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https://fr.slideshare.net/sonangrai/data-mining-approaches-and-methods-108692929
[ "# Data mining approaches and methods\n\n5 Aug 2018", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "", null, "1 sur 85\n\n### Data mining approaches and methods\n\n• 1. Data mining techniques and tasks Prepared by : Prabesh Pradhan\n• 2. The process of collecting, searching through, and analyzing a large amount of data in a database, as to discover patterns or relationships • Extraction of useful patterns from data sources, e.g., databases, data warehouses, web. • Patterns must be valid, novel, potentially useful, understandable. DATA MINING\n• 3. DATA MINING MODELS AND TASKS\n• 4. Predictive:- It makes prediction about values of data using known results from different data or based on historical data. Descriptive:- It identifies patterns or relationship in data, it serves as a way to explore properties of data.\n• 5. Data mining tasks The process of collecting, searching through, and analyzing a large amount of data in a database, as to discover patterns or relationships  Extraction of useful patterns from data sources,e.g. databases, data warehouses, web.  Patterns must be valid, novel, potentially useful, understandable.\n• 6. CLASSIFICATION  Classification derives a model to determine the class of an object based on its attributes.  Given a collection of records, each record contains a set of attributes, one of the attributes is the class.  For eg: pattern recognition\n• 7. • The value of attribute is examined as it varies over time. • A time series plot is used to visualize time series. • Ex:- stock exchange TIME SERIES ANALAYSIS\n• 8. • Clustering is the task of segmenting a diverse group into a number of similar subgroups or clusters. • Most similar data are grouped in clusters • Ex:-Bank customer CLUSTERING\n• 9. • Abstraction or generalization of data resulting in a smaller set which gives general overview of a data. • alternatively,summary type information can be derived from data. SUMMARIZATION\n• 10. Data mining techniques  Association  Classification  Clustering  Prediction  Sequential Patterns  Decision trees\n• 11. Association  The pattern is discovered based on a relationship between items in the same transaction  The association technique is also known as relation technique  The association technique is used in market basket analysis to identify a set of products that customers frequently purchase together.\n• 12. Classification  It classify each item in a set of data into one of a predefined set of classes or groups.  It makes use of mathematical techniques such as decision trees, linear programming, neural network, and statistics  We develop the software that can learn how to classify the data items into groups.  For example, we can apply classification in the application that “given all records of employees who left the company, predict who will probably leave the company in a future period.”\n• 13. Clustering  It makes a meaningful or useful cluster of objects which have similar characteristics using the automatic technique.  The clustering technique defines the classes and puts objects in each class, while in the classification techniques, objects are assigned into predefined classes.\n• 14. Prediction  The prediction analysis technique can be used in the sale to predict profit for the future if we consider the sale is an independent variable, profit could be a dependent variable.  It is based on the historical sale and profit data, we can draw a fitted regression curve that is used for profit prediction\n• 15. Sequential patterns  It seeks to discover or identify similar patterns, regular events or trends in transaction data over a business period.  Eg: In sales, with historical transaction data, businesses can identify a set of items that customers buy together different times in a year. Then businesses can use this information to recommend customers buy it with better deals based on their purchasing frequency in the past.\n• 16. Classification and prediction Prepared by : Sonahang Rai\n• 17. Decision Tree  It is a classification scheme which generates a tree and a set of rules from given data set.  A decision tree consist of root node, edges and leaf.  Each internal node denotes a test on an attribute.  Each branch node denotes outcome of the test.  Each leaf node holds the class label.\n• 18. Decision tree example\n• 19. ID3 algorithm i. Calculate the entropy of every attribute using the dataset. ii. Split the set into subsets using the attribute for which entropy is minimum(or information gain is maximum) iii. Make a decision tree node containing that attribute iv. Recurse on subset using remaining attributes\n• 20. Entropy  Info(D)=- 𝑖=1 𝑚 𝑝𝑖 𝑙𝑜𝑔2 (𝑝𝑖) where D=number of rows 𝑝𝑖 = class/D  𝐼𝑛𝑓𝑜 𝐴(D)= 𝑗=1 𝑣 |𝐷 𝑗| 𝐷 ∗ 𝐼𝑛𝑓𝑜(𝑑) Information gain  Gain(A)=Info(d)- 𝐼𝑛𝑓𝑜 𝐴(D)\n• 21. ID3 example\n• 22. Finding entropy and gain  Finding info(d) Info(D)= - 9 14 𝑙𝑜𝑔2( 9 14 )- 5 14 𝑙𝑜𝑔2( 5 14 )= 0.940 bits  Finding for age 𝐼𝑛𝑓𝑜 𝑎𝑔𝑒(D)= 5 14 * (- 2 5 𝑙𝑜𝑔2( 2 5 )- 3 5 𝑙𝑜𝑔2( 3 5 ))+ 4 14 * (- 4 4 𝑙𝑜𝑔2( 4 4 )- 0 4 𝑙𝑜𝑔2( 0 4 ))+ 5 14 * (- 3 5 𝑙𝑜𝑔2( 3 5 )- 2 5 𝑙𝑜𝑔2( 2 5 )) = 0.694 bits Thus, Gain(age)=Info(D)- 𝐼𝑛𝑓𝑜 𝑎𝑔𝑒(D)=0.945-0.694=0.246 bits Similarly we can find gain of all other attributes. Gain(income)=0.029,Gain(student)=0.151,Gain(credit_rating)=0.048 Among all the gains the gain of age is the maximum thus it is taken as the root node.\n• 23. Rule Based Classification  It uses the set of IF-THEN rules for the classification.  IF-THEN rule is an expression of the form IF condition THEN conclusion.  IF part is called rule antecedent or precondition, it can consist of one or more attributes test.  THEN part is called rule consequent, it consist a class prediction. Ex: R1:IF age=youth and student=yes THEN buys_computer=yes Or R1: (age=youth)Λ(student=yes)=>(buys_computer=yes)\n• 24.  A rule R can be assessed by its coverage and accuracy –Given a tuple X from a data D –Let n cover: # of tuples covered by R –n correct: # of tuples correctly classify by R –|D|: # of tuples in D Coverage(R)= 𝑛 𝑐𝑜𝑣𝑒𝑟𝑠 |𝐷| Accuracy(R)= 𝑛 𝑐𝑜𝑟𝑟𝑒𝑐𝑡 𝑛 𝑐𝑜𝑣𝑒𝑟𝑠\n• 25. R: IF age=youth AND student=yes THEN buys_computer=yes |D| = 14 N cover = 2 N correct = 2 Coverage(R)= 2 14 =14.25% Correct(R)= 2 2 =100%\n• 26. Rules extraction from the decision tree  One rule is created for each path from the root to a leaf node  Each splitting criterion is logically AND to form the rule antecedent (IF part)  Leaf node holds the class prediction for rule consequent (THEN part)  Logical OR is implied between each of the extracted rules\n• 28. Genetic algorithm  It is used for finding optimized solutions to search problems.  It is based on the theory of natural selection and evolution of biology. Selection: Survival of the fittest Evolution: Origin of species from a common descendent  It is excellent in searching large and complex data sets.\n• 29.  Gene: A part of chromosome.  Chromosome: A set of gene.  Population : No of individuals present with same length of chromosome.  Fitness: It is the value assigned to individual.  Fitness function: Function which assigns fitness value.  Selection: Selecting values for next generation.  Mutation: Changing a random gene.\n• 30. Algorithm 1. Generate random population of n chromosomes 2. Evaluate the fitness of each chromosome in the population 3. Select two parent chromosomes from a population according to their fitness 4. With a crossover probability cross over the parents to form a new offspring. 5. With a mutation probability mutate new offspring . 6. If the end condition is satisfied, stop, and return the best solution in current population\n• 31. Linear Regression  It is a data mining technique used to predict a range of numeric values (also called continuous values), given a particular dataset.  It is used to estimate a relationship between two variables.  Here involves a response/dependent variable y and a single predictor/independent variable x y = 𝑤𝑜+ 𝑤1 x where 𝑤𝑜 (y-intercept) and 𝑤1 (slope) are regression coefficients\n• 32. X years experience Y salary(in \\$ 1000s) 3 30 8 57 9 64 13 72 3 36 6 43 11 59 21 90 1 20 16 83\n• 33. Non-linear regression, Association and frequent pattern Prepared by : Biplap Bhattarai\n• 34. • Often the relationship between x and y cannot be approximated with a straight line. In this case, a nonlinear regression technique may be used. • Alternatively, the data could be preprocessed to make the relationship linear. • Most Non-linear models can be modeled by polynomial regression model can be transformed into linear regression model. • For Example: Y=w0+w1x+w2x2 +w3x3 +w4x4 Non- Linear Regression:\n• 35. • For Example: Y=w0+w1x+w2x2 +w3x3 +w4x4 Convertible to Linear with new Variables: X2= x2,x3=x3,x4=x4 Y=w0+w1x1+w2x2 +w3x3 +w4x4 Which is easily solved by method of least squares using software for regression analysis. Non- Linear Regression:\n• 36. Association Rules: Detects sets of attributes that frequently co-occur, and rules among them, e.g. 90% of the people who buy cookies, also buy milk (60% of all grocery shoppers buy both) Frequent Pattern: Frequent Pattern is a pattern (a set of items, subsequences) that occurs frequently in a dataset. For example, a set of items, such as milk and bread, that appear frequently together in a transaction data set, is a frequent itemset. A subsequence, such as buying first a PC, then a digital camera, and then a memory card, if it occurs frequently in a shopping history database, is a (frequent) sequential pattern. Data Mining Techniques\n• 37. Association Rule Mining: Association rule mining is a procedure which is meant to find frequent patterns, correlations, associations or casual structures from datasets found in various kind of databases (relational, transactional). Data Mining Techniques\n• 38. The Apriori Principle: If an itemset is frequent, then all of its subsets must also be frequent. Conversely, if an subset is infrequent, then all of its supersets must be infrequent, too. • Apriori uses a \"bottom up\" approach, where frequent subsets are extended one item at a time (a step known as candidate generation, and groups of candidates are tested against the data. • Apriori is designed to operate on database containing transactions (for example, collections of items bought by customers, or details of a website frequentation). DEFINITION OF APRIORI ALGORITHM\n• 39. • Apriori principle holds due to the following property of the support measure:∀X,Y:(X⊂Y)→s(X)≥s(Y) • For all x,y if x is the subset of y implies support of x is greater or equal to support of y. DEFINITION OF APRIORI ALGORITHM\n• 40. • Frequent Itemsets: All the sets which contain the item with the minimum support (denoted by Li For ith itemset) • Apriori Property: Any subset of frequent itemset must be frequent. • Join Operation: To find lk, a set of candidate k-itemsets is generated by joining Lk-1 with itself KEY CONCEPTS\n• 41. Given minimum required support s : 1. Search for all individual elements (1 element item set) that have a minimum support of s 2. Repeat 2.1From the result of the previous search for i-element item-sets, search for all i+1 element item-sets that have a minimum support of s 2.2 This becomes the sets of all frequent (i+1) element item-sets that are interesting 3. Until item-set size reaches maximum The Apriori Algorithm\n• 42. The Frequent itemsets are items in L1, L2, L3\n• 43. Pros of the Apriori algorithm • It is an easy-to-implement and easy-to-understand algorithm. • It can be used on large itemsets. Cons of the Apriori Algorithm • Sometimes, it may need to find a large number of candidate rules which can be computationally expensive. • Calculating support is also expensive because it has to go through the entire database. The Apriori Algorithm\n• 44. FP tree algorithm, which use to identify frequent patterns in the area of Data Mining. The Frequent Pattern Tree (FP-Tree) is a compact structure that stores quantitative information about frequent patterns in a database. Frequent Pattern Tree (FP Tree)\n• 45. 1. One root labeled as “null” with a set of item-prefix subtrees as children 2. Each node in the item-prefix subtree consists of three fields: i. Item-name: registers which item is represented by the node; ii. Count: the number of transactions represented by the portion of the path reaching the node; iii. Node-link: links to the next node in the FP-tree carrying the same item- name, or null if there is none. Frequent Pattern Tree (FP Tree)\n• 46. 1. Question :Find all frequent itemsets or frequent patterns in the following database using FP-growth algorithm. Take minimum support as 30%. Frequent Pattern Tree (FP Tree)\n• 47. Step 1 - Calculate Minimum support First should calculate the minimum support count. Question says minimum support should be 30%. It calculate as follows: Minimum support count(30/100 * 8) = 2.4 As a result, 2.4 appears but to empower the easy calculation it can be rounded to to the ceiling value. Now, Minimum support count is ceiling(30/100 * 8) = 3 Frequent Pattern Tree (FP Tree)\n• 48. Step 2 - Find frequency of occurrence Now time to find the frequency of occurrence of each item in the Table. For example, item A occurs in row 1,row 2,row 3,row 4 and row 7. Totally 5 times occurs in the Database table. You can see the counted frequency of occurrence of each item in Table below . Frequent Pattern Tree (FP Tree)\n• 49. Step 3 - Prioritize the items In Table 2 you can see the numbers written in Red pen. Those are the priority of each item according to it's frequency of occurrence. Item B got the highest priority (1) due to it's highest number of occurrences. At the same time you have opportunity to drop the items which not fulfill the minimum support requirement .For instance, if Table contain F which has frequency 1, then you can drop it. Frequent Pattern Tree (FP Tree)\n• 50. Step 4 -Order the items according to priority As you see in the Table below new column added to the Table before. In the Ordered Items column all the items are queued according to it's priority, which mentioned in the Red ink in Table. For example, in the case of ordering row 1, the highest priority item is B and after that D, A and E respectively. Frequent Pattern Tree (FP Tree)\n• 51. Row 1: Note that all FP trees have 'null' node as the root node. So draw the root node first and attach the items of the row 1 one by one respectively. And write their occurrences in front of it. Frequent Pattern Tree (FP Tree)\n• 52. Row 2: Then update the above tree by entering the items of row 2. Then without creating another branch you can go through the previous branch up to E and then you have to create new node after that for C. (When you going through the branch second time you should erase one and write two for indicating the two times you visit to that node. If you visit through three times then write three after erase two.) Figure 2 shows the FP tree after adding row 1 and row 2. Frequent Pattern Tree (FP Tree)\n• 53. Row 3: In row 3 you have to visit B,A,E and C respectively. So you may think you can follow the same branch again by replacing the values of B,A,E and C. But you can't do that you have opportunity to come through the B. But can't connect B to existing A overtaking D. As a result you should draw another A and connect it to B and then connect new E to that A and new C to new E. Frequent Pattern Tree (FP Tree)\n• 54. Row 4: Then row 4 contain B,D,A. Now we can just rename the frequency of occurrences in the existing branch. As B:4,D,A:3. Row 5: In fifth raw have only item D. Now we have opportunity draw new branch from 'null' node. Frequent Pattern Tree (FP Tree)\n• 55. Row 6:B and D appears in row 6. So just change the B:4 to B:5 and D:3 to D:4. Row 7: Attach two new nodes A and E to the D node which hanging on the null node. Then mark D,A,E as D:2,A:1 and E:1. Row 8 : Attach new node C to B. Change the traverse times.(B:6,C:1) Frequent Pattern Tree (FP Tree)\n• 56. Step 6 - Validation After the five steps the final FP tree as follows: How we know is this correct? Now count the frequency of occurrence of each item of the FP tree and compare it with Table. If both counts equal, then it is positive point to indicate your tree is correct. Frequent Pattern Tree (FP Tree)\n• 57. • FP Growth Stands for frequent pattern growth • It is a scalable technique for mining frequent pattern in a database • After constructing the FP-Tree it’s possible to mine it to find the complete set of frequent patterns • FP growth improves Apriority to a big extent • Frequent Item set Mining is possible without candidate generation • Only “two scan” to the database is needed FP-Growth\n• 58. Simply a two step procedure – Step 1: Build a compact data structure called the FP-tree Built using 2 passes over the data-set. – Step 2: Extracts frequent item sets directly from the FP- tree FP-Growth Algorithm Process\n• 59. FP-Growth Example: Example: With Min Support 3 FP-Tree\n• 60. FP-Growth Example: For T: We Start with drawing tree whose end nodes are Ts, Keeping only support of T\n• 61. FP-Growth Example: We Take out T one by one, and as we do so, we push its support to every node up the chain to the root that was part of the same transaction in which T was:\n• 62. FP-Growth Example: As, D is infrequent (min support=3), so we remove D Itemset={C,T},{W,T},{A,T},{C,W,T}, {C,A,T},{W,A,T},{T}\n• 63. FP-Growth Example: We Then, starting from main fp-tree, we consider each item that appears in the tree and create new FP-trees for C, W, A, and D.\n• 64. Market Basket Analysis • Market Basket Analysis is a modelling technique based upon the theory that if you buy a certain group of items, you are more (or less) likely to buy another group of items. • For example, if you are in an US, and purchase Diaper, Milk then you are likely to buy beer. • The set of items a customer buys is referred to as an itemset, and market basket analysis seeks to find relationships between purchases.\n• 65. Market Basket Analysis • Typically the relationship will be in the form of a rule: • IF {milk, diaper} THEN {beer}. • The probability that a customer will buy milk without a diaper or vice versa is referred to as the support for the rule. The conditional probability that a customer will purchase beer is referred to as the confidence.\n• 66. How is it used? • In retailing, most purchases are bought on impulse. Market basket analysis gives clues as to what a customer might have bought if the idea had occurred to them . • Market basket analysis can be used in deciding the location and promotion of goods inside a store.\n• 67. How is it used? • In retailing, most purchases are bought on impulse. Market basket analysis gives clues as to what a customer might have bought if the idea had occurred to them . • Market basket analysis can be used in deciding the location and promotion of goods inside a store.\n• 68. Types: • There are two main types of MBA: • Predictive MBA is used to classify cliques of item purchases, events and services that largely occur in sequence. • Differential MBA removes a high volume of insignificant results and can lead to very in-depth results. It compares information between different stores, demographics, seasons of the year, days of the week and other factors.\n• 69. Clustering Prepared by : Trilok Pratap Kafle\n• 70. Clustering Cluster :- Cluster is a group of objects that belongs to the same class. similar objects are grouped in one cluster and dissimilar objects are grouped in another cluster. Clustering is the process of making a group of abstract(something different) objects into classes of similar objects.\n• 71. Application of cluster analysis  Clustering can help marketers discover distinct groups in their customer base. And they can characterize their customer groups based on the purchasing patterns.  Clustering analysis is broadly used in many applications such as market research, pattern recognition, data analysis, and image processing.  Clustering also helps in classifying documents on the web for information discovery.\n• 72. Clustering methods  Partitioning method  Hierarchical method\n• 73. Partitioning method  Suppose we are given a database of ‘n’ objects and the partitioning method constructs ‘k’ partition of data. Each partition will represent a cluster and k ≤ n. It means that it will classify the data into k groups, which satisfy the following requirements −  Each group contains at least one object.  Each object must belong to exactly one group. Types of Partitioning method 1. K-mean 2. K-medoids\n• 74. K-mean  K-Means is one of the most popular \"clustering\" algorithms.  K-means stores K centroids that it uses to define clusters.  A point is considered to be in a particular cluster if it is closer to that cluster's centroid than any other centroid.\n• 75. Steps in K-mean 1. Partition objects into k nonempty subsets 2. Compute seed points as the centroids of the clusters of the current partition. Centroid is the centre (mean point) of the cluster. 3. Assign each object to the cluster with the nearest seed point. 4. Go back to Step 2, stop when no more new assignment.\n• 76. =>2, 3, 6, 8, 9, 12, 15, 18, 22 – break into 3 clusters – Cluster 1 - 2, 12, 18 – mean = 10.6 – Cluster 2 - 6, 9, 22 – mean = 12.3 – Cluster 3 – 3, 8, 15 – mean = 8.6 • Re-assign – Cluster 1 - mean = 0 – Cluster 2 – 12, 15, 18, 22 - mean = 16.75 – Cluster 3 – 2, 3, 6, 8, 9 – mean = 5.6 • Re-assign – Cluster 1 – 2 – mean = 2 – Cluster 2 – 12, 15, 18, 22 – mean = 16.75 – Cluster 3 = 3, 6, 8, 9 – mean = 6.5 Re-assign – Cluster 1 – 2, 3 – mean = 2.5 – Cluster 2 – 12, 15, 18, 22 – mean = 16.75 – Cluster 3 – 6, 8, 9 – mean = 7.6 • Re-assign – Cluster 1 – 2, 3 – mean = 2.5 – Cluster 2 – 12, 15, 18, 22 - mean = 16.75 – Cluster 3 – 6, 8, 9 – mean = 7.6 • No change, so we’re done\n• 77. K-Mediods  It is also a algorithm which breaks the data sets into group.  It also attempt to minimize the distance between points labeled to be the cluster of that cluster.  Data point is taken as center and work with a generalization of the Manhattan Norm.\n• 79. Hierarchical Method Hierarchical clustering, also known as hierarchical cluster analysis, is an algorithm that groups similar objects into groups called clusters. The endpoint is a set of clusters, where each cluster is distinct from each other cluster, and the objects within each cluster are broadly similar to each other. For example, all files and folders on the hard disk are organized in a hierarchy. There are two types of hierarchical clustering:- 1. Divisive 2. Agglomerative\n• 80. Divisive Method In divisive or top-down clustering method we assign all of the observations to a single cluster and then partition the cluster to two least similar clusters. Finally, we proceed recursively on each cluster until there is one cluster for each observation. There is evidence that divisive algorithms produce more accurate hierarchies than agglomerative algorithms in some circumstances but is conceptually more complex.\n• 82. Agglomerative Method In agglomerative or bottom-up clustering method we assign each observation to its own cluster. Then, compute the similarity (e.g., distance) between each of the clusters and join the two most similar clusters. Repeat the process until there is only a single cluster left. Before any clustering is performed, it is required to determine the proximity matrix containing the distance between each point using a distance function. Then, the matrix is updated to display the distance between each cluster. The following three methods differ in how the distance between each cluster is measured.\n• 83. Single Linkage In single linkage hierarchical clustering, the distance between two clusters is defined as the shortest distance between two points in each cluster. For example, the distance between clusters “r” and “s” to the left is equal to the length of the arrow between their two closest points. Complete Linkage In complete linkage hierarchical clustering, the distance between two clusters is defined as the longest distance between two points in each cluster. For example, the distance between clusters “r” and “s” to the left is equal to the length of the arrow between their two furthest points.\n• 84. Average Linkage In average linkage hierarchical clustering, the distance between two clusters is defined as the average distance between each point in one cluster to every point in the other cluster. For example, the distance between clusters “r” and “s” to the left is equal to the average length each arrow between connecting the points of one cluster to the other.\n\n### Notes de l'éditeur\n\n1. Correlations:- a mutual relationship or connection between two or more things. // interdependence of variable quantities. The causal relations between points are interpreted as describing which events in spacetime can influence which other events. A data set (or dataset) is a collection of data. Most commonly a data set corresponds to the contents of a single database table, or a single statistical data matrix, where every column of the table represents a particular variable, and each row corresponds to a given member of the data set in question. A transactional database is a database management system (DBMS) that has the capability to roll back or undo a database transaction or operation if it is not completed appropriately.\n2. Scalability is the capability of a system, network, or process to handle a growing amount of work, or its potential to be enlarged to accommodate that growth\n3. An impulse purchase or impulse buying is an unplanned decision to buy a product or service, made just before a purchase.\n4. An impulse purchase or impulse buying is an unplanned decision to buy a product or service, made just before a purchase." ]
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https://math.stackexchange.com/questions/1252144/does-every-cover-have-an-irredundant-subcover?noredirect=1
[ "# Does every cover have an irredundant subcover?\n\nWhile composing an answer for this question, I got troubled by a technical point. I wanted to assert the existence of an irredundant subcover of a given open cover, but realized I'm not sure how to guarantee that this exists. I got around this technicality in that particular situation by using other aspects of the setup, but now I want to understand the general situation. I'll phrase the question in the language of topology, but it is really purely a set-theoretic question.\n\nLet us call an open cover $\\{U_\\lambda\\}_{\\lambda\\in\\Lambda}$ irredundant if no $U_\\lambda$ can be dropped, i.e. if $\\{U_\\lambda\\}_{\\lambda\\in\\Lambda'}$ is never a cover if $\\Lambda'$ is a proper subset of $\\Lambda$; equivalently, if for each $\\lambda\\in\\Lambda$, $\\bigcap_{\\mu\\neq \\lambda} (U_\\mu)^c$ is nonempty.\n\nGiven a topological space $X$ with an arbitrary open cover $\\{U_\\lambda\\}_{\\lambda\\in\\Lambda}$, does there always exist an irredundant subcover? Why?\n\nClearly there is no problem if $\\Lambda$ is finite (or if $X$ is compact so that we can first pass to a finite subcover): just drop redundant $U_\\lambda$'s one at a time until the cover is irredundant.\n\nBut what if $\\Lambda$ has much bigger cardinality? At first I thought we ought to be able to construct an irredundant subcover using some appropriate form of the axiom of choice. After all, I thought, all we have to do is drop the redundant $U_\\lambda$'s. (I.e. those such that $\\bigcap_{\\mu\\neq \\lambda}(U_\\mu)^c$ is empty.) We can't drop them all at once, unfortunately, since we might not be left with a cover. But if we drop them one at a time, and reevaluate which are redundant after each drop, then, well, AC is designed for organizing an infinite sequence of choices of this kind.\n\nFor example we could try: by the well-ordering theorem, impose a well-order on $\\Lambda$. Then the set of $\\lambda$'s corresponding to redundant $U_\\lambda$'s has a least element, and this is what we drop first. Rinse and repeat.\n\nOr (this was my first idea), the setup seems custom made for Zorn's lemma: the subcovers of a given cover form a nonempty poset under reverse inclusion, and the irredundant covers are precisely the maximal elements of this poset.\n\nThe problem is that in the end, I don't actually think one can generally arrive at an irredundant cover, even when it exists, by dropping redundant $U_\\lambda$'s one at a time. The example I have in mind is, let $X$ be any nonempty space at all, let $\\Lambda = \\mathbb{N}$, and let $U_1,U_2,\\dots = X$. This example shows that both of the above approaches will fail. If we try to construct an irredundant subcover by repeatedly dropping the first redundant $U_n$, we get the sequence of subcovers\n\n$$\\{U_n\\}_{n\\geq 1}\\supset \\{U_n\\}_{n\\geq 2}\\supset \\dots$$\n\nand the procedure never lands on an irredundant one since the limit is empty, which isn't a cover. This very sequence also shows the hypotheses of Zorn's lemma aren't met (in the attempt above to use Zorn's lemma): here is an increasing chain in the poset of subcovers that does not have an upper bound.\n\nThis example seems to me to show that the AC-based approaches are barking up the wrong tree. On the other hand, evidently there is an irredundant cover here: any individual $U_n$ will do the job. So maybe there is still hope that the question's answer is yes?\n\nAs you’ve already discovered, the answer is no. In fact, you can’t even guarantee an irreducible open refinement. For $n\\in\\Bbb N$ let $U_n=\\{k\\in\\Bbb N:k<n\\}$, and let $\\tau=\\{U_n:n\\in\\Bbb N\\}\\cup\\{\\Bbb N\\}$; then $\\tau$ is a $T_0$ topology on $\\Bbb N$, and $\\tau\\setminus\\{\\Bbb N\\}$ is an open cover of $\\Bbb N$ with no irreducible open refinement.\n\nA well-known positive result is that every point-finite open cover of a space has an irreducible subcover. Thus, every open cover of a metacompact space has an irreducible open refinement. (A space $X$ is metacompact if every open cover of $X$ has a point-finite open refinement. A family of sets is point-finite if each point of the space lies in only finitely many of the sets.)\n\n• +1 \"Does every open cover have an irredundant open refinement?\" was going to be my next question! (Aside: I see the argument for the positive result because the Zorn's lemma approach goes through: point-finiteness shows that the poset of subcovers satisfies the ascending chain condition.) – Ben Blum-Smith Apr 26 '15 at 16:55\n• Actually I think I'm waving my hands my aside here. Let $X=\\mathbb{N}$ with the discrete topology, let $\\Lambda = \\mathbb{N}\\times \\{0,1\\}$, and let $U_{(n,i)} = \\{n\\}$ for both $i=0,1$. Let $\\mathcal{F}_k = \\{U_{n,1}\\}_{n\\geq k} \\cup \\{U_{n,0}\\}_{n\\geq 1}$. Then $\\mathcal{F}_1\\prec \\mathcal{F}_2\\prec\\dots$ is a nonterminating ascending chain in the poset of subcovers. – Ben Blum-Smith May 2 '15 at 15:49\n• But the Zorn's lemma approach still goes through! What point-finiteness does is to force the poset of subcovers to be closed under taking intersections of chains, thus ascending chains have upper bounds. If $\\mathcal{F}_1\\prec\\mathcal{F}_2\\prec\\dots$ is an ascending chain of subcovers (i.e. descending under inclusion), and the intersection is not a cover, there is an uncovered $x\\in X$. Then the set of $k$ for which some set of $\\mathcal{F}_K\\setminus\\mathcal{F}_{k+1}$ contains $x$ must be cofinal in $\\mathbb{N}$. But this implies infinitely many sets of the cover contain $x$. – Ben Blum-Smith May 2 '15 at 16:01\n• @Ben: Yes, that’s the argument that I gave here and essentially the argument in Engelking. – Brian M. Scott May 2 '15 at 18:39\n\nAs often happens when I write questions here, I realized something while writing. Here I actually realized the answer.\n\nIt is no.\n\nHere is an open cover of $\\mathbb{R}$ with no irredundant subcover:\n\n$\\Lambda=\\mathbb{N}$.\n\n$U_n = (-n,n)$.\n\nBecause $U_1\\subset U_2\\subset U_3\\subset\\dots$, given any pair of $U_n$'s, one is contained in the other. Therefore any subcover is redundant unless it consists of a single $U_n$. But no single $U_n$ forms a cover. Thus no subcover is irredundant.\n\nI'm not sure if it helps you with your original question, but let me try proposing an alternative concept capturing the intuitive notion of irredundancy: for each point, take the “smallest” open set in the cover containing that point.\n\nFormally, let $\\{U_{\\lambda}\\}_{\\lambda\\in\\Lambda}$ be an open cover of the topological space $X$, where $\\Lambda$ is a non-empty index set. Now endow $\\Lambda$ with a well-ordering $\\succsim$. For each point $x\\in X$, let $\\lambda_x$ be the least element of $\\{\\lambda\\in\\Lambda\\,|\\,x\\in U_{\\lambda}\\}$ according to the well-ordering. Then, $\\{U_{\\lambda_x}\\}_{x\\in X}$ is a refined subcover of $\\{U_{\\lambda}\\}_{\\lambda\\in\\Lambda}$." ]
[ null ]
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https://mathoverflow.net/questions/149391/on-radicals-of-a-lie-algebra
[ "# On radicals of a lie algebra\n\nLet $\\mathbb{k}$ be a field, $\\mathfrak{g}$ be a finite-dimensional Lie algebra over $\\mathbb{k}$. In Bourbaki's \"Lie Groups and Lie Algebras\", Ch I, he defines four radical-like ideals of $\\mathfrak{g}$:\n\n1. the radical $\\mathfrak{r}$, i.e. the maximal solvable ideal;\n2. the radical of Killing form $\\mathfrak{k}$, i.e. $\\mathfrak{k}=\\mathfrak{g}^\\perp$;\n3. the maximal nilpotent ideal $\\mathfrak{n}$;\n4. the nilpotent radical $\\mathfrak{s}$, i.e. intersection of all kernels of irreducible finite-dimensional representations of $\\mathfrak{g}$.\n\nHe also shows that, $\\mathfrak{r}=[\\mathfrak{g},\\mathfrak{g}]^\\perp$, $\\mathfrak{s}=[\\mathfrak{g}, \\mathfrak{g}]\\cap\\mathfrak{r}=[\\mathfrak{g},\\mathfrak{r}]$, and the following inclusion relations: $$\\mathfrak{r} \\supset \\mathfrak{k} \\supset \\mathfrak{n} \\supset \\mathfrak{s}.$$\n\nOn the other hand, in Jacobson's book, the nilpotent radical is defined as $\\mathfrak{n}$.\n\nMy question is, does $\\mathfrak{s}$ coincide with $\\mathfrak{n}$? or, are Bourbaki's nilradical and Jacobson's nilradical equivalent?\n\nI guess the answer is NO (otherwise Bourbaki should have proved it), but I cannot find any example. Could any one give me an example? Thank you!\n\n• $\\mathfrak{s}$ vanishes iff $\\mathfrak{g}$ is reductive, but it's easy to find reductive Lie algebras for which $\\mathfrak{n}$ fails to vanish (e.g. abelian ones). – Qiaochu Yuan Nov 20 '13 at 5:28\n• @Si-Qi Yu: Those parts of Bourbaki have a running hypothesis that char$(k)=0$ (look at the start of various sections); e.g., for $\\mathfrak{g}=\\mathfrak{sl}_p$ in characteristic $p>0$ the Killing form vanishes and the subalgebra ${\\rm{Lie}}(\\mu_p)$ of diagonal scalars form a nonzero central ideal yet if $p>2$ then $[\\mathfrak{g},\\mathfrak{g}]=\\mathfrak{g}$, etc. – Marguax Nov 20 '13 at 14:52\n• @Qiaochu Yuan: What is your definition of \"reductive Lie algebra\" in positive characteristic? – Marguax Nov 20 '13 at 14:53\n• @Marguax: I don't have one (I assume you're hinting that the equivalence between various possible definitions fails). Is positive characteristic an important issue here? – Qiaochu Yuan Nov 20 '13 at 18:50\n• @Qiaochu Yuan: The assertions in Bourbaki totally break down in positive characteristic, so it is more serious than a failure of equivalences. I am not aware of a good definition of \"reductive Lie algebra\" outside characteristic 0, so it was unclear to me if you had a definition. In the setting of Lie algebras (unlike for algebraic groups) it is safest to explicitly assume char. 0 for such things unless one provides a clear definition or reference for the terminology being used. (Bourbaki demands char. 0 in their definition of \"reductive Lie algebra\"; look at the start of section 6 of Ch. I.) – Marguax Nov 20 '13 at 19:56\n\nIf we let $\\mathbb{k}$ be the field itself thought of as a Lie algebra with trivial bracket, then $\\mathfrak{n}=\\mathbb{k}$ since this is a nilpotent Lie algebra but $\\mathbb{s}=\\{0\\}$, since the obvious representation of $\\mathbb{k}$ be scalar multiplication is faithful. In general, these will never coincide for a nilpotent Lie algebra.\nThe two definitions do never agree for a non-trivial nilpotent Lie algebra, as Ben has remarked. Indeed, if $\\mathfrak{g}$ is nilpotent then $\\mathfrak{s}=[\\mathfrak{g},\\mathfrak{r}]=[\\mathfrak{g},\\mathfrak{g}]$, whereas $\\mathfrak{n}=\\mathfrak{g}$. Since $\\mathfrak{g}$ is nilpotent, $\\mathfrak{g}\\neq [\\mathfrak{g},\\mathfrak{g}]$. For non-trivial abelian Lie algebras we have in particular $\\mathfrak{s}=0$ and $\\mathfrak{n}=\\mathfrak{g}$.\nIf $\\mathfrak{g}$ is solvable, then $\\mathfrak{s}=[\\mathfrak{g},\\mathfrak{g}]$ and $\\mathfrak{s}\\subseteq \\mathfrak{n}$, and both equality and strict inclusion can happen. For equality consider the $2$-dimensional non-abelian Lie algebra.\nOn the other hand, Serre and others in the Bourbaki group (at the time their treatise on Lie groups and Lie algebras began) were more steeped in Lie groups and linear algebraic groups. Even though Chevalley's classification seminar in the late 1950s mostly bypassed Lie algebras, it was becoming clear that the intrinsic Jordan decomposition in algebraic groups and their Lie algebras was an important new tool. Similarly, contemporary work on \"reductive\" Lie groups was making reductive Lie algebras natural to study alongside semisimple ones. And representation theory of many kinds was becoming more prominent. So it's not surprising that there is some divergence in Bourbaki and Jacobson when the various ideals mentioned here come into play. For Jacobson, only $\\mathfrak{r}$ and $\\mathfrak{n}$ played a major role.\nA final remark is that abelian Lie algebras are somewhat problematic, since their role in the absence of an intrinsic Jordan decomposition is ambiguous. This makes the contrast between $\\mathfrak{n}$ and $\\mathfrak{s}$ inevitable if you only discuss Lie algebras and their representations abstractly." ]
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https://uk.mathworks.com/matlabcentral/fileexchange/69510-natural-excitation-technique-next?s_tid=prof_contriblnk
[ "## Natural Excitation Technique (NExT)\n\nversion 1.0.4 (3.5 KB) by\nReturns impulse response functions (IRF) using Natural Excitation technique with time domain method and frequency domain method\n\nUpdated 16 Jul 2019\n\nReturns impulse response functions (IRF) using Natural Excitation technique with time domain method (NExTT) and frequency domain method (NExTF) for systems subjected to white noise excitation. Example file is provided for estimating IRF of 2DOF system subjected to Gaussian white noise excitation with added uncertainty (also Gaussian white noise) to the response.\n\n1-function IRF= NExTT(data,refch,maxlags)\n\nInputs :\n\ndata: An array that contains response data.its dimensions are (nch,Ndata) where nch is the number of channels. Ndata is the total length of the data\nrefch: A vecor of reference channels .its dimensions (numref,1) where numref is number of reference channels\nmaxlags: Number of lags in cross-correlation function\n\nOutputs :\n\nIRF: Impulse Response Function matrix of size (nch,numref*(maxlags+1))\n\n2-function IRF= NExTF(data,refch,window,N,p)\n\nInputs :\n\ndata: An array that contains response data.its dimensions are (nch,Ndata) where nch is the number of channels. Ndata is the total length of the data\nrefch: A vecor of reference channels .its dimensions (numref,1) where numref is number of reference channels\nwindow: window size to get spectral density\nN: Number of windows\np: overlap ratio between windows. from 0 to 1\n\nOutputs :\n\nIRF: Impulse Response Function matrix of size (nch,numref*(ceil(window/2+1)-1))\n\nReferences:\n------------------\n James, G. H., Thomas G. Carne, and James P. Lauffer. \"The natural excitation technique (NExT) for modal parameter extraction from operating structures.\" Modal Analysis-the International Journal of Analytical and Experimental Modal Analysis 10.4 (1995): 260.\n\n Al Rumaithi, Ayad, \"Characterization of Dynamic Structures Using Parametric and Non-parametric System Identification Methods\" (2014). Electronic Theses and Dissertations. 1325.\nhttps://stars.library.ucf.edu/etd/1325\n\n Al-Rumaithi, Ayad, Hae-Bum Yun, and Sami F. Masri. \"A Comparative Study of Mode Decomposition to Relate Next-ERA, PCA, and ICA Modes.\" Model Validation and Uncertainty Quantification, Volume 3. Springer, Cham, 2015. 113-133.\n\n### Cite As\n\nAyad Al-Rumaithi (2021). Natural Excitation Technique (NExT) (https://www.mathworks.com/matlabcentral/fileexchange/69510-natural-excitation-technique-next), MATLAB Central File Exchange. Retrieved .\n\n##### MATLAB Release Compatibility\nCreated with R2018b\nCompatible with any release\n##### Platform Compatibility\nWindows macOS Linux" ]
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https://pythonguides.com/matplotlib-invert-y-axis/
[ "# Matplotlib invert y axis\n\nIn this Python tutorial, we will discuss Matplotlib invert y axis in python. Here we will cover different examples related to inverting of the y-axis using matplotlib. And we will also cover the following topics:\n\n• Matplotlib invert y axis\n• Matplotlib invert y axis subplots\n• Matplotlib invert x and y axis\n• Matplotlib barh invert y axis\n• Matplotlib invert secondary y axis\n• Matplotlib 3D invert y axis\n• Matplotlib flip y axis label\n• Matplotlib invert y axis imshow\n\nIf you are new to python Matplotlir, check out, How to install matplotlib python.\n\n## Matplotlib invert y axis\n\nIn this section, we learn about how to invert the y-axis in matplotlib in Python. Now before starting the topic firstly, we discuss what does invert mean here:\n\nInvert means reverse or flip the order\n\nTo understand more clearly let’s take a common example:\n\nSuppose the y-axis starts from 0 to 10 and you want to start it from 10 to 0. So in that cases, we invert or flip the axes of the plot.\n\nIn matplotlib, we can invert the y-axis of a graph using different methods. The following are the different methods used for reversing the y-axis are as below.\n\n• Using invert_yaxis() method\n• Using ylim() method\n• Using axis() method\n\n### By using invert_yaxis() method\n\nTo invert Y-axis, we can use invert_yaxis() method.\n\nSyntax of the method is as below:\n\n``matplotlib.axes.Axes.invert_yaxis(self)``\n\nExample: (Without inverting axis)\n\n``````# Import Library\n\nimport matplotlib.pyplot as plt\nimport numpy as np\n\n# Define Data\n\nx = np.arange(0, 15, 0.2)\ny = np.sin(x)\n\n# Plot figure\n\nplt.plot(x, y)\n\n# Title\n\nplt.title(\"Sine Function Normal Plot\", fontsize= 15, fontweight='bold')\n\n# Generate Plot\n\nplt.show()``````\n• In the above example, we import the matplotlib.pyplot and numpy library.\n• After this we define data using np.arrange() and np.sin() method.\n• Next, we use the plt.plot() method to draw the plot.\n• By using plt.title() we define the title of the plot.\n• plt.show() method is used to generate the plot on the user screen.\n\nLook at the y-axis: Here it starts from -1.00 and ends at 1.00\n\nExample: (With inverting axis)\n\n``````# Import Library\n\nimport matplotlib.pyplot as plt\nimport numpy as np\n\n# Define Data\n\nx = np.arange(0, 15, 0.2)\ny = np.sin(x)\n\n# Plot figure\n\nplt.plot(x, y)\n\n# Invert y-axis\n\nax = plt.gca()\nax.invert_yaxis()\n\n# Title\n\nplt.title(\"Sine Function Invert Plot\", fontsize= 15, fontweight='bold')\n\n# Generate Plot\n\nplt.show()``````\n• In the above example, we include the plt.gca() method to get current axes.\n• After this, we use the ax.invert_yaxis() method to invert or reverse the y-axis of the plot.\n\nLook at the y-axis: Here it starts from 1.00 and ends at -1.00\n\nConclusion: By using invert_yaxis() method we can reverse the y-axis of the plot.\n\n### By using ylim() method\n\nylim() method is also used to invert axes of a plot in Matplotlib. Generally, this method is used to set limits for the axes.\n\nBut if we set the minimum value as the upper limit and maximum value as the lower limit we can revert the axes.\n\nThe syntax of the ylim() method is as below:\n\n``matplotlib.pyplot.ylim(bottom,top)``\n\nHere bottom and top specify the tuple of the new y-axis limits.\n\nLet’s see an example to understand it more clearly:\n\n``````# Import Library\n\nimport numpy as np\nimport matplotlib.pyplot as plt\n\n# Define Data\n\nx = np.linspace(5, 15, 35)\ny = 2*x+5\n\n# Create plot\n\naxes,(p1,p2) = plt.subplots(1, 2)\n\n# Normal plot\n\np1.plot(x, y)\np1.set_title(\"Normal Plot\")\n\n# Invert plot\n\np2.plot(x, y)\np2.set_title(\"Inverted Plot\")\nplt.ylim(max(y), min(y))\n\n# Show\n\naxes.tight_layout()\nplt.show()``````\n• In the above example, firstly we import numpy and matplotlib.pyplot library.\n• Next, we define the data and by using the plt.subplot() method we create subplots.\n• Now we use the plot() method to draw a simple plot.\n• plt.ylim() method is used to invert the y-axis here we pass max and min as a parameter.\n\nConclusion: In the normal plot, the y-axis starts from 1 and ends at 5. And In the inverted plot, the y-axis starts from 5 and ends at 1.\n\n### By using axis() method\n\nThe axis() method is also used to revert axes in Matplotlib. Basically, this method is used to set the minimum and maximum values of the axes.\n\nBut if we set the minimum value as the upper limit and the maximum value as the lower limit we can get inverted axes.\n\nThe syntax of the axis() method is as below:\n\n``matplotlib.pyplot.axis()``\n\nLet’ see an example:\n\n``````# Import Library\n\nimport numpy as np\nimport matplotlib.pyplot as plt\n\n# Define Data\n\nx = np.arange(0, 15, 0.2)\ny = np.tan(x)\n\n# Create plot\n\naxes,(p1,p2) = plt.subplots(1, 2)\n\n# Normal plot\n\np1.plot(x, y)\np1.set_title(\"Normal Plot\")\n\n# Invert plot\n\np2.plot(x, y)\np2.set_title(\"Inverted Plot\")\nplt.axis([max(x), min(x), max(y), min(y)])\n\n# Show\n\naxes.tight_layout()\nplt.show()``````\n• Here we import matplotlib.pyplot and numpy library and define data using np.arrange() and np.tan() method.\n• plt.subplots() method is used for creating subplots.\n• Then we use the plot() method to plot a graph and the set_title() method is used to add a title to the plot.\n• By using the plt.axis() method we revert the axes and here we pass the max and min values of the y and x axes.\n\n## Matplotlib invert y axis subplots\n\nHere we will discuss how to invert the y-axis of the specific subplot if we draw multiple plots in a figure area in Python matplotlib.\n\nWe use the invert_yaxis() method to flip the y-axis of the subplot.\n\nLet’s understand the concept with the help of an example:\n\n``````# Import Libraries\n\nimport numpy as np\nimport matplotlib.pyplot as plt\n\n# Define Data\n\nx1= [0.2, 0.4, 0.6, 0.8, 1]\ny1= [0.3, 0.6, 0.8, 0.9, 1.5]\n\nx2= [2, 6, 7, 9, 10]\ny2= [3, 4, 6, 9, 12]\n\nx3= [5, 8, 12]\ny3= [3, 6, 9]\n\nx4= [5, 8, 12]\ny4= [3, 6, 9]\n\nfig, ax = plt.subplots(2, 2)\n\n# Invert y-axis\n\nax[1,0].invert_yaxis()\n\n# Plot graph\n\nax[0, 0].plot(x1, y1)\nax[0, 1].plot(x2, y2)\nax[1, 0].plot(x3, y3)\nax[1, 1].plot(x4, y4)\n\n# Display Graph\n\nfig.tight_layout()\nplt.show()``````\n• In the above example, we plot multiple plots in a figure area. And we want to invert the y-axis of the specific plot.\n• Here we use the invert_yaixs() method to flip the y-axis of the plot.\n• We use the invert_yaxis() method with the third plot.\n\n## Matplotlib invert x and y axis\n\nHere we are going to learn how to invert the x-axis and y-axis of the plot in Python matplotlib.\n\nBy using invert_xaxis() and invert_yaxis() method we can flip the x-axis and y-axis respectively.\n\nThe syntax is as given below:\n\n``````# Invert x-axis\n\nmatplotlib.axes.Axes.invert_xaxis(self)\n\n# Invert y-axis\n\nmatplotlib.axes.Axes.invert_yaxis(self) ``````\n\nLet’s see an example related to this concept:\n\n``````# Import Library\n\nimport numpy as np\nimport matplotlib.pyplot as plt\n\n# Define Data\n\nx=[5, 10, 15, 20, 25,30]\ny=[0, 1, 2, 3, 4, 5]\n\n# Create Subplot\n\naxes,(p1,p2) = plt.subplots(1, 2)\n\n# Normal plot\n\np1.plot(x, y)\np1.set_title(\"Normal Plot\")\n\n# Invert plot\n\np2.plot(x, y)\np2.set_title(\"Inverted Plot\")\n\n# Invert axes\n\nax = plt.gca()\nax.invert_yaxis()\nax.invert_xaxis()\n\n# Show\n\naxes.tight_layout()\nplt.show()``````\n• In the above example, we import numpy and matplotlib libraries.\n• After this, we define data on x and y coordinates.\n• By using the plt.subplots() method we create subplots in a figure area.\n• Next, we use the plot() method to plot a graph and the set_title() method to set the title of the plot.\n• Then we use plt.gca() method to get current axes of the plot.\n• By using the invert_yaxis() and the invert_xaxis() method we flip the axes of the plot.\n• In last, we use the tight_layout() method to automatically set the plots and the show() method to display the plot on the user’s screen.\n\nAlso, read Matplotlib savefig blank image\n\n## Matplotlib barh invert y axis\n\nHere we are going to learn how we invert the y-axis of the horizontal bar chart using matplotlib in Python. Firstly, we have to know how to plot a horizontal bar chart.\n\nThe syntax to plot the horizontal bar chart is as below:\n\n``matplotlib.pyplot.barh(x,y)``\n\nHere x represents the x-axis coordinates and y represents the height of the bars.\n\nThe syntax to invert the y-axis of the barh chart is as given below:\n\n``````# Invert y-axis\n\nmatplotlib.axes.Axes.invert_yaxis(self) ``````\n\nExample:\n\n``````# Import Library\n\nimport numpy as np\nimport matplotlib.pyplot as plt\n\n# Define Data\n\nx=[1, 2, 3, 4, 5]\ny=[20, 15, 12, 6, 5]\n\n# Simple Bar Chart\n\nplt.figure()\nplt.barh(x,y)\n\n# Inverted Bar chart\n\nplt.figure()\nplt.barh(x,y)\nplt.gca().invert_yaxis()\n\n# Show\n\nplt.show()``````\n• In the above example, we first import the numpy and matplotlib.pyplot library.\n• Next, we define data.\n• By using the plt.barh() method we create a horizontal bar chart.\n• By using the plt.gca() method we get the current axes of the plot.\n• Then we use the invert_yaxis() method to flip the y-axis of the plot.\n\n## Matplotlib invert secondary y axis\n\nHere we are going to learn how we can invert the secondary y-axis in matplotlib in Python. Firstly, we have to understand what does secondary y-axis means and when we need it.\n\nOnce in a while, we need two x-axes or y-axes to get more insights into the data. At that moment we need to create secondary axes.\n\nIn python, matplotlib provides the functionality to create a plot that has two y-axes, and even we can provide different labels to both.\n\nWe can create a plot with two different y-axes by using two different axes objects. And to create different axes objects we use the twinx() method.\n\nLet’s see an example where we invert the secondary y-axis:\n\n``````# Import Library\n\nimport numpy as np\nimport matplotlib.pyplot as plt\n\n# Define Data\n\nx = np.arange(0, 10, 3.5)\ny1 = x**2\ny2 = x**4\n\n# Create subplot\n\nfig, ax = plt.subplots(figsize = (10, 5))\n\n# twinx() for creating axes object for secondary y-axis\n\nax2 = ax.twinx()\n\n# Plot graph\n\nax.plot(x, y1)\nax2.plot(x, y2)\n\n# Invert secondary y-axis\n\nax2.invert_yaxis()\n\n# Labels to axes\n\nax.set_xlabel('x-axis')\nax.set_ylabel('y-axis')\n\n# Label secondary y-axis\n\nax2.set_ylabel('Secondary y-axis', color = 'b')\n\n# Display layout\n\nplt.tight_layout()\n\n# Show plot\n\nplt.show()``````\n• In the above example, we import important libraries such as numpy and matplotlib.pyplot.\n• Next, we create data by using the np.arange() method here we define data between 0 to 10 with the difference of 3.5 at the x-axis.\n• Then by using plt.subplots() methods we create subplots.\n• By using the twinx() we create another axes object for the secondary y-axis.\n• set_xlabel() and set_ylabel() methods are used for adding labels on the axes.\n• By using the tight_layout() and show() method we define the layout and show the plot.\n\n## Matplotlib 3D invert y axis\n\nIn this section, we are going to study how to invert a 3D plot in Matplotlib in Python.\n\nThe syntax to create a 3D plot and invert the y-axis:\n\n``````# Create 3D plot\nax.plot3D(x,y,z)\n\n# Invert y-axis\nmatplotlib.pyplot.ylim(max(y),min(y))``````\n\nHere x, y, and z are the coordinates points.\n\nLet’s see an example related to this:\n\n``````# Import Libraries\n\nimport matplotlib\nfrom mpl_toolkits.mplot3d import Axes3D\nimport matplotlib.pyplot as plt\n\n# Create subplots\n\nfig = plt.figure(figsize=(12,5), dpi=80)\n\n# Simple plot\n\nx=[1,1,10,10]\ny=[1,10,10,10]\nz=[1,1,1,10]\nax1.plot(x,y ,z , marker=\"o\")\n\n# Inverted Plot\n\nx1=[1,1,10,10]\ny1=[1,10,10,10]\nz1= [1,1,1,10]\n\n# Function used for invert y-axis\n\nplt.ylim(max(y1),min(y1))\n\nax2.plot(x1,y1 ,z1, marker=\"o\")\n\n# Show Plot\n\nplt.show()\n``````\n• In the above example, we import important libraries such as matplotlib.pyplot, and mplot3D.\n• Next, we use the plot() method to plot a graph in a figure area.\n• By using the ylim() method we invert the y-axis of the plot. In function, we pass the max and min of y1 coordinates.\n\n## Matplotlib flip y axis label\n\nHere we are going to learn to flip labels at the y-axis in Matplotlib in Python. By using the ylabel() method we can add the label at the y-axis and flip it.\n\nExample:\n\n``````# Import Library\n\nfrom matplotlib import pyplot as plt\n\n# Define Data\n\nx=[0, 1, 2, 3, 4, 5]\ny=[2, 4, 6, 8, 10, 12]\n\n# Plot graph\n\nplt.plot(x,y)\n\n# Flip Y-axis Label\n\nplt.ylabel('Y-axis',rotation=0)\n\n# Show\n\nplt.draw()``````\n• In the above example, we import matplotlib.pyplot library for visualization.\n• Next, we define the data and use the plt.plot() method to draw a plot.\n• By using plt.ylabel() method we set the label at the y-axis and flip it horizontally by passing the rotation argument. Here we set the value of rotation to 0.\n\n## Matplotlib invert y axis imshow\n\nHere we learn to invert the y-axis in the imshow() method in Python Matplotlib. Firstly, understand what does imshow does:\n\ninshow() method shows an image of a color-mapped or 3D RGB array.\n\nThe syntax of the inshow() method is given below:\n\n``````matplotlib.pyplot.imshow(X,\ncmap=None,\nnorm=None,\naspect=None,\ninterpolation=None,\nalpha=None,\nvmin=None,\nvmax=None,\norigin=None,\nextent=None,\nshape=,\nfilternorm=1,\nimlim=,\nresample=None,\nurl=None,\ndata=None,\n*kwargs)``````\n\nThe parameters used above are described as below:\n\n• X: specify data of the image.\n• cmap: specifies colormap or registered colormap name.\n• norm: It is a normalized instance used to scale data.\n• aspect: Used to control the aspect ratio of the axes.\n• interpolation: It is an interpolation method used to display images.\n• alpha: specify the intensity of the color.\n• vmin, vmax: specify the range of the color bar.\n• origin: Used to place [0,0] index of the array in the upper left or lower corner of the axes.\n• extent: It is a bounding box in data coordinates.\n• filternorm: Used for the antigrain image resize filter.\n• url: set the URL of the axes image.\n\nExample:\n\n``````# Import Libraries\n\nimport numpy as np\nfrom matplotlib import pyplot as plt\n\n# Define data\n\nx = np.array([[0, 1, 2, 3],\n[1, 1, 1, 3],\n[1, 2, 2, 3],\n[2, 2, 3, 3]])\n\n# Create subplot\n\nfig, ax = plt.subplots(1,2)\n\n# Imshow and Invert Y-axis\n\nfor i in range(2):\nax.imshow(x, cmap = 'summer', vmin = 1, vmax = 3,)\nax.imshow(x, cmap = 'summer', vmin = 1, vmax = 3,\norigin='lower')\n# Show\n\nplt.show()``````\n• Here we define data using the np.array() method and use the imshow() method to plot the image of the colormap.\n• We pass the parameter origin to flip the y-axis and set its value to lower." ]
[ null ]
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https://intellipaat.com/community/8117/what-is-lrpolicy-in-caffe
[ "2 views\n\nI just try to find out how I can use Caffe. To do so, I just took a look at the different .prototxt files in the examples folder. There is one option I don't understand:\n\n# The learning rate policy\n\nlr_policy: \"inv\"\n\nPossible values seem to be:\n\n• \"fixed\"\n\n• \"inv\"\n\n• \"step\"\n\n• \"multistep\"\n\n• \"stepearly\"\n\n• \"poly\"\n\nCould somebody please explain those options?\n\nby (33.1k points)\n\nYou can check following description about lr_policy (Learning rate decay):\n\n// The learning rate decay policy. The currently implemented learning rate\n\n// policies are as follows:\n\n//    - fixed: always return base_lr.\n\n//    - step: return base_lr * gamma ^ (floor(iter / step))\n\n//    - exp: return base_lr * gamma ^ iter\n\n//    - inv: return base_lr * (1 + gamma * iter) ^ (- power)\n\n//    - multistep: similar to step but it allows non uniform steps defined by\n\n//      stepvalue\n\n//    - poly: the effective learning rate follows a polynomial decay, to be\n\n//      zero by the max_iter. return base_lr (1 - iter/max_iter) ^ (power)\n\n//    - sigmoid: the effective learning rate follows a sigmod decay\n\n//      return base_lr ( 1/(1 + exp(-gamma * (iter - stepsize))))\n\n//\n\n// where base_lr, max_iter, gamma, step, stepvalue and power are defined\n\n// in the solver parameter protocol buffer, and iter is the current iteration.\n\nHope this answer helps." ]
[ null ]
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https://www.fxsolver.com/browse/formulas/Area+of+a+circular+segment
[ "# Area of a circular segment\n\n## Description\n\nCircular segment is a region of a circle which is “cut off” from the rest of the circle by a secant or a chord. More formally, a circular segment is a region of two-dimensional space that is bounded by an arc (of less than 180°) of a circle and by the chord connecting the endpoints of the arc.\nCentral angle is an angle whose apex (vertex) is the center of a circle and whose legs (sides) are radii intersecting the circle in two distinct points and thereby subtending an arc between those two points whose angle is (by definition) equal to that of the central angle. The area of a circular segment can be calculated by the radius of the circle and the cental angle of the arc of the segment.\n\nRelated formulas\n\n## Variables\n\n Aseg Area of the circular segment (m2) R The radius of the circle (m) θ The central angle (radians)" ]
[ null ]
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https://www.personal-math-online-help.com/vertical-subtraction-with-regrouping-worksheets-3d-2d.html
[ "## Vertical SubtractionWith Regrouping Worksheets3 digits - 2 digits\n\nReminders & Tips for - Vertical Subtraction With Regrouping 3 digits - 2 digits Worksheet:\n• A Reminder: you should already know your subtraction to 18 with borrowing\n• A Tip: first you borrow a 10 from 10s to make the upper 1s bigger than lower 1s. Then borrow a 100 from 100s to make the upper 100s \"stronger\". Then just drop down the remaining 100s. :-)\n\nOK, Try these Vertical Subtraction With Regrouping worksheets below.\n\nBut if you want to try any of the steps - hover your mouse over a Step - and Click to practice it.\n\nOr you can try our similar vertical subtraction worksheets from the table below.\n\n Free Printable math vertical subtraction worksheets:", null, "", null, "", null, "", null, "", null, "", null, "" ]
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https://tellmeanumber.hostcoder.com/879261
[ "Question Is 879,261 a prime number?\n\nThe number 879,261 is NOT a PRIME number.\n\nHow to check if the number 879,261 is a prime number\n\nA prime number can be divided, without a remainder, only by itself and by 1. For example, 13 can be divided only by 13 and by 1. In this case, the number 879,261 that you looked for, is NOT a PRIME number, so it devides by 1,3, 293087, 879261, and of course 879,261.\n\nQuestion Where is the number 879,261 located in π (PI) decimals?\n\nThe number 879,261 is at position 1439006 in π decimals.\n\nSearch was acomplished in the first 100 milions decimals of PI.\n\nQuestion What is the roman representation of number 879,261?\n\nThe roman representation of number 879,261 is DCCCLXXIXCCLXI.\n\nLarge numbers to roman numbers\n\n3,999 is the largest number you can write in Roman numerals. There is a convencion that you can represent numbers larger than 3,999 in Roman numerals using an overline. Matematically speaking, this means means you are multiplying that Roman numeral by 1,000. For example if you would like to write 70,000 in Roman numerals you would use the Roman numeral LXX. This moves the limit to write roman numerals to 3,999,999.\n\nQuestion How many digits are in the number 879,261?\n\nThe number 879,261 has 6 digits.\n\nHow to get the lenght of the number 879,261\n\nTo find out the lenght of 879,261 we simply count the digits inside it.\n\nQuestion What is the sum of all digits of the number 879,261?\n\nThe sum of all digits of number 879,261 is 33.\n\nHow to calculate the sum of all digits of number 879,261\n\nTo calculate the sum of all digits of number 879,261 you will have to sum them all like fallows:\n\nQuestion What is the hash of number 879,261?\n\nThere is not one, but many hash function. some of the most popular are md5 and sha-1\n\nHere are some of the most common cryptographic hashes for the number 879,261\n\nCriptographic function Hash for number 879,261\nmd5 719b09fc6a0f41756baf88429376a320\nsha1 11be4c401d492504fc12166063b3c67023885945\nsha256 ce47c21c948863e52b7e3aab892ba8163d8f98c7fb846a508e825888bb864461\nsha512 c3aae967113455d603522f10a8cf234366ec7bf8054293685bbd5821385f30c9610bcd23ff258e6099eb5b80a0813d8d8b14e15c7f847c6f43a96755bec68c41\n\nQuestion How to write number 879,261 in English text?\n\nIn English the number 879,261 is writed as eight hundred seventy-nine thousand, two hundred sixty-one.\n\nHow to write numbers in words\n\nWhile writing short numbers using words makes your writing look clean, writing longer numbers as words isn't as useful. On the other hand writing big numbers it's a good practice while you're learning.\n\nHere are some simple tips about when to wright numbers using letters.\n\n Numbers less than ten should always be written in text. On the other hand numbers that are less then 100 and multiple of 10, should also be written using letters not numbers. Example: Number 879,261 should NOT be writed as eight hundred seventy-nine thousand, two hundred sixty-one, in a sentence Big numbers should be written as the numeral followed by the word thousands, million, billions, trillions, etc. If the number is that big it might be a good idea to round up some digits so that your rider remembers it. Example: Number 879,261 could also be writed as 879.2 thousands, in a sentence, since it is considered to be a big number\n\nWhat numbers are before and after 879,261\n\nPrevious number is: 879,260\n\nNext number is: 879,262" ]
[ null ]
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https://gateway.ipfs.io/ipfs/QmXoypizjW3WknFiJnKLwHCnL72vedxjQkDDP1mXWo6uco/wiki/Galois_connection.html
[ "Galois connection\n\nIn mathematics, especially in order theory, a Galois connection is a particular correspondence (typically) between two partially ordered sets (posets). The same notion can also be defined on preordered sets or classes; this article presents the common case of posets. Galois connections generalize the correspondence between subgroups and subfields investigated in Galois theory (named after the French mathematician Évariste Galois). They find applications in various mathematical theories.\n\nA Galois connection is rather weak compared to an order isomorphism between the involved posets, but every Galois connection gives rise to an isomorphism of certain sub-posets, as will be explained below.\n\nThe literature contains two closely related notions of \"Galois connection\". In this article, we will distinguish between the two by referring to the first as (monotone) Galois connection and to the second as antitone Galois connection.\n\nThe term Galois correspondence is sometimes used to mean bijective Galois connection; this is simply an order isomorphism (or dual order isomorphism, depending on whether we take monotone or antitone Galois connections).\n\nDefinitions\n\n(Monotone) Galois connection\n\nLet (A, ≤) and (B, ≤) be two partially ordered sets. A monotone Galois connection between these posets consists of two monotone functions: F : AB and G : BA, such that for all a in A and b in B, we have\n\nF(a) ≤ b if and only if aG(b).\n\nIn this situation, F is called the lower adjoint of G and G is called the upper adjoint of F. Mnemonically, the upper/lower terminology refers to where the function application appears relative to ≤; the term \"adjoint\" refers to the fact that monotone Galois connections are special cases of pairs of adjoint functors in category theory as discussed further below. Other terminology encountered here is left adjoint (resp. right adjoint) for the lower (resp. upper) adjoint.\n\nAn essential property of a Galois connection is that an upper/lower adjoint of a Galois connection uniquely determines the other:\n\nF(a) is the least element with aG(), and\nG(b) is the largest element with F() ≤ b.\n\nA consequence of this is that if F or G is invertible, then each is the inverse of the other, i.e. F = G −1 .\n\nGiven a Galois connection with lower adjoint F and upper adjoint G, we can consider the compositions GF : AA, known as the associated closure operator, and FG : BB, known as the associated kernel operator. Both are monotone and idempotent, and we have aGF(a) for all a in A and FG(b) ≤ b for all b in B.\n\nA Galois insertion of A into B is a Galois connection in which the closure operator GF is the identity on A.\n\nAntitone Galois connection\n\nThe above definition is common in many applications today, and prominent in lattice and domain theory. However the original notion in Galois theory is slightly different. In this alternative definition, a Galois connection is a pair of antitone, i.e. order-reversing, functions F : AB and G : BA between two posets A and B, such that\n\nbF(a) if and only if aG(b).\n\nThe symmetry of F and G in this version erases the distinction between upper and lower, and the two functions are then called polarities rather than adjoints. Each polarity uniquely determines the other, since\n\nF(a) is the largest element b with aG(b), and\nG(b) is the largest element a with bF(a).\n\nThe compositions GF : AA and FG : BB are the associated closure operators; they are monotone idempotent maps with the property aGF(a) for all a in A and bFG(b) for all b in B.\n\nThe implications of the two definitions of Galois connections are very similar, since an antitone Galois connection between A and B is just a monotone Galois connection between A and the order dual Bop of B. All of the below statements on Galois connections can thus easily be converted into statements about antitone Galois connections.\n\nExamples\n\nMonotone Galois connections\n\nPower set; implication and conjunction\n\nFor an order theoretic example, let U be some set, and let A and B both be the power set of U, ordered by inclusion. Pick a fixed subset L of U. Then the maps F and G, where F(M) = LM, and G(N) = N ∪ (U\\L), form a monotone Galois connection, with F being the lower adjoint. A similar Galois connection whose lower adjoint is given by the meet (infimum) operation can be found in any Heyting algebra. Especially, it is present in any Boolean algebra, where the two mappings can be described by F(x) = (ax) and G(y) = (y ∨ ¬a) = (ay). In logical terms: \"implication from a\" is the upper adjoint of \"conjunction with a\".\n\nLattices\n\nFurther interesting examples for Galois connections are described in the article on completeness properties. Roughly speaking, it turns out that the usual functions ∨ and ∧ are lower and upper adjoints to the diagonal map XX × X. The least and greatest elements of a partial order are given by lower and upper adjoints to the unique function X → {1}. Going further, even complete lattices can be characterized by the existence of suitable adjoints. These considerations give some impression of the ubiquity of Galois connections in order theory.\n\nTransitive group actions\n\nLet G act transitively on X and pick some point x in X. Consider", null, "the set of blocks containing x. Further, let", null, "consist of the subgroups of G containing the stabilizer of x.\n\nThen, the correspondence", null, ":", null, "is a monotone, one-to-one Galois connection. As a corollary, one can establish that doubly transitive actions have no blocks other than the trivial ones (singletons or the whole of X): this follows from the stabilizers being maximal in G in that case. See doubly transitive group for further discussion.\n\nImage and inverse image\n\nIf f  : XY is a function, then for any subset M of X we can form the image F(M) = f (M) = {f(m) | mM} and for any subset N of Y we can form the inverse image G(N) = f −1(N) = {xX | f(x) ∈ N}. Then F and G form a monotone Galois connection between the power set of X and the power set of Y, both ordered by inclusion ⊆. There is a further adjoint pair in this situation: for a subset M of X, define H(M) = {yY | f −1({y}) ⊆ M}. Then G and H form a monotone Galois connection between the power set of Y and the power set of X. In the first Galois connection, G is the upper adjoint, while in the second Galois connection it serves as the lower adjoint.\n\nIn the case of a quotient map between algebraic objects (such as groups), this connection is called the lattice theorem: subgroups of G connect to subgroups of G/N, and the closure operator on subgroups of G is given by H = HN.\n\nSpan and closure\n\nPick some mathematical object X that has an underlying set, for instance a group, ring, vector space, etc. For any subset S of X, let F(S) be the smallest subobject of X that contains S, i.e. the subgroup, subring or subspace generated by S. For any subobject U of X, let G(U) be the underlying set of U. (We can even take X to be a topological space, let F(S) the closure of S, and take as \"subobjects of X\" the closed subsets of X.) Now F and G form a monotone Galois connection between subsets of X and subobjects of X, if both are ordered by inclusion. F is the lower adjoint.\n\nSyntax and semantics\n\nA very general comment of William Lawvere is that syntax and semantics are adjoint: take A to be the set of all logical theories (axiomatizations), and B the power set of the set of all mathematical structures. For a theory TA, let F(T) be the set of all structures that satisfy the axioms T; for a set of mathematical structures S, let G(S) be the minimum of the axiomatizations which approximate S. We can then say that F(T) is a subset of S if and only if T logically implies G(S): the \"semantics functor\" F and the \"syntax functor\" G form a monotone Galois connection, with semantics being the lower adjoint.\n\nAntitone galois connections\n\nGalois theory\n\nThe motivating example comes from Galois theory: suppose L/K is a field extension. Let A be the set of all subfields of L that contain K, ordered by inclusion ⊆. If E is such a subfield, write Gal(L/E) for the group of field automorphisms of L that hold E fixed. Let B be the set of subgroups of Gal(L/K), ordered by inclusion ⊆. For such a subgroup G, define Fix(G) to be the field consisting of all elements of L that are held fixed by all elements of G. Then the maps E ↦ Gal(L/E) and G ↦ Fix(G) form an antitone Galois connection.\n\nAlgebraic topology: covering spaces\n\nAnalogously, given a path-connected topological space X, there is an antitone Galois connection between subgroups of the fundamental group π1(X) and path-connected covering spaces of X. In particular, if X is semi-locally simply connected, then for every subgroup G of π1(X), there is a covering space with G as its fundamental group.\n\nLinear algebra: annihilators and orthogonal complements\n\nGiven an inner product space V, we can form the orthogonal complement F(X) of any subspace X of V. This yields an antitone Galois connection between the set of subspaces of V and itself, ordered by inclusion; both polarities are equal to F.\n\nGiven a vector space V and a subset X of V we can define its annihilator F(X), consisting of all elements of the dual space V of V that vanish on X. Similarly, given a subset Y of V, we define its annihilator G(Y) = {xV | φ(x) = 0 ∀φY}. This gives an antitone Galois connection between the subsets of V and the subsets of V.\n\nAlgebraic geometry\n\nIn algebraic geometry, the relation between sets of polynomials and their zero sets is an antitone Galois connection.\n\nFix a natural number n and a field K and let A be the set of all subsets of the polynomial ring K[X1, ..., Xn] ordered by inclusion ⊆, and let B be the set of all subsets of Kn ordered by inclusion ⊆. If S is a set of polynomials, define the variety of zeros as", null, "the set of common zeros of the polynomials in S. If U is a subset of Kn, define I(U) as an ideal of polynomials vanishing on U, that is", null, "Then V and I form an antitone Galois connection.\n\nThe closure on Kn is the closure in the Zariski topology, and if the field K is algebraically closed, then the closure on the polynomial ring is the radical of ideal generated by S.\n\nMore generally, given a commutative ring R (not necessarily a polynomial ring), there is an antitone Galois connection between radical ideals in the ring and subvarieties of the affine variety Spec(R).\n\nMore generally, there is an antitone Galois connection between ideals in the ring and subschemes of the corresponding affine variety.\n\nConnections on power sets arising from binary relations\n\nSuppose X and Y are arbitrary sets and a binary relation R over X and Y is given. For any subset M of X, we define F(M) = {yY | mRymM}. Similarly, for any subset N of Y, define G(N) = {xX | xRnnN}. Then F and G yield an antitone Galois connection between the power sets of X and Y, both ordered by inclusion ⊆.\n\nMany antitone Galois connections arise in this way; examples include the original connection from Galois theory, the connections in linear algebra and the connection from algebraic geometry explained above.\n\nProperties\n\nIn the following, we consider a (monotone) Galois connection f = (f , f), where f  : AB is the lower adjoint as introduced above. Some helpful and instructive basic properties can be obtained immediately. By the defining property of Galois connections, f (x) ≤ f (x) is equivalent to xf(f (x)), for all x in A. By a similar reasoning (or just by applying the duality principle for order theory), one finds that f (f(y)) ≤ y, for all y in B. These properties can be described by saying the composite f f is deflationary, while ff  is inflationary (or extensive).\n\nNow consider x, yA such that xy, then using the above one obtains xf(f (y)). Applying the basic property of Galois connections, one can now conclude that f (x) ≤ f (y). But this just shows that f  preserves the order of any two elements, i.e. it is monotone. Again, a similar reasoning yields monotonicity of f. Thus monotonicity does not have to be included in the definition explicitly. However, mentioning monotonicity helps to avoid confusion about the two alternative notions of Galois connections.\n\nAnother basic property of Galois connections is the fact that f(f (f(x))) = f(x), for all x in B. Clearly we find that\n\nf(f (f(x))) ≥ f(x).\n\nbecause ff  is inflationary as shown above. On the other hand, since f f is deflationary, while f is monotonic, one finds that\n\nf(f (f(x))) ≤ f(x).\n\nThis shows the desired equality. Furthermore, we can use this property to conclude that\n\nf (f(f (f(x)))) = f (f(x))\n\nand\n\nf(f (f(f (x)))) = f(f (x))\n\ni.e., f f and ff  are idempotent.\n\nIt can be shown (see Blyth or Erné for proofs) that a function f is a lower (resp. upper) adjoint if and only if f is a residuated mapping (resp. residual mapping). Therefore, the notion of residuated mapping and monotone Galois connection are essentially the same.\n\nClosure operators and Galois connections\n\nThe above findings can be summarized as follows: for a Galois connection, the composite ff  is monotone (being the composite of monotone functions), inflationary, and idempotent. This states that ff  is in fact a closure operator on A. Dually, f f is monotone, deflationary, and idempotent. Such mappings are sometimes called kernel operators. In the context of frames and locales, the composite ff  is called the nucleus induced by f . Nuclei induce frame homomorphisms; a subset of a locale is called a sublocale if it is given by a nucleus.\n\nConversely, any closure operator c on some poset A gives rise to the Galois connection with lower adjoint f  being just the corestriction of c to the image of c (i.e. as a surjective mapping the closure system c(A)). The upper adjoint f is then given by the inclusion of c(A) into A, that maps each closed element to itself, considered as an element of A. In this way, closure operators and Galois connections are seen to be closely related, each specifying an instance of the other. Similar conclusions hold true for kernel operators.\n\nThe above considerations also show that closed elements of A (elements x with f(f (x)) = x) are mapped to elements within the range of the kernel operator f f, and vice versa.\n\nExistence and uniqueness of Galois connections\n\nAnother important property of Galois connections is that lower adjoints preserve all suprema that exist within their domain. Dually, upper adjoints preserve all existing infima. From these properties, one can also conclude monotonicity of the adjoints immediately. The adjoint functor theorem for order theory states that the converse implication is also valid in certain cases: especially, any mapping between complete lattices that preserves all suprema is the lower adjoint of a Galois connection.\n\nIn this situation, an important feature of Galois connections is that one adjoint uniquely determines the other. Hence one can strengthen the above statement to guarantee that any supremum-preserving map between complete lattices is the lower adjoint of a unique Galois connection. The main property to derive this uniqueness is the following: For every x in A, f (x) is the least element y of B such that xf(y). Dually, for every y in B, f(y) is the greatest x in A such that f (x) ≤ y. The existence of a certain Galois connection now implies the existence of the respective least or greatest elements, no matter whether the corresponding posets satisfy any completeness properties. Thus, when one upper adjoint of a Galois connection is given, the other upper adjoint can be defined via this same property.\n\nOn the other hand, some monotone function f  is a lower adjoint if and only if each set of the form {xA | f (x) ≤ b}, for b in B, contains a greatest element. Again, this can be dualized for the upper adjoint.\n\nGalois connections as morphisms\n\nGalois connections also provide an interesting class of mappings between posets which can be used to obtain categories of posets. Especially, it is possible to compose Galois connections: given Galois connections (f , f) between posets A and B and (g, g) between B and C, the composite (gf , fg) is also a Galois connection. When considering categories of complete lattices, this can be simplified to considering just mappings preserving all suprema (or, alternatively, infima). Mapping complete lattices to their duals, this categories display auto duality, that are quite fundamental for obtaining other duality theorems. More special kinds of morphisms that induce adjoint mappings in the other direction are the morphisms usually considered for frames (or locales).\n\nConnection to category theory\n\nEvery partially ordered set can be viewed as a category in a natural way: there is a unique morphism from x to y if and only if xy. A monotone Galois connection is then nothing but a pair of adjoint functors between two categories that arise from partially ordered sets. In this context, the upper adjoint is the right adjoint while the lower adjoint is the left adjoint. However, this terminology is avoided for Galois connections, since there was a time when posets were transformed into categories in a dual fashion, i.e. with arrows pointing in the opposite direction. This led to a complementary notation concerning left and right adjoints, which today is ambiguous.\n\nApplications in the theory of programming\n\nGalois connections may be used to describe many forms of abstraction in the theory of abstract interpretation of programming languages.\n\nNotes\n\n1. Monotonicity follows from the following condition. See the discussion of the properties. It is only explicit in the definition to distinguish it from the alternative antitone definition. One can also define Galois connections as a pair of monotone functions that satisfy the laxer condition that for all x in A, xg(f (x)) and for all y in B, f(g(y)) ≤ y.\n2. Gierz, p. 23\n3. Bistarelli, Stefano (2004). Semirings for Soft Constraint Solving and Programming. Lecture Notes in Computer Science. 2962. Springer-Verlag. p. 102. ISBN 3-540-21181-0. ISSN 0302-9743.\n4. Galatos, p. 145\n5. See Alperin, Bell, Groups and Representations (GTM 162), p. 32\n6. William Lawvere, Adjointness in foundations, Dialectica, 1969, available here. The notation is different nowadays; an easier introduction by Peter Smith in these lecture notes, which also attribute the concept to the article cited.\n7. Patrick Cousot; Radhia Cousot (Jan 1977). \"Abstract Interpretation: A Unified Lattice Model for Static Analysis of Programs by Construction or Approximation of Fixpoints\". Proc. 4th ACM Symp. on Principles of Programming Languages (POPL) (PDF). pp. 238–252.\nFor a counterexample for the false theorem in Sect.7 (p.243 top right), see: Jochen Burghardt; Florian Kammüller; Jeff W. Sanders (Dec 2000). Isomorphism of Galois Embeddings (Technical report). GMD. p. 73. ISSN 1435-2702. 122.\n8. Patrick Cousot; Radhia Cousot (Jan 1979). \"Systematic Design of Program Analysis Frameworks\". Proc. 6th ACM Symp. on Principles of Programming Languages (POPL) (PDF). ACM Press. pp. 269–282.\n\nReferences\n\nThe following books and survey articles include Galois connections using the monotone definition:\n\n• Brian A. Davey and Hilary A. Priestley: Introduction to lattices and Order, Cambridge University Press, 2002.\n• Gerhard Gierz, Karl H. Hofmann, Klaus Keimel, Jimmie D. Lawson, Michael W. Mislove, Dana S. Scott: Continuous Lattices and Domains, Cambridge University Press, 2003.\n• Marcel Erné, Jürgen Koslowski, Austin Melton, George E. Strecker, A primer on Galois connections, in: Proceedings of the 1991 Summer Conference on General Topology and Applications in Honor of Mary Ellen Rudin and Her Work, Annals of the New York Academy of Sciences, Vol. 704, 1993, pp. 103–125. (Freely available online in various file formats PS.GZ PS, it presents many examples and results, as well as notes on the different notations and definitions that arose in this area.)\n\nSome publications using the original (antitone) definition:\n\n• Mac Lane, Saunders (September 1998). Categories for the Working Mathematician (Second ed.). Springer. ISBN 0-387-98403-8.\n• Thomas Scott Blyth, Lattices and Ordered Algebraic Structures, Springer, 2005, ISBN 1-85233-905-5.\n• Nikolaos Galatos, Peter Jipsen, Tomasz Kowalski, and Hiroakira Ono (2007), Residuated Lattices. An Algebraic Glimpse at Substructural Logics, Elsevier, ISBN 978-0-444-52141-5.\n• Garrett Birkhoff: Lattice Theory, Amer. Math. Soc. Coll. Pub., Vol 25, 1940\n• Øystein Ore: Galois Connexions, Transactions of the American Mathematical Society 55 (1944), pp. 493–513" ]
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https://wiki.eigenvector.com/index.php?title=Alignpeaks
[ "# Alignpeaks\n\n## Contents\n\n### Purpose\n\nCalibrates wavelength scale using standard peaks.\n\n### Synopsis\n\ns = alignpeaks(x0,x1,ax,options)\ny = alignpeaks(s,y1)\n\n### Description\n\nALIGNPEAKS calibrates a wavelength scale using standard peak positions. Ideally, the axis scale (x0) would apply to a single instrument at time t = 0 and t > 0 or for two different instruments. However, (x1) at t > 0 doesn't typically match (x0) at t = 0 even though the numbers in the scales are identical. The result is that a plot of (x0,y0) and (x0,y1) appear shifted from one another.\n\nThe inputs to ALIGNPEAKS are (x0) a 1xK vector containing the axis locations of K peaks on the standard instrument at t = 0 (e.g., the true wavelengths), (x1) a 1xK vector containing the axis locations of the corresponding peaks on the field / test instrument at t > 0 (e.g., the peak positions on the field instrument), and ax a 1xN vector containing the axis scale where N > K. ALIGNPEAKS finds a polynomial fit between (x0) and (x1) and outputs the result in the structure array (s). The output (y) is a fit of (x1).\n\n### Options\n\nOptional input (options) is a structure array with the following fields:\n\n• name: 'options', name indicating that this is an options structure,\n• plots: [ 'none' | {'final'} ] governs level of plotting, and\n• order: [ {2} ] integer giving the polynomial order.\n\nExecuting options = alignpeaks('options'); gives an empty options structure.\n\n### Example\n\nA measurements at t = 0 gives a spectrum (y0) with axis (ax), and measurements at t > 0 of the same sample yields a spectrum (y1) with the same axis (ax) but with peaks shifted. Therefore\n\nplot(ax,y0,'b',ax,y1,'r')\n\nshows a shift in the peaks. The peak positions at t = 0 are listed in (x0) and the peak positions at t > 0 are listed in (x1). The polynomial fit is given by\n\ns = alignpeaks(x0,x1,ax);\n\nand the transformed spectrum is obtained with\n\ny10 = alignpeaks(s,y1);\n\nso that\n\nplot(ax,y0,'b',ax,y1,'r')\n\nshows less of a peak shift. See alignpeaksdemo." ]
[ null ]
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https://www.basicitbangla.com/2020/09/adder.html
[ "## Latest:\n\nlatest\n\nAdder plays an important role in digital devices. The addition process of the digital circuits is performed by an adder.\n\nBy using adder all the mathematical procedures of computers are done. In much computational processing, adders are used in the ALU(Arithmetic Logic Unit ).\n\nKnow what are the subtractors in Digital Electronics.\n\nAdders are mainly two types. They are,\n\nIt adds two binary bits. It has no carry addition ability that's why it is called half adder.\n\nIt has the ability to add two bits and also it can add carry. That's why it is called a full adder.\n\n###", null, "For two single bits here we will get a sum and a carry as output for each input combination.\n\n A B Sum Carry 0 0 0 0 0 1 1 0 1 0 1 0 1 1 0 1\n\nA truth table for half adder\n\n###", null, "In this circuit, there is a system that can add two bits and also two carries. It is called the Full adder. Let, 3 input sign of a full adder is A, B, Ci(Ci is the carry input) and two outputs are S(Addition) and Co(Carry output).\n\nHere is a truth table for a full adder circuit.\n\n Input Output A B Ci S Co 0 0 0 0 0 0 0 1 1 0 0 1 0 1 0 0 1 1 0 1 1 0 0 1 0 1 0 1 0 1 1 1 0 0 1 1 1 1 1 1\n\nOutput equation\n\nS = ĀB̄Cᵢ +ĀBC̄ᵢ + AB̄C̄ᵢ+ABCᵢ\n\nC₀ = ĀBCᵢ+AB̄Cᵢ+ABC̄ᵢ+ABC\n\nAnd also the equation of output carry can be modified like this -\n\nFrom modified equations of the addition of full adder (S) and carry output (Cₒ) the circuit diagram using X-OR gate will be like this-\n\nFull adder representation by using the basic logical gates\n\nA full adder can be represented by using the basic logic gates only. The circuit diagram is given below-\n\nThe full adder reduces the complexity of a logical circuit.\n\nWe have to use two half adders and also we need an extra OR gate for adding the carries for designing a full adder using a half adder.\n\nLet, the input signal for full adder is X and Y, carry Cᵢ and outputs are S (Addition) Co(Carry).\n\nIn the figure, if we see for the first half adder-\n\nSum,\nS₁ = X⊕Y ----(1)\n\nCarry\n\nC₁ = XY------(2)\n\nSum,\n\nS₂ = S₁⊕Cᵢ\n= X⊕Y⊕Cᵢ [From (1)]\n= S\n\nNow,\n\nC₂ = S₁Cᵢ = (X⊕Y)Cᵢ-----(3)\n\nNow total carry(C₀) will be the addition of first half adder carry(C₁) and second half adder carry(C₂)\n\nSo,\n\nC₀ = C₁+C₂ = XY+(X⊕Y)Cᵢ [From (2) and (3) ]\n\nThis is the full adder carry.\nFrom here we get,\nSum of full adder output, S = X⊕Y⊕Cᵢ\nTotal carry of the full adder, C₀ = XY+(X⊕Y)Cᵢ\n\nLet the 3 input signals of full adder are X, Y, Cᵢ ( Cᵢ is the carry input) and outputs are S(Sum) Cₒ (Carry output). The truth table for the full adder is given below.\n\n Input Output X Y Cᵢ S Cₒ 0 0 0 0 0 0 0 1 1 0 0 1 0 1 0 0 1 1 0 1 1 0 0 1 0 1 0 1 0 1 1 1 0 0 1 1 1 1 1 1\n\nSo, considering  all S = 1  we get,\n\nAgain for all Cₒ = 1, we get,\n\nHere is the diagram of the half adder to the full adder circuit." ]
[ null, "https://3.bp.blogspot.com/-EEO1TxoF_1o/XDA06xDCEhI/AAAAAAAAEaI/lPWQU-7SX6Ed9aGSJPSymdwCtaM_wLbyACPcBGAYYCw/s320/Half%2Badder%2Blogo%2Bfor%2Btwo%2Bsingle%2Bbits.png", null, "https://4.bp.blogspot.com/-l69H5h-zLeo/XHbL3hhGFCI/AAAAAAAAFTk/0vTRu0ef9NUfwNVte6z5NJHCFlEhewvcwCPcBGAYYCw/s1600/Full%2Badder.png", null ]
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https://docs.oracle.com/cd/B40099_02/books/eScript/eScript_JSReference189.html
[ "## Function Objects\n\nA Function object holds the definition of a function defined in eScript. In eScript, procedures are functions.\n\n##### Syntax A\n\nfunction funcName( [arg1 [, ..., argn]] )\n{\nbody\n}\n\n##### Syntax B\n\nvar funcName = new Function([arg1 [, ..., argn,]] body );\n\nParameter\nDescription\n\nfuncName\n\nThe name of the function to be created\n\narg1 [, ..., argn]\n\nAn optional list of parameters that the function accepts\n\nbody\n\nThe lines of code that the function executes\n\n##### Returns\n\nWhatever its code is set up to return. For more information, see return Statement.\n\n##### Usage\n\nSyntax A is the standard method for defining a function. Syntax B is an alternative way to create a function and is used to create Function objects explicitly.\n\nNote the difference in case of the keyword Function between Syntax A and Syntax B. Function objects created with Syntax B (that is, the Function constructor) are evaluated each time they are used. This is less efficient than Syntax A—declaring a function and calling it within your code—because declared functions are compiled instead of interpreted.\n\n##### Example\n\nThe following fragment of code illustrates creating a function AddTwoNumbers using a declaration:\n\n{\nreturn (a + b);\n}\n\nThe following fragment illustrates creating the same function using the Function constructor:\n\nAddTwoNumbers = new Function (\"a\", \"b\", \"return (a + b)\");\n\nThe difference between the two is that when AddTwoNumbers is created using a declaration, AddTwoNumbers is the name of a function, whereas when AddTwoNumbers is created using the Function constructor, AddTwoNumbers is the name of a variable whose current value is a reference to the function created using the Function constructor.\n\n#### length Property\n\nThe length property returns the number of parameters expected by the function.\n\n##### Syntax\n\nfuncName.length\n\nParameter\nDescription\n\nfuncName\n\nThe function whose length property is to be found\n\n##### Returns\n\nThe number of parameters expected by funcName.\n\n#### return Statement\n\nThe return statement passes a value back to the function that called it.\n\n##### Syntax\n\nreturn value\n\nParameter\nDescription\n\nvalue\n\nThe result produced by the function\n\n##### Usage\n\nThe return statement passes a value back to the function that called it. Any code in a function following the execution of a return statement is not executed.\n\n##### Example\n\nThis function returns a value equal to the number passed to it multiplied by 2 and divided by 5.\n\nfunction DoubleAndDivideBy5(a)\n{\nreturn (a*2)/5\n}\n\nThe following code fragment show an example of a script using the preceding function. This script calculates the mathematical expression `n = (10 * 2) / 5 + (20 * 2) / 5. `It then displays the value for `n`, which is 12.\n\nfunction myFunction()\n{\nvar a = DoubleAndDivideBy5(10);\nvar b = DoubleAndDivideBy5(20);\nTheApplication().RaiseErrorText(a + b);\n}" ]
[ null ]
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https://www.colorhexa.com/dbf7ce
[ "# #dbf7ce Color Information\n\nIn a RGB color space, hex #dbf7ce is composed of 85.9% red, 96.9% green and 80.8% blue. Whereas in a CMYK color space, it is composed of 11.3% cyan, 0% magenta, 16.6% yellow and 3.1% black. It has a hue angle of 101 degrees, a saturation of 71.9% and a lightness of 88.8%. #dbf7ce color hex could be obtained by blending #ffffff with #b7ef9d. Closest websafe color is: #ccffcc.\n\n• R 86\n• G 97\n• B 81\nRGB color chart\n• C 11\n• M 0\n• Y 17\n• K 3\nCMYK color chart\n\n#dbf7ce color description : Light grayish green.\n\n# #dbf7ce Color Conversion\n\nThe hexadecimal color #dbf7ce has RGB values of R:219, G:247, B:206 and CMYK values of C:0.11, M:0, Y:0.17, K:0.03. Its decimal value is 14415822.\n\nHex triplet RGB Decimal dbf7ce `#dbf7ce` 219, 247, 206 `rgb(219,247,206)` 85.9, 96.9, 80.8 `rgb(85.9%,96.9%,80.8%)` 11, 0, 17, 3 101°, 71.9, 88.8 `hsl(101,71.9%,88.8%)` 101°, 16.6, 96.9 ccffcc `#ccffcc`\nCIE-LAB 94.328, -16.382, 16.693 73.612, 86.037, 71.118 0.319, 0.373, 86.037 94.328, 23.389, 134.461 94.328, -13.718, 27.613 92.756, -20.664, 19.471 11011011, 11110111, 11001110\n\n# Color Schemes with #dbf7ce\n\n• #dbf7ce\n``#dbf7ce` `rgb(219,247,206)``\n• #eacef7\n``#eacef7` `rgb(234,206,247)``\nComplementary Color\n• #f0f7ce\n``#f0f7ce` `rgb(240,247,206)``\n• #dbf7ce\n``#dbf7ce` `rgb(219,247,206)``\n• #cef7d6\n``#cef7d6` `rgb(206,247,214)``\nAnalogous Color\n• #f7cef0\n``#f7cef0` `rgb(247,206,240)``\n• #dbf7ce\n``#dbf7ce` `rgb(219,247,206)``\n• #d6cef7\n``#d6cef7` `rgb(214,206,247)``\nSplit Complementary Color\n• #f7cedb\n``#f7cedb` `rgb(247,206,219)``\n• #dbf7ce\n``#dbf7ce` `rgb(219,247,206)``\n• #cedbf7\n``#cedbf7` `rgb(206,219,247)``\nTriadic Color\n• #f7eace\n``#f7eace` `rgb(247,234,206)``\n• #dbf7ce\n``#dbf7ce` `rgb(219,247,206)``\n• #cedbf7\n``#cedbf7` `rgb(206,219,247)``\n• #eacef7\n``#eacef7` `rgb(234,206,247)``\nTetradic Color\n• #abec8c\n``#abec8c` `rgb(171,236,140)``\n• #bbf0a2\n``#bbf0a2` `rgb(187,240,162)``\n• #cbf3b8\n``#cbf3b8` `rgb(203,243,184)``\n• #dbf7ce\n``#dbf7ce` `rgb(219,247,206)``\n• #ebfbe4\n``#ebfbe4` `rgb(235,251,228)``\n• #fbfefa\n``#fbfefa` `rgb(251,254,250)``\n• #ffffff\n``#ffffff` `rgb(255,255,255)``\nMonochromatic Color\n\n# Alternatives to #dbf7ce\n\nBelow, you can see some colors close to #dbf7ce. Having a set of related colors can be useful if you need an inspirational alternative to your original color choice.\n\n• #e5f7ce\n``#e5f7ce` `rgb(229,247,206)``\n• #e2f7ce\n``#e2f7ce` `rgb(226,247,206)``\n• #def7ce\n``#def7ce` `rgb(222,247,206)``\n• #dbf7ce\n``#dbf7ce` `rgb(219,247,206)``\n• #d8f7ce\n``#d8f7ce` `rgb(216,247,206)``\n• #d4f7ce\n``#d4f7ce` `rgb(212,247,206)``\n• #d1f7ce\n``#d1f7ce` `rgb(209,247,206)``\nSimilar Colors\n\n# #dbf7ce Preview\n\nText with hexadecimal color #dbf7ce\n\nThis text has a font color of #dbf7ce.\n\n``<span style=\"color:#dbf7ce;\">Text here</span>``\n#dbf7ce background color\n\nThis paragraph has a background color of #dbf7ce.\n\n``<p style=\"background-color:#dbf7ce;\">Content here</p>``\n#dbf7ce border color\n\nThis element has a border color of #dbf7ce.\n\n``<div style=\"border:1px solid #dbf7ce;\">Content here</div>``\nCSS codes\n``.text {color:#dbf7ce;}``\n``.background {background-color:#dbf7ce;}``\n``.border {border:1px solid #dbf7ce;}``\n\n# Shades and Tints of #dbf7ce\n\nA shade is achieved by adding black to any pure hue, while a tint is created by mixing white to any pure color. In this example, #010200 is the darkest color, while #f4fdf0 is the lightest one.\n\n• #010200\n``#010200` `rgb(1,2,0)``\n• #081203\n``#081203` `rgb(8,18,3)``\n• #0f2306\n``#0f2306` `rgb(15,35,6)``\n• #163409\n``#163409` `rgb(22,52,9)``\n• #1e450b\n``#1e450b` `rgb(30,69,11)``\n• #25560e\n``#25560e` `rgb(37,86,14)``\n• #2c6711\n``#2c6711` `rgb(44,103,17)``\n• #337814\n``#337814` `rgb(51,120,20)``\n• #3a8816\n``#3a8816` `rgb(58,136,22)``\n• #429919\n``#429919` `rgb(66,153,25)``\n• #49aa1c\n``#49aa1c` `rgb(73,170,28)``\n• #50bb1f\n``#50bb1f` `rgb(80,187,31)``\n• #57cc21\n``#57cc21` `rgb(87,204,33)``\nShade Color Variation\n• #5fdb25\n``#5fdb25` `rgb(95,219,37)``\n• #6cde36\n``#6cde36` `rgb(108,222,54)``\n• #78e147\n``#78e147` `rgb(120,225,71)``\n• #84e458\n``#84e458` `rgb(132,228,88)``\n• #91e669\n``#91e669` `rgb(145,230,105)``\n• #9de97a\n``#9de97a` `rgb(157,233,122)``\n• #a9ec8b\n``#a9ec8b` `rgb(169,236,139)``\n• #b6ef9b\n``#b6ef9b` `rgb(182,239,155)``\n• #c2f1ac\n``#c2f1ac` `rgb(194,241,172)``\n• #cff4bd\n``#cff4bd` `rgb(207,244,189)``\n• #dbf7ce\n``#dbf7ce` `rgb(219,247,206)``\n• #e7fadf\n``#e7fadf` `rgb(231,250,223)``\n• #f4fdf0\n``#f4fdf0` `rgb(244,253,240)``\nTint Color Variation\n\n# Tones of #dbf7ce\n\nA tone is produced by adding gray to any pure hue. In this case, #e2e3e2 is the less saturated color, while #d9fec7 is the most saturated one.\n\n• #e2e3e2\n``#e2e3e2` `rgb(226,227,226)``\n• #e1e5e0\n``#e1e5e0` `rgb(225,229,224)``\n• #e1e8dd\n``#e1e8dd` `rgb(225,232,221)``\n• #e0eadb\n``#e0eadb` `rgb(224,234,219)``\n• #dfecd9\n``#dfecd9` `rgb(223,236,217)``\n• #deeed7\n``#deeed7` `rgb(222,238,215)``\n• #ddf0d5\n``#ddf0d5` `rgb(221,240,213)``\n• #ddf3d2\n``#ddf3d2` `rgb(221,243,210)``\n• #dcf5d0\n``#dcf5d0` `rgb(220,245,208)``\n• #dbf7ce\n``#dbf7ce` `rgb(219,247,206)``\n• #daf9cc\n``#daf9cc` `rgb(218,249,204)``\n• #d9fbca\n``#d9fbca` `rgb(217,251,202)``\n• #d9fec7\n``#d9fec7` `rgb(217,254,199)``\nTone Color Variation\n\n# Color Blindness Simulator\n\nBelow, you can see how #dbf7ce is perceived by people affected by a color vision deficiency. This can be useful if you need to ensure your color combinations are accessible to color-blind users.\n\nMonochromacy\n• Achromatopsia 0.005% of the population\n• Atypical Achromatopsia 0.001% of the population\nDichromacy\n• Protanopia 1% of men\n• Deuteranopia 1% of men\n• Tritanopia 0.001% of the population\nTrichromacy\n• Protanomaly 1% of men, 0.01% of women\n• Deuteranomaly 6% of men, 0.4% of women\n• Tritanomaly 0.01% of the population" ]
[ null ]
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http://sigma.ontologyportal.org:8080/sigma/TreeView.jsp?lang=EnglishLanguage&flang=traditionalLogic&kb=SUMO&term=date
[ "", null, "", null, "Browsing Interface : Welcome guest : log in [  Home |  Graph |  ]  KB:  SUMO Language:  AlbanianLanguageArabicLanguageBasqueLanguageBulgarianLanguageCatalanLanguageChineseLanguageCroatianLanguageDanishLanguageEnglishLanguageFarsiLanguageFinnishLanguageFrenchLanguageGalicianLanguageGreekLanguageHebrewLanguageIcelandicLanguageIndonesianLanguageItalianLanguageJapaneseLanguageMalayLanguageNorwegianBokmalLanguageNorwegianNorskLanguagePolishLanguagePortugueseLanguageSpanishLanguageSwedishLanguageTaiwanChineseLanguageThaiLanguagede   Formal Language:  OWLSUO-KIFTPTPtraditionalLogic\n\n KB Term:", null, "Term intersection", null, "English Word:", null, "Any Noun Verb Adjective Adverb", null, "", null, "", null, "date", null, "Sigma KEE - date\n date\n\n appearance as argument number 1", null, "s__documentation(s__date__m,s__ChineseLanguage,'这是一个 BinaryPredicate, 它以绝对日历时间,以一天为限, 为特定的 Object 或 Process 指定一个 TimePosition。') Merge.kif 8660-8661 s__documentation(s__date__m,s__EnglishLanguage,'A BinaryPredicate that specifies a TimePosition in absolute calendar time, at the resolution of one day, for a particular Object or Process.') Merge.kif 8657-8659 s__domain(s__date__m,1,s__Physical) Merge.kif 8654-8654 The number 1 argument of date is an instance of physical s__domain(s__date__m,2,s__Day) Merge.kif 8655-8655 The number 2 argument of date is an instance of day s__instance(s__date__m,s__AsymmetricRelation) Merge.kif 8653-8653 date is an instance of asymmetric relation s__instance(s__date__m,s__BinaryPredicate) Merge.kif 8651-8651 date is an instance of binary predicate s__instance(s__SingleValuedRelation,s__SetOrClass) Merge.kif 8652-8652 date is an instance of single valued relation s__subrelation(s__date__m,s__time__m) Merge.kif 8656-8656 date is a subrelation of time\n\n appearance as argument number 2", null, "s__format(s__ChineseLanguage,s__date__m,'%1 的 date %n 是 %2') chinese_format.kif 441-441 s__format(s__EnglishLanguage,s__date__m,'date of %1 is %n %2') english_format.kif 266-266 s__termFormat(s__ChineseLanguage,s__date__m,'日期') chinese_format.kif 442-442 \"日期\" is the printable form of date in ChineseLanguage s__termFormat(s__EnglishLanguage,s__date__m,'date') domainEnglishFormat.kif 3522-3522 \"date\" is the printable form of date in english language\n\n antecedent", null, "( ∀ [V__TEXT,V__EDITION1,V__EDITION2,V__INT2,V__DATE1,V__INT1,V__DATE2,V__PUB1,V__PUB2,V__CBO1,V__CBO2]    ((s__subclass(V__TEXT,s__ContentBearingObject)s__and__ms__subclass(V__EDITION1,s__ContentBearingObject)s__and__ms__instance(V__EDITION1,s__SetOrClass)s__and__ms__subclass(V__EDITION2,s__ContentBearingObject)s__and__ms__instance(V__EDITION2,s__SetOrClass)s__and__ms__instance(V__INT2,s__PositiveInteger)s__and__ms__instance(V__DATE1,s__Day)s__and__ms__instance(V__INT1,s__PositiveInteger)s__and__ms__instance(V__DATE2,s__Day))     s__=>(((s__EditionFn(V__TEXT,V__INT1)         s__equal__mV__EDITION1)s__and__m(s__EditionFn(V__TEXT,V__INT2)       s__equal__mV__EDITION2)s__and__ms__greaterThan(V__INT2,V__INT1)     s__and__ms__instance(V__PUB1,s__Publication)s__and__ms__instance(V__PUB2,s__Publication)s__and__ms__instance(V__CBO1,V__EDITION1)   s__and__ms__instance(V__CBO2,V__EDITION2) s__and__ms__patient(V__PUB1,V__CBO1) s__and__ms__patient(V__PUB2,V__CBO2) s__and__ms__date(V__PUB1,V__DATE1) s__and__ms__date(V__PUB2,V__DATE2)) s__=>s__before(s__EndFn(V__DATE1) ,s__EndFn(V__DATE2)))) ) Merge.kif 15632-15649 If edition a positive integer of a kind of content bearing object is equal to another kind of content bearing object and edition another positive integer of a kind of content bearing object is equal to a third kind of content bearing object and the other positive integer is greater than the positive integer and a process is an instance of publication and another process is an instance of publication and an entity is an instance of another kind of content bearing object and another entity is an instance of a third kind of content bearing object and the entity is a patient of the process and the other entity is a patient of the other process and date of the process is a day and date of the other process is another day,then the end of the day happens before the end of the other day ( ∀ [V__DateOfWithdrawal,V__MaturityDate,V__CD,V__Withdrawal]    ((s__instance(V__DateOfWithdrawal,s__Day)s__and__ms__instance(V__MaturityDate,s__Day))     s__=>((s__instance(V__CD,s__CertificateOfDeposit)s__and__ms__maturityDate(V__CD,V__MaturityDate)       s__and__ms__instance(V__Withdrawal,s__Withdrawal)s__and__ms__origin(V__Withdrawal,s__CurrencyFn(V__CD))   s__and__ms__date(V__Withdrawal,V__DateOfWithdrawal) s__and__ms__before(s__EndFn(V__DateOfWithdrawal) ,s__BeginFn(V__MaturityDate))) s__=>(s__exists__m[V__Penalty] (s__instance(V__Penalty,s__Penalty)s__and__ms__destination(V__Penalty,s__CurrencyFn(V__CD)) s__and__ms__causes(V__Withdrawal,V__Penalty))))) ) FinancialOntology.kif 1032-1044 If a financial account is an instance of certificate of deposit and a day is a maturity date of the financial account and a process is an instance of withdrawal and the process originates at the currency of the financial account and date of the process is another day and the end of the other day happens before the beginning of the day,then there exists another process such that the other process is an instance of penalty and the other process ends up at the currency of the financial account and the process causes the other process ( ∀ [V__Amount,V__Day,V__Account,V__Amount1,V__Transaction,V__Cash]    ((s__instance(V__Amount,s__CurrencyMeasure)s__and__ms__instance(V__Day,s__Day)s__and__ms__instance(V__Account,s__FinancialAccount)s__and__ms__instance(V__Amount1,s__Quantity))     s__=>((s__instance(V__Transaction,s__FinancialTransaction)s__and__ms__origin(V__Transaction,s__CurrencyFn(V__Account))     s__and__ms__transactionAmount(V__Transaction,V__Amount)   s__and__ms__instance(V__Cash,s__Currency)s__and__ms__patient(V__Transaction,V__Cash) s__and__ms__date(V__Transaction,V__Day)) s__=>(s__exists__m[V__Amount2] (s__instance(V__Amount2,s__CurrencyMeasure)s__and__m(s__availableCash(V__Account,V__Day,V__Amount2) s__and__ms__greaterThanOrEqualTo(V__Amount1,V__Amount2)))))) ) FinancialOntology.kif 3675-3686 If a financial transaction is an instance of financial transaction and the financial transaction originates at the currency of a financial account and a currency measure is a transaction amount of the financial transaction and an entity is an instance of currency and the entity is a patient of the financial transaction and date of the financial transaction is a day,then there exists the currency measure2 such that the available cash of the financial account on the day is the currency measure2 and the currency measure1 is greater than or equal to the currency measure2 ( ∀ [V__Amount,V__Day,V__Account,V__Amount1,V__Transaction]    ((s__instance(V__Amount,s__CurrencyMeasure)s__and__ms__instance(V__Day,s__Day)s__and__ms__instance(V__Account,s__FinancialAccount)s__and__ms__instance(V__Account,s__Object)s__and__ms__instance(V__Amount1,s__Quantity))     s__=>((s__instance(V__Transaction,s__FinancialTransaction)s__and__ms__origin(V__Transaction,V__Account)       s__and__ms__transactionAmount(V__Transaction,V__Amount)     s__and__ms__date(V__Transaction,V__Day)) s__=>(s__exists__m[V__Amount2]    (s__instance(V__Amount2,s__CurrencyMeasure)s__and__m(s__availableBalance(V__Account,V__Day,V__Amount2)   s__and__ms__greaterThanOrEqualTo(V__Amount1,V__Amount2)))))) ) FinancialOntology.kif 3655-3664 If a financial transaction is an instance of financial transaction and the financial transaction originates at a financial account and a currency measure is a transaction amount of the financial transaction and date of the financial transaction is a day,then there exists the currency measure2 such that the available balance of the financial account on the day is the currency measure2 and the currency measure1 is greater than or equal to the currency measure2 ( ∀ [V__TEXT,V__INT2,V__DATE1,V__INT1,V__DATE2,V__VOLUME2,V__VOLUME1,V__PUB1,V__PUB2,V__CBO1,V__CBO2]    ((s__subclass(V__TEXT,s__Series)s__and__ms__instance(V__TEXT,s__SetOrClass)s__and__ms__instance(V__INT2,s__PositiveInteger)s__and__ms__instance(V__DATE1,s__Day)s__and__ms__instance(V__INT1,s__PositiveInteger)s__and__ms__instance(V__DATE2,s__Day)s__and__ms__subclass(V__VOLUME2,s__Text)s__and__ms__instance(V__VOLUME2,s__SetOrClass)s__and__ms__subclass(V__VOLUME1,s__Text)s__and__ms__instance(V__VOLUME1,s__SetOrClass))     s__=>((s__subclass(V__TEXT,s__Periodical)s__and__m(s__SeriesVolumeFn(V__TEXT,V__INT1)       s__equal__mV__VOLUME1)s__and__m(s__SeriesVolumeFn(V__TEXT,V__INT2)     s__equal__mV__VOLUME2)s__and__ms__greaterThan(V__INT2,V__INT1)   s__and__ms__instance(V__PUB1,s__Publication)s__and__ms__instance(V__PUB2,s__Publication)s__and__ms__instance(V__CBO1,V__VOLUME1) s__and__ms__instance(V__CBO2,V__VOLUME2) s__and__ms__patient(V__PUB1,V__CBO1) s__and__ms__patient(V__PUB2,V__CBO2) s__and__ms__date(V__PUB1,V__DATE1) s__and__ms__date(V__PUB2,V__DATE2)) s__=>s__before(s__EndFn(V__DATE1) ,s__EndFn(V__DATE2)))) ) Mid-level-ontology.kif 12368-12382 If a kind of series is a subclass of periodical and volume a positive integer in the series a kind of series is equal to a kind of text and volume another positive integer in the series the kind of series is equal to another kind of text and the other positive integer is greater than the positive integer and a process is an instance of publication and another process is an instance of publication and an entity is an instance of a kind of text and another entity is an instance of another kind of text and the entity is a patient of the process and the other entity is a patient of the other process and date of the process is a day and date of the other process is another day,then the end of the day happens before the end of the other day ( ∀ [V__Amount,V__Date,V__Payment,V__DueDate,V__AmountDue,V__Account]    ((s__instance(V__Amount,s__CurrencyMeasure)s__and__ms__instance(V__Date,s__Day)s__and__ms__instance(V__Payment,s__FinancialTransaction)s__and__ms__instance(V__DueDate,s__TimeInterval)s__and__ms__instance(V__AmountDue,s__CurrencyMeasure))     s__=>((s__transactionAmount(V__Payment,V__Amount)       s__and__ms__date(V__Payment,V__Date)     s__and__ms__instance(V__Account,s__FinancialAccount)s__and__ms__destination(V__Payment,s__CurrencyFn(V__Account)) s__and__ms__amountDue(V__Account,V__AmountDue,V__DueDate) s__and__ms__before(s__EndFn(V__Date) ,s__BeginFn(V__DueDate))) s__=>s__instance(V__Payment,s__Prepayment))) ) FinancialOntology.kif 779-787 If a currency measure is a transaction amount of a financial transaction and date of the financial transaction is a day and a financial account is an instance of financial account and the financial transaction ends up at the currency of the financial account and the financial account amount due the currency measureDue for a time interval and the end of the day happens before the beginning of the time interval,then the financial transaction is an instance of prepayment\n\n consequent", null, "No TPTP formula. May not be expressible in strict first order. FinancialOntology.kif 615-627 If a financial account amount due a currency measure for a time position and a cognitive agent holds account the financial account,then the cognitive agent is obliged to perform tasks of type the class described by a symbolic string ( ∀ [V__Amount,V__Loan,V__Date]    ((s__instance(V__Amount,s__CurrencyMeasure)s__and__ms__instance(V__Loan,s__Loan)s__and__ms__instance(V__Date,s__TimePoint)s__and__ms__instance(V__Date,s__Day))     s__=>((s__downPayment(V__Loan,V__Amount)       s__and__ms__agreementEffectiveDate(V__Loan,V__Date))   s__=>(s__exists__m[V__Payment]      (s__instance(V__Payment,s__FinancialTransaction)s__and__m(s__transactionAmount(V__Payment,V__Amount)     s__and__ms__date(V__Payment,V__Date)   s__and__ms__destination(V__Payment,s__CurrencyFn(V__Loan))))))) ) FinancialOntology.kif 757-765 If a currency measure is a down payment of a loan and a time point is an agreement effective date of the loan,then there exists a financial transaction such that the currency measure is a transaction amount of the financial transaction and date of the financial transaction is the time point and the financial transaction ends up at the currency of the loan ( ∀ [V__Amount,V__Date,V__Balance,V__Account,V__FinancialAccount]    ((s__instance(V__Amount,s__CurrencyMeasure)s__and__ms__instance(V__Date,s__TimePoint)s__and__ms__instance(V__Date,s__Day)s__and__ms__instance(V__Balance,s__CurrencyMeasure)s__and__ms__instance(V__Account,s__FinancialAccount)s__and__ms__instance(V__FinancialAccount,s__SetOrClass))     s__=>((s__instance(V__Account,V__FinancialAccount)       s__and__ms__minimumBalance(V__Account,s__OpeningAnAccount,V__Balance))   s__=>(s__exists__m[V__Payment]      (s__instance(V__Payment,s__FinancialTransaction)s__and__m(s__destination(V__Payment,s__CurrencyFn(V__Account))   s__and__ms__transactionAmount(V__Payment,V__Amount) s__and__ms__greaterThanOrEqualTo(V__Amount,V__Balance) s__and__ms__agreementEffectiveDate(V__Account,V__Date) s__and__ms__date(V__Payment,V__Date)))))) ) FinancialOntology.kif 646-656 If a financial account is an instance of a set or class and the financial account minimum balance opening an account for a currency measure,then there exists a financial transaction such that the financial transaction ends up at the currency of the financial account and another currency measure is a transaction amount of the financial transaction and the other currency measure is greater than or equal to the currency measure and a time point is an agreement effective date of the financial account and date of the financial transaction is the time point ( ∀ [V__Amount,V__Date,V__Balance,V__Account,V__FinancialAccount]    ((s__instance(V__Amount,s__CurrencyMeasure)s__and__ms__instance(V__Date,s__Day)s__and__ms__instance(V__Balance,s__CurrencyMeasure)s__and__ms__instance(V__Account,s__FinancialAccount)s__and__ms__instance(V__FinancialAccount,s__SetOrClass))     s__=>((s__instance(V__Account,V__FinancialAccount)       s__and__ms__minimumBalance(V__Account,s__UsingAnAccount,V__Balance)     s__and__ms__currentAccountBalance(V__Account,V__Date,V__Amount)   s__and__ms__lessThan(V__Amount,V__Balance)) s__=>(s__exists__m[V__Penalty] (s__instance(V__Penalty,s__Penalty)s__and__ms__date(V__Penalty,V__Date) s__and__ms__destination(V__Penalty,s__CurrencyFn(V__Account)))))) ) FinancialOntology.kif 658-668 If a financial account is an instance of a set or class and the financial account minimum balance using an account for a currency measure and the financial account current account balance a day for another currency measure and the other currency measure is less than the currency measure,then there exists a process such that the process is an instance of penalty and date of the process is the day and the process ends up at the currency of the financial account No TPTP formula. May not be expressible in strict first order. FinancialOntology.kif 1353-1363 If a loan is an instance of balloon loan and a day is a maturity date of the loan and a currency measure is a total balance of the loan and the loan is the borrower of a cognitive agent,then the cognitive agent is obliged to perform tasks of type the class described by a symbolic string ( ∀ [V__P,V__D]    ((s__instance(V__P,s__Human)s__and__ms__instance(V__D,s__Day))     s__=>(s__birthdate(V__P,V__D)     s__=>(s__exists__m[V__B]        (s__instance(V__B,s__Birth)s__and__ms__experiencer(V__B,V__P)       s__and__ms__date(V__B,V__D))))) ) Mid-level-ontology.kif 21974-21980 If a day is a birthdate of a human,then there exists a process such that the process is an instance of birth and the human experiences the process and date of the process is the day ( ∀ [V__Date,V__Statement]    ((s__instance(V__Date,s__Day)s__and__ms__instance(V__Statement,s__BankStatement))     s__=>(s__dateOfStatement(V__Statement,V__Date)     s__=>(s__exists__m[V__Copy]        (s__instance(V__Copy,s__ContentBearingPhysical)s__and__m(s__containsInformation(V__Copy,V__Statement)       s__and__ms__date(V__Copy,V__Date)))))) ) FinancialOntology.kif 3867-3872 If a day is a date of statement of a bank statement,then there exists a content bearing physical such that the content bearing physical contains information the bank statement and date of the content bearing physical is the day ( ∀ [V__P,V__T]    ((s__instance(V__P,s__Human)s__and__ms__instance(V__T,s__Day))     s__=>(s__deathdate(V__P,V__T)     s__=>(s__exists__m[V__D]        (s__instance(V__D,s__Death)s__and__ms__experiencer(V__D,V__P)       s__and__ms__date(V__D,V__T))))) ) Mid-level-ontology.kif 21988-21994 If a day is a deathdate of a human,then there exists a process such that the process is an instance of death and the human experiences the process and date of the process is the day", null, "Show simplified definition (without tree view)\nShow simplified definition (with tree view)", null, "Sigma web home      Suggested Upper Merged Ontology (SUMO) web home\nSigma version 2.99c (>= 2017/11/20) is open source software produced by Articulate Software and its partners" ]
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https://brilliant.org/problems/sudoku-graph/
[ "# Sudoku Graph\n\nSudoku can be seen as a graph coloring problem, where the squares of the grid are vertices and the numbers are colors that must be different if in the same row, column, or $3 \\times 3$ grid (such vertices in the graph are connected by an edge). The sudoku is then a graph of 81 vertices and chromatic number 9. How many edges does this 81-vertex graph have?\n\n×" ]
[ null ]
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https://www.engineering-society.com/2018/08/what-is-reinforcement-ratio.html
[ "", null, "What is Reinforcement Ratio\n\n# What is Reinforcement Ratio\n\nWhat is reinforcement ratio. Reinforcement ratio can be defined as the ratio of area of steel to the area of concrete. It has no units because its only the ratio of areas. Reinforcement ratio shows how much steel are used in any structural members. Reinforcement ratio have different ranges for different structural members. Some of these ranges are as:\n• Reinforcement ratio for beam is 1-2%\n• Reinforcement ratio for column is 1-8%\n• Reinforcement ratio for footing is 0.8-1%\n• Reinforcement ratio for slab is 1%\n\nContinue Reading about the \"What is Reinforcement Ratio\" on the next page below" ]
[ null, "https://www.facebook.com/tr", null ]
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https://www.colorhexa.com/44b03a
[ "# #44b03a Color Information\n\nIn a RGB color space, hex #44b03a is composed of 26.7% red, 69% green and 22.7% blue. Whereas in a CMYK color space, it is composed of 61.4% cyan, 0% magenta, 67% yellow and 31% black. It has a hue angle of 114.9 degrees, a saturation of 50.4% and a lightness of 45.9%. #44b03a color hex could be obtained by blending #88ff74 with #006100. Closest websafe color is: #339933.\n\n• R 27\n• G 69\n• B 23\nRGB color chart\n• C 61\n• M 0\n• Y 67\n• K 31\nCMYK color chart\n\n#44b03a color description : Dark moderate lime green.\n\n# #44b03a Color Conversion\n\nThe hexadecimal color #44b03a has RGB values of R:68, G:176, B:58 and CMYK values of C:0.61, M:0, Y:0.67, K:0.31. Its decimal value is 4501562.\n\nHex triplet RGB Decimal 44b03a `#44b03a` 68, 176, 58 `rgb(68,176,58)` 26.7, 69, 22.7 `rgb(26.7%,69%,22.7%)` 61, 0, 67, 31 114.9°, 50.4, 45.9 `hsl(114.9,50.4%,45.9%)` 114.9°, 67, 69 339933 `#339933`\nCIE-LAB 63.822, -53.4, 49.521 18.672, 32.584, 9.308 0.308, 0.538, 32.584 63.822, 72.827, 137.159 63.822, -48.393, 65.911 57.082, -41.505, 30.289 01000100, 10110000, 00111010\n\n# Color Schemes with #44b03a\n\n• #44b03a\n``#44b03a` `rgb(68,176,58)``\n• #a63ab0\n``#a63ab0` `rgb(166,58,176)``\nComplementary Color\n• #7fb03a\n``#7fb03a` `rgb(127,176,58)``\n• #44b03a\n``#44b03a` `rgb(68,176,58)``\n• #3ab06b\n``#3ab06b` `rgb(58,176,107)``\nAnalogous Color\n• #b03a7f\n``#b03a7f` `rgb(176,58,127)``\n• #44b03a\n``#44b03a` `rgb(68,176,58)``\n• #6b3ab0\n``#6b3ab0` `rgb(107,58,176)``\nSplit Complementary Color\n• #b03a44\n``#b03a44` `rgb(176,58,68)``\n• #44b03a\n``#44b03a` `rgb(68,176,58)``\n• #3a44b0\n``#3a44b0` `rgb(58,68,176)``\n• #b0a63a\n``#b0a63a` `rgb(176,166,58)``\n• #44b03a\n``#44b03a` `rgb(68,176,58)``\n• #3a44b0\n``#3a44b0` `rgb(58,68,176)``\n• #a63ab0\n``#a63ab0` `rgb(166,58,176)``\n• #2e7627\n``#2e7627` `rgb(46,118,39)``\n• #358a2d\n``#358a2d` `rgb(53,138,45)``\n• #3d9d34\n``#3d9d34` `rgb(61,157,52)``\n• #44b03a\n``#44b03a` `rgb(68,176,58)``\n• #4dc143\n``#4dc143` `rgb(77,193,67)``\n• #5fc756\n``#5fc756` `rgb(95,199,86)``\n• #71ce69\n``#71ce69` `rgb(113,206,105)``\nMonochromatic Color\n\n# Alternatives to #44b03a\n\nBelow, you can see some colors close to #44b03a. Having a set of related colors can be useful if you need an inspirational alternative to your original color choice.\n\n• #62b03a\n``#62b03a` `rgb(98,176,58)``\n• #58b03a\n``#58b03a` `rgb(88,176,58)``\n• #4eb03a\n``#4eb03a` `rgb(78,176,58)``\n• #44b03a\n``#44b03a` `rgb(68,176,58)``\n• #3ab03a\n``#3ab03a` `rgb(58,176,58)``\n• #3ab044\n``#3ab044` `rgb(58,176,68)``\n• #3ab04e\n``#3ab04e` `rgb(58,176,78)``\nSimilar Colors\n\n# #44b03a Preview\n\nThis text has a font color of #44b03a.\n\n``<span style=\"color:#44b03a;\">Text here</span>``\n#44b03a background color\n\nThis paragraph has a background color of #44b03a.\n\n``<p style=\"background-color:#44b03a;\">Content here</p>``\n#44b03a border color\n\nThis element has a border color of #44b03a.\n\n``<div style=\"border:1px solid #44b03a;\">Content here</div>``\nCSS codes\n``.text {color:#44b03a;}``\n``.background {background-color:#44b03a;}``\n``.border {border:1px solid #44b03a;}``\n\n# Shades and Tints of #44b03a\n\nA shade is achieved by adding black to any pure hue, while a tint is created by mixing white to any pure color. In this example, #050e05 is the darkest color, while #fefffe is the lightest one.\n\n• #050e05\n``#050e05` `rgb(5,14,5)``\n• #0b1c09\n``#0b1c09` `rgb(11,28,9)``\n• #112b0e\n``#112b0e` `rgb(17,43,14)``\n• #163a13\n``#163a13` `rgb(22,58,19)``\n• #1c4918\n``#1c4918` `rgb(28,73,24)``\n• #22571d\n``#22571d` `rgb(34,87,29)``\n• #276622\n``#276622` `rgb(39,102,34)``\n• #2d7527\n``#2d7527` `rgb(45,117,39)``\n• #33842b\n``#33842b` `rgb(51,132,43)``\n• #399230\n``#399230` `rgb(57,146,48)``\n• #3ea135\n``#3ea135` `rgb(62,161,53)``\n• #44b03a\n``#44b03a` `rgb(68,176,58)``\n• #4abf3f\n``#4abf3f` `rgb(74,191,63)``\n• #57c44d\n``#57c44d` `rgb(87,196,77)``\n• #65c95c\n``#65c95c` `rgb(101,201,92)``\n• #73ce6a\n``#73ce6a` `rgb(115,206,106)``\n• #81d379\n``#81d379` `rgb(129,211,121)``\n• #8fd888\n``#8fd888` `rgb(143,216,136)``\n• #9ddd97\n``#9ddd97` `rgb(157,221,151)``\n• #abe1a5\n``#abe1a5` `rgb(171,225,165)``\n• #b8e6b4\n``#b8e6b4` `rgb(184,230,180)``\n• #c6ebc3\n``#c6ebc3` `rgb(198,235,195)``\n• #d4f0d2\n``#d4f0d2` `rgb(212,240,210)``\n• #e2f5e0\n``#e2f5e0` `rgb(226,245,224)``\n• #f0faef\n``#f0faef` `rgb(240,250,239)``\n• #fefffe\n``#fefffe` `rgb(254,255,254)``\nTint Color Variation\n\n# Tones of #44b03a\n\nA tone is produced by adding gray to any pure hue. In this case, #717a70 is the less saturated color, while #17e604 is the most saturated one.\n\n• #717a70\n``#717a70` `rgb(113,122,112)``\n• #698367\n``#698367` `rgb(105,131,103)``\n• #628c5e\n``#628c5e` `rgb(98,140,94)``\n• #5a9555\n``#5a9555` `rgb(90,149,85)``\n• #539e4c\n``#539e4c` `rgb(83,158,76)``\n• #4ba743\n``#4ba743` `rgb(75,167,67)``\n• #44b03a\n``#44b03a` `rgb(68,176,58)``\n• #3db931\n``#3db931` `rgb(61,185,49)``\n• #35c228\n``#35c228` `rgb(53,194,40)``\n• #2ecb1f\n``#2ecb1f` `rgb(46,203,31)``\n• #26d416\n``#26d416` `rgb(38,212,22)``\n• #1fdd0d\n``#1fdd0d` `rgb(31,221,13)``\n• #17e604\n``#17e604` `rgb(23,230,4)``\nTone Color Variation\n\n# Color Blindness Simulator\n\nBelow, you can see how #44b03a is perceived by people affected by a color vision deficiency. This can be useful if you need to ensure your color combinations are accessible to color-blind users.\n\nMonochromacy\n• Achromatopsia 0.005% of the population\n• Atypical Achromatopsia 0.001% of the population\nDichromacy\n• Protanopia 1% of men\n• Deuteranopia 1% of men\n• Tritanopia 0.001% of the population\nTrichromacy\n• Protanomaly 1% of men, 0.01% of women\n• Deuteranomaly 6% of men, 0.4% of women\n• Tritanomaly 0.01% of the population" ]
[ null ]
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http://phlamethrower.co.uk/riscos/armforbeginners/1/index.htm
[ "ARM code for the truly petrified\n\nThe start of a new series by Matthew Bloch intended to squeeze every drop of speed from your programming.\n\nWhat do BASIC and ARM code programming have in common?  When you turn your machine on, the ARM chip starts on the instruction at memory address zero, and the whole of RISC OS is initialised from there.  After each instruction, the chip moves on four bytes, or 32 bits (the space needed to store a single ARM code instruction) and executes the next instruction, just like lines of BASIC.\n\nThe ARM chip has sixteen registers called R0-R15, and each register can store a 32-bit number.  The sixteenth register is called the program counter, and it stores the address at which the ARM chip is currently executing.  It is referred to for this reason as PC.  BASIC has a limitless number of variables, but in ARM code we have to make careful use of registers, and store those we are not using in the memory for recall later.\n\nSo, here's an instruction: MOV R0,R1.  This instruction moves the contents of register one (R1) into register zero (R0).  The 'destination' register, the one that will be changed, always comes first in ARM code instructions.  What the ARM chip sees is the code &E1A00001 stored in memory; the 'instruction' as we humans see it is only a longhand (mnemonic) so we don‘t have to work out these codes for ourselves.  What an assembler (or compiler) does is to take these lists of longhand instructions and translate (compile) them into unintelligible machine code.\n\nBASIC, conveniently, has an assembler built into it.  Once you‘ve assembled your code, you can then set the PC to start running your compiled code, which means you can make the ARM chip do your bidding!  It‘s as simple as reserving some memory in which to store your instructions, compile them there, and then run them.  Note that not all four-byte codes are legitimate instructions; trying to execute these will give an 'undefined instructon' error.  Other instructions include ADD, SUB(tract), MUL(tiply) and ORR (logical OR, with an extra R to make it three letters).  All ARM instructions can be executed conditionally, that is to say, you can set an instruction to execute depending on the result of a previous one.  You‘ll see examples of this below.\n\nSo, manipulating registers is all very well, but this seems a world away from writing 'real' programs to make graphics and sound.  The answer is in the memory; certain areas of it are 'mapped' onto external devices such as the video controller.  So if we write a byte into the screen memory, it will be displayed by the video controller.  There is also a sound buffer where any bytes stored will be converted to an analogue signal and output through the speakers.  Then on top of these crude methods, RISC OS provides us with a huge library of routines (introduced next month) to perform common tasks such as printing text, drawing garaphics and playing music without having to resort to writing directly to the hardware; in fact using system calls is the norm, since they cause fewer compatibility problems than direct hardware access.\n\nFast cube root\n\nTry this simple task: there's a square root function in BASIC, but there isn't a cube root, so write a function in BASIC to find the cube root of any positive whole number.  It only has to find it to the nearest integer, don't worry about the fraction part.  Chances are, those who aren't mathematicians (and I'm not) will have come up with something similar to figure 1, below.  This function will always give an overestimate if the input value isn't an exact cube.  Now let's see how fast this function is; try finding the cube of every number from 1 to 10,000.  My RISC PC gives a time of 4.62 seconds, though you may be waiting up to ten times this with an ARM2.  Either way it‘s still faster than doing it by hand.  Look at the 'CubeRoot' program on this month's cover disc to see how to do it in 0.2 seconds.\n\n Fig. 1 BASIC cube root function DEF FNcube_root(n%):check%=1:result%=0 WHILE(result%\n\nTo see how this is done, load the program into your favorite editor and take a look at how it's written: the PROCassemble function may look alien, but it demonstrates how to write a small ARM code routine with minimal effort.  The form of the DIM statement may be confusing without brackets: what it does is to reserve 256 bytes of memory and store the start address of the memory in the 'code' variable.  P% is a variable treated specially in BASIC; it tells the ARM code compiler where in memory to start compiling instructions.  When you want to start assembling, the [ character turns BASIC into a compiler; rather than look for lines of BASIC, it will take each subsequent line as ARM code and assemble it at P% until the next ].  Anything inbetween should be code.  The OPT switch should follow each [ character to set the various options for the compiler; OPT 2 is a straight compile, with errors reported and nothing else.  Its uses will become clear later; for now just use it!\n\nThe ARM code is going to mimic the flow of the BASIC function closely, so let‘s use R0 as our n% (number to check), R1 as the number we‘re currently checking (check%) and R2 to work the result of cubing R1 (result%).  Throughout this discussion, look back and see how each line of ARM code compares with the BASCIC function; note that we only actually need space for three integer variables.  We declare the start of the routine with a label, .cube_root.  This marks the start of the routine and stores it in the BASIC variable cube_root, so we can 'CALL cube_root' later.  CALL is a BASIC statement which executes an ARM code routine.  It passes the integer variables A% to G% in registers R0 to R7, so we can pass paremeters easily.  result% = USR(cube_root) will do the same thing, but USR is a function and will pass back R0 into a variable when the routine finishes.  When we call an ARM code routine from BASIC, we need to be able to pass control back to BASIC when the routine is finished.  What the interpreter does is pass the return address in R14, which is sometimes referred to as the link register.  Then when we need to return to BASIC, we just copy the link register into R15 with MOV PC,R14; this is equivalent to GOTO in BASIC.  You can see this instruction is the last one in the routine; if you don‘t include it, the processor will carry on romping through the memory executing instructions, data, and anything else it finds, probably resulting in a crash of some sort.\n\nWe must set R1 (check%) to zero before going into the main cube searching loop.  If you want to load registers with integer variables, you can, subject to certain restrictions: MOV R1,#1 will set R1=1, though not ALL numbers can be loaded; more on this later.  The top of this loop is marked out with .cube_search so we can jump back to this point easily.  For each cycle, we:\n\n•  Increase our counter R1 by 1.\n•  Cube it, leaving the result in R2 (i.e. R2 = R1*R1*R1).\n•  Check if it‘s greater than or equal to the number to be cube-rooted (R0).\n•  If R1 is smaller than R0, we loop around again until it isn‘t.\n•  Otherwise, return with our value of R1 as the nearest cube root.\nThe routine does this process with a few straightforward instructions, listed and explained in figure 2.  So, there‘s a simple ARM code routine in a few lines.\n\n Fig. 2 ARM code cube root run-through .cube_search this sets the BASIC variable cube_search to equal the address in memory of the next instruction ADD R1,R1,#1 means R1 = R1 + 1 (i.e. increase counter) MUL R2,R1,R1 means MULtiply, R2 = R1 * R1 MUL R2,R1,R2 means R2 = R1 * R2 since cubing has to be done with two MUL instructions) CMP R2,R0 stands for 'compare R2 with R0'.  The result of this comparison is stored in the processor`s status flags (explained later).  These status flags indicate (for the purposes of this routine) whether the last two numbers compared were greater than, equal to, or less than each other.  In this case, we only want to carry on the loop if our result register is less than the number we`re checking (i.e. if R2 < R0), otherwise we know we`ve found the nearest cube root. BLT cube_search This is the branch instruction (B) with a condition code attached.  A branch instruction makes the processor jump to another point in memory, usually marked out by an assembler label.  You can attach a condition code to any instruction, so it will only be executed under certain conditions.  Here, we see the LT condition code which stands for 'less than'.  So this will only (B)ranch back to the top of the loop if R2 was (L)ess (T)han R0, as decided in the previous instruction.  Some other condition codes include GT (greater than), GE (greater than or equal), and EQ (equal to). MOV R0,R1 R1 contains the cube root found, but R0 is the only register we can pass back to BASIC.  The result of the USR(...) function in BASIC is the contents of R0 when the routine exits, so we need to move the result into R0 before exiting.\n\nWe can then find a cube root by setting :\n\nA%=number\n\n... and then ...\n\ncube_root%=USR(cube_root)\n\nas the BASIC does.  Next month: a file processor and an introduction to SWIs.\n\n• Matthew Bloch" ]
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https://www.teledynelecroy.com/doc/3-phase-power-app-note
[ "### Introduction\n\nPower analyzers have been manufactured for many years and are used in a wide variety of applications. Often, many settings and preferences can have significant impact on the measurements. Or, there are “legacy” capabilities that may not be well-understood. This technical brief explains the settings in the Teledyne LeCroy Motor Drive Analyzer (MDA) to achieve results consistent with a Yokogawa Power Analyzer, and to explain why the results will be different in some cases.\n\n### Measurement Period (“Sync”) Calculation\n\nFirst, for proper power analysis, one must determine a measurement period within which all calculations take place. Both the Teledyne LeCroy MDA and a Yokogawa Power Analyzer use a “Sync” signal to determine the measurement period. In both cases, the Sync signal can be low-pass filtered to reduce the chances of finding an incorrect measurement period. See the images below:\n\nFor a nearly sinusoidal (e.g. low distortion) signal, both instruments should find the same measurement period with the same LPF cutoff selections, though the Teledyne LeCroy MDA offers a wider variety of selections.\n\nThe Teledyne LeCroy Motor Drive Analyzer also permits adjustment of hysteresis (band), allowing user-defined control of the software’s ignoring of non-monotonicities that interfere with the measurement period calculation. This is explained in detail in the MDA’s software instruction manual. Such control can be very useful for signals that have higher distortion (e.g. brushless DC six-step commutated signals) or signals that have high distortion during high stress or failure events.\n\nNote that the Teledyne LeCroy Motor Drive Analyzer also permits display of the filtered Sync signal with a measurement period overlay, rendering the Sync signal settings easily understandable. See the screen image below (the Sync signal with the overlays appears at bottom).\n\nLastly, the Teledyne LeCroy Motor Drive Analyzer applies the Sync filter and hysteresis settings as a post-acquisition software process, while most power analyzers apply Sync filtering and hysteresis settings to the waveform during the acquisition. Thus, in the Teledyne LeCroy MDA, it is possible to make changes post-acquisition whereas this is not usually possible with a power analyzer instrument. Combined with the Sync period overlay, one may use the MDA’s post-acquisition processing to fine tune the filter and hysteresis settings for optimum results without having to take a new acquisition and lose the acquired data.\n\n### Apparent Power Formula\n\nIn Yokogawa’s Power Analyzer instrument, users may measure apparent power (S) through selection of any of the following formulas in their setup menu:\n\n1. $$Vrms * Irms$$    Same as provided by Teledyne LeCroy, as described in this document\n2. $$Vmean * Imean$$    Product of rectified mean values calibrated to the RMS values\n3. $$Vdc * Idc$$     Product of simple averages of the voltage and current\n4. $$Vmean * Irms$$    Product of the voltage’s rectified mean value and the current’s true RMS value\n5. $$Vrmean * Irmean$$    Product of the voltage’s and current’s rectified mean values\n\nTeledyne LeCroy only provides capability for $$Vrms*Irms$$ calculation of apparent power. To correlate power values from the Yokogawa power analyzer to the Teledyne LeCroy MDA’s results, set the selection for apparent power calculation on the Power Analyzer to $$Vrms*Irms$$.\n\n### Three-Phase (Total) Power Calculations\n\nTeledyne LeCroy employs one method for calculation of power values whereas Yokogawa provides three different methods that return different results. The following is a simplified summary of the Teledyne LeCroy method and the Yokogawa methods for calculating power for a single power cycle – see the respective instruction manuals for complete formulaic descriptions. Note that the table below assumes use of the $$Vrms*Irms$$ formula in the Yokogawa Power Analyzer for Apparent Power calculations.\n\nTeledyne LeCroy Yokogawa Type 1 Yokogawa Type 2 Yokogawa Type 3\nReal Power “P” (in W) $$V*I$$ (instantaneous sample points)\nApparent Power “S” (in VA) $$Vrms*Irms$$ $$Vrms*Irms$$ $$Vrms*Irms$$ $$√(Q^2+ P^2 )$$\nReactive Power “Q” (in VAr) $$√(S^2- P^2 )$$ $$Vrms*Irms*sin⁡φ$$ $$√(S^2- P^2 )$$ $$Vrms*Irms*sin⁡φ$$\nPower Factor (λ) $$P⁄|S|$$ $$P⁄|S|$$ $$P⁄|S|$$ $$P⁄|S|$$\nPhase Angle (φ) $$cos^(-1)⁡λ$$ $$cos^(-1)⁡λ$$ $$cos^(-1)⁡λ$$ $$cos^(-1)⁡λ$$\n\nFor perfectly sinusoidal (zero-distortion) waveforms, it is possible to measure the phase angle φ between the voltage and current sinusoids. However, it is not possible to measure the phase angle φ when the waveforms are distorted (e.g. PWM drive output waveform). Therefore, the Teledyne LeCroy method or Yokogawa’s Type 2 method are the only methods that demonstrably produce accurate results for reactive power (and therefore power factor and phase angle) with distorted waveforms (both also produce accurate results with sinusoidal waveforms).\n\nYokogawa’s Power Analyzers offer the Type 3 method on models with the harmonic measurement-mode option. This option appears to enable definition of a fundamental signal from one of the PWM signals using a PLL source. Then, the instrument determines phase angle by comparing the fundamental voltage and fundamental current waveforms, with power determined for the fundamental and each harmonic through “N” harmonics. This should provide a similar result to values provided by the Teledyne LeCroy Harmonic Filter setting = “Fundamental” or “Fundamental + N” (see below), provided that the hardware PLL response in the Yokogawa power analyzer can accommodate any change in period of the measured signal during the acquisition window.\n\nNote that the Yokogawa power analyzer always calculates real power P correctly in all cases. If this is the only power value of interest, then all methods are suitable. However, to correctly calculate S, Q,λ, or φ, one must choose the correct Yokogawa power analyzer measurement method (if more than one is offered).\n\n### Per-Phase Power Calculations\n\nThe Yokogawa instrument calculates per-phase power using the same equations as total three-phase power, but on one phase at a time.\n\nThe Yokogawa Type 2 method with apparent power setting = $$Vrms*Irms$$ always correlates (assuming there is no problem with the Yokogawa power analyzer obtaining a proper Sync period) with Teledyne LeCroy’s MDA when using three-phase, four-wire (three voltages, three currents) wiring configurations with line-neutral or line-reference voltage probing.\n\nHowever, if using line-line voltage probing, then per-phase power calculations in the Yokogawa power analyzer will be unbalanced and incorrect, even though the three-phase total will be correct. The reasons for the differences are as follows:\n\n1. The Yokogawa three-phase, three-wire (three voltages, three currents) wiring configuration is natively defined as a two-wattmeter setup. This is beneficial in that switching from a three-voltage and three-current measurement to a two-voltage and two-current measurement requires no re-connection of wires to the power analyzer. However, it also means that the line-line voltages and currents are incorrectly associated with each other on a per-phase basis. See Figure 1 (Yokogawa) below and compare to Figure 2 (Teledyne LeCroy).\n2. The Teledyne LeCroy three-phase, three-wire (three voltages, three currents) wiring configuration also uses a two-wattmeter method for total three-phase power calculations, but maintains the correct per-phase vector relationships to obtain proper per-phase calculations. Teledyne LeCroy simply inverts one of the voltage waveforms for the total three-phase power calculation.\n3. The voltage associations made by Yokogawa have no impact on the total three-phase power (real, apparent, or reactive), phase angle, or power factor because the vector (voltage and current) relationships defined in their wiring setup are the correct relationships for the two-wattmeter method used to calculate their total three-phase power.\n4. Both instruments can perform a line-line to line-neutral conversion (referred to as a delta-star conversion by Yokogawa, which is an extra-cost option). However, while Teledyne LeCroy’s MDA will return accurate per-phase power calculations for P, S, Q,λ, and φ with this type of conversion, the Yokogawa power analyzer instrument will only return power calculations for P.\n\nThe practical impact of the Yokogawa wiring configuration is that the voltage and current pairs all have different phase relationships (which is what leads to the incorrect per-phase power calculations). This is shown below on actual three-phase acquisitions:\n\n Yokogawa Teledyne LeCroy 3-phase voltage and current pairs, separated by pair", null, "", null, "3-phase voltage and current pairs, overlaid", null, "", null, "Calculated results appear as follows with and without a line-line to line-neutral (delta-star) conversion.\n\n Yokogawa Without Line-Line to Line-Neutral conversion (Delta-Star)", null, "With Line-Line to Line-Neutral conversion (Delta-Star)", null, "Teledyne LeCroy Without Line-Line to Line-Neutral conversion", null, "With Line-Line to Line-Neutral conversion", null, "" ]
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https://thinking-about-science.com/2019/07/13/19-17-computer-modelling-the-simple-harmonic-oscillator/
[ "# 19.17 Computer modelling – the simple harmonic oscillator\n\nBefore you read this, I suggest you read the first 8 paragraphs of post 18.6.\n\nIn previous posts, we have seen how differential equations (post 19.10) can be used to represent diffusion (post 19.15), the conduction of heat (post 19.15) and the behaviour of waves (post 19.12). We also saw how a differential equation could be used to describe the behaviour of a simple harmonic oscillator – a system that is constantly exchanging potential and kinetic energy with negligible energy loss (post 18.6). However, there is a completely different way of investigating systems like this, without developing differential equations.", null, "In this post, I will illustrate this different approach by using it to investigate a simple harmonic oscillator. In the table above, a mechanical simple harmonic oscillator starts (n = 1) with potential energy U1 = 1.00 J (post 16.21). If we think of this oscillator being restored towards its undisturbed state by a spring, with spring constant k (post 16.49), then\n\nU = (k/2)x2\n\nwhere x is its displacement (post 16.49). So the initial displacement of the oscillator in the table is\n\nx1 = (2U1/k)1/2.\n\nIf k = 200 N.m-1 then\n\nx1 = (2 × 1/200)1/2 = 0.1 m.\n\nAt this initial position (n = 1), its kinetic energy, K1 (post), and, therefore, its speed, are both zero. We use this initial state to define a time t = 0.\n\nI have used Microsoft Excel to create the numbers in the table to 6 decimal places – the results do not reflect the precision with which the results can be calculated; if this comment isn’t clear – see post 16.7.\n\nNow we consider a later state (n = 2) when the oscillator has lost 0.01 J of potential energy, so that now U2 = 0.99 J. Using the same approach as previously, its position is\n\nx2 = (2 × 0.99/200)1/2 = 0.099499 m.\n\nThis “lost” potential energy is converted to 0.01 J of kinetic energy, so now K2 = 0.01 J. For an oscillator of mass m with speed v\n\nK = (m/2)v2\n\n(post 16.21). If our oscillator has a mass of 1 kg, its speed is then\n\nv2 = (2K2/m)1/2 = (2 × 0.01/1)1/2 = 0.141421 m.s-1.\n\nDuring the time that the 0.01 J of potential energy was being transferred into kinetic energy, the displacement of the oscillator was (x2x1) and its average speed was (v1 + v2)/2 so that the time interval for the exchange of energy was\n\nΔt = 2(x2x1)/ (v1 + v2) = 2(0.099499 + 0.1)/(0 + 0.141421) = 0.007089 s.\n\n(see post 16.12). Now, the total time that has elapsed is\n\nt2 = t1 + Δt = 0 + 0.007089 s.\n\nIn the table above, I have continued this process for stages n = 3, 4, 5, 6….. and so on. Below, you can see what happens when n is about 100.", null, "", null, "When n = 101, all the potential energy has been transformed into kinetic energy. Then the displacement, x, is in the opposite direction (it has a minus sign) and kinetic energy starts to be transformed into potential energy. As before, I calculate the effects of this transformation in steps of 0.01 J.", null, "I will continue the calculations until a time of 0.886 s has elapsed; the graph above then shows the displacement, x, plotted against time t. This graph shows that the behaviour of our oscillator repeats every 0.444 s – it has a time period (post 16.14) T = 0.444 s. (it is easier to see the exact result from a table, like the examples above.)\n\nWe could have obtained the same result by setting up the differential equation for an object bouncing on a spring and then solving it to obtain the result\n\nT = 2π(m/k)1/2\n\nas in post 18.11. Then, when m = 1 kg and k = 200 N.m-1,\n\nT = 2π(1/200)1/2 = 0.444 s.\n\nThe advantage of this approach is that it gives a general result that we can use for any value of k and m.\n\nThe method used in this post is simpler, because it uses only a few simple definitions and some simple arithmetic. It shows exactly what happens when m = 1 kg and k = 200 N.m-1 but cannot provide any general results. Sometimes, especially in engineering, a specific result is all that is required then this numerical or computational approach provides everything that is needed. This approach can also be useful when it is too difficult to set up or solve a differential equation.\n\nUsually, I prefer the differential equation approach – not only because it provides a more general result but also because it can help us to understand how we get that result.\n\nRelated posts" ]
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https://zbmath.org/1082.35140
[ "## Existence and uniqueness of the solution to the modified Schrödinger map.(English)Zbl 1082.35140\n\nThe author studies the initial value problem for a system of nonlinear Schrödinger equations in two space dimensions (modified Schrödinger map) which is derived from Schrödinger maps from $$\\mathbb{R}\\times \\mathbb{R}^2$$ to the unit sphere $$S^2$$ or to the hyperbolic space $$\\mathbb{H}^2$$ by using appropriate gauge change. The existence and uniqueness of the solution was known for data in $$H^s(\\mathbb{R}^2)$$ with $$s> 1$$. In this paper the local existence of the solution is proved for the initial data in $$H^s(\\mathbb{R}^2)$$ with $$s> 1/2$$. The uniqueness of the solution is also proved when the data belong to $$H^1(\\mathbb{R}^2)$$.\n\n### MSC:\n\n 35Q55 NLS equations (nonlinear Schrödinger equations) 35G25 Initial value problems for nonlinear higher-order PDEs\nFull Text:" ]
[ null ]
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https://christianlouca.com/algebra-2-quadratic-equations-graphing/
[ "# Algebra 2 Quadratic Equations Graphing\n\nAlgebra 2 Quadratic Equations Graphing has a variety pictures that related to locate out the most recent pictures of Algebra 2 Quadratic Equations Graphing here, and in addition to you can get the pictures through our best algebra 2 quadratic equations graphing collection. Algebra 2 Quadratic Equations Graphing pictures in here are posted and uploaded by Adina Porter for your algebra 2 quadratic equations graphing images collection. The images that existed in Algebra 2 Quadratic Equations Graphing are consisting of best images and high tone pictures.", null, "algebra 2 worksheets quadratic functions and inequalities worksheets from algebra 2 quadratic equations graphing\n\nThese many pictures of Algebra 2 Quadratic Equations Graphing list may become your inspiration and informational purpose. We hope you enjoy and satisfied as soon as our best portray of Algebra 2 Quadratic Equations Graphing from our store that posted here and in addition to you can use it for adequate needs for personal use only. The home Design Ideas team with provides the further pictures of Algebra 2 Quadratic Equations Graphing in high Definition and Best environment that can be downloaded by click on the gallery below the Algebra 2 Quadratic Equations Graphing picture.", null, "algebra 2 lessons best of algebra 2 homework smart quadratic formula from algebra 2 quadratic equations graphing", null, "easy graphing in algebra math and calculus from algebra 2 quadratic equations graphing\n\nYou Might Also Like :\n\nchristianlouca.com can support you to get the latest information practically Algebra 2 Quadratic Equations Graphing. modernize Ideas. We find the money for a top tone tall photo like trusted permit and everything if youre discussing the address layout as its formally called. This web is made to twist your unfinished room into a simply usable room in usefully a brief amount of time. suitably lets agree to a enlarged deem exactly what the algebra 2 quadratic equations graphing. is anything virtually and exactly what it can possibly accomplish for you. subsequently making an trimming to an existing address it is difficult to manufacture a well-resolved loan if the existing type and design have not been taken into consideration.", null, "algebra 2 worksheets quadratic functions and inequalities worksheets from algebra 2 quadratic equations graphing", null, "algebra 2 lessons best of algebra 2 homework smart quadratic formula from algebra 2 quadratic equations graphing\n\nSHARE ON\nTags:" ]
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https://quant.stackexchange.com/questions/4316/which-objective-function-should-i-choose-to-minimize-tracking-error
[ "# Which objective function should I choose to minimize tracking error?\n\nLet say I have $$n$$ assets and their returns over $$m$$ periods which are represented by a matrix $$X \\in \\mathbb{R}^{m \\times n}$$, and I have some other asset with return over the same period which is represented by a vector $$y \\in \\mathbb{R}^m$$.\n\nMy objective is to find a vector of weights $$w$$ such that\n\n$$w^* = \\underset{w}{\\arg \\min} ~ \\text{TE}(w)$$\n\nwhere $$\\text{TE}(w)$$ is the tracking error defined as follows:\n\n$$\\text{TE}(w) = \\sqrt{\\text{Var}(Xw - y)}$$\n\nand\n\n$$\\sum_{i=1}^n w_i =1$$\n\nIn short, I want to replicate $$y$$ using a portfolio of assets $$X$$.\n\nMy idea was to use the exact definition of the tracking error mentioned above through an optimizer.\n\nHowever, somebody suggested to use the following:\n\n$$w^* = \\underset{w}{\\arg \\min} ~ \\sum_{i=1}^m (Xw-y)_i^2$$\n\nI tried both and I get a better tracking error with the first one.\n\nIt seems clear to me that both should return exactly the same if indeed there exists some $$w$$ which perfectly replicates $$y$$.\n\nWhat if it's not the case?\n\nIs there another approach?\n\nWhen performing a tracking error optimization, you will obtain the same result by using the tracking error squared, which is just the variance of the relative portfolio weights. This would be just finding the minimum variance portfolio, but with conditions on the weights. For instance, it would be equivalent to instead set up the variance minimization assuming you have a fixed -100% weight on the benchmark and optimize with the overall sum of weights equal to zero.\n\nFor a short time horizon, if you can assume that the expected return is approximately zero, then your second formula is equivalent to minimizing the variance. When the time horizon is longer and it is no longer approximately true that the expected return on each asset is zero, then the second formula will not produce the same weights.\n\n• Where do the expected returns come from? I think they have no place in this context.\n– SRKX\nOct 10, 2012 at 17:11\n• Because $Var\\left(x\\right)=E\\left(x^{2}\\right)-E\\left(x\\right)^{2}$\n– John\nOct 10, 2012 at 17:25\n• oh right you meant it from a statistical expectation perspective.\n– SRKX\nOct 10, 2012 at 17:58\n\nIt is better to use a factor model, if one is available. Are you asking this question because you don't have access to one?\n\nAlso, what is the nature of the asset you want to track? Is it an index or a single security? What asset class? What risk factors is it exposed to (e.g. interest rate and credit risk vs. stock market volatility and other equity factors)? The answer to your question depends on what you are tracking." ]
[ null ]
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https://www.neuron.yale.edu/phpBB/viewtopic.php?f=8&t=4264&view=print
[ "Page 1 of 1\n\n### Action Potential propagation\n\nPosted: Sun Mar 15, 2020 2:06 pm\nHi,\nI have 3 questions:\n1: Would you please tell me, the model that NEURON uses is always based on cable theory ? Can we have point model of neuron ,too?\n\n2: I wrote this code:\ncreate soma, axon\naccess soma\n\nsoma.nseg = 1\nsoma.diam = 18.8\nsoma.L = 18.8\nsoma.Ra =123.0\nsoma insert hh\nsoma psection()\naxon.nseg = 1\naxon.diam = 18.8\naxon.L = 500\naxon.Ra =123.0\naxon insert hh\naxon psection()\nconnect axon(0),soma(0)\n\nobjectvar stim\nsoma stim = new IClamp(0.5)\nstim.del = 100\nstim.dur = 100\nstim.amp = 1\n\ntstop = 300\n\nand I want to see action potential propagation along the axon, so I plot axon.v(0.1) and axon.v(0.9) and I expected to see a time delay between spikes that I didn't see.\nCould you please tell me how can I fix this problem?\n\n3. And my last question is how can I compute intracellular voltage Vi = Vm + Ve ?!\n\nThanks\n\n### Re: Action Potential propagation\n\nPosted: Sun Mar 15, 2020 6:36 pm\n1. Point models are fine. If you want biophysical kinetics, just use a section with nseg=1. If you want something more like an integrate-and-fire type cell, use one of the built-in types (e.g. IntFire, IntFire2, IntFire4), find one on ModelDB, or create your own with a MOD file of type ARTIFICIAL_CELL.\n\n2. You set axon.nseg = 1; that means there's only one compartment for the axon, so whether you sample the 0.1 or 0.9 location doesn't matter; you'll still be in the same compartment.\n\nThat said, with your model even if you set \"axon nseg=101\" while you will see a difference between those two locations, it will be very slight. Why? A diameter of 18.8 is quite large and imposes little barrier to current flow. Try reducing the axon diameter to 2 microns and shortening your stimulus to just 1 ms. If you do that with an appropriate nseg, you'll see axon(0.9) follows axon(0.1) by about 1 ms.\n\nAs an aside, if you're new to NEURON, I strongly recommend learning Python instead of HOC. You'll find much more documentation on Python than in HOC (both in general and less-so-but-still-true with respect to NEURON), Python is a more broadly applicable skill, and Python offers vastly superior graphics and library support.\n\nHere's a Python version of your code, with the changes as described above:\n\nCode: Select all\n\n``````import matplotlib.pyplot as plt\nfrom neuron import h\nfrom neuron.units import ms, mV\n\nsoma = h.Section(name='soma')\naxon = h.Section(name='axon')\naxon.connect(soma(0))\n\nsoma.nseg = 1\nsoma.diam = soma.L = 18.8\n\naxon.nseg = 101\naxon.diam = 2\naxon.L = 500\n\nstim = h.IClamp(soma(0.5))\nstim.delay = 100 * ms\nstim.dur = 1 * ms\nstim.amp = 0.9\n\nfor sec in [soma, axon]:\nsec.Ra = 123\nsec.insert('hh')\n\nt = h.Vector().record(h._ref_t)\nv1 = h.Vector().record(axon(0.1)._ref_v)\nv2 = h.Vector().record(axon(0.9)._ref_v)\n\nh.finitialize(-65 * mV)\nh.continuerun(300 * ms)\n\nplt.plot(t, v1, label='axon(0.1).v')\nplt.plot(t, v2, label='axon(0.9).v')\nplt.xlim((99, 110))\nplt.xlabel('t (ms)')\nplt.legend()\nplt.show()\n``````", null, "### Re: Action Potential propagation\n\nPosted: Mon Mar 16, 2020 10:30 am\nDear Ramcdougal,\n\nIf I insert extracellular to my model, I have extracellular potential, haven't I?\nIf so, how can I code for intracellular voltage?\n\nThanks\n\n### Re: Action Potential propagation\n\nPosted: Mon Mar 16, 2020 11:36 am\nSee the documentation of extracellular in the Programmer's Reference.\nThe vext values are all referred to ground, which is assumed to have a potential of 0 mV.\n\nThe hoc name for the potential at a point just outside the cell membrane of the currently accessed section is\nvext(x)\nwhere x is the normalized distance of the point from the section's 0 end.\nBut what do you call it in Python? If the Python name of the section is foo, and extracellular has been \"inserted\" into foo, then the potential adjacent to the external surface of foo at location x is\nfoo(x).vext\n\nSo the intracellular potential at x, relative to ground, is the sum\nfoo(x).v + foo(x).vext\n\nYou could force recalculation of this value throughout a simulation, but that is slower than capturing the time courses of foo(x).v and foo(x).vext to a pair of Vectors during a simulation and then summing the vectors after the end of the simulation. For example, assuming that foov and foovext are the Python names for the Vectors that capture the time course of foo(x).v and foo(x).vext,\n\nCode: Select all\n\n``````h.run() # executes a simulation\nvintracell = foov + foovext # vintracell now contains the time course\n# of intracellular potential at foo(x)``````\nRead the Programmer's Reference entry about the Vector class's record() method. By the way, it's also a good idea to capture the time values h.t to another Vector." ]
[ null, "https://www.dropbox.com/s/h1nz67wikp5wd9p/propagating_wave.png", null ]
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https://deap.readthedocs.io/en/master/examples/gp_parity.html
[ "# Even-Parity Problem¶\n\nParity is one of the classical GP problems. The goal is to find a program that produces the value of the Boolean even parity given n independent Boolean inputs. Usually, 6 Boolean inputs are used (Parity-6), and the goal is to match the good parity bit value for each of the $$2^6 = 64$$ possible entries. The problem can be made harder by increasing the number of inputs (in the DEAP implementation, this number can easily be tuned, as it is fixed by a constant named PARITY_FANIN_M).\n\n## Primitives set used¶\n\nParity uses standard Boolean operators as primitives, available in the Python operator module :\n\npset = gp.PrimitiveSet(\"MAIN\", PARITY_FANIN_M, \"IN\")\n\n\nIn addition to the n inputs, we add two constant terminals, one at 0, one at 1.\n\nNote\n\nAs Python is a dynamic typed language, you can mix Boolean operators and integers without any issue.\n\n## Evaluation function¶\n\nIn this implementation, the fitness of a Parity individual is simply the number of successful cases. Thus, the fitness is maximized, and the maximum value is 64 in the case of a 6 inputs problems.\n\ndef evalParity(individual):\nfunc = toolbox.compile(expr=individual)\nreturn sum(func(*in_) == out for in_, out in zip(inputs, outputs)),\n\n\ninputs and outputs are two pre-generated lists, to speedup the evaluation, mapping a given input vector to the good output bit. The Python sum() function works on booleans (false is interpreted as 0 and true as 1), so the evaluation function boils down to sum the number of successful tests : the higher this sum, the better the individual.\n\n## Conclusion¶\n\nThe other parts of the program are mostly the same as the Symbolic Regression algorithm.\n\nThe complete examples/gp/parity.\n\n## Reference¶\n\nJohn R. Koza, “Genetic Programming II: Automatic Discovery of Reusable Programs”, MIT Press, 1994, pages 157-199." ]
[ null ]
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https://azabutokyodc.jp/sys/simon.php?infer=MmQ4NjY4YjM0ZGM1MjU3YTM5NTkxZDkyYWIyOWFiOGE-KYN&pubid=1515
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[ null ]
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https://www.gradesaver.com/textbooks/math/calculus/calculus-8th-edition/chapter-4-integrals-4-3-the-fundamental-theorem-of-calculus-4-3-exercises-page-327/22
[ "## Calculus 8th Edition\n\nEvaluate the integral: $\\int^1_0 (1 -8v^3 +16v^7) dv$ Recall the 2nd part of the Fundamental Theorem of Calculus: $\\int_a^bf(x)dx = F(b) - F(a)$ Find $F(v)$: $F(v) = \\int^1_0 (1 -8v^3 +16v^7) dv$ $F(v) =v - \\frac{8}{4}v^4 +\\frac{16}{8}v^8$ $F(v) =v - 2v^4 +2v^8$ Now evaluate $F(b) - F(a)$: $F(1) - F(0)$ $(1 - 2(1)^4 +2(1)^8 )- (0 - 2(0)^4 +2(0)^8)$ $(1-2+2) - 0=1$" ]
[ null ]
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https://www.colorhexa.com/002626
[ "# #002626 Color Information\n\nIn a RGB color space, hex #002626 is composed of 0% red, 14.9% green and 14.9% blue. Whereas in a CMYK color space, it is composed of 100% cyan, 0% magenta, 0% yellow and 85.1% black. It has a hue angle of 180 degrees, a saturation of 100% and a lightness of 7.5%. #002626 color hex could be obtained by blending #004c4c with #000000. Closest websafe color is: #003333.\n\n• R 0\n• G 15\n• B 15\nRGB color chart\n• C 100\n• M 0\n• Y 0\n• K 85\nCMYK color chart\n\n#002626 color description : Very dark (mostly black) cyan.\n\n# #002626 Color Conversion\n\nThe hexadecimal color #002626 has RGB values of R:0, G:38, B:38 and CMYK values of C:1, M:0, Y:0, K:0.85. Its decimal value is 9766.\n\nHex triplet RGB Decimal 002626 `#002626` 0, 38, 38 `rgb(0,38,38)` 0, 14.9, 14.9 `rgb(0%,14.9%,14.9%)` 100, 0, 0, 85 180°, 100, 7.5 `hsl(180,100%,7.5%)` 180°, 100, 14.9 003333 `#003333`\nCIE-LAB 12.773, -12.916, -3.798 1.043, 1.526, 2.073 0.225, 0.329, 1.526 12.773, 13.463, 196.386 12.773, -9.88, -2.133 12.353, -6.55, -1.303 00000000, 00100110, 00100110\n\n# Color Schemes with #002626\n\n• #002626\n``#002626` `rgb(0,38,38)``\n• #260000\n``#260000` `rgb(38,0,0)``\nComplementary Color\n• #002613\n``#002613` `rgb(0,38,19)``\n• #002626\n``#002626` `rgb(0,38,38)``\n• #001326\n``#001326` `rgb(0,19,38)``\nAnalogous Color\n• #261300\n``#261300` `rgb(38,19,0)``\n• #002626\n``#002626` `rgb(0,38,38)``\n• #260013\n``#260013` `rgb(38,0,19)``\nSplit Complementary Color\n• #262600\n``#262600` `rgb(38,38,0)``\n• #002626\n``#002626` `rgb(0,38,38)``\n• #260026\n``#260026` `rgb(38,0,38)``\n• #002600\n``#002600` `rgb(0,38,0)``\n• #002626\n``#002626` `rgb(0,38,38)``\n• #260026\n``#260026` `rgb(38,0,38)``\n• #260000\n``#260000` `rgb(38,0,0)``\n• #000000\n``#000000` `rgb(0,0,0)``\n• #000000\n``#000000` `rgb(0,0,0)``\n• #000d0d\n``#000d0d` `rgb(0,13,13)``\n• #002626\n``#002626` `rgb(0,38,38)``\n• #004040\n``#004040` `rgb(0,64,64)``\n• #005959\n``#005959` `rgb(0,89,89)``\n• #007373\n``#007373` `rgb(0,115,115)``\nMonochromatic Color\n\n# Alternatives to #002626\n\nBelow, you can see some colors close to #002626. Having a set of related colors can be useful if you need an inspirational alternative to your original color choice.\n\n• #00261d\n``#00261d` `rgb(0,38,29)``\n• #002620\n``#002620` `rgb(0,38,32)``\n• #002623\n``#002623` `rgb(0,38,35)``\n• #002626\n``#002626` `rgb(0,38,38)``\n• #002326\n``#002326` `rgb(0,35,38)``\n• #002026\n``#002026` `rgb(0,32,38)``\n• #001d26\n``#001d26` `rgb(0,29,38)``\nSimilar Colors\n\n# #002626 Preview\n\nThis text has a font color of #002626.\n\n``<span style=\"color:#002626;\">Text here</span>``\n#002626 background color\n\nThis paragraph has a background color of #002626.\n\n``<p style=\"background-color:#002626;\">Content here</p>``\n#002626 border color\n\nThis element has a border color of #002626.\n\n``<div style=\"border:1px solid #002626;\">Content here</div>``\nCSS codes\n``.text {color:#002626;}``\n``.background {background-color:#002626;}``\n``.border {border:1px solid #002626;}``\n\n# Shades and Tints of #002626\n\nA shade is achieved by adding black to any pure hue, while a tint is created by mixing white to any pure color. In this example, #001212 is the darkest color, while #feffff is the lightest one.\n\n• #001212\n``#001212` `rgb(0,18,18)``\n• #002626\n``#002626` `rgb(0,38,38)``\n• #003a3a\n``#003a3a` `rgb(0,58,58)``\n• #004d4d\n``#004d4d` `rgb(0,77,77)``\n• #006161\n``#006161` `rgb(0,97,97)``\n• #007474\n``#007474` `rgb(0,116,116)``\n• #008888\n``#008888` `rgb(0,136,136)``\n• #009c9c\n``#009c9c` `rgb(0,156,156)``\n• #00afaf\n``#00afaf` `rgb(0,175,175)``\n• #00c3c3\n``#00c3c3` `rgb(0,195,195)``\n• #00d7d7\n``#00d7d7` `rgb(0,215,215)``\n• #00eaea\n``#00eaea` `rgb(0,234,234)``\n• #00fefe\n``#00fefe` `rgb(0,254,254)``\n• #12ffff\n``#12ffff` `rgb(18,255,255)``\n• #26ffff\n``#26ffff` `rgb(38,255,255)``\n• #3affff\n``#3affff` `rgb(58,255,255)``\n• #4dffff\n``#4dffff` `rgb(77,255,255)``\n• #61ffff\n``#61ffff` `rgb(97,255,255)``\n• #74ffff\n``#74ffff` `rgb(116,255,255)``\n• #88ffff\n``#88ffff` `rgb(136,255,255)``\n• #9cffff\n``#9cffff` `rgb(156,255,255)``\n• #afffff\n``#afffff` `rgb(175,255,255)``\n• #c3ffff\n``#c3ffff` `rgb(195,255,255)``\n• #d7ffff\n``#d7ffff` `rgb(215,255,255)``\n• #eaffff\n``#eaffff` `rgb(234,255,255)``\n• #feffff\n``#feffff` `rgb(254,255,255)``\nTint Color Variation\n\n# Tones of #002626\n\nA tone is produced by adding gray to any pure hue. In this case, #121414 is the less saturated color, while #002626 is the most saturated one.\n\n• #121414\n``#121414` `rgb(18,20,20)``\n• #101616\n``#101616` `rgb(16,22,22)``\n• #0f1717\n``#0f1717` `rgb(15,23,23)``\n• #0d1919\n``#0d1919` `rgb(13,25,25)``\n• #0c1a1a\n``#0c1a1a` `rgb(12,26,26)``\n• #0a1c1c\n``#0a1c1c` `rgb(10,28,28)``\n• #091d1d\n``#091d1d` `rgb(9,29,29)``\n• #071f1f\n``#071f1f` `rgb(7,31,31)``\n• #062020\n``#062020` `rgb(6,32,32)``\n• #042222\n``#042222` `rgb(4,34,34)``\n• #032323\n``#032323` `rgb(3,35,35)``\n• #012525\n``#012525` `rgb(1,37,37)``\n• #002626\n``#002626` `rgb(0,38,38)``\nTone Color Variation\n\n# Color Blindness Simulator\n\nBelow, you can see how #002626 is perceived by people affected by a color vision deficiency. This can be useful if you need to ensure your color combinations are accessible to color-blind users.\n\nMonochromacy\n• Achromatopsia 0.005% of the population\n• Atypical Achromatopsia 0.001% of the population\nDichromacy\n• Protanopia 1% of men\n• Deuteranopia 1% of men\n• Tritanopia 0.001% of the population\nTrichromacy\n• Protanomaly 1% of men, 0.01% of women\n• Deuteranomaly 6% of men, 0.4% of women\n• Tritanomaly 0.01% of the population" ]
[ null ]
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https://www.rocksolidinc.com/products/life-of-fred-pre-algebra-0-with-physics-middle-school-math
[ "Life of Fred - Pre-Algebra 0 with Physics (Middle School Math)\n\n# Life of Fred - Pre-Algebra 0 with Physics (Middle School Math)\n\n\\$29.00\nThe third book in the Life of Fred Middle School Series\n\nLife of Fred is a series of math books that break the old pattern of drill and kill. Instead of nothing but dry exposition and endless drill exercises, they contain fun stories about Fred Gauss, a child prodigy math genius. During his hilarious adventures, he encounters situations that call for solving math problems. Dr. Stanley Schmidt wrote these to make math come alive with humor, clear explanations, and silly illustrations that will make math a fun subject. Your children actually want to read these books. The stories carry on through the exercises, leading the student through them.  Many of the books have a series of quizzes called Bridges every few chapters. Passing a quiz means the student is ready for the next chapter. Some books have all the problem solutions in them, while others have separate answer keys or companions. The textbooks are all hardbound, the answer keys are comb-bound.\n\nThis program relies on reading comprehension and thinking and is non-consumable. You will not find 30 problems on every page of rote spoon-fed learning that is quickly forgotten.  This is totally different, a new way of learning math, and everything you need is in the book. As a parent, you will quickly pick up on the novel way as you read along and learn with your student.  Books available for grades K - 12.\n\nFred does physics before algebra.\n\nLearn . . .\n\n• How ducks and cows pronounce μ differently\n• Why no one can weigh 55 kilograms\n• How Kingie could move a safe that Superman couldn't\n• . . . and even some elementary physics\n\nAll fun!\n\nJust open & enjoy.\n\nConcepts -\n• Numerals\n• Making models\n• Nineteen conversion factor problems\n• Area of a rectangle\n• Friction independent of speed\n• Constants of Proportionality\n• Exact speed of light\n• Continuous and discrete variables\n• Story of the meter\n• Oblate spheroids\n• Krypton vs. kryptonite\n• Square roots\n• Solving d = rt for r\n• Ordered pairs\n• Why rocks stop falling\n• Hunch-conjecture-theory-law\n• Simultaneity doesn’t exist\n• Inductive and deductive reasoning\n• How fossils and astronomy are connected\n• Hooke’s law\n• Four ways to stretch a spring\n• Three meanings of plastic\n• Static vs. kinetic friction\n• Nine forms of energy\n• Energy Cards game\n• Experimentally finding the coefficient of static friction without knowing the weight of the object\n• Similar triangles\n• Kelvin temperature\n• Law of conservation of energy\n• Perpetual motion machines\n• Kilowatt-hours\n• Metric system\n• Two ways to measure mass\n• Definition of pi\n• Newton’s first and second laws\n• Why cramming doesn’t work well, Definition of pressure\n• Exponents\n• Density of neutron stars\n• Computing the mass of an iron atom\n• Pressure at a given depth\n• Finding the volume of a desk lamp\n• 80-pound rubber ducky\n• Air has mass\n• Why 35-foot straws don’t work\n• Birds sitting on high-voltage power lines\n• How to buy a cafe\n• Electrons per second in an ampere\n• Computing resistance in parallel circuits\n• Orbital quantum number\n• Orbital magnetic quantum number\n• Spin magnetic quantum number\n• and more!\n\nWhew!\n\nHardback, ISBN 9781937032227, 288 pages\n\n Book Title Life of Fred - Pre-Algebra 0 with Physics (Middle School Math) Publisher: Z Twist Books - Life of Fred Author Stan Schmidt\nThe third book in the Life of Fred Middle School Series\n\nLife of Fred is a series of math books that break the old pattern of drill and kill. Instead of nothing but dry exposition and endless drill exercises, they contain fun stories about Fred Gauss, a child prodigy math genius. During his hilarious adventures, he encounters situations that call for solving math problems. Dr. Stanley Schmidt wrote these to make math come alive with humor, clear explanations, and silly illustrations that will make math a fun subject. Your children actually want to read these books. The stories carry on through the exercises, leading the student through them.  Many of the books have a series of quizzes called Bridges every few chapters. Passing a quiz means the student is ready for the next chapter. Some books have all the problem solutions in them, while others have separate answer keys or companions. The textbooks are all hardbound, the answer keys are comb-bound.\n\nThis program relies on reading comprehension and thinking and is non-consumable. You will not find 30 problems on every page of rote spoon-fed learning that is quickly forgotten.  This is totally different, a new way of learning math, and everything you need is in the book. As a parent, you will quickly pick up on the novel way as you read along and learn with your student.  Books available for grades K - 12.\n\nFred does physics before algebra.\n\nLearn . . .\n\n• How ducks and cows pronounce μ differently\n• Why no one can weigh 55 kilograms\n• How Kingie could move a safe that Superman couldn't\n• . . . and even some elementary physics\n\nAll fun!\n\nJust open & enjoy.\n\nConcepts -\n• Numerals\n• Making models\n• Nineteen conversion factor problems\n• Area of a rectangle\n• Friction independent of speed\n• Constants of Proportionality\n• Exact speed of light\n• Continuous and discrete variables\n• Story of the meter\n• Oblate spheroids\n• Krypton vs. kryptonite\n• Square roots\n• Solving d = rt for r\n• Ordered pairs\n• Why rocks stop falling\n• Hunch-conjecture-theory-law\n• Simultaneity doesn’t exist\n• Inductive and deductive reasoning\n• How fossils and astronomy are connected\n• Hooke’s law\n• Four ways to stretch a spring\n• Three meanings of plastic\n• Static vs. kinetic friction\n• Nine forms of energy\n• Energy Cards game\n• Experimentally finding the coefficient of static friction without knowing the weight of the object\n• Similar triangles\n• Kelvin temperature\n• Law of conservation of energy\n• Perpetual motion machines\n• Kilowatt-hours\n• Metric system\n• Two ways to measure mass\n• Definition of pi\n• Newton’s first and second laws\n• Why cramming doesn’t work well, Definition of pressure\n• Exponents\n• Density of neutron stars\n• Computing the mass of an iron atom\n• Pressure at a given depth\n• Finding the volume of a desk lamp\n• 80-pound rubber ducky\n• Air has mass\n• Why 35-foot straws don’t work\n• Birds sitting on high-voltage power lines\n• How to buy a cafe\n• Electrons per second in an ampere\n• Computing resistance in parallel circuits\n• Orbital quantum number\n• Orbital magnetic quantum number\n• Spin magnetic quantum number\n• and more!\n\nWhew!\n\nHardback, ISBN 9781937032227, 288 pages" ]
[ null ]
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https://bonndoc.ulb.uni-bonn.de/xmlui/handle/20.500.11811/4682
[ "Sosna, Pawel: Derived categories and scalar extensions. - Bonn, 2010. - Dissertation, Rheinische Friedrich-Wilhelms-Universität Bonn.\nOnline-Ausgabe in bonndoc: https://nbn-resolving.org/urn:nbn:de:hbz:5N-23498\n@phdthesis{handle:20.500.11811/4682,\nurn: https://nbn-resolving.org/urn:nbn:de:hbz:5N-23498,\nauthor = {{Pawel Sosna}},\ntitle = {Derived categories and scalar extensions},\nschool = {Rheinische Friedrich-Wilhelms-Universität Bonn},\nyear = 2010,\nmonth = nov,\n\nnote = {This thesis consists of three parts all of which deal with questions related to scalar extensions and derived categories.\nIn the first part we consider the question whether the conjugation of a complex projective K3 surface X by an automorphism of the complex numbers can produce a non-isomorphic Fourier-Mukai partner of X. The answer is affirmative. The conjugate surface is thus in particular a moduli space of locally free sheaves on X. We use our result to give higher-dimensional examples of derived equivalent conjugate varieties. We furthermore prove that a similar result holds for abelian surfaces.\nThe topic of the second part is the behaviour of stability conditions under scalar extensions. Namely, given a smooth projective variety X over some field K and its bounded derived category, one can associate to it a complex manifold of stability conditions. Given a finite Galois extension we compare the stability manifolds of X and of the base change scheme in general and under the additional assumption that the numerical Grothendieck group does not change under the scalar extension.\nIn the third and last part we consider the following question: Can one naturally define an L-linear triangulated category if a K-linear triangulated category and a field extension are given? We propose a construction and prove that our definition gives the expected result in the geometric case. It also gives the anticipated result when applied to the derived category of an abelian category with enough injectives and with generators. We furthermore prove that in the just mentioned cases the dimension of the triangulated category in question does not change for finite Galois extensions.},\n\nurl = {http://hdl.handle.net/20.500.11811/4682}\n}" ]
[ null ]
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http://unistudyguides.com/wiki/Topic_6_-_Normal_Distribution_and_Estimation
[ "# Topic 6 - Normal Distribution and Estimation\n\n## Contents\n\nGerald Keller (2011), Statistics for Management and Economics (Abbreviated), 9th Edition, pp. 270-287 & 335-353.\n\n### Normal Distribution Functions\n\n The Normal Distribution is symmetrical, uni-modal and is bell curve shaped. In this distribution, the mean = median = mode. The 2 factors that influence the shape of the bell curve are the mean (the middle number) and the variance (how steep/flat) Consequentially, we are able to define a normal distribution for the random variable 'X' in the following way:\n\nX ~ (μ,σ^2) where -∞≤x≤∞ This means 'X', the random variable is normally distributed with mean 'μ' and variance 'σ^2'\n\nStatisticians use Z scores to standardise data values so that we can more easily find probability values through a Z standard normal distribution (this link contains examples).\n\nZ Score = (x-μ)/σ (Linear Function)\n\nThe normal distribution for Z scores (standard normal distribution) is defined in the following way Z~N(0,1). Once we have standardised scores for the standard normal distribution we can use the standard normal table to find probability values for a random variable being a range of values e.g. if the random variable, 'X', is equal to the weight of a person in kilograms, we could use this method to find the probability of a persons weight being between 50kg. and 65kg.\n\n#### Normal Distribution Example\n\nX ~ (50,100)\n\n• Find: P(45 ≤ x ≤ 60)\n• Standardise Scores!!!\n• (45-50)/10 ≤ Z ≤ (60-50)/10\n• = -1/2 ≤ Z ≤ 1\n• = 0 ≤ Z ≤ 1/2 + 0 ≤ Z ≤ 1 (By Symmetry - Because P(-1/2 ≤ Z ≤ 0) = P(0 ≤ Z ≤ 1/2)). We do this because it is much easier to find the probability values in the standard normal table in this format\n\nX ~ (50,100)\n\n• Find Z_(0.025) and unstandardise it to find the corresponding 'X' value =\n• = 1.96\n• Unstandardise!!!!\n• (1.96 = X – 50 / 10)\n• (X = 50 + 19.6) = 69.6\n\n### Finding the Value of Z Given the Probabilities\n\nFor these questions, we must look at the probabilities within the standard normal table to find the critical z value.\n\n• ZA = 100(1-A)^th Percentile\n• Find The 97 ½ Percentile\n• P (Z > ZA) = A\n• Z_(0.025) (top 2.5%)\n• P (Z > Z_0.025) = 0.025\n• 1 - 0.025 = 0.9750\n• = 1.96\n\n#### Other Questions\n\nFind the value of a standard normal RV where the probability that the RV is GREATER than it is 5%\n\n• 95th Percentile\n• = 1.645\n\nFind the Value of a standard normal RV where the probability that the RV is LESS than it is 5%\n\n• 5th Percentile\n• = -1.645 (Symmetric)\n\n## Introduction To Estimation\n\n### Concepts of Estimation\n\nEstimations objective is determine the approximate value of the parameter (e.g. sample mean for population mean. There are 2 types of estimators defined below:\n\n• Point Estimator\n• Draws inferences about a population by estimating the value of an unknown parameter using a single value (this will be wrong since a probability of a point on a continuous random variables probability density function is virtually 0)\n• Interval Estimator\n• Draws inferences about a population by estimating the value of an unknown parameter using an interval\n\n### Characteristics of Good Estimators\n\n• Unbiased - E(Estimator) = Parameter (e.g. E(sample mean) = population mean)\n• Consistency - Difference between the estimator & parameters becomes smaller as sample size increases\n• Relative Efficiency - If 2 unbiased estimators of a parameter, the one who’s variance is lower has relative efficiency\n\n## End\n\nThis is the end of this topic. Click here to go back to the main subject page for Business and Economic Statistics." ]
[ null ]
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https://www.online-sciences.com/physics/ac-circuit-contains-ohmic-resistance-capacitor-and-inductive-coil-connected-in-series-rlc-circuit/
[ "# AC circuit contains ohmic resistance, capacitor and inductive coil connected in series (RLC-circuit)\n\n### Impedance\n\nIn an electric circuit containing an AC power supply together with inductive coils, capacitors & resistors, the AC current would be opposed by reactance (inductive reactance or capacitive reactance) in addition to the resistance of resistors and wires, The resistance and reactance together are called impedance and given the symbol (Z) and measured in Ohm (Ω).\n\nThe impedance (Z) is the equivalent to the resistance, capacitive reactance and inductive reactance together in an AC circuit, When the impedance of RLC circuit = 300 Ω, It means that the total opposition to the electric current in this circuit due to the resistance and the reactance of both the coil and capacitor = 300 Ω.\n\n##### AC circuit contains ohmic resistance and inductive coil connected in series (RL – circuit)\n\nIt is almost impossible practically to construct an inductive coil with zero resistance because any coil must have resistance due to the wires used in its fabrication.\n\nWhen electric circuit contains inductive coil, ohmic resistance and AC source connected in series, we noticed that the current passing through each of the resistance and the induction coil is the same in value and phase since they are connected in series.\n\nBut voltage in the coil (VL) leads current (I) by ¼ cycle (phase angle 90°) in the induction coil, the voltage in the resistance (VR) is in phase with current (I) in ohmic resistance.\n\nThe potential difference across a coil (VL) leads the potential difference across the resistance (VR) by a phase angle 90°, thus the total potential difference is out of phase with the current intensity (I).\n\nTotal voltage can be found using the vectors from the relation:\n\nV² = V²R + V²L\n\nV = I Z , VR = I R, VL = I XL\n\n( I Z )² = I² R² + I² X² = I² ( R² + X²L )\n\nZ ² = ( R² + X²L )\n\nThe phase angle can be determined between the total voltage (V) and the resistor voltage (VR) from the relation:\n\ntan θ = VL / VR, tan θ = IXL / I R , So,  tan θ = XL / R\n\n##### AC circuit contains ohmic resistance and capacitor connected in series (RC-circuit)\n\nWhen electric circuit contains capacitor, ohmic resistance and AC source connected in series, We notice that the current passing through each of the resistance and the capacitor is the same in value and phase since they are connected in series.\n\nBut voltage in the capacitor (VC) lags current (I) by ¼ cycle (phase angle 90°) in the capacitor, Voltage in the resistance (VR) is in phase with current (I) in ohmic resistance.\n\nThe potential difference across the capacitor (VC) lags the potential difference across the resistance (VR) by phase angle 90°, thus the total potential difference (V) is out of phase with current intensity (I).\n\nTotal voltage can be found using the vectors from the relation:\n\nV² = V²R + V²C\n\nV = I Z  ,  VR = I R   , VC = I XC\n\nI² Z² = I² R² + I² X²C\n\nI² Z² = I² (R² + X²C)\n\nZ² = (R² + X²C)\n\nThe phase angle (θ) can be determined between the total voltage difference (V) and the resistor voltage (VR) from the relation:\n\ntan θ = − VC / VR, tan θ = − IXC / I R, So,  tan θ = − XC / R\n\nThe negative sign means that the potential difference (VC) lags the potential difference (VR) by an angle of 90°.\n\n##### AC circuit contains ohmic resistance, induction coil and capacitor connected in series (RLC – circuit)\n\nWhen electric circuit contains capacitor, ohmic resistance, induction coil and AC source connected in series, We noticed that the current passing through each of the resistance, the induction coil & the capacitor is the same in value and phase since they are connected in series, But:\n\n• In the induction coil, voltage (VL) leads current (I) by phase angle 90°.\n• In the ohmic resistance, voltage (VR) is in phase with current (I).\n• In the capacitor, voltage (Vc) lags current (I) by phase angle 90°.\n\nThe coil voltage (VL) leads the resistance voltage (VR) by angle 90° and the capacitor voltage (Vc) lags the resistance voltage (VR) by angle 90° and thus the phase difference between (VL) and (Vc) is 180°.\n\nTotal voltage ( V ) can be found using the vectors from the relation :\n\nV² = V²R + ( VL− Vc\n\nWhere : V = I Z ,  VR = I R,   VL = I XL   , VC = I XC\n\nI² Z² = ( I R )² + ( I XL − I XC)² = I² [ ( R )² + (XL − XC)² ]\n\nZ² = ( R )² + (XL − XC\n\nFrom the previous figure, the phase angle can be determined from the relation:\n\ntan θ = ( VL − VC ) / VR\n\ntan θ = ( XL − XC ) / R\n\nThe phase angle θ is affected by changing the values of capacitive and inductive reactance then when:\n\n• VL > VC, XL > XC, The phase angle (θ) is positive, the total voltage (V) leads the current (I) by an angle (θ), That means inductive circuit behavior.\n• VL = VC, XL = XC, The phase angle (θ) equals zero, the total voltage (V) is in phase with the current (I), That means ohmic resistance behavior.\n• VL < VC, XL < XC, The phase angle ( θ ) is negative, the total voltage (V) lags the current (I) by an angle (θ), That means capacitive circuit behavior.\n\nThe real consumed power (Pw) in AC circuit, either RL, RC or RLC is only the power that consumed in the ohmic resistance in the form of heat energy.\n\nPw = I² R = V²R / R\n\nCapacitive reactance of capacitors network, AC current & AC voltage in a capacitor circuit\n\nThe oscillating circuit, Tuning or resonant circuit in the wireless radio receivers" ]
[ null ]
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https://puzzling.stackexchange.com/questions/40415/matchsticks-for-lengths
[ "# Matchsticks for lengths\n\nYou have been invited to an $n$-dimensional universe, where $n$ is an integer greater than $1$.\n\nHere, matchsticks are idealised lines of unit length, and they can pass through each other.\n\nThey want you to construct a ruler for them. (Never mind that they are already rulers themselves of this universe.)\n\nA ruler consists of a structure made out of matchsticks (of unit length). Matchsticks can be stuck together at their ends (with magical glue). Every pair of endpoints which are rigid with respect to each other can be used to make a measurement.\n\nFor example, when $n=2$, two equilateral triangles are affixed together, the $2$ furthest endpoints are rigid with respect to each other, and can measure a distance of $\\sqrt{3}$.", null, "You are not limited in the number of matchsticks you want to use in your ruler, the more matchsticks, the grander the ruler, of course.\n\nOf course, a ruler would be useless if it could not measure lengths. What sort of lengths can your ruler measure, for each number of dimensions?\n\n• Although this is a nice question and has a nice answer, I don't know of any way to resolve it that doesn't involve quite highbrow mathematics. Element118, do you? Aug 10, 2016 at 16:21\n\nI think the answer is that the ruler can measure\n\nany algebraic distance, in any number of dimensions.\n\nTake a look at this Wikipedia page under the heading beginning \"Representation of algebraic numbers\"; it claims that\n\nfor any algebraic number A \" for any two points p and q at distance A, there exists a finite rigid unit distance graph containing p and q such that any transformation of the plane that preserves the unit distances in this graph preserves the distance between p and q\"; the corresponding configuration of matchsticks will serve as a ruler for distance A. So in the plane, at least, we can measure any algebraic distance with such a configuration of matchsticks.\n\nOn the other hand,\n\nall distances measured by such rulers in any number of dimensions are algebraic, because if we fix one matchstick so as to rule out rigid motions of the whole structure (in the plane; in higher dimensions, we need to fix more but it is easy to ensure that all the coordinates of the points we fix are algebraic) then the coordinates of the ends of the others satisfy polynomial constraints given by the edge lengths, and the particular configuration we have is an isolated solution to these constraints (else the ruler wouldn't be rigid), and these conditions imply that the coordinates are algebraic numbers. This fact is pretty easy to prove and probably well known but the only actual reference I have is to my own PhD thesis, because when I happened to need that theorem a little bit of poking around didn't find it anywhere standard :-).\n\nWe still need to consider\n\nwhether we can measure arbitrary algebraic numbers in more dimensions. It feels as if the answer should be yes -- there should be a way to turn any rigid structure in dimension d into one in dimension d+1 by adding some sort of \"bracing\" -- but I'm not at all sure I should trust that intuition. The original Beckman-Quarles theorem, which says that preserving all unit distances implies isometry, applies in euclidean space of any dimension, but of course that's not at all the same thing. ... Aha! Although the original paper cited by the Wikipedia article doesn't appear to be publicly available, a followup by the same author is -- https://archive.org/details/arxiv-math0102023 -- and it indicates that the theorem does hold in any number of dimensions.\n\nSo, to recap:\n\nWhatever the (finite) dimensionality of your space, you can measure any algebraic distance and no other distances with rulers of this kind.\n\n• The \"bracing\" from 2 to 3 dimensions can be done with octaeders. An octaeder includes a rigid square. So you can extend a 2D structure to 3D by placing on each stick a rigid square that has two sides parallel to the additiona dimension. With rigid squares you can make rigid cubes and hypercubes. So you can probably extend this to any number of dimensions. Aug 10, 2016 at 16:00\n• Ah yes, that sounds like it would work. Aug 10, 2016 at 16:20\n• @FlorianF: I don't think octahedrons are rigid in >3D. You might be able to use general cross polytopes for the job, although I don't actually know if those are rigid. Aug 10, 2016 at 16:47\n• you can't measure number like Pi, at least in 2D, since they're transcendant numbers because you can't create such a number without circular shape. But you can't, you only have lines of unit length Aug 10, 2016 at 16:48\n• @rmilville: No one is claiming to be able to measure transcendental numbers like $\\pi$. (Though I think saying \"you can't create such a number without circular shape\" is going too far; it's not inconceivable that there might be some configuration that happens to produce a distance of $\\pi$, though it turns out that there isn't.) Aug 10, 2016 at 16:51" ]
[ null, "https://i.stack.imgur.com/zSupO.png", null ]
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http://lamecanicadelamor.com/math-addition-worksheet-maker/
[ "Home » Reading Comprehension Worksheets » 19 Math Addition Worksheet Maker\n\n# 19 Math Addition Worksheet Maker\n\nUploaded by Sarah Bailey under Reading Comprehension Worksheets [290 views ]\n\ncollection of base ten addition worksheets worksheet generator esl valid preschool subtraction worksheet valid math worksheet maker software refrence the 2 digit plus 1 digit the measuring length to the nearest half inch a math worksheet math worksheet generator fresh reading worksheet generator valid fancy maths sum generator math worksheets ideas free printable math worksheet maker save math addition worksheet math worksheets multiplication regrouping myscres grade 2 math worksheet generator fresh the mad minute math missing number addition up to 10 mental maths or early finisher 4", null, "Math Worksheet Maker Software Refrence The 2 Digit Plus 1 Digit from math addition worksheet maker , source:portaldefe.co", null, "Grade 2 Math Worksheet Generator New Rocket Math Multiplication from math addition worksheet maker , source:maginvest.co", null, "Missing Number Addition Up to 10 Mental Maths or Early Finisher 4 from math addition worksheet maker , source:pinterest.com", null, "Math Worksheets For Time Tables Refrence Time Table Worksheet from math addition worksheet maker , source:factorx.co", null, "Worksheet Generator Esl Valid Preschool Subtraction Worksheet Valid from math addition worksheet maker , source:portaldefe.co\n\nmath worksheet generator refrence math diagram new grade 2 math worksheet generator new rocket math multiplication addition tables worksheets beautiful the worksheets this page math worksheets for time tables refrence time table worksheet adding and subtracting with facts from 1 to 5 a math worksheet preschool subtraction worksheet refrence worksheets fresh worksheet free worksheets library download and print worksheets word problem math worksheet generator valid kindergarten mixed 2nd grade math worksheets ordering numbers myscres math worksheet distributive property inspirationa distributive\n\nmath facts worksheet generator fresh math fact worksheet maker collection of math worksheets maker math worksheet maker software new grade 2 math worksheet generator math worksheet generator app new algebra answer generator math facts worksheet generator new math worksheet grade 4 best math worksheet generator kidz activities math worksheet maker software fresh basic circle worksheets math math facts worksheet generator new super teacher math worksheet collection of multiplication integers worksheets 25 single digit addition questions with no regrouping a math" ]
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https://www.askiitians.com/iit-jee-progressions-and-series/arithmetic-mean-of-mth-power/
[ "#### Thank you for registering.\n\nOne of our academic counsellors will contact you within 1 working day.\n\nClick to Chat\n\n1800-5470-145\n\n+91 7353221155\n\nCART 0\n\n• 0\nMY CART (5)\n\nUse Coupon: CART20 and get 20% off on all online Study Material\n\nITEM\nDETAILS\nMRP\nDISCOUNT\nFINAL PRICE\nTotal Price: Rs.\n\nThere are no items in this cart.\nContinue Shopping\n\n# Arithmetic Mean of mth Power", null, "The concept of arithmetic mean has been already discussed in the previous sections. This concept can be extended till the mth power for terms and such mean is termed as the arithmetic mean of mth power. Mathematically, the arithmetic mean for mth power is defined as\n\nIf a1, a2, …, an be n positive real numbers (not all equal) and let m be a real number.", null, "• However if m ∈ (0, 1), then a1m + a2m+...+ anm/n < (a1+a2+...+an/n)m.\n\n• Obviously if m ∈ {0, 1}, then a1m + a2m+...+anm/n = (a1+a2+...+an/n)m.\n\nIllustration:\n\nIf a, b, c are positive real numbers such that a + b + c = 1, then prove that a/b + c + b/c+a + c/a+b > 3/2.\n\nSolution: We have to show that (a/b+c+1)+(b/c+a + 1)+(c/a+b + 1) > 3/2 + 3.\n\ni.e. 1/b+c + 1/c+1 + 1/a+b > 9/2.\n\nNow A.M. of mth power > mth power arithmetic mean (m = – 1 here)\n\n⇒ 1/3 [(b+c)–1 + (c+a)–1 + (a+b)–1] > [(b+c) + (c+a) + (a+b)/3]–1\n\n⇒ 1/b+c + 1/c+a + 1/a+b > 3.3/2(a+b+c) = 9/2.\n\nIllustration: Prove that\n\n1m + 2m + 3m + ….. + nm > n[1/2(n+1)]m.\n\nSolution: Taking ‘n’ quantities into consideration we have\n\nThen as stated above, arithmetic mean of mth powers > mth power of the arithmetic mean\n\n(1m + 2m + 3m + ….. + nm) / n > [(1+2+3+…. n) / n]m\n\nor (1m + 2m + 3m + ….. + nm) > n [ {n(n+1)/2}/n]m\n\n{Since the sum of first n natural numbers is [n(n+1)/2]}\n\nHence, (1m + 2m + 3m + ….. + nm) > n [ (n+1)/2}]m.\n\naskIITians offers extensive study material which covers all the important topics of IIT JEE Mathematics. The concepts of arithmetic mean of an A.P. or the arithmetic formula for the power have also been covered in the material. It is vital for the aspirants to be familiar with the concepts in order to remain competitive in the JEE.\n\nRelated resources:\n\nYou may also like to refer Geometric Mean and Harmonic Mean.\n\nTo read more, Buy study materials of Sequences and Series comprising study notes, revision notes, video lectures, previous year solved questions etc. Also browse for more study materials on Mathematics here." ]
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https://gauravtiwari.org/2011/04/
[ "# D’Alembert’s Ratio Test of Convergence of Series\n\nIn this article, we will formulate the D’ Alembert’s Ratio Test on convergence of a series. Let’s start. Statement of D’Alembert Ratio Test A series $\\sum {u_n}$ of positive terms is convergent if from and after some fixed term $\\dfrac {u_{n+1}} {u_n} < r < {1}$ , where r is a fixed…" ]
[ null ]
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https://bgods.cn/blog/post/59/
[ " bgods - NumPy 数组属性\n\n# NumPy 数组属性\n\n## 一、NumPy 数组属性\n\nNumPy 数组的维数称为秩(rank),秩就是轴的数量,即数组的维度,一维数组的秩为 1,二维数组的秩为 2,以此类推。\n\nNumPy 的数组中比较重要 ndarray 对象属性有:\n\nndarray.ndim 秩,即轴的数量或维度的数量\nndarray.shape 数组的维度,对于矩阵,n 行 m 列\nndarray.size 数组元素的总个数,相当于 .shape 中 n*m 的值\nndarray.dtype ndarray 对象的元素类型\nndarray.itemsize ndarray 对象中每个元素的大小,以字节为单位\nndarray.flags ndarray 对象的内存信息\nndarray.real ndarray元素的实部\nndarray.imag ndarray 元素的虚部\nndarray.data 包含实际数组元素的缓冲区,由于一般通过数组的索引获取元素,所以通常不需要使用这个属性。\n\n### 1、ndarray.ndim\n\nndarray.ndim 用于返回数组的秩,即轴的数量或维度的数量\n\n``````import numpy as np\na = np.arange(12) # 返回一个一维数组序列,和自带 range 方法类似\nprint(a.ndim) # a 现只有一个维度\n# 现在调整其大小\nb = a.reshape(4,3) # b 现在拥有2个维度\nprint(b.ndim)``````\n\n```1\n2\n```\n\n### 2、ndarray.shape\n\nndarray.shape 表示数组的维度,返回一个元组,这个元组的长度就是维度的数目,即 ndim 属性(秩)。比如,一个二维数组,其维度表示\"行数\"和\"列数\"。\n\n• 数组的维度\n``````import numpy as np\na = np.array([[1,2,3],[4,5,6]])\nprint(a.shape)``````\n\n`(2, 3)`\n• 调整数组大小\n\nndarray.shape 也可以用于调整数组大小。\n\n``````import numpy as np\na = np.array([[1,2,3],[4,5,6]])\na.shape = (3,2)\nprint(a)\nb = a.reshape(2,3) # NumPy 也提供了reshape函数来调整数组大小\nprint(b)``````\n\n```[[1 2]\n[3 4]\n[5 6]]\n\n[[1 2 3]\n[4 5 6]]```\n\n1.  a.shape 是数组对象的属性,修改只需要使用“=”重新赋值,会在原数组上修改;\n2.  a.reshape() 是数组对象的一个方法,会返回一个新的数组,原来数组不会改变。\n\n### 3、ndarray.size\n\n``````a = np.arange(24)   # 创建数组\na.shape = (4,3,2)  # 改变数组维度\nprint(a.shape)\nprint(a.size)``````\n\n`````` (4, 3, 2)\n24``````\n\n### 5、ndarray.itemsize\n\nndarray.itemsize 以字节的形式返回数组中每一个元素的大小。\n\n``````import numpy as np\n\n# 数组的 dtype 为 int8(一个字节)\nx = np.array([1,2,3,4,5], dtype = np.int8)\nprint (x.itemsize)\n\n# 数组的 dtype 现在为 float64(八个字节)\ny = np.array([1,2,3,4,5], dtype = np.float64)\nprint (y.itemsize)``````\n\n```1\n8```\n\n### 6、ndarray.flags\n\nndarray.flags 返回 ndarray 对象的内存信息,包含以下属性:\n\nC_CONTIGUOUS (C) 数据是在一个单一的C风格的连续段中\nF_CONTIGUOUS (F) 数据是在一个单一的Fortran风格的连续段中\nOWNDATA (O) 数组拥有它所使用的内存或从另一个对象中借用它\nWRITEABLE (W) 数据区域可以被写入,将该值设置为 False,则数据为只读\nALIGNED (A) 数据和所有元素都适当地对齐到硬件上\nUPDATEIFCOPY (U) 这个数组是其它数组的一个副本,当这个数组被释放时,原数组的内容将被更新\n``````import numpy as np\n\nx = np.array([1,2,3,4,5])\nprint (x.flags)``````\n\n``` C_CONTIGUOUS : True\nF_CONTIGUOUS : True\nOWNDATA : True\nWRITEABLE : True\nALIGNED : True\nWRITEBACKIFCOPY : False\nUPDATEIFCOPY : False```\n\n### 7、ndarray.real和ndarray.imag\n\nndarray.real 获取 ndarray 元素的实部,ndarray.imag 获取 ndarray 元素的虚部。如:\n\n``````a = np.array([1+3j, 2+4j])\nprint(\"数组a是:\", a)\nprint(\"实部:\", a.real)\nprint(\"虚部:\", a.imag)``````\n\n``````数组a是: [1.+3.j 2.+4.j]\n\n\n\n0 评论" ]
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https://www.greenlighttestprep.com/module/gre-probability/video/759
[ "# Lesson: Listing vs Counting vs Probability Rules\n\n## Comment on Listing vs Counting vs Probability Rules\n\n### At the 1:23 mark, why can't\n\nAt the 1:23 mark, why can't you follow the formula and 1/2 + 1/2?", null, "### We could have continued that\n\nWe could have continued that approach, but this video is all about examining our different options and probability questions involving \"at least\" are typically solved the fasted by using the complement.\n\nThat said, let's continue where we left off: P(1 heads) + P(2 heads)\n\nWe'll deal with each probability on its own.\n\nP(1 heads) = P(1st toss heads and 2nd toss tails OR 1st toss tails and 2nd toss heads)\n= P(1st toss heads and 2nd toss tails) + P(1st toss tails and 2nd toss heads)\n= (1/2)(1/2) + (1/2)(1/2)\n= 1/4 + 1/4\n= 1/2\n\n= (1/2)(1/2)\n= 1/4\n\nSo, P(1 heads) + P(2 heads) = 1/2 + 1/4 = 3/4\n\n### 6C2/10C2.. Can you solve it\n\n6C2/10C2.. Can you solve it in detail.. I mean do we have to simplify it like 6C2=180...Or there is a shortcut to solve this", null, "### Yes, there is definitely a\n\nYes, there is definitely a shortcut.\nHere's the video that explains how you can calculate 6C2 and 10C2 in your head: https://www.greenlighttestprep.com/module/gre-counting/video/789\n\nCheers,\nBrent\n\n### I got it.. Thanks\n\nI got it.. Thanks\n\n### Hello Brent,\n\nHello Brent,\n\nI solved the question as follows\nJoe is in a group consisting of N people (N > 4).\n\nIf 3 people from the group are randomly selected to be on a committee, what is the probability that Joe is selected?\n\nI assument N = 5 , there are total of 5C3 was to select people , this is my denominator that is 1/10.\nNow i have to choose Joe so 1 way now remaining 2 people can be selected in 4C2 ways that is (1 X 4 X 3)/ (2 X 1) which comes to 6.\n\nSO final answer is 6/10 = 3/5 hence option C. am i right.", null, "You're using the INPUT-OUTPUT approach to solve this question (covered here: https://www.greenlighttestprep.com/module/gre-word-problems/video/936)\n\nWhen N = 5, the probability = 3/5\n\nAt this point, we must check ALL 5 answer to see which one(s) evaluate to be 3/5 when N = 5\n\nA) When N = 5, (N²−2N−6)/(N−2)²+6 = 3/5\nC) When N = 5, N/5 = 3/5\n\nSo, the correct answer is EITHER A or C.\n\nFrom here, you must test a different value of N to determine the correct answer.\n\nCheers,\nBrent\n\n### Hi Brent,\n\nHi Brent,\nIn the last question of Reinforcement Activities, click on the link GRE practice question (difficulty level: 160 to 170) – Greenlight Test Prep\nInstead of asking of what is the probability that Joe is selected, he is asking what is the probabilty of selection three people, what would be the answer to this question?", null, "Sorry, but I'm not sure what you mean by \"probability of selection three people\"\n\n### It's great how you can try\n\nIt's great how you can try multiple approached to get the same answer with probability questions. The only issue I see here is which approach is the shortest. I don't think you can accurately assess that in the beginning. When you start with 1 approach, it's best to just carry it out to the end. However long it takes, it takes, and just hope that you get the right answer. If you get stuck, then you'll have to try a different approach if you can, which still eats up time. Really, the greatest enemy on the GRE is time. I keep coming back to this theme again and again.", null, "### Good points.\n\nGood points.\nIn general, I find that applying probability rules is typically faster than using counting techniques." ]
[ null, "https://www.greenlighttestprep.com/sites/default/files/styles/thumbnail/public/pictures/picture-1-1475568960.jpg", null, "https://www.greenlighttestprep.com/sites/default/files/styles/thumbnail/public/pictures/picture-1-1475568960.jpg", null, "https://www.greenlighttestprep.com/sites/default/files/styles/thumbnail/public/pictures/picture-1-1475568960.jpg", null, "https://www.greenlighttestprep.com/sites/default/files/styles/thumbnail/public/pictures/picture-1-1475568960.jpg", null, "https://www.greenlighttestprep.com/sites/default/files/styles/thumbnail/public/pictures/picture-1-1475568960.jpg", null ]
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https://math.stackexchange.com/questions/3016507/derivative-of-a-functional-with-respect-to-another-functional
[ "# Derivative of a functional with respect to another functional\n\nI am trying to make sense of functional derivatives and have a couple of questions bothering me:\n\n1. Let $$F[X]$$ be a functional of $$X(t)$$ and $$G[X]$$ another functional of $$X(t)$$.\n\nBy chain rule in the continum I intuitively guess that the derivative of the functional F[X] with respect to the functional G[X] is:$$\\frac{\\delta F}{\\delta G} = \\int dt \\frac{\\delta F[X]}{\\delta X(t)} \\frac{\\delta X(t)}{\\delta G[X]} = \\int dt \\frac{\\delta F[X]}{\\delta X(t)} \\left(\\frac{\\delta G[X]}{\\delta X(t)} \\right)^{-1}$$ Does this make any sense at all? Is there such thing as a derivative of a functional with respect to another functional given they are both dependent on the same underlying function X(t)?\n\n2. How would one calculate the functional derivatives $$\\frac{\\delta F[X]}{\\delta X(t)}$$ and $$\\frac{\\delta G[X]}{\\delta X(t)}$$? I came across Gateaux derivative and It seems to be similar to a directional derivative. Does it matter what direction is being chosen to evaluate the final functional derivative?\n\n• I am not sure what you are asking. Please rewrite. – Will M. Dec 11 '18 at 5:14\n• Thanks Will, just edited please let me know if it's still not clear. – ZeroCool Dec 11 '18 at 15:44\n• OK. It still makes no sense. However, two points to bring. (1) Frechet derivative is simply the usual derivative on learns from calculus 2 (at least in places like the one I studied where math rigour is imposed over being able to perform calculations) and (2) Gateaux derivatives are directional derivatives and, as always, they depend on the chosen direction. If you want to know the derivatives of a composition $g \\circ f,$ then simply apply the chain rule $g'(f(a)) \\circ f'(a).$ If you want to know how to calculate $f'$ or $g',$ you need to know the exact form first an apply rules then. – Will M. Dec 11 '18 at 18:05\n• @ZeroCool you might want to ask on MathOverflow. This site is for more elementary questions (usually pre-functional-derivative stage). – Nike Dattani May 30 '20 at 22:18" ]
[ null ]
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https://www.alglib.net/dataanalysis/generalprinciples.php
[ "# Dataset Format\n\nDatasets are represented as a matrices, with lines corresponding to sample components and with columns corresponding to variables. Three types of tasks to be performed and, respectively, three formats to be used can be distinguished:\n\n• Task One - this is a regression task, a problem of prediction of the value of a dependent variable (or several variables), if independent variable values are known (for example, currency rate prediction based on prior values). The predicted value has real type. In this case, independent variables are kept in the first NVars columns of the array, with columns featuring dependent variables following them.\n• Task Two - this is a classification task, a problem involved in referring an observation to one of the classes. The predicted variable has a nominal value. As in the previous case, the first NVars of the columns contain independent variables. The following column will contain the class number (from 0 to NClasses-1). Fractional values are rounded to the nearest integer.\n• Lastly, the third type is referred to the tasks which are not regression or classification problems, such as clustering. In such cases, a training set will contain, as a rule, only independent variables (the first NVars columns).\n\nNote #1\nData encoding in classification tasks is somewhat different from encoding used by many other packages. For example, it is customary in a number of neural-network libraries to encode adherence of an image to one of the classes by means of the NClasses-dimensional vector, through setting the relevant coordinate into 1 and making the rest equal to zero. This difference should be taken into account when the ALGLIB and other program packages are used simultaneously.\n\n# Nominal Variable Encoding\n\nNominal variables can be encoded in several ways: as integer or using either \"1-of-N\" or \"1-of-N-1\" encoding. Most ALGLIB algorithms can use any encoding, without requesting information about which variables are real and which are nominal, as well as concerning encoding used. The algorithm will just take a real matrix, and operate on it without going into particulars of its inner structure. It provides for flexibility and usability. However, different encodings have different action upon the speed and quality of algorithm operation. It is recommended to comply with the following conventions:\n\n• Real variables are kept as they are.\n• Nominal variables with two possible values are encoded by either \"0\" or \"1\" (that is, using the \"1-of-N-1\" encoding).\n• Nominal variables with three or more possible values are encoded using \"1-of-N\" encoding (e.g., \"red\", \"yellow\" and \"green\" can be encoded as \"1 0 0\", \"0 1 0\", \"0 0 1\").\n• No matter how many values are possible, a nominal variable can be encoded by integer (0, 1, 2, ...). However, such encoding is recommended to be used only in case values of the variable can be ordered, and to be applied only to nonlinear models (neural networks, decision trees). For instance, such values as \"cold\", \"room temperature\", \"heat\" can be arranged according to the increase of temperature, and encoded as \"0\", \"1\", \"2\". Meanwhile, reasonable arrangement of such values as \"sour\", \"bitter\", \"sweet\", \"salt\" is somewhat complicated.\n\nThe ALGLIB package can be used, even if the data are encoded without regard to these recommendations. However, some models may use such encoding to increase the speed and to improve quality of the results.\n\n# Missing Values Encoding\n\nOn the date this article was written, none of the algorithms can perform operations on datsets with missing values. However, this restriction can be avoided, if another value identifying the omission is added to like values of the variable. For example, if accepted values of the variable are \"0\", \"1\", \"2\", then the non-missing values can be encoded as \"1 0 0 0\", \"0 1 0 0\", \"0 0 1 0\", and the missing value can be transformed into \"0 0 0 1\". The following encoding will be analogous for the real variable: the non-missed value x is encoded as as \"x 0\", and the missing value is encoded as \"0 1\".\n\nOne more option is replacing the missing value by an average (or most probable) value for this variable.\n\n# Standard Error Codes\n\nMany data analysis subprograms accept the Info output parameter. This variable contains a return code of the subroutine. A positive value means normal completion, and a negative value is evidence of an error. Subroutines of this section solve similar problems, therefore their error codes make up a uniform system, too:\n\n• -1 - incorrect parameters (e.g., negative size of a training set).\n• -2 - errors in the training set (e.g., a class N3 is detected in the training set when dealing with a binary classification problem).\n• -3 - task is degenerate. Specific understanding of the word \"degenerate\" will be subject to the situation. For example, a clustering task shall be considered degenerate if five elements need referring to six clusters.\n• -4 - non-convergence of an iterative algorithm.\n\n# ALGLIB Classifiers and Posterior Probabilities\n\nThere are two basic views commonly held in statistics on how a classification problem solution should look like. The first viewpoint is that any object shall refer to one and only one of the classes. For example, if email classification is in question, then \"spam\" and \"non-spam\" classes can be distinguished. There can be some uncertainty in the classification (an email can be somewhat similar to spam), but only the terminal decision - whether it is spam or non-spam - will be returned.\n\nThe second approach consists in obtaining a vector of posterior probabilities, that is, a vector having component parts equal to probabilities that the object belongs to each class. The algorithm does not take any decision on the classification of an email. It just notifies how much probability there is that a particular email is spam, and how much probability there is that it is not. And the decision making based on this information is transferred to the user.\n\nThe second approach is more flexible than the first one, and it is more reasonable. How does the classification algorithm happen to know about the order of priority the user is sticking to? In some cases, it is necessary to minimize the error made in one of the classes, e.g., the misclassification of an email as spam. Then the email will be classified as spam only in that case if there is very little probability (e.g., less than 0.05%) that it is NON spam. In other cases, all classes are equal to each other, and a class with a maximum conditional probability can just be chosen. Therefore, the outcome of any classification algorithm of the ALGLIB package is a posterior probability vector, instead of the class which an object can be put into.\n\n# Model Error\n\nAfter the model is built, the error on a test (or training) set needs to be estimated. To estimate regression results, three measures of error can be used, that is, a root-mean-square error, an average error and an average relative error (the latter being calculated as per the records with a nonzero value of the dependent variable). These three measures of error are commonly known, and need not to be discussed.\n\nIf a classification problem is at issue, then five measures of error can be used. The first and best-known is the classification error (the number or percent of the incorrectly classified cases). The second equally known measure is cross-entropy. The ALGLIB package uses average cross-entropy per record estimated in bits (base 2 logarithm). The use of average cross-entropy (instead of total cross-entropy) permits comparable estimates for different test sets to be obtained.\n\nThe remaining three error measures are the root-mean-square error, average error and average relative error again. However, as opposed to the regression task, they are used here to characterize the posterior probability vector miscalculation. The error implies how much the probability vector calculated by means of a classification algorithm differs from the vector obtained on the basis of a test set (this vector's component parts are equal to 0 or 1, subject to the class which the object belongs to). The meaning of the root-mean-square error and average error is comprehensible: it is an error in conditional probability approximation that is averaged as per all probabilities. The average relative error is an average error in approximating the probability that an object is correctly classified (same as average error for binary tasks).\n\nALGLIB Project offers you two editions of ALGLIB:\n\nALGLIB Free Edition:", null, "delivered for free", null, "offers full set of numerical functionality", null, "extensive algorithmic optimizations", null, "no low level optimizations", null, "non-commercial license\n\nALGLIB Commercial Edition:", null, "flexible pricing", null, "offers full set of numerical functionality", null, "extensive algorithmic optimizations", null, "high performance (SMP, SIMD)", null, "commercial license with support plan\n\n## ALGLIB 3.16.0 for C++", null, "C++ library.\nDelivered with sources.\nMonolithic design.\nExtreme portability.\nEditions:   FREE   COMMERCIAL\n\n## ALGLIB 3.16.0 for C#", null, "C# library with native kernels.\nDelivered with sources.\nVB.NET and IronPython wrappers.\nExtreme portability.\nEditions:   FREE   COMMERCIAL\n\n## ALGLIB 3.16.0 for Delphi", null, "Delphi wrapper around C core.\nDelivered as precompiled binary.\nCompatible with FreePascal.\nEditions:   FREE   COMMERCIAL\n\n## ALGLIB 3.16.0 for CPython", null, "CPython wrapper around C core.\nDelivered as precompiled binary.\nEditions:   FREE   COMMERCIAL" ]
[ null, "https://www.alglib.net/img/plus_green.gif", null, "https://www.alglib.net/img/plus_green.gif", null, "https://www.alglib.net/img/plus_green.gif", null, "https://www.alglib.net/img/minus_red.gif", null, "https://www.alglib.net/img/minus_red.gif", null, "https://www.alglib.net/img/plus_green.gif", null, "https://www.alglib.net/img/plus_green.gif", null, "https://www.alglib.net/img/plus_green.gif", null, "https://www.alglib.net/img/plus_green.gif", null, "https://www.alglib.net/img/plus_green.gif", null, "https://www.alglib.net/img/alglib_red_cube_64.png", null, "https://www.alglib.net/img/alglib_green_cube_64.png", null, "https://www.alglib.net/img/alglib_delphi_cube_64.png", null, "https://www.alglib.net/img/alglib_python_cube_64.png", null ]
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http://publications.waset.org/16788/unscented-transformation-for-estimating-the-lyapunov-exponents-of-chaotic-time-series-corrupted-by-random-noise
[ "Commenced in January 2007\nFrequency: Monthly\nEdition: International\nPaper Count: 30455\n##### Unscented Transformation for Estimating the Lyapunov Exponents of Chaotic Time Series Corrupted by Random Noise\n\nAuthors: K. Kamalanand, P. Mannar Jawahar\n\nAbstract:\n\nMany systems in the natural world exhibit chaos or non-linear behavior, the complexity of which is so great that they appear to be random. Identification of chaos in experimental data is essential for characterizing the system and for analyzing the predictability of the data under analysis. The Lyapunov exponents provide a quantitative measure of the sensitivity to initial conditions and are the most useful dynamical diagnostic for chaotic systems. However, it is difficult to accurately estimate the Lyapunov exponents of chaotic signals which are corrupted by a random noise. In this work, a method for estimation of Lyapunov exponents from noisy time series using unscented transformation is proposed. The proposed methodology was validated using time series obtained from known chaotic maps. In this paper, the objective of the work, the proposed methodology and validation results are discussed in detail.\n\nDigital Object Identifier (DOI): doi.org/10.5281/zenodo.1335684\n\nReferences:\n\n N. L. Gerr, and J. C. Allen, “Stochastic versions of chaotic time series: generalized logistic and Henon time series models,” Physics D, vol. 68, 1993, pp. 232-249\n E. Takens, “Detecting nonlinearities in stationary time series,” International Journal of Bifurcation and Chaos, vol. 3, 1993, pp. 241- 256\n D. F. McCaffrey, S. Ellner, A. R. Gallant and D. W. Nychka, “Estimating the Lyapunov exponent of a chaotic system with nonparametric regression,” Journal of the Amer. Sta.l Assoc., vol. 87, 1992, pp. 682-695\n X. Zeng, R. Eykholt and R. A. Pielke, “Estimating the lyapunovexponent spectrum from short time series of low precision,” Phys. Rev. Let., vol. 66, 1991\n S. Mototsugu and L. Oliver, “Nonparametric neural network estimation of Lyapunov exponents and a direct test for chaos,” Journal of Econometrics, vol. 120, 2004, pp. 1–33\n A. N. Edmonds, “Time series prediction using supervised learning and tools from chaos theory,” Faculty of Science and Computing, University of Luton, Ph.D Thesis, 1996\n M. Ataei, A. Khaki-Sedigh, B. Lohmann and C. Lucas, “Estimating the lyapunov exponents of chaotic time series: a model based method,” Proceedings of European Control Conference, 2003\n H. Kantz, “A robust method to estimate the maximum Lyapunov exponent of a time series,” Phys. Lett. A, vol. 185, 1994, pp. 77-87\n M. Sano and Y. Sawada, “Measurement of the Lyapunov spectrum from a chaotic time series,” Phys. Rev. Let., vol. 55, 1985, pp. 1082-1085\n M. T. Rosenstein, J. J. Collins and C. J. De Luca, “A practical method for calculating largest Lyapunov exponents from small data sets,” Physica D, vol. 65, 1993, pp. 117-134\n A. Wolf, J. B. Swift, H. L. Swinney and J. A. Vastano, “Determining Lyapunov exponents from a time series,” Physica D, vol. 16, 1985, pp. 285-317\n J.-P. Eckmann and D. Ruelle, “Ergodic theory of chaos and strange attractors,” Reviews of Modern Physics, vol. 57, 1985, pp. 617–656\n J.-P. Eckmann, S. O. Kamphorst, D. Ruelle and S. Ciliberto, “Liapunov exponents from time series,” Physical Review A, vol. 34, 1986, pp. 4971–4979\n D. Nychka, S. Ellner, A. R. Gallant and D. McCaHrey, “Finding chaos in noisy system,” Journal of the Royal Statistical Society, Series B, vol. 54, 1992, pp. 399–426\n S. J. Julier and J. K. Uhlmann, “Unscented filtering and nonlinear estimation,” Proceedings of the IEEE, vol. 92, 2004, pp. 401-422\n Wan, E. and R. Van der Merwe, “The unscented Kalman filter,” Wiley Publishing, 2001\n Li Hongli, J. Wang, Y. Che, H. Wang and Y. Chen, “On neural network training algorithm based on the unscented Kalman filter,” Proceedings of 29th Chinese Control Conference, 2010, pp. 1447-1450\n J. C. Sprott, “Chaos and time series analysis,” oxford university press, 2003\n R. L. Devaney, “An introduction to chaotic dynamical systems,” 2nd edition, Addison Wesley, Redwood City, CA, 1989\n S. H. Strogatz, “Nonlinear dynamics and chaos,” Perseus publishing, 1994\n W. E. Ricker, “Stock and recruitment,” J. Fisheries Res. Board Can., vol. 11, 1954, pp. 559-623\n G. W. Frank, T. Lookman, M. A. H. Nerenberg, C. Essex, J. Lemieux and W. Blume, “Chaotic time series analysis of epileptic seizures,” Physica D, vol. 46, 1990, pp. 427\n P. Chen, “Empirical and theoretical evidence of economic chaos,” Sys. Dyn. Rev., vol. 4, 1988, pp. 81" ]
[ null ]
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https://www.unitconverters.net/energy/newton-meter-to-joule.htm
[ "Home / Energy Conversion / Convert Newton Meter to Joule\n\n# Convert Newton Meter to Joule\n\nPlease provide values below to convert newton meter [N*m] to joule [J], or vice versa.\n\n From: newton meter To: joule\n\n### Newton-meter\n\nDefinition: The newton-meter (N·m) is sometimes used as a unit of work or energy and in this context is equal to the joule, the SI unit of energy. In this use, it is defined as the energy transferred to an object by a one newton force acting on that object in the direction of its motion over a distance of one meter.\n\nHistory/origin: The use of the newton-meter as a unit of work or energy is derived from the fact that the joule, the SI (International System of Units) unit of energy, is dimensionally equivalent to the newton-meter.\n\nCurrent use: The newton-meter is more commonly used as a unit of torque rather than as a unit of work or energy. As such, the use of the newton-meter as a unit of work or energy is discouraged to avoid confusion regarding whether energy or torque is being expressed.\n\n### Joule\n\nDefinition: A joule (symbol: J) is a derived unit of energy in the International System of Units (SI). It is defined as the energy transferred to an object when a one newton force is applied to the object in the direction of its motion through a distance of one meter. It is also defined as the energy dissipated as heat when a 1 ampere electric current passes through a resistance of one ohm in the course of one second. It has a number of representations both in SI base units as well as other SI units such that:\n\nJ = kg·m2/s2 = N·m = Pa·m3 = W·s = C·V\n\nHistory/origin: The unit, joule, is named after James Prescott Joule, an English physicist and mathematician who helped develop the Kelvin scale. He also discovered the relationship between heat and mechanical work, leading to the law of conservation of energy, and subsequently, the first law of thermodynamics.\n\nCurrent use: As an SI derived unit, the joule is used within a variety of scientific contexts. Practical examples of energy measurement using joules include the energy required to lift objects, the energy released when objects fall, the heat required to raise temperature, and the kinetic energy of moving objects.\n\nOne of the dimensional representations of a joule is the N·m (Newton-meter), which is equivalent to the SI unit for torque. These units however, are different, and should be considered as such. Even though the joule is algebraically equal to the N·m, the N·m should not be used to represent the joule whenever possible, to avoid confusion with torque.\n\n### Newton Meter to Joule Conversion Table\n\nNewton Meter [N*m]Joule [J]\n0.01 N*m0.01 J\n0.1 N*m0.1 J\n1 N*m1 J\n2 N*m2 J\n3 N*m3 J\n5 N*m5 J\n10 N*m10 J\n20 N*m20 J\n50 N*m50 J\n100 N*m100 J\n1000 N*m1000 J\n\n### How to Convert Newton Meter to Joule\n\n1 N*m = 1 J\n1 J = 1 N*m\n\nExample: convert 15 N*m to J:\n15 N*m = 15 × 1 J = 15 J" ]
[ null ]
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http://encyclopedia.kids.net.au/page/qu/Quaternion
[ "", null, "", null, "## Encyclopedia > Quaternion\n\nArticle Content\n\n# Quaternion\n\nQuaternions are an extension of the real numbers, similar to the complex numbers. While the real numbers are extended to the complex numbers by adding a number i such that i2 = -1, quaternions are extended by adding elements i, j and k to the real numbers such that i2 = j2 = k2 = ijk = -1. A quaternion then is a number of the form a + bi + cj + dk, where a, b, c, and d are real numbers uniquely determined by the quaternion. The multiplication of quaternions could be deduced from the following multiplication table:\n\n · 1 i j k 1 1 i j k i i -1 k -j j j -k -1 i k k j -i -1\n\nThese products form the quaternion group of order 8, Q8.\n\nUnlike real or complex numbers, multiplication of quaternions is not commutative: ij = k, ji = -k, jk = i, kj = -i, ki = j, ik = -j. The quaternions are an example of a skew field, an algebraic structure similar to a field except for commutativity of multiplication. In particular, multiplication is still associative and every non-zero element has a unique inverse. They form a 4-dimensional associative algebra over the reals (in fact a division algebra) and contain the complex numbers, but they do not form an associative algebra over the complex numbers. The quaternions, along with the complex and real numbers, are the only finite dimensional skew fields over the field of real numbers.\n\nThe non-commutativity of multiplication has some unexpected consequences, among them that polynomial equations over the quaternions can have more solutions than the polynomial's degree indicates. The equation z2 + 1 = 0 for instance has the infinitely many quaternions z = bi + cj + dk with a2 + c2 + d2 = 1 as solutions.\n\nThe conjugate of the quaternion z = a + bi + cj + dk is defined as z* = a - bi - cj - dk, and the absolute value of z is the non-negative real number defined by |z| = √(zz*) = √(a2 + b2 + c2 + d2). Note that (wz)*z*w*, which is not in general equal to w*z*. The multiplicative inverse of the non-zero quaternion z can be conveniently computed as z-1 = z* / |z|2.\n\nBy using the distance function d(z,w) = |z - w|, the quaternions form a metric space and the arithmetic operations are continuous. We also have |zw| = |z| |w| for all quaternions z and w. Using the absolute value as norm, the quaternions form a real Banach algebra.\n\nAs is explained in more detail in quaternions and spatial rotation, the multiplicative group of non-zero quaternions acts by conjugation on the copy of R3 consisting of quaternions with real part equal to zero: it is not hard to see that the conjugation by a unit quaternion (a quaternion of absolute value 1) with real part cos t is a rotation by an angle 2t, the axis of the rotation being the direction of the imaginary part. Quaternions are sometimes used in computer graphics (and associated geometric analysis) to represent rotations or orientations of objects in 3d space. The advantages are: non singular representation (compared with Euler angles[?] for example), more compact (and faster) than matrices.\n\nThe set of all unit quaternions forms a 3-dimensional sphere S3 and a group (even a Lie group) under multiplication. S3 is the double cover of the group SO(3,R) of real orthogonal 3x3 matrices of determinant 1 since two unit quaternions correspond to every rotation under the above correspondence. The group S3 is isomorphic to SU(2), the group of complex unitary 2x2 matrices of determinant 1.\n\nLet A be the set of quaternions of the form a + bi + cj + dk where a, b, c and d are either all integers or all rational numbers with odd numerator and denominator 2. The set A is a ring and a lattice. There are 24 unit quaternions in this ring and they are the vertices of a regular polytope[?] called {3,4,3} in Schlafli's notation.\n\nThere are at least two ways of representing quaternions as matrices, in such a way that quaternion addition and multiplication correspond to matrix addition and matrix multiplication. One is to use 2x2 complex matrices, and the other is to use 4x4 real matrices.\n\nIn the first way, the quaternion a + bi + cj + dk is represented as:\n\n$\\begin{pmatrix} a-di & -b+ci \\\\ b+ci & a+di \\end{pmatrix}$\n\nThis representation has several nice properties:\n\nwith only real entries.\n• The absolute value of a quaternion is the same as the determinant of the corresponding matrix.\n• The conjugate of a quaternion corresponds to the conjugate transpose of the matrix.\n• Restricted to unit quaternions, this representation provides the isomorphism between S3 and SU(2). The latter group is important in quantum mechanics when dealing with spin; see all Pauli matrices.\n\nIn the second way, the quaternion a + bi + cj + dk is represented as:\n\n$\\begin{pmatrix} a & -b & d & -c \\\\ b & a & -c & -d \\\\ -d & c & a & -b \\\\ c & d & b & a \\end{pmatrix}$\n\n\nIn this representation, the conjugate of a quaternion corresponds to the transpose of the matrix.\n\nQuaternions were discovered by William Rowan Hamilton in 1843. Hamilton was looking for ways of extending complex numbers (which can be viewed as points on a plane) to higher spatial dimensions. He could not do so for 3-dimensions, but 4-dimensions produce quaternions. According to a story he told, he was out walking one day with his wife when the solution in the form of equation i2 = j2 = k2 = ijk = -1 suddenly occurred to him; he then promptly carved this equation into the side of nearby Brougham bridge.\n\nThis involved abandoning the commutative law, a radical step for the time. Vector algebra and matrices were still in the future. Not only this, but Hamilton had in a sense invented the cross and dot products of vector algebra. Hamilton also described a quaternion as an ordered four-element multiple of real numbers, and described the first element as the 'scalar' part, and the remaining three as the 'vector' part. If two quaternions with zero scalar parts are multiplied, the scalar part of the product is the negative of the dot product of the vector parts, while the vector part of the product is the cross product. But the significance of these was still to be discovered.\n\nHamilton proceeded to popularize quaternions with several books, the last of which, Elements of Quaternions, had 800 pages and was published shortly after his death.\n\nEven by this time there was controversy about the use of quaternions. Some of Hamilton's supporters viciously opposed the growing fields of vector algebra and vector calculus (from developers like Oliver Heaviside and Willard Gibbs), maintaining that quaternions provided a superior notation. While this may be true in three dimensions plus time (i.e., spacetime), quaternions cannot be used in other dimensions (though other deriverative exist like Octonions and Clifford algebras for this). Their scientific recognition compared to vectors has therefore decreased over time. They are today still used in computer graphics and Plasma physics.\n\nIf F is any field and a and b are elements of F, one may define a four-dimensional unitary associative algebra over F by using two generators i and j and the relations i2 = a, j2 = b and ij = -ji. These algebras are either isomorphic to the algebra of 2-by-2 matrices over F, or they are division algebras over F. They are called quaternion algebras[?].\n\nAll Wikipedia text is available under the terms of the GNU Free Documentation License\n\nSearch Encyclopedia\n Search over one million articles, find something about almost anything!\n\nFeatured Article\n Sanskrit language ... earliest dated illustrated Sanskrit manuscript in the world (http://ds.dial.pipex.com/town/avenue/xha71/pow2.htm) A ...", null, "", null, "" ]
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https://sqlservercode.blogspot.com/2018/01/
[ "## Monday, January 15, 2018\n\n### When uncompressing data, make sure to use the correct function", null, "SQL Server has offered data compression for a while now, you could either use PAGE compression or ROW compression, you had no ability so specify which columns.  That changed in SQL Server 2016\n\nSQL Server 2016 added the ability to compress data yourself by using the COMPRESS function. The COMPRESS function compresses the input expression using the GZIP algorithm. The result of the compression is byte array of type varbinary(max).\n\nLet's take a quick look at how this function works\n\nWe will create a table, insert one row and then update the SomeOtherColumn value by using the COMPRESS function on the SomeColumn column\n\n```CREATE TABLE test (Somecolumn varchar(200), SomeOtherColumn varbinary(max))\ngo```\n```INSERT test VALUES ('aaaaaaaaaaaaa', null)\n\n```\n```\n```\n```UPDATE test\nSET SomeOtherColumn = COMPRESS(Somecolumn)\ngo\n\nSELECT Somecolumn,SomeOtherColumn\nFROM test```\n\nHere is what the output looks like\n\nWhat if if told you now to create a new table by uncompressing the data via a SELECT INTO query followed by dropping the old table\n\nNo problem, if there is a COMPRESS function then surely there must be an UNCOMPRESS function... right?  Let's find out......\n\n```SELECT Somecolumn,CAST( UNCOMPRESS(SomeOtherColumn) AS varchar(max)) AS SomeOtherColumn\nINTO SomeNewTable\nFROM test\n\nDROP TABLE test```\n\n```SELECT *\nFROM SomeNewTable```\n\nWrong, while the UNCOMPRESS function exists, it is not the correct function\n\nHopefully you ran a test before just dropping a table after doing select into\n\nThe correct function is DECOMPRESS\n\nHere is what it all looks like\n\n```SELECT Somecolumn,SomeOtherColumn,\nCAST( DECOMPRESS(SomeOtherColumn) AS varchar(max)) AS CastedDecompressed,\nDECOMPRESS(SomeOtherColumn) as Decompressed FROM test\n\nSELECT Somecolumn,SomeOtherColumn,\nCAST( UNCOMPRESS(SomeOtherColumn) AS varchar(max)) AS CastedUncompressed,\nUNCOMPRESS(SomeOtherColumn) as Uncompressed FROM test\n```\n\nThis is the output\n\nAs you can see the UNCOMPRESS function returns a bunch of nonsense while the DECOMPRESS function works as expected\n\nSo the question is really wth is the uncompress function?" ]
[ null, "https://2.bp.blogspot.com/-zLH3cttwkPw/WBRCgh72wUI/AAAAAAAAGMY/Pvx_WlQjFIgSo41svDv--iGG70afDa9egCLcB/s320/sqlserver2016.PNG", null ]
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https://www.colorhexa.com/3b3617
[ "# #3b3617 Color Information\n\nIn a RGB color space, hex #3b3617 is composed of 23.1% red, 21.2% green and 9% blue. Whereas in a CMYK color space, it is composed of 0% cyan, 8.5% magenta, 61% yellow and 76.9% black. It has a hue angle of 51.7 degrees, a saturation of 43.9% and a lightness of 16.1%. #3b3617 color hex could be obtained by blending #766c2e with #000000. Closest websafe color is: #333300.\n\n• R 23\n• G 21\n• B 9\nRGB color chart\n• C 0\n• M 8\n• Y 61\n• K 77\nCMYK color chart\n\n#3b3617 color description : Very dark yellow [Olive tone].\n\n# #3b3617 Color Conversion\n\nThe hexadecimal color #3b3617 has RGB values of R:59, G:54, B:23 and CMYK values of C:0, M:0.08, Y:0.61, K:0.77. Its decimal value is 3880471.\n\nHex triplet RGB Decimal 3b3617 `#3b3617` 59, 54, 23 `rgb(59,54,23)` 23.1, 21.2, 9 `rgb(23.1%,21.2%,9%)` 0, 8, 61, 77 51.7°, 43.9, 16.1 `hsl(51.7,43.9%,16.1%)` 51.7°, 61, 23.1 333300 `#333300`\nCIE-LAB 22.409, -2.812, 20.063 3.277, 3.63, 1.339 0.397, 0.44, 3.63 22.409, 20.259, 97.978 22.409, 4.219, 17.709 19.053, -2.637, 9.171 00111011, 00110110, 00010111\n\n# Color Schemes with #3b3617\n\n• #3b3617\n``#3b3617` `rgb(59,54,23)``\n• #171c3b\n``#171c3b` `rgb(23,28,59)``\nComplementary Color\n• #3b2417\n``#3b2417` `rgb(59,36,23)``\n• #3b3617\n``#3b3617` `rgb(59,54,23)``\n• #2e3b17\n``#2e3b17` `rgb(46,59,23)``\nAnalogous Color\n• #24173b\n``#24173b` `rgb(36,23,59)``\n• #3b3617\n``#3b3617` `rgb(59,54,23)``\n• #172e3b\n``#172e3b` `rgb(23,46,59)``\nSplit Complementary Color\n• #36173b\n``#36173b` `rgb(54,23,59)``\n• #3b3617\n``#3b3617` `rgb(59,54,23)``\n• #173b36\n``#173b36` `rgb(23,59,54)``\nTriadic Color\n• #3b171c\n``#3b171c` `rgb(59,23,28)``\n• #3b3617\n``#3b3617` `rgb(59,54,23)``\n• #173b36\n``#173b36` `rgb(23,59,54)``\n• #171c3b\n``#171c3b` `rgb(23,28,59)``\nTetradic Color\n• #040402\n``#040402` `rgb(4,4,2)``\n• #161409\n``#161409` `rgb(22,20,9)``\n• #292510\n``#292510` `rgb(41,37,16)``\n• #3b3617\n``#3b3617` `rgb(59,54,23)``\n• #4d471e\n``#4d471e` `rgb(77,71,30)``\n• #605825\n``#605825` `rgb(96,88,37)``\n• #72682c\n``#72682c` `rgb(114,104,44)``\nMonochromatic Color\n\n# Alternatives to #3b3617\n\nBelow, you can see some colors close to #3b3617. Having a set of related colors can be useful if you need an inspirational alternative to your original color choice.\n\n• #3b2d17\n``#3b2d17` `rgb(59,45,23)``\n• #3b3017\n``#3b3017` `rgb(59,48,23)``\n• #3b3317\n``#3b3317` `rgb(59,51,23)``\n• #3b3617\n``#3b3617` `rgb(59,54,23)``\n• #3b3917\n``#3b3917` `rgb(59,57,23)``\n• #3a3b17\n``#3a3b17` `rgb(58,59,23)``\n• #373b17\n``#373b17` `rgb(55,59,23)``\nSimilar Colors\n\n# #3b3617 Preview\n\nText with hexadecimal color #3b3617\n\nThis text has a font color of #3b3617.\n\n``<span style=\"color:#3b3617;\">Text here</span>``\n#3b3617 background color\n\nThis paragraph has a background color of #3b3617.\n\n``<p style=\"background-color:#3b3617;\">Content here</p>``\n#3b3617 border color\n\nThis element has a border color of #3b3617.\n\n``<div style=\"border:1px solid #3b3617;\">Content here</div>``\nCSS codes\n``.text {color:#3b3617;}``\n``.background {background-color:#3b3617;}``\n``.border {border:1px solid #3b3617;}``\n\n# Shades and Tints of #3b3617\n\nA shade is achieved by adding black to any pure hue, while a tint is created by mixing white to any pure color. In this example, #030201 is the darkest color, while #fafaf3 is the lightest one.\n\n• #030201\n``#030201` `rgb(3,2,1)``\n• #110f06\n``#110f06` `rgb(17,15,6)``\n• #1f1c0c\n``#1f1c0c` `rgb(31,28,12)``\n• #2d2911\n``#2d2911` `rgb(45,41,17)``\n• #3b3617\n``#3b3617` `rgb(59,54,23)``\n• #49431d\n``#49431d` `rgb(73,67,29)``\n• #575022\n``#575022` `rgb(87,80,34)``\n• #655d28\n``#655d28` `rgb(101,93,40)``\n• #736a2d\n``#736a2d` `rgb(115,106,45)``\n• #827733\n``#827733` `rgb(130,119,51)``\n• #908438\n``#908438` `rgb(144,132,56)``\n• #9e903e\n``#9e903e` `rgb(158,144,62)``\n• #ac9d43\n``#ac9d43` `rgb(172,157,67)``\nShade Color Variation\n• #b8a94a\n``#b8a94a` `rgb(184,169,74)``\n• #beb058\n``#beb058` `rgb(190,176,88)``\n• #c3b766\n``#c3b766` `rgb(195,183,102)``\n• #c9bd74\n``#c9bd74` `rgb(201,189,116)``\n• #cec483\n``#cec483` `rgb(206,196,131)``\n• #d4cb91\n``#d4cb91` `rgb(212,203,145)``\n• #d9d19f\n``#d9d19f` `rgb(217,209,159)``\n• #dfd8ad\n``#dfd8ad` `rgb(223,216,173)``\n• #e4dfbb\n``#e4dfbb` `rgb(228,223,187)``\n• #eae5c9\n``#eae5c9` `rgb(234,229,201)``\n• #efecd7\n``#efecd7` `rgb(239,236,215)``\n• #f5f3e5\n``#f5f3e5` `rgb(245,243,229)``\n• #fafaf3\n``#fafaf3` `rgb(250,250,243)``\nTint Color Variation\n\n# Tones of #3b3617\n\nA tone is produced by adding gray to any pure hue. In this case, #2b2b27 is the less saturated color, while #514601 is the most saturated one.\n\n• #2b2b27\n``#2b2b27` `rgb(43,43,39)``\n• #2e2d24\n``#2e2d24` `rgb(46,45,36)``\n• #322f20\n``#322f20` `rgb(50,47,32)``\n• #35311d\n``#35311d` `rgb(53,49,29)``\n• #38341a\n``#38341a` `rgb(56,52,26)``\n• #3b3617\n``#3b3617` `rgb(59,54,23)``\n• #3e3814\n``#3e3814` `rgb(62,56,20)``\n• #413b11\n``#413b11` `rgb(65,59,17)``\n• #443d0e\n``#443d0e` `rgb(68,61,14)``\n• #483f0a\n``#483f0a` `rgb(72,63,10)``\n• #4b4107\n``#4b4107` `rgb(75,65,7)``\n• #4e4404\n``#4e4404` `rgb(78,68,4)``\n• #514601\n``#514601` `rgb(81,70,1)``\nTone Color Variation\n\n# Color Blindness Simulator\n\nBelow, you can see how #3b3617 is perceived by people affected by a color vision deficiency. This can be useful if you need to ensure your color combinations are accessible to color-blind users.\n\nMonochromacy\n• Achromatopsia 0.005% of the population\n• Atypical Achromatopsia 0.001% of the population\nDichromacy\n• Protanopia 1% of men\n• Deuteranopia 1% of men\n• Tritanopia 0.001% of the population\nTrichromacy\n• Protanomaly 1% of men, 0.01% of women\n• Deuteranomaly 6% of men, 0.4% of women\n• Tritanomaly 0.01% of the population" ]
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https://wiki.naturalphilosophy.org/index.php?title=Beyond_Einstein_and_E%3Dmc2
[ "# Beyond Einstein and E=mc2\n\nAuthor Error creating thumbnail: File missing Ajay Sharma 2015 Cambridge International Science Publishing Ltd. Cambridge ENGLAND 546 978-1907343315\n\n'           'Beyond Einstein and E=mc2'\n\nPublisher, Cambridge International Science Publisher, Cambridge, England)\n'\nBurn the candle of ‘doubt’ to get scientific light.'\n'\nShould scientists be regarded  above almighty GOD ?\n\n(i) Einstein’s 1905 paper of Theory of Relativity was published in Annalen der Physik  without  any peer review by experts. So whatever Einstein wrote was published. Einstein took this opportunity to publish work of Galileo (1632), Poincare (1898), Lorentz (1892 ) , time dilation Larmer (1897   ) ,length contraction  Fitzegerald (1889 )  etc. AS HIS OWN.  Einstein scored goals without goalkeeper in playground. So the theory of relativity is not Einstein’s. In scientific language it is called plagiarism and in general sense THEFT in broad day daylight. Einstein called work of Galileo and Poincare as postulates or hypothesis ….. but these are accepted realities in the literature when Einstein published them.\n\n(ii) Einstein’s derivation which leads to E=mc2 , also implies that WHEN A CANDLE BURNS ITS MASS MUST INCREASE. It is the biggest contradiction in science. Thus equation is derived in alternate way as dE=Ac2dm . Thus generalized equation is general equation and E=mc2 is its special case. A can be less, more or equal to unity.\n(iii)  In 1907 Einstein had also derived rest mass energy E(rme)=Mc2 . It is derived under condition when FIRST equation is zero, and last equation is E(rme)=Mc2. Thus we get OUTPUT without INPUT. It can be understood in analogous way as ……ground floor of the 10 storeyed building is demolished. Then according to Einstein’s logic, the remaining 9  storeyed building will FLOAT  in air. Thus Einstein’s deduction is BASELESS.\n(vi)  When velocity of body or particle becomes comparable to that of light, then its mass increases. Then its heavier mass (or actual mass) must be taken in account. However in nuclear\nchain reaction the velocity of neutrons is in relativistic region, so its mass must increase. But mass is taken as original mass. It is not justifies. Also E =mc2 cannot explain simultaneously the MASS DEFECT and BINDING ENERGY of deuteron.  The generalized equation dE=Ac2dm can  explain." ]
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https://primes.utm.edu/curios/page.php/7006693.html
[ "# 7006693\n\nThis number is a prime.", null, "The smallest emirp that is the sum of the 7 consecutive seven-digit primes (1000919+1000921+1000931+1000969+1000973+1000981+1000999=7006693). Note that its sum of digits is also emirp. [Bajpai]" ]
[ null, "https://primes.utm.edu/gifs/check.gif", null ]
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http://www.scholarpedia.org/article/Fuzzy_sets
[ "# Fuzzy sets\n\nPost-publication activity\n\nCurator: Milan Mares", null, "Figure 1: Bird's-eye view on a forest: Where is the boundary of the forest? Which location is in the forest and which is out of it? (See explanation in the text.)\n\nFuzzy set is a mathematical model of vague qualitative or quantitative data, frequently generated by means of the natural language. The model is based on the generalization of the classical concepts of set and its characteristic function.\n\n## History\n\nThe concept of a fuzzy set was published in 1965 by Lotfi A. Zadeh (see also Zadeh 1965). Since that seminal publication, the fuzzy set theory is widely studied and extended. Its application to the control theory became successful and revolutionary especially in seventies and eighties, the applications to data analysis, artificial intelligence, and computational intelligence are intensively developed, especially, since nineties. The theory is also extended and generalized by means of the theories of triangular norms and conorms, and aggregation operators.\n\n## Motivation\n\nThe expansion of the field of mathematical models of real phenomena was influenced by the vagueness of the colloquial language. The attempts to use the computing technology for processing such models have pointed at the fact that the traditional probabilistic processing of uncertainty is not adequate to the properties of vagueness. Meanwhile the probability, roughly speaking, predicts the development of well defined factor (e.g., which side of a coin appears, which harvest we can expect, etc.), the fuzziness analyzes the uncertain classification of already existing and known factors, e.g., is a color \"rather violet\" or \"almost blue\"? \"Is the patient's temperature a bit higher, or is it a fever?\", etc. The models of that type proved to be essential for the solution of problems regarding technical (control), economic (analysis of markets), behavioral (cooperative strategy) and other descriptions of activities influenced by vague human communication.\n\n## Mathematical formalism\n\nThe traditional deterministic set in a universum $$\\mathcal U$$ can be represented by the characteristic function $$\\varphi_A$$ mapping $$\\mathcal U$$ into two-element set $$\\{0,1\\}\\ ,$$ namely for $$x\\in{\\mathcal U}$$ $\\varphi_A(x)=0$ if $$x\\notin A\\ ,$$ and $\\varphi_A(x)=1$ if $$x\\in A\\ .$$\n\nA fuzzy subset $$A$$ of $$\\mathcal U$$ is defined by a membership function $$\\mu_A$$ mapping $$\\mathcal U$$ into a closed unit interval $$[0, 1]\\ ,$$ where for $$x\\in\\mathcal U$$ $\\mu_A(x)=0$ if $$x\\notin A\\ ,$$ $\\mu_A(x)=1$ if $$x\\in A\\ ,$$ and $\\mu_A(x)\\in(0,1)$ if $$x$$ possibly belongs to $$A$$ but it is not sure.\n\nFor the last case - the nearer to 1 the value $$\\mu_A(x)$$ is, the higher is the possibility that $$x\\in A\\ .$$\n\n### Example\n\nLet us consider the bird's-eye view of a forest in Figure 1.\n\n• Is location A in the forest? Certainly yes, $$\\mu_{\\rm forest}(A) = 1\\ .$$\n• Is location B in the forest? Certainly not, $$\\mu_{\\rm forest}(B) = 0\\ .$$\n• Is location C in the forest? Maybe yes, maybe not. It depends on a subjective (vague) opinion about the sense of the word \"forest\". Let us put $$\\mu_{\\rm forest}(C) = 0.6\\ .$$\n\n### Operations with fuzzy sets\n\nThe processing of fuzzy sets generalizes the processing of the deterministic sets. Namely, if $$A, B$$ are fuzzy sets with membership functions $$\\mu_A, \\mu_B\\ ,$$ respectively, then also the complement $$\\overline{A}\\ ,$$ union $$A\\cup B$$ and intersection $$A\\cap B$$ are fuzzy sets, and their membership functions are defined for $$x\\in{\\mathcal U}$$ by $\\mu_{\\overline{A}}(x)=1-\\mu_A(x)\\ ,$ $\\mu_{A\\cup B}(x)=\\max\\left(\\mu_A(x),\\mu_B(x)\\right)\\ ,$ $\\mu_{A\\cap B}(x)=\\min\\left(\\mu_A(x),\\mu_B(x)\\right)\\ .$ Moreover, the concept of inclusion of fuzzy sets, $$A\\subset B\\ ,$$ is defined by $\\mu_A(x)\\leq\\mu_B(x)$ for all $$x\\in{\\mathcal U}\\ ,$$ and the empty and universal fuzzy sets, $$\\emptyset$$ and $$\\mathcal U\\ ,$$ are defined by membership function $\\mu_\\emptyset(x)=0$ and $$\\mu_{ {\\mathcal U} }(x)=1$$ for all $$x\\in{\\mathcal U}\\ .$$ Even if all above operations and concepts consequently generalize their counterparts in the deterministic set theory, the resulting properties of fuzziness need not be identical with those of the deterministic theory, e.g., for some fuzzy set $$A\\ ,$$ the relation $$A\\cap\\overline{A}\\neq\\emptyset\\ ,$$ or even $$A\\subset\\overline{A}\\ ,$$ may be fulfilled.\n\n## Derived concepts\n\nThe basic definition of a fuzzy set can be easily extended to numerous set-based concepts. For example, a relation $$R$$ over the universe $$\\mathcal U$$ can be defined by a subset of $${\\mathcal U}\\times{\\mathcal U}\\ ,$$ $$\\{(x,y):y\\in{\\mathcal U},\\,y\\in{\\mathcal U},\\,x\\,R\\,y\\}\\ ,$$ a function $$f$$ over $$\\mathcal U$$ can be identified with its graph $$\\{(x,r):x\\in{\\mathcal U},\\,r\\in{\\mathbb R},\\,r=f(x)\\}\\subset {\\mathcal U}\\times{\\mathbb R}$$ (where $$\\mathbb R$$ is the set of real numbers). Then their fuzzy counterparts are defined as respective fuzzy set defined over $${\\mathcal U}\\times{\\mathcal U}$$ and $${\\mathcal U}\\times R\\ ,$$ respectively.\n\n## Related Theories\n\nAs the concept of sets is present at the background of many fields of mathematical and related models, it is applied, e.g., to mathematical logic (where each fuzzy statement is represented by a fuzzy subset of the objects of the relevant theory), or to the computational methods with vague input data (where each fuzzy quantity or fuzzy number is represented by a fuzzy subset of $$\\mathbb R$$).\n\nNamely, any fuzzy subset $$\\mathbf a$$ of $$\\mathbb R$$ is called fuzzy quantity iff there exist $$x_1<x_0<x_2\\in\\mathbb R$$ such that $$\\mu_{ {\\mathbf a}}(x_0)=1\\ ,$$ $$\\mu_{{\\mathbf a} }(x)=0$$ for $$x\\notin[x_1,x_2]\\ .$$\n\n• If $$\\mu_{ {\\mathbf a} }$$ is triangular then $$\\mathbf a$$ is called fuzzy number.\n• If it is trapezoidal then $$\\mathbf a$$ is a fuzzy interval.\n\nBinary algebraic operation $$x\\star y$$ is extended to fuzzy quantities by so called extension principle, i.e., $${\\mathbf a}\\star{\\mathbf b}\\ ,$$ where $$x\\in \\mathbb R\\ .$$ $\\mu_{ {\\mathbf a}\\star{\\mathbf b}}(x)=\\sup[\\min(\\mu_{ {\\mathbf a} }(y),\\mu_{{\\mathbf b} }(z): y,z\\in{\\mathbb R},x=y\\star z]\\ .$\n\nThe algebraic properties of extended operations are weaker than those of their patterns over real numbers, where the differences are mostly caused by the vagueness of fuzzy zero (or fuzzy one) and equality relation (see also Mares 1994).\n\n## Applications\n\nThe fuzzy set theory and related branches are widely applied in the models of optimal control, decision-making under uncertainty, processing vague econometric or demographic data, behavioral studies, and methods of artificial intelligence. For example, there already exists a functional model of a helicopter controlled from the ground by simple \"fuzzy\" commands in natural language, like \"up\", \"slowly down\" \"turn moderately left\", \"high speed\", etc. \"Fuzzy\" wash-machines, cameras or shavers are common commercial products. Fuzzy sets also can be applied in sociology, political science, and anthropology, as well as in any field of inquiry dealing with complex patterns of causation (Ragin 2000)." ]
[ null, "http://www.scholarpedia.org/w/images/thumb/e/ed/Fuzzy_Forest.gif/300px-Fuzzy_Forest.gif", null ]
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https://ask.cvxr.com/t/how-to-encode-a-summation-constraint-into-cvx/10357/2
[ "# How to encode a summation constraint into CVX\n\nI have to solve the following linear program in CVX. I choose d=2.\n\nI have written the following LP as a start but it has two issues\n\nn = 1000;\neps = 0.001;\ncvx_begin\nvariable y(n)\nvariable r(n)\nvariable p(n)\nvariable s\n\nminimize(s)\nsubject to\ny >= 0;\ny - r + p >= 0;\nr >= 0;\nfor i=1:n\nr(i) <= s;\nend\nones(1,n)*r == 1;\nones(1,n)*y <= eps;\ncvx_end\n\n1. I should be minimizing sqrt(d^n * s) but since s is nonnegative (from the constraints), I just minimized s directly. Does this make sense?\n\n2. I don’t know how to encode summation constraints. I need to replace the lines\n\nones(1,n)*r == 1;\nones(1,n)*y <= eps;\n\nwith the correct constraint which is the one involving some combinatorial prefactors and then a sum over r(k) and y(k). How should one encode such a sum constraint? This is my second attempt below but gives an error “Unrecognized field name “sol”.”\n\nn = 1000;\nd = 2;\neps = 1e-5;\n\nfor i = 1:n\nc(i) = nchoosek(n, (i-1))*(1/d)^(i-1)*(d - 1/d)^(n-i+1);\nend\n\ncvx_begin\nvariable y(n)\nvariable r(n)\nvariable p(n)\nvariable s\n\nminimize(s)\nsubject to\ny >= 0;\ny - r + p >= 0;\nr >= 0;\nfor i=1:n\nr(i) <= s;\nend\nc*r == 1;\nc*y <= eps;\ncvx_end\n\nFor n=1000 the computation of your c coefficients is so inaccurate that it produces some humonguous values. Are you not getting a ton of warnings related to calling nchoosek ? You will need to compute them in some more clever way that does not lead to overflows.\n\nThat’s why for n=1000 Mosek says\n\nMosek error: MSK_RES_ERR_HUGE_AIJ (A numerically huge value is specified for an element in A.)\n------------------------------------------------------------\nStatus: Error\nOptimal value (cvx_optval): NaN\n\nReference to non-existent field 'sol'.\n\n\nFor n=10 it solves nicely.\n\n1 Like\n\nAh thanks! Somehow the nchoosek warnings were being suppressed but now I see the issue is not CVX\n\nHi Michal,\n\nWould you have any suggestions on how to cleverly compute the coefficients to avoid overflows in such a case? I have a different (simpler) linear program where I run into the same issue which I include here\n\nclear all\ncvx_solver mosek\n\nN = 50;\neps = 0.01;\ndelta = 0.2;\n\nfor n=1:N\n\nfor i = 1:n+1\nw(i, 1) = delta^(i-1)*(1-delta)^(n-i+1);\nnck(1,i) = nchoosek(n, i-1);\nend\n\ncvx_begin\nvariable til_w(n+1)\nvariable p(n+1)\nvariable zeta\n\nminimize(zeta)\nsubject to\np >= 0;\nnck*p <= eps;\np - til_w + w >= 0;\nnck*til_w ==1;\ntil_w >= 0;\ntil_w <= zeta*ones(n+1, 1);\ncvx_end\n\nzeta_opt(n) = zeta;\nn_copies(n) = n;\nobj(n) = 1 + 1/n*log(zeta)/log(2);\nend\n\n\nI get warnings about nchoosek again but it’s not clear what is the best way to avoid this issue. Thank you.\n\nYour constraint nck*til_w ==1; will have coefficient span between 1 and 2^n (roughly asymptotically) while looking at the rest of the problem it seems like you are expecting the variable til_w in the solution to have values of order similar to w, that is to say 1/2^n when \\delta=1/2. There is no way to make this floating-point meaningful for n=50.\n\nI see. Somehow, the authors of https://arxiv.org/pdf/1807.05354.pdf manage to solve a similar LP by symmetrizing the SDP in my original post for n=10,000 (see Fig. 2).\n\nOf course, this is not necessarily a CVX question anymore but curious how they managed it since it appears it can be done somehow. Thanks anyway for your comments!\n\nI agree both that the question is interesting and not related to CVX :). Maybe asking the authors can help.\n\n1 Like" ]
[ null ]
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http://wusun.name/blog/2012-10-04-latex-floats-numbering/
[ "# Adding section numbers to LaTeX floats numbering and other tips\n\nI have been learning to use LaTeX for some time. Now I do most of my homework assignments in LaTeX. It wears quite well on me. I have encountered some issues, but most of the time I was able to find elegant solutions on TeX StackExchange. Here are a few tips I learned recently.\n\n## 1. Show chapter or section numbers in equation/figure/table numbering\n\nBy default, LaTeX assigns equation numbers continually across different sections. If you need the equation to be numbered like “Eq. (3.5)” for the 5th equation in section 3, add this to the preamble:\n\n\\usepackage{amsmath}\n\\numberwithin{equation}{section}\n\n\nTo include also the subsection number, change the second line to\n\n\\numberwithin{equation}{subsection}\n\n\nFor figures and tables, it is similar.\n\n\\usepackage{amsmath}\n\\numberwithin{table}{section}\n\\numberwithin{figure}{section}\n\n\n## 2. Scientific notation\n\nThe most elegant solution for scientific notation of numbers is to use the siunitx package.\n\n\\usepackage{siunitx}\n...\n\\num{6.022e23}\n\n\n\\num{6.022e23} will be rendered as “6.022 × 1023”.\n\nAn alternative solution that does not depend on siunitx is:\n\n\\newcommand{\\e}{\\ensuremath{\\times 10^{#1}}}\n\n\nThis new command can be used like 6.022\\e{23} to produce “6.022 × 1023”.\n\n## 3. Upright differential operator\n\nThe differential operator d in dy / dx should be typeset in upright not italic shape, because it is not a variable (Beccari, 1997, TUGboat). The upright differential operator is not provided by the amsmath package, and to do it properly requires much low-level TeX programming due to spacing requirements. An out-of-the-box solution is to use the commath package, which provides the following commands:\n\n• \\dif: This produces an upright d.\n• \\Dif: This produces an upright D (e.g., for Lagrangian derivative).\n• \\od: This takes two arguments for the function and the variable, respectively, and an optional argument for the order, e.g., \\od{f}{x} produces $\\dfrac{\\mathrm{d}^2 f}{\\mathrm{d} x^2}$.\n• \\pd: This works similarly to \\od but produces partial derivatives.\n\nThere are also many other useful commands in this package.\n\nAlternatively, a minimalist and nearly as good solution without using commath can be\n\n\\newcommand{\\dif}{\\mathrm{d}}\n\\newcommand{\\Dif}{\\mathrm{D}}\n\\newcommand{\\od}[]{\\ensuremath{\\dfrac{\\dif^{#1}#2}{\\dif #3^{#1}}}}\n\\newcommand{\\pd}[]{\\ensuremath{\\dfrac{\\partial^{#1}#2}{\\partial #3^{#1}}}}\n\n1. Beccari, C. (1997). Typesetting mathematics for science and technology according to ISO 31/XI. TUGboat, 18(1), 39–48. [link]" ]
[ null ]
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https://math.stackexchange.com/questions/3197636/rigid-motions-taking-a-regular-n-gon-back-to-itself-carry-vertices-to-vertices
[ "Rigid motions taking a regular $n$-gon back to itself carry vertices to vertices\n\nI have been reading Keith Conrad's expository paper Dihedral groups I and I have two questions about Theorem $$2.2$$, which deals with the size of $$D_n$$. In the first part of the proof you can read\n\nAn element $$g$$ of $$D_n$$ is a rigid motion taking the $$n$$-gon back to itself, and it must carry vertices to vertices (how are vertices unlike other points in terms of their distance relationships with all points on the polygon?) and $$g$$ must preserve adjacency of vertices.\n\nI think I understand why $$g$$ must preserve adjacency of vertices: if $$A$$ and $$B$$ are vertices, then $$g(A)$$ and $$g(B)$$ are vertices, and the distance of $$g(A)$$ from $$g(B)$$ equals the distance of $$A$$ from $$B$$. Therefore, $$g(A)$$ and $$g(B)$$ are adjacent. Is this reasoning correct?\n\nI think (but I'm not sure) that proving that $$g$$ preserves adjacency of vertices requires the fact that $$g$$ carries vertices to vertices. Why is that true? In particular, what is the answer to the author's question? (How are vertices unlike other points in terms of their distance relationships with all points on the polygon?) Does this question bear any relation to Lemma 2.1 in Conrad's notes?\n\nEDIT: I'm still confused. I don't completely understand @zipirovich's answer: how can I rigorously show that the maximum $$d(P)$$ exists and that the value of $$d(P)$$ is largest when $$P$$ is a vertex, and smaller for any other point in the polygon?\n\nMaybe my comment is a possible answer, but I think I'm using the fact that each rigid motion in $$D_n$$ extends uniquely to an isometry of $$\\mathbb{R}^2$$, and I don't know if I'm answering Conrad's question \"How are vertices unlike other points in terms of their distance relationships with all points on the polygon?\".\n\n• zipirovich’ answer shows that $g$ carries vertices to vertices. Your reasoning why $g$ preserves adjacency of vertices is correct. An application of Lemma 2.1 is not needed. May 19 '19 at 18:48\n\nI think that maybe he hints at the following argument. For any point $$P$$ in such a regular polygon $$G$$ define $$d(P)=\\max\\limits_{Q\\in G}\\{\\operatorname{dist}(P,Q)\\}$$, the maximal possible distance between the given point and all other points in the polygon. The value of $$d(P)$$ is largest when $$P$$ is a vertex, and smaller for any other point in the polygon. And since rigid motions preserve distances, the value of $$d(P)$$ would be preserved for any point. Thus vertices have to be mapped to vertices, where the value is again largest possible.\n• I'm not sure how can I prove that $d(P)$ is largest when $P$ is a vertex. Maybe another argument can work, too. A rigid motion in $D_n$ takes the polygon back to itself, so the circumscribed circle and its center remain the same. The vertices are the only points of the polygon whose distance from the center is equal to the radius of the circumscribed circle. Threfore, an element of $D_n$ must carry vertices to vertices. Is that correct? Jul 17 '19 at 15:41\nMy try: A boundary point of a convex $$n$$-gon $$K$$ has the special property that there exist sequences $$x_i \\in K$$ and $$y_i \\in \\mathbb{R}^2\\setminus K$$ that both converge to that point.\nA vertex has the special property that there exists a straight line passing through the point, such that there are sequences on both rays, which converge to the vertex. This is a property that makes the vertices unique among the points in $$K$$." ]
[ null ]
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https://www.cbsetips.in/2021/02/cbse-class-11-chemistry-mcq-and-online_37.html
[ "# CBSEtips.in\n\n## Sunday 21 February 2021\n\n### CBSE Class 11 Chemistry - MCQ and Online Tests - Unit 6 - Thermodynamics\n\n#### CBSE Class 11 Chemistry – MCQ and Online Tests – Unit 6 – Thermodynamics\n\nEvery year CBSE schools conducts Annual Assessment exams for 6,7,8,9,11th standards. These exams are very competitive to all the students. So our website provides online tests for all the 6,7,8,9,11th standard’s subjects. These tests are also very effective and useful for those who preparing for any competitive exams like Olympiad etc. It can boost their preparation level and confidence level by attempting these chapter wise online tests.\n\nThese online tests are based on latest CBSE syllabus. While attempting these our students can identify the weak lessons and continuously practice those lessons for attaining high marks. It also helps to revise the NCERT textbooks thoroughly.\n\n#### CBSE Class 11 Chemistry – MCQ and Online Tests – Unit 6 – Thermodynamics\n\nQuestion 1.\nThe enthalpies of combustion of carbon and carbon monoxide are -393.5 and -283.0 kJ mol-1 respectively. The enthalpy of formation of carbon monoxide is:\n(a) -676 kJ\n(b) 110.5 kJ\n(c) -110.5 kJ\n(d) 676.5 kJ\n\nExplanation:\nC(s) + O2 à CO2 ?H1 = -393.5\nCO + ($$\\frac {1}{2}$$) O2 à CO2 ?H2 = -283.0\nC(s) + ($$\\frac {1}{2}$$) O2 à CO ?H = ?H1 – ?H2\n= -393.5 + 283 = -110.5 KJ\n\nQuestion 2.\nThe amount of the heat released when 20 ml 0.5 M NaOH is mixed with 100 ml 0.1 M HCl is x kJ. The heat of neutralization is\n(a) -100 × kJ/mol\n(b) -50 × kJ/mol\n(c) 100 × KJ/mol\n(d) 50 × kJ/mol\n\nExplanation:\nNormality of NaOH = Molarity × acidity\n= 0.5 × 1 = 0.5 N\nTotal heat q produced = x kJ\nHeat of neutralisation\n= [(q)/ (Volume of acid or base)] ×1000× (1/normality of acid or base)\n= ($$\\frac {x}{20}$$) × 1000 × ($$\\frac {1}{0.5}$$)\n= 100 x kJmol-1\nSince heat is liberated, heat of neutralisation = -100 x kJmol-1\n\nQuestion 3.\nThe enthalpy of vaporisation of a substance is 8400 J mol-1 and its boiling point is –173°C. The entropy change for vaporisation is :\n(a) 84 J mol-1K-1\n(b) 21 J mol-1K-1\n(c) 49 J mol-1K-1\n(d) 12 J mol-1K-1\n\nExplanation:\n?S = (qrev)/ (T)\n= ($$\\frac {8400}{100}$$)\n= 84 J mol-1K-1\n\nQuestion 4.\nThe species which by definition has ZERO standard molar enthalpy of formation at 298 K is\n(a) Br2(g)\n(b) Cl2(g)\n(c) H2O(g)\n(d) CH4(g)\n\nExplanation:\nThis is possible only for elements, chlorine is a gas at this temperature, but bromine is a liquid, so it is possible only for chlorine.\n\nQuestion 5.\nIn a reversible process the system absorbs 600 kJ heat and performs 250 kJ work on the surroundings. What is the increase in the internal energy of the system?\n(a) 850 kJ\n(b) 600 kJ\n(c) 350 kJ\n(d) 250 kJ\n\nExplanation:\n?E = q + w\n= (600 – 250)\n?E = 350 J\n\nQuestion 6.\nWhich of the following is true for the reaction? H2O (l) ? H2O (g) at 100° C and 1 atm pressure\n(a) ?S = 0\n(b) ?H = T ?S\n(c) ?H = ?U\n(d) ?H = 0\n\nExplanation:\nEquilibrium\nTherefore, ? G = 0 = ? H – T ? S\nOr T? S = ?H\n\nQuestion 7.\nCalculate the heat required to make 6.4 Kg CaC2 from CaO(s) and C(s) from the reaction: CaO(s) + 3 C(s) ? CaC2(s) + CO (g) given that ?f Ho (CaC2) = -14.2 kcal. ?f H° (CO) = -26.4 kcal.\n(a) 5624 kca\n(b) 1.11 × 104 kcal\n(c) 86.24 × 10³\n(d) 1100 kcal\n\nAnswer: (b) 1.11 × 104 kcal\nExplanation:\nn = (Mass)/ (Molecular weight)\n= (6.4 × 10³)/ (64)\n= 100\nFor 1 mole of CaC2\n? H = ?Hf (CaC) + Hf (CO) – Hf (CaO)\n= -14.2 – 26.4 + 151.6 = 111.1 kcal\nFor 100 moles, ?H = 1.11 × 104 Kcal\n\nQuestion 8.\nIn a system where ?E = -51.0 kJ, a piston expanded against a pext of 1.2 atm giving a change in volume of 32.0 L. What was the change in heat of this system?\n(a) -36 kJ\n(b) -13 kJ\n(c) -47 kJ\n(d) 24 kJ\n\nExplanation:\nw = -1.2 (32) × 101.3\n= – 3.89 KJ\n= -4 (approx.)\n= ? E = – 51.0 KJ\nTherefore, E = q + w\n– 51 = q – 4\nTherefore, q = – 47 KJ\n\nQuestion 9.\nA system absorb 10 kJ of heat at constant volume and its temperature rises from 270 C to 370 C. The value of ? U is\n(a) 100 kJ\n(b) 10 kJ\n(c) 0 kJ\n(d) 1 kJ\n\nExplanation:\nAt constant volume w = 0\nTherefore, ? U = q = 10 kJ\n\nQuestion 10.\nThe bond energy (in kcal mol-1) of a C-C single bond is approximately\n(a) 1\n(b) 10\n(c) 83-85\n(d) 1000\n\nExplanation:\nC–C bond 83–85 kcal/mol\n\nIt is the energy required to break the bond .It is defined as the standard enthalpy change when a bond is cleaved by homolysis, with reactants and products of the homolysis reaction at 0 K (absolute zero)\n\nQuestion 11.\nThird law of thermodynamics provides a method to evaluate which property?\n(a) Absolute Energy\n(b) Absolute Enthalpy\n(c) Absolute Entropy\n(d) Absolute Free Energy\n\nExplanation:\nThe Third Law of Thermodynamics is concerned with the limiting behavior of systems as the temperature approaches absolute zero. Most thermodynamics calculations use only entropy differences, so the zero point of the entropy scale is often not important. However, the Third Law tells us about the completeness as it describes the condition of zero entropy.\n\nQuestion 12.\nOne mole of which of the following has the highest entropy?\n(a) Liquid Nitrogen\n(b) Hydrogen Gas\n(c) Mercury\n(d) Diamond\n\nExplanation:\nThe measure of randomness of a substance is called entropy. Greater the randomness of molecules of a substance greater is the entropy. Here hydrogen gas has more entropy as it shows more randomness/disorderliness due to less molar mass than all the given substances and also in the gas phase.\n\nQuestion 13.\nWhich thermodynamic function accounts automatically for enthalpy and entropy both?\n(a) Helmholtz Free Energy (A)\n(b) Internal Energy (E)\n(c) Work Function\n(d) Gibbs Free Energy\n\nExplanation:\nGibbs free energy combines the effect of both enthalpy and entropy. The change in free energy (?G) is equal to the sum of the change of enthalpy (?H) minus the product of the temperature and the change of entropy (?S) of the system.\n?G = ?H – T?S\n?G predicts the direction in which a chemical reaction will go under two conditions: (1) constant temperature and (2) constant pressure.\nIf ?G is positive, then the reaction is not spontaneous (it requires the input of external energy to occur) and if it is negative, then it is spontaneous (occurs without the input of any external energy).\n\nQuestion 14.\nWhich of the following salts will have maximum cooling effect when 0.5 mole of the salt is dissolved in same amount of water. Integral heat of solution at 298 K is given for each salt?\n(a) KNO3 (?H = 35.4 kJ mol-1)\n(b) NaCl (?H = 5.35 kJ mol-1)\n(c) HBr (?H = -83.3 kJ mol-1)\n(d) KOH ( ?H = -55.6 kJ mol-1)\n\nAnswer: (a) KNO3 (?H = 35.4 kJ mol-1)\nExplanation:\nMore the heat absorbed, more will be the cooling effect. Hence, more the positive value of ? H, more the cooling effect.\n\nQuestion 15.\nStandard enthalpy of vapourisation ?Hvap for water at 100oC is 40.66 kJmol-1. The internal energy of vapourisation of water at 100°C (in kJmol-1) is (Assume water vapour to behave like an ideal gas)\n(a) 43.76\n(b) 40.66\n(c) 37.56\n(d) -43.76\n\nExplanation:\nFor gaseous reactants and products, we have a relation between standard enthalpy of vaporization (?Hvap) and standard internal energy (?E) as-\n?Hvap = ?E+ ?ng? RT whereas,\n?ng = n2? – n1, i.e., difference between no. of moles of reactant and product.\nFor vaporization of water,\nH2O (l) ? H2O(g)\n?Therefore, ?ng = 1 – 0 = 1\nTherefore, ?Hvap = ?E+ ?ng RT\n? ?E = ?Hvap – ?ng\n?RT = 40.63 – (1×8.314×10-3 × 373) = 37.53 KJ/mol\nHence the value ?E for this process will be 37.53KJ/mol.\n\nQuestion 16.\nBased on the first law of thermodynamics, which one of the following is correct?\n(a) For an isothermal process, q = +w\n(b) For an isochoric process, ?U = -q\n(c) For an adiabatic process, ?U = -w\n(d) For a cyclic process, q = -w\n\nAnswer: (d) For a cyclic process, q = -w\nExplanation:\n(1) ?U = q + w. For an isochoric process, w = -P?V = 0. Hence, ?U = qv\n(2) For an adiabatic process, q = 0. Hence, ?U = w\n(3 ) For an isothermal process, ?U = 0 Hence, q = -w\n(4) For a cyclic process , ?U = 0. Hence, q = -w\n\nQuestion 17.\nA system absorb 10 kJ of heat at constant volume and its temperature rises from 270°C to 370°C. The value of ? U is\n(a) 100 kJ\n(b) 10 kJ\n(c) 0 kJ\n(d) 1 kJ\n\nExplanation:\nAt constant volume w = 0\nTherefore, ? U = q = 10 kJ\n\nQuestion 18.\nThe temperature of the system decreases in an ______.\n(b) Isothermal Expansion\n(c) Isothermal Compression\n\nExplanation:\nIn adiabatic process heat is neither added nor removed from system. So the work done by the system (expansion) in adiabatic process will result in decrease of internal energy of that system (from first law).\nAs internal energy is directly proportional to the change in temperature there will be temperature drop in an adiabatic process.\n\nQuestion 19.\nAn ideal gas is taken around the cycle ABCA as shown in P-V diagram The next work done by the gas during the cycle is equal to:", null, "(a) 12P1V1\n(b) 6P1V1\n(c) 5P1V1\n(d) P1V1\n\nExplanation:\nWork done = Area under P-V graph = ($$\\frac {1}{2}$$) (5P1) (2V1) = 5P1 V1\n\nQuestion 20.\nIn which of the following process, a maximum increase in entropy is observed?\n(a) Dissolution of Salt in Water\n(b) Condensation of Water\n(c) Sublimation of Naphthalene\n(d) Melting of Ice\n\nExplanation:\nThe order of entropy in solid, liquid and gas is gas > liquid > solid .Hence, in sublimation of naphthalene, maximum increase in entropy is observed.\n\nShare:" ]
[ null, "https://www.learninsta.com/wp-content/uploads/2020/11/MCQ-Questions-for-Class-11-Chemistry-Chapter-6-Thermodynamics-with-Answers-1.jpg", null ]
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https://physics.stackexchange.com/questions/133906/are-different-interpretations-of-quantum-mechanics-empirically-distinguishable
[ "# Are different interpretations of quantum mechanics empirically distinguishable?\n\nAre the different interpretations of Quantum mechanics just different viewpoints of the same physical reality? Or can experiments distinguish them? Are they empirically distinguishable or not?\n\nI have read a paper in which Asher Peres states that quantum mechanics needs no interpretation and we can understand it by a minimum number of necessary postulates. Here is the last paragraph of the paper:\n\nAll this said, we would be the last to claim that the foundations of quantum theory are not worth further scrutiny. For instance, it is interesting to search for minimal sets of physical assumptions that give rise to the theory. Also, it is not yet understood how to combine quantum mechanics with gravitation, and there may well be important insight to be gleaned there. However, to make quantum mechanics a useful guide to the phenomena around us, we need nothing more than the fully consistent theory we already have. Quantum theory needs no interpretation.\n\nThis is the link to the paper (it is a paper with only two pages) Peres\n\nCan you explain what he means when he says \"quantum mechanics needs no interpretation\"? i didn't get it from the paper!. Does he mean that we shouldn't try to assign any objective meaning to the wave function and consider it as reflection of our knowledge about the system? If yes, isn't it what Copenhagen interpretation says?!! (This is from wiki page of Copenhagen interpretation:\"The wave function reflects our knowledge of the system\")\n\nAnd finally, has anyone found that minimum number of postulates?\n\nNo, interpretations of quantum mechanics are not distiguishable in a physical experiment, otherwise they would be called theories rather than interpretations.\n\nIt should be noted that there are some theories whom their authors call \"interpretations\" but they in fact are not. For instance the \"objective collapse theories\" often (wrongly) called \"interpretations\". These theories can be physically proven or disproven and predict different observations than the standard quantum mechanics (with all its interpretations).\n\nThat said, it is not that interpretations cannot be experimentally distinguished at all. Maybe they can be, but the experiment that would be able to distinguish between them would not be a physical (or scientific) experiment in the sense it would not satisfy the requirements for scientific method.\n\nAll scientific experiments regarding quantum mechanics should produce the same results as far as different interpretations concerned.\n\nIt's not true that all the different interpretations are not (in principle) experimentally distinguishable. Let's consider the difference between Copenhagen Interpretation (CI), De Broglie–Bohm theory (BT) and the Many Worlds Interpretation (MWI). BT assumes that under normal circumstances we have so-called quantum equilibrium and only then do you get the usual predictions of standard quantum mechanics that you get when you assdume CI. This means that you can try to detect small deviations of exact quantum equilibrium, see here for details.\n\nIf the MWI is correct then time evolution is always exactly unitary. The CI doesn't explain how we get to a non-unitary collapse, but it does assume that there exists such a thing. This implies that at least in principle there should be detectable effects. Systems that are well isolated from the environment should undergo a non-unitary time evolution at a rate that is faster than can be explained as being caused by decoherence by the residual interactions it still has with the environment.\n\nDavid Deutsch has proposed a thought experiment to illustrate that MWI is not experimentally equivalent to CI. Suppose an artificially intelligent experimenter is simulated by a quantum computer. It will measure the operator A = |0><0| - |1><1|. The qubit is initialized in the state |1/sqrt(2)[|0> + |1>]. Then the CI predicts that after the measurement the state of the qubit undergoes a non-unitary collapse to one of the two possible eigenstates of A, i.e. |0> or |1>. The MWI asserts that the state of the entire quantum computer splits into two branches corresponding to either of the possible outcomes.\n\nTo decide who is right, the experimenter decides to let the computer perform the unitary time evolution corresponding to inverting the final state of the quantum computer (according to the MWI) to the initial state, but while keeping the record that a measurement has been performed. This transform to the modified initial state is still unitary and can therefore be implemented (all unitary transforms can be implemented using only the CNOT and single qubit rotations).\n\nThen it is easy to check that if the CI is correct that you don't get that desired modified initial state back and the difference between the two states if the qubit you end up with, can be easily detected by doing measurements on it.\n\n• Thanks for answer. You claim interpretations have different predictions, but if they do so , how can we call them interpretations of same thing in first place?!!! If MW has different predictions than CI then they are not(and can't be) interpretations of same physical theory, – user55867 Mar 29 '15 at 20:18\n• The development of quantum mechanics has been \"work in progress\" for quite a while. If you had asked Dirac in 1928 about the possibility of hidden variables, he would probably have told you that this is pure philosophy, assuming that he would have told you anything at all, of course. But after the late 1920s QM was basically finished as a tool for physicists, their conventions became standard. So, you can't read too much about the way things have been named. – Count Iblis Mar 30 '15 at 15:41\n• I see your point, anyway my question was more related to interpretations of same physical theory and how they differ, not the fact that some \"interpretations\" are called \"interpretations\" only for historical reasons, – user55867 Mar 30 '15 at 21:58\n\nOn paper, the difference between a theory and an interpretation is very clear. If two distinct sets of ideas/explanations generate experimentally distinguishable predictions, then they are two different theories. If they use different concepts but produce identical experimentally verifiable predictions, then they are two different interpretations of the same physical theory.\n\nIn practice, things are never so clear-cut. As a practical matter, we certainly do not currently possess either the theoretical or the experimental capability to unambiguously falsify either the many-worlds or Copenhagen interpretation in any experiment that can actually be performed in the real world. But as Count Iblis points out, there probably are some hypothetical experiments that distinguish them, which could be performed in principle but may never actually be feasible in practice. (I think the same is true of the de Broglie-Bohm interpretation, although I'm not familiar enough with that interpretation to say for sure.) For example, decoherence is defined to be the vanishing of all the elements of a system's reduced density matrix that are off-diagonal in some basis known as the \"pointer basis\". But perfect decoherence is an idealization; in practice the off-diagnonal elements will be exponentially small but never exactly zero. (Similarly, there will always be incredibly many-point tunneling terms connect different branches of the wavefunction that appear at zillionth order in perturbation theory.)\n\nSo as practical matter, the many-worlds and Copenhagen interpretations are equivalent as physical theories to within our current understanding. In principle, they are almost certainly distinguishable if one could perform arbitrarily precise experiments and had infinite processing power. I would argue that we do not yet understand the different interpretations well enough to judge whether they will ever be experimentally distingishable in practice with foreseeable technology.\n\nSo you could approach this situation in many ways, and take any of the following (defensible) perspectives:\n\n1. MWI's and Copenhagen's predictions are indistinguishable in practice, so they are different interpretations of the same theory.\n2. MWI's and Copenhagen's predictions are distinguishable in principle, so they are different theories but are equivalent in practice.\n3. We don't understand MWI and Copenhagen well enough to judge whether they will be experimentally distinguishable in the future. So we do not yet know whether they are different theories or simply different interpretations.\n4. We don't understand MWI and Copenhagen well enough to judge whether they will ever be experimentally distinguishable in the future. But we should reserve the term \"theory\" to mean \"something that we actually know how to distinguish in practice\", and use \"interpretations\" to mean \"ideas that we do not currently know how to distinguish experimentally\". So the distinction between a theory and an interpretation is dependent on the scientific community's current knowledge of the subject. MWI and Copenhagen are currently just two different interpretations of the same theory, but way well eventually become two different theories as our understanding and/or experimental technology advance.\n\nThis distinction between actual experiments and \"theoretical experiments\" (a term with an interestingly semi-contradictory nature) comes up in other areas of physics as well. For example, Scott Aaronson's essay \"Why Philosophers Should Care About Computational Complexity\" puts a slightly different spin on some related ideas, and argues persuasively that philosophers should take seriously the practical limitations on what experiments and calculations could actually be performed in the real world.\n\n• \"tunneling terms connect different branches of the wavefunction\" -what is this? Can you elaborate? – Anixx Aug 15 '19 at 18:49\n• MWI and Copenhagen use exactly the same mathematical equations to describe evolution any given closed system. This means they are interpretations rather than theories (any system can be analyzed as a part of a closed one with appropriate choice of the boundaries and the observer.) – Anixx Aug 15 '19 at 18:55\n• Moreover, I would argue that MWI, Copenhagen, von Neuman and several other interpretations differ only in the placement of the Heisenberg cut. Copenhagen puts it between the measured object and measurement apparatus (e.g. at finite distance from the observer, in the past but allows big freedom in choice). Von Neuman interpretation is a limit of Copenhagen when Heisenberg cut is approaching the observer and MWI is when Heisenberg cut distance from the observer is approaching negative infinity (or the observer is put at infinite future). Thus they are simply applications of the same theory. – Anixx Aug 15 '19 at 19:02\n• Thus, Brogle-Bohm put the Heisenberg cut in the infinite past, Copenhagen in finite past, von Neuman in present, Relative QM in the finite future and MWI into infinite future. – Anixx Aug 15 '19 at 19:07\n\nI do not know that whether or not all interpretations can be distinguishable from each other. But after going through the link once, I thought Asher Peres probably implied that all the interpretations(De Broglie Bohm, MWI etc) will not have any effect on the probability of measurement outcomes (predictions of QM) i.e. the number of times detectors' clicks. In that sense, all the experiments with measurements (observables in QM) will give probabilistic outcomes and different interpretations are to explain the results, which are probabilistic in nature and all the interpretations are just various ways to rule out that probabilistic nature i.e different way to interpret the reasons for indeterminism which presents itself as one of the basic postulates in QM (as pointed out by Tom).\n\nHowever experiments have been performed to Check whether or not QM is consistent with Local Hidden Variable Theory. One can measure joint probability and show that QM violates Bell's Inequality. In that sense, one can show that QM violates Local Hidden Variable Theory.(http://en.wikipedia.org/wiki/Bell_test_experiments). For other interpretations there are some thought experiments (as pointed out by @Count Iblis). But to my knowledge no such experiments has been performed till now.\n\nIn the name \"interpretations\" it is implied that these are believed to not be empirically distinguishable. What everyone agrees on is how to calculate empirically testable predictions. That is essentially mathematics, and if you are very mathematically minded, you can propose to axiomize it, that is, find a minimum number of axioms (postulates) from which it follows. Obviously, as with any system of axioms, there is a bit of personal preference involved: Many call the time-dependent Schroedinger equation such a postulate. I personally prefer to only use de Broglie's matter-wave duality as a postulate and derive e.g. the (non-relativistic) Schroedinger equation for free massive particles from the non-relativistic impulse-energy relationship expressed for plane waves (which are one possible and hence sufficient choice for a basis system to express any wave in). I am afraid all one can summarily say is that there is no widespread consensus on what postulates/axioms to use; we physicists only agree on the (well-tested) outcome and perhaps that how exactly one gets there is at least as much a question of mathematics as of physics.\n\nWhilst \"interpretations\" was certainly the correct word historically, one can make good arguments that some theories that carry the historical name \"interpretation\" can actually be tested, at least if you take a sufficiently broad approach to tests as to permit thought experiments. Most interpretations fail to resolve paradoxes, such as Schroedinger's cat, the EPR paradox, or how to determine what constitutes a measurement (or how a wave-function collapse is physically possible considering quantum mechanical evolution only permits unitary, that is non-collapsing, time-evolution). That means most \"interpretations\" do not pass the test of logical consistency since otherwise there would not be any such paradoxes.\n\nEven with regard to experimental tests, we have at least two: The violation of the Bell inequality has been experimentally demonstrated, which is a test against hidden local variables, which would otherwise remain fair game for outlandish \"interpretations.\" And a simplistic form of Schroedingers cat can be realized in a 2-qubit quantum computer, where modelling decoherence as interaction with an environment (that could be a real uncontrolled environment or simulated via more qubits) provides an experimentally verifiable detail theory of just how the cat would decohere out of its curious superposition. If you like, that constitutes an empirical test that the Schroedinger cat paradox is not really a paradox and any interpretation that is unable to resolve it must be an incorrect or at least incomplete theory.\n\nFinally there is the issue of the recurrence time. Since quantum mechanics only allows unitary transforms, essentially rotations (and reflections) in a high dimensional Hilbert space, it predicts that everything repeats eventually, although most likely, due to the high dimensionality, only after a time that is mind-bogglingly huge even when compared to cosmological timescales. That is at odds with thermodynamics and relativity (at least if that is valid for ever expanding universes). There obviously must be tests for it, but finding them is surprisingly difficult. For example, even in theory waiting out the recurrence time is frustrated by the fact that if it exists as such, all notes and memories would have reverted, and we would again wonder if we should start the experiment for the first time ever! Yet on systems small enough that we can isolate them sufficiently from the environment to have short and observable recurrences (that experimentalists have come to call \"revivals\"), they demonstrably occur. At least to the extent that you consider this good enough to be at least a partial test of recurrence for the universe as a whole, this is of course at odds with any postulate of wavefunction collapse.\n\nRegarding the interpretation of QM, there are several schools of thought. Apparently Asher belongs to the \"just shut up and calculate\" school. He knows that classical intuitions do not suffice in trying to understand QA. But your term \"objective meaning\" needs to be clarified since in QM, measurements of properties of an object (say an electron) cannot be independent of the system or observer doing the measurement when the measurement is made. Can there be such a thing as an objective meaning when the meaning must necessarily, for humans, be a narrative saturated with the subject's own embodied metaphors? I submit that an understanding of any object, especially one that cannot be directly observed, cannot be entirely purged of subject.\n\nHere are that minimum number of postulates I obtained from my on-line MIT course with professor Adams (which is really great): QM, lecture 3.\n\n1. The configuration or state of a quantum object is completely specified by a wavefunction denoted as $\\psi(x)$.\n\n2. $p(x) = |\\psi(x)|^2$ determines the probability (density) that an object in the state ψ(x) will be found at position $x$.\n\n3. Given two possible states of a quantum system corresponding to two wavefunctions $\\psi_a$ and $\\psi_b$, the system could also be in a superposition $\\psi = \\alpha\\psi_a + \\beta\\psi_b$ with $\\alpha$ and $\\beta$ as arbitrary complex coefficients satisfying normalization.\n\n• I can't find any material in this answer that addresses the question. – user4552 Aug 8 '19 at 15:06" ]
[ null ]
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https://datascientyst.com/progress-bars-pandas-python-tqdm/
[ "In this short guide, I'll show you how to show progress bars for most common operations in Pandas.\n\nTo start, here is the basic usage that might be applied in order show progress bar in Pandas:\n\n• simple Pandas operations\n• `groupby` and other operations\n``````import pandas as pd\nimport numpy as np\nfrom tqdm import tqdm\n\ndf = pd.DataFrame(np.random.randint(0, 100, (1000000, 100)))\n\ntqdm.pandas(desc=\"power DataFrame 1M to 100 random int!\")\n\ndf.progress_apply(lambda x: x**2)\ndf.groupby(0).progress_apply(lambda x: x**2)\n``````\n\nIn the next section, I’ll review the steps and details to apply the above syntax in real examples.\n\n## Step 1: Install and Update TQDM\n\nFirst let's see how to install and update the library. To install `tqdm` in Python you can use the code below:\n\n``````pip install tqdm\n``````\n\nMany new features and bug fixes come with the latest version. It's always a good idea to stay up to date with most Python libraries:\n\n``````pip install tqdm -U\n``````\n\n`tqdm` shows progress bar for loops and other operations. All you need is to wrap any iterable with `tqdm(iterable)`.\n\nA fun fact for `tqdm` which you probably don't know:\n\n• the name derives from the Arabic - taqaddum (تقدّم) which mean \"progress\" * there is Spanish abbreviation - \"te quiero demasiado\" - meaning - \"I love you so much\"\n\n## Step 2: Show Progress bar on loops\n\nAs we so in Step 1 - all you need to do is wrap iterable with `tqdm`.\n\nLet's check a small program which calculates the power of numbers in range from 0 to 2000000.\n\nIn order to follow the progress of this operation we can use the following syntax:\n\n``````import numpy as np\nfrom tqdm import tqdm\n\nmyrange = np.arange(2000000)\ni_2 = []\n\nfor i in tqdm(myrange):\ni_2.append(i**2)\n``````\n\nThe result is:\n\n``````100%|██████████| 2000000/2000000 [00:01<00:00, 1624316.35it/s]\n``````\n\n## Step 3: Change progress bar size and style\n\nIf you like to change the way `tqdm` shows the progress bar you can use the following options:\n\n• import `from tqdm.auto import tqdm` to show a different style\n• add parameter `bar_format='{desc:<5.5}{percentage:3.0f}%|{bar:50}{r_bar}'` or `bar_format='{l_bar}{bar:10}{r_bar}{bar:-10b}'`\n\nLet's see both in action. First changing the style a nicer one (at least in JupyterLab):\n\n``````import numpy as np\nfrom tqdm.auto import tqdm\n\nmyrange = np.arange(2000000)\ni_2 = []\n\nfor i in tqdm(myrange):\ni_2.append(i**2)\n``````\n\nChange the size of the progress bar:\n\n``````import numpy as np\nfrom tqdm import tqdm\n\nmyrange = np.arange(2000000)\ni_2 = []\n\nfor i in tqdm(myrange, bar_format='{desc:<5.5}{percentage:3.0f}%|{bar:50}{r_bar}'):\ni_2.append(i**2)\n``````\n\n## Step 4: Progress bar during Pandas operations\n\nIn this step we will see how to show the progress for the most common Pandas operations.\n\nAdding a progress bar to Pandas shouldn't impact the performance but in case of doubts it's better to be checked.\n\nYou can find a simple example for Pandas progress bar below:\n\n### Pandas iterrows and progress bar\n\nThe simplest usage of `tqdm` in Pandas is in combination of loop and `iterrows()`. You will need to provide the total number of all items - which can be get by - `df.shape`:\n\n``````from time import sleep\n\nfor index, row in tqdm(df.iterrows(), total=df.shape):\nsleep(0)\n``````\n\n### Pandas progress bar for lambda\n\n`progress_apply` is a `tqdm` method which can accept a lambda. It can perform simple operations on the operand like power on 2:\n\n``````tqdm.pandas(desc=\"power DataFrame 1M x 100 of random int!\")\n\ndf.progress_apply(lambda x: x**2)\n``````\n\n### Pandas progress bar for function with progress_map\n\n`tqdm` offers method `progress_map` which can be used to apply functions to Pandas DataFrame or Series. It'll show a progress bar:\n\n``````from tqdm import tqdm\n\ndef cube(x):\nreturn x ** 2\n\ntqdm.pandas()\n\ndf['cube'] = df.progress_map(cube)\n``````\n\n### Pandas progress bar for dictionary map\n\nIf you like to map the values of a dictionary to Pandas column and follow the progress with bar you can use the following syntax:\n\n``````mapping = {15:'a', 9:'b'}\n\ndf.progress_map(lambda x: mapping.get(x))\n``````\n\n### Pandas and progress_aggregate\n\nFinally let's check how to show progress bar on aggregation functions like:\n\n• sum\n• count\n• mean etc\n``````from tqdm import tqdm\ntqdm.pandas()\n\ndf.groupby(0).progress_aggregate(sum)\n``````" ]
[ null ]
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https://gossipmixed.com/find-the-next-term-in-the-given-sequence-within-51-seconds/
[ "# Find the Next Term in the Given Sequence Within 51 Seconds\n\n## Mind Teaser Overview:\n\nPuzzle video games known as “mind teasers” problem gamers to discover a answer to a given difficulty. Mind teasers are entertaining however generally mentally taxing. They’re an exquisite technique to extend your mind capability and lateral pondering skills, maintain your reminiscence robust, and make you cheerful. There are a number of strategies to arrange these actions. They usually take the form of puzzles that have to be solved. It regularly requires uncommon pondering whereas holding the limits in thoughts; often, it requires lateral pondering. Amongst the varied sorts of mind teasers are logic puzzles and riddles.\n\n## Prepared for Challange:\n\nChances are you’ll remedy the arithmetic puzzle in the picture proven under by having a look at it. Is it easy? Did you handle to determine the puzzle? Let’s make issues tough. Time your self for 29 seconds to see how shortly you’ll be able to reply this arithmetic downside. Convey out your mathematical pondering to deal with this difficult puzzle. Your time has begun.", null, "The mind could also be stretched and stimulated by fixing arithmetic puzzles, which might additionally serve to extend one’s understanding of and proficiency in the topic. Discovering the reply regularly includes utilizing reasoning and problem-solving abilities. Mathematical issues that depend on reasoning and extrapolating data from a given set of situations are known as logic puzzles. Though they could possibly be tough, the pleasure of succeeding could be satisfying.\n\nA win-win circumstance, sure?\n\nBe fast!\n\nThe time is operating out!\n\nHave you ever discovered the puzzle but?\n\nTime is up.\n\nA mathematical conundrum could be resolved by observing it, attempting to unravel it, and developing with an answer. If you’re unable to unravel the downside, we’ve got an answer. We now have the reply to this mathematical conundrum if you’re nonetheless attempting to unravel it. Chances are you’ll consider your observational abilities and sharpness by fixing this puzzle.\n\nTo reply mathematical riddles, use mathematical formulae and equations. It teaches the appropriate technique for responding to a mathematical downside.\n\nThe sample is as;\n\n82 – 6 = 76\n\n76 – 6 = 70\n\n70 – 6 = 64\n\nSo\n\nx – 6 = 58\n\nx = 58 +6 = 64" ]
[ null, "data:image/gif;base64,R0lGODlhAQABAAAAACH5BAEKAAEALAAAAAABAAEAAAICTAEAOw==", null ]
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http://article.sapub.org/10.5923.j.ijtmp.20170705.01.html
[ " Alternative Idea of Relativity", null, "International Journal of Theoretical and Mathematical Physics\n\np-ISSN: 2167-6844    e-ISSN: 2167-6852\n\n2017;  7(5): 95-112\n\ndoi:10.5923/j.ijtmp.20170705.01", null, "### Alternative Idea of Relativity\n\nWitold Nawrot\n\nCorrespondence to: Witold Nawrot, .\n Email:", null, "Copyright © 2017 Scientific & Academic Publishing. All Rights Reserved.\n\nThis work is licensed under the Creative Commons Attribution International License (CC BY).\nhttp://creativecommons.org/licenses/by/4.0/", null, "Abstract\n\nA new, alternative idea of the reality is presented. Instead of four-dimensional space-time with the signature defined with the metric tensor and dimensions deformed as a function of body’s motion, a four-dimensional absolute Euclidean space is proposed whose dimensions do not have a predetermined meaning of time or space. The dimensions of time and space are not the dimensions creating the reality any more, but they are only certain directions in Euclidean four-dimensional space. And these directions depend on the pair of observer – observed body. While observing bodies moving with various velocities we interpret various directions in the Euclidean reality as the space-time dimensions and that’s, in general, the difference of directions interpreted by us as the space-time dimensions and not the deformation of dimensions, becomes responsible for relativistic phenomena. The new approach significantly simplifies the description of reality – through the description in Euclidean space, it eliminates singularities and additionally answers many questions that the Theory of Relativity was not able to answer to for almost 100 years.\n\nKeywords: Euclidean relativity, Recession of galaxies, Dark energy, Time dilation, Lorentz transformation, Mach principle, Wave function\n\nCite this paper: Witold Nawrot, Alternative Idea of Relativity, International Journal of Theoretical and Mathematical Physics, Vol. 7 No. 5, 2017, pp. 95-112. doi: 10.5923/j.ijtmp.20170705.01.\n\n### 1. Introduction\n\nI have been working for years on creating a model of reality alternative to the model introduced by the Theory of Relativity. The motivation for undertaking the construction of a new model from the ground up instead of developing the existing Theory of Relativity was the unnecessary complexity of the model, excessive number of assumptions and postulates, and accepting certain phenomena as the basis for further consideration instead of searching for the sources of these phenomena, and the fact that the current model leaves many questions and doubts which, despite the fact that TR was created more than 100 years ago, have still not been answered.\nI wanted to begin the list of doubts and objections regarding the Theory of Relativity from the well-known problems, widely discussed over the years:\nThe first problem is that the Lorentz transformation predicts time dilation and the length contraction. Even though we can see the proof of the time dilation every day while driving and using GPS navigation, length contraction of objects in motion has not been confirmed so far.\nThe next problem is the recession of galaxies - RT cannot explain this phenomenon. One of the attempts at explaining the phenomenon of recession of galaxies assumes the existence of the so-called dark energy, which has not been detected. It remains to be clarified whether the observed increase in the speed of galaxies as a function of distance is a result of actual acceleration of galaxies or whether it's the result of some unknown phenomena related to the way of observing reality.\nThe Mach principle and the fact that it is impossible to explain it within TR is also one of the problems.\nAnd the next issue I would like to mention is the lack of connection between Quantum Mechanics and the Theory of Relativity. If the TR is a theory that properly describes the reality that surrounds us, then at some point the effects described by the QM should appear. But so far, those are two separate models describing different types of phenomena.\nThere is also a problem with the existence of singularities in the TR. The existence of infinite values in the true reality does not seem to be possible. Perhaps the singularities are not the property of the reality but they result only from the properties of the current model, i.e. they are the properties of the accepted description. Perhaps, accepting another model would allow to avoid singularities in the description.\nTo the above well-known problems I would like to add a few of my personal remarks and doubts:\nI would like to start from the covariant notation itself. The introduction of time as a fourth dimension to the description of the reality was based on the introduction of a metric tensor with the signature 1-1-1-1, whose form was chosen to assure compatibility with the observations. However, there is no deeper justification for this and not another form of metric tensor. The use of metric tensor does not explain the source of any phenomenon. It only says: if-then, therefore it describes the problems and does not explain them. To justify my view of this problem I can give the following example: if I wanted to describe how the lights in my room work, I could define the tensor, analogous to the metric tensor, with the signature of zeros and ones, for instance 111101101, where zero corresponds to a broken bulb, and one to a good one. This signature, is accepted because it is consistent with the observation of the behavior of the lights (we do not need to know how the bulb works or what the construction of the bulbs is). Multiplying this tensor by a zero-one vector of the state of switches, we get a description of the operation of the lights. Such a method allows us to describe the operation of the lights. But does it allow us to understand the essence of electricity? Of course not, there is no Ohm’s law, electric potentials, motion of electrons, electrical charges, quantum emission, etc. Meanwhile, this kind of description is the basis we use for building the relativistic equations. By applying the tensor notation we can describe practically all physical phenomena - analogous to the description of electricity described above - but it is always a description only. Of course it will allow us in many cases, to draw conclusions about behavior of the phenomena under new conditions; however, it is still just a description and not an explanation of the essence of the phenomenon.\nAnother problem is the premature - in my opinion - acceptance of the postulate of constancy of the speed of light. Accepting this postulate allowed, on the one hand, to quite quickly develop the Theory of Relativity to its present form and to achieve many spectacular successes with the TR at the beginning of the last century; however, it also blocked research on the physics that is responsible for the phenomenon of constancy of the speed light. Of course, such research would have delayed the development of the RT at an early stage, but resolving the problem of constancy of the speed of light instead of adopting it as a postulate would probably allow knowledge to progress further than it has in this past century. If the velocity of light behaves strangely from our point of view – i.e. is constant regardless of the velocity of the observer – then, when solving this problem, we do not need to match the model to the observed phenomena at the cost of complexity and accepting many unexplained phenomena as basic assumptions and postulates. Perhaps the use of the notion of velocity should be limited only to non-relativistic mechanics - hence the unusual behavior of velocity of light for higher velocities of observers. Maybe instead of adjusting and complicating the model to fit the familiar notions of velocity to the relativistic phenomena - to which this notion may not apply - we should think about describing the relativistic motion with another, yet unknown, variable? Finally, about 500 years ago, attempts were made to adapt the model describing the motion of the planets to their motions observed on the firmament, which led to the unnecessarily complicated model describing the motion of the heavenly bodies. It was enough to move the reference system from Earth to the Sun for everything to become easy to explain. In case of velocity we may be dealing with a similar mechanism.\nAnother problem is the time dilation as a function of the motion of bodies. In the TR it is accepted that the time in a frame in motion slows according to the following formula:", null, "(1)\nwhere", null, "– time in the frame in motion,", null, "- time in the frame of an observer.\nMultiple experiments confirmed this relationship. However, this experimental evidence has one fundamental flaw, which I already described in my previous papers [1, 2] namely in the experiment of Hafele and Keating from 1971, and in case of the motions of GPS satellites, this formula is true only for curved routes. Therefore, these experiments are an evidence for the General Theory of Relativity and cannot be treated as a proof for the time dilation for rectilinear and constant motion, i.e. for the STR – as it is currently accepted. Moreover, the mistake made by Hafele and Keating while deriving formula (1) with the help of the STR is also repeated in case of other experiments which prove the correctness of the time dilation as a function of velocity. Therefore, currently we are not able to unequivocally state if the formula (1) proves that the uniform, rectilinear motion is responsible for time dilation, because during the experiment one of the participants must change its velocity to register the actual time difference, and it is very likely that this velocity change is responsible for the mechanism of actual dilation of time.\nAs one can see, though the TR is describing many phenomena correctly and has been successful in many areas, there are some important issues that do not seem to be solved within the TR.\n\n### 2. The Basis of the New Approach to Problems of Space-Time\n\nIt turns out that it is possible to create a model of reality that, apart from explaining the problems described by the \"classical\" Theory of Relativity, also allows to answer all the questions and doubts mentioned above. While there are still problems that have not been completely resolved, it can be said that the milestones have been developed for the new model of reality which allows to simplify the description of phenomena and expands the description potential, within one model, for a wider range of phenomena than before.\nArguments for seriously considering the approach proposed below include greatly simplified description of many phenomena, the possibility of describing and solving, within one model, many problems and phenomena, such as the recession of galaxies, time dilation, Mach principle, wave properties of particles, etc., which up till now required different models, a significantly wider scope of described phenomena in relation to the capacity of the Theory of Relativity, and the fact that the new model in its current state can be experimentally verified.\nThe essence of the idea presented here relies on the assumption that the \"true\" reality is built of different dimensions than the observed dimensions of time and space, namely:\n1. The “true” reality is a four-dimensional, absolute Euclidean space, its dimensions denote certain distances, which do not have the meaning of time or space distances assigned in advance. The dimensions creating the four-dimensional absolute Euclidean space will be marked with letters abcd to distinguish them from dimensions of time and space – xyzt, perceived by us. The four-dimensional, absolute Euclidean space described with the letters abcd, together with bodies existing in it, in further parts of this paper will be named FER – Four-dimensional Euclidean Reality. The notion “space-time”, in this paper, will denote the “traditional” four-dimensional Minkowski space-time.\n2. The space-time dimensions xyzt (because of the lack of covariant notation, for the purpose of this article I will not be marking space-time dimensions as “xi”, etc.), in this model, are not the dimensions creating the reality any more. The dimensions xyzt observed by us are nothing more than certain directions in the “true” Euclidean reality (FER); these directions are not stable but depend on the observer and the currently observed bodies. The rules for defining the space-time dimensions in the FER will be described in the following points.\n3. In the four-dimensional absolute reality (FER), there are bodies. These bodies are “moving” along trajectories in the FER (the notion of “trajectory” in the FER replaces the notion of “world line”, which is proper for the space-time). The term \"move\" means that in case of rectilinear trajectories, the length of the trajectory traveled by the body is the measure of proper time of this body. Trajectory for a specified body has a direction and order and is interpreted by the body as its time dimension. All trajectories are allowed and equivalent.\n4. As the space-dimensions we interpret three directions in FER orthogonal to each other, perpendicular to the trajectory of the currently observed body. It means that the observer, while observing different bodies, interprets different directions in the FER as its space-dimensions. Thus, in FER, in relativistic cases, for observation of each specific body, a different set of directions interpreted as the space coordinates is defined, and the direction interpreted as the time dimension (the trajectory of an observer) is not, in general, perpendicular (in FER) to the directions interpreted as the space-dimensions (see for instance Fig. 1). This is an illustration of the fact that the dimensions themselves cannot be observed, and we learn about the existence of space and the number of its dimensions through observation of the surrounding bodies.\n5. The idea of absolute space needs to be complemented with the concept of an absolute time. The absolute time is not the fifth dimension. It is a parameter and corresponds to the distance between points in the FER. In the case of rectilinear trajectories, the absolute time is equal to the time that passed in the coordinate system of the body moving along that trajectory.\nI will show how the new model works using specific problems as examples.\n\n### 3. Absolute and Relative Motion. Speed, Mach Principle, Singularities\n\nFrom the assumptions above it follows that bodies exist in the FER and move along trajectories – for the time being, rectilinear. According to the assumptions, the “motion” means travelling along the trajectory, and the length of the trajectory traveled by a body is equal to the time measured by the clock of that body. Therefore, in case of rectilinear trajectories, each body moves relative to the absolute space at an absolute velocity equal to 1. Since the measure of time of a body is the length of the trajectory traveled by this body, then the motion of the body relative to the absolute space is interpreted by the body as the time flow, and the trajectory in FER is the time axis of the body’s coordinate system.\nNow, if two bodies move along trajectories inclined to each other at an angle then the observer interprets directions perpendicular to the trajectory of the observed body as its space-dimensions. This situation is presented in Figure 1.", null, "Figure 1. Mutual observation of bodies. Two bodies move along their trajectories which are the time axes of their local coordinate systems. The FER directions perpendicular to the trajectory (the time axis) of the observed body are interpreted by the observer as its space-dimensions. In Fig. a, the body 1 is the observer (coordinate system x1t1); in Fig. b, the body 2 is the observer (coordinate system x2t2). In FER, for relativistic cases the time axis of the observer is not perpendicular to its space dimensions\nDue to the proposed way of observing bodies along the directions perpendicular to the trajectory of the observed body, although the space is absolute and the motion of the bodies relative to space is absolute, the mutual motion of the bodies is relative and is described not by the motion relative to space but by the angle between the trajectories of the bodies. Looking at Fig.1, we can see that the relative velocity of bodies is described with formula (2)", null, "(2)\nwhere i=1,2.\nFrom this formula and the mechanism of observation shown above, a number of instant conclusions can be drawn:\n1. The relative motion of bodies measured by the relative inclination of the trajectories of the bodies, and the absolute motion relative to the space, i.e. the motion of the bodies along their trajectories, are distinct phenomena that are not mutually exclusive each other.\n2. Since all the trajectories are equivalent, the physical phenomena cannot depend on the angle of the trajectory in the FER, i.e. on the relative speed, and this automatically fulfills the first postulate of the TR.\n3. The absence of a distinguished direction in the FER indicates that there is no absolute angle of inclination of the trajectory, i.e. the rectilinear motion of the bodies in the sense of formula (2) is relative -the angle of inclination of the trajectory can be determined only with respect to the trajectory of another body. In other words, the velocity measured according to the formula (2) can be determined only in relation to another object. However, in case of non-inertial motions – along a curved trajectory - the radius of curvature of the trajectory does not depend on the choice of any observer’s reference frame in the FER, because the radius of curvature of trajectory is determined in relation to the previous parts of the same trajectory, i.e. a specified trajectory, and it can be described with the absolute Euclidean coordinate system abcd.\nFor instance, in a two-dimensional plane, the curved trajectory can be described with the formula which depends only on the absolute coordinates", null, "(where a and b are the absolute coordinates).\nThen the radius of curvature will be equal to:", null, "(3)\nThe radius of curvature of the trajectory does not depend on the choice of the observer. Therefore, it is an absolute value. Since the inertial forces depend on the curvature of the trajectory, the existence of the inertial forces is a consequence of existence of absolute reality or, in other words the existence of the whole Universe. It is an idea similar to the Mach principle; however, it is connected with the existence and structure of absolute space and not with the mass distribution in the Universe. So, according to the presented model, the Mach principle in general is correct but there are some important differences. The chapter “Example: The quantized time dilation in case of twin paradox” suggests some idea about how the interaction of bodies with the rest of the Universe causes inertial forces. Due to the absolute property of curvature of trajectory of bodies, which unequivocally determines the non-inertial observer, the relativity of motion in the sense known from the Theory of Relativity can be applied only for rectilinear trajectories, i.e. for inertial motions.\n4. The velocity defined by the formula (2) is limited to a value of 1 – which, as it is easy to guess, is the speed of light; it will be described in detail in the following chapters (the speed of light is equal to one because all dimensions are in the same scale). This limitation means that the velocity can only be defined for trajectories inclined to the observer’s trajectory at an angle less than 90°. This is not a limitation regarding trajectory, because all trajectories are allowed. This is a limitation concerning only the observation performed in the xyzt coordinate system (space-time): it means that we are unable to observe bodies moving along trajectories inclined to the trajectory of the observer at an angle 90° and greater. It is still possible to accelerate the body to the trajectory inclined to an observer's trajectory at an angle greater than 90°; however, observation of transition to such trajectory will last until infinity and the time in the accelerated body’s frame will be observed as if it was decreasing to zero (the problem of time dilation will also be discussed later). It will result in singularities specific to the speed of light. To summarize this point: To describe the motion of bodies, a trajectory is a more general notion than velocity and allows to describe a broader class of motions, while singularities do not occur in the FER. The singularities appear only during transformation to description using space-time xyzt coordinates, when the trajectory of the observed body becomes perpendicular to the trajectory of the observer. Singularities are the result of a specific process of performing observations of bodies – with the use of directions (interpreted as the space coordinates) perpendicular to the trajectory of the observed body – and are only the property of the Minkowski model of space-time.\n\n### 4. The Speed of Light\n\nThe limit of velocity for bodies defined by formula (2) is equal to 1. According to the model presented here, the velocity of propagation of the interactions is also equal to 1, but it results from a completely different mechanism.\nIn my earlier papers I suggested that quanta are sent by the observed body perpendicularly to its trajectory, i.e. along the spatial axis of the observer, and the quanta propagate along this axis at a constant velocity equal to 1 relative to that axis. This axis is then \"carried” along the observer’s trajectory. Thus, the resulting trajectory of quantum in FER depends on the trajectory of the body sending the signal and the trajectory of the body receiving that signal. This mechanism is shown in Fig. 2. It shows why the speed of light does not depend on the angle between the trajectories of the bodies, i.e. the velocity. The dependence of the resultant trajectory of quantum in the FER from the trajectory of the body receiving the quantum suggests, however, the existence of instantaneous communication between quantum-communicating bodies.", null, "Figure 2. Propagation of light in FER. The quantum is sent in point A by a body moving along trajectory t’. The quantum is propagating along the x-axis of the observer – the AO segment. This axis is “carried” along the trajectory of the observer – t. The resultant trajectory of the quantum is represented by the AC segment. The segments AO and OC are equal\nIt has recently been found that it is possible to justify such quantum behavior in a much simpler way and without making assumptions about instant communication.\nIt is enough to assume that bodies send and receive signals along directions perpendicular to their trajectories in FER. A body moving along its trajectory in the FER sends a signal. The signal propagates along the space direction perpendicular to the trajectory of the body at the speed of 1. Since the body keeps moving along its trajectory, the signal propagates also along the trajectory of the body at the speed of 1. Thus, the signal propagates at an angle 45° to the trajectory of the body sending the signal at an absolute velocity equal to", null, "A similar mechanism takes place for the body receiving the signal. The described situation for pair of observers – sender and recipient of the signal - is shown in Fig. 3. At the beginning, both bodies (sender and recipient) are in the common point S.\nNow, if the observer in the coordinate system x1t1 positioned on the trajectory at point A (Fig. 3) sends a signal, the signal propagates along the segment AD and then along the segment DC in the FER. Namely, the signal travels the distance d along the trajectory t1 and the distance d along the direction x1 perpendicular to t1. Halfway, the spatial directions of both bodies, the one sending and the one receiving the signal, have a common point - point D in Figure 3. From this point on, the signal can propagate along the direction perpendicular to the trajectory of the body receiving the signal and, again, the signal is traveling the distance d along the direction x2 and the distance d along the trajectory t2 and finally reaches point C. Thus, in absolute space, the signal traveled distance 2d along the trajectories of the bodies, and the distance 2d along the directions perpendicular to those trajectories, interpreted as the space-dimensions of the local coordinates systems of both bodies - sender and recipient of the signal.\nTherefore, the above can be expressed with the formula:", null, "(4)\nWhere V – velocity of signal registered by observers, described in the system of absolute coordinates, and the segments AE and BF are equal to each other.\nThus, considering the motion of the signals in the absolute space, we have a constant speed of propagation of the signals, regardless of the angle between the trajectories of the bodies. At the same time, the signal sent at point A on trajectory t1 reaches the trajectory t2 at point C, identical to that in Figure 2. The segments AO and OC on both figures are identical.\nThe flaw of this model is that it works correctly only when the line defined by the SD segment is the bisector of the angle between the trajectories, which means that in practice both bodies should meet at the same point in the FER (here – point S). This problem has not yet been completely solved, but this example shows that under the above conditions, assuming propagation of signals only along directions perpendicular to the trajectories of the bodies, the constancy of the speed of light can be explained independently of the relative speed (an angle between trajectories) of the source and the receiver. At the same time, it is easy to see that for trajectories inclined to each other at an angle ≥ 90°, the signal never reaches the recipient, i.e. we are not able to observe, with the help of quantum, objects moving along such trajectories; in Fig. 3 for the angle between trajectories t1 and t2 equal to 90°, the quanta’s trajectory (AD) will be parallel to the bisector of the angle between the trajectories (SD), so the transition of the signal to the coordinate system x2t2 will not be possible. However, even though we are unable to observe these bodies, we can interact with them - for example, through collisions. There is another problem: the non-visible part of the Universe (particles/objects moving along trajectories inclined to the trajectory to observer at an angle 90°-180°) should carry additional mass similar to the mass of the observed part of the Universe. Will this additional mass affect processes in the visible part of our Universe, and if so, how? At this moment, it is difficult to answer these questions clearly, but, as we see, the new model allows for many more tools for describing and interpreting various phenomena than were previously available.\nWe have considered propagation of signals in the absolute space FER. The velocities at which the observers move along their trajectories are equal to 1, the velocities of the signals are equal to", null, "and the trajectories of the signals are inclined to the trajectories of the bodies sending/receiving signals at an angle 45°.\nHow does this problem look from the point of view of the observer? In Fig. 3, the body in coordinate system x2t2 is the observer because it receives the signal. The observer knows only that the signal was sent by the observed body at point A and was received at point C, but does not know the true route of the signal, i.e. the segments AD and DC. He also knows (Fig.3) that the speed of propagation of the signals is constant, so the triangle generated by the AC trajectory, the path on its trajectory (t2), corresponding to the time from sending to receiving the signal, and the space direction must be isosceles. Therefore, the space direction - along which, from the point of view of the observer, the signal propagates - must be the segment AO, equal to the segment OC on the observer’s trajectory (resulting from simple geometric relations). In this way we arrive at the justification of the diagram shown in Figure 2 and justification of the fact that by observing other objects with the help of interactions propagating along the space dimensions of the local coordinates systems of the bodies, the directions perpendicular to the trajectory of the observed object are interpreted by us as our space dimensions. It should be noted that the directions in the FER interpreted as the space-dimensions depend on the manner of exchanging interactions – for instance, in case of interfering particles treated as waves, the space dimensions will be assumed to be perpendicular to the time axis of the observer. It is described in the chapter “Energy of particles and energy of macroscopic bodies”.\nIt should be emphasized that in the absolute space according to Fig.3 points A and B are simultaneous, because they are positioned at the same distance from the point S, common for both trajectories, (assuming that at point S the two bodies meet). Meanwhile, from the point of view of the observer, the simultaneous points are A and O (Fig. 3). Since the length of the trajectory is a measure of the time that has passed in the coordinate system of the observer, the observer sees that when the time equal to the length of the SO passed in his frame, a shorter time equal to the length of segment SA passed in the coordinate system of the observed body. Hence the observed dilation of time in the coordinate system of the body in motion. This problem is described in detail in the chapter „Dilation of time and the twin paradox”.", null, "Figure 3. Suggested mechanism of propagation of EM signals. A signal is sent from point A by a body moving along trajectory t1 and it propagates along direction x1 perpendicular to trajectory t1. It travels distance d along trajectory t1 and distance d along direction x1 (segment AD). In point D quantum is „captured” by a body propagating along trajectory t2 and now it propagates along direction x2 perpendicular to trajectory t2. Now it travels distance d along trajectory t2 and distance d along direction x2 (segment DC)\n\n### 5. Interpretation of Results of the MM Interferometer Experiment\n\nAccepting the FER model in which space is absolute is, in a way, a return to the hypothesis of ether .\nThe basic argument against the existence of ether was the Michelson Morley experiment. However, in this experiment it was assumed that the motion of quantum and the motion of bodies relative to the medium are the same phenomenon. In the model presented here, the motion of bodies along their trajectories and the motion of quantum are absolute motions relative to the space, but what we observe as motion of bodies of nonzero mass is the result of motion of bodies along the trajectories inclined to each other wherein a measure of the relative velocity is the angle of their inclination. Now, if we consider the MM experiment in the FER, then the motion of quantum and the mirrors’ trajectories are absolute movements, while the interferometer velocity is only the angle of inclination of the trajectories. By changing the velocity of the interferometer we only change the angle of inclination of all trajectories, which does not affect the propagation of signals and the movement of mirrors along their trajectories in relation to each other. The way the MM interferometer works in the FER is shown in Figure 4.", null, "Figure 4. Light propagation in MM interferometer in the FER. The mirrors are in rest relative to each other, so they are moving along parallel trajectories. Light is emitted and reflected at a 45° angle relative to these trajectories, independently of the angle of inclination of trajectories, i.e. velocity equals:. Therefore, the angle of inclination of trajectories of the MM interferometer has no impact on the propagation of light in the interferometer\nAs we can see, the present concept of absolute reality - FER- cannot be verified with a MM interferometer. A detailed description of the experiments using the MM and Sagnac interferometers from the point of view of the FER model is presented in .\n\n### 6. Other Problems Related to the Model of Observation Described Above: The Recession of Galaxies and the Shape of Space-Time Interval\n\nThe recession of galaxies\nOne very strong argument for the method of observing reality proposed here is the phenomenon of the recession of galaxies. Adopting the assumption that we interpret the directions perpendicular to the trajectory of the observed bodies as our space dimensions allows us to instantly explain all the properties of the phenomenon of the recession of galaxies. An example of observation of the recession of galaxies is shown in Fig.5. t = 0 is when the Big Bang - the beginning of the Universe – takes place. Trajectories of all objects in the Universe have their common origin at this point. The observer moves along the trajectory t. Time t0 on the trajectory of the observer corresponds to the age of the Universe because it’s the distance measured along the trajectory (time measured in the observer’s frame) from the Big Bang to the moment of time when the observation is being performed. The observer, located at the point t0, performs the observation of galaxies moving along trajectories t1 and t2. When observing each of the galaxies, the observer interprets different directions in the FER as his space dimensions. In Fig.5, for a galaxy moving along trajectory t1 it is the direction x1, for a galaxy moving along trajectory t2 it is x2. The observer measures the distances from the galaxies along these directions (interpreted by the observer as his space dimensions) and the distances are equal to r1 and r2, respectively.", null, "Figure 5. The recession of galaxies in the FER. An observer and two galaxies move along trajectories with a common origin – the Big Bang. The observer that moves along trajectory t at point t0 observes each of the galaxies along a different direction, perpendicular to the trajectory of an observed galaxy. The distances from galaxies 1 and 2, registered by the observer, are equal to r1 and r2 respectively\nThe velocities observed in the observer’s frame using so defined dimensions are equal to:", null, "(5)\nWhere i=1,2 – number of the trajectory of the galaxy, t0 – the age of the Universe, H – Hubble’s constant.\nAs one can see, the velocity of the galaxy observed by the observer at point t0 depends on the distance from the galaxy. However, the increase of the velocity with the distance is not the result of any actual acceleration, but is merely a result of performing observations along directions in the FER that are perpendicular to the trajectories of galaxies in the FER and interpreted by observers as their space dimensions. In fact, the galaxies do not accelerate but they move along their trajectories at an absolute velocity equal to 1 relative to the absolute space, exactly like all other bodies in the FER. Therefore, there is no actual acceleration of galaxies and there is no need to search for external solutions like dark energy. At the same time, we have a natural explanation for the value of the Hubble constant as the inverse of the age of the Universe, and from the fact that the observer moves along its trajectory (time axis), it follows that the Hubble constant must decrease with time.\nOf course, the diagram shown in Figure 5 is simplified because the trajectories of galaxies are presented as straight lines. In practice, the galaxies rotate, perform different motions, so the formula (5) will not accurately describe the speeds of galaxies, but the basic principle is the same, and the fact that the FER model provides such a simple explanation of such a complex problem is one of its major advantages.\nThe same mechanism that leads us to observe the acceleration of galaxies explains the shape of the space-time interval and the time dilation phenomenon.\nShape of the space-time interval\nLet us consider two observers observing the same body. Since the observer interprets directions perpendicular to the trajectory of the currently observed body as his space-dimensions, then all observers observing this body will interpret the same directions in FER as their space dimensions. An example of several observers observing the same body is shown in Figure 6.\nWe can see that each of the observers sees that the time that passed in the coordinate system of the observed body, i.e. the length of the trajectory of the observed body, can be described in his coordinate system by the following equation (6):", null, "(6)\nwhere i=1,2 (Fig.6).\nWe can see that the choice of space axes of the observer as perpendicular to the trajectory of the observed body naturally leads to the equation of the space-time interval without the need to define the metric tensor.\nHowever, this equation is limited only to cases of observation of bodies. According to the FER model the space-time interval is not an internal property of the reality (the space-time according to TR). It is simply a rule by which we can determine the relationship between the coordinates of observers observing the same body. Such a meaning of the space-time interval is reduced only to the proper time of an observed body and can only have real values. Any conclusions about the consequences of complex solutions of equation (6) cease to make sense. It is easy to guess that the relationship between the observer’s coordinates shown in Fig. 6 will lead to a different transformation of coordinates than the Lorentz transformation and to a different rule of composition of velocity, but it will be described in the following chapters.", null, "Figure 6. Two observers moving along trajectories t1 and t2 observe a body moving along trajectory t’. The observers interpret directions perpendicular to trajectory t’ as their space dimensions\n\n### 7. Dilation of Time and the Twin Paradox\n\nAs it was described above, the observer, while observing the body, interprets directions perpendicular to the trajectory of the observed body as his space-dimensions. The rule of mutual observation of bodies was presented in the previous chapters. We will base our further considerations on Fig. 1. As follows from Fig.1, the observer observing the moving body sees that time in the frame in motion flies slower than in his reference frame – Fig.1a. The situation is symmetrical, because from the frame of the moving observer, a similar time dilation can be observed in its neighbor’s reference frame (Fig.1b). From the geometrical relationships in Fig. 1, one can immediately derive the formulas for the observed dilation of time:", null, "(7a)\nand", null, "(7b)\nHowever, as we can see, the dilation of time is only an effect of mutual observation and has nothing to do with the actual time dilation we observe - for example in the GPS system.\nTo properly describe actual time dilation, we must make a counterintuitive assumption, which for the time being has to be simply accepted, although explaining it is probably only a matter of time.\nLet us consider the detector placed in the observer’s frame at the space distance r0 from the origin of the coordinate system. At the time t0 the detector is hit simultaneously by several particles moving at different velocities or, in other words, along trajectories inclined at different angles to the trajectory of the observer.\nAs we can see, the representation of the xyzt point in the observed space-time (Fig.7a) is, in the FER, the sphere with the radius", null, "and with origin in point t0 on the observer’s trajectory (Fig.7b). All points on the sphere must describe the same time – therefore, motion between any two points of the sphere takes no time. If we apply this to our observation we’ll get the situation shown in Fig.8.", null, "Figure 7. The point positioned at the time t0 and at the space distance r0 from the origin of the space-time coordinate system -Fig. a - corresponds to the sphere with the radius r0 and center at the point t0 on the trajectory in the FER – Fig. b\nIn Fig. 8 we see that as long as both observers are moving along rectilinear trajectories then the effect of time dilation will be symmetrical so that both observers will observe the same slowing of time in the neighbor’s system - exactly as shown in Fig.1. At the moment of the velocity change of, the observer, who changes his speed, travels some part of his route on the surface of the sphere shown in Fig.7b - here the trajectory AB. On the segment AB there is no time flow so the total flow of time in reference frame of body 2 relative to the time flow in the reference frame of body 1 is equal to:", null, "(8)", null, "Figure 8. Twins paradox. Observer 2, when changing his velocity travels some part of his trajectory along arc AB. The time flow between points A and B is equal to zero. Due to the change of the velocity of body 2 from V=sinϕa to V=sinϕb, the observed, mutually symmetrical change of time becomes the actual change of time\nThus, the change of the speed of the body, whose time in its reference frame is supposed to be shorter, is a necessary condition for changing the observed symmetrical dilation of time of one body relative to another into the actual change of time in the frame of the body whose speed has changed. Hence, the time dilation in the frame in motion is not only the result of velocity but, primarily, the result of the change of the velocity. However, the resulting formula is the only a function of velocity, which has been a source of misunderstandings for many years [1, 2]. Therefore, the time dilation resulting from the motion of satellites of the GPS system requires the change of direction or value of the velocity and it is only under this condition that the formula describing the time dilation, nota bene identical as the one derived from the Special Theory of Relativity (1), properly describes the indications of the satellite’s clock. More about the physics of the time dilation can be found in the chapter “Example: The quantized time dilation in case of twin paradox”.\n\n### 8. Transformation of Coordinates versus the Lorentz Transformation\n\nIn the chapter “Form of the space-time interval” I have shown how the shape of the space-time interval can be obtained. At the same time, the problem of observation of a body by several observers, shown in Fig.6, allows to find the transformation between coordinate systems of observers of the same body. From simple geometric transformations resulting from Fig.6 one can obtain formulas for transformation of coordinates which also satisfies the equation of space-time interval; however, it differs from the Lorentz transformation. The new transformation formulas take the following form:", null, "(9)", null, "(10)\nwhere:\nThe velocity of observer 1 relative to observer 2 is:", null, "(11)\nwhereas the velocity of the body observed by the two observers (moving along trajectory t’ in Fig.6) relative to observer 1 is:", null, "(12)\nThe time dilation formula resulting from formula (7) is no different from the analogous formula resulting from the Lorentz transformation:", null, "(13)\nwhile the relativistic length contraction, according to formula (8) should not take place:", null, "(14)\nThus, the proposed approach explains the observed dilation of time in reference frames in motion, while also explaining the failure in proving the relativistic length contraction.\nAccording to the proposed model, the Lorentz transformation is mathematically correct but non-physical, because the two equations of Lorentz transformation describe two different bodies moving along different trajectories, and both equations have a common solution only at the point of intersection of these trajectories. The exact explanation of this problem and the extended form of formulas (9) and (10) are available in .\n\n### 9. Composition of Velocities and Proposal of Experimental Test Confirming the New Approach\n\nThe new transformation of coordinates leads to the new rule of composition of velocities. Since velocity is a function of an angle between trajectories, the composition of velocities relies on the addition of angles, according to Figure 6. If the angle between the trajectory t' and t1 is ϕ1 and the angle between the trajectories t1 and t2 is equal to ϕ12 then the velocity of the body traveling along the trajectory t’ relative to body traveling along trajectory t2 is:", null, "(15)\nwhich, rewritten using velocities described by the formulas (11) and (12), takes the following form:", null, "(16)\nA similar relationship was also derived by another author using a different method .\nA comparison of rules of composition of velocities for two identical velocities for Galilean and Lorentz transformations and according to the FER model presented here is shown in Fig. 9.", null, "Figure 9. Composition of two identical velocities according to Galilean and Lorentz transformations and according to the FER model presented here\nAccording to formula (16), we still cannot exceed the speed of light, but by composing the appropriate velocities we can reach a 90° angle between the trajectories, which corresponds to the speed of light (Fig.9). This should lead to registering experimental results. A proposal of such an experiment for obtaining measurements of total proton-proton cross-sections shows that in the case of two colliding beams we should observe doubling of total cross-section for the energy of each of colliding beams corresponding to the velocity of each beam V = sin (45°). When these speeds are exceeded, a discrepancy between the total cross section for collisions of fast protons with the stationary protons, with analogous experiments using two colliding beams of the same relative velocity resulting from the Lorentz transformation, should occur. The occurrence of such discrepancies in measurements of cross section for high energy protons of cosmic origin with the protons in the atmosphere was previously described in .\nHowever, the following question may be asked: if for the colliding beams of energies corresponding to velocity V = sin (45°) for each beam, there should occur a clear difference between experimental results and the predictions of TR and the difference occurs for the values of energy achieved in typical experimental devices, why has no one observed such effects so far?\nAccording to the calculations from , such anomalies occur only in a very narrow energy range and require very homogeneous energy of beams. For example, for this experiment with total proton-proton cross-section measurements, with a proton beam’s energy of about 0.4 GeV, proton energies should match the desired energy to the up to several hundred eV. Greater width of distribution of energy will result in detecting only a slightest increase in statistical errors at this energy.\nSimilarly as in the described experiment, it should be possible to observe the anomalies in a strictly defined energy range in other experimental devices as well, but it requires very narrow energy distribution of the colliding beams.\n\n### 10. Description of Phenomena in FER and Description of Phenomena in Relativity Theory - Summary and Introduction of Complex Notation\n\nIn Theory of Relativity it was assumed that the reality surrounding us is built of three space dimensions and one time dimension. Phenomena were therefore described as functions of space-time dimensions. However, the equations of TR describe the variability of these phenomena not with respect to these coordinates but with respect to three space dimensions and a space-time interval - instead of the dimension of time.\nIn the FER, we assume that there are four identical dimensions abcd creating the Euclidean space (space, not space-time, because the ideas of time and space refer to the perception of dimensions abcd through the observation of bodies in that space and they are a property of observation rather than the dimensions of reality). All phenomena are functions of these four dimensions, and their variability is also related to these dimensions and not to any other values, that are not the dimensions of reality - as it was done in the case of TR. In practice, when describing the motion of a body in FER, we do not have to use the dimensions abcd of which the FER is composed. We can use any orthogonal coordinate system - for example, a coordinate system consisting of the time axis of the reference system of observed body - t' (trajectory of observed body in FER) and the three space-dimensions of the observer of this body (perpendicular to the trajectory of the observed body). It is a coordinate system of four orthogonal directions in FER so we can use it to describe phenomena, because there is no distinguished direction in space in FER that would force the selection of a set of orthogonal directions to describe phenomena.\nTherefore, when describing events in FER we can, similarly as in TR, relate the variability of phenomena to the spatial coordinates of the observer and proper time of the observed body - which is, in the case of observation of a specified body, the space-time interval, but unlike in TR, the phenomena are also functions of the same coordinates - xyzt' instead of xyzt. A similar approach has been previously suggested in literature attempting to describe the reality with the help of Euclidean model, e.g. in [9-11]. However, the fundamental difference between the use of xyzt’ coordinates to describe reality in previous works and the FER model presented here is that in those works the xyz coordinates (t' was individually chosen) were a part of the reality (objective dimensions creating reality) so they were common for all bodies, while according to the FER model, the only common dimensions are abcd, whereas the FER directions interpreted as xyzt' dimensions are chosen individually for each observed body. In other words, for each case of observation, the dimensions of xyzt' are orthogonal to each other but they are rotated in FER in relation to the directions xyzt' describing another observed body. And this difference in the orientation of the xyzt’ dimensions relative to the orientation of the dimensions of other bodies is the sole source of the relativistic effects in uniform rectilinear motion.\nIf we describe phenomena as functions of the observed body's proper time and space dimensions of the observer, it is convenient to use complex notation to separate the phenomena that are the function of the absolute motion of the body along its trajectory from the phenomena associated with the relative motion of the bodies and the exchange of interactions along three spatial directions. We use this complex notation here in an unusual way, because we assume one dimension to be imaginary and the other three to be real. The imaginary direction is not the property of space but merely the property of observation. It means that by describing the observation of a body we describe its trajectory as an imaginary direction - only for the purpose of describing the observation of that particular body. For phenomena with spherical symmetry in space, the following description of coordinates can be used:", null, "(17)\nwhere", null, "(18)\nSo, in very general terms, if the observer during observation travels the distance dt along his trajectory, then in relation to the observed body he will travel a distance dr along directions interpreted by him as space dimensions, where the distance dr is defined by the formula (18), and the distance dt’ along imaginary direction determined by the proper time of the observed body.\nBy calculating the module of so defined distance (17), we will obtain the equation of space-time interval for the case of observation of a particular body - formula (6). Thus, introducing covariant notation is no longer necessary.\n\n### 11. Wave Structure of Particles and Description of Quantum Mechanics Phenomena\n\nIf particles move at constant velocity with respect to the absolute medium - FER – then we no longer have any obstacles to describing the particle directly as a wave propagating in the elastic medium; thus the FER can now be considered as such. The amplitude of the wave should disappear at infinite distance measured along the direction perpendicular to the trajectory of the particle/wave and it should have a frequency calculated from the dependence", null, "(19)\nI’m going to suggest the following formula describing the wave corresponding to this particle:", null, "(20)\nwhere a – the amplitude of wave\nt – the observer’s time described with the formula (17).\nWave is a function of the position of the particle on its trajectory in FER. If we want to describe this function as a function of the space-time coordinates (xyzt) of an observer then we can use the following relationship:", null, "(21)\nSubstituting (19) and (21) in the formula describing the wave in FER (20) we obtain:", null, "(22)\nAs we can see, the wave defined in the FER with the formula (20) after transformation to space-time coordinate system takes form of a well-known wave function, which is a solution of the Schrödinger equation, multiplied by the segment describing the amplitude distribution as a function of the distance from the particle (22). While the wave function in formula (22) is not directly measurable in the “classical” space-time, the corresponding wave in FER described by formula (20) describes the real deformation in the FER. So, the abstract wave functions known from the currently used model correspond to waves in FER. Instead of using complex and abstract tools of Quantum Mechanics we can solve problems of particles/waves interaction by examining the interactions of waves representing the particles in the FER, which can be treated here as an elastic medium in which the interactions propagate. The tools to solve these problems will be simpler and more intuitive than the analogous tools provided by Quantum Mechanics. Many of the problems that appear in Quantum Mechanics can be explained and described by the FER model in a much simpler way than in QM and the new approach can explain some enigmatic properties of particles.\nLet us start by looking at the function describing a particle as a wave in FER, using the form proposed by equation (20).\nThe function can be written as follows:", null, "(23)\nBearing in mind that imaginary values refer to the direction determined by the trajectory of the observed body, we see that the equation (23), describing a particle, describes transverse oscillations perpendicular to the trajectory of the particle (the real values) and longitudinal oscillations along the trajectory of the particle (the imaginary values). It is clear that the equation describing a particle in practice does not describe the vibrations but the rotation (or superposition of rotations) in plane (planes) formed by directions perpendicular to the trajectory of the particle and the direction determined by the particle’s trajectory. The amplitude of the oscillation is here at the same time the radius of rotation with the center in the center of the particle/wave. At the present stage a model of such a particle is not yet complete, but the fact that what we observe or interpret as waves is in practice the rotation, and the waves observed by us are only projections of this rotational movement on the directions interpreted by us as spatial dimensions, allows us to explain, in a trivially simple way, such properties of particle/wave as, for example, the spin.\nIf we use the formula for the angular momentum of the rigid body:", null, "(24)\nthen for a particle with the wave frequency described by the formula (19), the formula for the angular momentum takes the following form:", null, "(25)\nWhere T – period of oscillation of the particle/wave.\nIf we now assume that the velocity of rotation in the plane, e.g. xt', is", null, "(26)\nthen it follows that the angular momentum of a given particle is:", null, "(27)\nand it is directed along one of the space-dimensions. Thus, by registering a particle in the space-time, we observe it as a particle, described by a wave function that has an angular momentum. Such angular momentum does not have to be considered a mysterious property of particles - in this case, the angular momentum is a result of the actual rotation of the body/wave. The actual value of the angular momentum of the particle will be different than the one given in (27) - the particle structure may differ from the model shown here: the rotations may occur in differently oriented planes, the particle/wave may be a superposition of various waves, etc. This problem has not been sufficiently analyzed yet; however, as we can see, the model offers ways to obtain various solutions which will hopefully be consistent with the actual state of knowledge.\n\n### 12. Waves of Matter and the Time Flow\n\nThe representation of a body directly as a wave, with the wavelength/(period of oscillations) of the waves of matter (not in the sense of the de Broglie waves of matter; the problem will be described in more detail below) defined by the formula (19), propagating along one of the directions in the FER interpreted by the body as its time-dimension, gives a different view on the problem of time. By measuring time in everyday life or in laboratories, we always use oscillations - from the oscillation of the pendulum of the clock to atomic oscillations. In the case of presenting a particle as a wave, i.e. as oscillations of a medium, it is natural for the body to accept the number of oscillations as a measure of the particle’s proper time. So, if the wavelength (or period of oscillations) of particle/wave is equal to T then the particle's proper time can be represented as multiples of the periods of oscillations of the particle/wave", null, "(28)\nSince all trajectories are equivalent, identical particles moving along different rectilinear trajectories have identical periods and amplitudes of oscillations.\nThe measure of the time that flows in the particle’s system will not be the length of the trajectory traveled by that body in the FER but the number of the particle/wave oscillations on the route between the two points in the FER.\nIn this way, the definition of a particle as a wave naturally introduces the quantization of time, which is no longer a continuous but a discrete value - measured by the number of periods of body’s waves. The quantum of time for a given particle will be the period of oscillations of waves of matter defined by the formula (19).\nI will remind you that in addition to the time we perceive, which is measured by the number of particle/wave oscillations, absolute time is also introduced in the FER model. In practice, the absolute time corresponds to the distance traveled between two FER points, and for all bodies traveling between these points, the absolute time flow is identical. On the other hand, the number of oscillations – i.e. the measure of the proper time of the body - is different for each body and depends on the trajectory along which the body crossed that distance. A little more about this in the next chapter.\nExample: The quantized time dilation in case of twin paradox\nThe rule of observation of the relative time dilation was shown previously in Fig.1. The same situation for two identical particles/waves (with identical vibration periods) is shown in Fig.10.", null, "Figure 10. The situation is identical to that shown in Fig.1, however, the proper times of the reference frames of bodies are not expressed by the length of the trajectory but by the number of oscillations. For two identical bodies, the number of oscillations per unit of length of the trajectory is identical for both bodies. The observed time difference is the result of interpreting a direction perpendicular to the trajectory of the observed body as the space-dimension of the observer’s coordinate system\nNow, we can rewrite formulas (7) for the observed time dilation, for the case of quantized time, where the quantum of time is the period of body’s oscillation/wavelength equal to T. Then the times of bodies can be written in the following form:", null, "(29)", null, "(30)\nwhere", null, "is the number defining the time flow in the reference frame of observer \"i\" with the help of number of wave’s oscillation periods.\nIn this case, the observed dilation of time can be written\nfrom point of view of observer 1:", null, "(31)\nfrom point of view of observer 2:", null, "(32)\nNow, analogously to the description of the twin paradox presented in the chapter “Dilation of time and the twin paradox”, we can present the problem from Fig.8 with the help of time expressed by the number of periods of oscillations of particles - Fig. 11. As we can see, in the case of infinite acceleration corresponding to the movement of the particle from point A to point B in Fig.11, the oscillations of particle do not take place - so the time flowing in the reference frame of the particle is equal to zero for the arc AB. Thus, the time flowing in the reference frame of body 2, measured by the number of oscillations, will be shorter than the time in the reference frame of body 1.", null, "(33)\nIn practice, for non-inertial motions - as a conclusion from the Fig.11 - one should expect a decrease in the number of oscillations and extension of periods of oscillation along curved trajectories. And it is this extension of the periods of oscillations for the curved trajectory that is responsible for observing the dilation of time (lower number of oscillations) in the reference frames of the GPS system satellites or in the Hafele-Keating experiment [1, 2] (I am not taking into account the gravitational change of time here). In other experiments confirming the dilation of time phenomena, the most important factor determining the value of the time dilation is the change of velocity as shown in Fig.11, while the oscillation periods of the body do not change. Meanwhile, according to the TR, in all the cases described above, the time dilation is the result only of the linear velocity of the bodies. The extension of the oscillation period as a result of changing the direction of body/wave propagation (motion) in the FER is not yet completely explained and mathematically described. It will most likely be connected with the nature of the oscillations and with behavior of these oscillations when changing the direction of propagation of the oscillations - especially since the particle described by wave according to equation (20) is not limited to specific dimensions in space but it extends to infinity, so any change of direction will disturb the shape of the wave up to infinity, which will have to lead to the changing of the wave’s oscillation period of at different distances from the center of the body/wave. The illustration of this predicted mechanism is shown in Fig. 12. It probably results from the fact that in the region where the oscillation period ”T” is shorter (in Fig. 12 b the region below the segment AB), the energy of wave (described with the formula: E=h/T) increases, while in the region where the oscillation period is longer (in Fig 12 b the region over the segment AB), the energy of the wave decreases; this will result in shifting the center of the wave to the region of lower energies with longer oscillation periods. As we can see, the change of direction of motion of the wave in the four-dimensional space should cause deformation of the waves, which on the one hand causes the effect of time dilation, but on the other hand it must also cause tensions in the medium, therefore the change of direction of body/wave must be related to the occurrence of forces which we probably recognize as forces of inertia. Thus, the mechanism proposed in Fig. 12b most probably justifies the time dilation as well as the inertial forces and, in a simple way, shows the relationship between these two phenomena. The problem of mathematical description remains open, but the main idea is defined here and, in my opinion, finding a mathematical description of the oscillation - or rather the rotation of a medium - following the already known laws concerning such dilation of time and inertial forces is only a matter of time.", null, "Figure 11. The situation is identical to that shown in Figure 8, but here the time is presented as the number of body/wave oscillations. There are no oscillations along the AB curve, hence the time (number of oscillations) of body 2 is shorter than the time (number of oscillations) of body 1", null, "Figure 12. A wave propagating along a straight line is shown in Fig.a. In Fig.b, the same wave is propagating along a curve. The dots show the maximum amplitude of the wave. The AB distances on both drawings are identical but the time in the particle’s system, measured by the number of oscillations, is shorter in the reference system of a particle propagating along the arc. In Fig.a time is equal to 9 periods while in Fig.b - to 7 periods\nWe can see that the mechanism of the time flow in the body’s reference frame in motion is defined by the number of oscillations of the period, which in the case of inertial movements is constant while it is extended in the case of non-inertial motions. The decrease in the number of oscillations caused by the change in direction of velocity (Fig. 11) or caused by the change in the period of oscillations (Fig. 12) is detected as the time dilation.\n\n### 13. Energy of Particles and Energy of Macroscopic Bodies\n\nIf we consider the energy of macroscopic bodies it is easy to guess that if we want to obtain the known relationship between momentum, energy and the rest mass of the observed body (here equal to its rest energy), energy and momentum can be presented in the FER as vectors overlapping the trajectory of the observed body and the coordinates of the observer ‘s coordinate system, as shown in Fig.13.", null, "Figure 13. Diagram showing the relation between energy, momentum and rest energy (mass) of a body in the FER. The observed body moves along trajectory t’, an observer along trajectory t\nThus, the body’s energy observed in the observer’s reference frame relates to the rest energy of the body similarly to the relations between times of the observer and the observed body (7):", null, "(34)\nIf we now consider a particle as a wave - according to Fig.10 - we observe the change of time, but this change of time is related to the number of oscillations with a fixed period rather than to the change in observed oscillation period.\nIf a similar relation to (34) is to occur for the energy of the wave of matter defined by the formula", null, "(35)\nthen the observer must observe not the change in the number of oscillations but a change in the wavelength/oscillation period (these two concepts are, in the FER, equivalent) of the wave of matter.\nIf in case of motions of macroscopic objects we have chosen the directions perpendicular to the trajectory of an observed body as the space axes of the observer, then in case of interference of waves responsible (according to the FER model) for the occurrence of quantum effects, we will have to adopt another approach.\nIf the dependence (34) is to be conserved, then for a wave moving relative to the observer’s coordinate system, the space dimensions of the observer’s coordinate system should be perpendicular to the trajectory of the observer, and not to the trajectory of the observed body, as in the case of macroscopic motions. The described situation is illustrated in Fig. 14. The reasons such a mechanism needs to be applied here still require a proper explanation, but for now, in order to preserve the coherency of the model, we need to accept such an assumption. Therefore, for all further considerations regarding direct interactions of/with the waves of matter, we are going to use coordinate systems in which the space directions are perpendicular to the time axis of an observer.", null, "Figure 14. In case of direct interactions of bodies/waves (interference), we describe the energy of the body/wave in the observer's rest frame (the observer's spatial axis is perpendicular to the observer's trajectory)\nIn this case, we can describe the particle’s energy as follows:\nThe rest energy of observed particle", null, "(36)\nThe energy of a particle in the observer’s frame according to Fig. 14 can be expressed with the formula:", null, "(37)\nWe should remember that the direction in the FER that we interpret as a space dimension is not constant but depends on the way of performing the observation or, in other words, from the manner in which the interactions are exchanged. The exact interpretation of the situation shown in Figure 14 needs to be developed further; however, accepting such a description allows to bind the wave character of particle described above with the relativistic dependences between motion and energy in macroscopic cases.\nAt the same time, it should be noted that to determine the energy of a particle/wave we must know its trajectory in FER, because the energy is defined by the angle between the trajectories of the particle and the observer (37). For this we must observe at least one full cycle - equal to the period of oscillation.\nThus, the observation time t must be longer than the wave/particle period:", null, ", and because", null, ", the following dependence must be satisfied:", null, "(38)\nThis is the property that results directly from the wave nature of the particle and from the fact that the energy (velocity) can be determined by knowing the angle of inclination of trajectory of the observed body to the observer’s trajectory.\nToo short time of measurement- shorter than the period of wave/particle oscillation - results in a less accurate determination of trajectory and hence of the energy of particle.\n\n### 14. Momentum of Particles/Waves Versus Momentum of Macroscopic Particles\n\nIf we are using a unit system in which c = 1, then, according to the situation shown in Fig. 13, the momentum of the particle should be defined by the relation:", null, "(39)\nwhich in the case of non-relativistic particles, with which we deal in typical experiments and applications, may be written as:", null, "(40)\nWhere the observed wavelength λ is equal to:", null, "(41)\nThe wavelength λ described with the formula (41) is already known as the de Broglie waves of matter. According to the FER model the de Broglie waves of matter are the intersection of the surfaces of constant phases of the waves of matter described by formulas (19) and (20) with the space-dimensions of the observer’s reference frame, as shown in Fig. 15. If we want to measure the momentum and position of the particle/wave then from the fact that to determine the trajectory, the time of measurement must be greater than the oscillation period, it follows that the observed distance in the xyz space must be greater than", null, "or", null, "which means that if", null, "then:", null, "(42)", null, "Figure 15. The intersection of the surfaces of constant phases of the waves of matter of observed body with the spatial dimensions of the observer's system gives the de Broglie waves of matter, the length of which is a function of velocity, and therefore also a function of momentum, of the particle/wave\nSo, according to the formulas (38) and (42), analogous to Heisenberg's inequality, if we are considering the particle/wave, then defining the trajectory along which this wave propagates requires measurements that take into account the distance equal to or greatfer than the wavelength of this wave, because for shorter distances we are not able to determine its trajectory with sufficient accuracy.\n\n### 15. Particle Size, Probability, Particle Diffraction on the Slit\n\nAs shown above, while analyzing the wave/particle structure we deal with several values. For the time being, we will be using these values to describe an electron. They are only an example, because if the distribution of the amplitude of the electron’s wave differs from the distribution given for the simple wave described above (20), then these values will also vary.\n1. The radius “a” in the formulas (20), (23), in the case of a projection of rotation on space-dimensions, is the amplitude of oscillations. For an electron, the amplitude \"a\" is equal to approx. 4E-13m (computed on the base of formulas (19) and (26)).\n2. If we substitute the values corresponding to this amplitude to the formula (20) determining the amplitude of the wave as a function of distance, we will get the width of the amplitude distribution at mid-height of about 4E-20m. This distribution was chosen as the simplest one for the purposes of the description, but it is expected that the shape of amplitude will differ from the one assumed in formula (20).\n3. If we calculate the length/period of the electron wave from the dependence", null, "for FER where c=1, then the length of the wave of matter will be equal to 2,5E12m – that is, equal to the circumference of the circle defined by the radius “a” calculated in point 1 (from the condition that the linear velocity on a circle of radius a is equal to 1).\nNote that the particle’s size measured along the direction perpendicular to the particle’s trajectory, for the case of an electron, is about 4E-20m while the wavelength of matter is approximately. λ0=2,5E-12m. These dimensions will allow us to determine the behavior of an electron on a slit.\nLet consider a two-dimensional plane on which we have a designated slit and an electron’s trajectory perpendicular to the slit. The observer's time axis is perpendicular to this plane – Fig.16a. The particle is shown as a wave. In the case of the three-dimensional space shown in Fig.16, we have two directions interpreted as space dimensions - xy - and the third direction interpreted as time-dimension. As the time axis, we took the trajectory of the slit in the graph. The particle’s trajectory is inclined to the slit trajectory at an angle ϕ, so the particle’s velocity relative to the slit is", null, "– Fig.16b.\nIn the 3-dimensional case presented on the diagram, the surfaces of the constant phase for the wave are planes perpendicular to the trajectory of the particle. The wavelength of matter determined from the formula E=hν is equal to the wave’s oscillation period T. The projection of a surface of constant phase of a wave on the XY plane gives the de Broglie waves with wavelength λ=T/sinϕ on the plane XY (Fig. 16 b, 17, formula (41)).", null, "Figure 16. A particle/wave passing through a slit. Fig. a shows the view in the xy plane, in Fig. B, the view in the xt plane. The time axis is chosen as parallel to the trajectory of the slit. Projection of the wavelength T of matter on the xy plane (fig. b) is the de Broglie’s wave of matter - identical like in Fig.15\nIt should be noted that while the wavelength observed in our space depends on the momentum of the particle, the particle size measured along the direction perpendicular to the particle’s trajectory resulting from the wave amplitude distribution is constant and many orders of magnitude smaller than the wavelength of the particle in space (see point 2 above). This means that if a particle falls on a slit, the diffraction result is determined by two factors - the de Broglie wavelength of the particle resulting from the momentum of the particle, and the location of the maximum amplitude of particle/wave relative to the slit.\nThe described situation is shown in Fig.17, where the dot indicates the area of maximum amplitude (which, as I wrote above, is many orders of magnitude smaller than the wavelength, and therefore also smaller than the size of the gap which in Fig.17 is comparable to wavelength). Changing the position of the maximum amplitude relative to the slit will result in different intensity distributions of the diffraction image for single particles (Fig. 17a and 17b). It has nothing to do with the probability being some mysterious feature of a particle. This is simply a result of the structure of particle treated as a wave in FER.", null, "Figure 17. The dependence of image behind the slit for the particle passing through the slit as shown in Fig.16 from the position of the maximum amplitude relative to the slit. In Fig.16a, the maximum amplitude of the particle is in the center of the slit, in Fig.16b, the maximum amplitude of particle is shifted towards the edge of the slit\n\n### 16. Particles and Fields\n\nThe described particle model as a wave in a medium such as FER allows for a different look on the problem of fields and particles. The wave amplitude distribution given in formula (20) was chosen at random and would most likely have to be adjusted to the actual particle properties. However, according to amplitude distribution, a small portion of the particle appears to be a region with an amplitude much larger than in the rest of the region, but the disturbance of space extends to infinity. It means that it will probably be possible to describe the entire wave as roughly divided into two areas: the center of the wave treated as a particle, and the remote region treated as a field. Particles, even very distant, can interact with each other through the space disturbances that they generate, and the space, as one can expect, should affect the particle system in a way that decreases the total energy of the system. Such interaction should have the properties of a field. At this stage, it is only a concept not yet supported by calculations, but it is to be expected that we will be able to find such amplitude distribution and the parameters of the space treated as a kind of elastic medium that the interactions between the waves at long distances will have the properties of fields.\nIf we treat the FER as an elastic medium, the energy of oscillation of this medium for slight deformation in the case of oscillation in one direction should be proportional to the square of amplitude of oscillations. In the case of a particle described as a wave, the energy is determined by the formula", null, "(43)\nIf we use the formula for the fine-structure constant, then in the unit system where c = 1, the energy equation will take the following form:", null, "(44)\nThus, according to the formula (44), if FER is assumed to be an elastic medium, the value of the electrical charge should be related to the deformation of the medium - compression or stretching. Compression or stretching of the space would probably determine in this case the sign of the electric charge. We therefore have a proposal of the concept of electric charge treated as deformation of space. This is a suggestion indirectly based on the assumptions of the model. Time will tell if this suggestion is justified.\n\n### 17. Conclusions\n\nThe idea of a new description of reality presented here is based on accepting a model of reality in which the \"true\" reality is as simple as possible, while our perception makes us interpret different directions in this space as our space-time dimensions. Directions interpreted as space-time dimensions are not the objective properties of reality but depend on the bodies currently observed. This is logical because we learn about the existence of space, the number and structure of dimensions, indirectly - through observation of the surrounding particles. The idea to bind the space-dimension of the observer not to the space but to the currently observed body allowed to achieve a much simpler description of the relativistic phenomena and allowed to explain, within a single model, many of the phenomena which have so far been described with different models. For instance, the mechanism mentioned above explains the limitation of the speed value to the speed of light, the constancy of the speed of light, the time dilation, the phenomenon of the recession of galaxies, and removes the singularities occurring in the previous models. At the same time, the interpretation of the relative motion of the body as an angle of inclination between the trajectories in absolute space allows to connect the absolute movement of particles relative to FER along their trajectories (time flow) with the relative motion of bodies (angle between trajectories), explains the Mach principle, and allows to describe the particle directly as a wave, to which the projection on observed space-time (xyzt) gives the wave function.\nMoreover, the description of the particle as a wave allows to connect Quantum Mechanics with the phenomena described so far by the Theory of Relativity, explain the quantum nature of time in a simple way, gives a simple interpretation of Heisenberg’s uncertainty principle, and gives the basis for unifying description of particle and field. Simultaneously, the conclusions allow a simple interpretation of the electric charge as deformation of space. The proposed approach is not complete yet. Not all ideas have been described mathematically. However, all the ideas and conclusions described here make a coherent and closed model in which all elements support each other. The issue of mathematical description of many phenomena is open, but it is only a matter of solving the problems unambiguously defined in this work.\nIn this paper, I am proposing a new model of reality. This model still requires a lot of work, such as finding the particle amplitude distribution, specifying the properties of space, describing wave interactions in a way that explains the EM fields and gravity. On the other hand, accepting a new model will result in changing the mathematical apparatus used to describe reality. There will be no need for covariant notation or for the use of operators used in TR and QM up until now. Of course, TR and QM tools can still be used for many years to describe physical phenomena, but one needs to be aware that the range of phenomena described by these tools will be limited and not as broad as the description proposed by the new model. Accordingly, the description of the reality proposed in this paper may not be accepted by many physicists accustomed to the tools already used to describe reality. However, I hope that, even though adopting a new model may lead to students knowing more about a new theory than their professors for a while, the theory will be taken seriously and at least tested experimentally , which is currently possible with the use of available experimental systems and diagnostic tools.\n\n### References\n\n W. Nawrot \"The Hafele and Keating Paradox\" - Phys. Ess. 17, 518 (2004). W. Nawrot, \"The Hafele-Keating paradox - Serious problems of the special theory of relativity (SRT)?\" Phys. Ess. 27, 4, pp 598-600 (2014). W. Nawrot \"Proposal of simpler description of SRT\" - Galilean Electrodynamics 18, 43-48 (2007). W. Nawrot, \"New philosophy of Aether in Euclidean Reality model and interpretation of indications of Sagnac and MM interferometers\" Proceedings of the 20 NPA Minneapolis, MN USA 2013. W. Nawrot \"Is the Lorentz Transformation a physically correct solution of the space-time interval equation?\" - Galilean Electrodynamics Vol. 20, Special Issue 2, 34-37 (2009). Rob van Linden, “Dimensions in Special Relativity Theory”, Galilean Electrodynamics 18, 12-18 (2007). W. Nawrot, \"Proposal of experiment disproving the Theory of Relativity\" Accepted for publication in the Galilean Electrodynamics. Available at http://euclideanreality.com/pdf/DisproofOfSTR.pdf. J. Velasco, J. Perez-Peraza, A. Gallegos-Cruz, M. Alvarez-Madrigal, A. Faus-Golfe, A. Sanchez-Hertz, “σpptot Estimations At Very High Energies” arXiv: hep-ph/9910484v1 (1999). Hans Montanus “Special relativity in an absolute Euclidean Space-Time” (Physics Essays, vol. 4, nr 3, 1991). Jose Almeida “An alternative to Minkowski space-time” (arXiv:gr-qc/0104029, 2001) Giorgio Fontana “The Four Space-times Model of Reality” (arXiv.org, physics/0410054A). W. Nawrot \"The structure of time and the wave structure of the matter\" - Galilean Electrodynamics 18, 49-53, (2007). W. Nawrot \"Four-Dimensional Euclidean Reality - The basic properties of the model\" Proc. International Scientific Congress \"Fundamental Problems of Natural Science and Engineering\" Saint-Petersburg, Russia 2008. W. Nawrot \"Euclidean Reality Theory - Spectacular Conclusions and New Problems\" - Proc. International Scientific Congress \"Fundamental Problems of Natural Science and Engineering\" Saint-Petersburg, Russia 2008. W. Nawrot \"Recession of galaxies, simpler explanation\" - Galilean Electrodynamics Vol 20, Special Issue 2, 38-40 (2009). W. Nawrot, \"Euclidean model of the space-time - is the reality exactly as we can observe it?\" - Mathematics, Physics and Philosophy in the Interpretations of Relativity Theory, Budapest, 4 - 6 September 2009. W. Nawrot, \"Explanation of twin paradox according to the Euclidean Reality Model\" Proceedings of the 20 NPA Minneapolis, MN USA 2013." ]
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https://www.studypug.com/pre-algebra/determine-probabilities-using-tree-diagrams-and-tables
[ "# Determining probabilities using tree diagrams and tables\n\n### Determining probabilities using tree diagrams and tables\n\nTables and tree diagrams are useful tools to calculate probabilities. With them, you can list all the possible outcomes of an event (sample space) in a clear and easy to understand way. Therefore, we can determine the probabilities of events effectively.\n\n#### Lessons\n\n• Introduction\na)\nIntroduction to Probability\n• What is probability?\n• How to write probability as a fraction, decimal, and percent?\n• How to draw a tree diagram?\n\nb)\nHow to draw a tree diagram?\n\n• 1.\nKen flips a coin and draws out a marble from a bag with 5 marbles of different colours: green, blue, red, orange and yellow.\na)\nDraw a tree diagram to show the sample space.\n\nb)\nWhat is the probability of P(H, R)?\n\nc)\nWhat is the probability of not getting the head?\n\n• 2.\nTwo standard six-sided dice are rolled.\na)\nDraw a table to display the sample space.\n\nb)\nWhat is the probability of P(doubles)?\n\nc)\nWhat is the probability of P(sum less than 10)?\n\nd)\nWhat is the probability of P(two even numbers)?\n\n• 3.\nAssume that there will only be rain or sunshine in the next 4 days. Draw a table to display the sample space. Determine the probability of:\na)\nThere is rain 4 days in a row.\n\nb)\nThere is rain or no rain 4 days in a row.\n\nc)\nThere is rain in any 2 days.\n\nd)\nThere is rain in at least 1 day." ]
[ null ]
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http://www.scriptspot.com/forums/3ds-max/general-scripting/lighting-animation-dancing-lights
[ "# Lighting animation, dancing lights\n\nhi everybody, i have many lights in a scene that need to turn on and off over time, but not the same time , there should be variation or time offset for each one of them … this simple maxscript code is what I have ended up with as a test but can’t figure out about time variation for each\n… any help is much appreciated … thanks …\n\npoint_lights = selection\n\nwith animate on (\n\nfor i = animationRange.start to animationRange.end do\n\n(\n\nv = 1\n\nsliderTime = i\n\nt = slidertime as float\n\nf = sin (t * 0.04) * v\n\nfor j = 1 to point_lights.count do\n\n( --ran = (random 1 to 9) * 0.1\n\npoint_lights[j].multiplier = f\n\n)\n\n)\n\n)" ]
[ null ]
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http://www.moomoomath.com/Probabilities-and-Percents.html
[ "", null, "", null, "Master the 7 pillars of school success\n\nThis is an \"or\" problem so you will add, and you have for white shirts, and two black shirts, and ten shirts total.", null, "Dependent events depend on the actions of the previous event. The result of one event has an impact on other events.\n\nDependent events using \"and\"\n\nUse the formula: P(A and B) =P(A) x P(B, given A)\n\nFor example: If you have three red marbles, and three blue marbles. What are the chances of picking a blue marble, and then a red marble? Because the marbles are not replaced each time, there is a smaller number of marbles which will impact the next event.\n\nIndependent events using \"or\"\nUse the formula: P(A or B ) = P(A) + P(B)\n\nFor example:\nWhat is the probability of rolling a 5 the first roll, or a 6 the second time?", null, "", null, "1/6        +   1/6      =2/6 =1/3\nRoll 1         Roll 2\nadd the fractions because it is an \"or\" event\nTherefore, you will have a 1/3 chance of rolling a 5 or a 6\nIndependent events involving “and”\n\nWhen you have independent events along with the statement “and” use the formula\nP(A and B) = P(A) x P(B)\n\nPlease note P( ) means the probability of an event. The event is placed in the ( ) for example\nWhat is the probability of rolling a 5 on a six sided die can be written P(5)", null, "", null, "", null, "", null, "", null, "1. Use this formula:    Positive Outcomes\nTotal Outcomes\n2. Reduce the fraction for your probability.\n\n3. In order to convert it to a percent, divide the numerator ( top number) by the denominator ( bottom number) and multiply by 100.\n\nExample 1 : If you have 5 red marbles, 2 blue marbles, and 3 green marbles. What is the probability you will pick a green marble?\n\nStep 1. Use the formula:\n\nStep 2. Divide the numerator by the denominator   3/10 = .3\n\nStep 3. Multiply by 100 to get the percent.          .3 x 100 = 30 %\n\n# Probability Examples\n\nPositive outcomes  (which is green marbles) = 3\nTotal Outcomes                                      5 + 2 + 3 = 10\n\n## Probability of Independent Events\n\nIndependent Events:  Events are independent if the result of the second event is not affected by the actions of the first event.\nYou may think of independent events as isolated events.\n\nFor example: Flipping a coin. Each flip of the coin has no impact on the next flip.\nIf you have three red marbles, and three blue marbles placed on a table. What are the chances of picking a blue marble, and then a red marble if the marbles are replaced each time? Because the marbles are replaced each time they have no bearing on the next event.", null, "", null, "## Probability of Dependent Events", null, "Becky has a deck cards.  What is the probability that she will draw a face card, then a red card with out replacement?\nProbability of “or” with dependent events.\n\nP(A or B ) = P(A) + P(B) – P(A and B )\n\nBob has several shirts of different colors. In a box he has 2 yellow with pockets, 2 red, 4 white with pockets, and 2 black.\n\nWhat is the probability of randomly picking a white shirt, or a black shirt.", null, "", null, "What is the probability of randomly choosing a star from Group 1, and an arrow from group 2?\n\nStep 1.  Multiply the probability of the group 1 times the probability of group 2. Group one has four stars, and seven total objects. Group two has three arrows out of six objects total.\n4/7 x 3/6\n\nStep 2.  With \"and\" problems you multiply\n4/7 x 1/2 = 4/14\n\nStep 3.  Reduce the fraction\n= 2/7\n\n= 2 ÷ 7\n\n= 0.285714\n\n0.285714 x 100 = 28.5714%\n\nThe probability of choosing a star and an arrow equals 28.57%.\n\nVideo Tutorial Probability of Independent Events\nWhat is the probability of choosing a white shirt, or a shirt with a pocket?\n\n​4/10 +2/10 =6/10\n=3/5 = .60\n= .60 *100 = 60%\n4/10+6/10-4/10= 6/10\n=3/5= .60\n=.60*100 = 60%\nVideo Answer to the last two problems\n3/6 x 3/5 =9/30 =3/10= 30%\n\nYou do not replace the marbles each time so when you make  the second pick you only have 5 marbles.\n12/52 x12/51 = 144/2652\n= 12/221 = .o542\n= .0542 x 100 = 5.42%\nVideo Solution to Dependent events with \"and\"\nWhat is probability? In simple terms it is how \" likely\" an event will occur. For instance, if you flip a coin how likely is it you will flip a heads ? In order to calculate probability follow these steps. span>" ]
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https://toutiao.sanhao.com/news-detail-42607.html
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[c_tagid] => 26 [c_tagname] => 高中家长 [c_tag_enname] => gaozhongjiazhang [c_tag_pid] => 6 [c_sort] => 0 ) => Array ( [c_tagid] => 3 [c_tagname] => 教学经验 [c_tag_enname] => jsb [c_tag_pid] => 7 [c_sort] => 0 ) => Array ( [c_tagid] => 113 [c_tagname] => 优师支招 [c_tag_enname] => mingshizhizhao [c_tag_pid] => 7 [c_sort] => 0 ) => Array ( [c_tagid] => 124 [c_tagname] => 互动专区 [c_tag_enname] => hudongzhuanqu [c_tag_pid] => 7 [c_sort] => 0 ) => Array ( [c_tagid] => 114 [c_tagname] => 热门专题 [c_tag_enname] => zhuanti [c_tag_pid] => 8 [c_sort] => 0 ) => Array ( [c_tagid] => 99 [c_tagname] => 三好资讯 [c_tag_enname] => news [c_tag_pid] => 9 [c_sort] => 0 ) => Array ( [c_tagid] => 116 [c_tagname] => 公益巡讲 [c_tag_enname] => gonyixunjiang [c_tag_pid] => 9 [c_sort] => 0 ) => Array ( [c_tagid] => 117 [c_tagname] => 战略发布 [c_tag_enname] => zhanluefabu [c_tag_pid] => 9 [c_sort] => 0 ) => Array ( [c_tagid] => 125 [c_tagname] => 校长论坛 [c_tag_enname] => xzlt [c_tag_pid] => 9 [c_sort] => 0 ) => Array ( [c_tagid] => 126 [c_tagname] => 学前学普 [c_tag_enname] => putonghua [c_tag_pid] => 9 [c_sort] => 0 ) )\n\n# 2020年国庆中秋长假,初三数学学科复习方法建议", null, "初中数学 10-01 浏览量: 分享:", null, "### 会员评论评论:0", null, "" ]
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https://percent-of.com/calculate/what-is-8-of-8419/
[ "# We use percentages in almost everything.\n\nPercentages are a very important part of our daily lives. They are used in Economics, Cooking, Health, Sports, Mathematics, Science, Jewellery, Geography, Medicine and many other areas.\n\n## Percent of Calculator\n\nCalculate percentage of X, quick & simple.\n\n%\n?\n\n8% of 8419 is:\n673.52\n\n## Percent of - Table For 8419\n\nPercent of Difference\n1% of 8419 is 84.19 8334.81\n2% of 8419 is 168.38 8250.62\n3% of 8419 is 252.57 8166.43\n4% of 8419 is 336.76 8082.24\n5% of 8419 is 420.95 7998.05\n6% of 8419 is 505.14 7913.86\n7% of 8419 is 589.33 7829.67\n8% of 8419 is 673.52 7745.48\n9% of 8419 is 757.71 7661.29\n10% of 8419 is 841.9 7577.1\n11% of 8419 is 926.09 7492.91\n12% of 8419 is 1010.28 7408.72\n13% of 8419 is 1094.47 7324.53\n14% of 8419 is 1178.66 7240.34\n15% of 8419 is 1262.85 7156.15\n16% of 8419 is 1347.04 7071.96\n17% of 8419 is 1431.23 6987.77\n18% of 8419 is 1515.42 6903.58\n19% of 8419 is 1599.61 6819.39\n20% of 8419 is 1683.8 6735.2\n21% of 8419 is 1767.99 6651.01\n22% of 8419 is 1852.18 6566.82\n23% of 8419 is 1936.37 6482.63\n24% of 8419 is 2020.56 6398.44\n25% of 8419 is 2104.75 6314.25\n26% of 8419 is 2188.94 6230.06\n27% of 8419 is 2273.13 6145.87\n28% of 8419 is 2357.32 6061.68\n29% of 8419 is 2441.51 5977.49\n30% of 8419 is 2525.7 5893.3\n31% of 8419 is 2609.89 5809.11\n32% of 8419 is 2694.08 5724.92\n33% of 8419 is 2778.27 5640.73\n34% of 8419 is 2862.46 5556.54\n35% of 8419 is 2946.65 5472.35\n36% of 8419 is 3030.84 5388.16\n37% of 8419 is 3115.03 5303.97\n38% of 8419 is 3199.22 5219.78\n39% of 8419 is 3283.41 5135.59\n40% of 8419 is 3367.6 5051.4\n41% of 8419 is 3451.79 4967.21\n42% of 8419 is 3535.98 4883.02\n43% of 8419 is 3620.17 4798.83\n44% of 8419 is 3704.36 4714.64\n45% of 8419 is 3788.55 4630.45\n46% of 8419 is 3872.74 4546.26\n47% of 8419 is 3956.93 4462.07\n48% of 8419 is 4041.12 4377.88\n49% of 8419 is 4125.31 4293.69\n50% of 8419 is 4209.5 4209.5\n51% of 8419 is 4293.69 4125.31\n52% of 8419 is 4377.88 4041.12\n53% of 8419 is 4462.07 3956.93\n54% of 8419 is 4546.26 3872.74\n55% of 8419 is 4630.45 3788.55\n56% of 8419 is 4714.64 3704.36\n57% of 8419 is 4798.83 3620.17\n58% of 8419 is 4883.02 3535.98\n59% of 8419 is 4967.21 3451.79\n60% of 8419 is 5051.4 3367.6\n61% of 8419 is 5135.59 3283.41\n62% of 8419 is 5219.78 3199.22\n63% of 8419 is 5303.97 3115.03\n64% of 8419 is 5388.16 3030.84\n65% of 8419 is 5472.35 2946.65\n66% of 8419 is 5556.54 2862.46\n67% of 8419 is 5640.73 2778.27\n68% of 8419 is 5724.92 2694.08\n69% of 8419 is 5809.11 2609.89\n70% of 8419 is 5893.3 2525.7\n71% of 8419 is 5977.49 2441.51\n72% of 8419 is 6061.68 2357.32\n73% of 8419 is 6145.87 2273.13\n74% of 8419 is 6230.06 2188.94\n75% of 8419 is 6314.25 2104.75\n76% of 8419 is 6398.44 2020.56\n77% of 8419 is 6482.63 1936.37\n78% of 8419 is 6566.82 1852.18\n79% of 8419 is 6651.01 1767.99\n80% of 8419 is 6735.2 1683.8\n81% of 8419 is 6819.39 1599.61\n82% of 8419 is 6903.58 1515.42\n83% of 8419 is 6987.77 1431.23\n84% of 8419 is 7071.96 1347.04\n85% of 8419 is 7156.15 1262.85\n86% of 8419 is 7240.34 1178.66\n87% of 8419 is 7324.53 1094.47\n88% of 8419 is 7408.72 1010.28\n89% of 8419 is 7492.91 926.09\n90% of 8419 is 7577.1 841.9\n91% of 8419 is 7661.29 757.71\n92% of 8419 is 7745.48 673.52\n93% of 8419 is 7829.67 589.33\n94% of 8419 is 7913.86 505.14\n95% of 8419 is 7998.05 420.95\n96% of 8419 is 8082.24 336.76\n97% of 8419 is 8166.43 252.57\n98% of 8419 is 8250.62 168.38\n99% of 8419 is 8334.81 84.190000000001\n100% of 8419 is 8419 0\n\n### Here's How to Calculate 8% of 8419\n\nLet's take a quick example here:\n\nYou have a Target coupon of \\$8419 and you need to know how much will you save on your purchase if the discount is 8 percent.\n\nSolution:\n\nAmount Saved = Original Price x Discount in Percent / 100\n\nAmount Saved = (8419 x 8) / 100\n\nAmount Saved = 67352 / 100\n\nIn other words, a 8% discount for a purchase with an original price of \\$8419 equals \\$673.52 (Amount Saved), so you'll end up paying 7745.48.\n\n### Calculating Percentages\n\nSimply click on the calculate button to get the results of percentage calculations. You will see the result on the next page. If there are errors in the input fields, the result page will be blank. The program allows you to calculate the difference between two numbers in percentages. You can also input a percentage of any number and get the numeric value. Although it is a simple calculator, it can be very useful in many scenarios. Our goal is to give you an easy to use percentage calculator that gives you results you want fast.\n\nPercentage in mathematics refers to fractions based in 100. It is usually represented by “%,” “pct,” or “percentage.” This web app allows a comma or dot as a decimal separator. So you can use both freely.\n\nWe have provided several examples for you to use. You can use the examples to feed in your own data correctly. We hope you will find this site useful for calculang percentages. You can even use it for crosschecking the accuracy of your assignment results.\n\nNB. Americans use “percent,” which the British prefer “per cent.”\n\n#### Examples\n\nExample one\n\nCalculate 20% of 200?\n20% of 200 =____\n(200/100) x 20 = _____\n2 x 20 = 40\n\nIt is quite easy. Just divide 200 by 100 to get one percent. The result is 2. Then multiply it by 20 ( 20% = 20 per hundred) = 20 x 2 = 40\n\nExample two\n\nWhat percentage of 125 is 50?\n\n50 = ---% of 125\n50 x (100/125) = 40%\n\nGet the value of one percent by dividing 100 by 125. After that, multiply the value by 50 to get the percentage value of 50 units, which is 40% That is how to calculate the percentage.\n\nExample three\n\nWhat is the percentage (%) change (increase or decrease) from 120 to 150?\n\n(150-120) x (100/120) = 36\n\nSince 150 represents 100%. One percent will be equal to 100/150. 150-120 is 30. Therefore, 30 units represents 30 x (100/150) = 36 % This is how to calculate the percentage increase.\n\nwe do not use a percentage at all times. There are scenarios where we simply want to show the ratio of numbers. For instance, what is 20% of 50? This can also be interpreted as 20 hundredths of 50. This equates to 20/100 x 50 = 10.\n\nYou can use a calculation trick here. Anyme you want to divide a number by 100, just move the decimal two places to the left. 20/100 x 50 calculated above can also be writen as (20 x 50)/100. Since 20x 50 =1000. You can simply divide 1000 by 100 by moving two decimal places to the left, which gives you 10.\n\nIn another scenario, you want to calculate the percentage increase or decrease. Supposing you have \\$10 and spend \\$2 to buy candy, then you have spent 20% of your money. So how much will be remaining? All the money you have is 100%, if you spend 20%, you will have 80% remaining. You can simply use the percentage reduction tool above to calculate this value.\n\n#### Origin\n\nThe word percent is derived from the Latin word percenter which means per hundred, and it is designated by %" ]
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https://www.digglicious.com/uncategorized/what-is-modeling-and-simulation-in-matlab/
[ "## What is modeling and simulation in MATLAB?\n\nModel and simulate dynamic system behavior with MATLAB, Simulink, Stateflow, and Simscape. Modeling is a way to create a virtual representation of a real-world system that includes software and hardware.\n\n### What is system Modelling and simulation?\n\nModeling and simulation (M&S) is the use of a physical or logical representation of a given system to generate data and help determine decisions or make predictions about the system. M&S is widely used in the social and physical sciences, engineering, manufacturing and product development, among many other areas.\n\n#### What is MATLAB simulation?\n\nAdvertisements. Simulink is a simulation and model-based design environment for dynamic and embedded systems, integrated with MATLAB. Simulink, also developed by MathWorks, is a data flow graphical programming language tool for modelling, simulating and analyzing multi-domain dynamic systems.\n\nWhat do you mean by system Modelling?\n\nSystem modeling is the process of developing abstract models of a system, with each model presenting a different view or perspective of that system. It is about representing a system using some kind of graphical notation, which is now almost always based on notations in the Unified Modeling Language (UML).\n\nThe Simulink approach is based on time based and multi rate system. SO that will be useful for HDL code generation. Whereas, MATLAB is for the mathematical based algorithm development and which will not consider the time while in simulation (independent of time). Simulink is graphical and more interactive to the user.\n\n## What is MATLAB & Simulink used for?\n\nSimulink provides a graphical editor, customizable block libraries, and solvers for modeling and simulating dynamic systems. It is integrated with MATLAB®, enabling you to incorporate MATLAB algorithms into models and export simulation results to MATLAB for further analysis.\n\n### What are the 4 types of system models?\n\nTypes of systems modeling\n\n• Functional modeling.\n• Systems architecture." ]
[ null ]
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https://site.financialmodelingprep.com/weighted-average-cost-of-capital/RBBN
[ "# Weighted Average Cost Of Capital\n\n#### \\$3.36\n\n+0.06 (+1.82%)\n###### DCFDCF Levered\nShare price \\$ 3.36 0.953 147.57 14.87 3.04% 7.290 442.87 495.85 938.73 47.18 52.82\n\nThere are a number of methods that can be used to determine discount rates. A good approach – and the one we’ll use in this tutorial – is to use the weighted average cost of capital (WACC) – a blend of the cost of equity and after-tax cost of debt. A company has two primary sources of financing – debt and equity – and, in simple terms, WACC is the average cost of raising that money. WACC is calculated by multiplying the cost of each capital source (debt and equity) by its relevant weight and then adding the products together to determine the WACC value." ]
[ null ]
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https://uk.mathworks.com/help/ident/ug/line-fitting-with-online-recursive-least-squares-estimation.html
[ "# Line Fitting with Online Recursive Least Squares Estimation\n\nThis example shows how to perform online parameter estimation for line-fitting using recursive estimation algorithms at the MATLAB command line. You capture the time-varying input-output behavior of the hydraulic valve of a continuously variable transmission.\n\n### Physical System\n\nThe system is a continuously variable transmission (CVT) driven by a hydraulic valve, inspired by reference . The valve pressure is connected to the CVT which allows it to change its speed ratio and to transmit torque from the engine to the wheels. The input-output behavior of the valve can be approximated by:\n\n`$y\\left(t\\right)=k\\left(t\\right)u\\left(t\\right)+b\\left(t\\right)\\phantom{\\rule{0.2777777777777778em}{0ex}}\\phantom{\\rule{0.2777777777777778em}{0ex}}for\\phantom{\\rule{0.2777777777777778em}{0ex}}\\phantom{\\rule{0.2777777777777778em}{0ex}}\\frac{-b\\left(t\\right)}{k\\left(t\\right)}`\n\nHere, t is the current time, y(t) is the valve pressure in bar, u(t) is the unitless input in the range of [0, 1]. The condition $\\frac{-b}{k} is the dead-band of the valve.\n\nThe slope, k(t), and offset, b(t), depend on the system temperature. They vary as the system warms up from cold start to typical operating temperature. You want to estimate k(t) and b(t) based on noisy measurements of u(t) and y(t).\n\n### Data\n\nThe true slope and offset parameters are k(0)=70 and b(0)=-15 at time t=0s. At t=50s the engine starts. The parameters vary over time until they reach k(950)=50 and b(950)=-13 at t=950s. The sample time is Ts=0.1s.\n\nThe content of the input signal u is critical for parameter estimation. Consider a case where u, and hence y, is constant. Then there are infinitely many k and b values that satisfy y = k u + b. u(t) must be persistently exciting the system for successful estimation of k(t) and b(t). In this example, the input u:\n\n• is zero from t=0s until t=50s.\n\n• has step changes to 0.40, 0.45, 0.50, 0.55, 0.60, 0.55, 0.50, 0.45, 0.40 every 100s, from t=50s until t=950s.\n\n• a Gaussian random variable with zero mean, 0.02 standard deviation was added at each time step from t=50s until t=950s to provide extra excitation of system dynamics for identification purposes.\n\nThe output is generated with the aforementioned true values of k(t), b(t) along with the input signal u(t), using y(t) = k(t) u(t) + b(t) + e(t). e(t), measurement noise, is a Gaussian random variable with zero mean and standard deviation 0.05.\n\n```load LineFittingRLSExample u y k b t; figure(); subplot(2,1,1); plot(t,u); ylabel('Input signal, u, [unitless]'); subplot(2,1,2); plot(t,y); ylabel('Valve pressure, y, [bar]'); xlabel('Time [s]');```", null, "### Online Parameter Estimation Using Recursive Least Squares\n\nWrite the valve input-output model using vector notation:\n\n`$\\begin{array}{ll}y\\left(t\\right)& =k\\left(t\\right)u\\left(t\\right)+b\\left(t\\right)+e\\left(t\\right)\\\\ & =\\left[u\\left(t\\right)\\phantom{\\rule{0.2777777777777778em}{0ex}}1\\right]\\left[k\\left(t\\right)\\phantom{\\rule{0.2777777777777778em}{0ex}}b\\left(t\\right){\\right]}^{T}+e\\left(t\\right)\\\\ & =H\\left(t\\right)x\\left(t\\right)+e\\left(t\\right)\\end{array}$`\n\nwhere $H\\left(t\\right)=\\left[u\\left(t\\right)\\phantom{\\rule{0.2777777777777778em}{0ex}}1\\right]$ is the regressors and $x=\\left[k\\left(t\\right)\\phantom{\\rule{0.2777777777777778em}{0ex}}b\\left(t\\right){\\right]}^{T}$ is the parameters to be estimated. e(t) is the unknown noise. You use the recursiveLS estimation command to create a System object for online parameter estimation. You then use the step command to update the parameter estimates, x(t), at each time-step based on H(t) and y(t).\n\nYou specify the following recursiveLS System Object properties:\n\n• Number of parameters: 2.\n\n• EstimationMethod: 'ForgettingFactor' (default). This method has only one scalar parameter, ForgettingFactor, which requires limited prior information regarding parameter values.\n\n• ForgettingFactor: 0.95. The parameters are expected to vary over time, hence less than 1. $\\frac{1}{1-\\lambda }=20$ is the number of past data samples that influence the estimates most.\n\n• InitialParameters: [70; -15], an initial guess for the parameter values. Optional, but recommended for reducing initial transients.\n\n• InitialParameterCovariance: Your estimate of uncertainty in the initial parameter guess. Set it to a small value, 1% of the absolute value of the initial parameters, if you have confidence in the initial parameter guesses. Optional but recommended, especially when you specify InitialParameters. This is only utilized with the ForgettingFactor and KalmanFilter estimation methods.\n\n```X = recursiveLS(2,... % 2=number of estimated parameters 'EstimationMethod','ForgettingFactor',... 'ForgettingFactor',0.95,... 'InitialParameters',[70; -15],... 'InitialParameterCovariance',[0.7 0.15]);```\n\nThis example simulates the online operation of the estimator by providing one (y(t),H(t)) pair to the estimator at a time. Call the step command to update parameters with each new pair. The parameter adaptation is enabled only when the input u is outside the dead band (u>0.3).\n\n```theta = zeros(numel(u),2); yHat = zeros(numel(u),1); PHat = zeros(numel(u),2,2); for kk=1:numel(u) % enable parameter estimation only when u is outside the dead-band if u(kk)>=0.3 X.EnableAdaptation = true(); else X.EnableAdaptation = false(); end [theta(kk,:),yHat(kk)] = step(X,y(kk),[u(kk) 1]); % get estimated parameters and output PHat(kk,:,:) = X.ParameterCovariance; % get estimated uncertainty in parameters % perform any desired tasks with the parameters end```\n\n### Estimated Parameters\n\nThe true and estimated parameter values are:\n\n```figure(); subplot(2,1,1); plot(t,theta(:,1),t,k); % Estimated and real slope, respectively ylabel('Slope'); xlabel('Time'); ylim([49 71]); legend('Estimated','Real','Location','Best'); subplot(2,1,2); plot(t,theta(:,2),t,b); % Estimated and real offset, respectively ylabel('Offset'); xlabel('Time'); ylim([-15.25 -12.75]);```", null, "### Validating the Estimated Model\n\nThe estimator provides the following two tools to judge the quality of the parameter estimates:\n\n1. Output estimate $\\underset{}{\\overset{ˆ}{y}}\\left(t\\right)$: The second output argument of the step method is $\\underset{}{\\overset{ˆ}{y}}\\left(t\\right)=H\\left(t\\right)\\underset{}{\\overset{ˆ}{x}}\\left(t\\right)$. The relative and absolute error between $y$ and $\\underset{}{\\overset{ˆ}{y}}$ are measures of the goodness of the fit.\n\n2. Parameter covariance estimate $\\underset{}{\\overset{ˆ}{P}}\\left(t\\right)$: This is available with the ForgettingFactor and KalmanFilter algorithms. It is stored in the ParameterCovarianceMatrix property of the estimator. The diagonals of $\\underset{}{\\overset{ˆ}{P}}$ are the estimated variances of the parameters. The lower the better.\n\nThe output measurement and its estimate, as well as the associated absolute and relative errors when the engine is on are:\n\n```engineOn = t>50 & t<950; figure(); subplot(2,1,1); absoluteError = y-yHat; plot(t(engineOn),absoluteError(engineOn)); ylim([-0.15 0.15]); ylabel('Abs. Error [bar]'); subplot(2,1,2); relativeError = (y-yHat)./y; plot(t(engineOn),relativeError(engineOn)); ylim([-0.025 0.025]); ylabel('Rel. Error [unitless]'); xlabel('Time [s]');```", null, "The absolute errors are about 0.1bar. The relative errors are below 2%. Both quantities are small.\n\nThe diagonals of the parameter covariance matrix, scaled by the variance of the residuals $y\\left(t\\right)-\\underset{}{\\overset{ˆ}{y}}\\left(t\\right)$, capture the variances of parameter estimates. The square-root of the variances are the standard deviations of the parameter estimates.\n\n```noiseVariance = var(y(engineOn)-yHat(engineOn)); figure(); subplot(2,1,1); hold on; plot(t,sqrt(PHat(:,1,1)*noiseVariance)); ylim([0 1]); ylabel('Std. dev. of slope k'); subplot(2,1,2); plot(t,sqrt(PHat(:,2,2)*noiseVariance)); ylim([0 1]); ylabel('Std. dev. of offset b'); xlabel('Time [s]'); hold on;```", null, "The standard deviation of the slope k fluctuates around 0.7. This is small relative to the range of values of k [50, 70]. This gives confidence in the parameter estimates. The situation is similar with the offset b, which is in the range [-15 -13].\n\nNote that the parameter standard deviations are also estimates. They are based on the assumption that the residuals $y\\left(t\\right)-\\underset{}{\\overset{ˆ}{y}}\\left(t\\right)$ are white. This depends on the estimation method, its associated parameters, structure of the estimated model, and the input signal u. Differences between the assumed and the actual model structure, lack of persistent input excitation, or unrealistic estimation method settings can lead to overly optimistic or pessimistic uncertainty estimates.\n\n### Summary\n\nYou performed a line fit using recursive least squares to capture the time-varying input-output behavior of a hydraulic valve. You evaluated the quality of fit by looking at two signals: the error between estimated and measured system output, and the parameter covariance estimates.\n\n### References\n\n Gauthier, Jean-Philippe, and Philippe Micheau. \"Regularized RLS and DHOBE: An Adaptive Feedforward for a Solenoid Valve.\" Control Systems Technology, IEEE Transactions on 20.5 (2012): 1311-1318", null, "" ]
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https://gcc.gnu.org/ml/gcc-patches/2006-10/msg00545.html
[ "This is the mail archive of the [email protected] mailing list for the GCC project.\n\nIndex Nav: Message Nav: [Date Index] [Subject Index] [Author Index] [Thread Index] [Date Prev] [Date Next] [Thread Prev] [Thread Next] [Raw text]\n\n# Re: [PATCH] define-constraints rewrite for s390 back end\n\n• From: Wolfgang Gellerich <gellerich at de dot ibm dot com>\n• To: gcc-patches at gcc dot gnu dot org, uweigand at de dot ibm dot com\n• Date: Tue, 10 Oct 2006 16:22:29 +0200\n• Subject: Re: [PATCH] define-constraints rewrite for s390 back end\n\n```%% > As discussed, the patch appended below is a rewrite for the s390 back\n%% > end to exploit the new define-constraints framework.\n\n%% Thanks! The patch looks good, except for some minor coding style\n%% issues, see below. Also, please provide a ChangeLog entry.\n\nHere are the modified patch and the Changelog entry:\n\n2006-10-10 Wolfgang Gellerich <[email protected]>\n\n* config/s390/contraints.md: new file\n* config/s390/s390-protos.h: added protos for new functions\ns390_mem_constraint, s390_O_constraint_str,\ns390_N_constraint_str, s390_float_const_zero_p\n* config/s390/s390.c (s390_extra_constraint_str): removed.\n(s390_mem_constraint): new.\n(s390_const_double_ok_for_constraint_p): removed.\n(s390_O_constraint_str): new.\n(s390_const_ok_for_constraint_p): removed.\n(s390_N_constraint_str): new.\n(s390_float_const_zero_p): new.\n* config/s390/s390.h (REG_CLASS_FROM_LETTER): removed.\n(CONST_OK_FOR_CONSTRAINT_P): removed.\n(s390_const_ok_for_constraint_p): removed.\n(CONST_DOUBLE_OK_FOR_CONSTRAINT_P): removed.\n(s390_const_double_ok_for_constraint_p): removed.\n(EXTRA_CONSTRAINT_STR): removed.\n(s390_extra_constraint_str): removed.\n(EXTRA_MEMORY_CONSTRAINT): removed.\n(CONSTRAINT_LEN): removed.\n\nRegards, Wolfgang\n\n-------------------------------------------------\n\nCommon subdirectories: s390-ORI/.svn and s390/.svn\ndiff -p -c -N s390-ORI/constraints.md s390/constraints.md\n*** s390-ORI/constraints.md\tThu Jan 1 01:00:00 1970\n--- s390/constraints.md\tMon Oct 9 16:19:09 2006\n***************\n*** 0 ****\n--- 1,438 ----\n+ ;; Constraints definitions belonging to the gcc backend for IBM S/390.\n+ ;; Copyright (C) 2006 Free Software Foundation, Inc.\n+ ;; Written by Wolfgang Gellerich, using code and information found in\n+ ;; files s390.md, s390.h, and s390.c.\n+ ;;\n+ ;; This file is part of GCC.\n+ ;;\n+ ;; GCC is free software; you can redistribute it and/or modify it under\n+ ;; Software Foundation; either version 2, or (at your option) any later\n+ ;; version.\n+ ;;\n+ ;; GCC is distributed in the hope that it will be useful, but WITHOUT ANY\n+ ;; WARRANTY; without even the implied warranty of MERCHANTABILITY or\n+ ;; FITNESS FOR A PARTICULAR PURPOSE. See the GNU General Public License\n+ ;; for more details.\n+ ;;\n+ ;; You should have received a copy of the GNU General Public License\n+ ;; along with GCC; see the file COPYING. If not, write to the Free\n+ ;; Software Foundation, 51 Franklin Street, Fifth Floor, Boston, MA\n+ ;; 02110-1301, USA.\n+\n+\n+ ;;\n+ ;; Special constraints for s/390 machine description:\n+ ;;\n+ ;; a -- Any address register from 1 to 15.\n+ ;; c -- Condition code register 33.\n+ ;; d -- Any register from 0 to 15.\n+ ;; f -- Floating point registers.\n+ ;; t -- Access registers 36 and 37.\n+ ;; G -- Const double zero operand\n+ ;; I -- An 8-bit constant (0..255).\n+ ;; J -- A 12-bit constant (0..4095).\n+ ;; K -- A 16-bit constant (-32768..32767).\n+ ;; L -- Value appropriate as displacement.\n+ ;; (0..4095) for short displacement\n+ ;; (-524288..524287) for long displacement\n+ ;; M -- Constant integer with a value of 0x7fffffff.\n+ ;; N -- Multiple letter constraint followed by 4 parameter letters.\n+ ;; 0..9,x: number of the part counting from most to least significant\n+ ;; H,Q: mode of the part\n+ ;; D,S,H: mode of the containing operand\n+ ;; 0,F: value of the other parts (F - all bits set)\n+ ;;\n+ ;; The constraint matches if the specified part of a constant\n+ ;; has a value different from its other parts. If the letter x\n+ ;; is specified instead of a part number, the constraint matches\n+ ;; if there is any single part with non-default value.\n+ ;; O -- Multiple letter constraint followed by 1 parameter.\n+ ;; s: Signed extended immediate value (-2G .. 2G-1).\n+ ;; p: Positive extended immediate value (0 .. 4G-1).\n+ ;; n: Negative extended immediate value (-4G .. -1).\n+ ;; These constraints do not accept any operand if the machine does\n+ ;; not provide the extended-immediate facility.\n+ ;; P -- Any integer constant that can be loaded without literal pool.\n+ ;; Q -- Memory reference without index register and with short displacement.\n+ ;; R -- Memory reference with index register and short displacement.\n+ ;; S -- Memory reference without index register but with long displacement.\n+ ;; T -- Memory reference with index register and long displacement.\n+ ;; A -- Multiple letter constraint followed by Q, R, S, or T:\n+ ;; Offsettable memory reference of type specified by second letter.\n+ ;; B -- Multiple letter constraint followed by Q, R, S, or T:\n+ ;; Memory reference of the type specified by second letter that\n+ ;; does *not* refer to a literal pool entry.\n+ ;; U -- Pointer with short displacement.\n+ ;; W -- Pointer with long displacement.\n+ ;; Y -- Shift count operand.\n+ ;;\n+\n+\n+ ;;\n+ ;; Register constraints.\n+ ;;\n+\n+ (define_register_constraint \"a\"\n+ \"Any address register from 1 to 15.\")\n+\n+\n+ (define_register_constraint \"c\"\n+ \"CC_REGS\"\n+ \"Condition code register 33\")\n+\n+\n+ (define_register_constraint \"d\"\n+ \"GENERAL_REGS\"\n+ \"Any register from 0 to 15\")\n+\n+\n+ (define_register_constraint \"f\"\n+ \"FP_REGS\"\n+ \"Floating point registers\")\n+\n+\n+ (define_register_constraint \"t\"\n+ \"ACCESS_REGS\"\n+ \"@internal\n+ Access registers 36 and 37\")\n+\n+\n+ ;;\n+ ;; General constraints for constants.\n+ ;;\n+\n+ (define_constraint \"G\"\n+ \"@internal\n+ Const double zero operand\"\n+ (and (match_code \"const_double\")\n+ (match_test \"s390_float_const_zero_p (op)\")))\n+\n+\n+ (define_constraint \"I\"\n+ \"An 8-bit constant (0..255)\"\n+ (and (match_code \"const_int\")\n+ (match_test \"(unsigned int) ival <= 255\")))\n+\n+\n+ (define_constraint \"J\"\n+ \"A 12-bit constant (0..4095)\"\n+ (and (match_code \"const_int\")\n+ (match_test \"(unsigned int) ival <= 4095\")))\n+\n+\n+ (define_constraint \"K\"\n+ \"A 16-bit constant (-32768..32767)\"\n+ (and (match_code \"const_int\")\n+ (match_test \"ival >= -32768 && ival <= 32767\")))\n+\n+\n+\n+ (define_constraint \"L\"\n+ \"Value appropriate as displacement.\n+ (0..4095) for short displacement\n+ (-524288..524287) for long displacement\"\n+ (and (match_code \"const_int\")\n+ (match_test \"TARGET_LONG_DISPLACEMENT ?\n+ (ival >= -524288 && ival <= 524287)\n+ : (ival >= 0 && ival <= 4095)\")))\n+\n+\n+ (define_constraint \"M\"\n+ \"Constant integer with a value of 0x7fffffff\"\n+ (and (match_code \"const_int\")\n+ (match_test \"ival == 2147483647\")))\n+\n+\n+ (define_constraint \"P\"\n+ \"@internal\n+ Any integer constant that can be loaded without literal pool\"\n+ (and (match_code \"const_int\")\n+\n+\n+ \"Shift count operand\"\n+\n+ ;; Simply check for the basic form of a shift count. Reload will\n+ ;; take care of making sure we have a proper base register.\n+\n+ (match_test \"s390_decompose_shift_count (op, NULL, NULL)\" ))\n+\n+\n+ ;; N -- Multiple letter constraint followed by 4 parameter letters.\n+ ;; 0..9,x: number of the part counting from most to least significant\n+ ;; H,Q: mode of the part\n+ ;; D,S,H: mode of the containing operand\n+ ;; 0,F: value of the other parts (F = all bits set)\n+ ;;\n+ ;; The constraint matches if the specified part of a constant\n+ ;; has a value different from its other parts. If the letter x\n+ ;; is specified instead of a part number, the constraint matches\n+ ;; if there is any single part with non-default value.\n+ ;;\n+ ;; The following patterns define only those constraints that are actually\n+ ;; used in s390.md. If you need an additional one, simply add it in the\n+ ;; obvious way. Function s390_N_constraint_str is ready to handle all\n+ ;; combinations.\n+ ;;\n+\n+\n+ (define_constraint \"NxQS0\"\n+ \"@internal\"\n+ (and (match_code \"const_int\")\n+ (match_test \"s390_N_constraint_str (\\\"xQS0\\\", ival)\")))\n+\n+\n+ (define_constraint \"NxQD0\"\n+ \"@internal\"\n+ (and (match_code \"const_int\")\n+ (match_test \"s390_N_constraint_str (\\\"xQD0\\\", ival)\")))\n+\n+\n+ (define_constraint \"N3HD0\"\n+ \"@internal\"\n+ (and (match_code \"const_int\")\n+ (match_test \"s390_N_constraint_str (\\\"3HD0\\\", ival)\")))\n+\n+\n+ (define_constraint \"N2HD0\"\n+ \"@internal\"\n+ (and (match_code \"const_int\")\n+ (match_test \"s390_N_constraint_str (\\\"2HD0\\\", ival)\")))\n+\n+\n+ (define_constraint \"N1SD0\"\n+ \"@internal\"\n+ (and (match_code \"const_int\")\n+ (match_test \"s390_N_constraint_str (\\\"1SD0\\\", ival)\")))\n+\n+\n+ (define_constraint \"N1HS0\"\n+ \"@internal\"\n+ (and (match_code \"const_int\")\n+ (match_test \"s390_N_constraint_str (\\\"1HS0\\\", ival)\")))\n+\n+\n+ (define_constraint \"N1HD0\"\n+ \"@internal\"\n+ (and (match_code \"const_int\")\n+ (match_test \"s390_N_constraint_str (\\\"1HD0\\\", ival)\")))\n+\n+\n+ (define_constraint \"N0SD0\"\n+ \"@internal\"\n+ (and (match_code \"const_int\")\n+ (match_test \"s390_N_constraint_str (\\\"0SD0\\\", ival)\")))\n+\n+\n+ (define_constraint \"N0HS0\"\n+ \"@internal\"\n+ (and (match_code \"const_int\")\n+ (match_test \"s390_N_constraint_str (\\\"0HS0\\\", ival)\")))\n+\n+\n+ (define_constraint \"N0HD0\"\n+ \"@internal\"\n+ (and (match_code \"const_int\")\n+ (match_test \"s390_N_constraint_str (\\\"0HD0\\\", ival)\")))\n+\n+\n+ (define_constraint \"NxQDF\"\n+ \"@internal\"\n+ (and (match_code \"const_int\")\n+ (match_test \"s390_N_constraint_str (\\\"xQDF\\\", ival)\")))\n+\n+\n+ (define_constraint \"N1SDF\"\n+ \"@internal\"\n+ (and (match_code \"const_int\")\n+ (match_test \"s390_N_constraint_str (\\\"1SDF\\\", ival)\")))\n+\n+\n+ (define_constraint \"N0SDF\"\n+ \"@internal\"\n+ (and (match_code \"const_int\")\n+ (match_test \"s390_N_constraint_str (\\\"0SDF\\\", ival)\")))\n+\n+\n+ (define_constraint \"N3HDF\"\n+ \"@internal\"\n+ (and (match_code \"const_int\")\n+ (match_test \"s390_N_constraint_str (\\\"3HDF\\\", ival)\")))\n+\n+\n+ (define_constraint \"N2HDF\"\n+ \"@internal\"\n+ (and (match_code \"const_int\")\n+ (match_test \"s390_N_constraint_str (\\\"2HDF\\\", ival)\")))\n+\n+\n+ (define_constraint \"N1HDF\"\n+ \"@internal\"\n+ (and (match_code \"const_int\")\n+ (match_test \"s390_N_constraint_str (\\\"1HDF\\\", ival)\")))\n+\n+\n+ (define_constraint \"N0HDF\"\n+ \"@internal\"\n+ (and (match_code \"const_int\")\n+ (match_test \"s390_N_constraint_str (\\\"0HDF\\\", ival)\")))\n+\n+\n+ (define_constraint \"N0HSF\"\n+ \"@internal\"\n+ (and (match_code \"const_int\")\n+ (match_test \"s390_N_constraint_str (\\\"0HSF\\\", ival)\")))\n+\n+\n+ (define_constraint \"N1HSF\"\n+ \"@internal\"\n+ (and (match_code \"const_int\")\n+ (match_test \"s390_N_constraint_str (\\\"1HSF\\\", ival)\")))\n+\n+\n+ (define_constraint \"NxQSF\"\n+ \"@internal\"\n+ (and (match_code \"const_int\")\n+ (match_test \"s390_N_constraint_str (\\\"xQSF\\\", ival)\")))\n+\n+\n+ (define_constraint \"NxQHF\"\n+ \"@internal\"\n+ (and (match_code \"const_int\")\n+ (match_test \"s390_N_constraint_str (\\\"xQHF\\\", ival)\")))\n+\n+\n+ (define_constraint \"NxQH0\"\n+ \"@internal\"\n+ (and (match_code \"const_int\")\n+ (match_test \"s390_N_constraint_str (\\\"xQH0\\\", ival)\")))\n+\n+\n+\n+\n+ ;;\n+ ;; Double-letter constraints starting with O follow.\n+ ;;\n+\n+\n+ (define_constraint \"Os\"\n+ \"@internal\n+ Signed extended immediate value (-2G .. 2G-1).\n+ This constraint will only match if the machine provides\n+ the extended-immediate facility.\"\n+ (and (match_code \"const_int\")\n+ (match_test \"s390_O_constraint_str ('s', ival)\")))\n+\n+\n+ (define_constraint \"Op\"\n+ \"@internal\n+ Positive extended immediate value (0 .. 4G-1).\n+ This constraint will only match if the machine provides\n+ the extended-immediate facility.\"\n+ (and (match_code \"const_int\")\n+ (match_test \"s390_O_constraint_str ('p', ival)\")))\n+\n+\n+ (define_constraint \"On\"\n+ \"@internal\n+ Negative extended immediate value (-4G .. -1).\n+ This constraint will only match if the machine provides\n+ the extended-immediate facility.\"\n+ (and (match_code \"const_int\")\n+ (match_test \"s390_O_constraint_str ('n', ival)\")))\n+\n+\n+\n+\n+ ;;\n+ ;; Memory constraints follow.\n+ ;;\n+\n+ (define_memory_constraint \"Q\"\n+ \"Memory reference without index register and with short displacement\"\n+ (match_test \"s390_mem_constraint (\\\"Q\\\", op)\"))\n+\n+\n+\n+ (define_memory_constraint \"R\"\n+ \"Memory reference with index register and short displacement\"\n+ (match_test \"s390_mem_constraint (\\\"R\\\", op)\"))\n+\n+\n+ (define_memory_constraint \"S\"\n+ \"Memory reference without index register but with long displacement\"\n+ (match_test \"s390_mem_constraint (\\\"S\\\", op)\"))\n+\n+\n+ (define_memory_constraint \"T\"\n+ \"Memory reference with index register and long displacement\"\n+ (match_test \"s390_mem_constraint (\\\"T\\\", op)\"))\n+\n+\n+\n+ (define_memory_constraint \"AQ\"\n+ \"@internal\n+ Offsettable memory reference without index register and with short displacement\"\n+ (match_test \"s390_mem_constraint (\\\"AQ\\\", op)\"))\n+\n+\n+ (define_memory_constraint \"AR\"\n+ \"@internal\n+ Offsettable memory reference with index register and short displacement\"\n+ (match_test \"s390_mem_constraint (\\\"AR\\\", op)\"))\n+\n+\n+ (define_memory_constraint \"AS\"\n+ \"@internal\n+ Offsettable memory reference without index register but with long displacement\"\n+ (match_test \"s390_mem_constraint (\\\"AS\\\", op)\"))\n+\n+\n+ (define_memory_constraint \"AT\"\n+ \"@internal\n+ Offsettable memory reference with index register and long displacement\"\n+ (match_test \"s390_mem_constraint (\\\"AT\\\", op)\"))\n+\n+\n+\n+ (define_constraint \"BQ\"\n+ \"@internal\n+ Memory reference without index register and with short\n+ displacement that does *not* refer to a literal pool entry.\"\n+ (match_test \"s390_mem_constraint (\\\"BQ\\\", op)\"))\n+\n+\n+ (define_constraint \"BR\"\n+ \"@internal\n+ Memory reference with index register and short displacement that\n+ does *not* refer to a literal pool entry. \"\n+ (match_test \"s390_mem_constraint (\\\"BR\\\", op)\"))\n+\n+\n+ (define_constraint \"BS\"\n+ \"@internal\n+ Memory reference without index register but with long displacement\n+ that does *not* refer to a literal pool entry. \"\n+ (match_test \"s390_mem_constraint (\\\"BS\\\", op)\"))\n+\n+\n+ (define_constraint \"BT\"\n+ \"@internal\n+ Memory reference with index register and long displacement that\n+ does *not* refer to a literal pool entry. \"\n+ (match_test \"s390_mem_constraint (\\\"BT\\\", op)\"))\n+\n+\n+\n+ \"Pointer with short displacement\"\n+ (match_test \"s390_mem_constraint (\\\"U\\\", op)\"))\n+\n+\n+\n+ \"Pointer with long displacement\"\n+ (match_test \"s390_mem_constraint (\\\"W\\\", op)\"))\ndiff -p -c -N s390-ORI/s390-protos.h s390/s390-protos.h\n*** s390-ORI/s390-protos.h\tThu Sep 28 09:58:58 2006\n--- s390/s390-protos.h\tMon Oct 9 16:19:09 2006\n*************** along with GCC; see the file COPYING. I\n*** 19,24 ****\n--- 19,36 ----\nSoftware Foundation, 51 Franklin Street, Fifth Floor, Boston, MA\n02110-1301, USA. */\n\n+\n+\n+ /* Prototypes of functions used for constraint evaluation in\n+ constraints.c. */\n+\n+ extern int s390_mem_constraint (const char *str, rtx op);\n+ extern int s390_O_constraint_str (const char c, HOST_WIDE_INT value);\n+ extern int s390_N_constraint_str (const char *str, HOST_WIDE_INT value);\n+ extern int s390_float_const_zero_p (rtx value);\n+\n+\n+\n/* Declare functions in s390.c. */\n\nextern void optimization_options (int, int);\ndiff -p -c -N s390-ORI/s390.c s390/s390.c\n*** s390-ORI/s390.c\tThu Sep 28 09:58:58 2006\n--- s390/s390.c\tMon Oct 9 16:19:09 2006\n*** 1843,1856 ****\nreturn true;\n}\n\n! /* Return 1 if OP is a valid operand for a C constraint, 0 else. */\n\nint\n! s390_extra_constraint_str (rtx op, int c, const char * str)\n{\n!\n! gcc_assert (c == str);\n\n/* Check for offsettable variants of memory constraints. */\nif (c == 'A')\n--- 1843,1858 ----\nreturn true;\n}\n\n!\n! /* Evaluates constraint strings described by the regular expression\n! ([A|B](Q|R|S|T))|U|W and returns 1 if OP is a valid operand for the\n! constraint given in STR, or 0 else. */\n\nint\n! s390_mem_constraint (const char *str, rtx op)\n{\n! char c = str;\n\n/* Check for offsettable variants of memory constraints. */\nif (c == 'A')\n*************** s390_extra_constraint_str (rtx op, int c\n*** 1860,1867 ****\nreturn 0;\n\n! \t ? !offsettable_memref_p (op)\n! \t : !offsettable_nonstrict_memref_p (op))\nreturn 0;\n\nc = str;\n--- 1862,1868 ----\nreturn 0;\n\n! \t ? !offsettable_memref_p (op) : !offsettable_nonstrict_memref_p (op))\nreturn 0;\n\nc = str;\n*************** s390_extra_constraint_str (rtx op, int c\n*** 1929,1935 ****\nif (GET_CODE (op) != MEM)\nreturn 0;\n! \t so accept it for the most generic constraint. */\nreturn 0;\n--- 1930,1936 ----\nif (GET_CODE (op) != MEM)\nreturn 0;\n! so accept it for the most generic constraint. */\nreturn 0;\n*************** s390_extra_constraint_str (rtx op, int c\n*** 1949,1955 ****\nif (!TARGET_LONG_DISPLACEMENT)\nreturn 0;\n! \t so accept it for the most generic constraint. */\nreturn 0;\n--- 1950,1956 ----\nif (!TARGET_LONG_DISPLACEMENT)\nreturn 0;\n! so accept it for the most generic constraint. */\nreturn 0;\n*************** s390_extra_constraint_str (rtx op, int c\n*** 1969,2100 ****\nreturn 1;\n}\n\n! /* Return true if VALUE matches the constraint STR. */\n\nint\n! s390_const_double_ok_for_constraint_p (rtx value,\n! \t\t\t\t int c,\n! \t\t\t\t const char * str)\n{\n! gcc_assert (c == str);\n\n! switch (str)\n{\n! case 'G':\n! /* The floating point zero constant. */\n! return (GET_MODE_CLASS (GET_MODE (value)) == MODE_FLOAT\n! && value == CONST0_RTX (GET_MODE (value)));\n!\ndefault:\n! return 0;\n}\n}\n\n! /* Return true if VALUE matches the constraint STR. */\n\nint\n! s390_const_ok_for_constraint_p (HOST_WIDE_INT value,\n! \t\t\t\tint c,\n! \t\t\t\tconst char * str)\n{\nenum machine_mode mode, part_mode;\nint def;\nint part, part_goal;\n\n- gcc_assert (c == str);\n-\n- switch (str)\n- {\n- case 'I':\n- return (unsigned int)value < 256;\n-\n- case 'J':\n- return (unsigned int)value < 4096;\n-\n- case 'K':\n- return value >= -32768 && value < 32768;\n-\n- case 'L':\n- return (TARGET_LONG_DISPLACEMENT ?\n- \t (value >= -524288 && value <= 524287)\n- \t : (value >= 0 && value <= 4095));\n- case 'M':\n- return value == 2147483647;\n-\n- case 'N':\n- if (str == 'x')\n- \tpart_goal = -1;\n- else\n- \tpart_goal = str - '0';\n-\n- switch (str)\n- \t{\n- \tcase 'Q': part_mode = QImode; break;\n- \tcase 'H': part_mode = HImode; break;\n- \tcase 'S': part_mode = SImode; break;\n- \tdefault: return 0;\n- \t}\n-\n- switch (str)\n- \t{\n- \tcase 'H': mode = HImode; break;\n- \tcase 'S': mode = SImode; break;\n- \tcase 'D': mode = DImode; break;\n- \tdefault: return 0;\n- \t}\n-\n- switch (str)\n- \t{\n- \tcase '0': def = 0; break;\n- \tcase 'F': def = -1; break;\n- \tdefault: return 0;\n- \t}\n\n! if (GET_MODE_SIZE (mode) <= GET_MODE_SIZE (part_mode))\n! \treturn 0;\n!\n! part = s390_single_part (GEN_INT (value), mode, part_mode, def);\n! if (part < 0)\n! \treturn 0;\n! if (part_goal != -1 && part_goal != part)\n! \treturn 0;\n\nbreak;\n!\n! case 'O':\n! if (!TARGET_EXTIMM)\n! \treturn 0;\n!\n! switch (str)\n! \t{\n! \tcase 's':\n! \t return trunc_int_for_mode (value, SImode) == value;\n!\n! \tcase 'p':\n! \t return value == 0\n! \t || s390_single_part (GEN_INT (value), DImode, SImode, 0) == 1;\n!\n! \tcase 'n':\n! \t return\n! \t (value == -1\n! \t || s390_single_part (GEN_INT (value), DImode, SImode, -1) == 1)\n! \t && value != -((HOST_WIDE_INT)1 << 32);\n!\n! \tdefault:\n! \t gcc_unreachable ();\n! \t}\nbreak;\n\n! case 'P':\n\ndefault:\nreturn 0;\n}\n\nreturn 1;\n}\n\n/* Compute a (partial) cost for rtx X. Return true if the complete\ncost has been computed, and false if subexpressions should be\nscanned. In either case, *TOTAL contains the cost result.\n--- 1970,2089 ----\nreturn 1;\n}\n\n!\n!\n! /* Evaluates constraint strings starting with letter O. Input\n! parameter C is the second letter following the \"O\" in the constraint\n! string. Returns 1 if VALUE meets the respective constraint and 0\n! otherwise. */\n\nint\n! s390_O_constraint_str (const char c, HOST_WIDE_INT value)\n{\n! if (!TARGET_EXTIMM)\n! return 0;\n\n! switch (c)\n{\n! case 's':\n! return trunc_int_for_mode (value, SImode) == value;\n!\n! case 'p':\n! return value == 0\n! \t|| s390_single_part (GEN_INT (value), DImode, SImode, 0) == 1;\n!\n! case 'n':\n! return value == -1\n! \t|| s390_single_part (GEN_INT (value), DImode, SImode, -1) == 1;\n!\ndefault:\n! gcc_unreachable ();\n}\n}\n\n!\n! /* Evaluates constraint strings starting with letter N. Parameter STR\n! contains the letters following letter \"N\" in the constraint string.\n! Returns true if VALUE matches the constraint. */\n\nint\n! s390_N_constraint_str (const char *str, HOST_WIDE_INT value)\n{\nenum machine_mode mode, part_mode;\nint def;\nint part, part_goal;\n\n! if (str == 'x')\n! part_goal = -1;\n! else\n! part_goal = str - '0';\n\n+ switch (str)\n+ {\n+ case 'Q':\n+ part_mode = QImode;\nbreak;\n! case 'H':\n! part_mode = HImode;\nbreak;\n+ case 'S':\n+ part_mode = SImode;\n+ break;\n+ default:\n+ return 0;\n+ }\n\n! switch (str)\n! {\n! case 'H':\n! mode = HImode;\n! break;\n! case 'S':\n! mode = SImode;\n! break;\n! case 'D':\n! mode = DImode;\n! break;\n! default:\n! return 0;\n! }\n\n+ switch (str)\n+ {\n+ case '0':\n+ def = 0;\n+ break;\n+ case 'F':\n+ def = -1;\n+ break;\ndefault:\nreturn 0;\n}\n\n+ if (GET_MODE_SIZE (mode) <= GET_MODE_SIZE (part_mode))\n+ return 0;\n+\n+ part = s390_single_part (GEN_INT (value), mode, part_mode, def);\n+ if (part < 0)\n+ return 0;\n+ if (part_goal != -1 && part_goal != part)\n+ return 0;\n+\nreturn 1;\n}\n\n+\n+ /* Returns true if the input parameter VALUE is a float zero. */\n+\n+ int\n+ s390_float_const_zero_p (rtx value)\n+ {\n+ return (GET_MODE_CLASS (GET_MODE (value)) == MODE_FLOAT\n+ \t && value == CONST0_RTX (GET_MODE (value)));\n+ }\n+\n+\n/* Compute a (partial) cost for rtx X. Return true if the complete\ncost has been computed, and false if subexpressions should be\nscanned. In either case, *TOTAL contains the cost result.\ndiff -p -c -N s390-ORI/s390.h s390/s390.h\n*** s390-ORI/s390.h\tThu Sep 28 09:58:58 2006\n--- s390/s390.h\tMon Oct 9 16:19:09 2006\n*************** extern const enum reg_class regclass_map\n*** 481,514 ****\n: MODE)\n\n- /* Define various machine-dependent constraint letters. */\n-\n- #define REG_CLASS_FROM_LETTER(C) \\\n- ((C) == 'a' ? ADDR_REGS : \\\n- (C) == 'd' ? GENERAL_REGS : \\\n- (C) == 'f' ? FP_REGS : \\\n- (C) == 'c' ? CC_REGS : \t\t\t\t\t\t\\\n- (C) == 't' ? ACCESS_REGS : NO_REGS)\n-\n- #define CONST_OK_FOR_CONSTRAINT_P(VALUE, C, STR) \\\n- s390_const_ok_for_constraint_p ((VALUE), (C), (STR))\n-\n- #define CONST_DOUBLE_OK_FOR_CONSTRAINT_P(VALUE, C, STR)\t\t\t\\\n- s390_const_double_ok_for_constraint_p ((VALUE), (C), (STR))\n-\n- #define EXTRA_CONSTRAINT_STR(OP, C, STR) \t\\\n- s390_extra_constraint_str ((OP), (C), (STR))\n- #define EXTRA_MEMORY_CONSTRAINT(C, STR)\t\t\t\t\t\\\n- ((C) == 'Q' || (C) == 'R' || (C) == 'S' || (C) == 'T' || (C) == 'A')\n- ((C) == 'U' || (C) == 'W' || (C) == 'Y')\n-\n- #define CONSTRAINT_LEN(C, STR) \t\\\n- ((C) == 'N' ? 5 : \t \\\n- (C) == 'O' ? 2 :\t\t\t\t\t\t\t\\\n- (C) == 'A' ? 2 :\t\t\t\t\t\t\t\\\n- (C) == 'B' ? 2 : DEFAULT_CONSTRAINT_LEN ((C), (STR)))\n-\n/* Stack layout and calling conventions. */\n\n/* Our stack grows from higher to lower addresses. However, local variables\n--- 481,486 ----\ndiff -p -c -N s390-ORI/s390.md s390/s390.md\n*** s390-ORI/s390.md\tThu Sep 28 09:58:58 2006\n--- s390/s390.md\tMon Oct 9 16:19:09 2006\n***************\n*** 22,72 ****\n;; 02110-1301, USA.\n\n;;\n! ;; Special constraints for s/390 machine description:\n! ;;\n! ;; a -- Any address register from 1 to 15.\n! ;; c -- Condition code register 33.\n! ;; d -- Any register from 0 to 15.\n! ;; f -- Floating point registers.\n! ;; t -- Access registers 36 and 37.\n! ;; G -- Const double zero operand\n! ;; I -- An 8-bit constant (0..255).\n! ;; J -- A 12-bit constant (0..4095).\n! ;; K -- A 16-bit constant (-32768..32767).\n! ;; L -- Value appropriate as displacement.\n! ;; (0..4095) for short displacement\n! ;; (-524288..524287) for long displacement\n! ;; M -- Constant integer with a value of 0x7fffffff.\n! ;; N -- Multiple letter constraint followed by 4 parameter letters.\n! ;; 0..9,x: number of the part counting from most to least significant\n! ;; H,Q: mode of the part\n! ;; D,S,H: mode of the containing operand\n! ;; 0,F: value of the other parts (F - all bits set)\n! ;;\n! ;; The constraint matches if the specified part of a constant\n! ;; has a value different from its other parts. If the letter x\n! ;; is specified instead of a part number, the constraint matches\n! ;; if there is any single part with non-default value.\n! ;; O -- Multiple letter constraint followed by 1 parameter.\n! ;; s: Signed extended immediate value (-2G .. 2G-1).\n! ;; p: Positive extended immediate value (0 .. 4G-1).\n! ;; n: Negative extended immediate value (-4G+1 .. -1).\n! ;; These constraints do not accept any operand if the machine does\n! ;; not provide the extended-immediate facility.\n! ;; P -- Any integer constant that can be loaded without literal pool.\n! ;; Q -- Memory reference without index register and with short displacement.\n! ;; R -- Memory reference with index register and short displacement.\n! ;; S -- Memory reference without index register but with long displacement.\n! ;; T -- Memory reference with index register and long displacement.\n! ;; A -- Multiple letter constraint followed by Q, R, S, or T:\n! ;; Offsettable memory reference of type specified by second letter.\n! ;; B -- Multiple letter constraint followed by Q, R, S, or T:\n! ;; Memory reference of the type specified by second letter that\n! ;; does *not* refer to a literal pool entry.\n! ;; U -- Pointer with short displacement.\n! ;; W -- Pointer with long displacement.\n! ;; Y -- Shift count operand.\n;;\n;; Special formats used for outputting 390 instructions.\n;;\n;; %C: print opcode suffix for branch condition.\n--- 22,30 ----\n;; 02110-1301, USA.\n\n;;\n! ;; See constraints.md for a description of constraints specific to s390.\n;;\n+\n;; Special formats used for outputting 390 instructions.\n;;\n;; %C: print opcode suffix for branch condition.\n***************\n*** 243,248 ****\n--- 201,209 ----\n;; Predicates\n(include \"predicates.md\")\n\n+ ;; Constraint definitions\n+ (include \"constraints.md\")\n+\n;; Other includes\n(include \"tpf.md\")\n\n```\n\nIndex Nav: Message Nav: [Date Index] [Subject Index] [Author Index] [Thread Index] [Date Prev] [Date Next] [Thread Prev] [Thread Next]" ]
[ null ]
{"ft_lang_label":"__label__en","ft_lang_prob":0.54312307,"math_prob":0.94944805,"size":26510,"snap":"2019-51-2020-05","text_gpt3_token_len":7760,"char_repetition_ratio":0.19833246,"word_repetition_ratio":0.37258595,"special_character_ratio":0.39060733,"punctuation_ratio":0.26864657,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9706935,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2019-12-05T18:06:56Z\",\"WARC-Record-ID\":\"<urn:uuid:8dbbcdc7-c407-4e21-9566-f8e2f99dc58b>\",\"Content-Length\":\"35478\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:e00e8fde-9f00-4251-84a3-e934f08c964f>\",\"WARC-Concurrent-To\":\"<urn:uuid:de65a572-a7fe-4ae3-a662-214094428d16>\",\"WARC-IP-Address\":\"209.132.180.131\",\"WARC-Target-URI\":\"https://gcc.gnu.org/ml/gcc-patches/2006-10/msg00545.html\",\"WARC-Payload-Digest\":\"sha1:LAAWJI62QZS3X4MV2JLYP2NQQ7BMLKZS\",\"WARC-Block-Digest\":\"sha1:5NZDSK3YQAJT7GK2IH36E4RLLN3MMLFO\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2019/CC-MAIN-2019-51/CC-MAIN-2019-51_segments_1575540481281.1_warc_CC-MAIN-20191205164243-20191205192243-00320.warc.gz\"}"}
https://assignmentpress.com/the-following-data-show-the-number-of-hours-studied-for-an-exam/
[ "Finance\n\n# The following data show the number of hours studied for an exam,\n\nThe following data show the number of hours studied for an exam, x, and the grade received on the exam, (is measured in 10s; that is, y = 8 means that the grade, rounded to the nearest 10 points, is 80).\n\nDon't use plagiarized sources. Get Your Custom Essay on\nThe following data show the number of hours studied for an exam,\nJust from \\$13/Page\n x 2 3 3 4 4 5 5 6 6 6 7 7 7 8 8 y 5 5 7 5 7 7 8 6 9 8 7 9 10 8 9\n\na. Draw a scatter diagram of the data.\n\nb. Find the equation of the line of best fit and graph it on the scatter diagram. y_ 8\n\nc. Find the ordinates that correspond to χ = 2, 3, 4, 5, 6, 7, and 8.\n\nd. Find the five values of that are associated with the points where χ = 3 and χ = 6.\n\ne. Find the variance", null, "of all the points about the line of best fit.\n\nCheck Also\nClose\n• ### Joe Fast started a mobile snack food service on January 2, 2006, investing \\$15,000 cash deposited… 1 answer below »\n\nOrder your essay today and save 30% with the discount code ESSAYHELP" ]
[ null, "https://files.transtutors.com/book/qimage/questions4082014183.png", null ]
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https://www.numbers.education/6290.html
[ "Is 6290 a prime number? What are the divisors of 6290?\n\n## Parity of 6 290\n\n6 290 is an even number, because it is evenly divisible by 2: 6 290 / 2 = 3 145.\n\nFind out more:\n\n## Is 6 290 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 6 290 is about 79.310.\n\nThus, the square root of 6 290 is not an integer, and therefore 6 290 is not a square number.\n\n## What is the square number of 6 290?\n\nThe square of a number (here 6 290) is the result of the product of this number (6 290) by itself (i.e., 6 290 × 6 290); the square of 6 290 is sometimes called \"raising 6 290 to the power 2\", or \"6 290 squared\".\n\nThe square of 6 290 is 39 564 100 because 6 290 × 6 290 = 6 2902 = 39 564 100.\n\nAs a consequence, 6 290 is the square root of 39 564 100.\n\n## Number of digits of 6 290\n\n6 290 is a number with 4 digits.\n\n## What are the multiples of 6 290?\n\nThe multiples of 6 290 are all integers evenly divisible by 6 290, that is all numbers such that the remainder of the division by 6 290 is zero. There are infinitely many multiples of 6 290. The smallest multiples of 6 290 are:\n\n## Numbers near 6 290\n\n### Nearest numbers from 6 290\n\nFind out whether some integer is a prime number" ]
[ null ]
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http://fenghs.com/qspevdu_t1001005/
[ "• 防诈骗中心\n• 客服中心 |\n• 网站导航 |\n• 设为主页 |\n• 加入收藏\n• 您当前位置: 首页>产品库>原材料>精细化学品\n相关分类:\n• 湖南\n• 长沙市\n• 常德市\n• 郴州市\n• 衡阳市\n• 怀化市\n• 娄底市\n• 邵阳市\n• 湘潭市\n• 湘西土家族苗族自治州\n• 益阳市\n• 永州市\n• 岳阳市\n• 张家界市\n• 株洲市\n• 山西\n• 长治市\n• 大同市\n• 晋城市\n• 晋中市\n• 临汾市\n• 吕梁市\n• 朔州市\n• 太原市\n• 忻州市\n• 阳泉市\n• 运城市\n• 安徽\n• 安庆市\n• 蚌埠市\n• 亳州市\n• 巢湖市\n• 池州市\n• 滁州市\n• 阜阳市\n• 合肥市\n• 淮北市\n• 淮南市\n• 黄山市\n• 六安市\n• 马鞍山市\n• 宿州市\n• 铜陵市\n• 芜湖市\n• 宣城市\n• 广西\n• 百色市\n• 北海市\n• 崇左市\n• 防城港市\n• 贵港市\n• 桂林市\n• 河池市\n• 贺州市\n• 来宾市\n• 柳州市\n• 南宁市\n• 钦州市\n• 梧州市\n• 玉林市\n• 河南\n• 安阳市\n• 鹤壁市\n• 焦作市\n• 开封市\n• 洛阳市\n• 漯河市\n• 南阳市\n• 平顶山市\n• 濮阳市\n• 三门峡市\n• 商丘市\n• 新乡市\n• 信阳市\n• 许昌市\n• 郑州市\n• 周口市\n• 驻马店市\n• 吉林\n• 白城市\n• 白山市\n• 长春市\n• 吉林市\n• 辽源市\n• 四平市\n• 松原市\n• 通化市\n• 延边朝鲜族自治州\n• 广东\n• 潮州市\n• 东莞市\n• 佛山市\n• 广州市\n• 河源市\n• 惠州市\n• 江门市\n• 揭阳市\n• 茂名市\n• 梅州市\n• 清远市\n• 汕头市\n• 汕尾市\n• 韶关市\n• 深圳市\n• 阳江市\n• 云浮市\n• 湛江市\n• 肇庆市\n• 中山市\n• 珠海市\n• 辽宁\n• 鞍山市\n• 本溪市\n• 朝阳市\n• 大连市\n• 丹东市\n• 抚顺市\n• 阜新市\n• 葫芦岛市\n• 锦州市\n• 辽阳市\n• 盘锦市\n• 沈阳市\n• 铁岭市\n• 营口市\n• 湖北\n• 鄂州市\n• 恩施土家族苗族自治州\n• 黄冈市\n• 黄石市\n• 荆门市\n• 荆州市\n• 直辖行政单位\n• 十堰市\n• 随州市\n• 武汉市\n• 咸宁市\n• 襄阳市\n• 孝感市\n• 宜昌市\n• 江西\n• 抚州市\n• 赣州市\n• 吉安市\n• 景德镇市\n• 九江市\n• 南昌市\n• 萍乡市\n• 上饶市\n• 新余市\n• 宜春市\n• 鹰潭市\n• 浙江\n• 杭州市\n• 湖州市\n• 嘉兴市\n• 金华市\n• 丽水市\n• 宁波市\n• 衢州市\n• 绍兴市\n• 台州市\n• 温州市\n• 舟山市\n• 青海\n• 果洛藏族自治州\n• 海北藏族自治州\n• 海东地区\n• 海南藏族自治州\n• 海西蒙古族藏族自治州\n• 黄南藏族自治州\n• 西宁市\n• 玉树藏族自治州\n• 甘肃\n• 白银市\n• 定西市\n• 甘南藏族自治州\n• 嘉峪关市\n• 金昌市\n• 酒泉市\n• 兰州市\n• 临夏回族自治州\n• 陇南市\n• 平凉市\n• 庆阳市\n• 天水市\n• 武威市\n• 张掖市\n• 贵州\n• 安顺市\n• 毕节市\n• 贵阳市\n• 六盘水市\n• 黔东南苗族侗族自治州\n• 黔南布依族苗族自治州\n• 黔西南布依族苗族自治州\n• 铜仁地区\n• 遵义市\n• 陕西\n• 安康市\n• 宝鸡市\n• 汉中市\n• 商洛市\n• 铜川市\n• 渭南市\n• 西安市\n• 咸阳市\n• 延安市\n• 榆林市\n• 西藏\n• 阿里地区\n• 昌都地区\n• 拉萨市\n• 林芝地区\n• 那曲地区\n• 日喀则地区\n• 山南地区\n• 宁夏\n• 固原市\n• 石嘴山市\n• 吴忠市\n• 银川市\n• 中卫市\n• 福建\n• 福州市\n• 龙岩市\n• 南平市\n• 宁德市\n• 莆田市\n• 泉州市\n• 三明市\n• 厦门市\n• 漳州市\n• 内蒙古\n• 阿拉善盟\n• 巴彦淖尔市\n• 包头市\n• 赤峰市\n• 鄂尔多斯市\n• 呼和浩特市\n• 呼伦贝尔市\n• 通辽市\n• 乌海市\n• 乌兰察布市\n• 锡林郭勒盟\n• 兴安盟\n• 云南\n• 保山市\n• 楚雄彝族自治州\n• 大理白族自治州\n• 德宏傣族景颇族自治州\n• 迪庆藏族自治州\n• 红河哈尼族彝族自治州\n• 昆明市\n• 丽江市\n• 临沧市\n• 怒江傈僳族自治州\n• 曲靖市\n• 思茅市\n• 文山壮族苗族自治州\n• 西双版纳傣族自治州\n• 玉溪市\n• 昭通市\n• 新疆\n• 阿克苏地区\n• 阿勒泰地区\n• 巴音郭楞蒙古自治州\n• 博尔塔拉蒙古自治州\n• 昌吉回族自治州\n• 哈密地区\n• 和田地区\n• 喀什地区\n• 克拉玛依市\n• 克孜勒苏柯尔克孜自治州\n• 直辖行政单位\n• 塔城地区\n• 吐鲁番地区\n• 乌鲁木齐市\n• 伊犁哈萨克自治州\n• 黑龙江\n• 大庆市\n• 大兴安岭地区\n• 哈尔滨市\n• 鹤岗市\n• 黑河市\n• 鸡西市\n• 佳木斯市\n• 牡丹江市\n• 七台河市\n• 齐齐哈尔市\n• 双鸭山市\n• 绥化市\n• 伊春市\n• 香港\n• 香港\n• 九龙\n• 新界\n• 澳门\n• 澳门\n• 其它地区\n• 台湾\n• 台中市\n• 台南市\n• 高雄市\n• 台北市\n• 基隆市\n• 嘉义市\n•", null, "真石漆保温吗-开封真石漆-墙面真石漆\n\n品牌:沪一,胜亚,\n\n出厂地:大化瑶族自治县(大化镇)\n\n报价:面议\n\n上海夺冠化工科技有限公司\n\n黄金会员:", null, "主营:真石漆,水包水,水包砂,无机涂料,弹性涂料\n\n•", null, "水包水多彩仿石漆供货厂家-质量好的水包水多彩仿石漆哪里有卖\n\n品牌:沪一,胜亚,\n\n出厂地:大化瑶族自治县(大化镇)\n\n报价:面议\n\n上海夺冠化工科技有限公司\n\n黄金会员:", null, "主营:真石漆,水包水,水包砂,无机涂料,弹性涂料\n\n•", null, "水包水特色-上海市哪里买好用的水包水多彩仿石漆\n\n品牌:沪一,胜亚,\n\n出厂地:大化瑶族自治县(大化镇)\n\n报价:面议\n\n上海夺冠化工科技有限公司\n\n黄金会员:", null, "主营:真石漆,水包水,水包砂,无机涂料,弹性涂料\n\n•", null, "水包水多彩仿石漆价格行情-福建水包水多彩仿石漆厂家电话\n\n品牌:沪一,胜亚,\n\n出厂地:大化瑶族自治县(大化镇)\n\n报价:面议\n\n上海夺冠化工科技有限公司\n\n黄金会员:", null, "主营:真石漆,水包水,水包砂,无机涂料,弹性涂料\n\n•", null, "外墙真石漆施工报价-真石漆与外墙砖哪个更耐用\n\n品牌:沪一,胜亚,\n\n出厂地:大化瑶族自治县(大化镇)\n\n报价:面议\n\n上海夺冠化工科技有限公司\n\n黄金会员:", null, "主营:真石漆,水包水,水包砂,无机涂料,弹性涂料\n\n•", null, "真石漆施工合同-真石漆与外墙砖哪个更耐用\n\n品牌:沪一,胜亚,\n\n出厂地:大化瑶族自治县(大化镇)\n\n报价:面议\n\n上海夺冠化工科技有限公司\n\n黄金会员:", null, "主营:真石漆,水包水,水包砂,无机涂料,弹性涂料\n\n•", null, "农村外墙真石漆效果图|上海市优良的真石漆供应\n\n品牌:沪一,胜亚,\n\n出厂地:大化瑶族自治县(大化镇)\n\n报价:面议\n\n上海夺冠化工科技有限公司\n\n黄金会员:", null, "主营:真石漆,水包水,水包砂,无机涂料,弹性涂料\n\n•", null, "硅丙真石漆供应商|供应上海市实惠的真石漆\n\n品牌:沪一,胜亚,\n\n出厂地:大化瑶族自治县(大化镇)\n\n报价:面议\n\n上海夺冠化工科技有限公司\n\n黄金会员:", null, "主营:真石漆,水包水,水包砂,无机涂料,弹性涂料\n\n•", null, "天然真石漆房孑效果图-真石漆墙面-天然真石漆\n\n品牌:沪一,胜亚,\n\n出厂地:大化瑶族自治县(大化镇)\n\n报价:面议\n\n上海夺冠化工科技有限公司\n\n黄金会员:", null, "主营:真石漆,水包水,水包砂,无机涂料,弹性涂料\n\n•", null, "上海水包水仿石漆-厂家推荐专业的水包水多彩仿石漆\n\n品牌:沪一,胜亚,\n\n出厂地:大化瑶族自治县(大化镇)\n\n报价:面议\n\n上海夺冠化工科技有限公司\n\n黄金会员:", null, "主营:真石漆,水包水,水包砂,无机涂料,弹性涂料\n\n• 没有找到合适的供应商?您可以发布采购信息\n\n没有找到满足要求的供应商?您可以搜索 精细化学品批发 精细化学品公司 精细化学品厂\n\n### 最新入驻厂家\n\n相关产品:\n真石漆保温吗 水包水多彩仿石漆供货厂家 水包水特色 水包水多彩仿石漆价格行情 外墙真石漆施工报价 真石漆施工合同 农村外墙真石漆效果图 硅丙真石漆供应商 天然真石漆房孑效果图 上海水包水仿石漆" ]
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https://socratic.org/questions/how-do-you-solve-2-1-m-16-using-the-distributive-property
[ "# How do you solve 2(1+m)=16 using the distributive property?\n\nApr 29, 2017\n\nSee the solution process below:\n\n#### Explanation:\n\nFirst, expand the terms on the left side of the equation by multiplying each term within the parenthesis by the term outside the parenthesis:\n\n$\\textcolor{red}{2} \\left(1 + m\\right) = 16$\n\n$\\left(\\textcolor{red}{2} \\cdot 1\\right) + \\left(\\textcolor{red}{2} \\cdot m\\right) = 16$\n\n$2 + 2 m = 16$\n\nNext, subtract $\\textcolor{red}{2}$ from each side of the equation to isolate the $m$ term while keeping the equation balanced:\n\n$- \\textcolor{red}{2} + 2 + 2 m = - \\textcolor{red}{2} + 16$\n\n$0 + 2 m = 14$\n\n$2 m = 14$\n\nNow, divide each side of the equation by $\\textcolor{red}{2}$ to solve for $m$ while keeping the equation balanced:\n\n$\\frac{2 m}{\\textcolor{red}{2}} = \\frac{14}{\\textcolor{red}{2}}$\n\n$\\frac{\\textcolor{red}{\\cancel{\\textcolor{b l a c k}{2}}} m}{\\cancel{\\textcolor{red}{2}}} = 7$\n\n$m = 7$" ]
[ null ]
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https://www.mathematicalway.com/mathematics/geometry/altitude-triangle/
[ "# Altitude of a Triangle", null, "", null, "", null, "", null, "", null, "(No Ratings Yet)", null, "Loading...", null, "The altitude of a triangle, or height, is a line from a vertex to the opposite side, that is perpendicular to that side. It can also be understood as the distance from one side to the opposite vertex.\n\nEvery triangle has three altitudes (ha, hb and hc), each one associated with one of its three sides. If we know the three sides (a, b, and c) it’s easy to find the three altitudes, using the Heron’s formula:", null, "## Altitudes and Orthocenter", null, "The three altitudes of a triangle (or its extensions) intersect at a point called orthocenter.\n\nThe altitude can be inside the triangle, outside it, or even coincide with one of its sides, it depends on the type of triangle it is:\n\nWhere is the orthocenter located?\n\n## Altitude of an Equilateral Triangle", null, "The altitude (h) of the equilateral triangle (or the height) can be calculated from Pythagorean theorem. The sides a, a/2 and h form a right triangle. The sides a/2 and h are the legs and a the hypotenuse.\n\nApplying the Pythagorean theorem:", null, "And we obtain that the height (h) of equilateral triangle is:", null, "", null, "Another procedure to calculate its height would be from trigonometric ratios.\n\nWith respect to the angle of 60º, the ratio between altitude h and the hypotenuse of triangle a is equal to sine of 60º. Therefore:", null, "## Altitude of an Isosceles Triangle", null, "The altitude (h) of the isosceles triangle (or height) can be calculated from Pythagorean theorem. The sides a, b/2 and h form a right triangle. The sides b/2 and h are the legs and a the hypotenuse.", null, "And it is obtained that the height h is:", null, "In a isosceles triangle, the height corresponding to the base (b) is also the angle bisector, perpendicular bisector and median.", null, "In a right triangle the altitude of each leg (a and b) is the corresponding opposite leg. Thus, ha = b and hb = a. The altitude of the hypotenuse is hc.\n\nThe three altitudes of a triangle intersect at the orthocenter H which for a right triangle is in the vertex C of the right angle.\n\nTo find the height associated with side c (the hypotenuse) we use the geometric mean altitude theorem.", null, "We can calculate the altitude h (or hc) if we know the three sides of the right triangle.", null, "Download this calculator to get the results of the formulas on this page. Choose the initial data and enter it in the upper left box. For results, press ENTER.\n\nNote. Courtesy of the author: José María Pareja Marcano. Chemist. Seville, Spain.\n\n## Exercise", null, "Find the lengths of the three altitudes, ha, hb and hc, of the triangle Δ ABC, if you know the lengths of the three sides: a=3 cm, b=4 cm and c=4.5 cm.\n\nFirstly, we calculate the semiperimeter (s).", null, "We get that semiperimeter is s = 5.75 cm. Then we can find the altitudes:", null, "The lengths of three altitudes will be ha=3.92 cm, hb=2.94 cm and hc=2.61 cm.\n\n## Lines Associated with a Triangle\n\nAUTHOR: Bernat Requena Serra\n\nYEAR: 2020" ]
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https://www.enotes.com/homework-help/what-is-the-formula-for-pressure-125729
[ "# What is the formula for pressure?\n\nThe formula for pressure is P = F/A, in which P is pressure, F is force, and A is area.", null, "The formula for pressure is\n\nP = F/A\n\nIn this equation, P stands for pressure while F stands for force and A stands for area.  Pressure is typically measured in a unit called the Pascal.\n\nSo what this means is that the amount of pressure that is exerted on an area is determined by the size of that area and by the amount of force that is pressing against it.\n\nTherefore, if you have a given amount of force, you will have more pressure if it presses down on a small area than if it presses down on a large area." ]
[ null, "https://static.enotescdn.net/images/main/illustrations/illo-answer.svg", null ]
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http://ignoumbaassignments.com/ms-8-ignou-mba-assignments-jan-jun-2017/?replytocom=767
[ "# MS 8 IGNOU MBA Assignments Jan – Jun 2017\n\n1. The net incomes of a sample of large importers of antiques were organized into the following table:\n\n Net Income (\\$ millions) Number of Importers 2 up to 6 1 6 up to 10 4 10 up to 14 10 14 up to 18 3 18 up to 22 2\n\n(a) What is the table called?\n(b) Based on the distribution, what is the estimate of the arithmetic mean net income?\n(c) Based on the distribution, what is the estimate of the standard deviation?\n\n2. The employees of Cartwright Manufacturing are awarded efficiency ratings based on such factors as monthly output, attitude, and attendance. The distribution of the ratings follows the normal probability distribution. The mean is 400, the standard deviation 50.\n\n(a) What is the area under the normal curve between 400 and 482? Write this area in probability notation.\n(b) What is the area under the normal curve for ratings greater than 482? Write this area in probability notation.\n(c) Show the facets of this problem in a chart.\n\n3. Advertisements by Star Fitness Center claim that completing its course will result inlosing weight. A random sample of eight recent participants showed the following weights before and after completing the course. At the .01 significance level, can we conclude that the students lost weight?\n\n Name Before After Himmat 155 154 Chandan 228 207 Mohan 141 147 Meera 162 157 Cimola 211 196 Peterson 164 150 Reddy 184 170 Prakash 172 165\n\n(a) State the null hypothesis and the alternate hypothesis.\n(b) What is the critical value of t?\n(c) What is the computed value of t?\n(d) Interpret the result. What is the p-value?\n(e) What assumption needs to be made about the distribution of the differences?\n\n4. What is time series analysis? Decompose a time series into its various components and describe them.\n\n5. What is a random variable? How is it used to define a probability distribution? Make the\nprobability distribution of “scores facing up” in a throw of two dice.\n\n1.", null, "Tanya sharma says\n\nWhere is answer of ms-8 plzz give me a ans of newmarical of ms-8\n\n•", null, "admin says\n\nDear Tanya,\n\nYou can purchase the assignment for Rs 150.\n\nRegards\n\nIMA\n9818565507\n\n•", null, "heba says\n\ncan u provide ans of q1, q2,q3 before 8 am tomorrw ?" ]
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https://www.zbmath.org/?q=an%3A1432.65079
[ "# zbMATH — the first resource for mathematics\n\nIterative solution of piecewise linear systems for the numerical solution of obstacle problems. (English) Zbl 1432.65079\nSummary: We investigate the use of piecewise linear systems, whose coefficient matrix is a piecewise constant function of the solution itself. Such systems arise, for example, from the numerical solution of linear complementarity problems and in the numerical solution of free-surface problems. In particular, we here study their application to the numerical solution of both the (linear) parabolic obstacle problem and the obstacle problem. We propose a class of effective semi-iterative Newton-type methods to find the exact solution of such piecewise linear systems. We prove that the semi-iterative Newton-type methods have a global monotonic convergence property, i.e., the iterates converge monotonically to the exact solution in a finite number of steps. Numerical examples are presented to demonstrate the effectiveness of the proposed methods.\n\n##### MSC:\n 65K10 Numerical optimization and variational techniques 90C33 Complementarity and equilibrium problems and variational inequalities (finite dimensions) (aspects of mathematical programming) 90C53 Methods of quasi-Newton type\nFull Text:" ]
[ null ]
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https://www.comsol.com/multiphysics/heat-transfer-conservation-of-energy?parent=fluid-flow-heat-transfer-and-mass-transport-0402-442
[ "", null, "", null, "## Heat Transfer: Conservation of Energy\n\nFluid Flow, Heat Transfer, and Mass Transport   Heat Transfer: Conservation of Energy\n\n### The Energy Equation\n\nThe first law of thermodynamics defines the internal energy by stating that the change in internal energy for a closed system, ΔU, is equal to the heat supplied to the system,", null, ", minus the work done by the system,", null, ":\n\n(1)", null, "If the system is allowed to move, Equation (1) can be extended to include the kinetic energy for the system,", null, ":\n\n(2)", null, "Equation (2) can be written for an infinitely small volume of fluid and the result is known as the equation for conservation of total internal energy (Ref. 1):\n\n(3)", null, "In this equation:\n\n•", null, "is the density\n•", null, "is the internal energy per unit mass\n•", null, "is the velocity vector\n•", null, "is the square of the velocity magnitude\n•", null, "is the conductive heat flux vector\n•", null, "is the total stress tensor\n•", null, "is the body force per unit mass; i.e., the volume force\n\nThe total stress tensor is commonly written as:\n\n(4)", null, "where", null, "denotes pressure and", null, "is the viscous stress tensor.\n\nUsing this definition of", null, ", the second term on the right-hand side of Equation (3), which represents the work of surface forces, can be written as\n\n(5)", null, "The first term on the right-hand side is commonly referred to as pressure work, while the second term is known as viscous work. These terms can be further decomposed in the following way:\n\n(6)", null, "The upper row in Equation (6) represents reversible effects; i.e., they can describe work that increases the internal energy and how internal energy can produce work. The bottom row describes irreversible effects; i.e., how work increases the internal energy through so-called viscous dissipation and how viscous effects reduce the kinetic energy.\n\nEquation (3) contains the equation for conservation of kinetic energy. This equation can be derived by taking the dot product of the velocity,", null, ", with the momentum equation. Some algebraic manipulation yields: (7)", null, "It can be seen that all of the work of the body forces in the total energy equation (3) goes to change the kinetic energy. The rest of the right-hand side of Equation (7) consists of the parts of the surface force work term described in Equation (6) as affecting the kinetic energy. Subtracting Equation (7) from Equation (3) gives the equation for internal energy: (8)", null, "In case there are internal heat sources caused by, for example, reactions or interaction with radiation, an additional internal heat source term,", null, ", is added and the internal energy equation becomes:\n\n(9)", null, "### The Enthalpy Equation\n\nInternal energy is a thermodynamic state variable that is seldom used in practical applications. A more commonly used quantity is the enthalpy,", null, ", that is related to the internal energy through:\n\n(10)", null, "Using Equation (10) in (9) and rearranging it gives the enthalpy equation (Ref. 2):\n\n(11)", null, "Equation (11) is written in its so-called conservative form. This refers to the way that the left-hand side is written with the density and velocity inside the divergence operator. A so-called nonconservative form of the enthalpy equation can be derived by use of the continuity equation. The left-hand side of Equation (11) can be expanded in the following way:\n\n(12)", null, "The first term on the right-hand side of Equation (12) is the continuity equation multiplied by the enthalpy, and it is therefore identically zero. Equation (11) can hence be written as:\n\n(13)", null, "Equation (13) still describes the conservation of enthalpy, even if the equation form is denoted nonconservative.\n\n### The Temperature Equation\n\nAll engineers are familiar with the concept of temperature, therefore it is convenient to express the conservation of energy in terms of temperature. Enthalpy is related to temperature,", null, ", and pressure through the following differential relation:\n\n(14)", null, "where", null, "is the heat capacity at constant pressure and β is the bulk expansion coefficient.\n\nEquation (14) can be used to replace", null, "in Equation (13). Invoking the continuity equation once again gives the temperature equation:\n\n(15)", null, "The final step is to define the conduction heat flux vector,", null, ", using Fourier's law of conduction,", null, ", where", null, "is the thermal conductivity. The temperature equation then reads:\n\n(16)", null, "Observe that the temperature equation cannot be recast on a conservative form without reverting to enthalpy or internal energy.\n\nThe temperature equation is yet another way to express conservation of energy that is mathematically equivalent to Equation (3). However, the different conservation equations do not behave equivalently when implemented using a numerical method. Many commercial codes are based on a finite volume method and they solve a transport equation on conservative form for the total enthalpy. In this way, the commercial codes achieve conservation of total energy. The total enthalpy equation, however, is prone to numerical oscillations that reduce the numerical accuracy. It is much more robust and accurate to solve the temperature equation. The finite element method allows for the solution of the temperature equation and still conserves total energy (Ref. 3).\n\n### Special Cases of Energy Conservation\n\nFor ideal gases, the term", null, "is equal to unity, and (16) becomes: (17)", null, "If the fluid is incompressible, the pressure work term vanishes and Equation (16) reduces to:\n\n(18)", null, "The pressure work term can also be neglected for most engineering applications, unless the system undergoes a significant pressure change or if the Mach number is close to unity or higher.\n\nThe viscous heating is important in some special cases involving very high shear rates. Some engineering examples are bearings and hydraulic systems. However, viscous heating can be neglected in most other cases, and Equation (18) then simplifies further to:\n\n(19)", null, "Published: June 29, 2018" ]
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null, 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null, 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null, 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null, 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null, 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", null, 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null, 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null, 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null, 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null, 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null, 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null, 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null, 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null, 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null, 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null, 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null, 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mVsACFQUy1BZG9iZS0yLjAgRVBTRi0yLjBgJCIfAAAAAElFTkSuQmCC", null, 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", null, 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null, 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", null, 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null, 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null, 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null, 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null, 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null, 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", null, 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null, 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", null, 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null, 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mLlhFAMvSwFU1xIPDPp6oAybzqOSEWASilBiPrWqhVbGLCGbduCSXpWHGMB0A899Hc4RUNFT34pwh9I1oYOAnkRjU9LRu7wZlca3+LqZSnocSFpnO3B6u/eMZRzW7qBub7rXR2k6kH1zHAtF1pLttBvDauyBWKGYzxSw8RGKz3xxspCoolHMD0Xo4aKSl75QtcXA2TNedLGhtRJ62ajlyX7RX9QR33IyGrHI6Wd6+hSwH28qP6Rpfemn9PIMCNdXVRuTs31Xe/oQCWo9cHEwZZd5jLYQo81rM4WmOFArlgnpVH65l2aD9+eoKFfZYFV713EKfPaqWMBNCqgkym0sdOu624z1LZkWllqj6BnFlY3ExK9fYtuR/ZFf7HRpfftBscTv6+nmsnN8l036kDUJnItPdiwhQFrWJktqGTSwZom6Wu+dMTB9ZJM01DWk7PabUlcAQrVvdYqiGwQQGHLbTAaHb8cISTWWKjhYCoBSCJEghQJBK4qNchS3cQiszCXK7FTy3Ygq0kH1cguwLWlBxu2gF5r2LYt9MzIS0IYZuTTNPQru01KMx9iOgGIKVvZE7V+PFIpBe2WZ8ImyhUSl2pvlARk1taqiGTW7lKKJ34bZCmwMm3wNNHroBYMI8HaIzsbtmC0zIxt24JpRs6LBpAkpGkUN01DxZz8jBM9IPFABIlseFO1ChEkBVlrOw+V0ge+6AsPpMhmDp3hv4qIk1SRVpZ5QR0WeCWsZYHSJ61Mv4DeHhIwCsAg8DE/scMkW9BK4tIWXtd/r/QSf3CizP0LvU95gobKVQdi4FlrnD9ckKhaZ+JLeEhTdnNxc4BU3Sr94I+KdLLMKOu5RNwUXSDmXGeZ0lvXzFIkceQpksZEMw3JQRJPRdr/6drDDVB/SCBdopkZawtLWMOr2rChTUNJJ3UFSHRHRl0ZJmhoSZ/kmd68lzwSh+PfzE93kasu4m09N95oWV/v7IplXBLLIpNGRTMt4ruef/dnuXjEbdnC+2IOK6/1OTKYNLSOQyMEBQCCVwaBbdyeQG6h9G6KpLnJlmbR2Guxye5sYTytPfLpvzZoaB2VPEsKsBFVOKKVIumFZEszIIkAEUKKrK9FH9kWXtBdn4bWUck9g3RSJM1OtjSr9GjDPuILQM93HP9kakCz458Gf2vUkPNKnjkczl9ge7l8xwmGxpbfTpG0x7i8tdqCu9Pd8vLvmHmsVYbzSu62j3CdYGhs+eYUSej3/NrUuevHtgV7HPpIZtcJhsaWb06RBKDf88ufuz4S17ZgE+c9uTtcJxiaUL4hRVJOn+eXP3d9FK5twS5H7sn7EwytpvyeFEmYlmzJY8S1LVjlyJW8P8HQeso3p0gCtn46ylpwbQtWOXIl708wtJ7yzSmSgK2fjrIWXNuCVQ47J3edYGh8+aYUSTnbjsVaBa5twTaHreTvSDC0WPnaFElricvbAa5twTLHreQCkboTd+bZPKF8FdMHJGTtWCfU3WGGIYYAAncI8PmHKe8W17ZgmePOySViQLmbz04qX6Xqoc4vuGgEeIBDqjsiQ4DqkXFtC5Y5aE/+tpiqtZT/UCnJfBwgX7zWznBtC/Y5ak/+lgRD6ylfpVQs0C2evHDzuLYF6xy1kt9nnIG67fJl7uIRYsFs87vAtS1Y56DDdZsJhlZVfrXmLhGThMTZL7s1cW0L9jloJT8K5XYbA1e/4X3jDslRh+tHQ+7NVdMzHl/JDwAxCMQkXr+SZ4v44foQnC75q7efsr4UKm0n8KEwd+TcWVClR4ev5P0kSMrTtfZUIXh5V36WvntmpMz0eDxbws/JPZ6d83/z/3SqkZq0+gAAACV0RVh0ZGF0ZTpjcmVhdGUAMjAyMC0wOS0wMlQxMjozMzozMSswMDowMPIBWyQAAAAldEVYdGRhdGU6bW9kaWZ5ADIwMjAtMDktMDJUMTI6MzM6MzErMDA6MDCDXOOYAAAAEXRFWHRwZGY6U3BvdENvbG9yLTAAK87xEVgAAAARdEVYdHBkZjpTcG90Q29sb3ItMQArzzN7bwAAACJ0RVh0cHM6SGlSZXNCb3VuZGluZ0JveAAyOTl4MzgrMTU2KzYxNolTFFsAAAAfdEVYdHBzOkxldmVsACFQUy1BZG9iZS0yLjAgRVBTRi0yLjBgJCIfAAAAAElFTkSuQmCC", null, 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null, 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null, 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", null, 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null, 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null, 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null, 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", null, 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null, 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", null, 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https://www.dummies.com/personal-finance/investing/technical-analysis/how-to-find-a-pivot-point-support-and-resistance-channel-in-a-trading-chart/
[ "", null, "How to Find a Pivot Point Support and Resistance Channel in a Trading Chart - dummies\n\n# How to Find a Pivot Point Support and Resistance Channel in a Trading Chart\n\nOne technique for dealing with sideways moves within a trading chart channel is to draw horizontal support and resistance lines off pivot points. Technical traders use the term pivot point in a few different ways.\n\n• One standard definition is that the pivot point is the center bar of three bars (or more) where the center bar is the highest high or lowest low.\n\n• Another definition of pivot is the median price (the numerical average of the high, low, and close). Today, this version is probably the most accepted.\n\n## Calculating the first zone of support and resistance\n\nThe logic of the pivot point is that after a trend pauses, you need a breakout that’s a significant distance from the median price to decide whether the old trend will resume or a reversal is really at hand. So you start with the median price:\n\n• Add a factor to get upside resistance.\n\n• Subtract a factor to get downside support.\n\nTo calculate the first (inner) line of resistance:\n\n1. Multiply the pivot point value by two.\n\n2. From the number you calculate in Step 1, subtract the low of the pivot day.\n\nThe result is named R1.\n\nTo calculate the first (inner) line of support, or S1:\n\n1. Multiply the pivot value by two.\n\n2. From the number you calculate in Step 1, subtract the high of the pivot day.\n\nThis procedure sounds like a lot of arithmetic, but don’t sweat it. It’s easy enough to do in a spreadsheet or by hand, and many trading platforms offer it as a standard option. Plus, the procedure itself is quite sensible — you use a multiple of the median price to estimate a range going forward that subtracts the high and the low to yield a norm. Any price higher or lower would be an extreme. If the upcoming price breaks the horizontal support and resistance lines calculated this way, the direction of the breakout is your clue that the trend is truly over.\n\nYou can create a series of pivot support and resistance lines according to these formulas or some variation of them:\n\n• Pivot Point = (High + Close + Low)/3\n\n• Support 1 = 2 × Pivot – High\n\n• Support 2 = Pivot – (R1 – S1)\n\n• Support 3 = Low – 2 × (High – Pivot)\n\n• Resistance 1 = 2 × Pivot – Low\n\n• Resistance 2 = Pivot + (R1 – S1)\n\n• Resistance 3 = High + 2 × (Pivot – Low)\n\nIn this figure, R3 is very close to the highest high and S3, while higher than the recent lowest low, meets the hand-drawn support line connecting two lows.", null, "When many market participants are looking at the same pivot-point lines, you can expect price movement at exactly those lines.\n\n## Using pivot support and resistance\n\nIn the case presented in this figure, if you bought at Point A, you’d set your target at R1 if you’re risk averse, R2 if you’re an optimist, and R3 if you’re swinging at the bases. Note that a test of a previous high is commonplace in a bounce off a low. If you’re able to go short, you may sell at R3 and target a gain to S3, which conveniently meets the hand-drawn support line.", null, "What’s important about the pivot-based support and resistance lines is that they effectively outline a period of activity where traders don’t know the trend. Bulls try to make a new high and get only a few pennies worth. Bears try to make a new low but fail to get a significant lower low.\n\nPivot analysis is most useful in periods of congestion or sideways action after an old trend has ended and a new one has not yet emerged." ]
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https://www.physicsforums.com/threads/dfa-regular-expression.265064/
[ "# DFA -> Regular Expression\n\n## Main Question or Discussion Point\n\nIs there an algorithm for converting DFA (or NFA) into regular expressions?\n\nYes, while I have no idea whether it is the most efficient (probably not), one of the easiest ways is to convert the DFA or NFA into a GNFA (generalized nondeterministic finite automaton) and start collapsing its states till only one transition is left, and then take that as the regular expression.\n\nA GNFA is simply a NFA that accepts regular expressions on arrows instead of just symbols. The general idea is as follows:\n1. Take any NFA, and add two states we call start and end. Add an epsilon-arrow from start to the previous start state, and add an epsilon-arrow from all previous final states to the end state. Now start is the only start state, and end is the only end state.\n2. If start and end are the only states then we take the regular expression on the arrow between them and are done, if not we go to 3.\n3. We pick a state Q that is not start or end. Let R be the arrow from Q to itself. Now from every state A that has an arrow C to Q, for every state B that has an arrow D from Q we add an arrow from A to B with the label CR*D.\n4. We remove the state Q and all arrows to it, since we have constructed replacements.\n5. If there exist two states A and B such that there are several arrow from A to B, then we reduce them to one by taking the union of all the arrows.\n6. Go to step 2." ]
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https://answers.everydaycalculation.com/compare-fractions/2-50-and-2-20
[ "Solutions by everydaycalculation.com\n\n## Compare 2/50 and 2/20\n\n2/50 is smaller than 2/20\n\n#### Steps for comparing fractions\n\n1. Find the least common denominator or LCM of the two denominators:\nLCM of 50 and 20 is 100\n\nNext, find the equivalent fraction of both fractional numbers with denominator 100\n2. For the 1st fraction, since 50 × 2 = 100,\n2/50 = 2 × 2/50 × 2 = 4/100\n3. Likewise, for the 2nd fraction, since 20 × 5 = 100,\n2/20 = 2 × 5/20 × 5 = 10/100\n4. Since the denominators are now the same, the fraction with the bigger numerator is the greater fraction\n5. 4/100 < 10/100 or 2/50 < 2/20\n\nMathStep (Works offline)", null, "Download our mobile app and learn to work with fractions in your own time:\nAndroid and iPhone/ iPad\n\nand" ]
[ null, "https://answers.everydaycalculation.com/mathstep-app-icon.png", null ]
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https://or.stackexchange.com/questions/4834/how-to-represent-time-window-as-constraint-in-a-vehicle-routing-problem
[ "How to represent time window as constraint in a vehicle routing problem\n\nHi I am trying to solve a vehicle routing problem using Tabu search, I have successfully completed implementation of constraints for CVRP by giving penalties to objective function , how do I implement time window as a constraint?\n\n• You can define a penalty for each node and activate it when the time window is violated. Sep 11 '20 at 21:23\n\nVehicle Routing Problem with Time Window constraints Let imagine a logistics network consisting of a warehouse and numerous retailers. All stocks enter into the logistics network through the depot and from this one the goods are distributed to the retails via a fleet of vehicles. Each retailer (customer) specifies to the load to be delivered. In addition, if retailer specifies a period of time (time window) in which the delivery should occur then the model is called Vehicle Routing Problem with Time Window constraints(VRPTW). The objective is to find a set of routes which minimizes the total length of the routes or the number of used vehicles without violating the vehicle capacity and time window constraints. Let the index set of the $$n$$ retailers be denoted $$N=1,2, \\cdots, n$$.\n\nLet the load which has to be delivered be $$w_i$$.\n\nLet the earliest starting time for the service of unload be $$r_i$$. The value of $$r_i$$ can be thought as a release time of the i-th job in machine scheduling environment so that it designates the time job (retailer) is available for processing.\n\nLet the duration of unloading activity be $$d_i$$ that is the time required to complete the service. The value of $$d_i$$ can be thought as the processing time of the i-th job in the machine scheduling environment\n\nLet the latest termination time for the service be $$l_i$$ that is the time the service can end. The value of $$l_i$$ can be thought as the due date for the i-th job.\n\nFor the depot (the depot is located at the origin, $$i=0$$ ) and for each retailer there is a time window\n\n$$[r_i, l_i]$$\n\nduring which it must be served where $$i=0,1, 2, \\cdots, n$$. The service start time at each node must be $$\\geq r_i$$ and the arrival time at each node must be $$\\leq l_i$$. If a vehicle arrives at time $$ then the vehicle must wait before starting to serve the retailer.\n\n$$r_i < l_i - d_i$$\n\nor $$r_i = l_i - d_i$$ if there is not a slack between release time and due date.\n\nNote that $$r_i, l_i, d_i$$ are parameters and are known without uncertainty.\n\nTW Constraint\n\nLet $$x_{i,k,m}$$ be a Boolean variable: $$x_{i,k,m} = 1$$ if m-th vehicle travels from i-th node to k-th node, zero otherwise. For simplicity, we will suppose m=1. Let $$t_k$$ be a continuous decision variable representing the arrival time at node $$k$$ that is instant the service can start. We assign a travel time $$t_{ij}$$ to every edge i-j. The time window constraint can be formulated as:\n\n$$t_i \\geq r_i$$ and $$t_i \\leq l_i$$ for all $$i=1,2, \\cdots, n$$.\n\nLet assume the travel times $$t_{ij}$$ satisfy the triangle inequality, i.e.\n\n$$t_{ik} + t_{kj} \\geq t_{ij}$$ for all $$i=1,2, \\cdots, n$$.\n\nThe generic temporal constraints can be formulated as\n\n$$\\left\\{ \\begin{array}{l} t_j \\geq t_i + (r_j – l_i + d_i + t_{ij} ) \\cdot x_{i,j} – M \\cdot (l_i – r_j) \\cdot (1- x_{i,j}) \\\\ t_i \\geq r_i \\\\ t_i \\leq l_i \\\\ t_i , t_j \\ge 0 \\end{array} \\right.$$\n\n• I have solved the problem by considering traveling time instead of distance, and checked( total time travelled + unloading time < latest delivery time) Sep 24 '20 at 4:46" ]
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https://journals.calstate.edu/pump/article/view/147
[ "# Differences of Harmonic Numbers and the abc-Conjecture\n\n• Natalia da Silva California State University, Dominguez Hills\n• Serban Raianu California State University, Dominguez Hills\n• Hector Salgado California State University, Dominguez Hills\nKeywords: harmonic numbers; modular arithmetic; exponential Diophantine equation; Gersonides' Theorem; abc-conjecture; Dirichlet's Theorem\n\n### Abstract\n\nOur main source of inspiration was a talk by Hendrik Lenstra on harmonic numbers, which are numbers whose only prime factors are two or three. Gersonides proved 675 years ago that one can be written as a difference of harmonic numbers in only four ways: 2-1, 3-2, 4-3, and 9-8. We investigate which numbers other than one can or cannot be written as a difference of harmonic numbers and we look at their connection to the abc-conjecture. We find that there are only eleven numbers less than 100 that cannot be written as a difference of harmonic numbers (we call these ndh-numbers). The smallest ndh-number is 41, which is also Euler's largest lucky number and is a very interesting number. We then show there are infinitely many ndh-numbers, some of which are the primes congruent to 41 modulo 48. For each Fermat or Mersenne prime we either prove that it is an ndh-number or find all ways it can be written as a difference of harmonic numbers. Finally, as suggested by Lenstra in his talk, we interpret Gersonides's theorem as \"The abc-conjecture is true on the set of harmonic numbers\" and we expand the set on which the abc-conjecture is true by adding to the set of harmonic numbers the following sets (one at a time): a finite set of ndh-numbers, the infinite set of primes of the form 48k+41, the set of Fermat primes, and the set of Mersenne primes.\n\nPublished\n2018-01-05\nHow to Cite\nda Silva, N., Raianu, S., & Salgado, H. (2018). Differences of Harmonic Numbers and the abc-Conjecture. The PUMP Journal of Undergraduate Research, 1, 1-13. Retrieved from https://journals.calstate.edu/pump/article/view/147\nSection\nArticles" ]
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https://www.bartleby.com/solution-answer/chapter-18-problem-42p-college-physics-11th-edition/9781305952300/a-coffee-maker-is-rated-at-1-200-w-a-toaster-at-1-100-w-and-a-waffle-maker-at-1-400-w-the-three/91bb43ec-98d6-11e8-ada4-0ee91056875a
[ "", null, "", null, "", null, "Chapter 18, Problem 42P\n\nChapter\nSection\nTextbook Problem\n\nA coffee maker is rated at 1 200 W, a toaster at 1 100 W, and a waffle maker at 1 400 W. The three appliances are connected in parallel to a common 120-V household circuit. (a) What is the current in each appliance when operating independently? (b) What total current is delivered to the appliances when all are operating simultaneously? (c) Is a 15-A circuit breaker sufficient in this situation? Explain.\n\n(a)\n\nTo determine\n\nThe current passing through coffee maker, toaster and waffle maker.\n\nExplanation\n\nGiven Info: The rated power of the coffee maker is 1200 W and toaster is 1100 W, the potential difference across the household circuit is 120V.\n\nFormula to calculate the current drawn by coffee maker operating separately is,\n\nIC=PCΔV\n\n• IC is the current drawn by coffee maker,\n• PC is the rated power of the coffee maker,\n• ΔV is the potential difference across the household circuit,\n\nSubstitute 1200W for PC and 120V for ΔV.\n\nIC=1200W120V=10A\n\nThus, the current drawn by coffee maker is 10A.\n\nFormula to calculate the current drawn by toaster operating separately is,\n\nIT=PTΔV\n\n• IT is the current drawn by toaster,\n• PT is the rated power of the toaster,\n• ΔV is the potential difference across the household circuit,\n\nSubstitute 1100W for PT and 120V for ΔV\n\n(b)\n\nTo determine\n\nThe total current delivered to the three appliances.\n\n(c)\n\nTo determine\n\nThe total required current of 15 A exceeds the limit of the circuit breaker.\n\nStill sussing out bartleby?\n\nCheck out a sample textbook solution.\n\nSee a sample solution\n\nThe Solution to Your Study Problems\n\nBartleby provides explanations to thousands of textbook problems written by our experts, many with advanced degrees!\n\nGet Started", null, "" ]
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https://ncatlab.org/nlab/show/chromatic%20homotopy%20theory
[ "# nLab chromatic homotopy theory\n\nContents\n\ncohomology\n\n### Theorems\n\n#### Stable Homotopy theory\n\nstable homotopy theory\n\nIntroduction\n\n# Contents\n\n#### Higher algebra\n\nhigher algebra\n\nuniversal algebra\n\n# Contents\n\n## Idea\n\nBy the construction of complex oriented cohomology theories from formal groups (via the Landweber exact functor theorem), the height filtration of formal groups induces a “chromaticfiltration on complex oriented cohomology theories. Chromatic homotopy theory is the study of stable homotopy theory and specifically of complex oriented cohomology theories by means of and along this chromatic filtration.\n\nMore abstractly, this filtering is induced by the prime spectrum of a symmetric monoidal stable (∞,1)-category of the (∞,1)-category of spectra for p-local finite spectra, which is labeled by the Morava K-theories.\n\nMore in detail, for each prime $p \\in \\mathbb{N}$ and for each $n \\in \\mathbb{N}$ there is a Bousfield localization of spectra\n\n$L_n \\coloneqq L_{K(0)\\vee \\cdots \\vee K(n)} \\,,$\n\nwhere $K(n)$ is the $n$th Morava K-theory (for the given prime $p$). These arrange into the chromatic tower which for each spectrum $X$ is of the form\n\n$X \\to \\cdots \\to L_n X \\to L_{n-1} X \\to \\cdots \\to L_0 X \\,.$\n\nThe chromatic convergence theorem states mild conditions under which the homotopy limit over this tower is the $p$-localization\n\n$X \\to X_{(p)}$\n\nof $X$.\n\nSince moreover $L_n X$ is the homotopy fiber product (see at smash product theorem and see this remark at fracture square )\n\n$L_n X \\simeq L_{K(n)}X \\underset{L_{n-1}L_{K(n)}X}{\\times} L_{n-1}X$\n\nit follows that in principle one may study a spectrum $X$ by understanding all its “chromatic pieces” $L_{K(n)} X$.\n\n## Examples\n\nchromatic homotopy theory\n\nchromatic levelcomplex oriented cohomology theoryE-∞ ring/A-∞ ringreal oriented cohomology theory\n0ordinary cohomologyEilenberg-MacLane spectrum $H \\mathbb{Z}$HZR-theory\n0th Morava K-theory$K(0)$\n1complex K-theorycomplex K-theory spectrum $KU$KR-theory\nfirst Morava K-theory$K(1)$\nfirst Morava E-theory$E(1)$\n2elliptic cohomologyelliptic spectrum $Ell_E$\nsecond Morava K-theory$K(2)$\nsecond Morava E-theory$E(2)$\nalgebraic K-theory of KU$K(KU)$\n3 …10K3 cohomologyK3 spectrum\n$n$$n$th Morava K-theory$K(n)$\n$n$th Morava E-theory$E(n)$BPR-theory\n$n+1$algebraic K-theory applied to chrom. level $n$$K(E_n)$ (red-shift conjecture)\n$\\infty$complex cobordism cohomologyMUMR-theory\n\n### Stable case\n\nA quick idea is given in section 6 of\n\nA good historical introduction is in\n\nComprehensive lecture notes are in\n\nBrief surveys include\n\nA lightning review of results by Henn with Goerss, Mahowald, Rezk, and Karamanov is in\n\n• Hans-Werner Henn, Recent developments in stable homotopy theory (pdf,)\n\nA collection of various lecture notes and other material is kept at\n\nRandom useful discussion is in\n\n• Glossary for stable and chromatic honotopy theory (pdf)\n\nDiscussion of generalization of elliptic cohomology to higher chromatic homotopy theory is discussed in\n\n• Doug Ravenel, Toward higher chromatic analogs of elliptic cohomology pdf\n\n• Doug Ravenel, Toward higher chromatic analogs of elliptic cohomology II, Homology, Homotopy and Applications, vol. 10(1), 2008, pp.1-36 (pdf, pdf slides)\n\nRelation of chromatic homotopy theory to Goodwillie calculus is discussed in\n\n• Greg Arone, Mark Mahowald, The Goodwillie tower of the identity functor and the unstable periodic homotopy of spheres, Inventiones mathematicae\n\nFebruary 1999, Volume 135, Issue 3, pp 743-788 (pdf)\n\n• Nicholas Kuhn, Goodwillie towers and chromatic homotopy: an overview, Geom. Topol. Monogr. 10 (2007) 245-279 (arXiv:math/0410342)\n\nCategorical ultraproducts are used to provide asymptotic approximations in\n\n• Tobias Barthel, Tomer Schlank, Nathaniel Stapleton, Chromatic homotopy theory is asymptotically algebraic, (arXiv:1711.00844)\n\n### Unstable case\n\nThere are also chromatic approximations in ordinary (not stabilized) homotopy theory:" ]
[ null ]
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https://www.geckodrive.com/support/step-motor-basics.html
[ "Support\n\nStep Motor Basics\n\nYou can read our famous Stepper Motor Basics Guide all on one page here or skip to any chapter by clicking the links in the drop-down menu to the right.\n\nSection 1: Motor Theory\n\nA stepper motor is a constant output power transducer, where power is defined as torque multiplied by speed. This means motor torque is the inverse of motor speed. To help understand why a step motor’s power is independent of speed, we need to construct (figuratively) an ideal step motor.\n\nAn ideal stepper motor would have zero mechanical friction, its torque would be proportional to ampere-turns and its only electrical characteristic would be inductance. Ampere-turns simply means that torque is proportional to the number of turns of wire in the motor’s stator multiplied by the current passing through those turns of wire.\n\nAnytime there are turns of wire surrounding a magnetic material such as the iron in the motor’s stator, it will have an electrical property called inductance. Inductance describes the energy stored in a magnetic field anytime current passes through this coil of wire.\n\nInductance (L) has a property called inductive reactance, which for the purposes of this discussion may be thought of as a resistance proportional to frequency and therefore motor speed.\n\nAccording to Ohm’s law, the current is equal to voltage divided by resistance. In this case, we substitute inductive reactance for resistance in Ohm’s law and conclude motor current is the inverse of motor speed.\n\nSince torque is proportional to ampere-turns (current times the number of turns of wire in the winding), and current is the inverse of speed, torque also has to be the inverse of speed.\n\nIn an ideal stepper motor, as speed approaches zero, its torque would approach infinity while at infinite speed torque would be zero. Because current is proportional to torque, the motor current would be infinite at zero as well.\n\nElectrically, a real motor differs from an ideal one primarily by having a non-zero winding resistance. Also, the iron in the motor is subject to magnetic saturation, as well as having eddy current and hysteresis losses. Magnetic saturation sets a limit on the current to torque proportionally while eddy current and hysteresis (iron losses) along with winding resistance (copper losses) cause motor heating.\n\nSection 2: Speed-Torque Curve Basics\n\nIn the previous section, it was shown that motor torque varies inversely with speed. This then is the motor’s natural speed-torque curve. Below a certain speed, called the corner speed, the current would rise above the motor’s rated current, ultimately to destructive levels as the motor’s speed is reduced further. This can be seen in Figure 1.", null, "Figure 1\n\nTo prevent this, the drive must be set to limit the motor current to its rated value. Because torque is proportional to current, motor torque is constant from zero speed to the corner speed. Above the corner speed, motor current is limited by the motor’s inductive reactance.", null, "Figure 2\n\nThe result now is a two-part speed-torque curve that features constant torque from zero speed until it intersects the motor’s natural load line, called the corner speed, beyond which the motor is in the constant power region. This is illustrated in Figure 2.\n\nA real stepper motor has losses that modify the ideal speed-torque curve. The most important effect is the contribution of detent torque. Detent torque is usually specified in the motor datasheet. It is always a loss when the motor is turning and the power consumed to overcome it is proportional to speed. In other words, the faster the motor turns the greater the detent torque contributes power loss at the motor’s output shaft. This power loss is proportional to speed and must be subtracted from the ideal, flat output power curve past the corner speed. This now constitutes a practical speed-torque curve.", null, "Figure 3\n\nNotice how in Figure 3 the power output decreases with speed because of the constant-torque loss due to detent torque and other losses. The same effect causes a slight decrease in torque with speed in the constant torque region as well. Finally, there is a rounding of the torque curve at the corner speed because the drive gradually transitions from being a current source to being a voltage source. The drive limits current to the motor below the corner speed and thus is a current source. Above the corner speed, the motor’s inductive reactance limits the current and the drive becomes a voltage source as it applies all of the power supply voltage to the motor.\n\nSection 3: Mid-Band Instability\n\nA stepper motor is highly resonant because it is a mass-spring system. The “mass” portion is the rotor and load inertia while the “spring” portion is the restoring torque of the magnetic field that drags the rotor along. Because of this, velocity lags torque by 90 degrees.\n\nThe drive is a current source in the constant torque region and adds no additional phase lag. In the constant power region, however, the drive is a voltage source so it introduces an additional 90-degree phase lag. The total phase lag now is 180 degrees, which is a setup for a sustained and building motor oscillation. This oscillation is commonly called mid-band instability or mid-band resonance.\n\nThe drive remedies this instability by adding a second-order, or viscous, damping. This damping decreases the total phase lag so the motor cannot sustain oscillation, much in the same way shock absorbers damp the mass-spring suspension of a vehicle. This is illustrated in Figure 4.\n\nThe figure below shows the effect of uncompensated mid-band resonance. Though it is possible to accelerate through the resonant region, it is not possible to operate the motor continuously in the speed band. This is because the oscillation that causes the motor to stall takes from half a second to 10 seconds to build to an amplitude sufficient to stall the motor.", null, "Figure 4\n\nSection 4: Motor Power Basics\n\nThe motor power output (speed times torque) is determined by the power supply voltage and the motor’s inductance. The motor’s output power is proportional to the power supply voltage divided by the square root of the motor inductance.\n\nIf one changes the power supply voltage, then a new family of speed-torque curves results. As an example, if the power supply voltage is doubled then a new curve is generated; the curve now has twice the torque at any given speed in region 2. Since power equals torque times speed, the motor now generates twice as much power as well. This is illustrated in Figure 5.", null, "Figure 5", null, "Figure 6\n\nFigure 6 shows the effect of rewiring the motor from full-winding to half-winding while keeping the same power supply voltage. A half-winding connected motor delivers twice as much power as a full-winding connection at a given power supply voltage. This is because full-winding inductance is four times higher than half-winding inductance.\n\nAlso, note from Figure 5 that motor output doubles when the power supply voltage is doubled for either series or parallel-wired motors. Notice that a parallel-connected motor delivers performance identical to a series-connected motor running at twice the power supply voltage.\n\nFigure 7 shows the effect of setting the motor current to twice the rated value. This abuses the motor because it will dissipate four times as much heat as setting the current to its proper value. The actual increase in low-speed torque is considerably less than double because of the magnetic saturation of the motor iron.", null, "Figure 7\n\nWhat can be seen is there is not increase in the power output; the motor simply reaches its maximum power at a lower speed, all at the great expense of a four-fold increase in motor heating.\n\nIt is recommended the motor current always be set at the rated value also to get the best microstep smoothness. Setting the current higher degrades the linearity of the motor and causes microstep bunching and attendant low-speed vibration.\n\nWhat comes with the increased motor power with increased power supply voltage is increased motor heating; this heating increases more rapidly than output power and ultimately sets the maximum output power from the motor. That is to say, the limiting factor in how much power a motor can deliver is ultimately determined by how much heat it can safely dissipate.\n\nSection 5: Motor Connections\n\nStepper motors have four, six, or eight wires; older motors may have five wires, but they will not be covered here.\n\nFour-wire motors are the simplest to connect and offer no connection options. Simply connect one winding to the terminals labeled “Phase A” and “Phase /A” and connect the other winding to the terminals that say “Phase B” and “Phase /B”. If it is unknown which wires belong to which phase, simply use an ohmmeter and test which wires have continuity. The ones that have continuity will belong to the same phase; if the motor turns the wrong direction when connected just swap “Phase A” and “Phase /A”. A typical four-wire motor connection is illustrated in Figure 8.", null, "Figure 8\n\nSix-wire motors are the most common. There are two connection options: Full-winding and half-winding. A six-wire motor is just like a four-wire motor except there is a center tap on each of two windings, for a total of six wires. For a half-winding connection, the center tap and one of the end wires are used. This is illustrated in Figure 9.", null, "Figure 9\n\nFor a full-winding connection as seen in Figure 10, the center tap is ignored and both end wires are used. The term “full-winding” is exactly equivalent to “series” connected while “half-winding” is virtually identical to “parallel” connected. The choice between the two is application dependent, which is discussed later; just remember to set the drive current to exactly half the motor’s rated unipolar current rating if it is wired in full-winding and set it to the unipolar current rating if wired in half-winding.", null, "Figure 10\n\nEight-wire motors are about 3% more efficient when parallel-connected than an equivalent half-winding connected six-wire motor, but are considerably more complicated to connect. There is no advantage when comparing a series connection to a full-winding connection. As in a six-wire motor, the choice between series versus parallel connection is application dependent. Remember to set the drive current to exactly half of the motor’s rated parallel (as wired in Figure 11) current rating when using the series connection shown in Figure 12.", null, "Figure 11", null, "Figure 12\n\nSection 6: Power Supplies\n\nThe choice of a power supply is determined by the voltage, current, and power supply type (i.e. switching versus linear, regulated versus unregulated, etc.). By far the most problematic and complicated factor is voltage, which will be discussed last.\n\nThe easiest factor in choosing a power supply is its current rating, which is based on your motor ratings. A motor control will always draw less than 2/3 of the motor’s rated current when it is parallel (or half-winding) connected and 1/3 of the motor’s rated current when it is series (or full-winding) connected. That is to say, a 6 amp per phase motor will require a 4 amp power supply when wired in parallel and a 2 amp power supply when wired in series. If multiple motors and drives are used, add the current requirements of each to arrive at the total power supply current rating.", null, "Figure 13\n\nWhen using multiple drives from a common power supply, use individual supply and ground wires to each drive and return them to a common point back at the power supply. This is called a “star” power supply distribution; never use a “daisy-chain” power distribution, where the supply and ground wires for the next drives are picked up from the previous one.\n\nThe voltage of your power supply is entirely dependent on the inductance rating of your motor, which we learned is translatable to the number of turns of wire in the stator. Every motor model will have a different inductance rating and will therefore have a different maximum voltage. To figure out what the maximum power supply voltage should be, use the following formula with the motor’s inductance in millihenries (mH) used for the L value.\n\n32 * SQRT (L) = VMAX\n\nIf you are using several different models of motors on the same power supply use the lowest inductance rating in the above formula. This will ensure that your motors will not overheat due to the voltage being too high.\n\nShould a motor not list the inductance it will generally list the voltage rating of each winding, which will be very low. An acceptable way of determining your power supply voltage if this is the only information you have is to multiply this number by any number between 4 and 20. In Figure 14 you could use a power supply voltage anywhere from 8.8V to 44V if wired in parallel.", null, "Figure 14\n\nAn unregulated power supply will be sufficient and is recommended for most applications because of its simplicity. If a motor with a large inertial load decelerates quickly it will act as an alternator and send voltage back to the drive which then sends it back to the power supply. Because many regulated power supplies feature protection circuitry this may cause the power supply to fault or reset; however, if the supply is unregulated it will simply get absorbed by the filter capacitor.\n\nTo make your own power supply you must have three key components: a transformer, bridge rectifier, and filter capacitor. The transformer’s current rating must be sufficient to adequately run all motors that will be run from it using the above current formula. The DC output voltage will be 1.4 times the transformer’s AC voltage rating of the secondary. For example, a 24VAC transformer secondary will provide about 34VDC at the output of the supply. The bridge rectifier’s voltage and current ratings must exceed what the supply will deliver. Finally, the minimum filter capacitor size must be calculated. Use the following equation to do this:\n\n(80,000 * I) / V = C\n\nThe result will be in microfarads for the capacitor if the value for “I” is amperes of current needed and “V” is the output voltage of the supply. When picking the capacitor, any value equal to or greater than the calculated value can be used. Be sure to use a capacitor with a voltage rating of at least 20% higher than the output voltage of the power supply. A sample 68VDC 5A power supply is shown in Figure 15.", null, "Figure 15\n\nThere is a special consideration if the power supply will be at or near the maximum voltage rating of the drive. If the motor will be rapidly decelerating a large inertial load from a high speed, care has to be taken to absorb the returned energy. The energy stored in the momentum of the load must be removed during deceleration and be safely dissipated. Because of its efficiency, the drive has no means of dissipating this energy so it returns it to the power supply. In effect, instead of drawing current from the power supply, the drive becomes a source of current itself. This current may charge the power supply capacitor to destructive voltage levels.\n\nIf more than one drive is being operated from the power supply this is not a problem since the other drive(s) will absorb this current for its needs, unless it is decelerating as well. For this case or for a single drive it may be necessary to place a voltage clamp across the power supply in the form of a Zener diode. The voltage of this diode must be greater than the maximum expected power supply voltage, yet low enough to protect the drive. A good choice would be either 82 volts or 91 volts as standard values.\n\nSection 7: Motor Heating and Power Supply Voltage\n\nThere are two major causes of motor heating: copper losses and iron losses. Copper losses are the easiest to understand; this is the heat generated by current passing through a resistance, as in the current passing through the motor’s winding resistance. Often this is referred to as “I2R” dissipation.\n\nThis cause of motor heating is at a maximum when the motor is stopped and rapidly diminishes as the motor speeds up since the inductive current is inversely proportional to speed.\n\nEddy current and hysteresis heating are collectively called iron losses. The former induces currents in the iron of the motor while the latter is caused by the re-alignment of the magnetic domains in the iron. You can think of this as “friction heating” as the magnetic dipoles in the iron switch back and forth. Either way, both cause the bulk heating of the motor. Iron losses are a function of AC current and therefore the power supply voltage.\n\nAs shown earlier, the motor output power is proportional to the power supply voltage, doubling the voltage doubles the output power. However, iron losses outpace motor power by increasing non-linearly with increasing power supply voltage. Eventually, the point is reached where the iron losses are so great that the motor cannot dissipate the heat generated. In a way, this is nature’s way of keeping someone from getting 500HP from a NEMA 23 motor by using a 10kV power supply.\n\nAt this point, it is important to introduce the concept of overdrive ration. This is the ratio between the power supply voltage and the motor’s rated voltage. An empirically derived maximum is 25:1, meaning the power supply voltage should never exceed 25 times the motor’s rated voltage or 32 times the square root of motor inductance. Below is a graph of measured iron losses for a 4A, 3V motor. Notice in Figure 16 how the iron losses range from insignificant to being the major cause of heating in the motor compared to a constant 12W copper loss (4A times 3V).", null, "Figure 16\n\nSection 8: Accuracy and Resolution\n\nStepper motors, by and large, are used in open-loop positioning and velocity applications. There is not a feed-back transducer to set the ultimate accuracy of the system. Consequently, it falls on the motor and the drive’s precision and behavior to determine the accuracy of the application.\n\nThrough microstepping, second-order damping and precision sine/cosine current references, the drive has cured the stepper motor of its inherent vices to make it a candidate for precision motion control applications. Neglecting the drive, the motor still has characteristics that must be considered in regard to ultimate accuracy in any application.\n\nA stepper motor is a mechanical device that is manufactured to a certain tolerance. Typically a standard motor has a tolerance of +/- 5% nonaccumulative error regarding the location of any given step. This means that any step on a typical 200 step per revolution motor will be within a 0.18-degree error range. Stated otherwise, the motor can accurately resolve 2000 radial locations. Coincidentally this is the resolution of a 10 microstep drive.\n\nAny microstep resolution beyond 10, such as 125, yields no additional accuracy, only empty resolution. By analogy, a voltmeter having a 6 digit display while having 1% accuracy would have meaningful information only in the first two digits. There are two exceptions justifying higher resolutions: The stepper motor is being run in a closed-loop application with a high-resolution encoder or the application requires smooth operation at very low speeds (below 5 full steps per second).\n\nAnother factor affecting accuracy is motor linearity. Motor linearity refers to how the motor behaves between its ordinal step locations. Ideally, a 1.8 degree per step motor should move exactly 0.18 degrees for every step pulse sent to a 10 microstep drive. In reality, all stepper motors exhibit some non-linearity, meaning the microsteps bunch together rather than being spread evenly over the span of a full step. This has two effects: Statically the motor position is not optimum and dynamically low-speed resonances occur because of the cyclic acceleration where the microsteps are spread apart and deceleration where they bunch up. Figure 17 shows a motor with excellent linearity and one with horrible linearity.\n\nFinally, the static friction load applied to the motor affects accuracy. A stopped motor, which has 100 oz/in of holding torque, is fundamentally different than a brake that has the same holding torque.", null, "Figure 17\n\nThe brake will not turn at all until its holding torque is exceeded. However, a stepper motor only generated restoring torque if it is displaced from its rest position. Using the brake analogy, think of the output shaft being connected to the break with a torsional spring; now when applying a load, the output shaft has to be laterally displaced to apply torque to the brake.\n\nWhen lateral torque sufficient enough to overcome the holding torque is applied to a step motor, the shaft will jump to the next stable location which is four full steps ahead or behind the original one, depending on the direction of the lateral torque. Peak restoring torque occurs a full step ahead or behind the original location, beyond which it weakens and reverses at the two full step position to attract the shaft to a four full step location ahead or behind the original one.\n\nThe relationship between restoring torque and shaft error angle is approximately sinusoidal as shown in Figure 18.", null, "Figure 18\n\nFrom this one may approximate that a static torque load equal to 15 percent of the holding torque will displace the motor shaft one-tenth of a full step from the origin.\n\nSection 9: Choosing a Step Motor and Power Supply Voltage\n\nThe choice of a stepper motor and power supply voltage is entirely application dependent. Ideally, the motor should deliver sufficient at the highest speed the application requires and no more.\n\nAny torque capability in excess of what the application requires comes at the high cost of unnecessary motor heating. Excess torque capability beyond a reasonable safety margin will never be used but will exact the penalty of an oversized power supply, drive stress, and motor temperature.\n\nLearn to distinguish the difference between torque and power; high initial torque at low speed does not mean efficient motor utilization. Usually, power is the more important measure of a motor’s suitability to an application. To determine this, you must bias the motor’s operating point through power transmission gearing to operate the motor at its maximum power; normally just past its corner frequency.\n\nThe maximum shaft power sustainable with a drive running at 80VDC and 7A is around 250W, or one-third of a horsepower. This is primarily achieved with double or triple stacked NEMA 34 motors.\n\nNEMA 23 motors are physically too small to dissipate the resultant hear and NEMA 42 motors are too big to be properly impedance matched; if their current is less than a 7A drive’s limit then the voltage will generally be above the maximum voltage of 80VDC and vice versa.\n\nThe detent torque on a NEMA 42 motor is significantly higher than in smaller motors and is always a loss that must be subtracted from the potentially available power output of the motor. In other words, the output power of a NEMA 42 motor drops more rapidly with speed than smaller motors. A NEMA 42 motor should be used only if high torque is required at low speed and it is not practical to gear down a smaller motor.\n\nAn efficient motor, defined as the smallest motor sufficient to meet the demands of the application, will run hot. Think of the motor as having fixed power conversion efficiency: Some percentage of the input power will be converted to heat and the rest will be converted to mechanical power. To get the maximum performance from the motor, the waste heat must be just under what the motor can tolerate. Usually, this motor will be biased to operate just past the corner speed as well.\n\nThe place to start is to determine the load torque in oz/in, including the torque necessary to accelerate the load. The next step is to come up with the maximum speed the application has to operate at in full steps per second using the formula below. RPI is the revolutions per inch after the motor turns through the transmission, RPS is revolutions per second and PPS is the number of pulses per second from your step pulse source.\n\n(DESIRED IPM * RPI) / 60 = RPS\n\nRPS * 200 = PPS\n\nMultiply the PPS value by the number of oz/in determined previously and divide the total by 4506. The answer will be how many watts mechanical are required the motor to meet the load from the application.\n\nWhen picking a motor, choose one with 40% more than the calculated power. Below is an example of the equation completed for a load requiring 450 oz/in with a 3 TPI leadscrew and the desired IPM of 300.\n\n(300 * 3) / 60 = 15\n\n15 * 200 = 3000\n\n(3000 * 450) / 4506 = 299 OZ/IN\n\n299 * 1.4 = 419 OZ/IN\n\nAs you can see, you will want to use a motor with a rating of 419 oz/in for this application.\n\nGeckodrive is a leading manufacturer of stepper motor drives in the United States. Our products are used in applications across a range of industries. Looking to purchase a high-quality stepper motor driver? Browse our selection of industry-leading motor controllers today.\n\n1. Motor Theory Section 1: Motor Theory  A stepper motor is a constant output power transducer, where power is defined as torque multiplied by speed. This means motor torque is the inverse of motor speed. To help understand why a step motor’s power is independent of speed, we need to construct ...\n2. Speed-Torque Section 2: Speed-Torque Curve Basics In the previous section, it was shown that motor torque varies inversely with speed. This then is the motor’s natural speed-torque curve. Below a certain speed, called the corner speed, the current would rise above the motor’s rated current, ultimately ...\n3. Mid-Band Instability Section 3: Mid-Band Instability A stepper motor is highly resonant because it is a mass-spring system. The “mass” portion is the rotor and load inertia while the “spring” portion is the restoring torque of the magnetic field that drags the rotor along. Because of this, velocity lags ...\n4. Motor Power Section 4: Motor Power Basics The motor power output (speed times torque) is determined by the power supply voltage and the motor’s inductance. The motor’s output power is proportional to the power supply voltage divided by the square root of the motor inductance. If one changes the power ...\n5. Motor Wiring Section 5: Motor Connections Stepper motors have four, six, or eight wires; older motors may have five wires, but they will not be covered here.  Four-wire motors are the simplest to connect and offer no connection options. Simply connect one winding to the terminals labeled “Phase A” ...\n6. Power Supply Basics Section 6: Power Supplies The choice of a power supply is determined by the voltage, current, and power supply type (i.e. switching versus linear, regulated versus unregulated, etc.). By far the most problematic and complicated factor is voltage, which will be discussed last. The easiest ...\n7. Motor Heating Section 7: Motor Heating and Power Supply Voltage There are two major causes of motor heating: copper losses and iron losses. Copper losses are the easiest to understand; this is the heat generated by current passing through a resistance, as in the current passing through the motor’s winding ...\n8. Accuracy and Resolution Section 8: Accuracy and Resolution Step motors by and large are used in open loop positioning and velocity applications. There is not feed-back transducer to set the ultimate accuracy of the system. Consequently it falls on the motor and the drive’s precision and behavior to determine the ...\n9. Choosing a Motor Section 9: Choosing a Step Motor and Power Supply Voltage The choice of a stepper motor and power supply voltage is entirely application dependent. Ideally, the motor should deliver sufficient at the highest speed the application requires and no more. Any torque capability in excess of what ...\nSet Descending Direction" ]
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https://cs.stackexchange.com/questions/93202/dfs-and-bfs-time-and-space-complexities-of-number-of-islands-on-leetcode
[ "# DFS and BFS Time and Space complexities of 'Number of islands' on Leetcode\n\nHere is the question description. The first 2 suggested solutions involve DFS and BFS. This question refers to the 1st two approaches: DFS and BFS. Apparently, the grid can be viewed as a graph.\n\nI have included the problem statement here for easier reading.\n\nGiven a 2d grid map of '1's (land) and '0's (water), count the number of\nislands. An island is surrounded by water and is formed by connecting adjacent\nlands horizontally or vertically. You may assume all four edges of the grid are\nall surrounded by water.\n\nExample 1:\n\nInput:\n11110\n11010\n11000\n00000\n\nOutput: 1\n\nExample 2:\n\nInput:\n11000\n11000\n00100\n00011\n\nOutput: 3\n\n\nI am unclear as to why the time complexity for both DFS and BFS is O(rows * columns) for both. I see how this is the case where the grid is just full of 0's - we simply have to check each cell. However, doesn't the DFS approach add more time to the search? Even if we mark the cells we visited by changing them to 0 in the dfs methods, we still would revisit all the cells because of the two outer loops. If dfs could be have time complexity of O(n) in the case of a big grid with large row and column numbers, wouldn't the time complexity be O(rows * columns * max[rows, cols])? Moreover, isn't the same case with the BFS approach where it is O(rows * cols * possibleMaxSizeOfQueue) where possibleMaxSizeOfQueue could again be max[rows, cols]?\n\nfor (int r = 0; r < nr; ++r) {\nfor (int c = 0; c < nc; ++c) {\nif (grid[r][c] == '1') {\n++num_islands;\ndfs(grid, r, c);\n}\n}\n}\n\n\nHow is DFS's space complexity O(rows*cols)? Is it not possible/common to consider the call stack space as freed when a recursion branch returns? How is the space complexity for BFS O(min(rows, cols))? The way I see it, the queue could be full of all elements in the case of a grid with just 1's thereby giving O(rows*cols) for BFS space complexity.\n\nDFS Solution\n\nclass Solution {\nvoid dfs(char[][] grid, int r, int c) {\nint nr = grid.length;\nint nc = grid.length;\n\nif (r < 0 || c < 0 || r >= nr || c >= nc || grid[r][c] == '0') {\nreturn;\n}\n\ngrid[r][c] = '0';\ndfs(grid, r - 1, c);\ndfs(grid, r + 1, c);\ndfs(grid, r, c - 1);\ndfs(grid, r, c + 1);\n}\n\npublic int numIslands(char[][] grid) {\nif (grid == null || grid.length == 0) {\nreturn 0;\n}\n\nint nr = grid.length;\nint nc = grid.length;\nint num_islands = 0;\nfor (int r = 0; r < nr; ++r) {\nfor (int c = 0; c < nc; ++c) {\nif (grid[r][c] == '1') {\n++num_islands;\ndfs(grid, r, c);\n}\n}\n}\n\nreturn num_islands;\n}\n}\n\n\nTime complexity : O(M×N) where M is the number of rows and N is the number of columns.\n\nSpace complexity : worst case O(M×N) in case that the grid map is filled with lands where DFS goes by M×N deep.\n\nBFS Solution\n\nclass Solution {\npublic int numIslands(char[][] grid) {\nif (grid == null || grid.length == 0) {\nreturn 0;\n}\n\nint nr = grid.length;\nint nc = grid.length;\nint num_islands = 0;\n\nfor (int r = 0; r < nr; ++r) {\nfor (int c = 0; c < nc; ++c) {\nif (grid[r][c] == '1') {\n++num_islands;\ngrid[r][c] = '0'; // mark as visited\nwhile (!neighbors.isEmpty()) {\nint id = neighbors.remove();\nint row = id / nc;\nint col = id % nc;\nif (row - 1 >= 0 && grid[row-1][col] == '1') {\ngrid[row-1][col] = '0';\n}\nif (row + 1 < nr && grid[row+1][col] == '1') {\ngrid[row+1][col] = '0';\n}\nif (col - 1 >= 0 && grid[row][col-1] == '1') {\ngrid[row][col-1] = '0';\n}\nif (col + 1 < nc && grid[row][col+1] == '1') {\ngrid[row][col+1] = '0';\n}\n}\n}\n}\n}\n\nreturn num_islands;\n}\n}\n\n\nTime complexity : O(M×N) where M is the number of rows and N is the number of columns.\n\nSpace complexity : O(min(M,N)) because in worst case where the grid is filled with lands, the size of queue can grow up to min(M,N)." ]
[ null ]
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https://howtodiscuss.com/t/how-is-150-related-to-30-on-the-unit-circle/14772
[ "", null, "# How is \\$150^@\\$ related to \\$30^@\\$ on the unit circle?\n\nHow is 150 related to 30 on the unit circle??\n\nCarl S.\n\nMar 13, 2018\n\n150˚ is the mirror image of 30˚ across the x-axis if that makes sense…\n\nExplanation:\n\nIf you look at the unit circle you can see that both angles are rotated by 60˚ from 90˚ (the x-axis) but in opposite directions.\n30˚ = 90˚ - 60˚\n150˚ = 90˚ + 60˚\nThis means that\nsin(30˚)= sin(150˚)\nand\ncos(30˚) = -cos(150˚)" ]
[ null, "https://howtodiscuss.com/uploads/default/original/2X/4/4f8caf28ea0fd81cc384aecad0bc0eb7d8fb041a.png", null ]
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https://www.physicsforums.com/threads/resistors-in-a-circuit.369228/
[ "# Resistors in a Circuit\n\n• the-alchemist\n\n## Homework Statement\n\nI have been stuck at the following question for some time now. All help is appreciated.", null, "P=IV, V=IR\n\n## The Attempt at a Solution\n\nI have resolved the right side of the circuit into a 10 ohm resistor. I have also found the current in the 20 ohm resistor (0.4A). I then used Ohm's Law to get the current in the 10 ohm resolved resistor and found it to be 5A. Then using Kirchoff's Current Law, I got 5.4A in the unknown resistor R, which gives a resistance of 9.26 ohms.\n\nThis 9.26 ohms however disagrees with the given answer of 10 ohms.\n\nWhere have I went wrong? All help is appreciated!\n\nThanks!\n\nYou didn't apply Ohm's Law correctly. 50 volts isn't the voltage drop across any of the individual resistors; it's the voltage drop across the entire combination of resistors. Each resistor will have a smaller voltage drop across it.\n\nIf you take the two equations you have, you can combine them to get\n\n$$P=\\frac{V^2}{R}$$\n\nP is the power dissipated by a resistor of resistance R, and V is the voltage drop across the resistor. Since you're given the power dissipated by the 20-ohm resistor, you can use the formula to calculate the voltage across the 20-ohm resistor. Then you can use Ohm's Law to calculate the current through the resistor.\n\nUltimately, what you want to figure out is the voltage drop across the unknown resistor and the current flowing through it because then you can use Ohm's Law to calculate its resistance.\n\nYou didn't apply Ohm's Law correctly. 50 volts isn't the voltage drop across any of the individual resistors; it's the voltage drop across the entire combination of resistors. Each resistor will have a smaller voltage drop across it.\n\nIf you take the two equations you have, you can combine them to get\n\n$$P=\\frac{V^2}{R}$$\n\nP is the power dissipated by a resistor of resistance R, and V is the voltage drop across the resistor. Since you're given the power dissipated by the 20-ohm resistor, you can use the formula to calculate the voltage across the 20-ohm resistor. Then you can use Ohm's Law to calculate the current through the resistor.\n\nUltimately, what you want to figure out is the voltage drop across the unknown resistor and the current flowing through it because then you can use Ohm's Law to calculate its resistance.\n\nI've tried this method as well but I get stuck after calculating the voltage for the 20 ohm resistor. Correct me if I'm wrong but I thought any resistor that is parallel to an ideal voltage source has no effect on the voltage or current in the rest of the circuit.\n\nI'm still unable to get the answer of 10 ohms. Shucks.\n\nI've tried this method as well but I get stuck after calculating the voltage for the 20 ohm resistor. Correct me if I'm wrong but I thought any resistor that is parallel to an ideal voltage source has no effect on the voltage or current in the rest of the circuit.\nYes, this is true. The voltage source will source as much current as is needed to maintain a fixed voltage across its terminals. Anything connected to those terminals will see that voltage drop regardless of what else is connected to them as well, like a resistor.\n\nTwo elements in a circuit are in parallel only if they are connected to the same two nodes of the circuit, so in the circuit, none of the resistors is in parallel with the voltage source because none of them connect directly to both the top and the bottom of the source.\n\nI'm still unable to get the answer of 10 ohms. Shucks.\nWhat did you get for the current and voltage for the 20-ohm resistor?\n\nThe 20-ohm resistor and 10-ohm resistor are in parallel, right? So what quantity do they have in common?\n\nHow is the current through R related to the currents through the 20-ohm and 10-ohm resistors?\n\nTwo elements in a circuit are in parallel only if they are connected to the same two nodes of the circuit, so in the circuit, none of the resistors is in parallel with the voltage source because none of them connect directly to both the top and the bottom of the source.\n\nThis really helped me! Thanks!\n\nWhat did you get for the current and voltage for the 20-ohm resistor?\n\nThe 20-ohm resistor and 10-ohm resistor are in parallel, right? So what quantity do they have in common?\n\nHow is the current through R related to the currents through the 20-ohm and 10-ohm resistors?\n\nI think I got it now. Correct me if I'm wrong, the current for the 20 ohm resistor is 1A and voltage of 20V.\n\nThe 20 ohm and 10 ohm resistors are parallel thus they share the same voltage drop.\n\nUsing the voltage divider principle I was able to get 10 ohms for R after resolving the parallel resistors 20 and 10 ohms into 6.67 ohms with 20V as the voltage drop across the 6.67 ohm resistor. Can anyone confirm that this method/ way of doing is appropriate and correct?\n\nYes, that's correct.\n\nYou could have also calculated the current through the 10-ohm resistor since you know the voltage across it. The current through R would be the sum of the currents through the 10-ohm and 20-ohm resistors, and voltage across R would be the difference between the 50 V supplied by the battery and the 20-V drop across the 20-ohm and 10-ohm resistor combination. Divide the voltage by the current, and you'd get the same answer." ]
[ null, "https://www.physicsforums.com/attachments/whzoe-png.131361/", null ]
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https://factorization.info/greatest-common-factor/61/724/gcf-of-61-and-724.html
[ "GCF of 61 and 724", null, "On this page we will define the GCF of 61 and 724, teach you the different ways of calculating the GCF of 61 and 724, and show you what you can use the GCF of 61 and 724 for.\n\nWhat is the GCF of 61 and 724?\nGCF is the abbreviation for Greatest Common Factor. Therefore, the GCF of 61 and 724 is the same as the Greatest Common Factor of 61 and 724. The GCF of 61 and 724 is the largest positive integer by which both 61 and 724 can be divided. Furthermore, both 61 and 724 have a set of factors and the GCF is the greatest factor that 61 and 724 have in common.\n\nCompare factors to get GCF of 61 and 724\nPer definition above, to find the GCF of 61 and 724, you can compare the factors of 61 with the factors of 724 to see which factor is the greatest. When we did that, we found that the Greatest Common Factor (GCF) of 61 and 724 is 1.\n\nUse LCM to get GCF of 61 and 724\nThe Least Common Multiple (LCM) of 61 and 724 is 44164. You can find the GCF of 61 and 724 by dividing the product of 61 and 724 by the LCM of 61 and 724. Here is the formula and math:\n\n Product of 61 and 724 LCM of 61 and 724\n=  GCF\n\n 61 × 724 44164\n=  1\n\nUse computer spreadsheet to get GCF of 61 and 724\nIf you have a computer, you can also use a spreadsheet in Excel or Numbers to calculate the GCF of 61 and 724. You want to type =gcf(61, 724) into a cell to get the answer.\n\ngcf(61, 724) = 1\n\nUse the GCF of 61 and 724 to simplify a fraction\nThe GCF of 61 and 724 can be used for many things. You can, for example, simplify a fraction by dividing the numerator and denominator by the GCF like this:\n\n 61 ÷ 1 724 ÷ 1\n=\n 61 724\n\nUse GCF of 61 and 724 to simplify a ratio\nSimilarly, you can use the GCF of 61 and 724 to simplify a ratio by dividing each part of the ratio by the GCF like this:\n\n= 61 : 724\n= (61 ÷ 1) : (724 ÷ 1)\n= 61 : 724\n\nUse the GCF of 61 and 724 to find the LCM of 61 and 724\nSince using the Least Common Multiple (LCM) is one of the ways to find the GCF of 61 and 724, you can use the GCF of 61 and 724 to find the LCM of 61 and 724. The LCM of 61 and 724 can, for example, be used to add and subtract fractions with denominators of 61 and 724. The LCM of 61 and 724 is the product of 61 and 724 divided by the GCF of 61 and 724. Here is the math:\n\n Product of 61 and 724 GCF of 61 and 724\n=  LCM\n\n 61 × 724 1\n=  44164\n\nThat is all there is to it! We hope this page accomplished its goal of defining the GCF of 61 and 724 by showing you how to calculate the GCF, examples of its uses, and how it relates to LCM.\n\nGCF Calculator\nUse the GCF Calculator to solve a problem similar to the one explained on this page.\n\nGCF of 61 and 725\nHere is the next GCF on our list that we have calculated and explained for you." ]
[ null, "https://factorization.info/images/gcf.png", null ]
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https://mathoverflow.net/questions/292015/zeros-of-holomorphic-function-in-n-variables/292030
[ "# zeros of holomorphic function in n variables\n\nConjecture: Let $f:{\\mathbb C}^n\\rightarrow{\\mathbb C}$ be an entire function in $n$ complex variables. Assume that for every $x\\in{\\mathbb R}^n$ there exists a $y_x\\in{\\mathbb R}^n$ such that $f(x+iy_x)\\equiv f(x_1+iy_{x,1},\\ldots,x_n+iy_{x,n})=0$. Then $f\\equiv 0$. (We don't assume continuity of $x\\mapsto y_x$.)\n\nRemarks:\n\n1. The conjecture is true for $n=1$: If $f$ satisfies the hypothesis, it has uncountably many different zeros, namely $\\{ x+iy_x\\ | \\ x\\in{\\mathbb R}\\}$. Since ${\\mathbb C}$ is $\\sigma$-compact, there exists a compact $K\\subset{\\mathbb C}$ containing uncountably many zeros of $f$. Thus the set of zeros of $f$ has an accumulation point in $K$, and by a well-known result $f$ vanishes identically.\n\n2. The argument for $n=1$ does not adapt trivially to higher $n$ since holomorphic functions of severable variables have no isolated zeros.\n\n3. In the conjecture it is important that $x$ consists of the real and $y$ of the imaginary parts of the variables. For example, the following is not true: Assuming that\n$f:{\\mathbb C}^2\\rightarrow{\\mathbb C}$ is entire and for every $z_1=x_1+iy_1$ there is a $z_2=x_2+iy_2$ such that $f(z_1,z_2)=0$, we have $f\\equiv 0$. A trivial counterexample is $f(z_1,z_2)=z_1-z_2$.\n\n4. Most books on holomorphic functions in several variables devote some attention to the set of zeros of such a function. Usually this leads to a proof of Weierstrass' preparation theorem, where the discussion ends. This is of no immediate help to me, since I would actually be happy with a proof of the conjecture for polynomials in $n$ complex variables! In this case, Weierstrass' theorem does not give any new information.\n\nThe conjecture is obviously false even for $n=2$. Check $f(z,w)=(w-z^2)(z-(w+1)^2)$. Write $z=x+iy$ and $w=u+iv$. Given $x$ and $u$, I can make first term zero unless $u>x^2$. I can make the second term zero unless $x>(u+1)^2$. Since both inequalities can not be true, we are done.\n\n• Thanks. Nice answer. I'll have to see whether there are additional hypotheses in the application that I have in mind. – M Mueger Feb 2 '18 at 17:01\n\nNot a complete answer, but perhaps in the many-variable case you could leverage Theorem 5.1 from\n\nChirka, E.M., Complex analytic sets. (Kompleksnye analiticheskie mnozhestva), Moskva: ”Nauka”. Glavnaya Redaktsiya Fiziko-Matematicheskoj Literatury. 272 p. R. 3.70 (1985). ZBL0586.32013.\n\nWhich states that for an analytic set $Z \\subset \\mathbb{C}^n$, like the zero set of $f(z) = 0$, the regular part $\\operatorname{reg} Z \\subset Z$ (which consists of all points around which $Z$ is a complex submanifold) consists of a union of connected components $\\operatorname{reg} Z = \\bigcup_j S_j$, which is locally finite. That is, for any compact $K\\subset \\mathbb{C}^n$, $K$ intersects at most finitely many of the $S_j$. The singular part $\\operatorname{sng} Z = Z \\setminus \\operatorname{reg} Z$ is also an analytic set, but of lower dimension. So a similar argument applies to it.\n\nThe above reference also contains a wealth of other information about complex analytic sets that might be of use.\n\n• Well, the zero-set of a holomorphic function is an analytic set and therefore locally a unit of holomorphic (n-1)-manifolds. But I don't see how this helps approaching the conjecture, where real and imaginary parts of the variables are treated differently. – M Mueger Feb 2 '18 at 15:32\n• As the counter example in Oleg's answer showed, the obstruction to the conjecture is local (unlike in the $n=1$ case). Had there been non local obstruction, the local finiteness of the union of connected components might have come in useful. – Igor Khavkine Feb 3 '18 at 10:12" ]
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https://lists.boost.org/Archives/boost/2002/04/27733.php
[ "", null, "# Boost :\n\nFrom: Joerg Walter (jhr.walter_at_[hidden])\nDate: 2002-04-07 15:02:37\n\nHi Peter,\n\nyou wrote:\n\n> > Yes ;-) I think, the corresponding documentation doesn't state clearly\n> > enough, that the assignment of proxies like matrix_range has the same\n> > semantics as the assignment of containers, i.e. the referenced elements\nare\n> > copied but not the references itself.\n>\n> I'm not sure wether I understand this, shouldn't\n>\n> TpMatrixRange r1 = TpMatrixRange( U, numerics::range( 0,1),\n> numerics::range( 0,1) );\n>\n> TpMatrixRange r2 = TpMatrixRange( U, numerics::range( 0,1),\n> numerics::range( 0,2) );\n> r2 = TpMatrixRange( U, numerics::range( 0,1), numerics::range( 0,1) );\n>\n> or at least\n> r2 = r1;\n>\n> then work ? (At least it doesn't ).\n> What is the purpose of the assigment operator then ?\n\nLet me try to explain it another way: proxies like vector_range and\nmatrix_range implement operator=(), operator+=() and operator-=() with the\nsame semantics as containers like vectors and matrices. The operations\nchange instead of whole vectors and matrices the corresponding parts of the\nreferenced vectors or matrices.\n\nFor example:\n\nTpMatrixRange r1( U, numerics::range( 0,1), numerics::range( 0,1) );\nTpMatrixRange r2( V, numerics::range( 0,1), numerics::range( 0,1) );\nr2 = r1;\nr2 += r1;\nr2 -= r1;\n\nassigns U(0, 0) to V (0, 0), adds U(0, 0) to V (0, 0) and so on.\n\n> > BTW, the default constructor of matrix_range is currently useless for an\n> > application and is therefore not documented.\n> Shouldn't it be private/protected then ?\n\nYes, but we currently need it to be public for concepts.h ;-(\n\nBest regards\n\nJoerg" ]
[ null, "https://lists.boost.org/boost/images/boost.png", null ]
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https://www.colorhexa.com/b47338
[ "# #b47338 Color Information\n\nIn a RGB color space, hex #b47338 is composed of 70.6% red, 45.1% green and 22% blue. Whereas in a CMYK color space, it is composed of 0% cyan, 36.1% magenta, 68.9% yellow and 29.4% black. It has a hue angle of 28.5 degrees, a saturation of 52.5% and a lightness of 46.3%. #b47338 color hex could be obtained by blending #ffe670 with #690000. Closest websafe color is: #cc6633.\n\n• R 71\n• G 45\n• B 22\nRGB color chart\n• C 0\n• M 36\n• Y 69\n• K 29\nCMYK color chart\n\n#b47338 color description : Moderate orange.\n\n# #b47338 Color Conversion\n\nThe hexadecimal color #b47338 has RGB values of R:180, G:115, B:56 and CMYK values of C:0, M:0.36, Y:0.69, K:0.29. Its decimal value is 11825976.\n\nHex triplet RGB Decimal b47338 `#b47338` 180, 115, 56 `rgb(180,115,56)` 70.6, 45.1, 22 `rgb(70.6%,45.1%,22%)` 0, 36, 69, 29 28.5°, 52.5, 46.3 `hsl(28.5,52.5%,46.3%)` 28.5°, 68.9, 70.6 cc6633 `#cc6633`\nCIE-LAB 54.293, 20.197, 42.298 25.668, 22.252, 6.684 0.47, 0.408, 22.252 54.293, 46.872, 64.476 54.293, 51.312, 41.91 47.172, 14.575, 24.619 10110100, 01110011, 00111000\n\n# Color Schemes with #b47338\n\n• #b47338\n``#b47338` `rgb(180,115,56)``\n• #3879b4\n``#3879b4` `rgb(56,121,180)``\nComplementary Color\n• #b4383b\n``#b4383b` `rgb(180,56,59)``\n• #b47338\n``#b47338` `rgb(180,115,56)``\n• #b4b138\n``#b4b138` `rgb(180,177,56)``\nAnalogous Color\n• #383bb4\n``#383bb4` `rgb(56,59,180)``\n• #b47338\n``#b47338` `rgb(180,115,56)``\n• #38b4b1\n``#38b4b1` `rgb(56,180,177)``\nSplit Complementary Color\n• #7338b4\n``#7338b4` `rgb(115,56,180)``\n• #b47338\n``#b47338` `rgb(180,115,56)``\n• #38b473\n``#38b473` `rgb(56,180,115)``\n• #b43879\n``#b43879` `rgb(180,56,121)``\n• #b47338\n``#b47338` `rgb(180,115,56)``\n• #38b473\n``#38b473` `rgb(56,180,115)``\n• #3879b4\n``#3879b4` `rgb(56,121,180)``\n• #7a4e26\n``#7a4e26` `rgb(122,78,38)``\n• #8d5a2c\n``#8d5a2c` `rgb(141,90,44)``\n• #a16732\n``#a16732` `rgb(161,103,50)``\n• #b47338\n``#b47338` `rgb(180,115,56)``\n• #c48041\n``#c48041` `rgb(196,128,65)``\n• #ca8d55\n``#ca8d55` `rgb(202,141,85)``\n• #d09a68\n``#d09a68` `rgb(208,154,104)``\nMonochromatic Color\n\n# Alternatives to #b47338\n\nBelow, you can see some colors close to #b47338. Having a set of related colors can be useful if you need an inspirational alternative to your original color choice.\n\n• #b45438\n``#b45438` `rgb(180,84,56)``\n• #b45e38\n``#b45e38` `rgb(180,94,56)``\n• #b46938\n``#b46938` `rgb(180,105,56)``\n• #b47338\n``#b47338` `rgb(180,115,56)``\n• #b47d38\n``#b47d38` `rgb(180,125,56)``\n• #b48838\n``#b48838` `rgb(180,136,56)``\n• #b49238\n``#b49238` `rgb(180,146,56)``\nSimilar Colors\n\n# #b47338 Preview\n\nThis text has a font color of #b47338.\n\n``<span style=\"color:#b47338;\">Text here</span>``\n#b47338 background color\n\nThis paragraph has a background color of #b47338.\n\n``<p style=\"background-color:#b47338;\">Content here</p>``\n#b47338 border color\n\nThis element has a border color of #b47338.\n\n``<div style=\"border:1px solid #b47338;\">Content here</div>``\nCSS codes\n``.text {color:#b47338;}``\n``.background {background-color:#b47338;}``\n``.border {border:1px solid #b47338;}``\n\n# Shades and Tints of #b47338\n\nA shade is achieved by adding black to any pure hue, while a tint is created by mixing white to any pure color. In this example, #000000 is the darkest color, while #faf5f1 is the lightest one.\n\n• #000000\n``#000000` `rgb(0,0,0)``\n• #0f0a05\n``#0f0a05` `rgb(15,10,5)``\n• #1e1309\n``#1e1309` `rgb(30,19,9)``\n• #2d1d0e\n``#2d1d0e` `rgb(45,29,14)``\n• #3c2713\n``#3c2713` `rgb(60,39,19)``\n• #4b3017\n``#4b3017` `rgb(75,48,23)``\n• #5a3a1c\n``#5a3a1c` `rgb(90,58,28)``\n• #694321\n``#694321` `rgb(105,67,33)``\n• #784d25\n``#784d25` `rgb(120,77,37)``\n• #87562a\n``#87562a` `rgb(135,86,42)``\n• #96602f\n``#96602f` `rgb(150,96,47)``\n• #a56933\n``#a56933` `rgb(165,105,51)``\n• #b47338\n``#b47338` `rgb(180,115,56)``\n• #c37d3d\n``#c37d3d` `rgb(195,125,61)``\n• #c7874c\n``#c7874c` `rgb(199,135,76)``\n• #cc915b\n``#cc915b` `rgb(204,145,91)``\n• #d19b6a\n``#d19b6a` `rgb(209,155,106)``\n• #d5a579\n``#d5a579` `rgb(213,165,121)``\n• #daaf88\n``#daaf88` `rgb(218,175,136)``\n• #dfb997\n``#dfb997` `rgb(223,185,151)``\n• #e3c3a6\n``#e3c3a6` `rgb(227,195,166)``\n• #e8cdb5\n``#e8cdb5` `rgb(232,205,181)``\n• #edd7c4\n``#edd7c4` `rgb(237,215,196)``\n• #f1e1d3\n``#f1e1d3` `rgb(241,225,211)``\n• #f6ebe2\n``#f6ebe2` `rgb(246,235,226)``\n• #faf5f1\n``#faf5f1` `rgb(250,245,241)``\nTint Color Variation\n\n# Tones of #b47338\n\nA tone is produced by adding gray to any pure hue. In this case, #7e766e is the less saturated color, while #ea7002 is the most saturated one.\n\n• #7e766e\n``#7e766e` `rgb(126,118,110)``\n• #877565\n``#877565` `rgb(135,117,101)``\n• #90755c\n``#90755c` `rgb(144,117,92)``\n• #997453\n``#997453` `rgb(153,116,83)``\n• #a2744a\n``#a2744a` `rgb(162,116,74)``\n• #ab7341\n``#ab7341` `rgb(171,115,65)``\n• #b47338\n``#b47338` `rgb(180,115,56)``\n• #bd732f\n``#bd732f` `rgb(189,115,47)``\n• #c67226\n``#c67226` `rgb(198,114,38)``\n• #cf721d\n``#cf721d` `rgb(207,114,29)``\n• #d87114\n``#d87114` `rgb(216,113,20)``\n• #e1710b\n``#e1710b` `rgb(225,113,11)``\n• #ea7002\n``#ea7002` `rgb(234,112,2)``\nTone Color Variation\n\n# Color Blindness Simulator\n\nBelow, you can see how #b47338 is perceived by people affected by a color vision deficiency. This can be useful if you need to ensure your color combinations are accessible to color-blind users.\n\nMonochromacy\n• Achromatopsia 0.005% of the population\n• Atypical Achromatopsia 0.001% of the population\nDichromacy\n• Protanopia 1% of men\n• Deuteranopia 1% of men\n• Tritanopia 0.001% of the population\nTrichromacy\n• Protanomaly 1% of men, 0.01% of women\n• Deuteranomaly 6% of men, 0.4% of women\n• Tritanomaly 0.01% of the population" ]
[ null ]
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https://www.gradesaver.com/textbooks/math/algebra/algebra-1/chapter-8-polynomials-and-factoring-8-1-adding-and-subtracting-polynomials-practice-and-problem-solving-exercises-page-478/21
[ "## Algebra 1\n\n$18v^{4}w^{3}$\nIn order to add monomials, we combine like terms. Like terms are terms that have the same variable raised to the same power. Note, by this definition, $3xy^{2}$ and $9xy^{2}$ are like terms, for these two terms have the same two variables raised to the same powers. Additionally, when we combine like terms, we add and subtract them just like we add and subtract numbers.Thus, we combine like terms to obtain the answer: $18v^{4}w^{3}$" ]
[ null ]
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https://datascience.stackexchange.com/questions/73587/test-data-for-statistical-t-test-in-python
[ "# Test data for statistical t-test in Python\n\nfirst of all sorry if this is not the proper place to ask but i have been trying to create some dummy variables in order to run a students t-test as well as a welch t-test and then run a monte-carlo simulation.Problem is, I am only given the sample size and standard deviation of the 2 populations. How can I go about creating some sort of representation for this data in order for me to run these tests? I wish to run these tests in either python or R. Thanks in advance.\n\nEDIT : both populations come from a normal distribution\n\n• So is your question, how to generate n points generated from a normal distribution given a mean (mu) and standard deviation (sigma)? May 5, 2020 at 10:35\n• Yes, exactly, sorry for not being more precise May 5, 2020 at 11:01\n• Sure, no problem, I'll write up an answer now May 5, 2020 at 11:04\n\nIn Python, to generate random numbers from a certain distribution you would pick the corresponding distribution from np.random (documentation) and pass the corresponding parameters. Thus to draw from a normal distribution you would do\n\nimport numpy as np\n\n# for reproducible results, seed the number generator\nnp.random.seed(42)\n\nn = 100\nmu_1, std_1 = 0, 1\nmu_2, std_2 = 0.2, 1.5\n\ndataset1 = np.random.normal(loc=mu_1, scale=std_1, size=n)\ndataset2 = np.random.normal(loc=mu_2, scale=std_2, size=n)\n\n\nAnd the output\n\nprint('dataset 1:')\nprint(f'mean: {dataset1.mean():.2f}')\nprint(f'std: {dataset1.std():.2f}')\nprint(f'shape: {dataset1.shape}')\nprint('--------------')\nprint('dataset 2:')\nprint(f'mean: {dataset2.mean():.2f}')\nprint(f'std: {dataset2.std():.2f}')\nprint(f'shape: {dataset2.shape}')\n\n--------------\ndataset 1:\nmean: -0.10\nstd: 0.90\nshape: (100,)\n--------------\ndataset 2:\nmean: 0.23\nstd: 1.42\nshape: (100,)\n\n\nPS: You don't have to use np.random.seed that's just to make the random generator consistent with the output every time the code is run.\n\nEDIT: Also, if you want to use a t-test on python you can use scipy.stats, thus if you want to calculate the T-test for the means of two independent samples use scipy.stats.ttest_ind, or if you want to calculate the t-test on two related samples use scipy.stats.ttest_rel\n\n• thank you, aso, how would one go about using the code above when the std_2 and n1 vary? just run independent ttests ? May 5, 2020 at 14:01\n• You can simply create n1 and n2 and pass each n. Also, std_2 already is different in this piece of code. May 5, 2020 at 14:26\n• Hi @LucaMarinescu if this or any answer has solved your question please consider accepting it by clicking the check-mark. This indicates to the wider community that you've found a solution and gives some reputation to both the answerer and yourself. There is no obligation to do this. May 10, 2020 at 13:26" ]
[ null ]
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https://ralenenelson.com/how-is-interest-calculated-for-a-mortgage/
[ "# How Is Interest Calculated for a Mortgage?\n\nPosted on: March 14, 2019 Posted by: rnelson Comments: 0", null, "Each month you make payments on your new mortgage, a portion of the payment goes to paying down your balance, or principal, while the other portion pays your interest charge. The proportion of your payment that pays interest versus principal changes every month. Even though you can find a wide variety of different online mortgage calculators that will perform the calculation for you, it’s smart to learn exactly how the interest is calculated.\n\n## Mortgage Amortization\n\nWhen you establish a mortgage account, the lender determines your interest costs based on an amortization schedule. Amortization is simply a method of reducing an installment loan debt until it reaches zero. It takes into account both payments toward the loan balance and payments of interest. An amortization table lists the amount of interest and principal paid every month over the life of the loan, as well as the principal and interest totals paid to date, in a convenient and simple-to-follow format.\n\n## Information Needed\n\nIn order to calculate the interest expense for a mortgage, you need to know several key details. First, you need to know the term of the mortgage; most are for 30 years, but other terms are available. Then you need the mortgage principal, which is the amount you financed. Next, you need to know the interest rate on the loan, which will remain the same throughout the term if you have a fixed-rate mortgage. Finally, you must know your monthly payment on the mortgage so that you can determine what portion of each payment is going to pay principal versus interest for each month of the loan.\n\n## Calculation\n\nThe way the mortgage company calculates your interest is pretty straightforward. You can do this by multiplying the balance by the monthly interest rate. So, for instance, if your interest rate on a \\$100,000 30-year loan is 7 percent, the monthly interest rate is 0.58333 percent, which you get by dividing the yearly interest rate by 12; 7 divided by 12 is .58333 percent or .0058333. When you multiply that monthly rate by the initial balance of \\$100,000, it results in the first month’s interest cost of \\$583.33. Your monthly payment on this hypothetical loan is \\$665.30, so this means that the principal paid down that month is \\$81.97: the payment of \\$665.30 minus the interest payment of \\$583.33. Deduct the principal from the previous balance — \\$100,000 minus \\$81.97 — to get the loan’s new balance of \\$99,918.03 for the next month. Then repeat this process to determine the interest cost for the next month and each subsequent month thereafter.\n\n## Less Interest with Time\n\nAs you continue to calculate interest for the mortgage in this way, you’ll notice that the amount of interest you pay each month goes down as the amount of the loan balance you pay each month goes up. Eventually, the portion of your monthly mortgage payment that goes toward principal will exceed the amount going to interest until the balance of your loan is paid off.\n\nSource: budgeting.thenest.com ~ By: By Louise Balle ~ Image: pixabay.com\n\nThis site uses Akismet to reduce spam. Learn how your comment data is processed." ]
[ null, "https://i1.wp.com/ralenenelson.com/wp-content/uploads/2019/03/calculator-428294_960_720.jpg", null ]
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https://tex.stackexchange.com/tags/symbols/new
[ "# Tag Info\n\n1\n\nI add some proposals.... \\documentclass[11pt]{article} \\usepackage{newtxtext} \\usepackage{newtxmath} \\usepackage{MnSymbol} \\usepackage{wasysym} \\begin{document} $$f \\star g$$, \\verb|classic star| $$f \\mathbin{\\filledstar} g$$, \\verb|MnSymbol package| $f \\mathrel{\\thinstar} g$, \\verb|MnSymbol package| $f \\mathbin{\\APLstar} g$, \\verb|Table 330: ...\n\n1\n\nYou could borrow the \\star from Latin Modern. \\documentclass[11pt]{article} \\usepackage{newtxtext} \\usepackage{newtxmath} \\DeclareSymbolFont{LMletters}{OML}{lmm}{m}{it} \\DeclareMathSymbol{\\lmstar}{\\mathbin}{LMletters}{63} \\begin{document} $$f \\star g$$ $$f \\lmstar g$$ \\end{document}\n\n2\n\nFor example using mathrsfs package give to you the symbol O: \\documentclass[12pt]{article} \\usepackage{mathrsfs} \\begin{document} $\\mathscr{O}$ \\end{document}\n\n1\n\nI confronted a similar problem with a need for a pretty bar over various characters with \\mathbf, \\mathcal, \\mathfrak, etc. By \"pretty,\" I mean that the bar seems very appropriate to the character shape and size, and this means adjusting the length and placement (left and right offsets) until it looks right. Further, the commands used must be ...\n\n3\n\nThis is more of a comment, but requires an example. The problem described does not occur with Computer Modern, and the reason is the difference in the metrics in the .tfm file: the \"d\" in the alphabet used for math does not have an italic correction. This is by design, since \"d\" is most often used by Knuth for the differential operator; ...\n\n0\n\nI tried several of those options all leading to a small square instead of «». This did the trick for me. \\documentclass{article} \\usepackage[francais]{babel} % guillemets \\og text \\fg{} \\usepackage{aeguill} % guillemets \\begin{document} \\og text \\fg{} \\end{document}\n\n0\n\nThe above link to the «Short Math Guide for LaTeX» by the AMS seems to be broken. Correct link is: http://tug.ctan.org/info/short-math-guide/short-math-guide.pdf (As answer as I cannot comment)\n\n2\n\n\\XeTeXglyphindex \"ass_completa_CONT\" \\relax should expand to the integer glyphid then \\XeTeXglyph ⟨glyph slot⟩ should typeset it, so \\XeTeXglyph \\XeTeXglyphindex \"ass_completa_CONT\" \\relax Probably works...\n\n7\n\nThe beamer class loads, by default, both amsmath and amssymb (unless these are explicitly disabled with the relevant class options). The \\square and \\Box command are indeed provided by amssymb and loading this package would suffice for using them; however, if a document uses those symbols it is likely about mathematics and so amsmath is recommended as well. ...\n\n2\n\nTo add to @domperor's answer, for symbols in text mode, the \\usefont command can be used. MWE \\documentclass{article} \\DeclareFontFamily{U}{FdSymbolA}{} \\DeclareFontShape{U}{FdSymbolA}{m}{n}{<->FdSymbolA-Book}{} \\newcommand\\vardiamondsuit{{\\usefont{U}{FdSymbolA}{m}{n}\\char182}} \\newcommand\\varheartsuit{{\\usefont{U}{FdSymbolA}{m}{n}\\char184}} \\begin{...\n\n0\n\nIn the recent version 1.18 of newtxmath there are new math accents and macros. The macro \\widering, as written into the guide, places a ring centered over an \\overgroup, not dissimilar from its use in yhmath. But for my tastes the command \\widering given by newtxmath have a better arc: \\documentclass[a4paper,12pt]{article} \\usepackage{newtxmath,newtxtext} \\...\n\n6\n\nThis is a short working example: \\documentclass{article} \\DeclareFontFamily{U}{FdSymbolA}{} \\DeclareFontShape{U}{FdSymbolA}{m}{n}{<->FdSymbolA-Book}{} \\DeclareSymbolFont{extrasymbols}{U}{FdSymbolA}{m}{n} \\DeclareMathSymbol{\\vardiamondsuit}{\\mathord}{extrasymbols}{182} \\DeclareMathSymbol{\\varheartsuit}{\\mathord}{extrasymbols}{184} \\begin{document} $\\... 12 This happens when you use the T1 encoding. You can disable the ligature that maps >> to » with microtype. I also removed the ligature from << to « for symmetry. The first line shows that the ligatures are not suppressed altogether, but only when using the monospaced font. \\documentclass{article} \\usepackage[T1]{fontenc} \\usepackage{courier} \\... 14 The addition of a group around the central > will prevent each from seeing the others, and therefore should prevent (for lack of a better word) the ligature from forming. Note: See comments to this answer, which are very illuminating, which explains why this technique will work in pdflatex but not lualatex! \\documentclass{article} \\usepackage[T1]{fontenc} ... 1 From the log sniplet you posted we can see that you're using MikTeX. To keep sizes down, sadly, MikTeX use a metafont font as the default font. This font is not scalable, and thus at high resolution you see pixelations like you show here You have two choices install the cm-super package, this installs a vector version of the default font. It is also the ... 5 I have changed the initial code completely: there are the combination of two particular packages: accents and scalerel. With these packages I have created a macro called \\arcsup with the arc only above the character . If you want to have a large horizontal arc you can increase the value of \\hstretch{1.8} to stretch horizzontally the arc. \\documentclass[... 2 Not exactly the answer to your question, but the package yhmath have the \\widering command which can be useful to you: \\documentclass[twoside]{article} \\usepackage{fancyhdr} \\usepackage{nameref} \\usepackage{abraces} \\usepackage{amsfonts,amsmath, amssymb, mathtools} \\usepackage{yhmath} \\makeatletter \\newcommand*{\\currentname}{\\@currentlabelname} \\makeatother ... 5 Perhaps with the use of stacks. The current \\circ elevation is controlled by the -2pt optional argument to \\stackon. \\documentclass{article} \\usepackage{abraces} \\usepackage{amsfonts,amsmath, amssymb, mathtools} \\usepackage{stackengine} \\stackMath \\begin{document} $\\left((\\overline{M})_{\\tau_1}\\right)^\\mathsf{c} = (\\stackon[-2pt]{\\aoverbrace[L1R] {M^\\... 1 The comments are perfect! But if a day you would to use two accents my suggestion is to adopt accents package. Here a MWE with a screenshot. \\documentclass[12pt]{article} \\usepackage{accents} \\begin{document} \\hat{A}_{12}, \\hat{\\accentset{\\circ}{A}}_{12}, \\hat{\\accentset{\\diamond}{A}}_{12} \\end{document} 12 Using the \\multimap symbol...rotated using also scalerel package. \\documentclass[12pt]{article} \\usepackage{amsmath,amssymb} \\usepackage{graphicx} \\newcommand{\\circmap}{\\raisebox{.7\\depth}{\\rotmap}} \\newcommand{\\rotmap}{\\rotatebox[origin=c]{-90}{\\multimap}} \\usepackage{scalerel} \\usepackage{parskip} \\begin{document} Euler's formula is remarkable: e^{i\\... 13 As @Noone pointed out, there is a similar unicode character (U+2AF0). As for most unicode characters, it is included in the STIX font. It can be accessed without loading the whole font as in the following example. \\documentclass{article} \\DeclareFontEncoding{LS1}{}{} \\DeclareFontSubstitution{LS1}{stix}{m}{n} \\DeclareSymbolFont{symbols4}{LS1}{stixbb}{m}{it} \\... 1 Had the same issue, but wanted the uncertainties to not extend outside the original text height too much. \\documentclass{article} \\usepackage{amsmath} \\begin{document} 1.06{\\raisebox{0.5ex}{\\tiny\\substack{+0.04 \\\\ -0.05}}} or 1.06{\\raisebox{0.5ex}{\\tiny^{+0.04}_{-0.05}} as opposed to 1.06^{+0.04}_{-0.05} \\end{document} Turned out to ... 15 Is this what you want? \\documentclass{article} \\usepackage{amsmath,pict2e} \\makeatletter \\newcommand{\\disjoint}{}% for safety \\DeclareRobustCommand{\\disjoint}{% \\mathrel{% \\mathpalette\\disjoint@\\relax }% } \\newcommand{\\disjoint@}{% \\begingroup \\setlength{\\unitlength}{\\disjoint@height{#1}}% \\begin{picture}(1.4,2) \\roundcap \\... 5 I sometimes use Euler or Computer Modern Upright Italic for upright math symbols distinct from operators. Usually, though, that’s been constants in ISO style. Other available math alphabets include \\mathsf, \\mathtt, \\mathcal and \\mathfrak. Examples Here is a sample that defines a new symbol \\dimension, as the letter d in Computer Modern Upright Italic: \\... 2 The features of scalerel can accomplish this. \\documentclass[12pt]{article}%, border=2pt]{standalone} \\usepackage{MnSymbol} \\usepackage{sansmath} \\usepackage{stackengine, amsfonts,scalerel} % \\newcommand{\\leftharpoontriangleX}{\\mathord{\\ensurestackMath{% \\stackinset{c}{0pt}{c}{-0.3ex}{\\scriptstyle\\leftharpoonup}% {\\largetriangleup}}}} \\newcommand{\\... 3 A bit of a fusion of the previous two answers, which declares either Unicode characters for use with PDFLaTeX or tipa-compatible commands for use with LuaLaTeX or XeLaTeX: \\documentclass{article} \\tracinglostchars=2 \\usepackage{iftex} \\pagestyle{empty} % format this MWE for TeX.SX \\usepackage[paperwidth=10cm]{geometry} \\iftutex \\usepackage{fontspec} \\... 13 See Sergio's answer if you can use a modern Unicode engine like LuaLaTeX (or XeLaTeX). If you want to access the symbol in pdfLaTeX, it helps to know that this is an obsolete IPA symbol, so you can use the tipa package: It provides the symbol as \\textctt (standing for text curly tail t): \\documentclass{article} \\usepackage[safe]{tipa} \\begin{document} \\... 4 It is the Unicode Character 'LATIN SMALL LETTER T WITH CURL' (U+0236), see https://www.fileformat.info/info/unicode/char/0236/index.htm If you use XeLaTeX and STIX Two fonts (see https://ctan.mirror.garr.it/mirrors/CTAN/fonts/stix2-otf/StixTwoMath.pdf, page 8), you can get that character by inserting the unicode code/name in the way your editor accepts it. ... 1 Use mathematical kerns, that automatically adapt to the style. \\documentclass{article} \\DeclareRobustCommand{\\AAA}{A\\mkern-5mu A} \\begin{document} \\[ \\AAA\\frac{\\AAA}{AA}\\textstyle\\frac{\\AAA}{AA}\\scriptstyle\\frac{\\AAA}{AA}$ \\end{document} 3 Set it up to account for the math style. \\documentclass{article} \\newcommand\\dblA{\\mathchoice {A\\hspace{-.7ex}A} {A\\hspace{-.7ex}A} {A\\hspace{-.58ex}A} {A\\hspace{-.55ex}A}% } \\begin{document}$\\dblA AA\\scriptstyle\\dblA AA\\scriptscriptstyle\\dblA AA$\\end{document} 0 After some searching I found a suitable answer. It is not exactly what I was hoping for in terms of a master list but I am happy with the results I have for now, so I am posting this answer for anyone that has the same problems. I made use of the standalone package along with the nomenclpackage. I added the following to my preamble: \\usepackage{standalone} \\... 2 What I frequently do when I encounter pesky invisible characters in an equation is to (a) switch from pdfLaTeX to LuaLaTeX and (b) make sure to load the unicode-math package. That way, invisible characters such as U+2061 (FUNCTION APPLICATION) show up in the pdf file -- see the first line in the screenshot below. This makes it straightforward to locate and ... 6 It is included in the STIX font. It can be imported without importing the whole font as in the following example. \\documentclass{article} \\DeclareFontEncoding{LS1}{}{} \\DeclareFontSubstitution{LS1}{stix}{m}{n} \\DeclareSymbolFont{symbols}{LS1}{stixscr}{m}{n} \\DeclareMathSymbol{\\blackinwhitesquare}{\\mathord}{symbols}{\"BA} \\begin{document} $$\\... 7 This is ▣ (U+25A3} in Unicode, and you can use it in fontspec. Examples \\documentclass{article} \\usepackage{unicode-math} \\setmathfont{STIX Two Math} \\begin{document} \\( \\blackinwhitesquare$$ \\end{document} The XITS Math and STIX Two Math fonts have this symbol. You can import only this symbol while using another math font. \\setmathfont{Latin Modern Math}... 8 Same size as \\square. Works across math styles. The .5 scale of the inner box can be adjusted to suit. \\documentclass{article} \\usepackage{amssymb,stackengine,graphicx,scalerel} \\newcommand\\dsquare{\\ThisStyle{\\ensurestackMath{% \\stackinset{c}{}{c}{}{\\scalebox{.5}{$\\SavedStyle\\blacksquare$}} {\\SavedStyle\\square}}}} \\begin{document}$\\square\\blacksquare \\...\n\n2\n\nFits within the existing size of \\square. Let the bowling commence! \\documentclass{article} \\usepackage{scalerel,amssymb,stackengine} \\DeclareRobustCommand\\boxdiag{\\boxslsh{1}} \\DeclareRobustCommand\\boxbslash{\\boxslsh{-1}} \\newcommand\\boxslsh{ \\mathchoice{ \\ensurestackMath{\\stackengine{0pt}{\\square} {\\stretchrel*{\\hstretch{#1}{/}}{\\square}}{O}{c}{...\n\n2\n\nDefinitely not perfect, but it was fun to play with pict2e again. The scaling does not work well in all math styles because \\square sticks out of its box by the same amount in all math styles. \\documentclass{article} \\usepackage{amsmath,amssymb,pict2e} \\makeatletter \\DeclareRobustCommand{\\boxdiagup}{{\\m@th\\mathpalette\\@boxdiagup\\relax}} \\newcommand*{\\@...\n\n4\n\nJust I add only the symbol \\Game from the Table 204: 𝒜ℳ𝒮 Letter-like Symbols of the Comprensive list symbols: \\documentclass[12pt]{article} \\usepackage{amsmath,amssymb} \\begin{document} $\\Game^a_b$ \\end{document}\n\n0\n\nAnother idea is to use the fontsawesome5 package with \\faRProject.\n\n3\n\nBy chance, I noticed that I already have the package graphicx loaded (without clashes), which means I can rotate a symbol. Thus the gruesome \\rotatebox[origin=c]{90}{$\\mathrlap{\\smallsetminus}\\square$} (which of course I meanwhile macro-ed with \\newcommand) does the trick without any side effects, and looks nearly as perfect as the native box-with-diagonal ...\n\n3\n\nI would combine the \\substack{...} macro of the amsmath package and the \\smashoperator[r]{...} macro of the mathtools package. The \\substack macro permits introducing line breaks in the argument of \"large\" operators (such as \\bigcup). The \\smashoperator[r] macro permits joining up the operator to the material to its right. \\documentclass{article} \\...\n\n1\n\nIn the modern toolchain, with unicode-math, you can substitute this glyph from a different font. \\documentclass{article} \\usepackage{unicode-math} \\setmainfont{TeX Gyre Termes} \\setmathfont{TeX Gyre Termes Math} \\setmathfont{XITS Math}[range=\\mitlambda,Scale=MatchLowercase] \\pagestyle{empty} \\begin{document} $\\lambda$ \\end{document}\n\n0\n\nThis is the solution to insert musical rhythms in a text: \\documentclass{tufte-book} \\usepackage{musicography} \\begin{document} the package musicography allows the insertion of rhythms cells as the following example \\musSixteenth\\ \\musCorchea \\musCorchea\\ \\musQuarter\\ . \\end{document} The result is as follows:\n\n7\n\nThe unicode-math package includes all the math symbols in Unicode, under the same names as stix and stix2. You can import them with \\setmathfont[ range={\\hexagonblack,\\varhexagonblack}, Scale=MatchUppercase ]{STIX Two Math} XITS Math is a fork of the STIX 1 font, and other fonts might or might not have these symbols.\n\n13\n\nJust it is a bit complex but I had used thus how I have written in the image a combination between tikz and \\usetikzlibrary{shapes} that get the hexagon symbol: regular polygon sides=6. After I have used \\mathord like suggested by user @Thruston in the recent comment. \\documentclass[a4paper,12pt]{article} \\usepackage{amsmath} \\usepackage{amssymb} \\usepackage{...\n\n7\n\nThe symbols in marvosym are meant to be used in text. \\documentclass{article} \\usepackage{amsmath} \\usepackage{marvosym} \\begin{document} Wrong: \\verb|$a=\\HexaSteel$| $\\to$ $a=\\HexaSteel$ Right: \\verb|$a=\\text{\\HexaSteel}$| $\\to$ $a=\\text{\\HexaSteel}$ \\end{document} Of course, if you plan to use this as a math symbol, you can do \\newcommand{\\hexagon}{\\...\n\n15\n\nAs for most unicode symbols, there are filled hexagons in the STIX font. They can be imported without importing the whole font. \\documentclass{article} \\DeclareFontEncoding{LS1}{}{} \\DeclareFontSubstitution{LS1}{stix}{m}{n} \\DeclareSymbolFont{symbols4}{LS1}{stixbb}{m}{it} \\DeclareMathSymbol{\\varhexagonblack}{\\mathord}{symbols4}{\"DD} \\DeclareMathSymbol{\\...\n\n9\n\nThe STIX font also has two versions of the symbol (in different rotations). For pdfLaTeX you can use the stix2 package. Downside is that STIX becomes the font for your entire document. \\documentclass{article} \\usepackage{stix2} \\begin{document} $$a+b=\\varhexagonblack$$. $$b+a=\\hexagonblack$$. \\end{document}\n\n8\n\nYou can print this symbol without any package from the font MarVoSym.ttf: \\font\\marvosym=umvs {\\marvosym\\char146}\n\nTop 50 recent answers are included" ]
[ null ]
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https://ludwig.ai/0.5/developer_guide/add_a_loss_function/
[ "At a high level, a loss function evaluates how well a model predicts a dataset. Loss functions should always output a scalar. Lower loss corresponds to a better fit, thus the objective of training is to minimize the loss.\n\nLudwig losses conform to the `torch.nn.Module` interface, and are declared in `ludwig/modules/loss_modules.py`. Before implementing a new loss from scratch, check the documentation of torch.nn loss functions to see if the desired loss is available. Adding a torch loss to Ludwig is simpler than implementing a loss from scratch.\n\n## Add a torch loss to Ludwig¶\n\nTorch losses whose call signature takes model outputs and targets i.e. `loss(model(input), target)` can be added to Ludwig easily by declaring a trivial subclass in `ludwig/modules/loss_modules.py` and registering the loss for one or more output feature types. This example adds `MAELoss` (mean absolute error loss) to Ludwig:\n\n``````@register_loss(\"mean_absolute_error\", [NUMBER, TIMESERIES, VECTOR])\nclass MAELoss(torch.nn.L1Loss, LogitsInputsMixin):\ndef __init__(self, **kwargs):\nsuper().__init__()\n``````\n\nThe `@register_loss` decorator registers the loss under the name `mean_absolute_error`, and indicates it is supported for `NUMBER`, `TIMESERIES`, and `VECTOR` output features.\n\n## Implement a loss from scratch¶\n\n### Implement loss function¶\n\nTo implement a new loss function, we recommend first implementing it as a function of logits and labels, plus any other configuration parameters. For this example, lets suppose we have implemented the tempered softmax from \"Robust Bi-Tempered Logistic Loss Based on Bregman Divergences\". This loss function takes two constant parameters `t1` and `t2`, which we'd like to allow users to specify in the config.\n\nAssuming we have the following function:\n\n``````def tempered_softmax_cross_entropy_loss(\nlogits: torch.Tensor,\nlabels: torch.Tensor,\nt1: float, t2: float) -> torch.Tensor:\n# Computes the loss, returns the result as a torch.Tensor.\n``````\n\n### Define and register module¶\n\nNext, we'll define a module class which computes our loss function, and add it to the loss registry for `CATEGORY` output features with `@register_loss`. `LogitsInputsMixin` tells Ludwig that this loss should be called with the output feature `logits`, which are the feature decoder outputs before normalization to a probability distribution.\n\n``````@register_loss(\"tempered_softmax_cross_entropy\", [CATEGORY])\nclass TemperedSoftmaxCrossEntropy(torch.nn.Module, LogitsInputsMixin):\n``````\n\nNote\n\nIt is possible to define losses on other outputs besides `logits` but this is not used in Ludwig today. For example, loss could be computed over `probabilities`, but it is usually more numerically stable to compute from `logits` (rather than backpropagating loss through a softmax function).\n\n### constructor¶\n\nThe loss constructor will receive any parameters specified in the config as kwargs. It must provide reasonable defaults for all arguments.\n\n``````def __init__(self, t1: float = 1.0, t2: float = 1.0, **kwargs):\nsuper().__init__()\nself.t1 = t1\nself.t2 = t2\n``````\n\n### forward¶\n\nThe forward method is responsible for computing the loss. Here we'll call the `tempered_softmax_cross_entropy_loss` after ensuring its inputs are the correct type, and return its output averaged over the batch.\n\n``````def forward(self, logits: torch.Tensor, target: torch.Tensor) -> torch.Tensor:\nlabels = target.long()\nloss = tempered_softmax_cross_entropy_loss(logits, labels, self.t1, self.t2)" ]
[ null ]
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https://stuvel.eu/post/2014-02-28-counting-pixels-in-blender/
[ "# Counting pixels in Blender\n\nUPDATE 2019: the image of the node setup has been lost.\n\nFor my research, I’m using Blender to generate images. I wanted to know how visible a certain object is in the final render (i.e. how many pixels it occupies). For this there is the “object index” render pass (aka “IndexOB” in the compositor). I’ve been struggling with it, since it always outputs that the index is 0, even though there are multiple objects in the scene.\n\nWell, with the help of mfoxdogg on the #blender IRC channel, we found a solution: You need to set the index by hand, for every object you’re interested in. If you go to the object properties (in the properties explorer), in the section “Relations” there is a slider “Pass Index”. This is set to 0 by default, and you can set it to any positive number you want. This is then reflected in the output of the “IndexOB” render pass.\n\nSo to solve my problem, I needed to count the pixels that a certain object occupies in the image. For this I connected a viewer node to the “IndexOB” pass. Once you’ve rendered, you can then access the pixel data using `bpy.data.images['Viewer Node'].pixels`. It’s a one-dimensional array of floats, in the RGBA format. This means that every pixel is represented as four consecutive floats.\n\nThe IndexOB data is stored in the RGB channels, and the alpha channel is set to 1.0. You could write some code to only inspect the R channel for its value and count the ones that are equal to the object index you’re interested in. I chose a more lazy approach of counting all RGBA values that are equal to the index, then dividing by 3. For this you do need an object index larger than 1, as the alpha channel is always set to 1 too. So here is the code:\n\n``````import bpy\n\n# I'm interested in the object named \"L\"\nob_name = 'L'\n\n# Set the \"pass index\"\nbpy.data.objects[ob_name].pass_index = 42\n\n# Render the image\nbpy.ops.render.render()\n\n# Count all pixels that have value = 42. We count all R, G and B components\n# separately, so divide by 3 to get the actual number of pixels\npixel_count = sum(1 for p in bpy.data.images['Viewer Node'].pixels if p == 42) / 3\nprint('Pixel count for object %r : %i' % (ob_name, pixel_count))\n``````", null, "" ]
[ null, "https://stuvel.eu/author/dr.-sybren-a.-stuvel/avatar_hue2f8e1e58ca785cadc9404f0d240e59b_517464_270x270_fill_q90_lanczos_center.jpg", null ]
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https://www.astronomyclub.xyz/spherical-aberration-2/l.html
[ "# L\n\nwhere L = M2I2 in Figs. 2.11 and 2.12. In terms of ray trace parameters L = s2. Note that Eq. (2.57) is only valid if |L| > |d1|, i.e. if b > 0, since otherwise the true length of the system is given by |d1|, not |L|.\n\nAnother fundamental parameter of these compound telescope forms is the axial obstruction ratio Ra. This is given by\n\nyi / f from the geometry of Figs. 2.11 and 2.12. Eqs. (2.57) and (2.58) give the simple relationship\n\nThis result essentially explains why the compound (2-mirror) telescope has triumphed over the single mirror form and is the standard solution for modern astronomy. Historically it was desirable to have a large scale (see § 2.2.6 below) and therefore a long focal length f . A solution with a large T giving reduced length is exactly what is needed. The fact that a large value of T gives a small axial obstruction from (2.59) is a marvellous added attraction. Of course, we have said nothing about the difficulties of manufacture and test which, as we shall see in Chap. 5 and in RTO II, Chap. 1 and 3, have been formidable.\n\nFormally, from (2.57) and (2.59), there is no difference between the Gregory and Cassegrain solutions. However, there is a further parameter to be introduced which makes the Cassegrain solution much superior for normal purposes, i.e. where a real primary image is of no consequence. The notable exception is the Gregory form for solar telescopes, in which the intense heat of the bulk of the solar image can be absorbed at the real prime focus. The parameter favouring the Cassegrain form is the position of the final image I2. For a fixed, convenient position behind the primary and a given value of\n\nRa, the Cassegrain allows a larger relative aperture u2 or a shorter value of / because L is shorter. This is evident from Figs. 2.11 and 2.12 but will be proven by the formulae below.\n\nApplying (2.34) and (2.35) to the secondary, we have\n\ngiving with L = s2", null, "" ]
[ null, "https://www.astronomyclub.xyz/images/downloads/eJw9yksKgCAQANDbuFTLfgTSUcLPkEPpiBleP9q0easXas2rEA1PbGClnHkkIu4oCk8tXWT8Hk0yBxRxQ_I8h7wZV5GSzujqU4D9Eb0eJ2UXBdPgQHUs6H6UrH2-8wMkXQ.jpg", null ]
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https://homework.cpm.org/category/CCI_CT/textbook/apcalc/chapter/4/lesson/4.1.3/problem/4-31
[ "", null, "", null, "### Home > APCALC > Chapter 4 > Lesson 4.1.3 > Problem4-31\n\n4-31.\n\nDifferentiate the following equations with respect to $x$. That is, what is $\\frac { d y } { d x }$?\n\n1. $y = \\frac { x + 1 } { x }$\n\nSimplify the fraction:\n\n$y=1+\\frac{1}{x}$\n\n$= 1 + x ^{−1}$\n\nDifferentiate:\n\n$\\frac{dy}{dx}=-x^{-2}$\n\n$=-\\frac{1}{x^{2}}$\n\n2. $y=\\cos\\left(x\\right)+\\sin\\left(x\\right)$\n\nBe careful about $+$ and $−$ signs.\n\n3. $y = x \\cdot \\sqrt [ 3 ] { x ^ { 2 } }$\n\nBefore you differentiate, rewrite with exponents.\n\n4. $y = \\left(6 – 5x\\right)\\left(1 – 2x\\right)$\n\nBefore you differentiate, expand." ]
[ null, "https://homework.cpm.org/dist/7d633b3a30200de4995665c02bdda1b8.png", null, 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", null ]
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https://studytipslab.com/study/make-math-short-notes/
[ "# How to make math short notes | Quick 4 step process", null, "Short notes are essential as you learn mathematics. This is because our class notes or reference books are too large. If you do not have short notes, doing a final math revision before the exam is very complicated.\n\nBut the problem is that most students do not know how to make math short notes. So, let’s understand my four-step process to do it correctly.\n\n1. Find the reference book or class notebook.\n2. Take all the materials you need.\n3. Make a mind map\n4. Making math short notes\n\n## 1) Find the reference book and class notebook.\n\nFirst of all, you have to find your reference book and the class notebook from your math subject. If you haven’t a class notebook making a short note is useless. Which means you haven’t enough knowledge to make a short note.\n\nBecause we can say that a student is well versed in making math short note if he has learned the lecture at least. So you need to have a well-organized notebook, or even you have a plain notebook, it also beautiful.\n\nThe requirement is you should have knowledge about the subject.\n\nWhat if I haven’t a notebook?\n\nSo if you don’t have a math notebook, you can learn your own and make your own notebook.\n\nWhat if I don’t have enough time to make a note?\n\nNow is the time to use the reference book. First of all, you have to find your academic curriculum. Then find out your math subject. Then note down it with its subtopics.\n\nLet’s assume your subject as a probability. So now note down all the topics with their subtopics. This is enough for step one. Now step forward.\n\n## 2) Take all the materials you need.", null, "Here are all the materials you need,\n\n• A new exercise book.\n• Pens with multiple colors\n• Highlighters\n• Pencil\n• Eraser\n• A couple of A3 papers\n• Files\n• A4 papers\n\n## 3) Make a mind map to make math short notes\n\nSo now you have all the stuff that you need. Now takeout your topics and subtopics list. Use this list to make a mind map.\n\nI have covered this same part in “How to learn math on your own? | 7 step process “article. For your easiness, I will put it here also.\n\n#### Why do we need to make a mind map in order to make math short notes?\n\nBy creating a mind map, you will see an accessible overview of your subject. So every time you learn and move forward, you can see the mind map and identify what you can and cannot do.\n\nNow take an A3 paper and start making your mindmap.\n\nOkay, let’s assume the subject that you are learning is Probability. You can make a mind map below.\n\nSo be sure to stick this in a place you can quickly see.\n\n## 4) Makingmath short notes", null, "Now is the time to start making the short note. Then get your class notebook. Now you have written theories and solved examples. So now get your new notebook.\n\n• Write titles and subtitles in perfect order.\n• Then write the exact theory part for a particular topic.\n• Don’t forget to writedown equations and special things.\n•  Now write down one or two solved examples to understand the theory.\n\nSo this way, repeat this until every subtopic is over. You will receive an excellent short note at the end.\n\n#### But what if I don’t have a class notebook, can’t I make math short notes?\n\nIf you do not have a class notebook, it means that you have not studied the subject in the lecture hall. I think you haven’t enough time to make a notebook.\n\nDon’t worry, I will help you. If you do this correctly, you probably can get high marks for the math exam.\n\n• When you complete step1, now you have all the topics and subtopics. And also, after the finish step3, you have a mind map.\n• You should now get your reference book.\n• Now choose your first topic and read that section in the reference book.\n• If you can understand that topic, now write the theory on your short notebook by using your own words. And don’t forget to write the equations and other special stuff.\n• Now you must understand an example given in the reference book. Then write it on the book after the theory. One or two examples are enough.\n• But understanding only two problems is not enough. Now get your file and write the subject name.\n• Now get some A4 sheets and solve about 5 or 6 problems. Be sure to put up numbers for all the problems you solve.\n• Now repeat the same process for all the topics and subtopics.\n\n#### IMPORTANT:\n\nIf you can’t understand some theories, try to understand them by,\n\n• Still unable to ask from a friend who is good at math\n\nI think now you have a pleasant and helpful short note. You can use it when the exam time comes.\n\nTip\n\nWhen you have free time, just look at the mind map and pick a topic randomly. Then try to remember that theory part or solve one of the questions from that section.\n\nWork hard and win the world.\n\nCONCLUSION\n\nIf you want to do your math exam correctly, you should definitely make a short note. But how to make math short notes? Well, In this article, I have discussed a successful 4 step process to make your math short note.\n\nSo how many maks you can score for maths? Comment below and let us know.\n\nYou will also like\n\nHow to understand lectures?| BTPT method" ]
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https://willhoffer.com/2021-12-02/convergence-of-Dirichlet-series-2/
[ "02 Dec 2021\n\n$\\newcommand{\\HH}{\\mathbb{H}} \\newcommand{\\CC}{\\mathbb{C}} \\newcommand{\\sc}{\\sigma_c} \\newcommand{\\sac}{\\sigma_{\\text{a.c.}}}$\n\n## Introduction\n\nThis post is a follow up to this previous post wherein we established that Laplace transforms of complex measures converge absolutely in half-planes. More generally, in fact, this result holds for local complex measures $\\mu$ whose magnitude grows at most exponentially— that is to say, the measure $\\vert\\mu\\vert$ has a cumulative distribution function $F(t)=\\vert\\mu\\vert([0,t])$ which is of exponential order, viz. $F(t)=O(\\exp(At))$ for some $A>0$ as $t\\to\\infty$.\n\nAs a corollary, we obtained that a generalized Dirichlet series (realized as a Laplace transform of a discrete measure) converges absolutely in regions shaped like half-planes.\n\nHere, we shall show that a generalized Dirichlet series can converge absolutely in any half-plane $$\\HH_x=\\{ s\\in\\CC : \\Re(s) > x\\}$$, $x\\in\\mathbb{R}$. We will prove more in fact: we shall demonstrate a examples of a generalized Dirichlet series whose abscissa of convergence $\\sc$ and whose abscissa of absolute convergence $\\sac$ can be any two real numbers, provided that $\\sc\\leq \\sac$.\n\nWe will not make comment about the convergence behavior at points in the boundaries of such half-planes, only on the open interior of such half-planes.\n\n## Dirichlet Series with Prescribed Half-Planes of Convergence\n\n#### The Starting Example\n\nWe shall start by considering the following (classical) Dirichlet series:\n\n$f(s)= \\sum_{n=1}^\\infty \\frac{(-1)^{n+1}}{n^s}$\n\nThis is sometimes known as the alternating zeta function, or the Dirichlet eta function.\n\nBy elementary techniques, we are able to deduce the following:\n\n#### Theorem\n\nThe Dirichlet series $f$ converges in the half plane $\\HH_0$ and converges absolutely in the half-plane $\\HH_1$. In other words, $\\sc=0$ and $\\sac=1$.\n\n#### Proof\n\nWe have that the absolute version of the series takes the form:\n\n$\\sum_{n=1}^\\infty \\left\\vert\\frac{(-1)^{n+1}}{n^s}\\right\\vert = \\sum_{n=1}^\\infty \\frac{1}{n^\\sigma}$\n\nThe left hand side is a $p$-series with parameter $p=\\sigma$, so the series $f$ converges absolutely when $\\sigma>1$.\n\nMeanwhile, when $\\sigma>0$ we have that the sequence $a_n=n^{-\\sigma}=\\vert n^{-s}\\vert$ is monotonically decreasing to zero as $n\\to\\infty$. Since the terms are alternating in sign, Leibniz’s alternating series test ensures the the series converges.\n\n$\\blacksquare$\n\n#### Modification of the Example\n\nWe now write the series above as a generalized Dirichlet series:\n\n$f(s) = \\sum_{n=1}^\\infty (-1)^{n+1}e^{-s\\log n}$\n\nApply the transformation linear transformation:\n\n$s\\mapsto \\frac{s-x_0}{x_1-x_0}$\n\nto obtain the new series, $g(s) := f\\left(\\frac{s-x_0}{x_1-x_0}\\right)$.\n\n#### Theorem (Arbitrary Abscissa of Convergence, $\\sac>\\sc$)\n\nLet $x_1,x_0$ be any two real numbers with $x_1>x_0$. The series $g$ as defined is a generalized Dirichlet series of the form:\n\n$g(s) = \\sum_{n=1}^\\infty b_n e^{-\\lambda_n s}$\n\nFurther, we have that abscissa of convergence $\\sc=x_0$ and abscissa of absolute convergence $\\sc=x_1$.\n\n#### Proof\n\nWe first compute that $g$ remains a generalized Dirichlet series:\n\n\\begin{align*} g(s) &= \\sum_{n=1}^\\infty (-1)^{n+1}e^{-\\left(\\frac{s-x_0}{x_1-x_0}\\right)\\log n} \\\\ &= \\sum_{n=1}^\\infty (-1)^{n+1}n^{\\frac{x_0}{x_1-x_0}}e^{-s\\frac{\\log n}{x_1-x_0}} \\\\ &= \\sum_{n=1}^\\infty b_n e^{-\\lambda_n s} \\end{align*}\n\nwhere we make the assignments $b_n=(-1)^{n+1}n^{\\frac{x_0}{x_1-x_0}}$ and $\\lambda_n=\\frac{\\log n}{x_1-x_0}$.\n\nWe remark that the condition $x_1> x_0$ ensures that each $\\lambda_n>0$ (so that they forms an increasing sequence). When $x_1-x_0=1$, the series above reduces to a classical Dirichlet series with coefficients $a_n=(-1)^{n+1} n^{x_0}$.\n\nSince $f(t) = g((x_1-x_0)t+x_0))$ absolutely converges when $\\Re(t)>1$ and converges when $\\Re(t)>0$, $g$ converges under these same conditions. In the variable $s=(x_1-x_0)t+x_0$, it follows that $g(s)$ converges absolutely when $\\Re(s)>x_1$ and converges when $\\Re(s)>x_0$.\n\n$\\blacksquare$\n\nThus, we have shown that the convergence of a generalized Dirichlet series may have arbitrary abscissa of convergence $\\sc=x_0$ and abscissa of absolute convergence $\\sac=x_1> x_0$. Note that this construction involves dividing by $x_1-x_0$, which fails when they are equal.\n\n#### Equal Abscissae Case\n\nWe next proceed similarly but with a different example to prove the theorem when the abscissa of convergence coincide.\n\nIn the spirit of the previous proof, we shall also take a known example and modify it with a linear transformation. In this case, the ordinary Riemann zeta function will do:\n\n$\\zeta(s) = \\sum_{n=1}^\\infty \\frac{1}{n^s}$\n\nThis series is absolutely convergent when $\\Re(s)>1$, and it diverges when $\\Re(s)<1$. These can be seen, for instance, by using the integral test and comparison with the harmonic series, respectively. (Any other technique to prove this result for such a $p$-series would do.) Thus, the abscissae of convergence coincide and equal to one.\n\nNote that the absolute convergence for real valued $s$ is automatic from convergence since the coefficients are positive, and absolute convergence of the series with complex $s=\\sigma+i\\tau$ follows from comparison to the series with real parameter $\\sigma$.\n\n#### Theorem (Arbitrary Abscissa of Convergence, $\\sac=\\sc$)\n\nFor any real number $x_0$, there is a classical Dirichlet series $g$ whose abscissa of convergence and of absolute convergence coincide and equal this number: $\\sac=\\sc=x_0$.\n\n#### Proof\n\nDefine the new Dirichlet series $g(s) = \\zeta(s-(x_0-1))$ for $x_0\\in\\mathbb{R}$, which converges when $\\Re(s)-x_0+1>1$, or $\\Re(s)>x_0$. Thus $\\sc=x_0$ for $g$. The abcissa of absolute convergence is the same for the $\\zeta$ function, and hence for $g$ as well.\n\nSince this transformation is only a shift by $x_0-1$, the series $g$ remains a classical Dirichlet series:\n\n\\begin{align*} g(s) &= \\sum_{n=1}^\\infty \\frac{1}{n^{s-x_0+1}} = \\sum_{n=1}^\\infty \\frac{n^{x_0-1}}{n^{s}} \\end{align*}\n\nSince $x_0$ is a arbitrary real number, we are done.\n\n$\\blacksquare$\n\nIn summary, we have shown that for any two real numbers $x_1,x_0\\in\\mathbb{R}$ with $x_1\\geq x_0$, there is a generalized Dirichlet series $g$ whose abcissae satisfy $\\sc=x_0$ and $\\sac=x_1$." ]
[ null ]
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