pi r_j)} \\rho_j(n) \\overline{\\rho_j(m)} + \\frac{1}{\\pi} \\int_{-\\infty}^\\infty \\frac{ (n/m)^{it} \\sigma_{-2it}(n) \\sigma_{2it}(m) } { \\lvert \\zeta(1 + 2it) \\rvert^2 } h(t) \\, dt \\\\ &\\qquad = \\sum_{c = 1}^\\infty \\frac{S(m, n; c)}{c} k^*(4 \\pi \\sqrt{mn} \\; / c) + \\frac{4}{\\pi} \\delta_{[m=n]} k(0). \\end{align*}\n\nHere, the coefficients $\\rho_j(n)$ are the $n$th coefficients of the $j$th Maass form (which has eigenvalue $\\frac{1}{4} + r_j^2$), normalized so that the Maass form has norm $1$.\n\nAfter choosing $m = 1$, this gives an expression for \\begin{equation*} \\sum_{j \\geq 1} \\frac{\\rho_j(n)}{\\cosh(\\pi r_j)} h(r_j). \\end{equation*} Choosing $h$ to be essentially a bump function on certain intervals and squinting a bit, this looks like \\begin{equation} \\sum_{j \\geq 1} a_f(n) w_f \\end{equation} for a set of weights $w_f$ — very similar to \\eqref{eq:murmuration} and \\eqref{eq:maassmurmur}.\n\nOn this last note, Kumar Murty wrote down a short note containing the Kuznetsov trace formula statement. This is available here.4 4And as the date might suggest, I didn't upload this particularly quickly.\n\n## Ongoing Research and Discussion\n\nThere are several things to examine further here!\n\nI will continue to act as a fulcrum this, and I welcome discussion. If you would like to add something, send me an email or comment here (which still amounts to sending me an email in a certain way).\n\nbold, italics, and plain text are allowed in comments. A reasonable subset of markdown is supported, including lists, links, and fenced code blocks. In addition, math can be formatted using $(inline math)$ or $$(your display equation)$$." ]
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https://www.mrexcel.com/board/threads/true-false-values-based-on-contiguous-cells-interval.1052130/
[ "# TRUE/FALSE Values Based on Contiguous Cells (Interval)\n\n#### rkaczano\n\n##### Board Regular\nHi I need help with a conditional logic test that spans a range of predefined contiguous cells.\n\nI have a column of random numbers in A1:A10. In B1:B10, in each row, I do a True/False Test to see if a number is Less Then or Equal to its equivalent (i.e. B1 = IF(3 is <=A1, TRUE, FALSE). So I have a bunch of random TRUE and FALSE items in Column B.\n\nNow in column C I want to be able to test whether my TRUE results in Column B occur consecutively over a preset interval (range of cells). For example assume I have an interval or range input set to 4. So for example in C4 I want to be able to test whether the value in B4 is TRUE AND whether it is within a 4 cell range (interval) of values that are also TRUE. Effectively I want to identify if my TRUE is part of a collection of TRUEs.\n\nSo if you see below, I want to isolate the TRUE values in column B that are part of a 4 cell range (interval) AND are TRUE. In this example it would be the range B3:B6 that is the relevant range that conforms to the interval I have set up. It is a forward looking range so B7 would be excluded from that range. So C3:C6 would be TRUE and C7 would be FALSE. I am assuming the formula in C needs to incorporate an OFFSET function incorporating the interval and/or it needs to be an Array function.\n\nNumber Test = 3\nInterval = 4\n\nA1 7; B1 TRUE; C1 FALSE\nA2 1; B2 FALSE; C2 FALSE\nA3 10; B3 TRUE; C3 TRUE\nA4 12; B4 TRUE; C4 TRUE\nA5 15; B5 TRUE; C5 TRUE\nA6 16; B6 TRUE; C6 TRUE\nA7 2; B7 TRUE; C7 FALSE\nA8 1; B8 FALSE; C8 FALSE\nA9 0; B9 TRUE; C9 FALSE\nA10 1; B10 FALSE; C10 FALSE\n\nAny ideas?\n\n### Excel Facts\n\nGet help while writing formula\nClick the italics \"fx\" icon to the left of the formula bar to open the Functions Arguments dialog. Help is displayed for each argument.\n\n#### rkaczano\n\n##### Board Regular\nNo takers on this? Let me simplify. I have range of TRUE/FALSEs in column B. I want to reproduce those TRUE/FALSE in column C based on a constraint that says I can only have so many contiguous TRUEs. So for example, I can only have three TRUEs back-to-back. I want a formula in Column C that reads the raw data in Column B and makes the adjustment to the data based on the constraint I enter. Column B will have too many TRUEs. Column C will adjust (reduce) these.\n\nI want the constraint to be a variable (input) that I can change.\n\nThanks again.\n\n#### Marcelo Branco\n\n##### MrExcel MVP\nSee if this does what you need\n\n1st step\nCreate a named constant vertical array\nFormula > Names Manager > New\nName: arr\nRefers to: ={-3;-2;-1;0}\n\n2nd step\nArray formula in C1 copied down\n=OR(IFERROR((ROW(OFFSET(B1,N(arr),0))>=ROW(B\\$1))*(ROW(OFFSET(B1,N(arr),0))<=ROW(B\\$10)-3)*COUNTIF(OFFSET(B1,arr,0,4,1),TRUE),0)=4)\nconfirmed with Ctrl+Shift+Enter\n\nM.\n\n#### Joyner\n\n##### Well-known Member\nOk, more testing needed, but does this work?\n\n=IF(B1=FALSE,FALSE,IFERROR(COUNTIFS(B1:OFFSET(B1,-4,0),TRUE)<=4,TRUE))\n\nBy the way this:\n\n=IF(3 is <=A1, TRUE, FALSE)\n\nCould just be this:\n\n=3<=A1\n\nEdit: I think I missed this part: TRUE AND whether it is within a 4 cell range (interval)\n\nLast edited:\n\n#### Eric W\n\n##### MrExcel MVP\nA possible 2-formula solution:\n\nABCDEFGH\n1interval4\n27TRUEFALSE1FALSE\n31FALSEFALSE0FALSE\n410TRUETRUE1TRUE\n512TRUETRUE2TRUE\n615TRUETRUE3TRUE\n716TRUETRUE4TRUE\n82TRUEFALSE0FALSE\n91FALSEFALSE0FALSE\n100TRUEFALS\nE\n1FALSE\n111FALSEFALSE0FALSE\n12\n\n<tbody>\n</tbody>\nSheet3\n\nWorksheet Formulas\nCellFormula\nD2=IF(B2=FALSE,0,IF(D1=\\$H\\$1,0,D1+1))\nE2=IF(AND(B2=TRUE,MAX(OFFSET(D2,0,0,\\$H\\$1))=\\$H\\$1),TRUE)\n\n<tbody>\n</tbody>\n\n<tbody>\n</tbody>\n\n#### rkaczano\n\n##### Board Regular\nFor clarification, your two formula solution focuses on columns D and E. What is the formula are you using in Column C and how does this feed into Column D and E?\n\nThanks\n\n#### Eric W\n\n##### MrExcel MVP\nI just left in column C from your example to show that the values I generated in column E matched. Without that, it would look something like:\n\nABCDEF\n1interval4\n27TRUE1FALSE\n31FALSE0FALSE\n410TRUE1TRUE\n512TRUE2TRUE\n615TRUE3TRUE\n716TRUE4TRUE\n82TRUE0FALSE\n91FALSE0FALSE\n100TRUE1FALSE\n111FALSE0FALSE\n12\n\n<tbody>\n</tbody>\n\nWorksheet Formulas\nCellFormula\nC2=IF(B2=FALSE,0,IF(C1=\\$F\\$1,0,C1+1))\nD2=IF(AND(B2=TRUE,MAX(OFFSET(C2,0,0,\\$F\\$1))=\\$F\\$1),TRUE)\n\n<tbody>\n</tbody>\n\n<tbody>\n</tbody>\n\nNote that the formulas do require an empty row above the top line. Also, you can hide column C after you put the formulas in.\n\n#### rkaczano\n\n##### Board Regular\nYup that worked! Thanks again." ]
[ null ]
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https://worddisk.com/wiki/Integer-valued_function/
[ "# Integer-valued function\n\nIn mathematics, an integer-valued function is a function whose values are integers. In other words, it is a function that assigns an integer to each member of its domain.", null, "The floor function on real numbers. Its discontinuities are pictured with white discs outlines with blue circles.\n\nFloor and ceiling functions are examples of an integer-valued function of a real variable, but on real numbers and generally, on (non-disconnected) topological spaces integer-valued functions are not especially useful. Any such function on a connected space either has discontinuities or is constant. On the other hand, on discrete and other totally disconnected spaces integer-valued functions have roughly the same importance as real-valued functions have on non-discrete spaces.\n\nAny function with natural, or non-negative integer values is a partial case of integer-valued function." ]
[ null, "https://upload.wikimedia.org/wikipedia/commons/thumb/e/e1/Floor_function.svg/288px-Floor_function.svg.png", null ]
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https://mcqsfoundry.com/quantitative-reasoning-mcqs-with-answers-pdf-most-repeated-mcqs-in-gat-general-page-8/
[ "# Quantitative Reasoning Mcqs with Answers Pdf | Most Repeated Mcqs in GAT General Page 8\n\nQuantitative Reasoning Mcqs pdf for GAT Test Preparation | Mcqs Questions | GAT Test Preparation | Important Questions. However Today we will discuss about the important GAT / nts quantitative reasoning mcqs with answers pdf from which Quantitative Reasoning Mcqs pdf for GAT Test can be set up for the Subject of gat quantitative reasoning pdf for GAT Test upcoming paper on 12th September 2021.Similarly We have also set small quantitative and analytical reasoning mcqs pdf , verbal reasoning test pdf with answers for the GAT Test Preparation. Moreover we have recorded all GAT Test related preparation videos and sessions for the subject of quantitative reasoning mcqs with solutions , analytical reasoning mcqs for gat , verbal reasoning mcqs for gat test and most repeated mcqs in gat general for GAT Test Preparation.\n\n351         A vertical tower stands on ground and is surmounted by a vertical flagpole of height 18 m. At a point on the ground, the angle of elevation of the bottom and the top of the flagpole are 30° and 60° respectively. What is the height of the tower?\n\nA.            10.40 m\n\nB.            15.57 m\n\nC.            9 m\n\nD.            12 m\n\n352         A is two years older than B who is twice as old as C. If the total of the ages of A, B and C be 27, then how old is B?\n\nA.            10 Years\n\nB.            12 Years\n\nC.            14 Years\n\nD.            16 Years\n\n353         The value of {0.54- 0.44} / {0.52- 0.42} is?\n\nA.            0.02\n\nB.            0.05\n\nC.            0.09\n\nD.            0.11\n\n354      An aeroplane when 900 m high passes vertically above another aeroplane at an instant when their angles of elevation at same observing point are 60° and 45° respectively. Approximately, how many meters higher is the one than the other?\n\nA.        381 m\n\nB.         211 m\n\nC.         169 m\n\nD.        254 m\n\n355      Train is moving with speed of 90 Km/h. How much distance it will cover in 12 mints?\n\nA.        18 km\n\nB.         16 km\n\nC.         14 km\n\nD.        12 km\n\n356      When the sun’s altitude changes from 30° to 60°, the length of the shadow of a tower decreases by 70m. What is the height of the tower?\n\nA.        60.6 m\n\nB.         140 m\n\nC.         35 m\n\nD.        20.2 m\n\n357      An accurate clock shows 8 o’clock in the morning. Through how may degrees will the hour hand rotate when the clock shows 2 o’clock in the afternoon?\n\nA.        110 degree\n\nB.         120 degree\n\nC.        180 degree\n\nD.        360 degree\n\n358      The H.C.F. of two numbers is 5 and their L.C.M. is 150. If one of the numbers is 25, then the other is:\n\nA.        20\n\nB.         28\n\nC.         24\n\nD.        30\n\n359      What is the value of a and b, If a2 – b2 = 36 and a + b = 6\n\nA.        a = 1, b = 9\n\nB.         a = 6, b = 0\n\nC.         a = 3, b = 9\n\nD.        a = 0, b = 3\n\n360      The sum of the polynomials, 6x2 + 9x – 8 and 2x2 – 5x + 3 is:\n\nA.        2x2 + 4 x – 4\n\nB.         4x2 + 4 x – 1\n\nC.        8x2 + 4 x – 5\n\nD.        6x2 + 3 x – 5\n\n## GAT Test Preparation for all Subjects | NTS Quantitative Reasoning Mcqs\n\nAll important subjects like non verbal reasoning test pdf with answers, analytical reasoning mcqs with answers pdf , Quantitative reasoning mcqs with answers pdf MCQ’s are shared in detail at this platform. This is the only platform for the NTS GAT Test Preparation in which we will try to figure out verbal reasoning test with answers pdf 11 plus , and all the important areas and important type of Verbal reasoning mcqs for GAT Test Preparation questions that a candidate must be practiced and must know.\n\n361      Which of the following integers has the most number of divisors?\n\nA.        99\n\nB.         101\n\nC.         182\n\nD.        176\n\n362      The least number which should be added to 28523 so that the sum is exactly divisible by 3, 5, 7 and 8 is\n\nA.        32\n\nB.         42\n\nC.         41\n\nD.        37\n\n363      What is the greatest possible length which can be used to measure exactly the lengths 8 m, 4 m 20 cm and 12 m 20 cm?\n\nA.        30 cm\n\nB. 25 cm\n\nC.        20 cm\n\nD. 10 cm\n\n364      In class of 24 students, 1/4 are male, then % of females is:\n\nA.        60%\n\nB.         65%\n\nC.         70%\n\nD.        75%\n\n365      A is two years older than B who is twice as old as C. If the total of the ages of A, B and C be 27, then how old is B?\n\nA.        10 Years\n\nB.         12 Years\n\nC.         14 Years\n\nD.        16 Years\n\n366      A father said to his son, “I was as old as you are at the present at the time of your birth”. If the father’s age is 38 years now, the son’s age five years back was:\n\nA.        14 Years\n\nB.         16 Years\n\nC.         18 Years\n\nD.        20 Years\n\n367      The product of two 2 digit numbers is 2028 and their HCF is 13. What are the numbers?\n\nA.        13, 156\n\nB.         26, 78\n\nC.         36, 68\n\nD.        39, 52\n\n368      The product of two numbers is 2028 and their HCF is 13. What are the number of such pairs?\n\nA.        2\n\nB.         3\n\nC.         4\n\nD.        1\n\n369      A cable breaks if stretched by more than 2 mm it is cut into two equal parts how much either part can be stretched without breaking?\n\nA.        1 mm\n\nB.         2 mm\n\nC.         3 mm\n\nD.        4 mm\n\n370      Faryal got a new piggy bank and counted the change she put into it.  She had one more nickel than dimes and two fewer quarters than nickels.  The value of her change was \\$1.40.  How many total coins did she have?\n\nA.        10\n\nB.         11\n\nC.        12\n\nD.        13\n\n371      A bullet is short from a rifle. As a result the rifle recoils, the kinetic energy of rifle as compared to that of bullet is\n\nA.        Less K.E\n\nB.         Greater K.E\n\nC.         Equal K.E\n\nD.        None of these\n\n372      N is the greatest number which divides 1305, 4665 and 6905 and gives the same remainder in each case. What is the sum of the digits in N?\n\nA.        5\n\nB.         4\n\nC.         6\n\nD.        3\n\n373      A boy divided the numbers 7654, 8506 and 9997 by a certain largest number and he gets same remainder in each case. What is the common remainder?\n\nA.        156\n\nB.         211\n\nC.         231\n\nD.        199\n\n374      The average binding energy of a nucleon inside an atomic nucleus is about\n\nA.        2 MeV\n\nB.         4 MeV\n\nC.        8 MeV\n\nD.        10 MeV\n\n375      Two-fifth of a certain number is 30. What is the number?\n\n(A)       75\n\n(B)       25\n\n(C)       90\n\n(D)       150\n\n376      Sara weighs 25 pounds more than Umar. If together they weigh 205 pounds, what is the weight of Sara?\n\n(A)       90\n\n(B)       105\n\n(C)       115\n\n(D)       135\n\n377      If the sum of two numbers is 36, and the larger is three times as larger as the smaller, what is the larger number?\n\n(A)       27\n\n(B)       30\n\n(C)       15\n\n(D)       18\n\n378      A, B, C subscribe Rs. 50,000 for a business. A subscribes Rs. 4000 more than B and B Rs. 5000 more than C. Out of a total profit of Rs. 35,000, A receives:\n\nA.        Rs. 12,700\n\nB.         Rs. 13,700\n\nC.        Rs. 14,700\n\nD.        Rs. 15,700\n\n379      A, B and C start at the same time in the same direction to run around a circular stadium. A completes a round in 252 seconds, B in 308 seconds and C in 198 seconds, all starting at the same point. After what time will they again at the starting point?\n\nA.        46 minutes 12 seconds\n\nB. 36 minutes 12 seconds\n\nC.        36 minutes 22 seconds\n\nD. 46 minutes 22 seconds\n\n380      The ratio of two numbers is 4: 5. If the HCF of these numbers is 6, what is their LCM?\n\nA.        30\n\nB.         120\n\nC.         60\n\nD.        90\n\n381      What is the HCF of 2.04, 0.24 and 0.8?\n\nA.        1\n\nB.         0.04\n\nC.         2\n\nD.        0.02\n\n382      If HCF of two numbers is 11 and the product of these numbers is 363, what is the the greater number?\n\nA.        22\n\nB.         11\n\nC.        33\n\nD.        9\n\n383      What is the greatest number which on dividing 1223 and 2351 leaves remainders 90 and 85 respectively?\n\nA.        42\n\nB.         1100\n\nC.         127\n\nD.        1133\n\n384      Which quantity is greater?\n\nQuantity A: 7-5                        Quantity B: 49-3\n\nA.        Quantity A is greater.            `\n\nB.         Quantity B is greater.\n\nC.         The two quantities are equal\n\nD.        The relationship cannot be determined from the information given\n\n385      What digit appears in the units place when 2102is multiplied out?\n\nA.        2\n\nB.         4\n\nC.         6\n\nD.        8\n\n386      A farmer has 44 feet of fence, and wants to fence in his sheep. He wants to build a rectangular pen with an area of 120 square feet. Which of the following is a possible dimension for the side opposite the barn?\n\nA.        5 ft.\n\nB.         10 ft.\n\nC.         15 ft.\n\nD.        20 ft.\n\n387      A man was 26 years old when his daughter was born. Now, he is three times as old as his daughter. How many years old is the daughter now?\n\n(A)       13 years\n\n(B)       22 years\n\n(C)       15 years\n\n(D)       12 years\n\n388      Solve for x: (x2 – x) / (x – 1) = 1\n\nA.        0\n\nB.         1\n\nC.         -1\n\nD.        No Solution\n\n389      Given that: x2 – 3x – 18 = 0\n\nQuantity A: x                          Quantity B: 6\n\nA.        Quantity A is greater\n\nB.         Quantity B is greater.\n\nC.         The two quantities are equal.\n\nD.        The relationship can’t be determined from given information\n\n390      Two masses of 1 g and 4 g are moving with equal kinetic energies the ratio of the magnitudes of their linear moments is:\n\nA.        0:10\n\nB.         1:02\n\nC.         2:1\n\nD.        1:04\n\n391      How much water a pump of 2kW can raise in one minute to a height of 10 m. take g = 10 m/s2?\n\nA.        1000 litres\n\nB.         1200 litres\n\nC.         20000 litres\n\nD.        22000 litres\n\n392      What is the least multiple of 7 which leaves a remainder of 4 when divided by 6, 9, 15 and 18 ?\n\nA.        343\n\nB.         350\n\nC.         371\n\nD.        364\n\n393      Three numbers which are co-prime to each other are such that the product of the first two is 119 and that of the last two is 391. What is the sum of the three numbers?\n\nA.        43\n\nB.         51\n\nC.        47\n\nD.        53\n\n394      What is the greatest number which divides 24, 28 and 34 and leaves the same remainder in each case?\n\nA.        2\n\nB.         1\n\nC.         3\n\nD.        4\n\n395      Six bells start ringing together and ring at intervals of 4, 8, 10, 12, 15 and 20 seconds respectively. How many times will they ring together in 60 minutes?\n\nA.        31\n\nB.         15\n\nC.         30\n\nD.        16\n\n396      What is the least number which when divided by 8, 12, 15 and 20 leaves in each case a remainder of 5?\n\nA.        125\n\nB.         112\n\nC.         117\n\nD.        132\n\n397      Jamal has \\$15,000 to invest. If he invests two-thirds of it into a high-yield savings account with an annual interest rate of 8%, compounded quarterly, and the other third in a regular savings account at 6% simple interest, how much does Jamal earn after one year?\n\nA.        \\$1024.32\n\nB.         \\$1124.32\n\nC.         \\$1224.32\n\nD.        \\$1324.32\n\n398      The HCF of two numbers is 23 and the other two factors of their LCM are 13 and 14. What is the largest number?\n\nA.        282\n\nB. 322\n\nC.         312\n\nD. 299\n\n399      What is the smallest number which when diminished by 12, is divisible 8, 12, 22 and 24?\n\nA.        272\n\nB.         268\n\nC.        276\n\nD.        264\n\n400      A and B invest in a business in the ratio 3: 2. If 5% of the total profit goes to charity and A’s share is Rs. 855, the total profit is:\n\nA.        Rs. 1200\n\nB.         Rs .1300\n\nC.         Rs. 1400\n\nD.        Rs. 1500\n\nMCQsFoundry.com brings to you all Quantitative Reasoning Mcqs pdf for GAT Test Preparation with answers pdf which are new and latest. These Quantitative Reasoning Mcqs pdf for GAT Test Preparation  with answers pdf are never published on internet so far. For full information about all GAT / PPSC / FPSC / CSS / PMS latest jobs visit theiteducation.com\n\nWe are providing accurate Quantitative Reasoning Mcqs pdf . Firstly You can read Quantitative Reasoning Mcqs pdf for GAT Test Preparation . Secondly What you have to do is to attempt Quantitative Reasoning Mcqs pdf  test with answers For GAT Test Preparation. Thirdly If you want to attempt Quantitative Reasoning Mcqs pdf Quiz and also for the other preparations then keep visiting this website.\n\nMoreover At this platform you are able to read non verbal reasoning test with answers pdf , analytical reasoning mcqs with answers pdf , logical reasoning test with answers pdf and 11+ verbal reasoning test with answers pdf for the NTS / GAT Test Preparation then you are at the right place . Moreover if you want to test yourself or want to take any quiz, related to these Quantitative Reasoning Mcqs pdf then you are also able to take Quantitative Reasoning Mcqs pdf Quiz ." ]
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https://www.ncatlab.org/nlab/show/duality
[ "duality\n\n# Duality\n\n## Idea\n\nInstances of “dualities” relating two different, maybe opposing, but to some extent equivalent concepts or phenomena are ubiquitous in mathematics (and in mathematical physics, see at dualities in physics). The term “duality” is widespread and doesn’t have a single crisp meaning, but a rough guiding intuition is of pairs of concepts that are mirror images of one another.\n\n## General notions\n\nIn terms of general abstract concepts in logic and category theory, instances of dualities might be (and have been) organized as follows.\n\n### Abstract/formal/axiomatic duality\n\nInstances here include projective duality, duality in lattice theory, and duality in category theory. In each case, one has a theory whose signature admits a nontrivial involution, in such a way that “dualizing” or applying the involution to any axiom of the theory (but otherwise preserving the logical structure of formulae) results in another theorem of the theory. For example, for the theory of projective planes, the involution swaps points and lines, meets and joins, etc., and for each theorem there is a dual theorem. Similarly, in category theory, the involution swaps the domain and codomain and order of composition, etc., and for any theorem of formal category theory, the corresponding dual statement is also a theorem (because the set of axioms of category theory are closed under taking formal duals).\n\nSuch formal duality can also be expressed at the level of models of the theory $T$: for each model $M$ there is a “dual” or “opposite” model $M^{op}$ obtained by re-interpreting each formal sort/function/relation of the theory as the dual sort/function/relation. This further induces an involution $Mod(T) \\to Mod(T)$ on the category of models. For example, in the case of category theory, this operation $C \\mapsto C^{op}$, mapping a category $C$ to its opposite category, gives an involution $(-)^{op}: Cat \\to Cat$ on the category Cat of (small) categories, viewing $Cat$ here as a 1-category. In fact this is the only non-trivial automorphism of Cat, see here).\n\nThis involution $(-)^{op}: Cat \\to Cat$ is also known as abstract duality. While the construction is a priori tautologous, any given opposite category often is equivalent to a category known by other means, which makes abstract duality interesting (particularly so in cases of concrete duality, which we discuss next).\n\n### Concrete dualities\n\nInstances here include linear duality, Stone duality, Pontryagin duality, and projective inversions with respect to a conic hypersurface. In each such case there is some contravariant process of “homming into” a suitable structure $V$ called a dualizing object, which in the classical cases of what we will call “perfect duality”, induces an equivalence of categories $C^{op} \\stackrel{\\sim}{\\to} D$ where typically $C$ is the category of models of one type of concrete structure, and the equivalence maps the formal categorical dual $C^{op}$ to a category of models $D$ consisting of “dual” concrete structures.\n\nIn other cases one might not obtain an equivalence or perfect duality, but in any case a contravariant adjoint pair of functors $S: C \\to D$, $T: D \\to C$ between categories which can be termed a duality of sorts, in that concepts developed in $C$ are mapped to dual concepts in $D$ and vice-versa. Quoting (Lawvere-Rosebrugh, chapter 7):\n\nNot every statement will be taken into its formal dual by the process of dualizing with respect to $V$, and indeed a large part of the study of mathematics\n\nspace vs. quantity\n\nand of logic\n\ntheory vs. example\n\nmay be considered as the detailed study of the extent to which formal duality and concrete duality into a favorite $V$ correspond or fail to correspond. (p. 122)\n\nSome examples follow.\n\n• In linear duality, say for vector spaces over a field $k$, the dual of a space $W$ is $W^\\ast = \\hom(W, k)$, the hom of $k$-linear maps into $k$. This induces a contravariant functor $(-)^\\ast: Vect_k \\to Vect_k$ that is adjoint to itself, in that there is a double-dual embedding $\\delta_W: W \\to W^{\\ast\\ast}$ such that\n\n$1_{W^\\ast} = (W^\\ast \\stackrel{\\delta_{W^\\ast}}{\\to} W^{\\ast\\ast\\ast} \\stackrel{(\\delta_W)^\\ast}{\\to} W^\\ast).$\n\nThis becomes a perfect duality if we restrict to finite-dimensional vector spaces, i.e., the contravariant functor $(-)^\\ast: Vect_{fd} \\to Vect_{fd}$ is adjoint-equivalent to itself (i.e., the covariant functor $((-)^\\ast)^{op}: Vect_{fd} \\to Vect_{fd}^{op}$ is left adjoint to $(-)^\\ast: Vect_{fd}^{op} \\to Vect_{fd}$ and the adjunction is an adjoint equivalence).\n\n• More generally, given a (usually symmetric) monoidal closed category $\\mathcal{C}$, any object $D$ induces an operation $[-,D] : \\mathcal{C} \\to \\mathcal{C}^{op}$ obtained by forming the internal hom into $D$, sending each object to what may be termed its $D$-dual object. There is a corresponding double-dual embedding $\\delta_C: C \\to [ [C, D], D]$ obtained as the composite\n\n$C \\to [ [C, D], C \\otimes [C, D]] \\to [ [C, D], [C, D] \\otimes C] \\to [ [C, D], D]$\n\nwhere the first arrow uses the unit of an adjunction $(- \\otimes B) \\dashv [B, -]$ where $B = [C, D]$, the second uses a symmetry isomorphism $C \\otimes B \\cong B \\otimes C$, and the third uses the counit of an adjunction $(- \\otimes C) \\dashv [C, -]$, aka an evaluation map. It may be shown that the contravariant functor $(-)^\\ast \\coloneqq [-, D]: \\mathcal{C} \\to \\mathcal{C}$ is again dual to itself, exactly as in the case of linear duality above, where we have a triangular equation\n\n$1_{C^\\ast} = (\\delta_C)^\\ast \\circ \\delta_{C^\\ast}$\n\nfor an adjunction $[-, D]^{op} \\dashv [-, D]$. Under certain circumstances, we have perfect duality, i.e., double dualization $[ [-, D], D]: \\mathcal{C} \\to \\mathcal{C}$ is an equivalence; see dualizing object in a closed category and star-autonomous category. Particular special cases of this may obtain when $D = I$, the monoidal unit, or even more particularly when every object has a dual object in the sense of monoidal categories; see also compact closed category. On the other hand, there is also a mild generalization of this type of example where we deal with a biclosed monoidal category; here the double dualization will involve both the left and right internal hom.\n\n• More general still is a concrete duality induced by a dualizing object. In this case one is given a pair of categories together with underlying-set functors\n\n$U: \\mathcal{C} \\to Set, \\qquad V: \\mathcal{D} \\to Set$\n\n(and often when one says “concrete”, one intends that these functors be faithful as well, so that $\\mathcal{C}, \\mathcal{D}$ can be viewed as “sets with structure”; see stuff, structure, property). The concrete duality consists of a pair of objects $C \\in \\mathcal{C}, D \\in \\mathcal{D}$ together with an isomorphism $\\omega: U C \\cong V D$, such that the contravariant homs $\\hom(-, C): C^{op} \\to Set$ and $\\hom(-, D): D^{op} \\to Set$ lift to a contravariant adjunction between $C$ and $D$, in the sense described here. Frequently in practice, such concrete dualities are “naturally represented” in the sense described here, involving certain lifts adapted from the theory of topological concrete categories.\n\nAgain, in all of these examples, one can consider the further condition of “perfect duality” where the units and counits of the (lifted) adjunctions are isomorphisms.\n\nPerhaps the loosest general notion of “duality” is that of adjunction, as in pairs of adjoint functors (Lambek 81). Here one may omit any concretizations via functors to $Set$, or even for that matter any explicit mention of opposite categories, and just work at the level of abstract categories themselves.\n\nNevertheless, many adjunctions come packaged in “dual pairs”. A famous slogan from Categories for the Working Mathematician is that “all concepts are Kan extensions”, and in that light the dual pairs are instances of the general dual pair “(right Kan extension, left Kan extension)” which are formal duals in the axiomatic sense described earlier. Via the many incarnations of universal constructions in category theory, we have for example\n\nWhen the adjoint functors are monads and hence modalities, then adjointness between them has been argued to specifically express the concept of duality of opposites.\n\nAgain, adjunctions and specifically dual adjunctions (“Galois connections”) may be thought of as generalized dualities, more general than “perfect duality” which involves equivalences between categories (“Galois correspondences”). However, it should also be noted that any such adjunction (or dual adjunction) restricts to a maximal (dual) equivalence between subcategories, by considering objects where the appropriate units and counits are isomorphisms. This generalizes the manner by which any Galois connection induces a Galois correspondence (where in this special case, one need only take the images of the poset maps which constitute the connection).\n\n## Dualizing objects\n\nOf particular interest are concrete dualities between concrete categories $C, D$, i.e. categories equipped with faithful functors\n\n$f : C \\to Set$\n\nto Set, which are represented by objects $a \\in C$, $\\hat a \\in D$ with the same underlying set $f(a) = \\hat f(\\hat a)$. Such objects are known as dualizing objects.\n\nDiscussion of duality specifically in homological algebra and stable homotopy theory with emphasis on the concept of dualizing object in a closed category (and the induced Umkehr maps etc.) is in" ]
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http://swift-nav.github.io/plover/tutorials.html
[ "View on GitHub\n\n# Plover Tutorials\n\nThis part of the documentation gives worked examples of using Plover.\n\n# Matrix Multiplications\n\nA quick application of using Plover is to create bespoke functions which operate on matrices. A very basic example is a matrix times a vector:\n\nmul_mat_vec {m,n} (A :: double[m,n]) (v :: double[n]) :: double[m]\n:= A * v;\n\n\nThis function takes two implicit arguments (m and n) which give the dimensions of the $$m\\times n$$ matrix A and an $$n$$-dimensional vector v. Putting this into a file called mats.plv, we compile it with Plover using\n\n$plover mats.plv which creates two files, mats.c and mats.h. The resulting C definition is void mul_mat_vec (const s32 m, const s32 n, const double * A, const double * v, double * result) { for (s32 idx = 0; idx < m; idx++) { double sum = 0; for (s32 idx2 = 0; idx2 < n; idx2++) { sum += A[n * idx + idx2] * v[idx2]; } result[idx] = sum; } } with a corresponding definition in the header file. The rules for creating the C function type from a Plover type are simple: the parameters for the C function appear in the same order as they appear in the Plover definition, and if the result is a vector type (i.e., non-scalar), it is appended as the last argument. The caller is responsible for allocating the memory of the returned vector. Another example is computing a quadratic form $$v^TAv$$: mat_quad_form {n} (A :: double[n,n]) (v :: double[n]) :: double := (v^T * A * v); Multiplication is left-associative, so the inner expression is the same as (v^T * A) * v. The rule for taking the transpose of an $$n$$-dimensional vector is that it becomes a $$1\\times n$$-dimensional matrix, and so the product with the $$n\\times n$$ matrix A, giving a $$1\\times n$$ matrix. This is then multiplied by the vector, and a matrix times a vector results in a vector, in this case $$1$$-dimensional. This is indexed to get the sole entry. Alternatively, the body of the function could equivalently be (A * v) * v, without indexing, where the second * is a dot product between vectors. Compiling this, the resulting C is double mat_quad_form (const s32 n, const double * A, const double * v) { double sum = 0; for (s32 idx = 0; idx < n; idx++) { double sum2 = 0; for (s32 idx2 = 0; idx2 < n; idx2++) { sum2 += v[idx2] * A[n * idx2 + idx]; } sum += sum2 * v[idx]; } return sum; } Notice that the Plover compiler does not generate the intermediate matrix product. This is because the later multiplication informs the first that it will only be evaluating each element of the first at most once, so the elements may be computed on demand. Suppose that the vector were instead a matrix. That is, mat_quad_prod {n,m} (A :: double[n,n]) (B :: double[n,m]) :: double[m,m] := B^T * A * B; Plover generates the following code: void mat_quad_prod (const s32 n, const s32 m, const double * A, const double * B, double * result) { double tmp [m * n]; for (s32 idx = 0; idx < m; idx++) { for (s32 idx2 = 0; idx2 < n; idx2++) { double sum = 0; for (s32 idx3 = 0; idx3 < n; idx3++) { sum += B[m * idx3 + idx] * A[n * idx3 + idx2]; } tmp[n * idx + idx2] = sum; } } for (s32 idx = 0; idx < m; idx++) { for (s32 idx2 = 0; idx2 < m; idx2++) { double sum = 0; for (s32 idx3 = 0; idx3 < n; idx3++) { sum += tmp[n * idx + idx3] * B[m * idx3 + idx2]; } result[m * idx + idx2] = sum; } } } Since the second product will use the elements of the first product multiple times, the compiler memoizes (or spills) the result onto the stack. If n is large relative to m this might be unacceptable behavior on an embedded system, and we may be willing to trade stack space for computation time. Plover gives the nomemo operator to control whether a request to memoize an intermediate value will be acknowledged. This does not change the result of a computation, but it might change whether the computation is computable on a given system. Concretely: mat_quad_prod_safe {n,m} (A :: double[n,n]) (B :: double[n,m]) :: double[m,m] := nomemo (B^T * A) * B; gives void mat_quad_safe (const s32 n, const s32 m, const double * A, const double * B, double * result) { for (s32 idx = 0; idx < m; idx++) { for (s32 idx2 = 0; idx2 < m; idx2++) { double sum = 0; for (s32 idx3 = 0; idx3 < n; idx3++) { double sum2 = 0; for (s32 idx4 = 0; idx4 < n; idx4++) { sum2 += B[m * idx4 + idx] * A[n * idx4 + idx3]; } sum += sum2 * B[m * idx3 + idx2]; } result[m * idx + idx2] = sum; } } } # Computing Correlation Vectors The cross-correlation of two (real-valued) signals $$f$$ and $$g$$ is defined to be \\begin{equation*} (f \\star g)[i] = \\sum_{j=-\\infty}^\\infty f[j] g[j+i] \\end{equation*} For periodic signals with period $$N$$, the bounds of the sum can be restricted to having length $$N$$, and, if we model $$f$$ and $$g$$ as being vectors of length $$N$$, this amounts to a dot product of $$f$$ by a cyclic shift of $$g$$. In Plover, the right-hand side can be written as f * (g[i:] # g[:i]). The * operator computes the dot product when given vector operands, and the # operator concatenates two vectors. Like in Python or Matlab, vectors can be sliced by indexing them with a range of values. The lower- or upper- bounds may be omitted on the range operator :, and they default to the bounds of the sliced vector. Here, i: and :i are equivalent to the vectors vec(i,i+1,...,N-1) and vec(0,1,...,i-1), respectively. With this, we can make a function which computes all of the cross-correlations of two vectors of length N: cross_cor {N} (f :: double[N]) (g :: double[N]) :: double[N] := vec i in N -> f * (g[i:] # g[:i]); The declaration for the function gives N as an implicit parameter, f and g as vectors of length N with double-precision floating-point numbers as values, and a return type which is also a vector of length N with doubles as values. The body of the function is given after the := definition operator. The body creates a new vector of length N with i iterating over that range, computing the cross-correlation for each offset i. Note The cross-correlation function can also be written as: cross_cor {N} (f :: double[N]) (g :: double[N]) :: double[N] := vec i in N -> f * g[(i:i+N) % N]; since arithmetic operators coerce their operands into vectors of compatible size and then vectorize the operation elementwise. Auto-correlation is the cross-correlation of a vector with itself. Given the above definition, we may write auto_cor {N} (f :: double[N]) :: double[N] := cross_cor f f; Since the first argument to cross_cor is implicit, Plover will try to determine a valid argument to place there, which it will determine using f and the return type for auto_cor. If we wish to be explicit, we may instead write cross_cor {N} f f to pass the implicit argument N. Putting these into a file called cor.plv, we may compile them to C by entering the directory and running $ plover cor.plv\n\n\nThis creates a files called cor.h and cor.c, with cor.c containing the following definitions:\n\nvoid cross_cor (const s32 N, const double * f, const double * g, double * result)\n{\nfor (s32 idx = 0; idx < N; idx++) {\ns32 i = idx;\ndouble sum = 0;\n\nfor (s32 idx2 = 0; idx2 < N; idx2++) {\ndouble tmp;\n\nif (idx2 < -i + N) {\ntmp = g[i + idx2];\n} else {\ntmp = g[idx2 - (-i + N)];\n}\nsum += f[idx2] * tmp;\n}\nresult[idx] = sum;\n}\n}\nvoid auto_cor (const s32 N, const double * f, double * result)\n{\ncross_cor(N, f, f, result);\n}\n\n\nThe auto-correlation of a random vector approximates a delta function as the length of the vector goes to infinity. We will make a test which demonstrates this.\n\nimport prelude;\n\nmain () :: int :=\n( v := normalize (vec i in 1000 -> rand_normal());\nprint_vec $auto_cor v; return 0; ); This imports the standard Plover library, and defines a main function. The function creates a vector of 1000 random doubles, normally distributed, and normalizes the vector so that its Euclidean length is 1. After this, the auto-correlation vector is printed. In Plover, the dollar sign acts like an open parenthesis which extends to the end of an expression. Compiling and running this file with: $ plover cor.plv\n$gcc cor.c prelude.c -o cor$ ./cor\n\n\nshows that the 0th element is 1.0 (since this entry represents the dot product of the vector with itself), and the rest are relatively small. We can measure this with the following code:\n\nvec_mean {n} (v :: double[n]) :: double :=\nsum v / n;\n\nmain () :: int :=\n( w := vec N in 2:2000 -> (\nv := normalize $vec i in N -> rand_normal(); av := auto_corr v; vec_mean$ av[1:] .* av[1:]\n);\nprint_vec w;\nreturn 0;\n);\n\n\nThe .* operator is the point-wise product (\"Hadamard\" product) and effectively squares each element in the array. So w is a vector of the mean of the squares of the non-zero-offset auto-correlations for various sizes of random vectors. Plotting this vector in a graphing application, one can see the errors decrease with the inverse of the size of the vectors.\n\n# Programming a QR Least Squares Solver\n\nWe're going to step through the implementation of a textbook algorithm: a QR least squares solver for overdetermined systems. That is, given $$A\\in \\R^{m\\times n}$$ and $$b\\in \\R^m$$ with $$m \\geq n$$, we want to find a vector $$x\\in\\R^n$$ such that the squared error $$\\norm{Ax-b}$$ is minimized. We give a brief explanation of the math first, following [MC2013].\n\nSuppose we can compute an orthogonal matrix $$Q\\in\\R^{m\\times m}$$ such that\n\n\\begin{equation*} Q^T A = R = \\begin{bmatrix}R_1 \\\\ 0 \\end{bmatrix} \\begin{matrix} \\scriptstyle n \\\\ \\scriptstyle m-n \\end{matrix} \\end{equation*}\n\nwhere $$R_1\\in \\R^{n\\times n}$$ is upper triangular. Then we can write\n\n\\begin{equation*} Q^T b = \\begin{bmatrix}c \\\\ d \\end{bmatrix} \\begin{matrix} \\scriptstyle n \\\\ \\scriptstyle m-n \\end{matrix} \\end{equation*}\n\nand we note that\n\n\\begin{equation*} \\norm{Ax-b} = \\norm{Q^TAx-Q^Tb} = \\norm{R_1x-c}+\\norm{d} \\end{equation*}\n\nIf $$A$$ is full rank, we can solve the system $$R_1x=c$$ exactly, and the remaining error is $$d$$.\n\nThe essential steps are:\n\n1. Apply orthogonal transformations to $$A$$ and $$b$$ until $$A$$'s first $$n$$ rows are upper triangular.\n2. Backsolve the triangular system.\n3. Return the solution and the error.\n\nWe will attempt to mindlessly follow the implementation given in [MC2013].\n\n## QR Factorization\n\nFirst we apply a sequence of Givens rotations to introduce zeroes into our matrix $$A$$. A Givens rotation is a pair $$c=\\cos(\\theta)$$ and $$s=\\sin(\\theta)$$ such that\n\n\\begin{equation*} \\begin{bmatrix} c & s \\\\ -s & c \\end{bmatrix}^T \\begin{bmatrix} a \\\\ b \\end{bmatrix} = \\begin{bmatrix} r \\\\ 0 \\end{bmatrix} . \\end{equation*}\n\nPseudocode to calculate such a pair follows:\n\ngivens (a, b) returns [$$c, s$$]\nif $$b = 0$$\n$$c = 1; s = 0$$\nelse if $$\\abs{b} > \\abs{a}$$\n$$\\tau = -a/b; s = 1/\\sqrt{1+\\tau^2}; c = s\\tau$$\nelse\n$$\\tau = -b/a; c = 1/\\sqrt{1+\\tau^2}; s = c\\tau$$\n\nThe plover version is below. We will step through it line by line.\n\nstatic givens (a :: double) (b :: double) :: double[2,2] := (\nc :: double;\ns :: double;\nif b == 0 then (\nc <- 1; s <- 0\n) else if fabs b > fabs a then (\ntau := -a/b; s <- 1/sqrt(1+tau^2); c <- s*tau\n) else (\ntau := -b/a; c <- 1/sqrt(1+tau^2); s <- c*tau;\n);\n\nmat( c, s ;\n-s, c );\n);\n\n\nstatic givens (a :: double) (b :: double) :: double[2,2] := (\n...\n);\n\n\nPlover is statically typed, and all functions require a type signature, although in many cases types can be inferred (see the language reference section on type holes). This function signature indicates that the function givens is static (declared static in the generated C file, with no prototype in the header file), takes two arguments a and b of type double, and returns a 2-by-2 matrix of doubles. Function declarations and variable initializations use the := operator and must be terminated by a semicolon. Blocks are enclosed by parentheses, and the expressions within a block are separated by semicolons.\n\nc :: double;\ns :: double;\n\n\nA new local variable may either be declared with a type (var :: type;) or with an initial value (var :: optional_type := value;), in which case the type is optional and can be inferred. In this case, c and s are set by each branch of the if expression below, so we declare them with only their types. Declaring a variable does not initialize it.\n\nif b == 0 then (\nc <- 1; s <- 0\n)\n\n\nThe condition of an if expression does not need enclosing parentheses. The condition must be followed by the keyword then and an expression. In this case, we have a block which updates the values of c and s. Updating variables must be done with <- . An if should be terminated by a semicolon when used as a statement.\n\nNote\n\nIn Plover, everything is an expression. Sometimes it is convenient to call an expression appearing in a block a statement.\n\nelse if fabs b > fabs a then (\ntau := -a/b; s <- 1/sqrt(1+tau^2); c <- s*tau\n) else (\ntau := -b/a; c <- 1/sqrt(1+tau^2); s <- c*tau\n);\n\n\nif statements are optionally followed by an else clause and another expression or block. Here, the fabs function is called on b and on a, and these values are compared to choose the branch. The local tau is initialized, and c and s are updated as shown in the pseudocode above. The fabs and sqrt functions are included in Plover's prelude module.\n\nmat( c, s ;\n-s, c );\n\n\nThe final expression in a block is treated as the value for that block. Here, the function returns a 2-by-2 matrix literal containing the values we've just computed. The output code below shows how this is translated into C.\n\nLet's take a look at the C code generated so far:\n\n// excerpt, qr.c\nstatic void givens (const double a, const double b, double * result);\nvoid givens (const double a, const double b, double * result)\n{\ndouble c;\ndouble s;\n\nif (b == 0) {\nc = 1;\ns = 0;\n} else {\nif (fabs(a) < fabs(b)) {\ndouble tau;\n\ntau = -(a / b);\ns = 1 / sqrt(1 + tau * tau);\nc = s * tau;\n} else {\ndouble tau;\n\ntau = -(b / a);\nc = 1 / sqrt(1 + tau * tau);\ns = c * tau;\n}\n}\nresult[2 * 0] = c;\nresult[2 * 0 + 1] = s;\nresult[2 * 1] = -s;\nresult[2 * 1 + 1] = c;\n}\n\n\nWe can see that Plover passes the result matrix as an extra argument, and stores the dense matrix in a flat array in row-major order. Arguments are by default passed const, but modifications are allowed with the out and inout parameter options; see the language reference. The rest of the code matches the input closely.\n\nNow we will use this routine to factor our matrix. Starting at the lower left corner, we go up and then right, introducing zeros with one Givens rotation at a time. Pseudocode from [MC2013]:\n\nqr_factor (m, n, A)\nfor $$j = 1:n$$\nfor $$i=m:-1:j+1$$\n$$R$$ = givens($$A(i-1,j),A(i,j)$$)\n$$A(i-1:i,j:n) = R^T A(i-1:i, j:n)$$\n\nWe pick a rotation that introduces a zero at location $$(i,j)$$ and apply it to rows i and i-1 of $$A$$, updating them in-place. Note that the second loop counts down from $$m$$ to $$j+1$$, and the arrays are one-indexed.\n\nThe Plover code:\n\nqr_update {m, n}\n(inout b :: double[m])\n(inout A :: double[m, n])\n:: Void := (\n\nfor j in 1 .. n,\ni in m .. j+1 : -1 -> (\n\n-- Givens rotation\nrot := givens A[i-2,j-1] A[i-1,j-1];\n-- Rotate one column at a time\nfor k in j..n -> (\nv := A[i-2 .. i-1, k-1];\nA[i-2 .. i-1, k-1] <- rot^T * v;\n);\n\n-- Rotate b vector\nv := b[i-2 .. i-1];\nb[i-2 .. i-1] <- rot^T * v;\n\n);\n);\n\n\nqr_update {m, n}\n(inout b :: double[m])\n(inout A :: double[m, n])\n\n\nWe use inout variables, mutating b and A as we go along. This way, we never store the Q matrix and simply return the upper triangular rotation of A.\n\n{m, n} denotes that qr_update takes two implicit int parameters. The function qr_update can be called simply with the (explicit) b and A arguments, and m and n will be inferred. If the dimensions of the explicit arguments don't match, Plover will report a type error. See the language reference for more details.\n\nfor j in 1 .. n,\ni in m .. j+1 : -1 -> (\n\n-- Givens rotation\nrot := givens A[i-2,j-1] A[i-1,j-1];\n...\n);\n\n\nPlover uses zero-indexing, but we keep the same loop bounds to avoid too much confusion in the translation. The expression a..b denotes the sequence of integers from a to b, inclusive, whereas a:b excludes the upper bound. The expression (a..b : -1) means: count from a to b with step size -1.\n\n-- Rotate one column at a time\nfor k in j..n -> (\nv := A[i-2 .. i-1, k-1];\nA[i-2 .. i-1, k-1] <- rot^T * v;\n);\n\n\nWe rotate one column at a time so that we can use a two element temporary vector v to avoid overwiting elements of A while they are still needed by the product computation. Currently, Plover will not warn you and will not automatically make a copy of the right hand side if one is needed to properly compute an update statment a <- b.\n\nThese lines also demonstrate the submatrix indexing facilities of Plover. We often use the notation v[a:b] to take the subvector of v at indices from a to b-1. These expressions can be used as l-values and as r-values, as above. They can also be passed as out arguments to a function, and the proper subvector will be updated. We can take subranges of objects with multiple indices as well: taking a row of a matrix is accomplished with M[i] or M[i, :], and taking a column is simply M[:, i]. A colon without upper or lower bounds is filled in appropriately.\n\n## Backsolving\n\nNow we have a square upper triangular constraint matrix and a target vector; we can solve this one row at a time, starting with the last.\n\nFor an upper-triangular system $$Rx=b$$, the value of $$x_i$$ is given by\n\n\\begin{equation*} x_i = \\left. \\left(b_i - \\sum_{j=i+1}^n R_{ij}x_j\\right)\\middle/ R_{ii} \\right. . \\end{equation*}\n\nThe algorithm will overwrite b[i] with this value, since it is not needed by later steps.\n\n-- Back substitution for upper triangular U\nstatic backsolve {n}\n(U :: double[n,n])\n(inout b :: double[n])\n:: s8 := (\nfor i in 0:n ->\nif U[i,i] == 0 then\nreturn -1;\n\nb[n-1] <- b[n-1]/U[n-1, n-1];\n\nfor i in n-1 .. 1 : -1 -> (\nb[i-1] <- (b[i-1] - U[i-1, i : n] * b[i : n]) / U[i-1, i-1];\n);\n\nreturn 0;\n);\n\n\nThe * inside the for loop is shorthand for a dot product. We add a check to see if any of the diagonal entries are 0 and return an error code as a signed byte.\n\n## Complete Solver\n\nFinally, the completed algorithm:\n\n-- Assumes m >= n\n-- See \"Matrix Computations\" 4th ed. Golub and Van Loan\nqr_solve {m, n}\n(inout A :: double[m, n])\n(inout b :: double[m])\n\n(out solution :: double[n])\n(out residual :: double)\n\n:: s8 := (\n\nqr_update (inout b) (inout A);\n\n-- A is now upper triangular; backsolve it into b\ncode := backsolve A[0:n, 0:n] (inout b[0:n]);\n\n-- Solution stored in first n elements\nsolution <- b[0:n];\n\n-- Norm of error = norm of last m-n elements\nresidual <- norm b[n:m];\n\nreturn code;\n);\n\n\nNote the way implicit arguments are resolved.\n\nThe generated C:\n\ns8 qr_solve (const s32 m, const s32 n, double * A, double * b, double * solution, double * const residual)\n{\nqr_update(m, n, b, A);\n\ns8 code;\ndouble arg [n * n];\ndouble arg2 [n];\n\nfor (s32 idx = 0; idx < n; idx++) {\nfor (s32 idx2 = 0; idx2 < n; idx2++) {\narg[n * idx + idx2] = A[n * idx + idx2];\n}\n}\nfor (s32 idx = 0; idx < n; idx++) {\narg2[idx] = b[idx];\n}\ncode = backsolve(n, arg, arg2);\nfor (s32 idx = 0; idx < n; idx++) {\nb[idx] = arg2[idx];\n}\nfor (s32 idx = 0; idx < n; idx++) {\nsolution[idx] = b[idx];\n}\n\ndouble arg3 [m - n];\n\nfor (s32 idx = 0; idx < m - n; idx++) {\narg3[idx] = b[n + idx];\n}\n*residual = norm(m - n, arg3);\nreturn code;\n}\n\n\nThe copying around inout b[0:n] is a bit inefficient in this case, but similar logic is needed for more complex matrix storage types.\n\n// qr.h\n#ifndef PLOVER_GENERATED_qr\n#define PLOVER_GENERATED_qr\n\n#include \"prelude.h\"\n\ns8 qr_solve (const s32 m, const s32 n, double * A, double * b, double * solution, double * const residual);\nvoid qr_update (const s32 m, const s32 n, double * b, double * A);\ns32 main (void);\n\n#endif /* PLOVER_GENERATED_qr */" ]
[ null ]
{"ft_lang_label":"__label__en","ft_lang_prob":0.76575994,"math_prob":0.99806523,"size":18844,"snap":"2019-51-2020-05","text_gpt3_token_len":5398,"char_repetition_ratio":0.13826963,"word_repetition_ratio":0.1662934,"special_character_ratio":0.32646996,"punctuation_ratio":0.17550626,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.99981374,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2020-01-22T16:49:26Z\",\"WARC-Record-ID\":\"<urn:uuid:764919b6-88df-4795-96a1-a1fe3cd32644>\",\"Content-Length\":\"59315\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:1318b1c7-035c-4895-8b95-070399131825>\",\"WARC-Concurrent-To\":\"<urn:uuid:cd5f0815-34b3-4e4a-b078-07a644e6a8be>\",\"WARC-IP-Address\":\"185.199.108.153\",\"WARC-Target-URI\":\"http://swift-nav.github.io/plover/tutorials.html\",\"WARC-Payload-Digest\":\"sha1:EYTMVZJOHFYAVM6PVLI24F4VQK44WYYP\",\"WARC-Block-Digest\":\"sha1:EQCWIVTQISWFZBBML3ZZICR3TVCMP5KJ\",\"WARC-Identified-Payload-Type\":\"application/xhtml+xml\",\"warc_filename\":\"/cc_download/warc_2020/CC-MAIN-2020-05/CC-MAIN-2020-05_segments_1579250607314.32_warc_CC-MAIN-20200122161553-20200122190553-00111.warc.gz\"}"}
https://cm-to-inches.appspot.com/3330-cm-to-inches.html
[ "Cm To Inches\n\n# 3330 cm to in3330 Centimeters to Inches\n\ncm\n=\nin\n\n## How to convert 3330 centimeters to inches?\n\n 3330 cm * 0.3937007874 in = 1311.02362205 in 1 cm\nA common question is How many centimeter in 3330 inch? And the answer is 8458.2 cm in 3330 in. Likewise the question how many inch in 3330 centimeter has the answer of 1311.02362205 in in 3330 cm.\n\n## How much are 3330 centimeters in inches?\n\n3330 centimeters equal 1311.02362205 inches (3330cm = 1311.02362205in). Converting 3330 cm to in is easy. Simply use our calculator above, or apply the formula to change the length 3330 cm to in.\n\n## Convert 3330 cm to common lengths\n\nUnitLengths\nNanometer33300000000.0 nm\nMicrometer33300000.0 µm\nMillimeter33300.0 mm\nCentimeter3330.0 cm\nInch1311.02362205 in\nFoot109.251968504 ft\nYard36.4173228346 yd\nMeter33.3 m\nKilometer0.0333 km\nMile0.0206916607 mi\nNautical mile0.0179805616 nmi\n\n## What is 3330 centimeters in in?\n\nTo convert 3330 cm to in multiply the length in centimeters by 0.3937007874. The 3330 cm in in formula is [in] = 3330 * 0.3937007874. Thus, for 3330 centimeters in inch we get 1311.02362205 in.\n\n## 3330 Centimeter Conversion Table", null, "## Alternative spelling\n\n3330 Centimeters to Inch, 3330 Centimeters in Inch, 3330 Centimeter to Inch, 3330 Centimeter in Inch, 3330 cm to Inch, 3330 cm in Inch, 3330 Centimeter to in, 3330 Centimeter in in, 3330 cm to in, 3330 cm in in, 3330 Centimeters to Inches, 3330 Centimeters in Inches, 3330 Centimeter to Inches, 3330 Centimeter in Inches" ]
[ null, "https://cm-to-inches.appspot.com/image/3330.png", null ]
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https://people.math.sc.edu/Burkardt/m_src/ball_grid/ball_grid.html
[ "# BALL_GRID Grid Points Within a 3D Ball\n\nBALL_GRID is a MATLAB library which generates a grid of points over the interior of an arbitrary ball in 3D.\n\nThe library allows the user to define an arbitrary ball by choosing its radius and center. The user also choose N, the number of subintervals into which a horizontal radius line will be subdivided. It then returns the gridpoints defined by that choice.\n\n### Languages:\n\nBALL_GRID is available in a C version and a C++ version and a FORTRAN90 version and a MATLAB version and a Python version.\n\n### Related Data and Programs:\n\nBALL_INTEGRALS, a MATLAB library which defines test functions for integration over the interior of the unit ball in 3D.\n\nBALL_MONTE_CARLO, a MATLAB library which applies a Monte Carlo method to estimate integrals of a function over the interior of the unit ball;\n\nCIRCLE_ARC_GRID, a MATLAB program which computes points equally spaced along a circular arc;\n\nCUBE_GRID, a MATLAB library which computes a grid of points over the interior of a cube in 3D.\n\nDISK_GRID, a MATLAB library which computes a grid of points over the interior of a disk in 2D.\n\nELLIPSE_GRID, a MATLAB library which computes a grid of points over the interior of an ellipse in 2D.\n\nELLIPSOID_GRID, a MATLAB library which computes a grid of points over the interior of an ellipsoid in 3D.\n\nHYPERCUBE_GRID, a MATLAB library which computes a grid of points over the interior of a hypercube in M dimensions.\n\nLINE_GRID, a MATLAB library which computes a grid of points over the interior of a line segment in 1D.\n\nPOLYGON_GRID, a MATLAB library which generates a grid of points over the interior of a polygon in 2D.\n\nPYRAMID_GRID, a MATLAB library which computes a grid of points over the interior of the unit pyramid in 3D;\n\nSIMPLEX_GRID, a MATLAB library which generates a regular grid of points over the interior of an arbitrary simplex in M dimensions.\n\nSPHERE_FIBONACCI_GRID, a MATLAB library which uses a Fibonacci spiral to create a grid of points on the surface of the unit sphere in 3D.\n\nSPHERE_GRID, a MATLAB library which provides a number of ways of generating grids of points, or of points and lines, or of points and lines and faces, on the surface of the unit sphere in 3D.\n\nSPHERE_LLQ_GRID, a MATLAB library which uses longitudes and latitudes to create grids of points, lines, and quadrilaterals on the surface of the unit sphere in 3D.\n\nSQUARE_GRID, a MATLAB library which computes a grid of points over the interior of a square in 2D.\n\nTETRAHEDRON_GRID, a MATLAB library which computes a grid of points over the interior of a tetrahedron in 3D.\n\nTRIANGLE_GRID, a MATLAB library which computes a grid of points over the interior of a triangle in 2D.\n\nWEDGE_GRID, a MATLAB library which computes a grid of points over the interior of the unit wedge in 3D.\n\n### Source Code:\n\nLast revised on 29 November 2018." ]
[ null ]
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https://www.jpost.com/israel/lapid-invites-peretz-to-opposition-meeting
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[ null ]
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https://softwareengineering.stackexchange.com/questions/375217/improving-my-inelegant-haskell-deduplication-function
[ "# Improving my inelegant Haskell deduplication function\n\nI'm working on learning Haskell, and one of the simple exercises I put myself through to this end is writing a function that deduplicates a list, removing all of the duplicate elements of a list such that every element in the output list is both unique and present in the original list.\n\nMy inelegant code for doing this is as follows:\n\n``````dedup [] = []\ndedup (n:ns) = theDedup n ns ns\nwhere theDedup n ns remains\n| ns == [] = n : []\n| remains == [] = n : theDedup (head ns) (tail ns) (tail ns)\n| n == head remains = theDedup (head ns) (tail ns) (tail ns)\n| otherwise = theDedup n ns \\$ tail remains\n``````\n\nFor every element of the original list `n:ns`, `theDedup` takes that element and recursively compares it to every other (`remains`), while keeping a copy of the items left to deduplicate as `ns`. When `remains` has run out, the current `n` has been compared to every other value and so must be unique, and when `ns` has run out, the entire list has been deduplicated, so `n` must be unique.\n\nThis is a rather confusing way of expressing a rather simple algorithm. How can it be done better?\n\n``````dedup :: [a] -> [a]" ]
[ null ]
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http://chinaaode.cn/qspevdu_t1005001
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https://askfilo.com/math-question-answers/z-2-alpha-z-beta-0-alpha-beta-are-complex-numbers-has-a-real
[ "", null, "World's only instant tutoring platform", null, "Question\nHard", null, "Solving time: 5 mins\n\n# are complex numbers) has a real root, then\n\nA\n\nB\n\nC\n\nD\nNone of these\n\n##", null, "Text solution\n\nLet be a real root of the given equation.\nThen, (1)\nTaking conjugate both sides\n(2)\nElimination from (1) and (2), we have\n71\nShare\nReport", null, "", null, "Stuck on the question or explanation?\n\nConnect with our Mathematics tutors online and get step by step solution of this question.\n\n231 students are taking LIVE classes", null, "One destination for complete JEE/NEET preparation\nLearn Practice Revision Succeed", null, "Instant 1:1 help, 24x7\n6000+ Expert tutors", null, "", null, "Textbook solutions\nHC verma, DP Pandey etc. solutions", null, "", null, "Complete study notes\nChapter wise short notes & formula sheet", null, "", null, "Question bank\nPractice every concept in the syllabus", null, "", null, "Test series & Mock tests\nEvaluate your exam preparation with 100+ tests", null, "Trusted by 1 crore+ students\n Question Text are complex numbers) has a real root, then Topic Complex Number and Quadratic Equations Subject Mathematics Class Class 11 Answer Type Text solution:1 Upvotes 71" ]
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https://www.clutchprep.com/calculus/derivatives-trigonometric-functions
[ "Ch.7: Derivatives (Part 2)WorksheetSee all chapters\n Ch.1: Pre-Calc (Part 1) 3hrs & 31mins 0% complete Worksheet Ch.2: Pre-Calc (Part 2) 2hrs & 53mins 0% complete Worksheet Ch.3: Pre-Calc (Part 3) 1hr & 40mins 0% complete Worksheet Ch.4: Limits (Part 1) 2hrs & 25mins 0% complete Worksheet Ch.5: Limits (Part 2) 1hr & 53mins 0% complete Worksheet Ch.6: Derivatives (Part 1) 3hrs & 13mins 0% complete Worksheet Ch.7: Derivatives (Part 2) 2hrs & 26mins 0% complete Worksheet Ch.8: Applications of Derivatives (Part 1) 3hrs & 1min 0% complete Worksheet Ch.9: Applications of Derivatives (Part 2) 2hrs & 1min 0% complete Worksheet Ch.10: Applications of Derivatives (Part 3) 3hrs 0% complete Worksheet Ch.11: Integrals 3hrs & 8mins 0% complete Worksheet\n\n# Derivatives Trigonometric Functions\n\nSee all sections\n\nConcept #1: Trig Derivatives (w/Chain Rule)\n\nConcept #2: Intro\n\nPractice: Derive the following function:", null, "Practice: Derive the following function:", null, "Practice: Derive the following function:", null, "Practice: Derive the following function:", null, "Practice: Derive the following function:", null, "Practice: Derive the following function:", null, "" ]
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https://www.brainkart.com/article/Exercise-5-1-(Congruent-and-Similar-Triangles)_44373/
[ "Home | | Maths 8th Std | Exercise 5.1 (Congruent and Similar Triangles)\n\n# Exercise 5.1 (Congruent and Similar Triangles)\n\n8th Maths : Chapter 5 : Geometry : Congruent Triangles and Similar Triangles : Exercise 5.1 : Text Book Back Numerical problems, Exercises Questions with Answers, Solution\n\nExercise 5.1\n\n1. Fill in the blanks with the correct term from the given list.\n\n(in proportion, similar, corresponding, congruent, shape, area, equal)\n\n(i) Corresponding sides of similar triangles are _______. [Answer: in proportion]\n\n(ii) Similar triangles have the same _________ but not necessarily the same size. [Answer: shape]\n\n(iii) In any triangle ______ sides are opposite to equal angles. [Answer: equal]\n\n(iv) The symbol ≡ is used to represent _______ triangles. [Answer: congruent]\n\n(v) The symbol ~ is used to represent ________ triangles. [Answer: similar]\n\n2. In the given figure, CIP ≡ COP and HIP ≡ HOP . Prove that IP ≡ OP.", null, "Solution:", null, "Statements : Reasons\n\n1. CI = CO  : CIP COP, by CPCTC\n\n2. IP = OP :  By CPCTC\n\n3. CP = CP : By CPCTC\n\n4. Also HI = HO : CPCTC ΔHIP HOP given\n\n5. IP = OP : By CPCTC and (4)\n\n6. IP OP : By (2) and (4)\n\n3. In the given figure, AC ≡ AD and CBD ≡ DEC . Prove that ∆ BCF ≡ ∆EDF .", null, "Solution:", null, "Statements : Reasons\n\n1. BFC = EFD : vertically opposite angles\n\n2. CBD = DEC : Angles on the same base given\n\n3. BCF = EDF : Remaining angles of ΔBCF and ΔEDF\n\n4. ΔBCF ΔEDF : By (1) and (2) AAA criteria\n\n4. In the given figure, ∆ BCD is isosceles with base BD and BAE DEA . Prove that AB ED .", null, "Solution:", null, "Statements : Reasons\n\n1. BAE DEA : Given\n\n2. AC = EC : By (1) sides opposite to equal angles are equal\n\n3. BC = DC : Given BCD is isosceles with base BD\n\n4. AC − BC = EC − DC : 2 − 3\n\n5. AB ED : By 4\n\n5. In the given figure, D is the midpoint of OE and CDE = 90°. Prove that ODC ≡ ∆EDC", null, "Solution:", null, "Statements : Reasons\n\n1. OD = ED : D is the midpoint of OE (given)\n\n2. DC = DC : Common side\n\n3. CDE = CDO = 90° : Linear pair and given CDE = 90°\n\n4. ΔODC ΔEDC : By RHS criteria\n\n6. Is PRQ QSP ? Why?", null, "Solution:\n\nIn ΔPRQ and ΔPSQ\n\nPRQ = PSQ = 90° given\n\nPR = QS = 3 cm given\n\nPQ = PQ = 5 cm common\n\nIt satisfies RHS criteria\n\nΔPRQ congruent to ΔQSP.\n\n7. From the given figure, prove that ∆ABC ~ ∆EDF", null, "Solution:\n\nFrom the ΔABC, AB = AC\n\nIt is an isosceles triangle\n\nAngles opposite to equal sides are equal\n\n∴ ∠B = C = 65°\n\n∴ ∠B + C = 65° + 65°\n\n= 130°\n\nWe know that sum of three angles is a triangle = 180°\n\nA + B + C = 180°\n\nA + 130° = 180°\n\nA = 180° − 130°\n\nA = 50°\n\nFrom ΔEDF, E = 50°\n\nSum of Remaining angles = 180° − 50° = 130°\n\nDE = FD\n\nD = F\n\nFrom ΔABC and ΔEDF\n\nD = 130/2 = 65°\n\nA = E = 50°\n\nB = D = 65°\n\nC = F = 65°\n\nBy AAA criteria ΔEDF ≈ ΔABC\n\n8.  In the given figure YH || TE . Prove that ∆WHY ~ ∆WET and also find HE and TE.", null, "Solution:\n\nStatements : Reasons\n\n1. ∠EWT = HWY : Common Angle\n\n2. ∠ETW = HYW : Since YH ‖‖ TE, corresponding angles\n\n3. WET = WHY : Since YH ‖‖ TE corresponding angles\n\n4. ΔWHY ΔWET : By AAA criteria\n\nAlso ΔWHY ~ ΔWET\n\nCorresponding sides are proportionated\n\nWH / WE = HY / TE = WY / WT\n\n6 / [ 6 + HE ] = 4/TE = 4/16\n\n6 / [6 + HE] = 4/16\n\n6 + HE = [6/4] × 16\n\n6 + HE = 24\n\nHE = 24 −  6\n\nHE = 18\n\nAgain 4/TE = 4/16\n\nET = 4/4\n\nTE = 16\n\n9. In the given figure, if ∆EAT ~ ∆BUN , find the measure of all angles.", null, "Solution:\n\nGiven ΔEAT ΔBUN\n\nCorresponding angles are equal\n\nE =  B  ...(1)\n\nA =  U\n\nT =  N\n\nE = x°\n\nA = 2x°\n\nSum of three angles of a triangle = 180°\n\nIn ΔEAT, x + 2xT = 180°\n\nT = 180° − (x° + 2x°)\n\nT = 180° − 3x° ……..(4)\n\nAlso in ΔBUN\n\n(x + 40)° + x° + U = 180°\n\nx + 40° + x + U = 180°\n\n2x° + 40° + U = 180°\n\nU = 180° − 2x − 40° = 140°− 2x°\n\nNow by (2)\n\nA = U\n\n2x = 140° − 2x°\n\n2x + 2x = 140°\n\n4x = 140°\n\nx = 140°/4 = 35°\n\nA = 2x° = 2 × 35° = 70°\n\nN = x + 40° = 35° + 40° = 75°\n\n∴  ∠T = N = 75°\n\nE = B = 35°\n\nA = U = 70°\n\n10. In the given figure, UB ||AT and CU CB Prove that ∆CUB ~ ∆CAT and hence ∆CAT is isosceles.", null, "Solution:\n\nStatements: Reasons\n\n1. CUB = CBU :   In ΔCUB, CU = CB\n\n2. CUB = CAB :   UB || AT, corresponding angle if CA is the transversal.\n\n3. CBU = CTA : CT is transversal UB || AT, corresponding angle common angle.\n\n4. UCB=  ACT : common angle\n\n5. ΔCUB ΔCAT : By AAA criteria\n\n6. CA = CT :   CAT = CTA\n\n7. Also ΔCAT is isosceles : By 1, 2 and 3 and sides opposite to equal angles are equal.\n\nObjective Type Questions\n\n11. Two similar triangles will always have ________angles\n\n(A) acute\n\n(B) obtuse\n\n(C) right\n\n(D) matching\n\n12. If in triangles PQR and XYZ, PQ/ XY = QR/YZ then they will be similar if\n\n(A) Q = Y\n\n(B) P = Y\n\n(C) Q = X\n\n(D) P = Z\n\n13. A flag pole 15 m high casts a shadow of 3 m at 10 a.m. The shadow cast by a building at the same time is 18.6 m. The height of the building is\n\n(A) 90 m\n\n(B) 91 m\n\n(C) 92 m\n\n(D) 93 m\n\n14. If ∆ABC ~ ∆PQR in which A = 53º and Q = 77º , then R is\n\n(A) 50°\n\n(B) 60°\n\n(C) 70°\n\n(D) 80°\n\n15. In the figure, which of the following statements is true?", null, "(A) AB = BD\n\n(B) BD < CD\n\n(C) AC = CD\n\n(D) BC = CD\n\nExercise 5.1\n\n1. (i) in proportion (ii) shape (iii) equal (iv) congruent (v) similar\n\n6. Yes, RHS Congruence\n\n8. HE =18,TE =16\n\n9. T = N = 75º,E = B = 35º,A = U = 70º\n\n11. (D) matching\n\n12.(A) Q =\n\n13. (D) 93 m\n\n14. (A) 50º\n\n15. (C) AC = CD\n\nTags : Questions with Answers, Solution | Geometry | Chapter 5 | 8th Maths , 8th Maths : Chapter 5 : Geometry\nStudy Material, Lecturing Notes, Assignment, Reference, Wiki description explanation, brief detail\n8th Maths : Chapter 5 : Geometry : Exercise 5.1 (Congruent and Similar Triangles) | Questions with Answers, Solution | Geometry | Chapter 5 | 8th Maths" ]
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https://gsebsolutions.com/gseb-solutions-class-9-maths-chapter-13-ex-13-5/
[ "# GSEB Solutions Class 9 Maths Chapter 13 Surface Areas and Volumes Ex 13.5\n\nGujarat Board GSEB Solutions Class 9 Maths Chapter 13 Surface Areas and Volumes Ex 13.5 Textbook Questions and Answers.\n\n## Gujarat Board Textbook Solutions Class 9 Maths Chapter 13 Surface Areas and Volumes Ex 13.5\n\nQuestion 1.\nA matchbox measures 4 cm x 2.5 cm x 1.5 cm. What will be the volume of a packet containing 12 such boxes?\nSolution:\nVolume of a matchbox = 4 x 2.5 x 1.5 cm3 = 15 cm3\n∴ Volume of a packet containing 12 such boxes = 15 x 12 cm3 = 180 cm3\n\nQuestion 2.\nA cuboidal water tank is 6 m long, 5 m wide and 4.5 m deep. How many litres of water can it hold? (1 m3 = 1000 L)\nSolution:\nCapacity of the tank = 6 x 5 x 4.5 m3 = 135 m3\n∴ The volume of water it can hold = 135 m3\n= 135 x 1000 L = 135000 L", null, "Question 3.\nA cuboidal vessel is 10 m long and 8 m wide. How high must it be made to hold 380 cubic metres of a liquid?\nSolution:\nLet the height of the cuboidal vessel be h m.\nl = 10 m\nb = 8 m\nCapacity of the cuboidal vessel = 380 m3\nlbh = 380\n⇒ (10) (8) = 380 ⇒ h = $$\\frac {380}{(10) (8)}$$4.75 m\n⇒ h = $$\\frac {19}{4}$$ ⇒ h = 4.75 m\nHence, the cuboidal vessel must be made 4.75 m high.\n\nQuestion 4.\nFind the cost of digging a cuboidal pit 8 m long, 6 m broad and 3 m deep at the rate of ? 30 per m3?\nSolution:\nl = 8 m, b = 6 m and h = 3 m\n∴ Volume of the cuboidal pit = Ibh = 8 x 6 x 3 m3 = 144 m3\n∴ Cost of digging the cuboidal pit @ ₹ 30 per m3 = ₹ (144 x 30) = ₹ 4320", null, "Question 5.\nThe capacity of a cuboidal tank is 50000 litres of water. Find the breadth of the tank, if its length and depth are respectively 2.5 m and 10 m.\nSolution:\nLet the breadth of the cuboidal tank be b m.\nl = 2.5 m\nh = 10 m\nCapacity of the cuboidal tank = 50000 litres\n= $$\\frac {50000}{1000}$$ m3 = 50 m3\nlbh = 50\n⇒ 2.5 x b x 10 = 50\n⇒ 25b = 50\n⇒ b = $$\\frac {50}{25}$$ = 2m\nHence, the breadth of the cuboidal tank is 2 m.", null, "Question 6.\nA village, having a population of 4000, requires 150 litres of water per head per day. It has a tank measuring 20 m x 15 m x 6 m. For how many days will the water of this tank last?\nSolution:\nRequirement of water per head per day = 150 lires\n∴ Requirement of water for the total population of the village per day\n= 150 x 4000 litres = 600000 litres\n= $$\\frac {600000}{1000}$$ m3 = 600 m3\n\nFor tank:\nl = 20 m, b = 15 m and h = 6 m\n∴ Capacity of the tank\n= 20 x 15 x 6 m3 = 1800 m3\n∴ Number of days for which the water of this tank last", null, "= $$\\frac {1800}{600}$$ = 3\nHence, the water of this tank will last for 3 days.", null, "Question 7.\nA godown measures 40 m x 25 m x 15 m. Find the maximum number of wooden crates each measuring 1.5 m x 1.25 m x 0.5 m that can be stored in the godown.\nSolution:\nFor godown:\nl = 40 m\nb = 25 m\nh = 15 m\n∴ Capacity of the godown = lbh\n= 40 x 25 x 15 m3 = 15000 m3\nFor a wooden crate:\nl = 1.5 m\nb = 1.25 m\nh = 0.5m\n∴ Capacity of a wooden crate = lbh\n= 1.5 x 1.25 x 0.5 m3 = 0.9375 m3\n\nWe have,\n$$\\frac {15000}{0.9375}$$ = 16000\nHence, the maximum number of wooden crates that can be stored in the godown is 16000.", null, "Question 8.\nA solid cube of side 12 cm is cut into eight cubes of equal volume. What will be the side of the new cube? Also, find the ratio between their surface areas.\nSolution:\nSide of the solid cube (a) = 12 cm\n∴ Volume of the solid cube = a3\n= (12)3 = 12 x 12 x 12 cm3 = 1728 cm3\n∴ It is cut into eight cubes of equal volume.\n∴ Volume of a new cube\n= $$\\frac {1728}{8}$$ cm3\n= 216 cm3\nLet the side of the new cube be x cm.\nThen, volume of the new cube = x3 cm3\nAccording to the question,\nx3 = 216\n⇒ x = (216)1/3\n⇒ x = (6 x 6 x 0)1/3\n⇒ x = 6 cm\nHence, the side of the new cube will be 6 cm.\nSurface area of the original cube\n= 6a2 = 6(12)2 cm2\nSurface area of the new cube = 6x2 = 6(6)2 cm2\n∴ Ratio between their surface areas", null, "= $$\\frac{6(12)^{2}}{6(6)^{2}}$$ = $$\\frac {4}{1}$$ = 4 : 1\nHence, the ratio between their surface areas is 4 : 1.", null, "Question 9.\nA river 3 m deep and 40 m wide is flowing at the rate of 2 km per hour. How much water will fall into the sea in a minute?\nSolution:\nIn one hour\nl = 2 km = 2 x 1000 m = 2000 m\nb = 40 m\nh = 3 m\n∴ Water fall into the sea in one hour = Ibh\n= 2000 x 40 x 3 m3\n∴ Water fall into the sea in a minute\n$$\\frac{2000 \\times 40 \\times 3}{60}$$m3 = 400 m3\nHence, 4000 m3 of water will fall into the sea in tha minute." ]
[ null, "https://i0.wp.com/gsebsolutions.com/wp-content/uploads/2020/07/GSEB-Solutions.png", null, "https://i0.wp.com/gsebsolutions.com/wp-content/uploads/2020/07/GSEB-Solutions.png", null, "https://i0.wp.com/gsebsolutions.com/wp-content/uploads/2020/07/GSEB-Solutions.png", null, "https://i0.wp.com/gsebsolutions.com/wp-content/uploads/2020/09/GSEB-Solutions-Class-9-Maths-Chapter-13-Surface-Areas-and-Volumes-Ex-13.5-1.png", null, "https://i0.wp.com/gsebsolutions.com/wp-content/uploads/2020/07/GSEB-Solutions.png", null, "https://i0.wp.com/gsebsolutions.com/wp-content/uploads/2020/07/GSEB-Solutions.png", null, "https://i2.wp.com/gsebsolutions.com/wp-content/uploads/2020/09/GSEB-Solutions-Class-9-Maths-Chapter-13-Surface-Areas-and-Volumes-Ex-13.5-2.png", null, "https://i0.wp.com/gsebsolutions.com/wp-content/uploads/2020/07/GSEB-Solutions.png", null ]
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http://ramanclasses.in/refresher.html
[ "", null, "", null, "## Instructors", null, "Register for the course now\n\n## Demo Lectures\n\n Newton's Laws of Motion | Physics Generating Waves | Physics\n The Need for Calculus | Maths Examining Figures\n An Insight into Limits | Maths What is Slope? | Maths\n Building Accuracy Errors in Measurements | Physics\n Coulomb's Law | Physics Intro to Kinematics | Physics\n What are Inequalities? | Maths Exponents and Logarithms | Maths\n Understanding Logarithms | Maths Heat & Thermodynamics | Physics\n Introduction to Trignometry | Maths- Understanding Trignometric Ratios | Maths\n Vectors  | Maths Keys to Excel" ]
[ null, "http://ramanclasses.in/images/header11.png", null, "http://ramanclasses.in/images/header2.png", null, "http://ramanclasses.in/images/RefresherFaculty-min.png", null ]
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https://cs.stackexchange.com/questions/110623/pseudo-polynomial-reduction-from-3-partition-to-partition
[ "# pseudo-polynomial reduction from 3-Partition to Partition\n\nA problem $$\\Pi'$$ is pseudo-polynomially reducible to the problem $$\\Pi$$ ($$\\Pi' \\leq_{pp} \\Pi$$) if, for any instance $$I'$$ of $$\\Pi'$$, an instance $$I$$ of $$Π$$ can be constructed in pseudo-polynomially bounded time, such that, given the solution $$S_I$$ to $$I$$, the solution $$S_I'$$ to $$I'$$ can be found in pseudo-polynomial time.\n\nIt follows that, $$\\forall \\Pi,\\Pi' \\in NP$$, if $$\\Pi'$$ is strongly NP-complete, and $$\\Pi' \\leq_{pp} \\Pi$$, then $$\\Pi$$ is strongly NP-complete.\n\nAnd it is easy to show that \"3-Partition $$\\leq_{pp}$$ Partition.\"\n\nHence, I can conclude that Partition is strongly NP-complete. (However, we already know that Partition problem is ordinary NP-complete.)\n\nAm I missing something!?\n\n• @TomvanderZanden: This comment is from another user here cs.stackexchange.com/questions/39753/…: Every known reduction from 3-Partition to 2-Partition creates numbers that are exponentially bigger than the original numbers. – Moh_NA_X Jun 13 at 15:20\n• Why do you think it is easy to reduce 3-partition to partition in pptime – narek Bojikian Nov 11 at 10:21\n\nThe claim\n\nIt follows that, $$\\forall \\Pi,\\Pi' \\in NP$$, if $$\\Pi'$$ is strongly NP-complete, and $$\\Pi' \\leq_{pp} \\Pi$$, then $$\\Pi$$ is strongly NP-complete.\n\nis wrong (at least for how \"pseudo-polynomically reducible\" is defined here).\n\nIf $$\\Pi'$$ is strongly $$NP$$-complete, then pseudo-polynomially reducible'' is equivalent to polynomially reducible.\n\nRecall that a problem is strongly $$NP$$-complete if it is $$NP$$-complete even if we assume all the integers that appear in the input are polynomial in the length of the input.\n\nRecall that an algorithm runs in pseudopolynomial time if it runs in polynomial time in the integers that appear in the input.\n\nSo, a pseudopolynomial reduction must run in time polynomial in the integers that appear in the input. Which, for a strongly $$NP$$-complete problem, can be assumed to be polynomial in the length of the input. Which means the reduction must run in time polynomial in the length of input.\n\nSo, if $$\\Pi'$$ is strongly $$NP$$-complete, $$\\Pi' \\leq_{pp} \\Pi$$ is equivalent to $$\\Pi' \\leq_p \\Pi$$. Clearly, the existence of such a reduction does not imply that $$\\Pi$$ is strongly $$NP$$-hard.\n\nThe only place in the literature that I can find any mention of this notion of pseudopolynomial reduction'' is in the appendix an OR & Management Science book. I cannot find any other literature mentioning this notion; one would expect to be able to find some mention of it in complexity theory circles.\n\nWe should use a different definition for $$\\leq_{pp}$$. A pseudopolynomial reduction should be defined as a reduction, running in pseudpolynomial time, that in addition does not increase integer values in the input more than polynomially. Then the claim would hold true.\n\n• The claim \"$\\forall \\Pi,\\Pi' \\in NP$, if $\\Pi'$ is strongly NP-complete, and $\\Pi' \\leq_{pp} \\Pi$, then $\\Pi$ is strongly NP-complete.\" is from books.google.com/… . – Moh_NA_X Jun 13 at 15:54\n• That book is wrong. – Tom van der Zanden Jun 13 at 17:01\n• Thanks for your answer. Actually, I want to show that the reduction \"3-Partition $\\leq_p$ Partition\" can't give an instance of the polynomially-bounded size of the input. – Moh_NA_X Jun 13 at 17:51\n• I'm not sure what you mean by \"an instance of the polynomially-bounded size of the input\". But I think you cannot prove what you want to prove without assuming $P\\not = NP$. – Tom van der Zanden Jun 13 at 18:18\n• @TomvanderZanden He basically means, that he determines the time complexity relating to the input length not magintude. For example the subset-sum problem has as input $n$ integers and integer $k$ (the target sum). If I would write $T(k,n)=k*n \\in O(k*n)$ this would be wrong, because $k$ depends on the actual number and not at the number of bits that are needed to encode $k$. Assume we add x bit to $k$, we would double $k$ $x$ times (cyclic left bitshift). Thus $T(n;k+x)= 2^x*k*n$ Here we would write $T(n) \\in O^{~}(k*n)$ to denote that we hide a logarithmic factor in $k$. – Panzerkroete Jun 14 at 2:02" ]
[ null ]
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https://smithfieldjustice.com/30-logical-fallacies-worksheet-with-answers/
[ "HomeTemplate ➟ 30 30 Logical Fallacies Worksheet with Answers\n\n# 30 Logical Fallacies Worksheet with Answers", null, "Quiz & Worksheet Identifying Logical Fallacies logical fallacy identification worksheet answer key, logical fallacies worksheet cumulative answer key, name that logical fallacy worksheet answers, logical fallacies guided notes worksheet answers, identifying logical fallacies worksheet answers, image source: study.com\n\n## 30 Composition Of Matter Worksheet\n\nCLASSIFICATION OF MATTER ppt video online the position of living matter worksheet answers, position of matter worksheet, position of matter worksheet answers, classification of matter section 1 position of matter worksheet answer key, chapter 9 reinforcement position of matter worksheet answers, image source: slideplayer.com\n\n## 30 Absolute Value Worksheet Pdf\n\nSolving Absolute Value Equations Worksheet graphing absolute value equations worksheet pdf, solving absolute value equations and inequalities worksheet pdf, graphing absolute value equations worksheet pdf answers, absolute value function worksheet pdf, absolute value piecewise functions worksheet pdf, image source: pinterest.com" ]
[ null, "https://smithfieldjustice.com/wp-content/uploads/2020/02/logical-fallacies-worksheet-with-answers.jpg", null ]
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https://www.britannica.com/science/system-of-equations
[ "# System of equations\n\nmathematics\nAlternative Title: simultaneous equations\n\nSystem of equations, orsimultaneous equations, In algebra, two or more equations to be solved together (i.e., the solution must satisfy all the equations in the system). For a system to have a unique solution, the number of equations must equal the number of unknowns. Even then a solution is not guaranteed. If a solution exists, the system is consistent; if not, it is inconsistent. A system of linear equations can be represented by a matrix whose elements are the coefficients of the equations. Though simple systems of two equations in two unknowns can be solved by substitution, larger systems are best handled with matrix techniques.", null, "East Asian mathematics: Solution of systems of simultaneous linear equations\nThe Nine Chapters devotes a chapter to the solution of simultaneous linear equations—that is, to collections of relations between…\nThis article was most recently revised and updated by William L. Hosch, Associate Editor.\nSystem of equations", null, "" ]
[ null, "https://cdn.britannica.com/s:225x225/59/91959-004-6B5B84CF/boards-markers-example-rods-systems-equations-China.jpg", null, "https://cdn.britannica.com/marketing/thistle-white.svg", null ]
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https://spinningnumbers.org/a/rc-step-response1.html
[ "When something changes in a circuit, the voltages and currents adjust to the new conditions. If the change is an abrupt step the response is called the step response.", null, "The $\\text{RC}$ step response is the most important analog circuit. In analog systems it is the building block for filters and signal processing. It sets the speed limit for how fast digital system run—happening billions of times a second inside computers and other digital devices.\n\nBefore diving into the step response derivation you may want to review two articles, RC natural response - intuition, and RC natural response - derivation. To gain an intuitive understanding for this circuit see RC step response - intuition. There is a fair amount of new vocabulary introduced in this derivation. Relax and let it soak in slowly.\n\nWritten by Willy McAllister.\n\n### Contents\n\nThe step response of an $\\text R\\text C$ circuit is,\n\n$v(t) = \\text V_\\text S + (\\text V_0 - \\text V_\\text S)\\,e^{-t/\\text{RC}}$\n\nwhere $v(t)$ is the voltage on the capacitor, $\\text V_0$ is the beginning voltage of the step, and $\\text V_\\text S$ is the ending voltage of the step.\n\nApply an abrupt step to a resistor-capacitor $(\\text{RC})$ circuit and watch the voltage across the capacitor. A step input is a common way to give a circuit a little “kick” to see what it does. The step response tells us quite a lot about the properties of the $\\text{RC}$ circuit.\n\nThis is the circuit we will study,", null, "The input is an abrupt voltage step that starts at $\\text V_0$ and instantly jumps to $\\text V_{\\text S}$ at $t = 0$.\nWe want to find the voltage on the capacitor, $\\goldC{v(t)}$, as a function of time.\n\ninstantaneous step\n\nA step function is a mathematical idea. The voltage has only two values, $\\text V_0$ and $\\text V_{\\text S}$. There are no in-between values. When we draw a step with an orange vertical line at $t = 0$ it’s simply a graphical connection between the top and bottom horizontal lines. The vertical line isn’t meant to suggest intermediate voltage values exist at $t = 0$.\n\nTechnically, the step function does not meet the definition of a mathematical function, since there’s this discontinuous weirdness at $t=0$. You will see how we deal with that when we determine the initial conditions.\n\nIn the real world step functions always have some finite slope. We still call it a step if the slope is really steep relative to the response of the $\\text{RC}$ circuit. It’s close enough to an ideal step if it looks like a step on the time scale we are interested in.\n\nIt is awkward to express a mathematical model of a step source. There is an equivalent way to draw this circuit. We change the source to a constant voltage $\\text V_{\\text S}$ and add a switch to cause the step. The initial voltage, $\\text V_0$, is placed directly on the capacitor,", null, "The starting voltage on the capacitor is the initial condition, also called the boundary condition. The moment of flipping the switch establishes a boundary.\n\nHow did $\\text V_0$ get there?\n\nIf you just have to know how the initial charge got onto $\\text C$, here’s a circuit that does that,", null, "Both switches are thrown at the exact same moment. The switch on the right opens, and the one on the left closes at $t = 0$. Prior to $t = 0$ the voltage source on the right charges the capacitor up to $\\text V_0$.\n\n## Model the circuit\n\nWe start by modeling the circuit with Kirchhoff’s Current Law for the two currents flowing out of the top right node, then replace each current with the proper $i$-$v$ expression,\n\n$\\begin{array}{cccc} i_\\text R & + & i_\\text C &= 0 \\\\ \\\\ \\dfrac{v - \\text V_\\text S}{\\text R} & + & \\text C\\,\\dfrac{dv}{dt}&= 0 \\end{array}$\n\nRearrange the terms a little to format it like a differential equation. Collect the $v$ terms on the left side and put the non-$v$ terms on the right side. We like to have a coefficient of $1$ on the $dv/dt$ term,\n\n$\\dfrac{v}{\\text R} - \\dfrac{\\text V_\\text S}{\\text R} + \\text C\\,\\dfrac{dv}{dt} = 0$\n\n$\\text C\\,\\dfrac{dv}{dt} + \\dfrac{v}{\\text R} = \\dfrac{\\text V_\\text S}{\\text R}$\n\n$\\dfrac{dv}{dt} + \\dfrac{v}{\\text{RC}} = \\dfrac{\\text V_\\text S}{\\text{RC}}\\qquad$ with initial condition: $v(0) = \\text V_0$\n\nThis is the differential equation we have to solve.\n\n## It is hard to solve\n\nThere’s an important difference between this equation and the one we derived for the $\\text{RC}$ natural response shown here,\n\n$\\dfrac{dv}{dt} + \\dfrac{v}{\\text{RC}} = 0\\qquad$ with initial condition: $v(0) = \\text V_0$\n\nThere was no voltage source for the natural response circuit, and the right side of the differential equation is $0$. The natural response equation is homogeneous. That means all terms involve the independent variable $v$ or derivatives of $v$.\n\nFor the step response we got a non-zero number on the right side,\n\n$\\dfrac{dv}{dt} + \\dfrac{v}{\\text{RC}} = \\dfrac{\\text V_\\text S}{\\text{RC}}\\qquad$ with initial condition: $v(0) = \\text V_0$\n\nThe term on the right, $\\dfrac{\\text V_\\text S}{\\text{RC}}$, is not related to $v$ or a derivative of $v$. Because of this, this equation is non-homogeneous.\n\nSolving a non-homogeneous differential equation is not the simplest thing in the world. In fact it is usually a pain in the neck. Fortunately, this non-homogeneous equation is solvable without too much torture. Lucky us.\n\nThe electrical reason the step response is challenging is because of the two energy sources. Energy comes from 1. the input voltage source and 2. the initial charge on the capacitor. The trouble is the two energy sources have no relationship to each other. This complicates the problem and makes it difficult to solve all at once.\n\nAs usual, when a problem involves two energy sources engineers wonder if superposition can somehow be applied. This is NOT a classical EE superposition (different energy sources), it is a differential equation theory. We are taking a “math route” to the answer\n\n## Solve a driven circuit\n\nWe find the step function using the method of homogeneous and particular solutions, based on a non-obvious theory of differential equations, stated here without proof,\n\nThe total solution to a non-homogeneous differential equation can be found by the sum of the general solution of the circuit’s natural response with any particular response (found without regard for the initial conditions), followed by applying the initial conditions to resolve unknown constants.\n\nThis is a pretty bold theory to state without proof. It is central to finding the step response. For the moment please take it on faith. Here is my attempt to explain. If you have taken a differential equation class, what we are doing is called the method of undetermined coefficients.\n\nIn mathematical vocabulary the the theory says,\n\nComplete solution = homogeneous solution + particular solution\n\n$v_c = v_h + v_p\\qquad$ subject to initial conditions\n\nThe subscripts $c$, $h$, and $p$ stand for complete solution, homogeneous solution, and a particular solution.\n\nIn circuit vocabulary the notation becomes,\n\nComplete response = Natural response (zero input) + forced response (zero state)\n\n$v_{tot} = v_n + v_f\\qquad$ subject to initial conditions\n\nwhere $tot$, $n$, and $f$ stand for total response, natural response, and the forced response.\n\nNOTE: These are not exactly the same thing according to Felipe Ribas.\n\nThe theory allows us to pick any particular response—we could choose any of the myriad solutions described by the general solution. However… Ingenious part: We hunt for exactly one particular response, one that is relatively easy to find and has a nice real-world significance. Somewhere in the family of curves represented by the general solution you always find the one particular response that corresponds to the long-term steady-state behavior of the circuit—the place the circuit ends up after the natural response dies out. You might say the forced response is one particular particular response.\n\nexample\n\nWhat is meant by,\n“Somewhere in the family of curves represented by the general solution you can always find the one particular response that corresponds to the the long-term behavior of the circuit.”?\n\nHere’s an example of what I’m talking about. This is the general solution to the $\\text{RC}$ natural response,\n\n$v = K\\,e^{-t/\\text{RC}}$\n\nLet’s look at what the general solution represents. The general solution is an infinite family of functions that all make the differential equation true. We plot this equation with different values of $K$. Here are a few of them,\n\nThe family of particular solutions represented by the general solution.\n\nThe natural response has no forcing function. The only energy in the system is the initial charge on the capacitor. After a long time that initial energy dissipates and the voltage approaches $0$. So the long-term steady-state response for any value of $K$ is $v = 0$.\n\nFind the particular response that’s a straight line along the time axis, the line $v = 0$ (bold orange). This particular response is interesting—out of all possible particular responses this one matches the steady-state response at all times, not just after a long time. (It is the particular solution we would choose if the initial voltage $\\text V_0$ happened to be $0$.)\n\nThe point of this example is to show how the long-term steady-state response appears somewhere in the general solution. We will use this little nugget in a little while.\n\nWhen we drive the RC circuit with a step function the steady-state response is no longer zero—it will be some other value.\n\n## Strategy\n\nThe steps to solve a driven circuit,\n\n1. Find the general form of the natural response. Do this by suppressing the driven input (set the input to $0$). Ignore the initial conditions for now.\n2. Find the forced response. The forced response is the one particular solution that looks like a scaled version of the input forcing function. Keep ignoring the initial conditions. (Sometimes the proposed solution might need to include the input function plus its derivatives.)\n3. Superimpose (add) the natural response to the forced response to get the total response.\n4. Last, apply the initial conditions to the total response and resolve the unknown constants.\n\nHolding off the initial conditions until this last step allows the natural and forced response to blend together to create the transition from initial state to steady state.\n\nso many terms\n\nThere are so many terms used in math and engineering related to this type of differential equation. Don’t try to memorize all this.\n\n• Natural response is the homogeneous solution or the force-free solution or the complementary solution (because it complements the particular solution). In control systems you might see it called the free response.\n\n• Forced response is a particular solution chosen from the general solution. Not just any particular solution but the one specifically derived from the the long term behavior of the circuit, the steady-state response.\n\n• Total response is also called the complete solution.\n\nEven more,\n\nOur differential equation is a mouthful, it is a\nnon-homogeneous first-order constant-coefficient ordinary differential equation.\n\nWhat does all this mean?\n\n• Homogeneous means the equation contains $v$ and derivatives of $v$, and nothing else. The natural response equation is homogeneous.\n• Non-homogeneous or inhomogeneous means there is some term that’s not $v$ or one of its derivatives. Our step response differential equation includes a $\\text V_{\\text S}$ term not related to $v$, so it is non-homogeneous.\n• First-order means the highest derivative is the first derivative $dv/dt$. If there was a second derivative, $dv^2/d^2v$, it would be a second-order equation. $\\text{LC}$ and $\\text{RLC}$ circuits produces second-order equations.\n• Constant coefficient means the values of the components $\\text R$ and $\\text C$ are constant and do not change as time goes by. This is also referred to as time invariant. You may see a system described by the acronym LTI for linear time invariant. LTI means if you run the circuit today and tomorrow with the same initial conditions it will do the same thing both days. It’s a nice property.\n• Ordinary means there is just one independent variable, $t$.\n\nLet’s work our strategy and see what happens.\n\n## Natural response\n\nTo find $v_n$, the natural response, we suppress (turn off, set to zero) the input,", null, "Find the natural response with the input suppressed. To suppress a voltage source, replace it with a short. (For more on suppressing sources see Superposition.)\n\nWe already worked through the $\\text{RC}$ natural response in great detail. We quickly repeat the derivation here.\n\nWrite a KCL equation for the upper right node. Then model the two passive components by their $i$-$v$ equations,\n\n$\\begin{array}{cccc} i_\\text C & + & i_\\text R &= 0 \\\\ \\\\ \\text C\\,\\dfrac{dv}{dt} & + & \\dfrac{v_n}{\\text R}&= 0 \\end{array}$\n\nto get this differential equation,\n\n$\\dfrac{dv_n}{dt} + \\dfrac{v_n}{\\text{RC}} = 0$\n\nNotice: When we suppress the input, the right side of the differential equation comes out $0$, so it is a homogeneous differential equation.\n\nPropose a solution in the form of an exponential with two adjustable parameters, $K_n$ and $s$,\n\n$v_n = K_n\\,e^{st}$\n\nTest the proposed solution to see if it makes the differential equation true. Plug $v_n$ into the homogeneous equation,\n\n$\\dfrac{d}{dt}K_n\\,e^{st} + \\dfrac{1}{\\text{RC}}K_n\\,e^{st} = 0$\n\nPerform the derivative in the first term,\n\n$sK_n\\,e^{st} + \\dfrac{1}{\\text{RC}}K_n\\,e^{st} = 0$\n\nThe common $K_n\\,e^{st}$ term can be factored out,\n\n$K_n\\,e^{st}\\,\\left (s + \\dfrac{1}{\\text{RC}} \\right ) = 0$\n\nTo make this equation true, one of the three terms in the product on the left side has to be $0$. We could set $K_n$ to $0$, which means there was no initial energy stored in the capacitor. Or, the term $e^{st}$ becomes zero if $s$ is negative and we wait for $t$ to go to infinity. (All natural responses approach $0$ if you wait long enough.) Something interesting happens if we make the third term $0$,\n\n$s + \\dfrac{1}{\\text{RC}} = 0$\n\nThis is the characteristic equation of the $\\text{RC}$ natural response. Solve the characteristic equation for $s$ (find the roots of the characteristic equation).\n\n$s=-\\dfrac{1}{\\text{RC}}$\n\nPut this value of $s$ back into the proposed solution. This gives us the general form of the natural response for $t > 0$,\n\n$v_n = K_n\\,e^{-t/\\text{RC}}$\n\nGeneral solution to the $\\text{RC}$ natural response. $v_n = K_n\\, e^{-t/\\text{RC}}$\n\nThis general solution is an infinite family of curves based on all possible values of $K_n$. The natural response is an exponential curve whose rate of descent is determined by the product $\\text{RC}$. If you set $t = 0$ the equation tells you $K_n$ corresponds to the voltage at $t = 0$. We hold off figuring out a specific value of $K_n$ until after we assemble the total response.\n\n## Forced response\n\nThe superposition theory says we win with any particular solution to the differential equation. However, we won’t go for any particular solution, but rather for a special one, the particular solution that corresponds to the long-term steady-state of the circuit. It gets a special name, the forced response.\n\n$\\dfrac{dv}{dt} + \\dfrac{v}{\\text{RC}} = \\dfrac{\\text V_\\text S}{\\text{RC}}$\n\nWhat? This again? You said this was really hard!\n\nWhen I first studied non-homogeneous equations I got depressed when the original equation showed up again. What’s with all this special superposition theory and natural response if we still have to solve the original hard equation? The key that unlocks the treasure: This time we get to ignore the initial condition while finding the forced response. That cracks the door open and keeps us from going crazy.\n\nThink back to when we derived the natural response. The solution had to make the differential equation happy and had to satisfy the initial conditions. That’s not the case for the forced response—we apply for the initial condition after we do the superposition.\n\nLook at the equation and make an intelligent guess at a voltage function that might solve it.\n\nWhatever $v$ is, if we hope to make both sides equal it has to bear some resemblance to the function on the right side—so let’s propose a solution that looks like the right side. Since the right side is a constant we propose a yet-to-be-determined1 arbitrary constant,\n\n$v_f = K_f$\n\nPop this into the non-homogeneous equation and see if this $v_f$ makes the equation true,\n\n$\\dfrac{d}{dt} K_f + \\dfrac{K_f}{\\text{RC}} \\stackrel{?}{=} \\dfrac{\\text V_\\text S}{\\text{RC}}$\n\nIn the first term, the derivative of a constant is always $0$,\n\n$0 + \\dfrac{K_f}{\\text{RC}} \\stackrel{?}{=} \\dfrac{\\text V_\\text S}{\\text{RC}}$\n\nThe equation comes true when what? When,\n\n$K_f = \\text V_\\text S$\n\nThis resolves the arbitrary constant $K_f$, which means we did what the superposition theory said, we found a particular solution for $v_f$,\n\n$v_f = \\text V_\\text S$\n\nA particular solution for the $\\text{RC}$ step is $v_f(t) = \\text V_\\text S$, also known as the forced response.\n\nWe call this particular response the forced response because our proposed solution was derived from the forced input.\n\n#### Things to notice about the forced response\n\nNotice: The particular solution turned out to be similar to the forcing input. That is why engineers give this particular solution a special name—the forced response.\n\nNotice: The forced response is exactly the input step. That doesn’t always happen for every forced input, but it did this time.\n\nNotice: The force response solves the equation but completely misses the initial condition, $v(0) = \\text V_0$. That’s okay. The natural response will take care of that when we do the superposition.\n\nNotice: While the forced response is plotted for all time after $t=0$ you can’t observe it with an oscilloscope. The same holds for the natural response component. When we do the upcoming superposition to find the total response we can observe that with an oscilloscope.\n\nWhat happens if the guess is wrong?\n\nWhat if you guess a forced response and it doesn’t work? Let’s see what that looks like. Here’s an example of a guess that doesn’t work.\n\nSuppose you guess the solution is a constant $\\times$ time, $v_f = K_f\\,t$.\nWhen you plug $v_f$ into the differential equation,\n\n$\\dfrac{d}{dt}K_f\\,t + \\dfrac{K_f\\,t}{\\text{RC}} = \\dfrac{\\text V_\\text S}{\\text{RC}}$\n\nYou get,\n\n$K_f + \\dfrac{K_f\\,t}{\\text{RC}} = \\dfrac{\\text V_\\text S}{\\text{RC}}$\n\nWhen you solve this for $K_f$ no amount of algebra will get rid of the $t$ term. This means $K_f$ depends on time, so it’s not constant. That’s a fail for this proposed solution.\n\nThe total response is the superimposition (sum) of the natural and forced responses,\n\n$\\begin{array}{cccc} v_{tot} = & v_n &+& v_f \\\\ \\\\ v_{tot} = & K_n\\,e^{-t/\\text{RC}} &+& \\text V_\\text S \\end{array}$\n\nThis equation represents the general solution to the step response because it has one remaining undetermined constant. The general solution is the infinite family of all possible particular solutions,\n\nGeneral solution to the $\\text{RC}$ step response. $v_{tot} = K_n\\, e^{-t/\\text{RC}} + \\text V_\\text S$\n\nLook at the plot and find the particular solution that is a horizontal straight line at $v = \\text V_\\text S$ (hint: the fifth one from the top). That’s the particular solution we found above—we named it the forced response.\n\n## Apply the initial conditions\n\nNow, finally, we apply the initial conditions to figure out the remaining unknown $K_n$.\n\nWe know the voltage at a particular point in time: At $t = 0$ the voltage is $\\text V_0$, the initial voltage on the capacitor. We find a $K_n$ such that the total response—not just the natural response—matches this boundary condition.\n\nIn the total response expression set $t$ to $0$ and replace $v_{tot}$ with $\\text V_0$,\n\n$\\text V_0 = K_n\\,e^{-0/\\text{RC}} + \\text V_\\text S$\n\nThe exponential expression becomes $1$ and we are left with,\n\n$\\text V_0 = K_n + \\text V_\\text S$\n\nSolving for $K_n$,\n\n$K_n = \\text V_0 - \\text V_\\text S$\n\n## Step response\n\nReplace $K_n$ in the total response and we have the step response we’ve been looking for,\n\n$\\boxed{v_{tot} = (\\text V_0 - \\text V_\\text S)\\,e^{-t/\\text{RC}} + \\text V_\\text S}$\n\nThe total response looks like this,\n\nThe $\\text{RC}$ step total response. $v_{tot} = (\\text V_0 - \\text V_\\text S)\\,e^{-t/\\text{RC}} + \\text V_\\text S$\n\nWe’ve done it! This is the response of an $\\text{RC}$ network to a step voltage.\n\nWhat did $K_n$ turn out to be? $K_n$ is the difference between the starting and ending voltages, $\\text V_0 - \\text V_\\text S$, which is just the right value to flip the natural response term over if needed and make it fit perfectly between start and end.\n\n## No charge on the capacitor\n\nIf the capacitor starts with no initial charge then $\\text V_0 = 0$, and the total response expression gets a little simpler,\n\n$v_{tot} = (0 - \\text V_\\text S)\\,e^{-t/\\text{RC}} + \\text V_\\text S$\n\n$v_{tot} = - \\text V_\\text S\\,e^{-t/\\text{RC}} + \\text V_\\text S$\n\nor\n\n$\\boxed{v_{tot} = \\text V_\\text S \\left (1 - e^{-t/\\text{RC}}\\right )}$\n\nIf the capacitor voltage starts at $0$ the RC step total response is $v_{tot} = \\text V_\\text S \\, \\left (1 - e^{-t/\\text{RC}}\\right )$.\n\n## What to remember\n\nYou don’t need to memorize the equation for the step response, but you should remember what happens,\n\n• The voltage starts at some initial value prior to the step, $\\text V_0$.\n• When the step arrives the voltage heads toward the destination voltage, $\\text V_\\text S$, rising (or falling) with a smooth exponential shape controlled by the time constant, $\\text{RC}$.\n• The output approaches $\\text V_\\text S$, the steady-state value forced by the input.\n\n## Concept check\n\nSuppose the input voltage makes another step in the downward direction a little later, from $\\text V_{\\text S}$ back down to $\\text V_0$. Assume the original $\\text V_0 = 2\\,\\text V$ and $\\text V_{\\text S} = 6\\,\\text V$.\n\nLet $\\text R = 3\\,\\text K\\Omega$, $\\text C = 0.4\\,\\mu\\text F$.\n\nHow does the capacitor voltage respond?\n\nHint: Reverse the roles of the high and low voltages, so you can think of it this way,\n$\\text V_0$ (starting voltage) $= 6\\,\\text V$ and $\\text V_{\\text S}$ (ending voltage) $= 2\\,\\text V$.\n\n$v(t) =$ ________\n\nThe moment of interest is the downward step, so reassign $t=0$ to be the time of the downward step. By repositioning $t=0$ we can use the step response expression above.\n\n$v(t) = \\text V_\\text S + (\\text V_0 - \\text V_\\text S)\\,e^{-t/\\text{RC}}$\n\n$v(t) = 2 + (6 - 2)\\,e^{-t/(3\\,\\text k \\,\\cdot \\, 0.4 \\,\\mu)}$\n\n$v(t) = 2 + 4\\,e^{-t/1.2\\,\\text{msec}}$\n\n## Simulation model\n\nTo explore further, run this simulation model in a new browser tab.\n\n• Click on DC in the top menu bar to perform a static DC analysis. What is the initial voltage on the capacitor?\n• Click on TRAN to run a transient analysis (voltage versus time). See the $\\text{RC}$ step response for voltage and current. What are the starting and ending voltages of the step input (red)? What is the final voltage on the capacitor (cyan)?\n• Double click on the voltage source. Change the start and end voltages and see what happens. What happens if the start voltage is higher than the end voltage?\n• Add a current probe anywhere in the loop and give it a distinct color. TRAN again. What is the current at the start and end? Describe what happens in between.\n• Change the voltage source from step to square. Reset the low and high voltages to 2V and 6V. Set the frequency to $50\\,\\text{Hz}$. Change the TRAN time to $29\\,\\text{msec}$. Compare the down step to an up step. What is different? What is the same?\n• Change the square wave frequency to $200\\,\\text{Hz}$ and TRAN again. Describe what happens.\n• Zoom out the schematic page and build a copy of the circuit next to the original. Try different values for $\\text R$ and $\\text C$ in the new circuit. Add a voltage probe to the new circuit. Simulate and compare both voltages on the same graph.\n\n## Summary\n\nWe solved an $\\text{RC}$ network driven by a step voltage. We used Kirchhoff’s Current Law to create a non-homogeneous differential equation representing the circuit. In differential equation vocabulary we superimposed the homogeneous solution with a particular solution. In engineering vocabulary we superimposed the natural response with the forced response.\n\n• The natural response is what the circuit does with its initial energy, with the input suppressed. The natural response always fades to $0$.\n\n• The forced response is the engineering name for the particular response corresponding to the long-term steady-state circuit response.\n\n• The total response is the natural response plus the forced response.\n\nThe step response of an $\\text R\\text C$ network is,\n\n$v = \\text V_\\text S + (\\text V_0 - \\text V_\\text S)\\,e^{-t/\\text{RC}}$\n\nwhere $\\text V_\\text S$ is the step voltage and $\\text V_0$ is the starting voltage on the capacitor.\n\nIf the capacitor voltage starts at $0$ the step response expression is a bit simpler,\n\n$v = \\text V_\\text S \\, \\left (1 - e^{-t/\\text{RC}}\\right )$\n\n## Appendix - Separable differential equation\n\nIt is possible to solve this non-homogeneous differential equation directly, without using the principle of superposition and without guessing an exponential solution.\n\n$\\dfrac{dv}{dt} + \\dfrac{v}{\\text{RC}} = \\dfrac{\\text V_\\text S}{\\text{RC}}$\n\nThis turns out to be a separable differential equation. If you learned this technique in a differential equations class you can solve both the $\\text{RC}$ and $\\text{RL}$ steps function with this method.\n\nA differential equation is separable if you can sort all the voltage terms, $v$’s and $dv$’s, into a product on one side and sort the time terms, $dt$’s, into a product on the other side. That happens with this equation.\n\nThis isn’t the usual way to teach this circuit because the method doesn’t generalize to other forcing inputs, and it does not provide insight into the natural and forced components of the solution.", null, "The non-homogeneous differential equation is,\n\n$\\dfrac{dv}{dt} + \\dfrac{v}{\\text{RC}} = \\dfrac{\\text V_\\text S}{\\text{RC}}\\qquad$ with initial condition: $v(0) = \\text V_0$\n\nRearrange terms to isolate the derivative,\n\n$\\dfrac{dv}{dt} = -\\dfrac{v - \\text V_\\text S}{\\text{RC}}$\n\nRearrange again to separate the $v$ and $dv$ terms to one side and $dt$ term to the other,\n\n$\\dfrac{dv}{v - \\text V_\\text S} = - \\dfrac{dt}{\\text{RC}}$\n\nIntegrate both sides and apply the initial condition,\n\n\\begin{aligned} \\displaystyle \\int_{\\text V_0}^{v(t)}{\\dfrac{dv}{v - \\text V_\\text S}} &= - \\int_0^t{\\dfrac{dt}{\\text{RC}}} \\\\ \\\\ \\ln(v - \\text V_\\text S) \\,\\bigg \\vert_{V_0}^{v(t)} &= - \\dfrac{t}{\\text{RC}}\\,\\bigg \\vert_0^{t} \\\\ \\\\ \\ln(v(t) - \\text V_\\text S) - \\ln(\\text V_0 - \\text V_\\text S) &= -\\dfrac{t}{\\text{RC}} + 0 \\\\ \\\\ \\ln \\dfrac{v(t) - \\text V_\\text S}{\\text V_0 - \\text V_\\text S} &= -\\dfrac{t}{\\text{RC}} \\end{aligned}\n\nClear the natural log by taking the exponential of both sides,\n\n$\\dfrac{v(t) - \\text V_\\text S}{\\text V_0 - \\text V_\\text S} = e^{-t/\\text{RC}}$\n\nRearrange to isolate $v(t)$ on the left side,\n\n$v(t) - \\text V_\\text S = (\\text V_0 - \\text V_\\text S) e^{-t/\\text{RC}}$\n\nAnd we get the same result we came up with in the main article,\n\n$v(t) = \\text V_\\text S + (\\text V_0 - \\text V_\\text S)\\,e^{-t/\\text{RC}}$\n\nSal has a sequence of videos where he covers this type of separable differential equation. He does a worked example to solve a population growth problem.\n\nThe derivation in this appendix is from Alexander and Sadiku, Fundamentals of Electric Circuits, 5th Edition, p. 274.\n\nFootnotes:\n\n1. yet-to-be-determined — Definition: do not know or have not decided; will in the future." ]
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https://www.freezingblue.com/flashcards/print_preview.cgi?cardsetID=70230
[ "# biometrics\n\n The flashcards below were created by user wvuong on FreezingBlue Flashcards. What is a Type I error? We reject H0 when it is actually true. it equals to alpha What is a Type II error we accept H0 when the alternative is true hypothesis testing: what is statistical power of a test? power is probability of rejecting null hypothesis when null hypotehsis is false. power equal to 1 - beta. hypothesis testing: general procedure for obtaining a decision rule? assume H0 is true, probability distribution of test statistic, set alpha. decreasing level of significance for test of hypothesis change the probability of Type II error? decreasing it would increase probability Type II error cuz its greater probability of assuming H0 is true when it should be rejected how to reduce probability of a Type II? two ways: 1. increase alpha, 2. increase sample size (increases power of test) why might fail to reject null hypothesis? 1. H0 is really true2. H0 is false, but not enough data to reject H0 assumptions of a t-test for two independent groups? assume they are independent of each other, following a normal distribution, means for two groups can be different but variances are equal degrees of freedom for Poisson and normal? Poisson have 1 parameter, means df= k-2 normal have 2 parameters, means df = k-3 why small value pose a problem for chi-square? small values poses a problem cuz cause the chi-square to be artificially high Authorwvuong ID70230 Card Setbiometrics Descriptionexam2 Updated2011-03-02T20:57:04Z Show Answers" ]
[ null ]
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https://myaptitude.in/cat/quant/if-the-harmonic-mean-between-two-positive-numbers-is-to-their-geometric-mean-as-12-13
[ "If the harmonic mean between two positive numbers is to their geometric mean as 12 : 13; then the numbers could be in the ratio\n\n1. 12 : 13\n2. 4 : 9\n3. 2 : 3\n4. 1/12 : 1/13\n\nLet a and b be two numbers.\n\nHarmonic Mean, HM = 2ab(a+b)\n\ngeometric Mean, GM = √(ab)\n\n2ab(a+b) : √(ab) = 12:13\n\n(a+b)/√(ab) = 13/6\n\n√(a/b) +√(b/a) = 13/6\n\nLet √(a/b) = x\n\nx + 1/x = 13/6\n\n6x2 - 13x + 6 = 0\n\nx = 2/3 or 3/2\n\na/b = x2\n\na/b = 4/9\n\nThe correct option is B." ]
[ null ]
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https://howardat58.wordpress.com/tag/construction/
[ "# Tag Archives: construction\n\n## Linear transformations, geometrically\n\nFollowing a recent blog post relating a transformation of points on a line to points on another line to the graph of the equation relating the input and output I thought it would be interesting to explore the linear and affine mappings of a plane to itself from a geometrical construction perspective.\n\nIt was ! (To me anyway)\n\nThese linear mappings  (rigid and not so rigid motions) are usually  approached in descriptive and manipulative  ways, but always very specifically. I wanted to go directly from the transformation as equations directly to the transformation as geometry.\n\nTaking an example, (x,y) maps to (X,Y) with the linear equations\n\nX = x + y + 1 and Y = -0.5x +y\n\nit was necessary to construct a point on the x axis with the value of X, and likewise a point on the y axis with the value of Y. The transformed (x,y) is then the point (X,Y) on the plane.\n\nThe construction below shows the points and lines needed to establish the point(X,0), which is G in the picture, starting with the point D as the (x,y)", null, "The corresponding construction was done for Y, and the resulting point (X,Y) is point J. Point D was then forced to lie on a line, the sloping blue line, and as it is moved along the line the transformed point J moves on another line", null, "Now the (x,y) point (B in the picture below, don’t ask why!) is forced to move on the blue circle. What does the transformed point do? It moves on an ellipse, whose size and orientation are determined by the actual transformation. At this point matrix methods become very handy.(though the 2D matrix methods cannot deal with translations)", null, "All this was constructed with my geometrical construction program (APP if you like) called GEOSTRUCT and available as a free web based application from\n\nhttp://www.mathcomesalive.com/geostruct/geostructforbrowser1.html\n\nThe program produces a listing of all the actions requested, and these are listed below for this application:\n\nLine bb moved to pass through Point A\nNew line cc created, through points B and C\nNew Point D\nNew line dd created, through Point D, at right angles to Line aa\nNew line ee created, through Point D, at right angles to Line bb\nNew line ff created, through Point D, parallel to Line cc\nNew point E created as the intersection of Line ff and Line aa\nNew line gg created, through Point E, at right angles to Line aa\nNew line hh created, through Point B, at right angles to Line bb\nNew point F created as the intersection of Line hh and Line gg\nNew line ii created, through Point F, parallel to Line cc\nNew point G created as the intersection of Line ii and Line aa\n\nG is the X coordinate, from X = x + y + 1 (added by me)\n\nNew line jj created, through Point G, at right angles to Line aa\nNew line kk created, through Point D, at right angles to Line cc\nNew point H created as the intersection of Line kk and Line bb\nNew point I created, as midpoint of points H and B\nNew line ll created, through Point I, at right angles to Line bb\nNew point J created as the intersection of Line ll and Line jj\n\nJ is the Y coordinate, from Y = -x/2 + y  (added by me)\nand K is the transformed point (X,Y) Point J chosen as the tracking point (added by me)\n\nNew Line mm\nPoint D moved and placed on Line mm\n\n1 Comment\n\n## Vertex of a parabola – language in math again\n\nHere are some definitions of the vertex of a parabola.\n\nOne is complete garbage, one is correct  though put rather chattily.\n\nThe rest are not definitions, though very popular (this is just a selection). But they are true statements\n\nMathwarehouse: The vertex of a parabola is the highest or lowest point, also known as the maximum or minimum of a\nparabola.\nMathopenref: A parabola is the shape defined by a quadratic equation. The vertex is the peak in the curve as shown on\nthe right. The peak will be pointing either downwards or upwards depending on the sign of the x2 term.\nVirtualnerd: Each quadratic equation has either a maximum or minimum, but did you that this point has a special name?\nIn a quadratic equation, this point is called the vertex!\nMathwords: Vertex of a Parabola: The point at which a parabola makes its sharpest turn.\nPurplemath: The point on this axis which is exactly midway between the focus and the directrix is the “vertex”; the vertex is the point where the parabola changes direction.\nWikibooks: One important point on the parabola itself is called the vertex, which is the point which has the smallest distance between both the focus and the directrix. Parabolas are symmetric, and their lines of symmetry pass through the vertex.\nHotmath: The vertex of a parabola is the point where the parabola crosses its axis of symmetry\n\nScoring is 10 points for finding the garbage definition and 5 points for the correctish definition !!!! Go for it!\n\nWhen I studied parabolas, back in 1958 or so (!) the parabola had an apex. So I checked the meaning of vertex, and found that the word was frequently misused.\n\nHere is a good account: https://en.wikipedia.org/wiki/Vertex_(curve)\n\nBasically a vertex of a curve is a point where the curvature is a maximum or a minimum (in non math terms, most or least curved).\n\nHere are two fourth degree polynomials, one has three vertices and the other has five. The maximum curvature points are indicated. The minimum curvature points are at the origin for the first curve, and at the points of inflexion for the second curve (curvature = zero)\n\nA hyperbola has two vertices, one on each branch; they are the closest of any two points lying on opposite branches of the hyperbola, and they lie on the principal axis. On a parabola, the sole vertex lies on the axis of symmetry. On an ellipse, two of the four vertices lie on the major axis and two lie on the minor axis.\n\nFor a circle, which has constant curvature, every point is a vertex.\n\nThe center of curvature at a (nice) point on a curve is the center of the closest matching circle at that point. This circle will usually lie “outside” the curve on one side of the point, and “inside” the curve on the other side. Look carefully at the picture. It is called the osculating or kissing circle (from the Latin).\n\nThe center of curvature can be estimated by taking two point close to the point of interest, finding the tangents at these points, and then the lines at right angles to them and through the points. the center of curvature is roughly at the point of intersection of these two lines", null, "The diagram below shows this estimate, for the blue parabola, at the vertex.", null, "Finally (this has gone on further than expected!) I found this delightful gif.", null, "Filed under conic sections, conics, construction, geometry, language in math, teaching\n\n## Real problems with conic sections (ellipse, parabola) part two\n\nSo suppose we have a parabolic curve and we want to find out stuff about it.\n\nIts equation … Oh, we have no axes.\n\nIts focus … That would be nice, but it is a bit out of reach.\n\nIts axis, in fact its axis of symmetry … Fold it in half? But how?\n\nTry the method of part one, with the ellipse. (previous post)", null, "This looks promising. I even get another axis, for my coordinate system, if I really want the equation.\n\nNow, analysis of the standard equation for a parabola (see later) says that a line at 45 deg to the axis, as shown, cuts the parabola at a point four focal lengths from the axis. In the picture, marked on the “vertical”axis, this is the length DH", null, "So I need a point one quarter of the way from D to H. Easy !", null, "and then the circle center D, with radius DH/4 cuts the axis of the parabola at the focal point (the focus).\n\nEven better, we get the directrix as well …", null, "and now for the mathy bit (well, you do the algebra, I did the picture)", null, "Yes, I know that this one points up and the previous one pointed to the right !\n\nAll diagrams were created with my geometrical construction program, GEOSTRUCT\n\nYou will find it here:\n\nwww.mathcomesalive.com/geostruct/geostructforbrowser1.html\n\nFiled under conic sections, construction, engineering, geometry, teaching\n\n## GEOSTRUCT, a program for investigative geometry\n\nI have been developing this computer software / program / application for some years now, and it is now accessible as a web page, to run in your browser.\n\nIt provides basic geometric construction facilities, with lines, points and circles, from which endless possibilities follow.\n\nJust try it out, it’s free.\n\nClick on this or copy and paste for later : www.mathcomesalive.com/geostruct/geostructforbrowser1.html\n\n.Here are some of the basic features, and examples of more advanced constructions, almost all based on straightedge and compass, from “make line pass through a point” to “intersection of two circles”, and dynamic constructions with rolling and rotating circles.", null, "Two lines, with points placed on them", null, "Three random lines with two points of intersection generated", null, "Five free points, three generated circles and a center point", null, "Three free points, connected as point pairs, medians generated", null, "Two free circles and three free points, point pairs and centers generated", null, "GIF showing points of intersection of a line with a circle", null, "Construction for locus of hypocycloid", null, "", null, "GIF showing a dilation (stretch) in the horizontal direction", null, "Piston and flywheel", null, "Construction for circle touching two circles", null, "Construction for the locus of a parabola, focus-directrix definition.\n\n1 Comment\n\nFiled under education, geometry, math, operations, teaching\n\n## Duality, fundamental and profound, but here’s a starter for you.\n\nDuality, how things are connected in unexpected ways. The simplest case is that of the five regular Platonic solids, the tetrahedron, the cube, the octahedron, the dodecahedron and the icosahedron. They all look rather different, BUT…..\n\ntake any one of them and find the mid point of each of the faces, join these points up, and you get one of the five regular Platonic solids. Do it to this new one and you get back to the original one. Calling the operation “Doit” we get\n\ntetrahedron –Doit–> tetrahedron –Doit–> tetrahedron\ncube –Doit–> octahedron –Doit–> cube\ndodecahedron –Doit–> icosahedron –Doit–> dodecahedron\n\nThe sizes may change, but we are only interested in the shapes.\n\nThis is called a Duality relationship, in which the tetrahedron is the dual of itself, the cube and octahedron are duals of each other, and the dodecahedron and icosahedron are also duals of each other.\n\nNow we will look at lines and points in the x-y plane.\n\n3x – 2y = 4 and y = (3/2)x + 2 and 3x – 2y – 4 = 0 are different ways of describing the same line, but there are many more. We can multiply every coefficient, including the constant, by any number not 0 and the result describes the same line, for example 6x – 4y = 8, or 0.75x – 0.5y = 1, or -0.75x + 0.5y + 1 = 0\n\nThis means that a line can be described entirely by two numbers, the x and the y coefficients found when the line equation is written in the last of the forms given above. Generally this is ax + by + 1 = 0\n\nNow any point in the plane needs two numbers to specify it, the x and the y coordinates, for example (2,3)\n\nSo if a line needs two numbers and a point needs two numbers then given two numbers p and q I can choose to use then to describe a point or a line. So the numbers p and q can be the point (p,q) or the line px + qy + 1 = 0\n\nThe word “dual” is used in this situation. The point (p,q) is the dual of the line px + qy + 1 = 0, and vice versa.", null, "The line joining the points C and D is dual to the point K, in red.  The line equation is 2x + y = 3, and we rewrite it in the “standard” form as  -0.67x – 0.33y +1 = 0  so we get  (-0.67, -0.33) for the coordinates of the dual point K.\n\nA quick calculation (using the well known formula) shows that the distance of the line from the origin multiplied by the distance of the point from the origin is a constant (in this case 1).\n\nThe second picture shows the construction of the dual point.", null, "What happens as we move the line about ? Parallel to itself, the dual point moves out and in.\n\nMore interesting is what happens when we rotate the line around a fixed point on the line:", null, "The line passes through the fixed point C.  The dual point traces out a straight line, shown in green.\n\nThis can be interpreted as “A point can be seen as a set of concurrent lines”, just as a line can be seen as a set of collinear points (we have fewer problems with the latter).\n\nIt gets more interesting when we consider a curve. There are two ways of looking at a curve, one as a (fairly nicely) organized set of points ( a locus), and the other as a set of (fairly nicely) arranged lines (an envelope).\n\nA circle is a set of points equidistant from a central point, but it is also the envelope of a set of lines equidistant from a central point (the tangent lines).\n\nSo what happens when we look for the dual of a circle? We can either find the line dual to each point on the circle, or find the point dual to each tangent line to the circle. Here’s both:", null, "In this case the circle being dualled is the one with center C, and the result is a hyperbola, shown in green.  The result can be deduced analytically, but it is a pain to do so.", null, "The hyperbola again.  It doesn’t look quite perfect, probably due to rounding errors.\n\nThe question remains – If I do the dualling operation on the hyperbola, will I get back to the circle ?\n\nAlso, why a hyperbola and not an ellipse ? Looking at what is going on suggests that if the circle to be dualled has the origin inside then we will get an ellipse. This argument can be made more believable with a little care !\n\nIf you get this far and want more, try this very heavy article:\n\nhttp://en.wikipedia.org/wiki/Duality_(mathematics)\n\nFiled under geometry, math, teaching\n\n## Egyptian fractions\n\nSuppose you have five loaves of bread and you want to divide them evenly among seven people.  You could cut the five loaves in thirds, then you’d have 15 thirds.  Give two of them to each of the seven people.  You’ll have one third of a loaf left.  Cut it into seven equal slices and give one to each person.", null, "There may be other solutions.   a = b = 3, c = 21.   (Egyptian Fractions)\n\n……………………………………………………………………………………………………\n\nFiled under arithmetic, fractions, math, operations\n\n## Interesting geometry result, again\n\nTo show that the angle bisector of an angle in a triangle splits the opposite side in the ratio of the two adjacent sides.\n\nMy first proof used angles in the same segment. See\n\nhttps://howardat58.wordpress.com/2014/05/14/interesting-geometry-result/\n\nSeveral tries later (today) and i came up with this annoyingly simple proof:", null, "Filed under geometry, math, teaching\n\n## The angle bisector theorem and a locus\n\nThe theorem states that if we bisect an angle of a triangle then the two parts of the side cut by the bisector are in the same ratio as the two other sides of the triangle. So I thought, what if we move the point, G in the gif below, so that GB always bisects the angle AGC, then where does it go ? Or, more mathematically, what is its locus. Geometry failed me at this point so I did a coordinate geometry version of the ratios and found that the locus was a circle ( a little surprised !). The algebra is fairly simple.", null, "What was a real surprise was that if we take the origin of measurements to be the other point where the circle cross the line ABC, then point C is at the harmonic mean of points A and B. There is YOUR problem from this post.\n\nGetting the construction to show all this was tricky. It is shown below.", null, "I did the construction on my geometry program, Geostruct (see my Software page).\n\nLine bb passes through A. Point D is on line bb. Point E is on this line and also on the line through C parallel to line cc joining B and D, So AD and DE are in the same ratio as AC and CB. When point D is moved the ratios are unchanged (feature of the program). So the point of interest is the intersection of a circle centre A, radius AD, and a circle centre C and radius DE (= FC)\n\nFiled under algebra, geometry, teaching\n\n## Quadrilaterals – a Christmas journey – part 1\n\nIt all started with an aside in a blog post in which the author said how\nsome students have a real problem with statements such as “A square is a\nrhombus”.\n\nFrom early years kids naturally like exclusive definitions, and have to be weaned off this. This would be easier if we were more careful with the word “is”. Even to me the statement ” a square is a rhombus” sounds weird, if not actually wrong. It would be better to be less brutal, and say “a square is also a rhombus” (and all the other such statements).\nEven better, and quite mathematical, is the phrasing “a square is a special case of a rhombus”, as the idea of special cases is very important, and usually overlooked.\nIt is odd that the classification of triangles is done entirely with adjectives and the difficulty is thus avoided (but see later).\nAfter fighting with a Venn Diagram I did a tree diagram to show the relationships:", null, "“triangle” : three angles\n“pentagon” and the rest : … angles\nThe odd one out is the quadrilateral.\nTake a look:", null, "It consists of four line segments, AB, BD, DC and CA\n\nLet us see what the full extended lines look like:", null, "Let ab be the name for the full line through A and B\nLikewise ac, bd and dc\nThen we can see that the quadrilateral is determined by the points of intersection of the two pairs of lines ab,cd and ac,bd.\n\nab and cd meet at point E; ac and bd meet at point F\nBut if we consider the four lines then there are three ways of pairing them up. The two others are ab,ac with bd,cd and ab,bd with ac,cd.\nThis gives us two more quadrilaterals, and they all have the property that each side falls on one only of the four lines.\nThe three quadrilaterals are ABCD, FCEB and FDEA\nABCD is convex, FCEB is twisted and FDEA is not convex (concave at A)\nNot only that, but also the first two are fitted together to give the third one.\nThis arrangement is called the “complete quadrilateral”, and has four lines and six points.\n\nMore next time.\n\n1 Comment\n\nFiled under abstract, education, geometry, language in math\n\n## Halloween fun\n\nFound on the net. With avocados raining down on my porch roof this seems a good use for them!", null, "“To hell with pumpkins, try the Guaco-lantern" ]
[ null, "https://howardat58.files.wordpress.com/2016/02/transform-of-x.png", null, "https://howardat58.files.wordpress.com/2016/02/gif-for-lin-affine-trans1.gif", null, "https://howardat58.files.wordpress.com/2016/02/gif-for-lin-affine-trans2.gif", null, "https://howardat58.files.wordpress.com/2015/06/01center-of-curvature.png", null, "https://howardat58.files.wordpress.com/2015/06/02center-of-curvature.png", null, "https://howardat58.files.wordpress.com/2015/06/01lissajous-curveosculatingcircle3vectors_animated.gif", null, "https://howardat58.files.wordpress.com/2015/06/parabola-find-the-focus1.png", null, "https://howardat58.files.wordpress.com/2015/06/parabola-find-the-focus2.png", null, "https://howardat58.files.wordpress.com/2015/06/parabola-find-the-focus3.png", null, "https://howardat58.files.wordpress.com/2015/06/parabola-find-the-focus4.png", null, "https://howardat58.files.wordpress.com/2015/06/parabola-find-the-focus-math.png", null, "https://howardat58.files.wordpress.com/2015/05/help-pic-1.png", null, "https://howardat58.files.wordpress.com/2015/05/help-pic-3.png", null, "https://howardat58.files.wordpress.com/2015/05/help-pic-6.png", null, "https://howardat58.files.wordpress.com/2015/05/help-pic-7.png", null, "https://howardat58.files.wordpress.com/2015/05/help-pic-5.png", null, "https://howardat58.files.wordpress.com/2015/04/gif-line-and-circle.gif", null, "https://howardat58.files.wordpress.com/2015/05/hypocycloid-locus.png", null, "https://howardat58.files.wordpress.com/2015/05/circle-in-a-segment.png", null, "https://howardat58.files.wordpress.com/2015/01/gif002.gif", null, "https://howardat58.files.wordpress.com/2015/02/gif-piston-cylinder.gif", null, "https://howardat58.files.wordpress.com/2015/02/gif-touching2circles.gif", null, "https://howardat58.files.wordpress.com/2015/02/gif-parabola.gif", null, "https://howardat58.files.wordpress.com/2015/05/dual-of-a-rotating-line-cleaned-up1.png", null, "https://howardat58.files.wordpress.com/2015/05/dual-of-a-rotating-line-construction1.png", null, "https://howardat58.files.wordpress.com/2015/05/gif-duality-rotating-line.gif", null, "https://howardat58.files.wordpress.com/2015/05/dual-of-a-circle4.png", null, "https://howardat58.files.wordpress.com/2015/05/dual-of-a-circle3.png", null, "https://i2.wp.com/qlx.is.quoracdn.net/main-3542566ac1fb26ea.png", null, "https://howardat58.files.wordpress.com/2015/02/bisector-of-angle-in-a-triangle-splits.png", null, "https://howardat58.files.wordpress.com/2015/01/gif-bisector-locus.gif", null, "https://howardat58.files.wordpress.com/2015/01/locus-angle-bisector-point-full.png", null, "https://howardat58.files.wordpress.com/2014/12/quadrilaterals-1-pic.png", null, "https://howardat58.files.wordpress.com/2014/12/arect2.png", null, "https://howardat58.files.wordpress.com/2014/12/arect3.png", null, "https://howardat58.files.wordpress.com/2014/10/guacolantern.jpg", null ]
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https://www.jpost.com/arts-and-culture/books/the-pleasure-principle
[ "(function (a, d, o, r, i, c, u, p, w, m) { m = d.getElementsByTagName(o), a[c] = a[c] || {}, a[c].trigger = a[c].trigger || function () { (a[c].trigger.arg = a[c].trigger.arg || []).push(arguments)}, a[c].on = a[c].on || function () {(a[c].on.arg = a[c].on.arg || []).push(arguments)}, a[c].off = a[c].off || function () {(a[c].off.arg = a[c].off.arg || []).push(arguments) }, w = d.createElement(o), w.id = i, w.src = r, w.async = 1, w.setAttribute(p, u), m.parentNode.insertBefore(w, m), w = null} )(window, document, \"script\", \"https://95662602.adoric-om.com/adoric.js\", \"Adoric_Script\", \"adoric\",\"9cc40a7455aa779b8031bd738f77ccf1\", \"data-key\");\nvar domain=window.location.hostname; var params_totm = \"\"; (new URLSearchParams(window.location.search)).forEach(function(value, key) {if (key.startsWith('totm')) { params_totm = params_totm +\"&\"+key.replace('totm','')+\"=\"+value}}); var rand=Math.floor(10*Math.random()); var script=document.createElement(\"script\"); script.src=`https://stag-core.tfla.xyz/pre_onetag?pub_id=34&domain=\\${domain}&rand=\\${rand}&min_ugl=0\\${params_totm}`; document.head.append(script);" ]
[ null ]
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https://nl.mathworks.com/help/phased/ref/phased.sumdifferencemonopulsetracker-system-object.html
[ "# phased.SumDifferenceMonopulseTracker\n\nSum and difference monopulse for ULA\n\n## Description\n\nThe `SumDifferenceMonopulseTracker` object implements a sum and difference monopulse algorithm on a uniform linear array.\n\nTo estimate the direction of arrival (DOA):\n\n1. Define and set up your sum and difference monopulse DOA estimator. See Construction.\n\n2. Call `step` to estimate the DOA according to the properties of `phased.SumDifferenceMonopulseTracker`. The behavior of `step` is specific to each object in the toolbox.\n\nNote\n\nStarting in R2016b, instead of using the `step` method to perform the operation defined by the System object™, you can call the object with arguments, as if it were a function. For example, ```y = step(obj,x)``` and `y = obj(x)` perform equivalent operations.\n\n## Construction\n\n`H = phased.SumDifferenceMonopulseTracker` creates a tracker System object, `H`. The object uses sum and difference monopulse algorithms on a uniform linear array (ULA).\n\n`H = phased.SumDifferenceMonopulseTracker(Name,Value)` creates a ULA monopulse tracker object, `H`, with each specified property Name set to the specified Value. You can specify additional name-value pair arguments in any order as (`Name1`,`Value1`,...,`NameN`,`ValueN`).\n\n## Properties\n\n `SensorArray` Handle to sensor array Specify the sensor array as a handle. The sensor array must be a `phased.ULA` object. Default: `phased.ULA` with default property values `PropagationSpeed` Signal propagation speed Specify the propagation speed of the signal, in meters per second, as a positive scalar. You can specify this property as single or double precision. Default: Speed of light `OperatingFrequency` System operating frequency Specify the operating frequency of the system in hertz as a positive scalar. The default value corresponds to 300 MHz. You can specify this property as single or double precision. Default: `3e8` `NumPhaseShifterBits` Number of phase shifter quantization bits The number of bits used to quantize the phase shift component of beamformer or steering vector weights. Specify the number of bits as a non-negative integer. A value of zero indicates that no quantization is performed. You can specify this property as single or double precision. Default: `0`\n\n## Methods\n\n step Perform monopulse tracking using ULA\nCommon to All System Objects\n`release`\n\nAllow System object property value changes\n\n## Examples\n\ncollapse all\n\nDetermine the direction of a target at a 60.1° broadside angle to a ULA starting with an approximate direction of 60°\n\n```array = phased.ULA('NumElements',4); steervec = phased.SteeringVector('SensorArray',array); tracker = phased.SumDifferenceMonopulseTracker('SensorArray',array); x = steervec(tracker.OperatingFrequency,60.1).'; est_dir = tracker(x,60)```\n```est_dir = 60.1000 ```\n\nexpand all\n\n## References\n\n Seliktar, Y. Space-Time Adaptive Monopulse Processing. Ph.D. Thesis. Georgia Institute of Technology, Atlanta, 1998.\n\n Rhodes, D. Introduction to Monopulse. Dedham, MA: Artech House, 1980.\n\n## Version History\n\nIntroduced in R2011a" ]
[ null ]
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https://www.physicsforums.com/threads/thermodynamics-gas-expansion-with-piston-friction.963282/
[ "# Thermodynamics: Gas Expansion with Piston Friction\n\n• Chestermiller\n\n#### Chestermiller\n\nStaff Emeritus\nHomework Helper\nA friend of mine and I have been discussing how to apply the first law of thermodynamics to analyze the quasi static expansion of an ideal gas in a cylinder featuring a piston having both mass and friction (with the cylinder). We have identified two different systems that can be used in the analysis:\n\n1. gas alone as system, with piston as part of the surroundings\n2. gas and piston (and cylinder) as system\n\nWe wanted to see how the analysis using the first law of thermodynamics would play out in each of these approaches, knowing that, ultimately, the answer would have to come out the same in each case. So here is my specification of the problem:\n\nThere is a vertical insulated cylinder cross sectional area A containing an ideal gas. There is a piston of mass m situated above the gas. The piston is insulated at the top and has negligible heat capacity so that any frictional heat generated by piston contact with the cylinder is ultimately transferred to the gas (rather than the surroundings). The frictional force F is always constant and present both initially and finally. This can be achieved if we say that the coefficient of static friction is equal to the coefficient of kinetic friction, and that, in the initial and final states, the piston is at the verge of slipping (This is an idealization which does not detract from what we are trying to achieve in our analysis). We have a force f applied downward on the piston which decreases gradually (quasi statically) from ##f_i## in the initial state of the system to ##f_f## in the final state of the system; this is how we bring about the desired volume increase. There are n moles of ideal gas in the cylinder, initially at temperature ##T_i##, and initially at mechanical equilibrium with the mass of the piston, the frictional force F, and the outside downward force ##f_i##.\n\nI am now going to stop and allow my friend to make comments and suggestions about the problem description. Is this basically what we had in mind? (Others are invited to participate).\n\nChet\n\nLast edited:\n•", null, "JD_PM\n\nYou are saying that in the initial and final state the piston is at the verge of slipping. Doesn't that imply that the net force (and hence pressure) on the piston is the same in the initial and final states?\n\nEDIT:NVM I now noticed about the external force F acting on the piston. Is the external force present in the initial and final states or is it present only during the movement of the piston?\n\nYou are saying that in the initial and final state the piston is at the verge of slipping. Doesn't that imply that the net force (and hence pressure) on the piston is the same in the initial and final states?\n\nEDIT:NVM I now noticed about the external force F acting on the piston. Is the external force present in the initial and final states or is it present only during the movement of the piston?\nI think I made that clear in the problem statement.\n\nThis problem is not about how the friction is handled. The focus of the problem is on the thermodynamics of the system. The friction force is as I say it is: F in the initial state, F during the gas expansion, and F in the final state.\n\nPerhaps I misunderstand the question but consider..\n\nA Champaign cork is held in by a combination of things, tension in the wire cage, friction between cork and bottle and the weight of the cork.\n\nIf you shake it up, increasing the pressure inside so the cork starts moving slightly the gas is allowed to expand. As it expands it does work loosing energy to all of the things that are opposing the motion of the cork... eg The energy stored in stretching the wire, friction, gravity and inertia. Conservation of energy basically says this lot must add up to the energy lost by the gas.\n\nThe slight complication is you say..\n\nany frictional heat generated by piston contact with the cylinder is ultimately transferred to the gas (rather than the surroundings).\n\nThat only slightly changes the sum you do when applying conservation of energy. I believe that ultimately it means you can ignore energy lost to friction because it appears on both sides of the equation.\n\nPerhaps I misunderstand the question but consider..\n\nA Champaign cork is held in by a combination of things, tension in the wire cage, friction between cork and bottle and the weight of the cork.\n\nIf you shake it up, increasing the pressure inside so the cork starts moving slightly the gas is allowed to expand. As it expands it does work loosing energy to all of the things that are opposing the motion of the cork... eg The energy stored in stretching the wire, friction, gravity and inertia. Conservation of energy basically says this lot must add up to the energy lost by the gas.\n\nThe slight complication is you say..\n\nThat only slightly changes the sum you do when applying conservation of energy. I believe that ultimately it means you can ignore energy lost to friction because it appears on both sides of the equation.\nThis is incorrect. The energy lost to friction cannot be ignored in the problem as I specified it. I refuse to change the problem description. It is exactly the way I want. The objective is not to decide what the exact model for frictional force should be. The friction model is what I said it is. The objective is to evaluate, using the first law of thermodynamics, the effect of specifying two different \"systems\" in the problem, and seeing if the different analyses lead to the same end result (as they must). So please, everyone, take your focus off the friction force model.", null, "", null, "Thank you inviting me to participate in the forum. Sorry for not jumping in sooner.\n\nThe subject for discussion is, as you said, to apply the first law in the analysis of a the quasi-static adiabatic expansion of an ideal gas in a cylinder having both mass and friction. I agree with your specification of the problem, although my original question during our prior discussion on the Physics Stack Exchange had to do with a non quasi-static, constant external pressure adiabatic expansion. I might still like to follow up on that after this analysis, if I still have issues.\n\nWith regard to the present problem description, I do have some questions on how to handle the piston mass when it is included as part of the system, as discussed later below.\n\nAs to the application of the first law, I think the system definition would only influence the manner in which energy transfers are accounted for, that is, how heat and/or work is determined, as defined by the first law equation. Of course the choice of system also determines where entropy is generated (internal or external to the system). In any case, I would like to use this a starting point for my comments on the initial analysis below.\n\nPlease refer to the diagrams abov, which are intended to help (at least me) visualize the two system definition approaches. The approach is similar to the one you introduced, regarding identification of system work based on system definition, in our previous discussion at the Physics Stack Exchange. (Note, however, I am using f for the imposed force on the outside face of the piston and F for the friction force in accordance with the current problem description, whereas they were reversed in our prior discussion).\n\nPISTON MASS:\n\nFirst you will note that I have left out the mass of the piston in this initial analysis, for the following reasons:\n\nIn the case of System 1, since the piston is part of the surroundings, one could simply add the force, mg, to the variable external force, f. This would simply modify the initial and final external force by a constant factor.\n\nIt is the case of System 2, where the piston is part of the system, where my questions arise. Here the gas is doing work in raising the piston (increasing its potential energy), but since the piston is part of the system the work does not cross the boundary, i.e. the work is not done on the surroundings. So technically this would not be W in the first law equation. On the other hand, there is no change in internal energy of the system since the decrease in the internal energy of the gas portion of the system equals the increase in potential energy of the mass portion of the system.\n\nQUESTION: Given that the increase in the potential energy portion of the system equals the decrease kinetic energy portion (gas), can we simply ignore the piston and apply the first law equation as if it were massless? Your thoughts?\n\nThe following pertains to the case where we ignore the mass of the piston in the two systems.\n\nSYSTEM 1:\n\nFriction, and therefore entropy, is generated outside the system. Since the cylinder walls and piston are part of the surroundings, the friction work occurs in the surroundings. Since the cylinder walls are part of the surroundings, and we know that friction work will increase the temperature of the cylinder walls, I am showing heat transfer (quasi-static) from the walls to the gas. But I am also showing the friction force F as part of the surroundings.\n\nQUESTION: Is this depiction correct? Should both the friction work and heat transfer be shown? I think so because in doing so the final conclusion about the change in internal energy will be consistent with that of System 2 which I think should be. Also, is it correct to interpret equation 7 to mean the work done by the system is equal to the reversible work, pdV, minus the irreversible (friction) work, dW F?\n\nSYSTEM 2:\n\nFor system 2, there is no heat transfer to the surroundings, so dQ=0. Friction work is internal to the system. So the only system work is dW f and we have the same as system 1. The change in internal energy is the same as System 1 and the system work is, once again, the reversible work minus the friction work.\n\nThat is a far as I can take it now, without resolving the questions asked. Any help or suggestions will be appreciated.\n\n#### Attachments\n\n•", null, "Delta2\nAfter my post and upon further thinking I believe I can answer some of my questions. This post is therefore a revision to my original post. (Not sure how to revise a post being new at the Forum). See revised diagrams. Regarding the following questions concerning System 1:\n\nIs this depiction correct? Should both the friction work and heat transfer be shown? I think so because in doing so the final conclusion about the change in internal energy will be consistent with that of System 2 which I think should be. Also, is it correct to interpret equation 7 to mean the work done by the system is equal to the reversible work, pdV, minus the irreversible (friction) work, dW F?\n\nI believe the depiction is incorrect. I can show the effect of friction as either negative work transfer (equivalent of gas compression) or as equivalent heat transfer but not both. Since the cylinder walls (and friction work) are outside the system (gas only) I am able to show it as heat transfer. See the revised diagram of System 1.\n\nRegarding the work done I think the interpretation is correct for System2. In System 1 you can view the process as reversible since the friction and thus entropy is generated is outside the system. But in System 2, the friction occurs within the system. So for System2 only the work is the reversible work minus the irreversible (friction) work, as shown in the updated depiction of System 2.", null, "#### Attachments\n\n•", null, "Delta2\nAfter my post and upon further thinking I believe I can answer some of my questions. This post is therefore a revision to my original post. (Not sure how to revise a post being new at the Forum). See revised diagrams. Regarding the following questions concerning System 1:\n\nIs this depiction correct? Should both the friction work and heat transfer be shown? I think so because in doing so the final conclusion about the change in internal energy will be consistent with that of System 2 which I think should be. Also, is it correct to interpret equation 7 to mean the work done by the system is equal to the reversible work, pdV, minus the irreversible (friction) work, dW F?\n\nI believe the depiction is incorrect. I can show the effect of friction as either negative work transfer (equivalent of gas compression) or as equivalent heat transfer but not both. Since the cylinder walls (and friction work) are outside the system (gas only) I am able to show it as heat transfer. See the revised diagram of System 1.\n\nRegarding the work done I think the interpretation is correct for System2. In System 1 you can view the process as reversible since the friction and thus entropy is generated is outside the system. But in System 2, the friction occurs within the system. So for System2 only the work is the reversible work minus the irreversible (friction) work, as shown in the updated depiction of System 2.\n\nView attachment 236873\nHi Bob.\n\nFirst of all, WELCOME TO PHYSICS FORUMS!\n\nSecondly, if you want to edit a previous post, go to the bottom of the page and hit the edit button. This will reopen the editing window. Afterwards, you can hit the SAVE EDITS button. If you want to reply to a post in sections, you hit the reply button at the bottom of the post.\n\nI had some trouble following the details of your analysis, so I am going to present my own short development. I think this will answer most of your questions.\n\nAs in your analysis, everything starts with the FORCE BALANCE ON THE PISTON:\n$$PA=mg+F+f$$or equivalently\n$$P=\\frac{mg}{A}+\\frac{F}{A}+\\frac{f}{A}$$\nAnd, if there is a differential change in volume dV, we have\n$$PdV=\\frac{mg}{A}dV+\\frac{F}{A}dV+\\frac{f}{A}dV\\tag{1}$$\n\nFIRST LAW OF THERMODYNAMICS APPLIED TO SYSTEM 1, THE GAS:\n$$dU=dQ-PdV\\tag{2}$$\nwhere dQ is the differential heat transferred from the piston to the gas.\n\nFIRST LAW OF THERMODYNAMICS APPLIED TO SYSTEM 2, THE GAS AND PISTON:\nIn this case, we need to use the more general form of the first law which includes the change in potential energy of whatever is present with the boundaries of the system (in this case, the piston).\n$$dE=dU+d(PE)=dU+\\frac{mg}{A}dV=-\\frac{f}{A}dV\\tag{3}$$where ##\\frac{F}{A}dV## is the work done by system 2 on its surroundings. Note that, in this case, there is no heat transfer because the combined system is adiabatic. If we substitute Eqns. 1 into this relationship, we obtain:\n$$dU=\\frac{F}{A}dV-PdV\\tag{4}$$From Eqns. 2 and 4, it follows that the heat transferred from the piston to the gas dQ is given by:\n$$dQ=\\frac{F}{A}dV\\tag{5}$$\n\nFIRST LAW OF THERMODYNAMICS APPLIED TO THE PISTON ALONE:\n\nWe can obtain the equation for the first law applied to the piston alone by subtracting Eqn. 2 from Eqn. 3 to yield:\n$$\\frac{mg}{A}dV=-dQ-\\left(\\frac{f}{A}-P\\right)dV\\tag{6}$$\nThe left hand side is the change in potential energy of the piston. Again, dQ is the heat transferred from the piston to the gas. The work done by the piston on its surroundings is ##\\left(\\frac{f}{A}-P\\right)dV##. Note that the piston does not do any work on the cylinder, since the displacement of the cylinder is zero.\n\nFURTHER DISCUSSION\nFor an ideal gas, Eqn. 4 becomes:\n$$nC_vdT=\\frac{F}{A}dV-\\frac{nRT}{V}dV\\tag{7}$$This equation does not have a simple analytic solution that I am aware of, and it would probably have to be integrated numerically. In any event, from this equation, it follows from this equation that the change in entropy of the gas is obtained from:\n$$dS=\\frac{F}{A}\\frac{dV}{T}$$\n\nLast edited:\nThanks Chester for your analysis and yes, it did help to answer some of my questions. I do have a question regarding your equation 1:\n\n$$PdV=\\frac{mg}{A}dV+\\frac{F}{A}dV+\\frac{f}{A}dV$$\n\nShouldn’t the friction work be negative? In which case, shouldn’t\n\n$$PdV = \\frac{mg}{A}dV-\\frac{F}{A}dV+\\frac{f}{A}dV$$\n\nThen\n\n$$PdV_{without friction}>PdV_{with friction}$$\n\nWhich would give us\n\n$$PdV_{reversible}>PdV_{irreversible}$$\n\nLast edited:\nThanks Chester for your analysis and yes, it did help to answer some of my questions. I do have a question regarding your equation 1:\n\n$$PdV=\\frac{mg}{A}dV+\\frac{F}{A}dV+\\frac{f}{A}dV$$\n\nShouldn’t the friction work be negative? In which case, shouldn’t\n\n$$PdV = \\frac{mg}{A}dV-\\frac{F}{A}dV+\\frac{f}{A}dV$$\nThe force balance from the free body diagram on the piston makes pretty clear that the sign on the friction term is correct. And, if you would rather I had written Eqn. 4 with a negative sign on the friction term, that would be consistent with moving the three terms on the right hand side of Eqn. 4 to the left-hand side, to yield:\n$$PdV-\\frac{mg}{A}dV-\\frac{F}{A}dV-\\frac{f}{A}dV=0$$For the pressure term, the displacement is in the same direction as the force, and, for the other three terms, the displacement is in the opposite direction of the force (as you pointed out for the friction term).\n\nThere is more that I can discuss on this problem with regard to the friction work and friction heat, with specific focus on the interface region between the cylinder and the piston. This is very tricky because velocity is discontinuous at the interface and the rate of doing work involves velocity. If you want to hear more about this, I would be glad to pursue it.\n\nI agree that the force balance would seem to indicate the friction work should be positive. I’m sure you’re right about the sign of the friction work, but consider the following.\n\nWe know it is the nature of friction that work against friction is negative. And we already acknowledged that for system 1 friction work is equivalent to heat transfer to the system. Given friction work increases internal energy and that\n\n$$dU=-dW$$\n\nThen shouldn’t the friction work component of dW be negative?\n\nPerhaps we need to revisit the force balance equation on the piston, keeping in mind that the externally applied forces always exist but the friction force only exists when opposing motion.\n\nFor system 1, during the expansion process, the externally applied force (mg + f) is gradually reduced so that there is always a small net force on the piston in the same direction as the displacement. The system work against mg + f positive and the contribution to the change in internal energy is negative. But during this time the sliding friction force is constant in the opposite direction of the displacement. The friction work is negative and the contribution to the internal energy is positive.\n\nWhere am I going wrong?\n\nI agree that the force balance would seem to indicate the friction work should be positive. I’m sure you’re right about the sign of the friction work, but consider the following.\n\nWe know it is the nature of friction that work against friction is negative. And we already acknowledged that for system 1 friction work is equivalent to heat transfer to the system. Given friction work increases internal energy and that\n\n$$dU=-dW$$\n\nThen shouldn’t the friction work component of dW be negative?\n\nPerhaps we need to revisit the force balance equation on the piston, keeping in mind that the externally applied forces always exist but the friction force only exists when opposing motion.\n\n1. If you feel that the force balance obtained from the free body diagram is an issue, please show your free body diagram for comparison. You can UPLOAD it using the UPLOAD button. Also, regarding friction, for simplicity, in my problem statement, I was very careful to specify \"The frictional force F is always constant and present both initially and finally. This can be achieved if we say that the coefficient of static friction is equal to the coefficient of kinetic friction, and that, in the initial and final states, the piston is at the verge of slipping (This is an idealization which does not detract from what we are trying to achieve in our analysis).\"\n\n2. When talking about \"work,\" it is very important to specify what is doing work on what. Please specify this in your wording.\n\nThanks Chester. I will deliberate on this further.\n\nThere must be some way to demonstrate that, for system 1 and/or system 2, the work done without friction (reversible adiabatic process) will be greater than the work done with friction (irreversible adiabatic process).\n\nThis goes to the heart of what I would like to see demonstrated by our example.\n\nBe back with you later.\n\nThanks Chester. I will deliberate on this further.\n\nThere must be some way to demonstrate that, for system 1 and/or system 2, the work done without friction (reversible adiabatic process) will be greater than the work done with friction (irreversible adiabatic process).\n\nBefore we start dealing with that, let's first make sure that we reach consensus on the actual analysis. However, you are aware that, if you have an adiabatic irreversible process on a closed system, it is impossible to define an adiabatic reversible process through the same two end states, correct?\n\nI'm going to go back and add to my analysis, providing much more detail, to help us reach consensus. This will include an idealized model of the gap/interface between the cylinder and piston to help us better quantify what is happening there with regard to the friction.\n\nChet\n\nIDEALIZED MODEL OF FRICTIONAL INTERFACE/\"GAP\" BETWEEN PISTON AND CYLINDER\n\nI'm introducing this idealized model of the interface/\"gap\" between the piston and cylinder so that I can more easily describe the application of the first law of thermodynamics to the piston, including its interaction with the cylinder (via the interface/\"gap\") and its mechanical and thermal interaction with the gas.", null, "In the figure, the cylinder is exerting a downward force F at one side of the interface/gap, while the piston is exerting an upward force F at the other side of the interface/gap. As a result of the work being done at the interface/gap, heat Q is being transferred from the gap to the piston. On the cylinder side of the interface/gap, no heat is being transferred because the cylinder is assumed to be non-conductive.\n\nLet's take a look at the work. Since the cylinder is stationary, the work done by the cylinder on the interface and by the interface on the cylinder are zero.\n\nAt the piston side of the interface/gap, the piston is moving upward with a displacement dV/A, where dV is the change in volume of the gas and A is the area of the piston. So, the work done by the piston on the interface/gap is ##+\\frac{F}{A}dV##, and the work done by the interface/gap on the piston is ##-\\frac{F}{A}dV##; the latter is the work done by the interface/gap on its surroundings. If we apply the first law of thermodynamics to the interface/gap, we have:\n$$dU=0=-dQ+\\frac{F}{A}dV$$or equivalently $$dQ=\\frac{F}{A}dV\\tag{1}$$. The change in internal energy of the interface/gap is zero because, in the limit, the interface/gap has no mass. According to this equation, the heat generated due to the friction at the interface is transferred to the piston.\n\nIn summary, all this idealized model of the interface really shows us is what we already knew:\n\n1. If the gas is expanding so that the piston moves upward, the interface exerts a downward friction (reaction) force on the piston\n2. the heat generated by friction at the interface is transferred to the piston.\n\nLet's next turn attention to how this analysis of the frictional interface/gap plays out in terms of applying the first law of thermodynamics specifically to the piston.\n\nAPPLICATION OF FIRST LAW OF THERMODYNAMICS TO PISTON\nThe figure below contains the information necessary to apply the first law of thermodynamics to the piston.", null, "First let's consider the work.\n\nFor the \"external\" force f, dV is in the opposite direction of f. So, work done by the surroundings on the piston = ##-\\frac{f}{A}dV## and work done by the piston on the surroundings = ##+\\frac{f}{A}dV##.\n\nFor the gas force PA, dV is in the same direction of PA. So, work done by surroundings (the gas) on piston = ##PdV## and work done by the piston on the surroundings (the gas) = ##-PdV##.\n\nFor the frictional force F from the interface/gap, dV is in the opposite direction of F. So, frictional work done by the surroundings on the piston = ##-\\frac{F}{A}dV## and frictional work done by the piston on the surroundings = ##+\\frac{F}{A}dV##\n\nIn terms of heat transfer, the piston receives dQ from the frictional interface/gap, and delivers dQ to the gas below.\n\nBased on all of this, the application of the first law of thermodynamics to the piston yields the following:\n$$dE=dU+\\frac{mg}{A}dV=\\frac{mg}{A}dV=dQ-dQ-\\frac{f}{A}dV+PdV-\\frac{F}{A}dV$$or, equivalently:\n$$\\frac{mg}{A}dV=-\\frac{f}{A}dV+PdV-\\frac{F}{A}dV$$where the internal energy change of the piston is assumed to be negligible. This is just the same as Eqn. 1 of post #8. If we combine this with Eqn. 1 of the present post, we obtain:\n$$\\frac{mg}{A}dV=-dQ+PdV-\\frac{f}{A}dV$$This is the same as Eqn. 6 of post #8.\n\n#### Attachments\n\nLast edited:\n\n$$\\frac{mg}{A}dV+\\frac{f}{A}dV=PdV-\\frac{F}{A}dV$$\n\nThen is it not correct to say:\n\n$$dW_{surroundings}=\\frac{mg}{A}dV+\\frac{f}{A}dV$$\n\n$$dW_{gas}=PdV$$\n\n$$dW_{friction}=-\\frac{F}{A}dV$$\n\n$$dW_{surroundings}=dW_{gas}-dW_{friction}$$\n\nFrom which we can conclude the work done on the surroundings is greater without friction than with friction?\nWhat are you specifically referring to when you write these equations for work, (a) the combination of piston, cylinder, and gas or (b) the combination of piston and gas, (c) the piston alone, or (d) the gas alone?\n\nThe work done by the combination of piston, gas, and cylinder on its surroundings is just\n$$dW=\\frac{f}{A}dV$$\nThis does not include the change in potential energy of the piston which is included in ##dE_{piston}=\\frac{mg}{A}dV##\n\nThe work done by the gas on its surroundings (the piston) is $$dW=PdV$$\n\nThe work done by the piston on its surroundings is $$dW=\\frac{f}{A}dV+\\frac{F}{A}dV-PdV$$Here again, this does not include the change in potential energy of the piston which is included in ##dE_{piston}=\\frac{mg}{A}dV##\n\nLast edited:\nWhen trying to make a sign correction in my post, I inadvertently deleted it. Sorry about that.\n\nIn any event, to answer your question, the work I am interested is work done by the combination of the piston, cylinder, and gas (as the system), since I want friction to be included within the system. Under these conditions (and I will ignore the change in potential energy in all of the following as you did) the work done on the surroundings is, as you indicated\n\n$$dW_{surroundings}=\\frac{f}{A}dV$$\n\nWhich I believe should equal the sum of work done by the gas and the friction work, or\n\n$$\\frac{f}{A}dV=PdV + \\frac{F}{A}dV$$\n\nSince the friction force is in the opposite direction of dV, F in this equation will be negative. Which means the friction work will be negative.\n\nBased on the above, the work done by the system on the surroundings will be a maximum when the friction work is or approaches zero (the process is reversible). This would then be consistent with the principle\n\n$$W_{reversible}>W_{irreversible}$$\n\nIncidentally, I came across an analysis titled “Irreversible Work and Internal Friction” on the website chem.libretexts.org. The system they analyzed is shown in the diagram below. The friction is between the piston rod R and the bushing B and is included as part of the system along with the gas. They concluded\n\n$$w=-\\int_{V1}^{V2}pdV-\\int_{V1}^{V2}\\frac{F}{A}dV$$\n\nWhere w on the left is the work done on the surroundings, the first term on the right is the work of expanding or compressing the gas and the second term is the frictional work where the friction force will be negative and thus the friction work will be positive. (Note that the negative signs on the work terms is due to their use the chemists version of the first law, dU = dQ + dW.).\n\nThey then state:\n\n“As a result, the irreversible work of expansion is less negative than the reversible work for the same volume increase, and the irreversible work of compression is more positive than the reversible work for the same volume decrease. These effects of piston velocity on the work are consistent with the minimal work principle.”\n\nThe different signs not withstanding, I believe this is consistent with my above conclusion.\n\nThey also make the following very interesting statement:\n\nConsider the situation when the piston moves very slowly in one direction or the other. In the limit of infinite slowness the friction force and friction work vanish, and the process is reversible with expansion work given by\n\n$$-\\int pdV$$\n\nIt seems to me this is tantamount to saying a quasi-static process with friction is reversible, or, alternatively, there is no friction force or friction work if the process is quasi-static. This is contrary to the premise that a quasi-static process with friction is irreversible.\n\nWhen trying to make a sign correction in my post, I inadvertently deleted it. Sorry about that.\n\nIn any event, to answer your question, the work I am interested is work done by the combination of the piston, cylinder, and gas (as the system), since I want friction to be included within the system. Under these conditions (and I will ignore the change in potential energy in all of the following as you did) the work done on the surroundings is, as you indicated\n\n$$dW_{surroundings}=\\frac{f}{A}dV$$\n\nWhich I believe should equal the sum of work done by the gas and the friction work, or\n\n$$\\frac{f}{A}dV=PdV + \\frac{F}{A}dV$$\n\nSince the friction force is in the opposite direction of dV, F in this equation will be negative. Which means the friction work will be negative.\n\nIt is very unconventional to treat the frictional force in this way. Since frictional force is a vector quantity, it is typically treated as a positive magnitude times an appropriately oriented unit vector (in this case, a unit vector in the negative z direction). It really goes against my comfort to say that the friction force is negative. The net result of all this is that your parameter F is the negative of my parameter F. Any chance you might consider going back and editing your posts so that our F's are the same?\nBased on the above, the work done by the system on the surroundings will be a maximum when the friction work is or approaches zero (the process is reversible). This would then be consistent with the principle\n\n$$W_{reversible}>W_{irreversible}$$\nI really don't like this interpretation. Even for the same volume change, the temperature and pressure histories are going to be different, so the reversible work the gas does with friction is going to be different from the reversible work it does without friction. It doesn't make sense to me to compare reversible and irreversible work in this way. Usually, one would compare them for processes between the same to end points for the same identical system. I' m thinking of going back and integrating the following equation numerically (after reducing it to dimensionless form) to enable us to make more rational comparisons between cases with and without friction:\n$$nC_vdT=\\frac{F}{A}dV-\\frac{nRT}{V}dV$$\nMeanwhile, based on the equations we are discussing here , the only interpretation I'm willing to make is that the work that gas has to do to overcome the frictional force and the external force is greater than the work the combined system has to do to overcome the external force alone.\n\nIncidentally, I came across an analysis titled “Irreversible Work and Internal Friction” on the website chem.libretexts.org. The system they analyzed is shown in the diagram below. The friction is between the piston rod R and the bushing B and is included as part of the system along with the gas. They concluded\n\n$$w=-\\int_{V1}^{V2}pdV-\\int_{V1}^{V2}\\frac{F}{A}dV$$\n\nWhere w on the left is the work done on the surroundings, the first term on the right is the work of expanding or compressing the gas and the second term is the frictional work where the friction force will be negative and thus the friction work will be positive. (Note that the negative signs on the work terms is due to their use the chemists version of the first law, dU = dQ + dW.).\n\nThey then state:\n\n“As a result, the irreversible work of expansion is less negative than the reversible work for the same volume increase, and the irreversible work of compression is more positive than the reversible work for the same volume decrease. These effects of piston velocity on the work are consistent with the minimal work principle.”\n\nThe different signs not withstanding, I believe this is consistent with my above conclusion.\n\nThey also make the following very interesting statement:\n\nConsider the situation when the piston moves very slowly in one direction or the other. In the limit of infinite slowness the friction force and friction work vanish, and the process is reversible with expansion work given by\n\n$$-\\int pdV$$\n\nIt seems to me this is tantamount to saying a quasi-static process with friction is reversible, or, alternatively, there is no friction force or friction work if the process is quasi-static. This is contrary to the premise that a quasi-static process with friction is irreversible.\nBob, I looked over what you have written here, but was unable to follow, and didn't understand the comment that, when the process is quasi-static, the process is reversible. Maybe you can provide the exact statement of the problem.\n\nLast edited:\nI've started to do calculations with the model I discussed in my previous post. The dimensionless parameters are as follows:\n$$\\bar{V}=\\frac{V}{V_0}$$\n$$\\bar{T}=\\frac{T}{T_0}$$\n$$\\bar{F}=\\frac{F}{AP_0}$$\n$$\\bar{W_f}=\\frac{\\int_{V_0}^V{\\frac{f}{A}dV}}{nC_vT_0}$$\n$$\\bar{W_P}=\\frac{\\int_{V_0}^V{PdV}}{nC_vT_0}$$where the subscript 0 refers to the initial state of the gas. The calculations are being performed for the case of ##\\bar{F}=0.5##, meaning that the frictional force and the external force initially contribute equally to supporting the initial pressure ##P_0##, or equivalently, the frictional force is always equal to half the initial pressure force. The calculations are also performed for ##\\gamma=\\frac{C_p}{C_v}=1.4##. So far, I've calculated the dimensionless temperature as a function of the dimensionless volume. This is shown in the figure below:", null, "Note the significant difference between the cases with and without friction. Note also that, with friction, the temperature first decreases with increasing volume, but then passes through a minimum and then starts increasing. The minimum corresponds to the point where the external force f has dropped to zero, and friction is supporting the entire pressure of the gas. Further increases in volume correspond to actually applying tension (rather than compression) to the upper surface of the piston (i.e., f < 0). In this situation, the gas pressure has dropped to the point where it is insufficient alone to overcome the friction.\n\nThe figure below shows the calculated work for (a) the gas acting on the piston (green line), (b) the external work done by the combined system (blue line), and (c) the gas and the external work for the case of no friction (where both curves coincide).", null, "The difference between the green curve and the blue curve is the work done to overcome friction. Note that the system does much less work on the surroundings than the gas does on the piston. Note also that the work done by the combined system increases for small volume increases, passes through a maximum, and then begins to decrease with further volume increases. The maximum work corresponds to the point where one needs to begin pulling on the piston from the outside to overcome friction; the gas no longer has enough pressure to do this on its own. The reversible case with no friction is only provided for comparison, and is not really directly related to the frictional case.\n\nChet\n\nLast edited:\n•", null, "dRic2\nIncidentally, I came across an analysis titled “Irreversible Work and Internal Friction” on the website chem.libretexts.org. The system they analyzed is shown in the diagram below. The friction is between the piston rod R and the bushing B and is included as part of the system along with the gas. They concluded\n\n$$w=-\\int_{V1}^{V2}pdV-\\int_{V1}^{V2}\\frac{F}{A}dV$$\n\nWhere w on the left is the work done on the surroundings, the first term on the right is the work of expanding or compressing the gas and the second term is the frictional work where the friction force will be negative and thus the friction work will be positive. (Note that the negative signs on the work terms is due to their use the chemists version of the first law, dU = dQ + dW.).\n\nThey then state:\n\n“As a result, the irreversible work of expansion is less negative than the reversible work for the same volume increase, and the irreversible work of compression is more positive than the reversible work for the same volume decrease. These effects of piston velocity on the work are consistent with the minimal work principle.”\n\nThe different signs not withstanding, I believe this is consistent with my above conclusion.\n\nThey also make the following very interesting statement:\n\nConsider the situation when the piston moves very slowly in one direction or the other. In the limit of infinite slowness the friction force and friction work vanish, and the process is reversible with expansion work given by\n\n$$-\\int pdV$$\n\nIt seems to me this is tantamount to saying a quasi-static process with friction is reversible, or, alternatively, there is no friction force or friction work if the process is quasi-static. This is contrary to the premise that a quasi-static process with friction is irreversible.\nI'm in disagreement with almost all aspects of this analysis. Let's take a look at what the force balance on the piston looks like when the gas is expanding and when it is being compressed. If ##\\mathbf{i_x}## represents a unit vector in the positive x direction, then for expansion, the friction force on the piston shaft is ##F(-\\mathbf{i_x})##, and, if the gas is being compressed, the friction force on the piston shaft ##F(+\\mathbf{i_x})##, where, in each case, F is the (positive) magnitude of the friction force. So, for expansion, the vector force balance on the piston is $$P_{ext}A(-\\mathbf{i_x})+F(-\\mathbf{i_x})+pA(+\\mathbf{i_x})=\\mathbf{0}$$\nOn the other hand, for compression, the vector force balance on the piston is $$P_{ext}A(-\\mathbf{i_x})+F(+\\mathbf{i_x})+pA(+\\mathbf{i_x})=\\mathbf{0}$$Note that the force balance equation, and thus the equations for the work are different, depending on whether there is expansion or compression. The component of each of these equations in the x-direction is $$P_{ext}A=pA-F\\tag{expansion}$$$$P_{ext}A=pA+F\\tag{compression}$$In both these equations, the magnitude F of the friction force is positive. If follows from these equations that the work done by the system on the surroundings is $$W=\\int_{V_1}^{V_2}{P_{ext}dV}=+\\int_{V_1}^{V_2}{\\left(p-\\frac{F}{A}\\right)dV}\\tag{expansion}$$and $$W=\\int_{V_1}^{V_2}{P_{ext}dV}=+\\int_{V_1}^{V_2}{\\left(p+\\frac{F}{A}\\right)dV}\\tag{compression}$$Based on these equations, in each case, $$\\Delta U=-W\\tag{expansion and compression}$$\n\nI assert that all these equations that I have written have the correct signs.\nThey then state:\n\n“As a result, the irreversible work of expansion is less negative than the reversible work for the same volume increase, and the irreversible work of compression is more positive than the reversible work for the same volume decrease. These effects of piston velocity on the work are consistent with the minimal work principle.”\n\nThe different signs not withstanding, I believe this is consistent with my above conclusion.\n\nThey also make the following very interesting statement:\n\nConsider the situation when the piston moves very slowly in one direction or the other. In the limit of infinite slowness the friction force and friction work vanish, and the process is reversible with expansion work given by\n\n$$-\\int pdV$$\n\nIt seems to me this is tantamount to saying a quasi-static process with friction is reversible, or, alternatively, there is no friction force or friction work if the process is quasi-static. This is contrary to the premise that a quasi-static process with friction is irreversible.\nNone of this makes any sense to me. It seems to me that, in the first part, they are comparing apples and oranges. In the second part, clearly, no matter how slowly the piston is being moved, the friction term is present and the process is irreversible. Maybe, in the problem they are solving, they are dealing with viscous fluid between the bearing and shaft, so that the frictional force varies with the velocity of shaft advance.\n\nI might also point out that there is another fundamental difference between our problem and this one. In our problem, the friction force and gas pressure force are in series, while in this problem, they are in parallel.\n\nLast edited:\nSecond Thoughts. Based on the results I presented in post #20, I think I can provide and apples-apples comparison/interpretation that will satisfy the intuition of my friend @Robert Davidson.\n\nFor the same change in volume, the work done by the gas in the overall adiabatic irreversible expansion involving piston friction will be greater than the work done by the gas in the adiabatic reversible expansion not involving piston friction; this is because of the higher temperatures of the gas in the frictional expansion, and the correspondingly higher pressures. However, the work done by the combined system on the external surroundings will be less with piston friction than without piston friction.\n\nChet,\n\nBob\n\nHi Chet,\n\nThanks for proving by mathematical analysis what I was only able to express qualitatively. After first pass, I must admit I didn’t follow the post 20 analysis completely (I will study further). Clearly, you are at a higher level than I.\n\nRegarding the following conclusion of your last post:\n\nFor the same change in volumethe work done by the combined system on the external surroundings will be less with piston friction than without piston friction.\n\nAm I correct that this conclusion is based on the comparison of the red and blue curves of dimensionless work from post 20? I only ask because the red curve says “gas & combined system” whereas the word “gas” is missing in the caption for the blue curve. I am assuming, however, that both curves are for the combined system (our system 2) which includes the gas.\n\nRegarding the following conclusion:\n\nFor the same change in volume, the work done by the gas in the overall adiabatic irreversible expansion involving piston friction will be greater than the work done by the gas in the adiabatic reversible expansion not involving piston friction; this is because of the higher temperatures of the gas in the frictional expansion, and the correspondingly higher pressures.\n\nCan I interpret this as well to mean that only part of the work done by the gas is, for want of a better term, “productive”, whereas the other part (against friction) is returned to the gas, the end result being a smaller decrease in internal energy (higher final temperature and pressure)? Or, to put it another way, only part of the work done by the gas is done on the surroundings of the combination system.\n\nIn post 14 you asked me the following question:\n\nHowever, you are aware that, if you have an adiabatic irreversible process on a closed system, it is impossible to define an adiabatic reversible process through the same two end states, correct?\n\nThe answer is yes, I was (and am) aware of that. In fact, that was the reason for my original example (that led us to the forum) to compare two constant pressure adiabatic expansions, one with and one without piston/cylinder friction, in which the question is which will result in a greater increase in height of the weighted piston (increase in volume of gas). The answer to that should clearly demonstrate whether more work is done on the weighted piston with or without friction, without the need to have the same initial and final end points (even taking into account that the piston with friction will get \"stuck\" when the net force on the piston equals the maximum static friction). Do you think it would be work while to pose this question in a new post? Or have we, as they say, beat this to death.\n\nAgain, thanks for your help. I feel I learned a lot.\n\nBob\n\nHi Chet,\n\nThanks for proving by mathematical analysis what I was only able to express qualitatively. After first pass, I must admit I didn’t follow the post 20 analysis completely (I will study further). Clearly, you are at a higher level than I.\nI didn't include all the analysis that led up to the results in post # 20. If you like, I can provide that. The graphs include only the final results of the analysis.\nRegarding the following conclusion of your last post:\n\nFor the same change in volumethe work done by the combined system on the external surroundings will be less with piston friction than without piston friction.\n\nAm I correct that this conclusion is based on the comparison of the red and blue curves of dimensionless work from post 20? I only ask because the red curve says “gas & combined system” whereas the word “gas” is missing in the caption for the blue curve. I am assuming, however, that both curves are for the combined system (our system 2) which includes the gas.\nCorrect.\nRegarding the following conclusion:\n\nFor the same change in volume, the work done by the gas in the overall adiabatic irreversible expansion involving piston friction will be greater than the work done by the gas in the adiabatic reversible expansion not involving piston friction; this is because of the higher temperatures of the gas in the frictional expansion, and the correspondingly higher pressures.\n\nCan I interpret this as well to mean that only part of the work done by the gas is, for want of a better term, “productive”, whereas the other part (against friction) is returned to the gas, the end result being a smaller decrease in internal energy (higher final temperature and pressure)? Or, to put it another way, only part of the work done by the gas is done on the surroundings of the combination system.\nYes. Exactly.\nIn post 14 you asked me the following question:\n\nHowever, you are aware that, if you have an adiabatic irreversible process on a closed system, it is impossible to define an adiabatic reversible process through the same two end states, correct?\n\nThe answer is yes, I was (and am) aware of that. In fact, that was the reason for my original example (that led us to the forum) to compare two constant pressure adiabatic expansions, one with and one without piston/cylinder friction, in which the question is which will result in a greater increase in height of the weighted piston (increase in volume of gas). The answer to that should clearly demonstrate whether more work is done on the weighted piston with or without friction, without the need to have the same initial and final end points (even taking into account that the piston with friction will get \"stuck\" when the net force on the piston equals the maximum static friction). Do you think it would be work while to pose this question in a new post? Or have we, as they say, beat this to death.\n\nAgain, thanks for your help. I feel I learned a lot.\n\nBob\nFor the process to be quasi-static, we cannot let the piston rise on its own. So it would have to involve gradual removal of weights from the top of the piston. This would entail problems with specifying the initial state, because, in one case, friction would be helping to balance the gas pressure initially, while, in the other case, it would not be helping. So, in the non-frictional case, we would have to start with a heavier piston (or more weights). If you want to take a shot at specifying this problem, we can proceed in the present thread. Here, instead of matching the final volumes, we would be doing something like matching the final amounts of weight removed (I guess).\n\nI'm thinking of the following comparison:\n\nSystem 1: massless piston with friction force F, and a pile of small masses totaling M sitting on top of the piston initially\n\nSystem 2: frictionless piston having mass m, such that mg for this system is equal to F for system 1, and the same pile of small masses totaling M sitting on top of the piston initially\n\nThe initial states of these two systems will be the same, but System 2 will experience an adiabatic reversible expansion and System 1 will experience an adiabatic irreversible expansion when the same pile of small masses is removed quasi-statically from the top of each piston.\n\nI didn't include all the analysis that led up to the results in post # 20. If you like, I can provide that. The graphs include only the final results of the analysis.\n\nYes, I would very much appreciate it if you could provide all the analysis.\n\nFor the process to be quasi-static, we cannot let the piston rise on its own…..\n\nI was not thinking of a quasi-static process. What I had in mind was to compare the final volume for two irreversible constant pressure adiabatic expansions, one with sliding friction and one without.\n\nI didn't include all the analysis that led up to the results in post # 20. If you like, I can provide that. The graphs include only the final results of the analysis.\n\nYes, I would very much appreciate it if you could provide all the analysis.\nI'll post this in a little while.\n\nFor the process to be quasi-static, we cannot let the piston rise on its own…..\n\nI was not thinking of a quasi-static process. What I had in mind was to compare the final volume for two irreversible constant pressure adiabatic expansions, one with sliding friction and one without.\nSo you would consider the same comparison as in my previous post, except with sudden removal of mass M at time zero?\n\nThe starting equations for the frictional analysis I alluded to in post #20 is:\n$$dU=nC_vdT=\\frac{F}{A}dV-\\frac{nRT}{V}dV\\tag{1}$$and $$dU=nC_vdT=-\\frac{f}{A}dV\\tag{2}$$Dividing Eqn. 1 by ##nC_vT## yields:\n$$\\frac{dT}{T}=\\frac{FdV}{AnC_vT}-\\frac{R}{C_v}\\frac{dV}{V}=\\left[\\frac{FV}{AnC_vT}-\\frac{R}{C_v}\\right]\\frac{dV}{V}\\tag{3}$$\nIn Eqn. 3, $$\\frac{FV}{AnC_vT}=\\frac{FV_0}{nC_vAT_0}\\frac{(V/V_0)}{(T/T_0)}=\\frac{FR}{AC_v}\\frac{V_0}{nRT_0}\\frac{(V/V_0)}{(T/T_0)}$$\nBut, from the ideal gas law, $$\\frac{nRT_0}{V_0}=P_0$$\nTherefore, $$\\frac{FV}{AnC_vT}=\\frac{F}{P_0A}\\frac{C_v}{R}\\frac{(V/V_0)}{(T/T_0)}\\tag{4}$$\nSubstituting Eqn. 4 into Eqn. 3 then yields:\n$$\\frac{dT}{T}=\\frac{C_v}{R}\\left[\\frac{F}{P_0A}\\frac{(V/V_0)}{(T/T_0)}-1\\right]\\frac{dV}{V}=(\\gamma -1)\\left[\\frac{F}{P_0A}\\frac{(V/V_0)}{(T/T_0)}-1\\right]\\frac{dV}{V}\\tag{5}$$\nWe now make the following dimensionless substitutions:\n$$\\bar{T}=T/T_0$$\n$$\\bar{V}=V/V_0$$\nThis then yields:\n$$\\frac{d\\ln{\\bar{T}}}{d\\ln{\\bar{V}}}=-(\\gamma -1)\\left[1-\\frac{F}{P_0A}e^{(ln{\\bar{V}}-\\ln{\\bar{T}})}\\right]\\tag{6}$$\nThis is the differential equation I integrated to get the results in post #20.\nTo get the work terms, I did the following: From Eqn. 2, if I divide by ##nC_vT_0## and integrate, I obtain:\n$$\\frac{\\left[\\int_{V_0}^V{\\frac{f}{A}dV}\\right]}{nC_vT_0}=1-\\bar{T}$$\nSimilarly, for the integral of the gas pressure, I get:\n$$\\frac{\\left[\\int_{V_0}^V{PdV}\\right]}{nC_vT_0}=(\\gamma-1)\\frac{F}{P_0A}(\\bar{V}-1)+(1-\\bar{T})\\tag{7}$$\n\nChet,\n\nThanks for the analysis.\n\nRegarding the new example, I had in mind the following:\n\nSystem 1: massless piston with friction between the piston and cylinder walls, and a pile of small masses sitting on top of the piston, such that the total downward force due to the masses plus the downward force due to atmospheric pressure equals the upward force due to the gas pressure. Or, the pressure upward exerted by the gas equals the pressure downward exerted by the weights plus atmospheric pressure.\n\nSystem 2: Same as system 1 except there is no friction.\n\nAn equal amount of weight is abruptly removed from each system so that the external downward pressure exerted by the weights plus the atmosphere is ½ the original external downward pressure.\n\nTo solve: What will be the final volume of the two systems?\n\nIf we can agree on the problem statement, I will give it a try on my own, with the benefit of the analysis you did on our previous example, and then post it.\n\nBob\n\nLast edited:\nChet,\n\nThanks for the analysis.\n\nRegarding the new example, I had in mind the following:\n\nSystem 1: massless piston with friction between the piston and cylinder walls, and a pile of small masses sitting on top of the piston, such that the total downward force due to the masses plus the downward force due to atmospheric pressure equals the upward force due to the gas pressure. Or, the pressure upward exerted by the gas equals the pressure downward exerted by the weights.\n\nSystem 2: Same as system 1 except there is no friction.\n\nAn equal amount of weight is abruptly removed from each system so that the external downward pressure exerted by the weights plus the atmosphere is ½ the original external downward pressure.\n\nTo solve: What will be the final volume of the two systems?\n\nIf we can agree on the problem statement, I will give it a try on my own, with the benefit of the analysis you did on our previous example, and then post it.\n\nBob\nBob,\n\nAlthough I don't think that the two cases are really going to be comparable, I think each of them is interesting on its own. So please proceed and let's see what you come up with. (Please note that, in both these cases, the gas experiences a non-quasistatic deformation, and entropy is generated within the gas in each case).\n\nChet\n\nI've been able to analytically solve the differential equation (Eqn. 6) of post #29 for the dimensionless temperature of the gas as a function of the dimensionless volume ratio. The result, which agrees with the numerical solution I presented in post #20 is:\n$$\\bar{T}=\\frac{(1-\\xi)}{\\bar{V}^{(\\gamma-1)}}+\\xi \\bar{V}$$where $$\\xi=\\frac{(\\gamma-1)}{\\gamma}\\frac{F}{P_0A}$$\n\nHi Chet,\n\nHaven’t forgot this. So far only tackled the easy case (system 2). Here’s what I have so far.\n\nGoing to assume dealing with ideal gas (air) with the following initial conditions and properties:\n\n##P_{i}=10atm##, ##T_{i}=300K##, ##n=1##, ##C_{v}=0.2053\\frac{l.atm}{mol.K}##, ##R_{u}=0.08205\\frac{l.atm}{mol.K}##, ##k=1.4##\n\nApplying the ideal gas equation to get the initial volume:\n\n$$V_{i}=\\frac{nRT_{i}}{P_{i}}=\\frac{(1)(0.08205)(300)}{10}=2.46 l$$\n\nWeight is abruptly removed to reduce the external pressure by one half, or to 5 atm, and the gas allowed to expand non-quasi-statically at constant pressure until equilibrium is reached.\n\nSince the final pressure is known, we can (1) determine the relationship between the final temperature and volume by applying the general gas equation to the initial and final states and (2) substitute the relationship into the first law equation for a constant pressure adiabatic process.\n\nApplying the general gas equation:\n\n$$\\frac{P_{i}V_{i}}{T_{i}}= \\frac{P_{f}V_{f}}{T_{f}}$$\n\n$$T_{f}=\\frac{P_{f}V_{f}T_{i}}{P_{i}V_{i}}$$\n\n$$T_{f}=\\frac{(5)(V_{f})(300)}{(10)(2.46)}=61V_{f}$$\n\nApplying the first law for an adiabatic process:\n\n$$\\Delta U=-W$$\n\n$$nC_{v}(T_{f}-T_{i})=-P_{f}(V_{f}-V_{i})$$\n\nSubstituting ##T_{f}=61V_{f}## and the other known values\n\n$$(1)(0.2053)[61V_{f}-300]=-5(V_{f}-2.46)$$\n\nWhich gives us ##V_{f}=4.22l## and ##T_{f}=257K##, and the work done is\n\n$$W=5(4.22-2.46)l.atm=892j$$\n\nComparing to the final volume and work done for a reversible adiabatic expansion with the same initial conditions and same final pressures:\n\n$$P_{i}V_{i}^{k}= P_{f}V_{f}^{k}$$\n\n$$V_{f}=6l$$\n\n$$W_{rev}=\\frac{(P_{f}V_{f}-P_{i}V_{i})}{1-k}$$\n\n$$W_{rev}= 13.5 l.atm=1368j$$\n\nWhich, as expected, is greater than the irreversible work.\n\nThe next step is to tackle system 1, which adds piston friction. I would like to bring system 2 to the same final pressure and then compare the work on the surroundings to system 2. I recall that in your analysis of the quasi-static expansion with friction it was necessary to apply an external tensile force to overcome static friction in order to reach the same volume as the non-friction system. It appears that will again be the case here, except it would be in order to reach the same final pressure.\n\nI was thinking about a possible alternative approach, such as assuming the surface of the cylinder at some point changes to a smooth service prior to reaching the maximum static friction force so that the expansion could be completed, albeit without friction work done at the end. But that would probably create more complications than it's worth.\n\nI approached this problem differently but, of course, arrived at the same results. My focus was on the final temperature, rather than the final volume.\n$$nC_v(T_f-T_i)=-P_f(V_f-V_i)=P_f\\left(\\frac{nRT_f}{P_f}-\\frac{nRT_i}{P_i}\\right)$$\nSolving for ##T_f## then yields:\n$$T_f=\\left[\\frac{1}{\\gamma}+\\left(1-\\frac{1}{\\gamma}\\right)\\frac{P_f}{P_i}\\right]T_i$$For ##\\gamma=1.4## and ##P_f/P_i=0.5##, this yields ##T_f=0.8571T_i##. And, for ##T_i=300\\ K##, ##T_f=257.1K##.\n\nThe work is given by: $$W=-\\Delta U=-nC_v(T_f-T_i)=-(1)(2.5)(8.314)(257.1-300)=892\\ J$$\nIt'll be interesting to compare the approach and results you get for system 2 with those that I obtained.\n\nHere's an interesting paradox for you. As ##P_f/P_i\\rightarrow 0##, $$\\frac{T_f}{T_i}\\rightarrow\\frac{1}{\\gamma}$$and then $$W\\rightarrow nC_vT_i\\left(1-\\frac{1}{\\gamma}\\right)>0$$But how can this be if ##P_f/P_i\\rightarrow 0## implies free expansion.\n\nLast edited:" ]
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http://mathcs.chapman.edu/~jipsen/structures/doku.php/cancellative_partial_monoids?rev=1533432251
[ "## Cancellative partial monoids\n\nAbbreviation: CanPMon\n\n### Definition\n\nA cancellative partial monoid is a partial monoid such that\n\n$\\cdot$ is left-cancellative: $x\\cdot y=x\\cdot z\\ne *$ implies $y=z$ and\n\n$\\cdot$ is right-cancellative: $x\\cdot z=y\\cdot z\\ne *$ implies $x=y$.\n\n##### Morphisms\n\nLet $\\mathbf{A}$ and $\\mathbf{B}$ be cancellative partial monoids. A morphism from $\\mathbf{A}$ to $\\mathbf{B}$ is a function $h:A\\rightarrow B$ that is a homomorphism: $h(e)=e$ and if $x\\cdot y\\ne *$ then $h(x \\cdot y)=h(x) \\cdot h(y)$.\n\nExample 1:\n\n### Properties\n\nClasstype first-order\n\n### Finite members\n\n$\\begin{array}{lr} f(1)= &1\\\\ f(2)= &2\\\\ f(3)= &3\\\\ f(4)= &9\\\\ f(5)= &21\\\\ f(6)= &125\\\\ f(7)= &\\\\ f(8)= &\\\\ f(9)= &\\\\ f(10)= &\\\\ \\end{array}$\n\n### Superclasses\n\n##### Toolbox", null, "" ]
[ null, "http://mathcs.chapman.edu/~jipsen/structures/lib/exe/indexer.php", null ]
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https://ipx.name/google-public-dns/
[ "`Pinging 8.8.8.8 with 32 bytes of data:`\n``` Reply from 8.8.8.8: bytes=32 time=91ms TTL=242 Reply from 8.8.8.8: bytes=32 time=90ms TTL=242 Reply from 8.8.8.8: bytes=32 time=90ms TTL=242 Reply from 8.8.8.8: bytes=32 time=89ms TTL=242 Ping statistics for 8.8.8.8: Packets: Sent = 4, Received = 4, Lost = 0 (0% loss), Approximate round trip times in milli-seconds: Minimum = 89ms, Maximum = 91ms, Average = 90ms Pinging 8.8.4.4 with 32 bytes of data: Reply from 8.8.4.4: bytes=32 time=89ms TTL=242 Reply from 8.8.4.4: bytes=32 time=90ms TTL=242 Reply from 8.8.4.4: bytes=32 time=91ms TTL=242 Reply from 8.8.4.4: bytes=32 time=91ms TTL=242 ```\n```Ping statistics for 8.8.4.4: Packets: Sent = 4, Received = 4, Lost = 0 (0% loss), Approximate round trip times in milli-seconds: Minimum = 89ms, Maximum = 91ms, Average = 90ms```" ]
[ null ]
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https://www.seslidj.com/illinois-woodland-xwro/b909d5-simulate-covariance-matrix
[ "World First Mobile Phone, Sharp Bend Meaning, Finger Knitting Hat, Washington Dc Commercial Property Taxes, Top Movies 1964, Where Can I Buy Thorntons Toffee, Influence Brand Jewelry, All-american Rejects 2020 Album, Christmas Peace On Earth, The Term Opportunity Cost Suggests That:, Contraceptive Pill 1960s, Healing Cap Implant, Tourmaline Birthstone Necklace, \" /> World First Mobile Phone, Sharp Bend Meaning, Finger Knitting Hat, Washington Dc Commercial Property Taxes, Top Movies 1964, Where Can I Buy Thorntons Toffee, Influence Brand Jewelry, All-american Rejects 2020 Album, Christmas Peace On Earth, The Term Opportunity Cost Suggests That:, Contraceptive Pill 1960s, Healing Cap Implant, Tourmaline Birthstone Necklace, \" />\niletişim:\n\n## simulate covariance matrix\n\nThis figure shows how simulate reduces the sample by using the values of NumDraws, Thin, and BurnIn. That means that the table has the same headings across the top as it does along the side. Simulated innovations covariance matrices, returned as a PriorMdl.NumSeries-by-PriorMdl.NumSeries-by-NumDraws array of positive definite numeric matrices. It can be seen that each element in the covariance matrix is represented by the covariance between each (i,j) dimensio… This can be a useful way to understand how different variables are related in a dataset. Covariance Matrix Formula Covariance Matrix is a measure of how much two random variables gets change together. Consider the 3-D VAR(4) model of Draw Coefficients and Innovations Covariance Matrix from Prior Distribution. [Coeff,Sigma] Σ xi2 / N is the variance of elements from the ith data set. the number of features like height, width, weight, …). Each column is an individual draw, and each row is an individual coefficient. As an example, let’s simulate 100 observations with 4 variables. cj is the model constant in the equation of response variable j. Bju is the regression coefficient of exogenous variable u in the equation of response variable j. Create covariance matrix using ratio and rotation degree. For example, you can set the number of random draws from the distribution or specify the presample response data. For more details on how simulate reduces the full sample, see Algorithms. As … In this tutorial we will learn how to create covariance matrix in Excel or covariance table in Excel. zt=[yt−1′yt−2′⋯yt−p′1txt′], which is a 1-by-(mp + r + 2) vector, and Zt is the m-by-m(mp + r + 2) block diagonal matrix. Compute the inflation rate, stabilize the unemployment and federal funds rates, and remove missing values. numseries is the number of response variables (PriorMdl.NumSeries). For all t, εt is a series of independent 3-D normal innovations with a mean of 0 and covariance Σ. To build a correlation matrix, you need to rescale the covariance matrix … Because the joint posterior distribution of a semiconjugate prior model is analytically intractable, simulate sequentially draws from the full conditional distributions. A Covariance Matrix, like many matrices used in statistics, is symmetric. A modified version of this example exists on your system. Specify the response variable names. You can also use a MATRIX OUT subcommand with MCONVERT to save the covariance matrix to another file. In the top left cell F16 we calculate the covariance between Microsoft and itself using =COVARIANCE.S(MSFT,MSFT) using those named ranges. Sigma is a 3-by-3-by-1000 array of randomly drawn innovations covariance matrices. Name must appear inside quotes. If you supply more rows than necessary, simulate uses the latest PriorMdl.P observations only. Active 3 years, 10 months ago. The MCONVERT command by itself replaces the correlation matrix in the working file with a covariance matrix in the example below. A correlation matrix is first created which contains a vector of standard deviations. Active 9 days ago. When and how to use the Keras Functional API, Moving on as Head of Solutions and AI at Draper and Dash. If PriorMdl.IncludeTrend is true, element PriorMdl.NumSeries*PriorMdl.P + 2 is the linear time trend coefficient. The following example shows how to create a covariance matrix in R. How to Create a Covariance Matrix in R X must have at least as many observations as the observations used after the presample period. A Bayesian VAR model treats all coefficients and the innovations covariance matrix as random variables in the m-dimensional, stationary VARX(p) model. Create a conjugate prior model. Columns correspond to individual response variables. If PriorMdl.IncludeConstant is true, element PriorMdl.NumSeries*PriorMdl.P + 1 is the model constant. Prior Bayesian VAR model, specified as a model object in this table. Accelerating the pace of engineering and science. Create a conjugate prior model for the 2-D VARX(1) model parameters. For example, if we have matrix M then the correlation matrix can be found as cor (M). Expected portfolio variance= SQRT (WT * (Covariance Matrix) * W) The above equation gives us the standard deviation of a portfolio, in other words, the risk associated with a portfolio. I am a beginner in Linear Algerbra. [In our case, a 5×5 matrix.] [ϕ1,11ϕ1,12ϕ2,11ϕ2,12ϕ3,11ϕ3,12c1β11β12β13β14︷y1,t  ϕ1,21ϕ1,22ϕ2,21ϕ2,22ϕ3,21ϕ3,22c2β21β22β23β24︷y2,t]. If you have a random vector, then cov() will just give you an estimate of the variance. Predictor data for the exogenous regression component in the model, specified as the comma-separated pair consisting of 'X' and a numobs-by-PriorMdl.NumPredictors numeric matrix. First, we simulate from each prior to study the a priori relationship between correlations and standard deviations. However I realize RandNormal was originally intended to accept the covariance matrix, not the correlation matrix, as its input. Rows and columns correspond to innovations in the equations of the response variables ordered by PriorMdl.SeriesNames. simulate uses the default value of Sigma0 for Σ and draws a value of Λ from π(Λ|Σ,Y,X), the full conditional distribution of the VAR model coefficients. Number of draws to remove from the beginning of the sample to reduce transient effects, specified as the comma-separated pair consisting of 'BurnIn' and a nonnegative scalar. π(Λ,Σ|Y,X,Y0), where: Y is a T-by-m matrix containing the entire response series {yt}, t = 1,…,T. The actual sample size is BurnIn + NumDraws*Thin. Create a semiconjugate Bayesian VAR(4) prior model for the three response series. How to Create a Variance-Covariance Matrix Ask Question Asked 4 years, 9 months ago. Compute the real GDP, investment, and personal consumption rate series. We will first fit two models using two predictors with low correlation between them, and then fit a third model with three predictors where pred1 and pred2 are highly correlated with each other. The number of unique sub-covariance matrices is equal to the number of elements in the lower half of the matrix, excluding the main diagonal. Observed multivariate response series to which simulate fits the model, specified as a numobs-by-numseries numeric matrix. Adjusted sample size multiplier, specified as the comma-separated pair consisting of 'Thin' and a positive integer. If x is an M × N matrix, then xcov(x) returns a (2M – 1) × N 2 matrix with the autocovariances and cross-covariances of the columns of x. Assume the following prior distributions: [Φcβ]′|Σ∼Ν4×2(Μ,V,Σ), where M is a 4-by-2 matrix of means and V is the 4-by-4 among-coefficient scale matrix. If PriorMdl.NumPredictors > 0, elements PriorMdl.NumSeries*PriorMdl.P + 3 through k compose the vector of regression coefficients of the exogenous variables. Based on your location, we recommend that you select: . In a Bayesian analysis, the distribution of the parameters is updated with information about the parameters obtained from the data likelihood. Return the estimation summary. See cov.. The result is the joint posterior distribution Consequently, Coeff and Sigma represent draws from the posterior distribution. We know that we can generate uniform random numbers (using the language's built-in random functions). Specify the response series names. Covariance is a measure of how much two random variables vary together. Variance(L z) = L I L' = L L` = M. Variance (L z) = L I L' = L L` = M. so, in fact, we are producing random data that follow the desired covariance matrix. cov for financial time series objects is based on the MATLAB ® cov function. How does this connect to our simulated data? For example, a three dimensional covariance matrix is shown in equation (0). This figure shows the structure of Coeff(L,j) for a 2-D VAR(3) model that contains a constant vector and four exogenous predictors. Viewed 518 times 3. I want to create a covariance matrix using given ratio and degree of rotation. [Coeff,Sigma] = simulate(PriorMdl) returns a random vector of coefficients Coeff and a random innovations covariance matrix Sigma drawn from the prior Bayesian VAR model PriorMdl. Display the selected coefficients with corresponding names and the innovations covariance matrix. Σ∼InverseWishart(Ω,ν), where Ω is the 2-by-2 scale matrix and ν is the degrees of freedom. Copyright © 2020 | MH Corporate basic by MH Themes, Click here if you're looking to post or find an R/data-science job, Introducing our new book, Tidy Modeling with R, How to Explore Data: {DataExplorer} Package, R – Sorting a data frame by the contents of a column, Whose dream is this? Set separate variables for the initial values each coefficient matrix and vector. Load the US macroeconomic data set. If you specify Coeff0, simulate draws a value of Σ from π(Σ|Λ,Y,X) to start the Gibbs sampler. Β is the m-by-r matrix of regression coefficients of the r-by-1 vector of observed exogenous predictors xt, where r = NumPredictors. By default, Sigma0 is the residual mean squared error from multivariate least-squares. 2. Estimate the posterior distribution. The Covariance Matrix is also known as dispersion matrix and variance-covariance matrix. = simulate(PriorMdl,Y) draws from the posterior distributions produced or updated by incorporating the response data Y. NaNs in the data indicate missing values, which simulate removes by using list-wise deletion. Let’s assume that we generate a vector z of random normally independently distributed numbers with mean zero and variance one (with length equal to the dimension of M), we can create a realization of our multivariate distribution using the product L z. Do the previous step times to generate an n-dimensional Gaussian vectorwith a known me… Monte Carlo simulation is subject to variation. For a financial time series object containing multiple series, where each row is an observation, and each series a variable, cov(X) is the covariance matrix. Create a diffuse Bayesian VAR(4) prior model for the three response series. To create a covariance matrix, we first need to find the correlation matrix and a vector of standard deviations is also required. Before considering the data, you impose a joint prior distribution assumption on (Λ,Σ), which is governed by the distribution π(Λ,Σ). We need to somehow use these to generate n-dimensional gaussian random vectors. This returns the covariance of the various observations mentioned in variable x and co returns the covariance which is scalar in nature if x is a vector. X is a T-by-m matrix containing the entire exogenous series {xt}, t = 1,…,T. For example, you create a variance-covariance matrix for three variables X, Y, and Z. In this case, assume that the prior distribution is semiconjugate. This action reduces the effective sample size. If you specify Y0, then X must have at least numobs rows (see Y). To get the population covariance matrix (based on N), you’ll need to set the bias to True in the code below. For details on how simulate reduces the full sample, see Algorithms. Specify a burn-in period of 10,000, and a thinning factor of 5. Now we can use the simulated data to learn something about the effects of collinearity when fitting multiple linear regressions. Viewed 134 times 0. Verify that the estimates from each run converge to similar values. Generate a simulated covariance matrix. Specify the response series names. R – Risk and Compliance Survey: we need your help! The simplest example, and a cousin of a covariance matrix, is a correlation matrix. In this equation, ' W ' is the weights that signify the capital allocation and the covariance matrix signifies the interdependence of each stock on the other. PriorMdl. Other MathWorks country sites are not optimized for visits from your location. Simulate coefficients and innovations covariance matrix of Bayesian vector autoregression (VAR) model. Posted on October 12, 2011 by Luis in R bloggers | 0 Comments. Rows and columns correspond to innovations in the equations of the response variables ordered by PriorMdl.SeriesNames. By continuing to use this website, you consent to our use of cookies. In my example it is possible to see the huge increase for the standard error for pred1 and pred2, when we use both highly correlated explanatory variables in model 3. Consider the 2-D VARX(1) model for the US real GDP (RGDP) and investment (GCE) rates that treats the personal consumption (PCEC) rate as exogenous: [RGDPtGCEt]=c+Φ[RGDPt-1GCEt-1]+PCECtβ+εt. By default, Coeff0 is the multivariate least-squares estimate. Covariance is a measure of how changes in one variable are associated with changes in a second variable. A good practice is to run simulate multiple times with different parameter starting values. Remove all missing values from the resulting series. If X is a financial time series object with one series, cov(X) returns the variance. If PriorMdl is a diffusebvarm model, then you must also supply Y because simulate cannot draw from an improper prior distribution. The diagonal entries of the covariance matrix are the variances and the other entries are the covariances. Rows correspond to observations, and the last row contains the latest observation. numobs is the sample size. Description. GET FILE='Employee data.sav'. Otherwise, simulate uses the Gibbs sampler to estimate the posterior. Φ1,…,Φp are the m-by-m AR coefficient matrices of lags 1 through p, where p = numlags. Σ xi xj / N is the covariance for elements from the ith and jth data sets. The resultant can also be normalized by the number of observations subtracted 1. Web browsers do not support MATLAB commands. Draw 1000 samples from the posterior distribution. MathWorks is the leading developer of mathematical computing software for engineers and scientists. If x is a matrix, then the rows of the matrix represent the random variables while the rows in them represent the different observations and the resultant co returns the covariance matrix with rows and columns where the variance is there in the diagonal. V is a c x c variance-covariance matrix. For details on the structure of Coeff0, see the output Coeff. For example, let’s say that we want to create an example of the effect of collinearity when fitting multiple linear regressions, so we want to create one variable (the response) that is correlated with a number of explanatory variables and the explanatory variables have different correlations with each other. Specify the exogenous predictor data. Start with a Correlation Matrix. where f is the m-dimensional multivariate normal density with mean ztΛ and covariance Σ, evaluated at yt. = simulate(___,Name,Value) specifies options using one or more name-value pair arguments in addition to any of the input argument combinations in the previous syntaxes. simulate removes the white rectangles from the sample. A short video on how to make the variance-covariance matrix in Excel, which is a basic skill needed if you are going to optimize portfolios. Simulate a few thousand observations by using simulate. Rows correspond to presample observations, and the last row contains the latest observation. By default, simulate uses the first p = 1 observations of the response data to initialize the dynamic component of the model, and removes the corresponding observations from the predictor data. If there is only one observ… simulate does not use the regression component in the presample period. The variance-covariance matrix has the following structure: [ v a r ( x) c o v ( x, y) c o v ( x, y) v a r ( y)] where v a r ( x) = 1 n − 1 ∑ ( x i − x ¯) 2 and c o v ( x, y) = 1 n − 1 ∑ ( x i − x ¯) ( y i − y ¯) . Read 3 answers by scientists with 1 recommendation from their colleagues to the question asked by Houman Parsaei on Mar 31, 2020 Rows and columns of Sigma correspond to the innovations in the response equations ordered by PriorMdl.SeriesNames. For this reason, the covariance matrix is sometimes called the variance-covariance ma… If PriorMdl is a semiconjugatebvarm object and you do not specify starting values (Coeff0 and Sigma0), simulate samples from the posterior distribution by applying the Gibbs sampler. In either case, if you supply more rows than necessary, simulate uses the latest observations only. ϕq,jk is element (j,k) of the lag q AR coefficient matrix. εt is an m-by-1 vector of random, serially uncorrelated, multivariate normal innovations with the zero vector for the mean and the m-by-m matrix Σ for the covariance. A (DxD) covariance matrices will have D*(D+1)/2 -D unique sub-covariance matrices. Equivalently, vec([Φcβ]′)|Σ∼Ν8(vec(Μ),Σ⊗ V). The function repeats steps 1 and 2 until convergence. c is the m-by-1 vector of model constants if IncludeConstant is true. If simulate uses Monte Carlo simulation, then estimates and inferences might vary when you call simulate multiple times under seemingly equivalent conditions. Obtain a summary of the prior distribution. This gives you the covariance between lagged values of the random vector. Name is Simulated VAR model coefficients, returned as a (PriorMdl.NumSeries*k)-by-NumDraws numeric matrix, where k = PriorMdl.NumSeries*PriorMdl.P + PriorMdl.IncludeIntercept + PriorMdl.IncludeTrend + PriorMdl.NumPredictors, which is the number of coefficients in a response equation. My problem is the following. All predictor variables are present in the regression component of each response equation. It is easy and useful to show the covariance between two or more variables. yt is the m-dimensional observed response vector, where m = numseries. Because we want to simulate 100 realizations, rather than a single one, it pays to generate a matrix of random numbers with as many rows as variables to simulate and as many columns as observations to simulate. A positive value indicates that two variables will … This assumption implies that the data likelihood is. Display the first coefficient drawn from the distribution with corresponding parameter names, and display the first drawn innovations covariance matrix. There is a matrix operation called Cholesky decomposition, sort of equivalent to taking a square root with scalars, that is useful to produce correlated data. The following formula is used for covariance determination. Start the Gibbs sampler by assuming the posterior mean of Σ is the 3-D identity matrix. If we have a covariance matrix M, the Cholesky descomposition is a lower triangular matrix L, such as that M = L L'. In this section we carry out a simulation based analysis to assess the performance of these different covariance matrix prior. Horizontally concatenate all coefficient means in this order: Vectorize the transpose of the coefficient mean matrix. The covariance matrix implies that you have a bivariate sample, not a univariate sample. Starting value of the VAR model coefficients for the Gibbs sampler, specified as the comma-separated pair consisting of 'Coeff0' and a numeric column vector with (PriorMdl.NumSeries*k)-by-NumDraws elements, where k = PriorMdl.NumSeries*PriorMdl.P + PriorMdl.IncludeIntercept + PriorMdl.IncludeTrend + PriorMdl.NumPredictors, which is the number of coefficients in a response equation. Each page is an individual draw. Number of random draws from the distributions, specified as the comma-separated pair consisting of 'NumDraws' and a positive integer. Y0 is a p-by-m matrix of presample data used to initialize the VAR model for estimation. xi is a deviation score from the ith data set. Λ=[Φ1Φ2⋯ΦpcδΒ]′, which is an (mp + r + 2)-by-m random matrix of the coefficients, and the m(mp + r + 2)-by-1 vector λ = vec(Λ). Second, we simulate data from the model and analyze posterior means to determine the impact prior choice has on posterior inference. for your data, x ¯ = ( 3 + 2) 2 = 5 2. y ¯ = ( 7 + 4) 2 = 11 2. v a r ( x) = ( 3 − 5 2) 2 + ( 2 − 5 2) 2. In probability theory and statistics, a covariance matrix (also known as auto-covariance matrix, dispersion matrix, variance matrix, or variance–covariance matrix) is a square matrix giving the covariance between each pair of elements of a given random vector. You can compute the autocovariance sequence. Any covariance matrix is symmetric and positive semi-definite and its main diagonal contains variances (i.e., the covariance of each element with itself). Covariance is one of the measures used for understanding how a variable is associated with another variable. Simulate directly from the posterior distribution. If A is a row or column vector, C is the scalar-valued variance.. For two-vector or two-matrix input, C is the 2-by-2 covariance matrix between the two random variables. The variances are along the diagonal of C. [Coeff,Sigma] Name1,Value1,...,NameN,ValueN. Specifically, it’s a measure of the degree to which two variables are linearly associated. COV (X,Y) = ∑(x – x) (y – y) / n The covariance matrix is a square matrix to understand the relationships presented between the different variables in a dataset. For all t, εt is a series of independent 2-D normal innovations with a mean of 0 and covariance Σ. The formula to calculate the covariance between two variables, X and Y is: COV (X, Y) = Σ (x-x) (y-y) / n simulate cannot draw values from an improper distribution, which is a distribution whose density does not integrate to 1. simulate draws a value of Σ from π(Σ|Λ,Y,X), the full conditional distribution of the innovations covariance matrix, by using the previously generated value of Λ. Rows correspond to observations, and the last row contains the latest observation. The model has one of the three forms described in this table. Choose a web site to get translated content where available and see local events and offers. Elements PriorMdl.NumSeries + 1 through 2*PriorMdl.NumSeries correspond to the lag 2 AR coefficients of the response variables ordered by PriorMdl.SeriesNames. This is the complete Python code to derive … Consider the 3-D VAR(4) model for the US inflation (INFL), unemployment (UNRATE), and federal funds (FEDFUNDS) rates. Here's how we'll do this: 1. Each page is a separate draw (covariance) from the distribution. 1. Please see our, Number of draws to remove from beginning of sample, Starting value of VAR model coefficients for Gibbs sampler, Starting value of innovations covariance matrix for Gibbs sampler, array of positive definite numeric matrices, Draw Coefficients and Innovations Covariance Matrix from Prior Distribution, Simulate Parameters from Analytically Tractable Posterior Distribution, Simulate Parameters from Analytically Intractable Posterior Distribution, Options for Semiconjugate Prior Distributions, Bayesian Vector Autoregression (VAR) Model, A Practical Guide to Modeling Financial Risk with MATLAB, Dependent, matrix-normal-inverse-Wishart conjugate model returned by, Independent, normal-inverse-Wishart semiconjugate prior model returned by, Normal conjugate model with a fixed innovations covariance matrix, returned by. Each column is a separate draw from the distribution. Specify optional example [ Coeff , Sigma ] = simulate( PriorMdl , Y ) draws from the posterior distributions produced or updated by incorporating the response data Y . Assume that a conjugate prior distribution π([Φ1,...,Φ4,c]′,Σ) governs the behavior of the parameters. Columns correspond to individual predictor variables. = simulate(PriorMdl) returns a random vector of coefficients Coeff and a random innovations covariance matrix Sigma drawn from the prior Bayesian VAR(p) model Coeff is a 39-by-1000 matrix of randomly drawn coefficients. By default, simulate uses Y(1:PriorMdl.P,:) as presample observations, and then estimates the posterior using Y((PriorMdl.P + 1):end,:). Draw a set of coefficients and an innovations covariance matrix from the prior distribution. comma-separated pairs of Name,Value arguments. Ask Question Asked 9 days ago. Columns must correspond to the response series in Y. AR{r}(j,k) is the AR coefficient of response variable k (lagged r units) in response equation j. In this case, assume that the prior distribution is diffuse. Load the US macroeconomic data set. To reproduce estimation results, set a random number seed by using rng before calling simulate. This website uses cookies to improve your user experience, personalize content and ads, and analyze website traffic. Cross-covariance or autocovariance, returned as a vector or matrix. With the covariance we can calculate entries of the covariance matrix, which is a square matrix given by Ci,j=σ(xi,xj) where C∈Rd×d and d describes the dimension or number of random variables of the data (e.g. Generate a bunch of uniform random numbers and convert them into a Gaussian random numberwith a known mean and standard deviation. Okay, Exercise 2 asks us to create that covariance matrix and for that we will use Excel's =COVARIANCE.S() function. In general, elements (q – 1)*PriorMdl.NumSeries + 1 through q*PriorMdl.NumSeries correspond to the lag q AR coefficients of the response variables ordered by PriorMdl.SeriesNames. where 0z is a 1-by-(mp + r + 2) vector of zeros. Therefore Variance(L z) = L I L' = L L` = M so, in fact, we are producing random data that follow the desired covariance matrix. Draw 1000 samples from the posterior distribution. For single matrix input, C has size [size(A,2) size(A,2)] based on the number of random variables (columns) represented by A.The variances of the columns are along the diagonal. The variance of z is the identity matrix I; remember that the random numbers have variance one and are independently distributed. Y represents the continuation of the presample response series in Y0. δ is the m-by-1 vector of linear time trend coefficients if IncludeTrend is true. Otherwise, X must have at least numobs – PriorMdl.P observations to account for the presample removal. For draw j, Coeff(1:k,j) corresponds to all coefficients in the equation of response variable PriorMdl.SeriesNames(1), Coeff((k + 1):(2*k),j) corresponds to all coefficients in the equation of response variable PriorMdl.SeriesNames(2), and so on. The covariance matrix can be decomposed into multiple unique (2x2) covariance matrices. The correlation matrix can be found by using cor function with matrix object. For a set of indices corresponding to an equation: Elements 1 through PriorMdl.NumSeries correspond to the lag 1 AR coefficients of the response variables ordered by PriorMdl.SeriesNames. PosteriorMdl is a conjugatebvarm model, which is analytically tractable. Consider the 3-D VAR(4) model of Draw Coefficients and Innovations Covariance Matrix from Prior Distribution. The covariance matrix is a matrix that only concerns the relationships between variables, so it will be a k x k square matrix. Rectangles represent successive draws from the distribution. If simulate estimates a posterior distribution (when you supply Y) and the posterior is analytically tractable, simulate simulates directly from the posterior. If PriorMdl is a normalbvarm object, all covariances in Sigma are equal to PriorMdl.Covariance. To assess convergence, draw a trace plot of the sample. N is the number of scores in each of the c data sets. the argument name and Value is the corresponding value. Every year there is at least a couple of occasions when I have to simulate multivariate data that follow a given covariance matrix. simulate does not return default starting values that it generates. You can also select a web site from the following list: Select the China site (in Chinese or English) for best site performance. Do you want to open this version instead? The reason why this works is that the Variance(L z) = L Variance(z) L' as L is just a constant. It is actually used for computing the covariance in between every column of data matrix. You clicked a link that corresponds to this MATLAB command: Run the command by entering it in the MATLAB Command Window. Starting value of the innovations covariance matrix for the Gibbs sampler, specified as the comma-separated pair consisting of 'Sigma0' and a PriorMdl.NumSeries-by-PriorMdl.NumSeries positive definite numeric matrix. 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https://it.mathworks.com/matlabcentral/cody/problems/2867-matlab-basics-rounding-iii/solutions/2902250
[ "Cody\n\n# Problem 2867. Matlab Basics - Rounding III\n\nSolution 2902250\n\nSubmitted on 2 Sep 2020 by Kunjunni Mohanan\nThis solution is locked. To view this solution, you need to provide a solution of the same size or smaller.\n\n### Test Suite\n\nTest Status Code Input and Output\n1   Pass\nx = 12358466243; y_correct = 12358470000; assert(isequal(round_ten_thou(x),y_correct))\n\n2   Pass\nx = 12358466243.325; y_correct = 12358470000.000; assert(isequal(round_ten_thou(x),y_correct))\n\n### Community Treasure Hunt\n\nFind the treasures in MATLAB Central and discover how the community can help you!\n\nStart Hunting!" ]
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http://programming4beginners.com/tutorial/chapter06/debugger
[ "## 6. Debugger\n\nThe execution of programs by hand provides insight into mechanics of any new program we encounter. Even the best programmers like to use it in order to better understand some complicated pieces of code. A debugger is a tool that provides a more sophisticated, computer-assisted way of doing pretty much the same thing, including a few nice bonuses, too.\n\nSince execution by hand plays an important role in this chapter, we kindly ask you to revisit it now by manually executing the program given below. This process will also help you understand how the given program works. So, pick up the usual accessories: a paper, a pencil and an eraser.\n\n```#include <iostream>\nusing namespace std;\n\nint main()\n{\ndouble sum=0;\ncout << \"Let us start out with the number 0.\" << endl;\n\nfor (double i=1; i<=5; i++)\n{\nsum = sum+i;\ncout << \"After adding the number \" << i << endl;\ncout << \"the total sum will be \" << sum << \".\" << endl;\n}\n}\n```\n\nBefore you begin executing this program, divide the piece of paper into three parts: one for the standard input, one for the standard output and one for the memory. Just to remind you what this process looks like, we will execute the first statement of the function `main`:\n\n`STDIN``STDOUT``MEMORY`\n```sum 0\n```\n\nAs you can see, this program has no values given on the standard input. This is not a problem, as it will not be reading any (as can be deduced from the absence of the `cin` statements in the source code).\n\nOne additional note: if you find yourself confused by this statement\n\n``` sum = sum+i;\n```\n\nthen go back to the chapter Variables, where we have covered this particular case in the section \"X Becomes x Plus 3\".", null, "All is ready now for execution by hand. Ready, steady, go!\n\nAs the result of executing this program by hand, the following text should appear on your standard output:\n\n```STDOUT\n\nLet us start out with the number 0.\nthe total sum will be 1.\nthe total sum will be 3.\nthe total sum will be 6.\nUpon completing the execution by hand, under memory section you should have the following values for the variables `sum` and `i`:[*]\n```sum 15" ]
[ null, "http://programming4beginners.com/images/pickaxe-web.png", null ]
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https://pure.york.ac.uk/portal/en/publications/approximate-marginal-densities-of-independent-parameters(3b88bb9b-0888-42ac-99b9-dd58e582bc35)/export.html
[ "## Approximate marginal densities of independent parameters\n\nResearch output: Contribution to journalArticlepeer-review\n\n### Standard\n\nApproximate marginal densities of independent parameters. / Kharroubi, Samer A.\n\nIn: Statistics: A Journal of Theoretical and Applied Statistics, Vol. 46, No. 4, 08.2011, p. 1-13.\n\nResearch output: Contribution to journalArticlepeer-review\n\n### Harvard\n\nKharroubi, SA 2011, 'Approximate marginal densities of independent parameters', Statistics: A Journal of Theoretical and Applied Statistics, vol. 46, no. 4, pp. 1-13. https://doi.org/10.1080/02331888.2010.540667\n\n### APA\n\nKharroubi, S. A. (2011). Approximate marginal densities of independent parameters. Statistics: A Journal of Theoretical and Applied Statistics, 46(4), 1-13. https://doi.org/10.1080/02331888.2010.540667\n\n### Vancouver\n\nKharroubi SA. Approximate marginal densities of independent parameters. Statistics: A Journal of Theoretical and Applied Statistics. 2011 Aug;46(4):1-13. https://doi.org/10.1080/02331888.2010.540667\n\n### Author\n\nKharroubi, Samer A. / Approximate marginal densities of independent parameters. In: Statistics: A Journal of Theoretical and Applied Statistics. 2011 ; Vol. 46, No. 4. pp. 1-13.\n\n@article{3b88bb9b088842ac99b9dd58e582bc35,\ntitle = \"Approximate marginal densities of independent parameters\",\nabstract = \"This paper presents an asymptotic approximation for the marginal density of any parameter of interest of a joint posterior density in the case of independent parameters. The approximation is based on the signed-root-based importance sampling algorithm considered in Kharroubi and Sweeting [Posterior simulation via signed root log-likelihood ratios, Bayesian Anal. (2010), in press] and gives rise to the alternative simulation-consistent scheme to Markov chain Monte Carlo for marginal densities. The consideration is illustrated by a censored regression model. \",\nkeywords = \"Statistics, Bayesian inference; , importance sampling; , signed root log-likelihood ratio; , simulation\",\nauthor = \"Kharroubi, {Samer A.}\",\nyear = \"2011\",\nmonth = aug,\ndoi = \"10.1080/02331888.2010.540667\",\nlanguage = \"English\",\nvolume = \"46\",\npages = \"1--13\",\njournal = \"Statistics: A Journal of Theoretical and Applied Statistics\",\nissn = \"0233-1888\",\npublisher = \"Taylor and Francis Ltd.\",\nnumber = \"4\",\n\n}\n\nTY - JOUR\n\nT1 - Approximate marginal densities of independent parameters\n\nAU - Kharroubi, Samer A.\n\nPY - 2011/8\n\nY1 - 2011/8\n\nN2 - This paper presents an asymptotic approximation for the marginal density of any parameter of interest of a joint posterior density in the case of independent parameters. The approximation is based on the signed-root-based importance sampling algorithm considered in Kharroubi and Sweeting [Posterior simulation via signed root log-likelihood ratios, Bayesian Anal. (2010), in press] and gives rise to the alternative simulation-consistent scheme to Markov chain Monte Carlo for marginal densities. The consideration is illustrated by a censored regression model.\n\nAB - This paper presents an asymptotic approximation for the marginal density of any parameter of interest of a joint posterior density in the case of independent parameters. The approximation is based on the signed-root-based importance sampling algorithm considered in Kharroubi and Sweeting [Posterior simulation via signed root log-likelihood ratios, Bayesian Anal. (2010), in press] and gives rise to the alternative simulation-consistent scheme to Markov chain Monte Carlo for marginal densities. The consideration is illustrated by a censored regression model.\n\nKW - Statistics\n\nKW - Bayesian inference;\n\nKW - importance sampling;\n\nKW - signed root log-likelihood ratio;\n\nKW - simulation\n\nUR - http://www.scopus.com/inward/record.url?scp=84863815889&partnerID=8YFLogxK\n\nU2 - 10.1080/02331888.2010.540667\n\nDO - 10.1080/02331888.2010.540667\n\nM3 - Article\n\nVL - 46\n\nSP - 1\n\nEP - 13\n\nJO - Statistics: A Journal of Theoretical and Applied Statistics\n\nJF - Statistics: A Journal of Theoretical and Applied Statistics\n\nSN - 0233-1888\n\nIS - 4\n\nER -" ]
[ null ]
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https://gre.magoosh.com/forum/315
[ "Source: Revised GRE PDF 1st Ed. Section 6: Math; #23 (p. 90)\n\n65\n\n# A developer has land that has x feet\n\nA developer has land that has x feet of lake frontage. The land is to be subdivided into lots, each of which is to have either 80 feet or 100 feet of lake frontage. If 1/9 of the lots are to have 80 feet of frontage each and the remaining 40 lots are to have 100 feet of frontage each, what is the value of x ? 400; 3,200; 3,700; 4,400; 4,760\n\n### 7 Explanations\n\n4\n\nKat Hidalgo\n\ni try to eliminate choices as fast as possible, so knowing from the start that 40 lots are 100ft means that the total size of the lake, x, is at least 40 x 100 = 4,000 ft. this eliminates the first three choices immediately.\n\nthat leaves us with options D. 4,400 and E. 4,760. or as we can also think of it as, 400ft and 760ft to be split into the remaining lots of 80ft. so we have 400/80 = 5 lots and 760/80 = 9.5 lots. first off, i'm already doubtful about the possibility of half of a lot so i'm leaning towards 5 lots (option D) already.\n\nto check, if E is correct and 1/9 of the lots = 9.5 lots, then that should mean the remaining 8/9 lots would be 76 lots (9.5 x 8 = 76). but the problem explicitly tells us that the remaining number of lots is 40, not 76. (check the math using chris' method!)\n\nso answer D. 4,400ft is what we go with.\n\nSep 25, 2019 • Comment\n\nThat's excellent logic! Thinking like this is a good way to ace the GRE :) Keep it up!\n\n2\n\nto find the number of lots for 80 feet we can use\n(40+x)/9 = x\n=>40+x=9x\n=>8x=40\n=>x=5\n\nMay 11, 2019 • Comment\n\nThat could definitely work!\n\nThanks and even\n40+X/9 = X\n(360+X)/9=X\n360=8x\nX=45\nWould work I guess\n\nSam Kinsman\n\nYes, that works! That will give us the total number of lots, which is 45.\n\n1\n\nAnna Roberts\n\nCan we solve by\n8/9 x = 40*100?\nI solved for x and got 4500 so picked 4400 the correct answer.\n\nAlso I am having doubts how to check backwards from answer like Chris mentioned.\nFor D should I check if 4000/4400 is roughly 8/9 and 400/4400 is roughly 1/9?\nAnd For E should I check if 760/4760 is close to 1/9?\nBtw neither of them is exact 1/9.\n\nNov 23, 2017 • Comment\n\nJonathan , Magoosh Tutor\n\n(8/9)x = 40 * 100 is not correct.\n\nIt would be correct if we were 8/9 of the total frontage comes from the 100-feet lots.\n\nRather:\n8/9 (number of lots) = 40 is correct\nso (number of lots) = 45\nand 1/9 of lots = 5 lots\n\nSo we have:\n\n5(80) + 40(100) = 4,400\n\nWe can work backwards because we know we have 40 lots with 100 feet of frontage. So we have 4,000 + something.\n(A), (B), and (C) are out immediately because they are less than 4000.\nTo check (D) 4,400:\n\n4,400 - 4000 = 400 which divided by 80 is 5\n\nIf 40 is 8/9 then is 1/9 equal to 5? Yes.\n\nSo, (D) is correct.\n\n4\n\nPhanindra Chandraprakash\n\nI had solved this problem in this way:\n\nLet x bet the total length of the lake frontage.\ngiven that, 1/9(x) = 80 and remaining are 40 plots with 100 feet length.\n\ntherefore,\n\n1/9(x)+(40*100) = x\n\nnow, solve for x,\nx+36000=9x\n8x=36000\nx=4500\nthe answer nearest to 4500 is D, i'e 4400.\n\nHence, D is the correct answer.\n\nSep 14, 2015 • Comment\n\nCydney Seigerman, Magoosh Tutor\n\nHi Phanindra :)\n\nIt looks like there's a slight conceptual mistake: (1/9)x = 80 is not actually true.\n\nWe are told that 1/9 of the lots have 80 feet of lake frontage, not that 1/9 of the length of the lake frontage is 80 feet.\n\nTo solve this question, we have to figure out how many lots have 80 feet of lake frontage, which is 1/9 of the total number of lots. We can use the fact that 40 lots are equal to 8/9 of the lots to determine that there are 45 lots total, 5 of which have 80 feet of lake frontage:\n\n* 5 lots of 80 feet = 400 feet of lake frontage\n* 40 lots of 100 feet = 4000 feet of lake frontage\n\nI hope this helps!\n\nCheers,\nCydney :)\n\nMayank Chandok\n\nWow, I just loved your explanation.\n\n3", null, "Jonathan , Magoosh Tutor\n\nHi Thomas,\nKevin mean 40 total of the REMAINING lots.\n\n40 remaining lots is 8/9 of the total. 40 represents 8 of the 9 parts, so there are 5 lots per part.\n\nAnd yes, that means the original number of lots is 45.\n\nI hope that clarifies.\n\nApr 14, 2015 • Comment\n\n3\n\nGabriella Gonzalez\n\nwhere did you get 5 from???\n\nOct 2, 2014 • Comment\n\n, Magoosh Tutor\n\nHi Gabriella,\n\nHappy to help! :) The 5 lots comes from seeing that there are 40 lots total. Then we can see that the difference between 1/9 and 8/9 is 8 times. Thus if we want to find the total lots that have 80 ft of frontage, we can set up this equation:\n\n40 / 8 = 5\n\nIn this way, we can work backwards from what we know, determine the multiples, and figure out how many lots have 80 feet of frontage.\n\nThen we move forward to solve the problem. :D\n\nI hope that this helps!\n\nCheers,\n\nKevin\n\nThomas Robinson\n\nDo you mean 45 lots? Doesn't 8/9x=40 mean there are 45 total lots: 5 at 80ft, 40 at 100ft?\n\n10", null, "Chris Lele, Magoosh Tutor\n\nSep 26, 2012 • Comment" ]
[ null, "https://secure.gravatar.com/avatar/f168ae963feab858840c0c1d22612dd9", null, "https://secure.gravatar.com/avatar/198545d5a4baea0ba0fd0c0fc8a5d466", null ]
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https://visualfractions.com/calculator/factors/factors-of-861/
[ "# Factors of 861\n\nSo you need to find the factors of 861 do you? In this quick guide we'll describe what the factors of 861 are, how you find them and list out the factor pairs of 861 for you to prove the calculation works. Let's dive in!\n\nWant to quickly learn or show students how to find the factors of 861? Play this very quick and fun video now!\n\n## Factors of 861 Definition\n\nWhen we talk about the factors of 861, what we really mean is all of the positive and negative integers (whole numbers) that can be evenly divided into 861. If you were to take 861 and divide it by one of its factors, the answer would be another factor of 861.\n\nLet's look at how to find all of the factors of 861 and list them out.\n\n## How to Find the Factors of 861\n\nWe just said that a factor is a number that can be divided equally into 861. So the way you find and list all of the factors of 861 is to go through every number up to and including 861 and check which numbers result in an even quotient (which means no decimal place).\n\nDoing this by hand for large numbers can be time consuming, but it's relatively easy for a computer program to do it. Our calculator has worked this out for you. Here are all of the factors of 861:\n\n• 861 ÷ 1 = 861\n• 861 ÷ 3 = 287\n• 861 ÷ 7 = 123\n• 861 ÷ 21 = 41\n• 861 ÷ 41 = 21\n• 861 ÷ 123 = 7\n• 861 ÷ 287 = 3\n• 861 ÷ 861 = 1\n\nAll of these factors can be used to divide 861 by and get a whole number. The full list of positive factors for 861 are:\n\n1, 3, 7, 21, 41, 123, 287, and 861\n\n## Negative Factors of 861\n\nTechnically, in math you can also have negative factors of 861. If you are looking to calculate the factors of a number for homework or a test, most often the teacher or exam will be looking for specifically positive numbers.\n\nHowever, we can just flip the positive numbers into negatives and those negative numbers would also be factors of 861:\n\n-1, -3, -7, -21, -41, -123, -287, and -861\n\n## How Many Factors of 861 Are There?\n\nAs we can see from the calculations above there are a total of 8 positive factors for 861 and 8 negative factors for 861 for a total of 16 factors for the number 861.\n\nThere are 8 positive factors of 861 and 8 negative factors of 861. Wht are there negative numbers that can be a factor of 861?\n\n## Factor Pairs of 861\n\nA factor pair is a combination of two factors which can be multiplied together to equal 861. For 861, all of the possible factor pairs are listed below:\n\n• 1 x 861 = 861\n• 3 x 287 = 861\n• 7 x 123 = 861\n• 21 x 41 = 861\n\nWe have also written a guide that goes into a little more detail about the factor pairs for 861 in case you are interested!\n\nJust like before, we can also list out all of the negative factor pairs for 861:\n\n• -1 x -861 = 861\n• -3 x -287 = 861\n• -7 x -123 = 861\n• -21 x -41 = 861\n\nNotice in the negative factor pairs that because we are multiplying a minus with a minus, the result is a positive number.\n\nSo there you have it. A complete guide to the factors of 861. You should now have the knowledge and skills to go out and calculate your own factors and factor pairs for any number you like.\n\nFeel free to try the calculator below to check another number or, if you're feeling fancy, grab a pencil and paper and try and do it by hand. Just make sure to pick small numbers!\n\nIf you found this content useful in your research, please do us a great favor and use the tool below to make sure you properly reference us wherever you use it. We really appreciate your support!\n\n• \"Factors of 861\". VisualFractions.com. Accessed on December 6, 2021. http://visualfractions.com/calculator/factors/factors-of-861/.\n\n• \"Factors of 861\". VisualFractions.com, http://visualfractions.com/calculator/factors/factors-of-861/. Accessed 6 December, 2021." ]
[ null ]
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https://fdocuments.net/document/the-1000000-netflix-contest.html
[ "• date post\n\n12-Jan-2016\n• Category\n\n## Documents\n\n• view\n\n35\n• download\n\n2\n\nTAGS:\n\n• #### prune steps\n\nEmbed Size (px)\n\ndescription\n\nThe \\$1,000,000 Netflix Contest. is to develop a \" ratings prediction program “ that can beat Netflix ’ s (called Cinematch) by 10% in predicting what rating users gave to movies. I.e., predict rating(M,U) where (M,U)  QUALIFYING(MovieID, UserID) . - PowerPoint PPT Presentation\n\n### Transcript of The \\$1,000,000 Netflix Contest\n\n• The \\$1,000,000 Netflix Contest is to develop a \"ratings prediction programthat can beat Netflixs (called Cinematch) by 10% in predicting what rating users gave to movies.I.e., predict rating(M,U) where (M,U) QUALIFYING(MovieID, UserID).\n\nNetflix uses Cinematch to decide which movies a user will probably like next (based on all past rating history). All ratings are \"5-star\" ratings (5 is highest. 1 is lowest. Caution: 0 means did not rate).\n\nUnfortunately rating=0 does not mean that the user \"disliked\" that movie, but that it wasn't rated at all. Most ratings are 0. Therefore, the ratings data sets are NOT vector spaces!\n\nOne can approach the Netflix contest problem as a data mining Classification or Prediction problem.\n\nA \"history of ratings by users to movies, TRAINING(MovieID, UserID, Rating, Date) is given with which to train your predictor, which will predict the ratings given to QUALIFYING movie-user pairs (Netflix knows the rating given to Qualifying pairs, but you don't.)\n\nSince the TRAINING is very large, Netflix also provides a smaller, but representative subset of TRAINING, PROBE(MovieID, UserID) (~2 orders of magnitude smaller than TRAINING).\n\nNetflix gives 5 years to submit QUALIFYING predictions. That contest window is about 1/2 gone now.\n\nA team can submit as many solution as they wish and at any time. Each October, Netflix give \\$50,000 to the team on top the so-called Netflix Leaderboard. Bellcore has won that twice.\n\n• The Netflix Contest (USER versus MOVIE voting)One can address the prediction or classification problem using several different \"approaches\".\n\nUSER VOTERs (approach 1): To predict the rating of a pair, (M,U), we take TRAINING as a vector space of user ratings vectors. The users are the points in the vector space and the movies are the dimensions in that vector space. Since there are 17,770 movies each user is tuple of 17770 ratings, if all movies are used as dimensions. Thats too many dimensions! The first dimension pruning: restrict to only those movies that U has rated ( =supportU ). We also allow another round of dimension pruning based on correlation with M.\n\nOnce the dimensions movie set is pruned, we pick a Set of Near Neighbor users to U, (NNS) from the users, V, who have rated M ( =supportM ). Near is defined based on correlation with U. One can think of this step as the voter pruning step. Note: most correlations calculations involve the other variable also. I.e., the result of a user pruning depends on the pruned movie set and vice versa. Thus, theoretically, the movie/user pruning steps could be alternated ad infinitum! Our current approach is to allow an initial global dimension prune, then the voter prune, then a final dimension prune. You will see these 3 prune steps in the .config files.\n\nWe then let voters vote, but they dont necessarily cast the straight-forward rating(M,V) vote.\n\nThe best way to think about the 3 pruning steps (and there could be more!) is: We prune down the dimensions so that vector space methods are tractable, emeliorating the curse of dimensionality (the first, which may be turned off, is a global dimension prune (not based on individual voters). The second is the voter prune based on the currently pruned dimensions. The third is a final dimension prune (different for each voter) which give the final vector space over which the vote by that voter is calculated. Then we let those VOTERS vote as to the best rating prediction to be made. There are many ways to prune, vote, tally, and decide on the final prediction. These choices make up the .config file.MOVIE VOTERs (approach 2) is identical with roles of Movies (voters) and Users (dimensions) reversed\n\n• The Netflix Contest (Using SLURM to generate a clustering)SLURM has been set up to run on the Penryn Cluster2 (32 8 processor machines - 1 terrabyte of main memory) so that one can create a .config file (must end in .config) which specifies all the parameters for the program. Issuing:\n\n./mpp-submit -S -i Data/probe-full.txt -c pf.0001/u.00.00/u.00.00.config -t .0001 -d ./pf.0001\n\nThe program pulls parameters from .config: -t .0001 means SquareError threshold = .0001 -d ./pf.0001 means results goto ./pf.0001 dir. The prog takes as input, the file Data/probe-full.txt (which is not quite the full probe but close) with format:mpp-submit S i InputFile.txt c ConfigFile.config t SqErrThrhd d DirTakesInputFile.txt (MovieID with interleaved UserIDs format or .txt format. See next slide)ConfigFile.config (shows which program to run. In .config format. See next slide)SqErrThrhld (if PredictionSqErr SqErrThrhld, put pair in Dir/lo-InputFile.txt, else put in Dir/hi-InputFile.txt)Directory (existing directory for the output)as inputPuts as output (in Dir)lo-InputFileName.txtHi-InputFileName.txtInputFileName.configInputFileName.rmse\n\n• The Netflix Contest (Using SLURM to generate a clustering)./mpp-submit -S -i Data/probe-full.txt -c pf.0001/u.00.00/u.00.00.config -t .0001 -d ./pf.0001\n\nInputFile ConfigFile: pf.0001/u.00.00/u.00.00.configData/probe-full.txt1: 30878 2647871 1283744 2488120 317050 1904905 1989766 14756 1027056 1149588 1394012 1406595 2529547 1682104 2625019 2603381 1774623 470861 712610 1772839 1059319 2380848 548064 2: 1959936 748922 1131325 1312846 2314531 1636093 584750 2418486 715897 1172326 etc.\n\nwhere 1: and 2: are movieIDs and the others are userIDs. Note, this in an interleaved format of a 2-column DB file, probe-full(movieID,userID)Program sets parameters as specified in the .config:\n\nuser_voting = enabled movie_voting = disabled user_vote_weight = 1\n\n# processed only if user voting enabled. [user_voting] Prune_Movie_in_SupU = disabledPrune_Users_in_SupM = enabled Prune_Movies_in_CoSupUV = enabled\n\n[Prune_Movies_in_SupU] method=MoviePrune leftside = 0 width = 30000 mstrt = 0 mstrt_mult=0 ustrt = 0 ustrt_mult=0 TSa = -100 TSb = -100 Tdvp = -1 Tdvs = -1 Tvdp = -1 Tvds = -1 TD = -1 TP = -1 PPm = .1 TV = -1 TSD = -1 Ch = 1 Ct = 1 [Prune_Movies_in_CoSupUV] method=MovieCommonCoSupportPrune leftside = 0 width = 2000 mstrt = 0 mstrt_mult=0 ustrt = 0 ustrt_mult=0 TSa = -100 TSb = -100 Tdvp = -1 Tdvs = -1 Tvdp = -1 Tvds = -1 TD = -1 TP = -1 PPm = .1 TV = -1 TSD = -1 Ch = 1 Ct = 1(Part identical to blue for movie voting params)[Prune_Users_in_SupM] method=UserCommonCoSupportPrune leftside = 0 width = 30000 mstrt = 0 mstrt_mult=0 ustrt = 0 ustrt_mult=0 TSa = -100 TSb = -100 Tdvp = -1 Tdvs = -1 Tvdp = -1 Tvds = -1 TD = -1 TP = -1 PPm = .1 TV = -1 TSD = -1 Ch = 1 Ct = 1 Only the method, leftside, width, Ch=Choice, Ct=Count parameters are used at this time.\n\nUsing this program, the many \"lo-u.xx.xx\" and, if movie voting is also enabled, \"lo-m.yy.yy\" files constitute what we have called a clustering (tho theyre not mutually exclusive). Once we have {z-lo.xx.yy | z=u of m } we can make a submission by: qualifying pair (m,u), use correlations to pick program to make that prediction.\n\n• The Netflix Contest (Using this scheme to predict Qualifying pair ratings)The above prediction scheme requires the existence of Square Errors (SqErr),e.g., clusters files, lo-u.vv.nn.txt and lo-m.nn.vv.txt are composed of all input pairs such that SqErr .0001\n\nTo predict rating(M,U) for pairs from Qualifying, we wont have answers, so we wont have SqErrs of our predictions relative to those answers.\n\nSo how can we form good cluster then?\n\nOnce thats decided what matchup algorithm should we use to match a cluster (program) to a Qualifying pair to be predicted?\n\nAfter the clusters are created, we can try the matchup algorithms that worked best for Probe predictions, but\n\nWe may want to develop new ones because the performance of those matchup algorithms may depend on the way the clusters were created.\n\nWe could use the same 288 configs to generate a new config-subset-collection of Qualifying pairs using, e.g., prediction some kind of prediction variation instead of thresholded prediction SqErr?\n\nlo-u.vv.nn.txt could be constructed to consist of Qualifying pairs as follows (a variation based method):Set all answers in Qualifying to 1. Use ./mpp-submit to create clusters as above (threshold=.0001) in a directory, q1. Set all answers in Qualifying to 2. Use ./mpp-submit to create clusters as above (threshold=.0001) in a directory, q2, etc. This will create a clustering of 288*5=1440 cluster sets (but, of course, only 288 different programs configs).\n\nOne could matchup a Qualifying pair using count-based correlations, Pearson-correlations, 1-perpendicular-correlations, or?One could matchup (M,U) with the cluster in which the sum of the M and U counts (or counts relative to cluster size) is max?Other?\n\n• The Netflix Files {Mi} i=1..17770 given by Netflix as:TRAINING as M-U interaction cube (Rolodex Model, m\\u)Pmh, 2TRAINING in MySQL with key (mID, uID) 11-bit day numbers starting at 1=1/1/99 and ending at 2922=12/31/06.Mi ( uID, Rating, Date )For each MovieID, Mi, this is a file of all users who rated it, the rating, the rating date.bit-sliced TRAINING: M-U interaction cube (Rolodex Model, m\\u)TRAINING in MySQL with key (uID, mID) 11-bit day numbers starting at 1=1/1/99 and ending at 2922=12/31/06.\n\n• The Program: Code Structure - the main modulesmpp-mpred.C reads a Neflix PROBE file Mi(Uid) and passes Mi and ProbeSupport(Mi) to mpp-user.C to make predictions for each pair (Mi,U), foreach UProbeSupport(Mi).It can also calls separate instances of mpp-user.C for many Us, to be processed in parallel (governed by the number of \"slots\" specified in 1st code line.)mpp-user.C loops thru ProbeSupport(M), the ULOOP, reading in the designated (matchedup) conf" ]
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https://softmath.com/math-com-calculator/factoring-expressions/statistics-math-answers.html
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What is the comparable salary today, assuming an inflation rate of 3% compounded annually? (Round your answer to the nearest cent.), fractions.\n\nLess a 30 trade discount, solving equations worksheets that create a punch line, Point Slope Formula, The Empire Carpet Company orders merchandise for \\$17,700, including \\$550 in shipping charges, from Mohawk Carpet Mills on May 4. Carpets valued at \\$1,390 will be returned because they are damaged. The terms of sale are 2/10, n30 ROG. The shipment arrives, define the term linear inequality, Fantasia Florist Shop purchases an order of imported roses with a list price of \\$2,375 less trade discounts of 15/20/20. What is the dollar amount of the trade discount?, Equations with Distributive Property.\n\nWrite a word problem involving a quadratic function. 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What is the dollar amount of the trade discount.\n\nJava polynomial code, Free Advanced Algebra Calculator, solving for y in terms of x worksheet.\n\nProblem solving equations for 7 year old kids, define positive number, radical equation solver, The Empire Carpet Company orders merchandise for \\$17,700, including \\$550 in shipping charges, from Mohawk Carpet Mills on May 4. Carpets valued at \\$1,390 will be returned because they are damaged. The terms of sale are 2/10, n30 ROG. The shipment arrives on May 26 and Empire wants to take advantage of the cash discount. By what date must Empire pay the invoice?, simplifying ratio of polynomials calculator.\n\n6th grade practice exam dilation, dividing square roots with variables, real life problem using polynomials, show fraction bar graph all numbers, map of states around the mississippi river, tenths worksheets, a unit fraction is a fraction whose numerator is 1 and whose denominator is a natural number greater than 1. if three unit fractions with distinct single-digit denominators have a sum of 5/8, what is the sum of the denominators?.\n\nAlgebra 2 littell 7.2 practice A, algebra questions for year 8, First Order Non-homogeneous Differential Equation, factor tree of 44, a color printer can print 36 pages in 3 minutes and 108 pages in 9 minutes. if the number of pages varies directly with the time, at what rate is the color printer printing?, mixed number to percent calculator, gridded answer comparing two dorm size refrigerators.\n\nA pizza shop makes a profit of 1.50 for each small pizza, Algebra Formula Sheet, solve radical equations calculator, equivalent equations deffinition.\n\nSimplifying polynomials with negative exponents worksheet, COMPLEX FRACTION PROBLEM SOLVER, 30 workers complete a project in 20 days, evaluating expressions solver with mixed numbers.\n\nWhat are the zeroes of x(x-3)(x-2) then how do you graph, simplify algebra expressions using algebra tiles powerpoints, equation for inverse function.\n\nYahoo visitors came to this page yesterday by entering these keywords :" ]
[ null, "https://softmath.com/images/video-pages/solver-top.png", null ]
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https://origin.geeksforgeeks.org/4-plot/
[ "# 4-Plot\n\n• Last Updated : 02 Jul, 2021\n\nA  4-plot is a collection of 4 different graphical Exploratory Data Analysis (EDA) tools, whose main motive is to test the assumptions that underlie most measurement processes.\n\nThe 4-plot consists of the following:\n\n• Run plot: A run sequence plot is used to test fixed location and variations. It has the following axes:\n• Vertical axis: Yi\n• Horizontal axis: i\n• Lag Plot: Lag plot is a type of scatter plot with one variable is lagged of the other. Here, lag means the value of the variable after some fixed amount of time. A log plot can be used to test the randomness of the process and can give important information about the distribution of the process.\n• Vertical axis: Yi\n• Horizontal axis: Yi-k\n• Histogram: Histogram is the plot of values of data vs their frequency in the dataset. The histogram is used to know the distribution of the process i.e whether it is uniform, normal, etc.\n• Vertical axis: counts/frequency/probability.\n• Horizontal axis: Y\n• Normal Probability: Normal probability plot is used to know how close the process distribution to normal distribution.\n• Vertical axis: Ordered Yi\n• Horizontal axis: The theoretical values from the normal distribution N(0,1).\n\n4-plot can answer the following questions:\n\n• Is the process in control, stable and predictable?\n• Is the process drifting with respect to the location?\n• Is the process drifting with respect to the variation?\n• Are the data random?\n• Is the observation related to an adjacent observation?\n• If the distribution is not-random, then what is the distribution?\n• Is sample mean a good estimator for the process, if not what is a good estimator?\n\nSome assumption that can be verified with 4-plot are:\n\n• Random generation.\n• Fixed Distribution.\n• The distribution having a fixed location\n• The distribution having a fixed variation with time.\n\nThere are some underlying assumptions that follow the necessity for 4-plot:\n\n• If the fixed location assumption holds, then the run sequence plot will be flat and non-drifting.\n• If the fixed variation assumption holds then the vertical spread in the run sequence plot will be approximately the same over the entire horizontal axis.\n• If the randomness assumptions hold then the lag plot will not form any type of structure.\n• If the normal distribution assumption holds then the histogram will be bell-plot.\n\nIf all the above assumptions hold, then the process is in control.\n\n### Implementation:\n\n• In this implementation, we will also use statsmodels library as well as some common data science packages (Numpy, Pandas, and Seaborn). All these libraries are preinstalled in Colab and can be installed in the local environment with pip install.\n• For this code, we will be using a heat flow meter dataset. The dataset can be downloaded from here.\n\n## Python3\n\n `# code` `import` `pandas as pd` `import` `matplotlib.pyplot as plt` `import` `seaborn as sns` `import` `statsmodels.api as sm` `%``matplotlib inline`   `heat_flow ``=` `pd.read_csv(``'heat_flow.txt'``, header ``=` `None``)` ` `  `heat_flow.head()` `sns.set_style(``'darkgrid'``)`   `# plot different components of 4 plot` `fig, ax  ``=` `plt.subplots(``2``,``2``)` `sns.lineplot(x ``=` `pd.Series(heat_flow.index),y ``=` `heat_flow[``0``],ax ``=` `ax[``0``,``0``])`   `ax[``0``,``0``].set_title(``'Run Sequence Plot'``)` `pd.plotting.lag_plot(heat_flow[``0``],ax ``=` `ax[``0``,``1``])`   `ax[``0``,``1``].set_title(``'Lag Plot with k=1'``)` `sns.histplot(heat_flow[``0``],kde ``=` `True``,ax ``=` `ax[``1``,``0``])`   `ax[``1``,``0``].set_title(``'Histogram'``)` `sm.ProbPlot(heat_flow[``0``]).qqplot(line ``=``'s'``, ax ``=` `ax[``1``,``1``],color ``=` `'blue'``);`   `ax[``1``,``1``].set_title(``'Normal Probability Plot'``)` `plt.show()`\n\n``` 0\n0 9.206343\n1 9.299992\n2 9.277895\n3 9.305795\n4 9.275351```", null, "4-plot\n\n• We can infer from the above 4-plot that:\n• Here, the run sequence plot is quite flat and non-drifting. Hence, the fixed location assumption holds.\n• The run sequence plot also has a quite similar vertical spread. Hence, the fixed variation assumption hold.\n• Here, the lag plot does not generate any non-random pattern. Hence, we can assume that distribution is random.\n• Here, the histogram generates quite symmetric bell-curve distribution. Hence, the process is normally distributed.\n• Indeed, the above point can be confirmed with the normal probability plot generating scatter quite similar to normal distribution.\n\n### References:\n\nMy Personal Notes arrow_drop_up\nRecommended Articles\nPage :" ]
[ null, "https://media.geeksforgeeks.org/wp-content/uploads/20210122125819/Screenshot68-660x545.png", null ]
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https://arinjayacademy.com/convert-ratio-to-percentage/
[ "# Convert Ratio to Percentage\n\nTo convert Ratio to Percentage we have to follow following steps:\nStep 1 – Convert the Ratio into Fraction.\nStep 2 Multiply the Fraction by 100 and put the Percentage sign to the result (%)\n\n## Convert Ratio to Percentage Examples\n\nExample 1\n\nConvert 15 : 125 into a Percentage.\n\nExplanation:\n\nTo convert Ratio to Percentage we have to follow following steps:\nStep 1 – Convert the ratio into Fraction\n15 : 125 = 15/125\n\nStep 2 – Multiply the Fraction by 100 and put the Percentage sign to the result (%)\n( 15/125 x 100 ) %\n\nOn solving the given Fraction, we get,\n= 12 %\n\nExample 2\n\nConvert 12 : 96 into a Percentage.\n\nExplanation:\n\nTo convert Ratio to Percentage we have to follow following steps:\nStep 1 – Convert the ratio into Fraction\n12 : 96 = 12/96\n\nStep 2 – Multiply the Fraction by 100 and put the Percentage sign to the result (%)\n( 12/96 x 100 ) %\n\nOn solving the given Fraction, we get,\n= 12.5 %\n\nExample 3\n\nConvert 11 : 25 into a Percentage.\n\nExplanation:\n\nTo convert the given ratio into Percentage we have to follow following steps:\nStep 1 – Convert the ratio into Fraction\n11 : 25 = 11/25\n\nStep 2 – Multiply the Fraction by 100 and put the Percentage sign to the result (%)\n( 11/25 x 100 ) %\n\nOn solving the given Fraction, we get,\n= 44 %\n\nExample 4\n\nConvert 48 : 120 into a Percentage.\n\nExplanation:\n\nTo convert the given ratio into Percentage we have to follow following steps:\nStep 1 – Convert the ratio into Fraction\n48 : 120 = 48/120\n\nStep 2 – Multiply the Fraction by 100 and put the Percentage sign to the result (%)\n( 48/120 x 100 ) %\n\nOn solving the given Fraction, we get,\n= 40 %\n\nExample 5\n\nConvert 8 : 25 into a Percentage.\n\nExplanation:\n\nTo convert the given ratio into Percentage we have to follow following steps:\nStep 1 – Convert the ratio into Fraction\n8 : 25 = 8/25\n\nStep 2 – Multiply the Fraction by 100 and put the Percentage sign to the result (%)\n( 8/25 x 100 ) %\n\nOn solving the given Fraction, we get,\n= 32 %\n\nExample 6\n\nConvert 12 : 25 into a Percentage.\n\nExplanation:\n\nTo convert the given ratio into Percentage we have to follow following steps:\nStep 1 – Convert the ratio into Fraction\n12 : 25 = 12/25\n\nStep 2 – Multiply the Fraction by 100 and put the Percentage sign to the result (%)\n( 12/25 x 100 ) %\n\nOn solving the given Fraction, we get,\n= 48 %" ]
[ null ]
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http://sandlab.mit.edu/index.php/research/order-reduction-and-closure-of-turbulent-flows
[ "# Closure and order-reduction of turbulent dynamical systems\n\nTurbulent dynamical systems are characterized by both a large dimensional phase space and a large dimension of persistent or intermittent instabilities (i.e., a large number of positive Lyapunov exponents on the attractor). They are ubiquitous in many complex systems with fluid flow such as, engineering turbulence at high Reynolds numbers, confined plasmas, as well as atmospheric and oceanic turbulence (movie below).\n\nThe scope of this work is i) to design effective turbulent closure schemes that respect the synergistic activity between unstable linear dynamics, nonlinear energy transfers, and stable dynamics, which is apparent in turbulent systems, and ii) to develop order-reduction techniques that take into account the nonlinear energy transfers associated with the omitted modes.\n\nIn these systems the energy of the unstable modes is continuously balanced by nonlinear energy transfer mechanisms that absorb energy from these modes and pass it to the stable ones, resulting in this way, a statistical steady state with broad energy spectrum. From a statistical point view these nonlinear energy transfers are directly connected with the existence of non-Gaussian statistics. Thus, any attempt to design uncertainty quantification algorithms for these systems without taking explicitly into account these nonlinear and non-Gaussian features will result in numerically unstable schemes or schemes that severely underestimate the system energy (to the point where there are no unstable directions in the dynamics).\n\nStatically accurate Modified Quasilinear Gaussian (MQG) closure for turbulent dynamical systems\n\nWe develop a second-order closure methodology for uncertainty quantification in damped forced nonlinear systems with high dimensional phase-space that possess a high-dimensional chaotic attractor. We exploit exact statistical relations between second order correlations and third order moments in statistical equilibrium in order to decompose the energy flux at equilibrium into precise additional damping and enhanced noise on suitable modes, while preserving statistical symmetries; in the second stage, we develop a nonlinear MQG dynamical closure which has this statistical equilibrium behavior as a stable fixed point of the dynamics. The resulted UQ scheme provide very accurate estimates of second order statistics even far away from the tuned energy level. Below we observe a comparison of the MQG scheme with direct Monte-Carlo simulations for three different energetic regimes of the Lorenz-96 system. More details can be found here.\n\n•", null, "•", null, "• Numerical solutions of L-96 model in space–time for various energetic regimes\n• Comparison of exact (Monte-Carlo) and approximate (MQG) spectrum for various energetic regimes\n\nBlending MQG closure and non-Gaussian reduced subspace methods for turbulent systems\n\nEven though MQG provides with accurate second order statistics even in extreme excitation scenarios, for many applications it is important to know higher order statistical (i.e. expensive) information but only for specific subspaces. In this work we develop a framework that brings together i) inexpensive, second-order modeling for a wide part of the spectrum with ii) higher-order stochastic modeling for a small set of important (possibly adapting, i.e. DO) modes. The coupling of the two approaches is based on arguments involving the nonlinear energy transfers. In the figures below we present the application of this blended approach to the prototype turbulent system Lorenz-96. More details for this work can be found here.\n\n•", null, "•", null, "• Spectrum evolution using the blended UQ approach and comparison with Monte-Carlo\n• Recovery of the third order statistics only inside a specific subspace of interest and comparison with Monte-Carlo\n\nRadical order-reduction of turbulent systems using reduced-order MQG (ROMQG)\n\nIn both MQG and blended MQG-DO approaches the goal is to model the nonlinear energy fluxes without solving (in MQG) or fully-solving (in MQG-DO) the non-Gaussian character of the statistics (closure problem). Here we go a step further by using these models for the nonlinear energy fluxes to develop radical order reduction methods for turbulent systems, which, despite the very small number of modes considered, are energetically accurate. This is because, in contrast with other approaches, the emphasis is now given on modeling the energy fluxes to the reduced set of modes as accurate as possible. [Read more...]\n\nWe illustrate the ROMQG algorithm in a two-layer baroclinic turbulence flow with over 125,000 degrees of freedom (see movie on the top of the page as well as the figure below). The inexpensive ROMQG algorithm with 252 modes (0.2% of the total modes) is able to capture the nonlinear response of the energy, the heat flux, and even the one-dimensional, energy and heat flux spectrum at each wavenumber.\n\n•", null, "•", null, "•", null, "Publications\n\n`T. Sapsis, A. Majda, Statistically Accurate Low Order Models for Uncertainty Quantification in Turbulent Dynamical Systems, Proceedings of the National Academy of Sciences, 110 (2013) 13705-13710. [pdf]`\n`T. Sapsis, A. Majda, Blending modified Gaussian closure and non-Gaussian reduced subspace methods for turbulent dynamical systems, Journal of Nonlinear Science, DOI 10.1007/s00332-013-9178-1 (2013). [pdf]`\n`T. Sapsis, A. Majda, Blended reduced subspace algorithms for uncertainty quantification of quadratic systems with a stable mean state, Physica D, 258 (2013) 61. [pdf]`\n`T. Sapsis, A. Majda, A statistically accurate modified quasilinar Gaussian closure for uncertainty quantification in turbulent dynamical systems, Physica D, 252 (2013) 34. [pdf]`" ]
[ null, "http://sandlab.mit.edu/images/article_images/Turbulence_MQG/Lorenz_96_response.png", null, "data:image/gif;base64,R0lGODlhAQABAJEAAAAAAP///////wAAACH5BAEHAAIALAAAAAABAAEAAAICVAEAOw==", null, "http://sandlab.mit.edu/images/article_images/Turbulence_MQG/MQG_DO_spectrum.png", null, "data:image/gif;base64,R0lGODlhAQABAJEAAAAAAP///////wAAACH5BAEHAAIALAAAAAABAAEAAAICVAEAOw==", null, "http://sandlab.mit.edu/images/article_images/Turbulence_MQG/vorticity_fields.png", null, "http://sandlab.mit.edu/images/article_images/Turbulence_MQG/Turbu_MQG_diagram.png", null, "http://sandlab.mit.edu/images/article_images/Turbulence_MQG/Turbu_MQG_spectrum.png", null ]
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https://androidkt.com/save-keras-training-history-object-to-file-using-callback/
[ "You can learn a lot about Keras models by observing their History objects after training. In this post, you will discover how you can save the history object into a CSV file of deep learning models training metrics over time during training.\n\nHistory callback is the default callback that is registered when training models. It records training metrics for each epoch. This includes the loss and the accuracy for the training dataset as well as the loss and accuracy for the validation dataset. Metrics are stored in a dictionary in the history member of the object returned.\n\nThe code below loads the CIFAR-10 dataset using the Keras API.\n\n```(x_train, y_train), (x_val, y_val) = tf.keras.datasets.cifar10.load_data()\n\nx_train = x_train.astype('float32')\nx_val = x_val.astype('float32')\nx_train /= 255\nx_val /= 255\n\nBATCH_SIZE=32\n```\n\nThe following code defines a simple convolutional neural network for image classification using a common pattern a stack of Conv2D and MaxPooling2D layers.\n\n```model = tf.keras.models.Sequential()\nmodel.add(layers.Conv2D(32, (3, 3), activation=tf.keras.layers.LeakyReLU(alpha=0.2), input_shape=(32, 32, 3)))\n\n```\n\n## Create CSVLOGGER Callback\n\nKeras provides the capability to register callbacks when training a model. It is an object that can perform actions at various stages of training like at the start or end of an epoch, before or after a single batch, etc.\n\n```filename='log.csv'\nhistory_logger=tf.keras.callbacks.CSVLogger(filename, separator=\",\", append=True)\n```\n\nThis callback streams epoch results to a CSV file. If append is “True” then it appends if the file exists. It is useful for continuing training. otherwise, overwrite the existing file. This callback supports all values that can be represented as a string, including 1D iterables such as np.ndarray.\n\nYou can pass this callback as the keyword argument callbacks to the .fit() method of a model:\n\n```history_const=model.fit(x_train, y_train,\nbatch_size=BATCH_SIZE,\nepochs=epochs,\ncallbacks=[history_logger],\nvalidation_data=(x_val, y_val),\nshuffle=True)\n```\n\nThe above code saves model history training in form of a datasheet file log.csv.\n\n## Save and load History object With Numpy\n\nA history object has a history field, it is a dictionary that holds different training metrics spanned across every training epoch. So e.g. history.history[‘loss’] will return a loss of your model in the 10th epoch of training. In order to save that you could pickle this dictionary.\n\n```np.save('history1.npy',history_const.history)" ]
[ null ]
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https://nerdparadise.com/programming/pygame/part4
[ "Just like the mixer module, the drawing API is fairly straightforward with a few examples. Therefore instead of re-iterating the documentation as part of this tutorial, I'll instead show you a few simple (and not-so-simple) examples of what can be doing with the draw module in PyGame and a few pitfalls to be aware of. At the end of this tutorial/demo you'll see a massive code dump of a sample application. Simply run this script and you'll be presented with a PyGame app that is a sequence of draw module demos.\n\nWhile running it, press spacebar to proceed through the demos.\n\n## Demo 1: Rectangle\n\npygame.draw.rect(surface, color, pygame.Rect(left, top, width, height))", null, "## Demo 2: Circle", null, "## Demo 3: Built in Outlines:\n\nThis is the first caveat you should be aware of. PyGame's method for creating \"thicker\" outlines for circles is to draw multiple 1-pixel outlines. In theory, it sounds okay, until you see the result:", null, "The circle has noticeable pixel gaps in it. Even more embarrassing is the rectangle, which uses 4 line-draw calls at the desired thickness. This creates weird corners.\n\nThe way to do this for most drawing API calls is to pass in an optional last parameter which is the thickness.\n# draw a rectangle\npygame.draw.rect(surface, color, pygame.Rect(1010100100), 10)\n# draw a circle\npygame.draw.circle(surface, color, (30060), 5010)\n\nMoral of the story: when you draw a polygon, rectangle, circle, etc, draw it filled in or with 1-pixel thickness. Everything else is not very well implemented.\n\n## Demo 4: Acceptable Outlines\n\nIf you must draw a rectangle that has 10-pixel-thick borders, then it's best that you re-implement the logic yourself with either 10 1-pixel-thick rectangle calls, or 4 10-pixel-thick rectangle calls for each side.", null, "For an example, see the do_nice_outlines function below.\n\n## Demo 5: Polygons\n\nThis API is pretty straightforward. The point list is a list of tuples of x-y coordinates for the polygon.", null, "pygame.draw.polygon(surface, color, point_list)\n\n## Demo 6: Lines\n\nLines are also straight-forward:\npygame.draw.line(surface, color, (startX, startY), (endX, endY), width)\n\nSo I decided to go a bit crazy and wrote a 3D spinning wireframe cube using the line method and a lot of math.", null, "import pygame\nimport math\nimport time\n\n# Ignore these 3 functions. Scroll down for the relevant code.\n\ndef create_background(width, height):\ncolors = [(255255255), (212212212)]\nbackground = pygame.Surface((width, height))\ntile_width = 20\ny = 0\nwhile y < height:\nx = 0\nwhile x < width:\nrow = y // tile_width\ncol = x // tile_width\npygame.draw.rect(\nbackground,\ncolors[(row + col) % 2],\npygame.Rect(x, y, tile_width, tile_width))\nx += tile_width\ny += tile_width\nreturn background\n\ndef is_trying_to_quit(event):\npressed_keys = pygame.key.get_pressed()\nalt_pressed = pressed_keys[pygame.K_LALT] or pressed_keys[pygame.K_RALT]\nx_button = event.type == pygame.QUIT\naltF4 = alt_pressed and event.type == pygame.KEYDOWN and event.key == pygame.K_F4\nescape = event.type == pygame.KEYDOWN and event.key == pygame.K_ESCAPE\nreturn x_button or altF4 or escape\n\ndef run_demos(width, height, fps):\npygame.init()\nscreen = pygame.display.set_mode((width, height))\npygame.display.set_caption('press space to see next demo')\nbackground = create_background(width, height)\nclock = pygame.time.Clock()\ndemos = [\ndo_rectangle_demo,\ndo_circle_demo,\ndo_horrible_outlines,\ndo_nice_outlines,\ndo_polygon_demo,\ndo_line_demo\n]\nthe_world_is_a_happy_place = 0\nwhile True:\nthe_world_is_a_happy_place += 1\nfor event in pygame.event.get():\nif is_trying_to_quit(event):\nreturn\nif event.type == pygame.KEYDOWN and event.key == pygame.K_SPACE:\ndemos = demos[1:]\nscreen.blit(background, (00))\nif len(demos) == 0:\nreturn\ndemos(screen, the_world_is_a_happy_place)\npygame.display.flip()\nclock.tick(fps)\n\n# Everything above this line is irrelevant to this tutorial.\n\ndef do_rectangle_demo(surface, counter):\nleft = (counter // 2) % surface.get_width()\ntop = (counter // 3) % surface.get_height()\nwidth = 30\nheight = 30\ncolor = (1280128# purple\n\n# Draw a rectangle\npygame.draw.rect(surface, color, pygame.Rect(left, top, width, height))\n\ndef do_circle_demo(surface, counter):\nx = surface.get_width() // 2\ny = surface.get_height() // 2\nmax_radius = min(x, y) * 4 // 5\nradius = abs(int(math.sin(counter * 3.14159 * 2 / 200) * max_radius)) + 1\ncolor = (0140255# aquamarine\n\n# Draw a circle\n\ndef do_horrible_outlines(surface, counter):\ncolor = (25500# red\n\n# draw a rectangle\npygame.draw.rect(surface, color, pygame.Rect(1010100100), 10)\n\n# draw a circle\npygame.draw.circle(surface, color, (30060), 5010)\n\ndef do_nice_outlines(surface, counter):\ncolor = (01280# green\n\n# draw a rectangle\npygame.draw.rect(surface, color, pygame.Rect(101010010))\npygame.draw.rect(surface, color, pygame.Rect(101010100))\npygame.draw.rect(surface, color, pygame.Rect(1001010100))\npygame.draw.rect(surface, color, pygame.Rect(1010010010))\n\n# draw a circle\ncenter_x = 300\ncenter_y = 60\niterations = 150\nfor i in range(iterations):\nang = i * 3.14159 * 2 / iterations\nx = center_x + dx\ny = center_y + dy\npygame.draw.circle(surface, color, (x, y), 5)\n\ndef do_polygon_demo(surface, counter):\ncolor = (2552550# yellow\n\nnum_points = 8\npoint_list = []\ncenter_x = surface.get_width() // 2\ncenter_y = surface.get_height() // 2\nfor i in range(num_points * 2):\nif i % 2 == 0:\nang = i * 3.14159 / num_points + counter * 3.14159 / 60\nx = center_x + int(math.cos(ang) * radius)\ny = center_y + int(math.sin(ang) * radius)\npoint_list.append((x, y))\npygame.draw.polygon(surface, color, point_list)\n\ndef rotate_3d_points(points, angle_x, angle_y, angle_z):\nnew_points = []\nfor point in points:\nx = point\ny = point\nz = point\nnew_y = y * math.cos(angle_x) - z * math.sin(angle_x)\nnew_z = y * math.sin(angle_x) + z * math.cos(angle_x)\ny = new_y\n# isn't math fun, kids?\nz = new_z\nnew_x = x * math.cos(angle_y) - z * math.sin(angle_y)\nnew_z = x * math.sin(angle_y) + z * math.cos(angle_y)\nx = new_x\nz = new_z\nnew_x = x * math.cos(angle_z) - y * math.sin(angle_z)\nnew_y = x * math.sin(angle_z) + y * math.cos(angle_z)\nx = new_x\ny = new_y\nnew_points.append([x, y, z])\nreturn new_points\n\ndef do_line_demo(surface, counter):\ncolor = (000# black\ncube_points = [\n[-1, -11],\n[-111],\n,\n[1, -11],\n[-1, -1, -1],\n[-11, -1],\n[11, -1],\n[1, -1, -1]]\n\nconnections = [\n(01),\n(12),\n(23),\n(30),\n(45),\n(56),\n(67),\n(74),\n(04),\n(15),\n(26),\n(37)\n]\n\nt = counter * 2 * 3.14159 / 60 # this angle is 1 rotation per second\n\n# rotate about x axis every 2 seconds\n# rotate about y axis every 4 seconds\n# rotate about z axis every 6 seconds\npoints = rotate_3d_points(cube_points, t / 2, t / 4, t / 6)\nflattened_points = []\nfor point in points:\nflattened_points.append(\n(point * (1 + 1.0 / (point + 3)),\npoint * (1 + 1.0 / (point + 3))))\n\nfor con in connections:\np1 = flattened_points[con]\np2 = flattened_points[con]\nx1 = p1 * 60 + 200\ny1 = p1 * 60 + 150\nx2 = p2 * 60 + 200\ny2 = p2 * 60 + 150\n\n# This is the only line that really matters\npygame.draw.line(surface, color, (x1, y1), (x2, y2), 4)\n\nrun_demos(40030060)\n\nNext up: Fonts and Text\n\nHey, there, Python folks. Hope you enjoyed the post. I just wanted to give a quick shout-out for a weekly Python code golf that I recently started up over on StringLabs.io. If you like Python puzzles please come check it out!" ]
[ null, "https://nerdparadise.com/images/programming/pygame/tutorial_draw_rect.png", null, "https://nerdparadise.com/images/programming/pygame/tutorial_draw_circle.png", null, "https://nerdparadise.com/images/programming/pygame/tutorial_draw_outline_1.png", null, "https://nerdparadise.com/images/programming/pygame/tutorial_draw_outline_2.png", null, "https://nerdparadise.com/images/programming/pygame/tutorial_draw_polygon.png", null, "https://nerdparadise.com/images/programming/pygame/tutorial_draw_line.png", null ]
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