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https://apps.dtic.mil/sti/citations/ADA158555
[ "# Abstract:\n\nThis document shows that a sum of dependent random variables is approximately compound Poisson when the variables are rarely nonzero and, given they are nonzero, their conditional distributions are nearly identical. It give several upper bounds on the total-variation distance between the distribution of such a sum and a compund Poisson distribution. Included is an example for Markovian occurrences of a rare event. The bounds are consistent with those that are known for Poisson approximations for sums of uniformly small random variables. Author\n\n# Subject Categories:\n\n• Statistics and Probability" ]
[ null ]
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https://www.arxiv-vanity.com/papers/1401.3305/
[ "arXiv Vanity renders academic papers from arXiv as responsive web pages so you don’t have to squint at a PDF. Read this paper on arXiv.org.\n\n# Open Quantum Walks on Graphs\n\nS. Attal Université de Lyon, Université de Lyon 1, C.N.R.S., Institut Camille Jordan, 21 av Claude Bernard, 69622 Villeubanne cedex, France F. Petruccione Quantum Research Group, School of Chemistry and Physics and National Institute for Theoretical Physics, University of KwaZulu-Natal, Durban, 4001, South Africa I. Sinayskiy Quantum Research Group, School of Chemistry and Physics and National Institute for Theoretical Physics, University of KwaZulu-Natal, Durban, 4001, South Africa\n###### Abstract\n\nOpen quantum walks (OQW) are formulated as quantum Markov chains on graphs. It is shown that OQWs are a very useful tool for the formulation of dissipative quantum computing algorithms and for dissipative quantum state preparation. In particular, single qubit gates and the CNOT-gate are implemented as OQWs on fully connected graphs. Also, dissipative quantum state preparation of arbitrary single qubit states and of all two-qubit Bell-states is demonstrated. Finally, the discrete time version of dissipative quantum computing is shown to be more efficient if formulated in the language of OQWs.\n\n###### keywords:\nOpen quantum walk, dissipative quantum computing, dissipative state engineering\njournal: Physics Letters A\n\n## 1 Introduction\n\nRecently, the experimental realization of a quantum computer has been the focus of extensive research QCR . One of the main problems of the physical implementation of well known quantum algorithms QA is the creation and manipulation of entanglement between qubits. Any physical system is subject to interaction with the environment, which inevitably leads to decoherence and dissipation toqs . One way to compensate for this destructive environmental influence in the unitary implementations of the quantum algorithms is to introduce error-correcting codes QECC . However, this approach treats the interaction with the environment as an effect the influence of which needs to be minimized.\n\nA paradigm shift in looking for alternative strategies to realize quantum computers was induced with the theoretical prediction that dissipation can be used to create complex entangled states Diehl and to perform universal quantum computation Vers . This fundamental change is based on the assumption that one can manipulate the coupling of a system to an environment in such a way that the system is driven towards a thermal state, which is the solution of a particular quantum computing task Vers or a target state in quantum state engineering Diehl ; Vers . The feasibility of this strategy was demonstrated by implementing dissipative quantum state engineering with ensembles of atoms Polzik and trapped ions Blatt .\n\nQuantum algorithms for universal quantum computing are conveniently formulated in the language of quantum walks uqwqc . For example, a discrete time quantum walk implementation of the search algorithm on complex graphs has been shown to be more efficient than other known implementations of this quantum algorithm QS . As for any other unitary implementation of quantum computing the efficiency of the quantum walk based realization decreases due to interaction with the environment. In view of the appeal of dissipative quantum computing it seems natural to formulate a dissipative version of the quantum walk so that algorithms for dissipative quantum computing and quantum state engineering are implemented efficiently. In other words, if dissipative quantum computing can make use of the interaction with the environment for performing universal quantum computation, can one introduce a framework which will use dissipative rather than unitary dynamics as a ”driving force” of the quantum walk?\n\nDuring the last few years attempts were made to take into account dissipation and decoherence in the description of quantum walks ken1 . In these approaches decoherence is treated as an extra modification of the unitary quantum walk scheme, the effect of which needs to be minimized and eliminated. In fact, the general framework of quantum stochastic walks was proposed qsw , which incorporates unitary and non-unitary effects of the quantum Markovian dynamics. In particular, by adding extra decoherence in experimental realizations of quantum walks, the transition from quantum to classical random walks was observed exp .\n\nRecently, a formalism for discrete time open quantum walks (OQW), which is exclusively based on the non-unitary dynamics induced by the environment was introduced APSS . OQWs are formulated in the language of quantum Markov chains gudder and rest upon the implementation of appropriate completely positive maps toqs ; kraus .\n\n## 2 Formalism\n\nTo review briefly the formalism of OQWs, we consider a random walk on a set of nodes or vertices with oriented edges as illustrated in Fig. 1(a). The number of nodes is considered to be finite or countable infinite. The space of states corresponding to the dynamics on the graph specified by the set of nodes will be denoted by and has an orthonormal basis . The internal degrees of freedom of the quantum walker, e.g. the spin or -energy levels, will be described by a separable Hilbert space attached to each node of the graph. More concisely, any state of the quantum walker will be described on the direct product of the Hilbert spaces .", null, "Figure 1: Schematic illustration of the formalism of the Open Quantum Walk. (a) The walk is realized on a graph with a set of vertices denoted by i,j,k∈V. The operators Bji describe transitions in the internal degree of freedom of the “walker” jumping from node (i) to node (j). (b) The simplest non-trivial example of the OQW on the finite graph is a walk on a two-node network. In this case the walk is performed using four operators Mji(i,j=1,2). In particular, the transitions between node 1 and node 2 are induced by the operators M21=B1⊗|1⟩⟨2| and M12=B2⊗|2⟩⟨1|; the operators describing changes in internal degrees of freedom of the ”walker”, if the ”walker” does not jump, are Mii=Ci⊗|i⟩⟨i|,(i=1,2).\n\nTo describe the dynamics of the quantum walker, for each edge we introduce a bounded operator . This operator describes the change in the internal degree of freedom of the walker due to the shift from node to node . By imposing for each that,\n\n ∑iBij†Bij=I, (1)\n\nwe make sure, that for each vertex of the graph there is a corresponding completely positive map on the positive operators of : Since the operators act only on and do not perform transitions from node to node , an operator can be introduced in the following form It is clear that, if the condition expressed in Eq. (1) is satisfied, then . This latter condition defines a completely positive map for density matrices on , i.e.,\n\n M(ρ)=∑i∑jMijρMij†. (2)\n\nThe above map defines the discrete time open quantum walk (OQW). For an arbitrary initial state the density matrix will take a diagonal form after just one step of the open quantum walk. By the direct insertion of an arbitrary initial condition in Eq. (2) we get\n\n M(∑k,mρk,m⊗|k⟩⟨m|) = ∑i,j,k,mBij⊗|i⟩⟨j|(ρk,m⊗|k⟩⟨m|)Bij†⊗|j⟩⟨i| (3) = ∑i,j,k,mBijρk,mBij†⊗|i⟩⟨i|δj,kδj,m = ∑i(∑jBijρj,jBij†)⊗|i⟩⟨i|.\n\nHence, we will assume that the initial state of the system has the form , with . It is straightforward to give an explicit formula for the iteration of the OQW from step to step : , where . This iteration formula gives a clear physical meaning to the mapping : the state of the system on site is determined by the conditional shift from all connected sites , which are defined by the explicit form of the operators . Also, one can see that . Generic properties of OQWs have been discussed in APSS .\n\nAs a first illustration of the application of the formalism of open quantum walks we consider the walk on a 2-node graph (see Fig. 1b). To be specific, the transition operators are and and the operators describing changes in internal degrees of freedom of the ”walker”, if the ”walker” does not jump, are . In this case for each node we have:\n\n B†iBi+C†iCi=I. (4)\n\nThe state of the walker after steps is given by,\n\n ρ[n]=ρ[n]1⊗|1⟩⟨1|+ρ[n]2⊗|2⟩⟨2|, (5)\n\nwhere the particular form of the is found by recursion,\n\n ρ[n]1=C1ρ[n−1]1C†1+B2ρ[n−1]2B†2, (6) ρ[n]2=C2ρ[n−1]1C†2+B1ρ[n−1]2B†1.", null, "Figure 2: Open quantum walk on Z. (a) A schematic representation of the OQW on Z: all transitions to the right are induced by the operator Bi+1i≡B, while all transitions to the left are induced by the operator Bi−1i≡C (see Eq. (7)); Figures (b)-(e) show the occupation probability distribution for the “walker” with the initial state I2/2⊗|0⟩⟨0| and transition operators given by Eq. (7) after 10, 20, 50 and 100 steps, respectively. Two distinctive behaviors of the walker are observed: a Gaussian wave-packet moving slowly to the left (dots) and a deterministic trapped state propagating to the right at a speed of 1 in units of cells per time step (cross).\n\nNext we consider an open quantum walk on the line. The situation is depicted in Fig. 2 (a). For this simple one-dimensional walk, the only non-zero transitions out of cell are given by operators of the form and . Obviously, the operators and satisfy the condition , as imposed in Eq. (1). Assuming the initial state of the system to be localized on site , i.e., , after one step the system will jump to sites so that the new density matrix will be . The procedure can easily be iterated. In Figs. 2(b)-(e) we show the probability to find a “walker” on a particular lattice site for different numbers of steps. For this simulation we have chosen the transition matrices and as follows,\n\n B=sinθ|−⟩⟨−|+|+⟩⟨+|,C=cosθ|−⟩⟨−|, (7)\n\nand . One can see that already after 10 steps, there are two distinctive behaviors of the “walker”. The first is a Gaussian wave-packet moving slowly to the left and the second one is a completely deterministic trapped state propagating to the right at a speed of 1 in units of cells per time step. Interestingly, the state of the “walker” in the “soliton like” part is given by , while in the other, Gaussian part is given by the , where, of course and states are defined as and is the probability to find the “walker” on the site . Even this simple example demonstrates a remarkable dynamical richness of OQW. Further examples of OQW on which show a behavior distinct from the classical random walk and the unitary quantum walk can be found in APSS .\n\n## 3 OQW for dissipative quantum computing and state engineering", null, "Figure 3: OQW preparation of the Bell-states of two qubits. A generic OQW walk on a 4-node graph is decomposed in two walks on two-nodes graphs: “left-right” and “down-up” walks. For an initial unpolarized state of two-qubits on any nodes ρ0=14I4⊗|i⟩⟨i| the corresponding Bell-pairs are obtained by measuring the position of the walkers after performing the OQW.\n\nTo motivate the potential of the suggested approach for the formulation of quantum algorithms for dissipative quantum computing and quantum state engineering we consider the example of an OQW on the 2-node fully connected graph in Fig. 1 (b). This example, will show that it is possible to implement all single-qubit gates and the CNOT-gate in the language of the suggested formalism. To be specific, in order to realize an X-gate with OQWs we prepare the system in some initial state in node 1 and we will read the result of the computation in the node 2 (See Fig. 1(b)). If we choose , , and , where and are positive constants such that , then the stationary state of this walk will have the following form . Therefore, the OQW on this graph realizes the X-gate with probability upon read-out of the presence of the “walker” in node 2. In a similar way, in order to implement the CNOT-gate we initially place two “walkers” in node 1. We choose , , and and if the presence of both “walkers” is measured in the node 2 then the OQW realized the CNOT-gate with probability .\n\nOn the same 2-node network we can also implement dissipative state preparation (see Fig. 1(b)). To this end, we consider trivial transition matrices on the node 1, i.e., and non-unitary transition matrices on the node 2, i.e., and , where and are positive constants such that , and . With this choice an arbitrary initial state will converge to a unique steady state, namely . The probability of detecting the system in the steady state after steps of the walk is given by , where are the elements of the initial density matrix of the system, .\n\nOQWs on more complex graphs allow the dissipative preparation of entangled multi-qubit states. With two “walkers” on a 4-node network (see Fig. 3) we can prepare all two-qubits Bell-states. In this particular case, the OQW can be decomposed in a combination of two walks on two independent 2-node networks. The first “walker” moves up and down, while the second one moves left and right (see Fig.3). We choose the transition operators to be , , and , where and denotes Pauli matrices acting on the corresponding qubit (). Starting with “walkers” initially in an unpolarized state in any node, i.e. , the OQW will converge to a state . This means that measuring the position of the “walkers” will determine corresponding Bell-state of their internal degrees of freedom note .", null, "Figure 4: Efficient transport with Open Quantum Walk. Fig. (a): a scheme of the chain of the N nodes with neighbor-neighbor interaction. Fig. (b): occupation probability distribution as a function of time and lattice sites. The initial state of the walker is localized in the first node and given by ρ0=12I2⊗|1⟩⟨1|.\n\nAnother application of the OQWs is a description of a dissipatively driven quantum bus between computational quantum registers. To this end we consider a chain of nodes (see Fig. 4(a)). Initially, the first node of the chain is in the exited state, so that . To be specific, we chose transition operators and as follows, and . It is very interesting to note that in this case the state propagates through the chain with velocity almost equal to 1 (in units of cells per time step): the initial excitation in node (1) is completely transferred to the last node (N) in N+2 steps. In Fig. 4 (b) we consider a 100 node chain with , , and show that the initial excitation reaches the final node (100) in 102 steps. The high performance of transport of excitations in the OQW formalism opens up new avenues of research into the understanding of quantum efficiency in open systems.\n\nOQWs include the discrete time version of the dissipative quantum computing (DQC) introduced by Verstraete et al. Vers . In the original setup a linear chain of time registers is considered and the initial state is prepared in the time register . A quantum computation is performed by the dissipative evolution of the system into its unique steady state Vers . The result of the quantum computation can be read-out by measuring the state of the system in the last time register which is given by , where is an appropriate sequence of unitary operators Vers . The probability of a successful read-out is . A discrete time version of DQC can be realized as an OQW on a linear chain of time registers (Fig. 5) by choosing the transition operators as it is shown in Fig. 5 and constants . However, with the same number of steps in the OQW formulation of DQC the probability of successful read-out can be increased arbitrarily close to one. In order to understand this dramatic improvement in efficiency we recall that in the original DQC formulation the probability of read-out of the final state is determined by the form of “jumping” operators between time registers, i.e., . The probability to ”jump” forward and backward in the time register is the same. In the OQW formulation of the DQC we have the freedom of choosing which induces the steady state of the OQW with probability of read-out of the final state between and .", null, "Figure 5: OQW formulation of dissipative quantum computing (DQC). The initial state is prepared in the time-register 0. After performing the OQW, the results of the algorithm can be readout from the time-register N. The internal state of the ”walker” in the register T will be given by |ψT⟩=UT…U1|ψ0⟩. The positive constants ω and λ satisfy ω+λ=1.\n\n## 4 Conclusion\n\nIn conclusion, we have shown that the recently introduced formalism of OQWs is a very useful tool for the formulation of dissipative quantum computing algorithms and for dissipative quantum state preparation. OQWs are to dissipative quantum computing what Hadamard quantum walks are to circuit based quantum computing. In particular, we have shown OQW implementation of circuit and dissipative models of quantum computing. Remarkably, the OQW discretisation of dissipative quantum computing increases the probability of successful implementation of the quantum algorithm with respect to the original formulation. It is to be expected, that OQWs will lead to the optimal formulation of certain classes of quantum algorithms. Furthermore, we have indicated that OQW can be used to explain non-trivial highly efficient transport phenomena not only in linear but also in more complex topologies of the underlying graphs. This implies that OQW as quantum walks which are driven by dissipation and decoherence are one of the candidates for understanding the remarkable transport efficiency in photosynthetic complexes qbt . We expect the potential of this framework to be soon revealed in the realms of quantum computing and quantum biology.\n\n## Acknowledgements\n\nThis work is based upon research supported by the South African Research Chair Initiative of the Department of Science and Technology and National Research Foundation. Work supported by ANR project “HAM-MARK” N ANR-09-BLAN-0098-01" ]
[ null, "https://media.arxiv-vanity.com/render-output/2952892/x1.png", null, "https://media.arxiv-vanity.com/render-output/2952892/x2.png", null, "https://media.arxiv-vanity.com/render-output/2952892/x3.png", null, "https://media.arxiv-vanity.com/render-output/2952892/x4.png", null, "https://media.arxiv-vanity.com/render-output/2952892/x5.png", null ]
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https://jp.maplesoft.com/support/help/maple/view.aspx?path=geometry/CrossRatio&L=J
[ "", null, "geometry - Maple Programming Help\n\nHome : Support : Online Help : Mathematics : Geometry : 2-D Euclidean : Point Functions : geometry/CrossRatio\n\ngeometry\n\n CrossRatio\n compute the cross ratio (or anharmonic ratio, or double ratio) of four points\n\n Calling Sequence CrossRatio(A, B, C, F)\n\nParameters\n\n A, B, C, F - four points\n\nDescription\n\n • Given four points A, B, C, F, the routine CrossRatio(A, B, C, F) computes the cross ratio of A, B, C, F taken in this order.\n • If A, B, C, F are four distinct points on an ordinary line, the cross ratio of A, B, C, F taken in this order is defined as:\n\n$\\frac{\\frac{\\mathrm{SensedMagnitude}\\left(A,C\\right)}{\\mathrm{SensedMagnitude}\\left(C,B\\right)}}{\\frac{\\mathrm{SensedMagnitude}\\left(A,F\\right)}{\\mathrm{SensedMagnitude}\\left(F,B\\right)}}$\n\n • The command with(geometry,CrossRatio) allows the use of the abbreviated form of this command.\n\nExamples\n\n > $\\mathrm{with}\\left(\\mathrm{geometry}\\right):$\n > $\\mathrm{point}\\left(A,0,0\\right),\\mathrm{point}\\left(B,3,3\\right),\\mathrm{point}\\left(C,7,7\\right),\\mathrm{point}\\left(F,\\frac{21}{11},\\frac{21}{11}\\right):$\n > $\\mathrm{CrossRatio}\\left(A,B,C,F\\right)$\n ${-}\\frac{\\sqrt{{98}}{}\\sqrt{{32}}{}\\sqrt{{882}}{}\\sqrt{{288}}}{{28224}}$ (1)\n > $\\mathrm{CrossRatio}\\left(A,C,B,F\\right)$\n $\\frac{\\sqrt{{18}}{}\\sqrt{{32}}{}\\sqrt{{882}}{}\\sqrt{{6272}}}{{28224}}$ (2)" ]
[ null, "https://bat.bing.com/action/0", null ]
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https://corporatefinanceinstitute.com/resources/excel/functions/choose-function/
[ "# CHOOSE Function\n\nReturns a value from an array corresponding to the index number provided\n\n## What is the CHOOSE Function?\n\nThe CHOOSE function is categorized under Excel Lookup and Reference functions. It will return a value from an array corresponding to the index number provided. The function will return the nth entry in a given list.\n\nAs a financial analyst, the CHOOSE function is very useful when creating scenarios in financial models.  By using the CHOOSE formula, an analyst is able to select between 5 different scenarios (for example) that can flow through the entire model.  Scenario analysis is an important part of building a robust financial model.", null, "### Formula\n\n=CHOOSE(index_num, value1, [value2], …)\n\nThe formula uses the following arguments:\n\n1. Index_num (required argument) – This is an integer that specifies which value argument is selected. Index_num must be a number between 1 and 254, or a formula or reference to a cell containing a number between 1 and 254.\n2. Value1, Value2 – Value1 is a required option but the rest are optional. It is a list of one or more values that we want to return a value from.\n\n#### Notes:\n\n1. If index_num is 1, CHOOSE returns value1; if it is 2, CHOOSE returns value2; and so on.\n2. Value1, value2 must be entered as individual values (or references to individual cells containing values).\n3. If the argument index_num is a fraction, it is truncated to the lowest integer before being used.\n4. If the argument index_num is an array, every value is evaluated when CHOOSE is evaluated.\n5. The value arguments can be range references, as well as single values.\n\n### How to use the CHOOSE Function in Excel?\n\nTo understand the uses of the CHOOSE function, let’s consider an example:\n\n#### Example 1\n\nSuppose we are given the following dates:", null, "We can calculate the fiscal quarter from the dates given above. The fiscal quarters start in a month other than January.\n\nThe formula to use is:", null, "The formula returns a number from the array 1-4, which corresponds to a quarter system that begins in April and ends in March.\n\nWe get the results below:", null, "### A few notes about the CHOOSE Function\n\n1. VALUE! error – Occurs when:\n• The given index_num is less than 1 or is greater than the given number of values.\n• The given index_num argument is non-numeric.\n1. #NAME? error – Occurs when the value arguments are text values that are not enclosed in quotes and are not valid cell references.\n\nThanks for reading CFI’s guide to important Excel functions! By taking the time to learn and master these functions, you’ll significantly speed up your financial modeling and analysis. To learn more, check out these additional CFI resources:\n\n• Excel for Finance" ]
[ null, "https://cdn.corporatefinanceinstitute.com/assets/scenarios-1024x534.png", null, "https://cdn.corporatefinanceinstitute.com/assets/choose-function01.png", null, "https://cdn.corporatefinanceinstitute.com/assets/choose-function02.png", null, "https://cdn.corporatefinanceinstitute.com/assets/choose-function03.png", null ]
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https://www.freesteel.co.uk/wpblog/2007/06/11/point-inside-triangle-correct/
[ "## Point inside triangle correct\n\nMonday, June 11th, 2007 at 11:02 am", null, "Following from the incorrect method for finding which triangle of a mesh a given point is inside, here is the right answer.\n\nThe trick is to know that the only lines you can reliably tell sidedness along are those parallel to the X or Y axes, and the special cases of the lines x = y and x = -y. All other lines, defined by, say, a + tv, are going to prove somewhat noisy close in when attempting to determine which side of them a given point lies if you use the standard relation:\n\n(p - a) . vT > 0\n\nIn particular, if you have three lines passing through the same point and that point is not the a point in all of them, they won’t, and you’ll get a little unexpected area inside the triangle where they don’t all meet.\n\nSo, the scan line method works along the Y-axis. The triangle here has, relative to this direction, ay < cy < by. All the intervals are half-open, which means the point p can hit the triangle only when ay <= py < cy. The triangle also separates into two parts, the lower where py < cy and the upper where py >= cy.\n\nIn this diagram p is in the upper part, so we find the intersections of the line Y = py with the lines ab and cb to get points xab and xcb (not labeled). It doesn’t matter what order because they can be sorted and then treated as a half-open interval for comparison to the value px.\n\nActually, it is a good question whether the condition xab < xcb will remain the same for all values of py. I don’t know the answer to this one, and it probably depends on how carefully you calculate it. Ideally, if it’s determined that c is to the right of the line ab, then it’s consistent for all Y.\n\nOne has to assume the 2D triangle meshes are very nasty because the problem we’re actually trying to solve is the intersection of a 3D line through a polyhedral mesh representing the surface of a solid volume. The first step is always to project the entire model onto the plane perpendicular to the line (so that the line becomes a point). Even though you began with a well-behaved triangular surface, there are projections where the triangles turn into slivers and shards.\n\n• 1. SJ replies at 12th June 2007, 5:52 am :\n\nBogus logic. If you start with line segments represented in terms of their endpoints, and triangles represented in terms of line segments with common endpoints, then you can solve the problem robustly using only that single ‘sign of the determinant’ function. But if you choose to throw away\ninformation (and accuracy) by converting the line representation to a ‘standard’ parametric one, you are introducing the noise yourself. Frankly, you are big-headed and unbearable…\n\n• 2. Julian replies at 21st November 2008, 4:18 pm :\n\nYou needed to follow the link given to know what it is correcting:\n\nhttp://www.freesteel.co.uk/wpblog/2007/05/finding-points-in-triangles/\n\nThe standard method is fine if you only have one triangle. The reason for this non-standard method is it guarentees that the point will be found in exactly one triangle of a mesh covering of the plane.\n\nBut obviously if you don’t know this, the method looks kind of stupid. Depending on how quick-witted you want to be, you can leap to the conclusion that you are right and I am wrong, if that’s how you’d like it to be.\n\n• 3. anderswallin.net ›&hellip replies at 17th December 2011, 11:39 am :\n\n[…] check if the CC point lies within the triangle, but that will have to wait until the next post… (Mr. Todd has some thoughts on this) This was written by admin. Posted on Monday, June 25, 2007, at 21:06. Filed under Drop-Cutter. […]" ]
[ null, "http://www.freesteel.co.uk/images/blog/insidetriangscan.png", null ]
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https://oemz-online.at/exportword?pageId=34373859
[ "Message-ID: <27643314.26951.1607169619488.JavaMail.confluence@omzconfluence> Subject: Exported From Confluence MIME-Version: 1.0 Content-Type: multipart/related; boundary=\"----=_Part_26950_716305635.1607169619488\" ------=_Part_26950_716305635.1607169619488 Content-Type: text/html; charset=UTF-8 Content-Transfer-Encoding: quoted-printable Content-Location: file:///C:/exported.html 2020/4/3 (EN): Mader\n\n=20\n=20\n=20\n=20\n\n# =E2=80=9ESoldier dri= ll=E2=80=9C in the k. (u.) k. Army\n\n=20\n=20\n=20\n=20\n=20\n=20\n\n=20\n=20\n=20\n=20\n=20\n=20\n\nHugo Kerchnawe, latter Austrian ma= jor general and military historian, authored the book =E2=80=9EMilitary and= Civilian=E2=80=9C as =E2=80=9EAnonymous=E2=80=9D in 1904. In this publication, Kerchnawe demonstrated ar= ticulately his critical distance towards the army and its practice of train= ing soldiers. In the introduction he writes that he =E2=80=9Edoes not try to hide his sympathy for the ar= my at all=E2=80=9D, but that he, on the other hand, =E2=80=9Ehad not been rendered blind=E2=80=9D for its= weaknesses and been hindered from discussing and =E2=80=9Evituperate=E2=80=9D them. Naturally, he knew t= hat this courage was resented and criticized by many in the army. Kerchnawe= proved convinced that the course taken by him was the only correct one and= would contribute to the best of the army. The hush-up system customary in = the country did not help the military much. It only strengthened its (numer= ous) opponents and achieved the opposite of what was to be purposed. Nevert= heless, there were some =E2=80=9Eshort-sighted=E2=80=9D circles in the army who suspected animosity or at= least inappropriate deprecation in such positive criticism. He himself wis= hed that these =E2=80=9Eshort-= sighted=E2=80=9D people understood that it certainly was not true exaltatio= n to deny the mistakes of one stands for, and not to mend them. In his book= , Kerchnawe also deals with the topic =E2=80=9Emaltreatment of soldiers=E2=80=9D. Apart from the reproach= of =E2=80=9Emilitarism=E2=80= =9D (military dominance), nothing was so often brought forward against the = military as these maltreatments of soldiers. There was not a single parliam= entary session without such accusations, which were discussed in the most <= span style=3D\"color: rgb(51,51,51);\">=E2=80=9Espiteful=E2=80=9D way.= An objective treatment of this problem did not exist in the Austrian press= - nearly the entire press =E2=80=9E<= /span>stood under the banner of the ideals of 1848 without exception=E2=80= =9D, opposing the military, bringing forward not a single word in its favou= r. Thus, Kerchnawe continued, one ought to advise the military authorities = emphatically to investigate every suspicion of maltreatment by a superior. = After an accurate investigation of the circumstances, the guilty must be pu= nished without lenience, thus stopping the spiteful palaver against the mil= itary. As Kerchnawe states, nothing was worse than the operated (popular) h= ush-up system. In the =E2=80=9Edarkness of keeping secrets=E2=80=9C and =E2=80=9Ein the uncertain twiligh= t of sugar-coated presentments=E2=80=9D, the maltreatments of soldiers look= ed even uglier than they were in reality. For this reason, the public were = permanently given the levelheadedness and verisimilitude they had the right= to receive. The military would =E2= =80=9Eprofit=E2=80=9D from that. Despite his understanding for super= iors sometimes losing their temper, Kerchnawe did not support =E2=80=9Eviolent pedagogy=E2=80=9D at all= , meaning that he depreciated brutality. As Kerchnawe pointed out, there we= re indirect maltreatments in the military as well. The originators were off= icers, often even with higher ranks, and their motives were recklessness an= d indifference for the well-being of their subordinates. Often together wit= h the ambition to =E2=80=9Eshi= ne with extraordinary military strains=E2=80=9D. These often resulted in (s= tartling) high numbers of sick soldiers, numerous sunstroke and heatstroke = cases, and even fatalities. So, this maltreatment of the personnel manifest= ed in =E2=80=9Eunreasonable an= d not seldom barbarous exigencies=E2=80=9D. Thus, Kerchnawe (stridently) cr= iticized the evils in the k. u. k. Army without questioning the entire syst= em. Military drill aims at forming up the drives and emotions of single sol= diers appropriately. That means that the training (drill) ought to evoke an= d consolidate military obedience with the soldiers (especially in the turmo= il of battle). According to that, the total character of the military is ba= sed on a strict hierarchy, as well as on certain assumptions concerning the= social behaviour both of the individual and the troops in the extraordinar= y situations of combat. The ultimate purpose of achieving military discipli= ne thus was eliminating of uncertainties in the face of the unpredictable c= ircumstances of war. The traditional appearance of the soldier of the 1860i= es was re-analysed due to different reasons, but pure humaneness was (mostl= y) not the impetus. On the contrary, many people realized that with soldier= s who had been =E2=80=9Eunlear= ned=E2=80=9D any independence one could not win wars. On the other hand, ho= wever, a deep hiatus arose between theory and practice as far as the =E2=80=9Edrill=E2=80=9D of soldiers = was concerned. Obviously, the (positive) theoretical considerations<= /p>\n\n=20\n=20\n=20\n=20\n=20\n=20\n\n=20\n=20\n=20\n=20\n\n=20\n=20\n=20\n=20\n\n=20\n=20\n=20" ]
[ null ]
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https://convertoctopus.com/30-3-hours-to-minutes
[ "## Conversion formula\n\nThe conversion factor from hours to minutes is 60, which means that 1 hour is equal to 60 minutes:\n\n1 hr = 60 min\n\nTo convert 30.3 hours into minutes we have to multiply 30.3 by the conversion factor in order to get the time amount from hours to minutes. We can also form a simple proportion to calculate the result:\n\n1 hr → 60 min\n\n30.3 hr → T(min)\n\nSolve the above proportion to obtain the time T in minutes:\n\nT(min) = 30.3 hr × 60 min\n\nT(min) = 1818 min\n\nThe final result is:\n\n30.3 hr → 1818 min\n\nWe conclude that 30.3 hours is equivalent to 1818 minutes:\n\n30.3 hours = 1818 minutes\n\n## Alternative conversion\n\nWe can also convert by utilizing the inverse value of the conversion factor. In this case 1 minute is equal to 0.00055005500550055 × 30.3 hours.\n\nAnother way is saying that 30.3 hours is equal to 1 ÷ 0.00055005500550055 minutes.\n\n## Approximate result\n\nFor practical purposes we can round our final result to an approximate numerical value. We can say that thirty point three hours is approximately one thousand eight hundred eighteen minutes:\n\n30.3 hr ≅ 1818 min\n\nAn alternative is also that one minute is approximately zero point zero zero one times thirty point three hours.\n\n## Conversion table\n\n### hours to minutes chart\n\nFor quick reference purposes, below is the conversion table you can use to convert from hours to minutes\n\nhours (hr) minutes (min)\n31.3 hours 1878 minutes\n32.3 hours 1938 minutes\n33.3 hours 1998 minutes\n34.3 hours 2058 minutes\n35.3 hours 2118 minutes\n36.3 hours 2178 minutes\n37.3 hours 2238 minutes\n38.3 hours 2298 minutes\n39.3 hours 2358 minutes\n40.3 hours 2418 minutes" ]
[ null ]
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https://www.amansmathsblogs.com/s-chand-icse-maths-solutions-class-10-chapter-5-quadratic-equations-exercise-5e/
[ "Thursday, August 11, 2022\nHome > ICSE Solutions for Class 10 Maths > S Chand ICSE Maths Solutions Class 10 Chapter 5 Quadratic Equations Exercise 5E\n\n# S Chand ICSE Maths Solutions Class 10 Chapter 5 Quadratic Equations Exercise 5E\n\nHi students, Welcome to Amans Maths Blogs (AMB). In this post, you will get S Chand ICSE Maths Solutions Class 10 Chapter 5 Quadratic Equations Exercise 5E. This is the chapter of introduction of ‘Quadratic Equations‘ included in ICSE 2020 Class 10 Maths syllabus.\n\nIn S Chand ICSE Maths Solutions Class 10 Chapter 5 Quadratic Equations Exercise 5E, word problems are given. First, we need to make a quadratic equation according to the given question and then we need to solve them.\n\n## S Chand ICSE Maths Solutions Class 10 Chapter 5 Quadratic Equations Exercise 5E\n\nS Chand ICSE Maths Solutions Class 10 Quadratic Equations Exercise 5E: Ques No 1\n\nThe sum of the squares of two consecutive positive even integers is 100. Find the integers.\n\nS Chand ICSE Maths Solutions:\n\nLet two consecutive positive even integers are x and (x + 2). Then, we have\n\nx2 + (x + 2)2 = 100\n\n⇒ x2 + x2 + 4x + 4 = 100\n\n⇒ 2x2 + 4x – 96 = 0\n\n⇒ x2 + 2x – 48 = 0\n\n⇒ x2 + 8x – 6x – 48 = 0\n\n⇒ x(x + 8) – 6(x + 8) = 0\n\n⇒ (x – 6)(x + 8) = 0\n\n⇒ x = 6 or -8\n\nSince x is positive even integer, then x = 6 and hence other positive even integer is (x + 2) = 8.\n\nThus, the required integers are 6 and 8.\n\nS Chand ICSE Maths Solutions Class 10 Quadratic Equations Exercise 5E: Ques No 2\n\nFind two rational numbers which differ by 3 and the sum of whose squares is 117.\n\nS Chand ICSE Maths Solutions:\n\nLet two rational numbers are x and (x + 3). Then, we have\n\nx2 + (x + 3)2 = 117\n\n⇒ x2 + x2 + 6x + 9 = 117\n\n⇒ 2x2 + 6x + 9 = 117\n\n⇒ 2x2 + 6x – 108 = 0\n\n⇒ x2 + 3x – 54 = 0\n\n⇒ x2 + 9x – 6x – 54 = 0\n\n⇒ x(x + 9) – 6(x + 9) = 0\n\n⇒ (x – 6)(x + 9) = 0\n\n⇒ x = 6 or -9\n\nIf x = 6, then (x + 3) = 9\n\nIf x = -9, then (x + 3) = -6\n\nThus, the required rational numbers are 6 and 9 or -9 and -6.\n\nS Chand ICSE Maths Solutions Class 10 Quadratic Equations Exercise 5E: Ques No 3\n\nWhat number increased by its reciprocal equals 65/8?\n\nS Chand ICSE Maths Solutions:\n\nLet the number is x. Then, we have\n\nx + 1/x = 65/8\n\n⇒ (x2 + 1)/x = 65/8\n\n⇒ 8(x2 + 1) = 65x\n\n⇒ 8x2 – 65x + 8 = 0\n\n⇒ 8x2 – 64x – x + 8 = 0\n\n⇒ 8x(x – 8) – 1(x – 8) = 0\n\n⇒ (8x – 1)(x – 8) = 0\n\n⇒ x = 1/8 or 8\n\nThus, the required number is 8 or 1/8.\n\nS Chand ICSE Maths Solutions Class 10 Quadratic Equations Exercise 5E: Ques No 4\n\nThe sum of the numerator and denominator of a certain fraction is 8. If 2 is added to the numerator and to the denominator, the value of the fraction is increased by 4/35. Find the fraction.\n\nS Chand ICSE Maths Solutions:\n\nLet the fraction is x / (8 – x). Then, we have\n\n(x + 2)/(8 – x + 2) = x/(8 – x) + 4/35\n\n⇒ (x + 2)/(10 – x) – x/(8 – x) = 4/35\n\n⇒ [(x + 2)(8 – x) – x(10 – x)]/(10 – x)(8 – x) = 4/35\n\n⇒ [8x – x2 + 16 – 2x – 10x + x2]/(80 – 10x – 8x + x2) = 4/35\n\n⇒ 35[16 – 4x] = 4(x2 – 18x + 80)\n\n⇒ 35[4 – x] = (x2 – 18x + 80)\n\n⇒ x2 + 17x – 60 = 0\n\n⇒ x2 + 20x – 3x – 60 = 0\n\n⇒ x(x + 20) – 3(x + 20) = 0\n\n⇒ (x – 3)(x + 20) = 0\n\n⇒ x = 3 or -20\n\nThus, the required fraction is x/(8 – x) = 3/5.\n\nS Chand ICSE Maths Solutions Class 10 Quadratic Equations Exercise 5E: Ques No 5\n\nThere are three consecutive integers such that the square of the first increased by the product of the other two gives 154. Find the integers.\n\nS Chand ICSE Maths Solutions:\n\nLet three consecutive integers are x, (x + 1) and (x + 2). Then, we have\n\nx2 + (x + 1)(x + 2) = 154\n\n⇒ x2 + x2 + 3x + 2 = 154\n\n⇒ 2x2 + 3x – 152 = 0\n\n⇒ 2x2 – 16x + 19x – 152 = 0\n\n⇒ 2x(x – 8) + 19(x – 8) = 0\n\n⇒ (2x + 19)(x – 8) = 0\n\n⇒ x = -19/2 or 8.\n\nThus, the required three consecutive integers are 8, 9, 10.\n\nS Chand ICSE Maths Solutions Class 10 Quadratic Equations Exercise 5E: Ques No 6\n\nThe sum of two numbers is 8 and 15 times the sum of their reciprocals is also 8. Find the numbers.\n\nS Chand ICSE Maths Solutions:\n\nLet two numbers are x and (8 – x). Then, we have\n\n15[1/x + 1/(8 – x)] = 8\n\n⇒ 15(8 – x + x)/x(8 – x) = 8\n\n⇒ 15(8) = 8x(8 – x)\n\n⇒ 15 = x(8 – x)\n\n⇒ x2 – 8x + 15 = 0\n\n⇒ x2 – 3x – 5x + 15 = 0\n\n⇒ x(x – 3) – 5(x – 3) = 0\n\n⇒ (x – 5)(x – 3) = 0\n\n⇒ x = 3 or 5\n\nIf x = 3, then (8 – x) = 5\n\nIf x = 5, then (8 – x) = 3\n\nThus, the required numbers are 3 and 5.\n\nS Chand ICSE Maths Solutions Class 10 Quadratic Equations Exercise 5E: Ques No 7\n\nA two digit number is such that the product of the digits is 12. When 36 is added to this number, the digits interchange their places. Find the number.\n\nS Chand ICSE Maths Solutions:\n\nLet the unit digit of the number is x, then its tens digit is 12/x. Then, we have\n\n10(12/x) + x + 36 = 10x + 12/x\n\n⇒ 9x – 9(12/x) = 36\n\n⇒ x – (12/x) = 4\n\n⇒ (x2 – 12)/x = 4\n\n⇒ (x2 – 12) = 4x\n\n⇒ x2 – 4x – 12 = 0\n\n⇒ x2 – 6x + 2x – 12 = 0\n\n⇒ x(x – 6) + 2(x – 6) = 0\n\n⇒ (x + 2)(x – 6) = 0\n\n⇒ x = -2 or 6\n\nSince x is a digit, then x = 6.\n\nThus, the unit digit is x = 6 and tens digit 12/x = 2 and hence the number is 26\n\nS Chand ICSE Maths Solutions Class 10 Quadratic Equations Exercise 5E: Ques No 8\n\nFive times a certain whole number is equal to three less than twice the square of the number. Find the number.\n\nS Chand ICSE Maths Solutions:\n\nLet the whole number is x. Then, we have\n\n5x = 2x2 – 3\n\n⇒ 2x2 – 5x – 3 = 0\n\n⇒ 2x2 – 6x + x – 3 = 0\n\n⇒ 2x(x – 3) + 1(x – 3) = 0\n\n⇒ (2x + 1)(x – 3) = 0\n\n⇒ x = -1/2 or 3\n\nSince x is a whole number, then the required number is x = 3.\n\nS Chand ICSE Maths Solutions Class 10 Quadratic Equations Exercise 5E: Ques No 9\n\nThree consecutive numbers are such that the square of the middle number exceeds the difference of the squares of the other two by 60. Assume the middle number to be x and form a quadratic equation satisfying the above statement. Hence, find the three numbers.\n\nS Chand ICSE Maths Solutions:\n\nLet the three number are (x – 1), x, (x + 1). Then, we have\n\nx2 = (x + 1)2 – (x – 1)2 + 60\n\n⇒ x2 = x2 + 2x + 1 – x2 + 2x – 1 + 60\n\n⇒ x2 – 4x – 60 = 0\n\n⇒ x2 – 10x + 6x – 60 = 0\n\n⇒ x(x – 10) + 6(x – 10) = 0\n\n⇒ (x + 6)(x – 10) = 0\n\n⇒ x = -6 or 10\n\nThus, the three numbers are 9, 10 and 11.\n\nS Chand ICSE Maths Solutions Class 10 Quadratic Equations Exercise 5E: Ques No 10\n\nThe sum of the ages (in years) of a son and his father is 35 and the product of their ages is 150. Find their ages.\n\nS Chand ICSE Maths Solutions:\n\nLet the father’s age is x years then his son’s age is (35 – x) years. Then, we have\n\nx(35 – x) = 150\n\n⇒ 35x – x2 = 150\n\n⇒ x2 – 35x + 150 = 0\n\n⇒ x2 – 30x – 5x + 150 = 0\n\n⇒ x(x – 30) – 5(x – 30) = 0\n\n⇒ (x – 5)(x – 30) = 0\n\n⇒ x = 5 or 30\n\nThus, the father’s age is x = 30 years then his son’s age is (35 – x) = 5 years\n\nS Chand ICSE Maths Solutions Class 10 Quadratic Equations Exercise 5E: Ques No 11\n\nAnjali was born in 1985 A.D. In the year x2 AD, she was (x – 5) years old. Find the value of x.\n\nS Chand ICSE Maths Solutions:\n\nIn the year x2 AD, Anjali was (x – 5) years old. Then, we have\n\nx2 – 1985 = (x – 5)\n\n⇒ x2 – x – 1980 = 0\n\n⇒ x2 – 45x + 44x – 1980 = 0\n\n⇒ x(x – 45) + 44(x – 45) = 0\n\n⇒ (x + 44)(x – 45) = 0\n\n⇒ x = -44 or 45\n\nSince x is year, x = 45.\n\nS Chand ICSE Maths Solutions Class 10 Quadratic Equations Exercise 5E: Ques No 12\n\nThe difference of mother’s age and her daughter’s age is 21 years and the twelfth part of the product of their ages is less than the mother’s age by 18 years. Find their ages.\n\nS Chand ICSE Maths Solutions:\n\nLet the daughter’s age is x years then her mother’s age is (x + 21) years. Then, we have\n\nx(x + 21) / 12 = (x + 21) – 18\n\n⇒ x2 + 21x = 12(x + 3)\n\n⇒ x2 + 21x = 12x + 36\n\n⇒ x2 + 9x – 36 = 0\n\n⇒ x2 + 12x – 3x – 36 = 0\n\n⇒ (x + 12) – 3(x + 12) = 0\n\n⇒ (x – 3)(x + 12) = 0\n\n⇒ x = 3 or -12\n\nSince x is an age, x = 3\n\nThus, daughter’s age is x = 3 years and mother’s age is (x + 21) = 24 years.\n\nS Chand ICSE Maths Solutions Class 10 Quadratic Equations Exercise 5E: Ques No 13\n\nReena is x year old, while her father Mr. Sunil is x2 years old. 5 years hence, Mr Sunil will be three times as old as Reena. Find their present ages.\n\nS Chand ICSE Maths Solutions:\n\nGiven that Reena is x year old, while her father Mr. Sunil is x2 years old.\n\nAfter 5 years, Mr Sunil will be three times as old as Reena.\n\nThen, we have\n\nx2 + 5 = 3(x + 5)\n\n⇒ x2 – 3x – 10 = 0\n\n⇒ x2 – 5x + 2x – 10 = 0\n\n⇒ x(x – 5) + 2(x – 5) = 0\n\n⇒ (x + 2)(x – 5) = 0\n\n⇒ x = -2 or 5\n\nSince x is an age, x = 5.\n\nThus, Reena is x = 5 year old and her father Mr. Sunil is x2 = 25 years old.\n\nS Chand ICSE Maths Solutions Class 10 Quadratic Equations Exercise 5E: Ques No 14\n\nForm a quadratic equation from the following information, taking as width x ∈ N.\n\n(i) The area of rectangle whose length is five more than twice its width is 75.\n\n(ii) Solve the equation and find its length.\n\nS Chand ICSE Maths Solutions:\n\nGiven that the width of rectangle is x, and hence the length of the rectangle is (2x + 5).\n\nThen, we have\n\nx(2x + 5) = 75\n\n⇒ 2x2 + 5x – 75 = 0 [This is required quadratic equation.]\n\n⇒ 2x2 + 15x – 10x – 75 = 0\n\n⇒ x(2x + 15) – 5(2x + 15) = 0\n\n⇒ (x – 5)(2x + 15) = 0\n\n⇒ x = 5 or -15/2\n\nThus, the width of the rectangle is x = 5.\n\nS Chand ICSE Maths Solutions Class 10 Quadratic Equations Exercise 5E: Ques No 15\n\nThe sides of a right angled triangle containing the right angle are 5x cm and (3x – 1) cm. If the area of the triangle be 60 cm2, calculate the lengths of the sides of triangle.\n\nS Chand ICSE Maths Solutions:\n\nGiven that the area of a right angled triangle, whose legs are 5x cm and (3x – 1) cm, is 60 cm2.\n\nThen, we have\n\n(1/2) × (5x) × (3x – 1) = 60\n\n⇒ 15x2 – 5x – 120 = 0\n\n⇒ 5(3x2 – x – 24) = 0\n\n⇒ 3x2 – x – 24 = 0\n\n⇒ 3x2 – 9x + 8x – 24 = 0\n\n⇒ 3x(x – 3) + 8(x – 3) = 0\n\n⇒ (3x + 8)(x – 3) = 0\n\n⇒ x = 3 or -8/3\n\nThus, the legs of the right angled triangle are 5x = 15 and (3x – 1) = 8 and hence its hypotenuse is √(82 + 152) = 17.\n\nS Chand ICSE Maths Solutions Class 10 Quadratic Equations Exercise 5E: Ques No 16\n\nThe hypotenuse of a right angle triangle is 13 cm and the difference between the other two sides is 7 cm.\n\n(i) Taking x as the length of the shorter of the two sides, write an equation in x that represents the above statement.\n\n(ii) Solve the equation obtained in (i) above and hence find the two unknowns sides of the triangle.\n\nS Chand ICSE Maths Solutions:\n\nLet the length of legs of right angled triangle are x and (x + 7). Then, we have\n\nx2 + (x + 7)2 = 132\n\n⇒ x2 + x2 + 14x + 49 = 169\n\n⇒ 2x2 + 14x – 120 = 0\n\n⇒ x2 + 7x – 60 = 0  [This is required quadratic equation.]\n\n⇒ x2 + 12x – 5x – 60 = 0\n\n⇒ x(x + 12) – 5(x + 12) = 0\n\n⇒ (x – 5)(x + 12) = 0\n\n⇒ x = 5 or -12\n\nThus, the two legs of the right angled triangle are x = 5 and (x + 7) = 12.\n\nS Chand ICSE Maths Solutions Class 10 Quadratic Equations Exercise 5E: Ques No 17\n\nThe length of a verandah is 3 m more than its breadth. The numerical value of its area is equal to the numerical value of its perimeter.\n\n(i) Taking x as the breadth of the verandah, write an equation in x that represents the above statement.\n\n(ii) Solve the equation in (i) above and hence find the dimension of the verandah.\n\nS Chand ICSE Maths Solutions:\n\nLet the dimension of the verandah are x and (x + 3). Then, we have\n\nx(x + 3) = 2(x + x + 3)\n\n⇒ x2 + 3x = 4x + 6\n\n⇒ x2 – x – 6 = 0  [This is required quadratic equation.]\n\n⇒ x2 – 3x + 2x – 6 = 0\n\n⇒ x(x – 3) + 2(x – 3) = 0\n\n⇒ (x + 2)(x – 3) = 0\n\n⇒ x = 3 or -2.\n\nThus, the dimension of the verandah are width as x = 3 and length as (x + 3) = 6.\n\nS Chand ICSE Maths Solutions Class 10 Quadratic Equations Exercise 5E: Ques No 18\n\nTwo squares have sides x cm and (x + 4) cm. The sum of their areas is 656 sq cm. Express this as an algebraic equation in x and solve the equation to find sides of the squares.\n\nS Chand ICSE Maths Solutions:\n\nTwo squares have sides x cm and (x + 4) cm. Then, we have\n\nx2 + (x + 4)2 = 656\n\n⇒ x2 + x2 + 8x + 16 = 656\n\n⇒ 2x2 + 8x – 640 = 0\n\n⇒ x2 + 4x – 320 = 0  [This is required quadratic equation.]\n\n⇒ x2 – 16x + 20x – 320 = 0\n\n⇒ x(x – 16) + 20(x – 16) = 0\n\n⇒ (x + 20)(x – 16) = 0\n\n⇒ x = -20 or 16\n\nSince x represents the length of the side of square, then x = 16.\n\nThus, the sides of the squares are 16 cm and 20 cm.\n\nS Chand ICSE Maths Solutions Class 10 Quadratic Equations Exercise 5E: Ques No 19\n\nThe perimeter of a rectangular plot is 180 m and its area is 1800 cm2. Take the length of plot as x m. Use the perimeter 180 m to write the value of the breadth in terms of x. Use the values of length, breadth and the area to write an equation in x. Solve the equation to calculate the length and breadth of the plot.\n\nS Chand ICSE Maths Solutions:\n\nGiven that the length of rectangular plot is x m. Then, we have\n\nNow, Area = 1800\n\nx(90 – x) = 1800\n\n90x – x2 = 1800\n\nx2 – 90x + 1800 = 0\n\nx2 – 60x – 30x + 1800 = 0\n\n⇒ x(x – 60) – 30(x – 60) = 0\n\n⇒ (x – 30)(x – 60) = 0\n\n⇒ x = 30 or 60.\n\nIf x = 30, then 90 – x = 60\n\nIf x = 60, then 90 – x = 30\n\nThus, length = 60 cm and width = 30 cm\n\nS Chand ICSE Maths Solutions Class 10 Quadratic Equations Exercise 5E: Ques No 20\n\nA rectangle has an area of 24 cm2. If its length is x cm, write down its breadth in terms of x. Given that its perimeter is 20 cm, form an equation in x and solve it.\n\nS Chand ICSE Maths Solutions:\n\nGiven that the length of rectangle is x m. Then, we have\n\nNow, Perimeter = 20\n\n2(x + 24/x) = 20\n\n(x + 24/x) = 10\n\nx2 + 24 = 10x\n\nx2 – 10x + 24 = 0\n\nx2 – 6x – 4x + 24 = 0\n\n⇒ x(x – 6) – 4(x – 6) = 0\n\n⇒ (x – 4)(x – 6) = 0\n\n⇒ x = 4 or 6\n\nSince x is length of the rectangle, then x = 6 and 24/x = 4.\n\nThus, length and breadth of the rectangle are 6 cm and 4 cm.\n\nS Chand ICSE Maths Solutions Class 10 Quadratic Equations Exercise 5E: Ques No 21\n\nA rectangular garden 10 m by 16 m is to be surrounded by a concrete path of uniform width. Given that the area of the path is 120 squares meters, assuming the width of the path to be x, form an equation in x and solve it to find the value of x.\n\nS Chand ICSE Maths Solutions:", null, "Given that the width of the wall to be x. Then, we have\n\n(2x + 16)(2x + 10) – 10 × 16 = 120\n\n⇒ 4x2 + 52x + 160 – 160 = 120\n\n⇒ 4x2 + 52x – 120 = 0\n\nx2 + 13x – 30 = 0\n\nx2 + 15x – 2x – 30 = 0\n\n⇒ x(x + 15) – 2(x + 15) = 0\n\n⇒ (x – 2)(x + 15) = 0\n\n⇒ x = 2 or -15\n\nThus, the width of the path is x = 2 cm.\n\nS Chand ICSE Maths Solutions Class 10 Quadratic Equations Exercise 5E: Ques No 22\n\nA man covers a distance of 200 km travelling with a uniform speed of x km per hour. The distance could have been covered in 2 hours less, had the speed been (x + 5)km/he. Calculate the value of x.\n\nS Chand ICSE Maths Solutions:\n\nAccording to question, we have\n\n200/x – 200/(x + 5) = 2\n\n⇒ 1/x – 1/(x + 5) = 1/100\n\n⇒ (x + 5 – x)/x(x + 5) = 1/100\n\n⇒ 5/x(x + 5) = 1/100\n\n⇒ x2 + 5x – 500 = 0\n\n⇒ x2 + 25x – 20x – 500 = 0\n\n⇒ x(x + 25) – 20(x + 25) = 0\n\n⇒ (x – 20)(x + 25) = 0\n\n⇒ x = 20 or -25.\n\nThus, required speed is x = 20 km/hr.\n\nS Chand ICSE Maths Solutions Class 10 Quadratic Equations Exercise 5E: Ques No 23\n\nAn express train makes a run of 240 km at a certain speed. Another train, whose speed is 12 km/hr less than the first takes an hour longer to make the same trip. Find the speed of the express train to km/hr.\n\nS Chand ICSE Maths Solutions:\n\nLet the speed of the express train is x km/hr, we have\n\n240/(x – 12) – 240/x = 1\n\n⇒ 1/(x – 12) – 1/x = 1/240\n\n⇒ (x – x + 12)/x(x – 12) = 1/240\n\n⇒ 12/x(x – 12) = 1/240\n\n⇒ x2 – 12x – 2880 = 0\n\n⇒ x2 – 60x + 48x – 2880 = 0\n\n⇒ x(x – 60) + 48(x – 60) = 0\n\n⇒ (x + 48)(x – 60) = 0\n\n⇒ x = -48 or 60\n\nThus, the speed of the express train is 60 km/hr.\n\nS Chand ICSE Maths Solutions Class 10 Quadratic Equations Exercise 5E: Ques No 24\n\nA train covers a distance of 90 km at a uniform speed. Had the speed been 15 km/hr more, it would have taken 30 minutes less for the journey. Find the original speed of the train.\n\nS Chand ICSE Maths Solutions:\n\nLet the original speed of the train is x km/hr, we have\n\n90/x – 90/(x + 15) = 1/2\n\n⇒ 1/x – 1/(x + 15) = 1/180\n\n⇒ (x + 15 – x)/x(x + 15) = 1/180\n\n⇒ 15/x(x + 15) = 1/180\n\n⇒ x2 + 15x – 2700 = 0\n\n⇒ x2 + 60x – 45x – 2700 = 0\n\n⇒ x(x + 60) – 45(x + 60) = 0\n\n⇒ (x – 45)(x + 60) = 0\n\n⇒ x = 45 or -60\n\nThus, the original speed of the train is x = 45 km/hr.\n\nS Chand ICSE Maths Solutions Class 10 Quadratic Equations Exercise 5E: Ques No 25\n\nA plane left 30 minutes later than the scheduled time and in order to reach its distance, 1500 km away it has to increase its speed by 250 km/hr from its usual speed. Find its usual speed.\n\nS Chand ICSE Maths Solutions:\n\nLet the usual speed of the plain is x km/hr, we have\n\n1500/x – 1500/(x + 250) = 1/2\n\n⇒ 1/x – 1/(x + 250) = 1/3000\n\n⇒ (x + 250 – x)/x(x + 250) = 1/3000\n\n⇒ 250/x(x + 250) = 1/3000\n\n⇒ x2 + 250x – 750000 = 0\n\n⇒ x2 + 1000x – 750x – 750000 = 0\n\n⇒ x(x + 1000) – 750(x + 1000) = 0\n\n⇒ (x – 750)(x + 1000) = 0\n\n⇒ x = 750 or -1000.\n\nThus, the usual speed of the plain is 750 km/hr.\n\nS Chand ICSE Maths Solutions Class 10 Quadratic Equations Exercise 5E: Ques No 26\n\nA boat takes 1 hour longer to go 36 km up a river than to return. If the river flows at 3 km/hr, find the rate at which the boat travels in still water.\n\nS Chand ICSE Maths Solutions:\n\nLet the speed of the boat in still water is x km/hr, we have\n\n36/(x – 3) – 36/(x + 3) = 1\n\n⇒ 1/(x – 3) – 1/(x + 3) = 1/36\n\n⇒ (x + 3 – x + 3)/(x + 3)(x – 3) = 1/36\n\n⇒ 6/(x + 3)(x – 3) = 1/36\n\n⇒ 1/(x2 – 9) = 1/216\n\n⇒ x2 = 225\n\n⇒ x = 15 or -15.\n\nThus, the speed of the boat in still water is x = 15 km/hr.\n\nS Chand ICSE Maths Solutions Class 10 Quadratic Equations Exercise 5E: Ques No 27\n\nA man purchased some horses for Rs. 3000. Three of them died, and he sold the rest at Rs. 65 more than what he paid for each horse and thus gained 6% more his outlay. How many horses did he buy?\n\nS Chand ICSE Maths Solutions:\n\nLet the number of horses purchased is x. Then, the price of each horse is Rs. 3000/x.\n\nNow, CP = 3000 and SP = 3000(1 + 6/100) = 3180.\n\nAccording to question, we have\n\n3180/(x – 3) = 3000/x + 65\n\n⇒ 636/(x – 3) – 600/x = 13\n\n⇒ 636x – 600x + 1800 = 13x(x – 3)\n\n⇒ 36x + 1800 = 13x2 – 39x\n\n⇒ 13x2 – 75x – 1800 = 0\n\n⇒ 13x2 – 195x + 120x – 1800 = 0\n\n⇒ 13x(x – 15) + 120(x – 15) = 0\n\n⇒ (13x + 120)(x – 15) = 0\n\n⇒ x = 15 or -120/13.\n\nThus, the number of horses purchased is x = 15.\n\nS Chand ICSE Maths Solutions Class 10 Quadratic Equations Exercise 5E: Ques No 28\n\nA trader bought a number of articles for Rs. 1200. Ten were damaged and he sold each of the rest at Rs. 2 more than what he paid for it, thus getting a profit of Rs. 60 on the whole transaction. Taking the number of article he bought as x, form an equation in x and solve.\n\nS Chand ICSE Maths Solutions:\n\nLet the number of article purchased is x. Then, the price of each article is Rs. 1200/x.\n\nNow, CP = 1200 and SP = 1200 + 60 = 1260.\n\nAccording to question, we have\n\n1260/(x – 10) = 1200/x + 2\n\n⇒ 625/(x – 10) – 600/x = 1\n\n⇒ 625/(x – 10) – 600/x = 1\n\n⇒ 625x – 600x + 6000 = x(x – 10)\n\n⇒ x2 – 40x – 6000 = 0\n\n⇒ x2 – 100x + 60x – 6000 = 0\n\n⇒ x(x – 100) + 60(x – 100) = 0\n\n⇒ (x + 60)(x – 100) = 0\n\n⇒ x = -60 or 100\n\nThus, the number of article purchased is x = 100.\n\nerror: Content is protected !!" ]
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https://camdenk.github.io/mlbplotR/reference/geom_mlb_logos.html
[ "geom_mlb_logos() and geom_mlb_scoreboard_logos() are used to plot MLB team and league logos instead of points in a ggplot. It requires x, y aesthetics as well as a valid MLB team abbreviation. The latter can be checked with valid_team_names() but is also cleaned before being plotted.\n\n## Usage\n\ngeom_mlb_logos(\nmapping = NULL,\ndata = NULL,\nstat = \"identity\",\nposition = \"identity\",\n...,\nnudge_x = 0,\nnudge_y = 0,\nna.rm = FALSE,\nshow.legend = FALSE,\ninherit.aes = TRUE\n)\n\ngeom_mlb_scoreboard_logos(\nmapping = NULL,\ndata = NULL,\nstat = \"identity\",\nposition = \"identity\",\n...,\nnudge_x = 0,\nnudge_y = 0,\nna.rm = FALSE,\nshow.legend = FALSE,\ninherit.aes = TRUE\n)\n\n## Arguments\n\nmapping\n\nSet of aesthetic mappings created by aes(). If specified and inherit.aes = TRUE (the default), it is combined with the default mapping at the top level of the plot. You must supply mapping if there is no plot mapping.\n\ndata\n\nThe data to be displayed in this layer. There are three options:\n\nIf NULL, the default, the data is inherited from the plot data as specified in the call to ggplot().\n\nA data.frame, or other object, will override the plot data. All objects will be fortified to produce a data frame. See fortify() for which variables will be created.\n\nA function will be called with a single argument, the plot data. The return value must be a data.frame, and will be used as the layer data. A function can be created from a formula (e.g. ~ head(.x, 10)).\n\nstat\n\nThe statistical transformation to use on the data for this layer, either as a ggproto Geom subclass or as a string naming the stat stripped of the stat_ prefix (e.g. \"count\" rather than \"stat_count\")\n\nposition\n\nPosition adjustment, either as a string naming the adjustment (e.g. \"jitter\" to use position_jitter), or the result of a call to a position adjustment function. Use the latter if you need to change the settings of the adjustment.\n\n...\n\nOther arguments passed on to ggplot2::layer(). These are often aesthetics, used to set an aesthetic to a fixed value. See the below section \"Aesthetics\" for a full list of possible arguments.\n\nnudge_x, nudge_y\n\nHorizontal and vertical adjustment to nudge labels by. Useful for offsetting text from points, particularly on discrete scales. Cannot be jointly specified with position.\n\nna.rm\n\nIf FALSE, the default, missing values are removed with a warning. If TRUE, missing values are silently removed.\n\nshow.legend\n\nlogical. Should this layer be included in the legends? NA, the default, includes if any aesthetics are mapped. FALSE never includes, and TRUE always includes. It can also be a named logical vector to finely select the aesthetics to display.\n\ninherit.aes\n\nIf FALSE, overrides the default aesthetics, rather than combining with them. This is most useful for helper functions that define both data and aesthetics and shouldn't inherit behaviour from the default plot specification, e.g. borders().\n\n## Value\n\nA ggplot2 layer (ggplot2::layer()) that can be added to a plot created with ggplot2::ggplot().\n\n## Aesthetics\n\ngeom_mlb_logos() and geom_mlb_scoreboard_logos() understand the following aesthetics (required aesthetics are in bold):\n\n• x - The x-coordinate.\n\n• y - The y-coordinate.\n\n• team_abbr - The team abbreviation. Need to use Savant's abbreviation.\n\n• alpha = NULL - The alpha channel, i.e. transparency level, as a numerical value between 0 and 1.\n\n• colour = NULL - The image will be colourized with this colour. Use the special character \"b/w\" to set it to black and white. For more information on valid colour names in ggplot2 see https://ggplot2.tidyverse.org/articles/ggplot2-specs.html?q=colour#colour-and-fill\n\n• angle = 0 - The angle of the image as a numerical value between 0° and 360°.\n\n• hjust = 0.5 - The horizontal adjustment relative to the given x coordinate. Must be a numerical value between 0 and 1.\n\n• vjust = 0.5 - The vertical adjustment relative to the given y coordinate. Must be a numerical value between 0 and 1.\n\n• width = 1.0 - The desired width of the image in npc (Normalised Parent Coordinates). The default value is set to 1.0 which is big but it is necessary because all used values are computed relative to the default. A typical size is width = 0.075 (see below examples).\n\n• height = 1.0 - The desired height of the image in npc (Normalised Parent Coordinates). The default value is set to 1.0 which is big but it is necessary because all used values are computed relative to the default. A typical size is height = 0.1 (see below examples).\n\n## Examples\n\n# \\donttest{\nlibrary(mlbplotR)\nlibrary(ggplot2)\n\nteam_abbr <- valid_team_names()\n# remove conference logos from this example\nteam_abbr <- team_abbr[!team_abbr %in% c(\"NL\", \"AL\", \"MLB\")]\n\ndf <- data.frame(\na = rep(1:6, 5),\nb = sort(rep(1:5, 6), decreasing = TRUE),\nteams = team_abbr\n)\n\n# keep alpha == 1 for all teams including an \"A\"\nmatches <- grepl(\"A\", team_abbr)\ndf$alpha <- ifelse(matches, 1, 0.2) # also set a custom fill colour for the non \"A\" teams df$colour <- ifelse(matches, NA, \"gray\")\n\n# scatterplot of all logos\nggplot(df, aes(x = a, y = b)) +\ngeom_mlb_logos(aes(team_abbr = teams), width = 0.075) +\ngeom_label(aes(label = teams), nudge_y = -0.35, alpha = 0.5) +\ntheme_void()", null, "# apply alpha via an aesthetic from inside the dataset df\n# please note that you have to add scale_alpha_identity() to use the alpha\nggplot(df, aes(x = a, y = b)) +\ngeom_mlb_scoreboard_logos(aes(team_abbr = teams, alpha = alpha), width = 0.075) +\ngeom_label(aes(label = teams), nudge_y = -0.35, alpha = 0.5) +\nscale_alpha_identity() +\ntheme_void()", null, "# apply alpha and colour via an aesthetic from inside the dataset df\n# please note that you have to add scale_alpha_identity() as well as\n# scale_colour_identity() to use the alpha and colour values in your dataset!\nggplot(df, aes(x = a, y = b)) +\ngeom_mlb_logos(aes(team_abbr = teams, alpha = alpha, colour = colour), width = 0.075) +\ngeom_label(aes(label = teams), nudge_y = -0.35, alpha = 0.5) +\nscale_alpha_identity() +\nscale_colour_identity() +\ntheme_void()", null, "# apply alpha as constant for all logos\nggplot(df, aes(x = a, y = b)) +\ngeom_mlb_scoreboard_logos(aes(team_abbr = teams), width = 0.075, alpha = 0.6) +\ngeom_label(aes(label = teams), nudge_y = -0.35, alpha = 0.5) +\ntheme_void()", null, "# it's also possible to plot league logos\nleague <- data.frame(a = 1:3, b = 0, teams = c(\"AL\", \"NL\", \"MLB\"))\nggplot(league, aes(x = a, y = b)) +\ngeom_mlb_logos(aes(team_abbr = teams), width = 0.3) +\ngeom_label(aes(label = teams), nudge_y = -0.4, alpha = 0.5) +\ncoord_cartesian(xlim = c(0.5,3.5), ylim = c(-0.75,.75)) +\ntheme_void()", null, "# }" ]
[ null, "https://camdenk.github.io/mlbplotR/reference/geom_mlb_logos-1.png", null, "https://camdenk.github.io/mlbplotR/reference/geom_mlb_logos-2.png", null, "https://camdenk.github.io/mlbplotR/reference/geom_mlb_logos-3.png", null, "https://camdenk.github.io/mlbplotR/reference/geom_mlb_logos-4.png", null, "https://camdenk.github.io/mlbplotR/reference/geom_mlb_logos-5.png", null ]
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https://www.tensorflow.org/versions/r2.0/api_docs/python/tf/signal/linear_to_mel_weight_matrix
[ "Watch keynotes, product sessions, workshops, and more from Google I/O\n\n# tf.signal.linear_to_mel_weight_matrix\n\nReturns a matrix to warp linear scale spectrograms to the mel scale.\n\nReturns a weight matrix that can be used to re-weight a `Tensor` containing `num_spectrogram_bins` linearly sampled frequency information from `[0, sample_rate / 2]` into `num_mel_bins` frequency information from `[lower_edge_hertz, upper_edge_hertz]` on the mel scale.\n\nFor example, the returned matrix `A` can be used to right-multiply a spectrogram `S` of shape `[frames, num_spectrogram_bins]` of linear scale spectrum values (e.g. STFT magnitudes) to generate a \"mel spectrogram\" `M` of shape `[frames, num_mel_bins]`.\n\n``````# `S` has shape [frames, num_spectrogram_bins]\n# `M` has shape [frames, num_mel_bins]\nM = tf.matmul(S, A)\n``````\n\nThe matrix can be used with `tf.tensordot` to convert an arbitrary rank `Tensor` of linear-scale spectral bins into the mel scale.\n\n``````# S has shape [..., num_spectrogram_bins].\n# M has shape [..., num_mel_bins].\nM = tf.tensordot(S, A, 1)\n# tf.tensordot does not support shape inference for this case yet.\nM.set_shape(S.shape[:-1].concatenate(A.shape[-1:]))\n``````\n\n`num_mel_bins` Python int. How many bands in the resulting mel spectrum.\n`num_spectrogram_bins` An integer `Tensor`. How many bins there are in the source spectrogram data, which is understood to be `fft_size // 2 + 1`, i.e. the spectrogram only contains the nonredundant FFT bins.\n`sample_rate` Python float. Samples per second of the input signal used to create the spectrogram. We need this to figure out the actual frequencies for each spectrogram bin, which dictates how they are mapped into the mel scale.\n`lower_edge_hertz` Python float. Lower bound on the frequencies to be included in the mel spectrum. This corresponds to the lower edge of the lowest triangular band.\n`upper_edge_hertz` Python float. The desired top edge of the highest frequency band.\n`dtype` The `DType` of the result matrix. Must be a floating point type.\n`name` An optional name for the operation.\n\nA `Tensor` of shape `[num_spectrogram_bins, num_mel_bins]`.\n\n`ValueError` If `num_mel_bins`/`num_spectrogram_bins`/`sample_rate` are not positive, `lower_edge_hertz` is negative, frequency edges are incorrectly ordered, `upper_edge_hertz` is larger than the Nyquist frequency, or `sample_rate` is neither a Python float nor a constant Tensor.\n\n[{ \"type\": \"thumb-down\", \"id\": \"missingTheInformationINeed\", \"label\":\"Missing the information I need\" },{ \"type\": \"thumb-down\", \"id\": \"tooComplicatedTooManySteps\", \"label\":\"Too complicated / too many steps\" },{ \"type\": \"thumb-down\", \"id\": \"outOfDate\", \"label\":\"Out of date\" },{ \"type\": \"thumb-down\", \"id\": \"samplesCodeIssue\", \"label\":\"Samples / code issue\" },{ \"type\": \"thumb-down\", \"id\": \"otherDown\", \"label\":\"Other\" }]\n[{ \"type\": \"thumb-up\", \"id\": \"easyToUnderstand\", \"label\":\"Easy to understand\" },{ \"type\": \"thumb-up\", \"id\": \"solvedMyProblem\", \"label\":\"Solved my problem\" },{ \"type\": \"thumb-up\", \"id\": \"otherUp\", \"label\":\"Other\" }]" ]
[ null ]
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https://chemistrygod.com/hund-rule
[ "Search the World of Chemistry\n\n×\n\n# Hund's Rule of Maximum Multiplicity\n\n28th Feb 2020 @ 6 min read\n\nPhysical Chemistry\n\n## Statement\n\nThe Hund rule of maximum multiplicity states:\n\n1. When two or more orbitals of equal energy (or very close energy) are available, electrons will fill the orbitals singly before filling doubly.\n2. All the electrons in the orbitals will have the same spin to maximize the multiplicity.\n\nIn simple words, the rule says the lowest-energy electronic configuration is attained with the maximum number of parallel electron spins.\n\nThe rule was formulated by Friedrich Hund, a German physicist, in 1925. Hund's contributions to quantum mechanics are significant, particularly in the electronic structure of atoms. He is also known for quantum tunneling.\n\n## Explanation\n\nAlong with the aufbau principle and Pauli exclusion principle, the Hund is very helpful in understanding the electronic configuration of an atom. The aufbau principle is used to predict the electronic configuration when the energy difference between orbitals is considerably large, and the Pauli exclusion principle restricts the maximum number of electrons in an orbital to two. The Hund rule useful to predict the ground state of atoms or molecules where the equal energy orbitals are available. This is especially seen in the orbitals of the same subshell which are equal in energy. For example, in the p subshell, all its orbitals (px, py, and pz) have the same energy. Such equal energy orbitals are called degenerate orbitals.\n\nAs the rule says electrons occupy the same energy orbital singly before pairing. It means the pairing of electrons does not occur until each equal energy orbital has the occupation of one electron. Also, all of these unpaired electrons must have the same spin, i.e., either spin up (↑) or spin down (↓).\n\n### Filling of p subshell\n\nLet's consider the filling of 2p orbitals. There are three orbitals in every p subshell, which are equal in energy. The first electron enters either of three orbitals since they are degenerate. Even though the first-occupied orbital is not completely filled and it can take one more electron, the second electron will not occupy it. Instead, it will enter another orbital with the same spin as the first electron. Similarly, the third will occupy the remaining orbital. Thus, the first three electrons occupy all three orbitals with either spin up (shown in the diagram below) or spin down.\n\nAfter singly filling, the following three electrons will fill the remaining vacancies, which results in pairing.\n\n### Filling of d subshell\n\nThe same is true for the d subshell. There are five d orbitals; each has the same energy. So, the first five electrons fill each orbital with the same spin. And the next five will form pairs.\n\nThe Hund rule is not only seen for the orbitals of the same subshell but also for the orbitals of different subshells with a small difference in energy. Chromium is one such example; it is discussed later in the article.\n\n## What is multiplicity?\n\nIn quantum chemistry, the multiplicity (or spin multiplicity) is defined as the total number of spin orientations and is given by 2S + 1. Here, S is the total spin quantum number, and its value is the sum of all unpaired half spins. According to the Hund rule, the lowest energy configuration is attained when the multiplicity, i.e., 2S + 1, is maximum.\n\nThe maximum value of S is obtained only when all the spins are either up or down.\n\nConsider an example of 2p orbitals with three electrons. The possible number of arrangements are shown below.\n\nThe maximum value of S is obtained in the first and fourth case, and it is calculated as:", null, "From the total spin quantum number, we can find the multiplicity.", null, "## Examples\n\n### Carbon\n\nCarbon has six electrons. Its electronic configuration is 1s2 2s2 2p2. The last two electrons are in 2p subshell, and both of them occupy the different orbitals with the same spin.\n\nThe total spin quantum number (S) of carbon is", null, ". And the multiplicity is 2S + 1 = 3.\n\n### Nitrogen\n\nAdding one more electron to carbon, we get the electronic configuration of nitrogen: 1s2 2s2 2p3. In nitrogen, all 2p orbitals are half-filled.\n\nS is equal to", null, ". And the multiplicity is 2S + 1 = 4.\n\n### Oxygen\n\nOxygen follows nitrogen and has an extra electron in its electronic configuration: 1s2 2s2 2p4. The fourth electron in 2p subshell forms a pair.\n\nS = 1 and the multiplicity is 2S + 1 = 3\n\n### Chromium\n\nChromium, a d block element, has the atomic number of 24. Its electronic configuration is [Ar] 3d54s1. The last two orbitals are 3d and 4s. The difference between the energies of these two orbitals is very small. As we can see from the diagram below, both orbitals are half-filled and all electrons have the same spin as per the rule.\n\nThere are six unpaired electrons in chromium. So,", null, "and the multiplicity is 2S + 1 = 7.\n\n### Oxygen molecule\n\nThe Hund rule is also used in molecular orbitals. The figure below is the molecular orbital diagram of dioxygen.\n\nThe filling of electrons in the π antibonding orbitals is achieved as per the Hund rule. Both molecular orbitals (π*\nx\nand π*\ny\n) are equal in energy and accept one electron each.\n\n## Justification\n\nThere are several justifications proposed for the explanation of the Hund rule. One of them is the electron-electron repulsion. The stability of the electronic system increases by minimizing the repulsion among electrons. This can be achieved by maximizing the spatial space. In a singly filled orbital, electrons are far apart from one another. This minimizes the repulsion and increases the stability.\n\nThe second justification is the shielding effect. In an atom, the columbic attraction between the nucleus and outer electrons is shielded by the inner electrons. Consequently, the outer electrons experience a lesser nuclear charge than the inner electrons. It causes the expansion of outer orbitals and increases the energy of the system. The energy of the system is lowered by decreasing the shielding effect, which is possible by the symmetrical distribution of electrons. Thus, the singly filled orbital has relatively small shielding and the stability is further increases.\n\nThe third factor that affects the energy of the system is the exchange energy. Electrons of the same spin residing in degenerate orbitals exchanges their positions. During these exchanges, the energy is released called the exchange energy. The more the exchanges, the more the stability. When degenerate orbitals are filled with unpaired electrons of the same spin, the number of exchanges is the highest, and the system reaches stability.\n\n## Associated articles\n\nIf you appreciate our work, consider supporting us on ❤️ patreon.\n\nCopy Article Cite\n\nWrite a response", null, "Joseph\n14th Oct 2020\nI'm truly amazed by how this was explained I don't fully understand everything because it's not all my level yet... But it's a great start", null, "" ]
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https://percent-of.com/calculate/what-is-36-of-1542/
[ "# 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\n36% of 1542 is:\n555.12\n\n## Percent of - Table For 1542\n\nPercent of Difference\n1% of 1542 is 15.42 1526.58\n2% of 1542 is 30.84 1511.16\n3% of 1542 is 46.26 1495.74\n4% of 1542 is 61.68 1480.32\n5% of 1542 is 77.1 1464.9\n6% of 1542 is 92.52 1449.48\n7% of 1542 is 107.94 1434.06\n8% of 1542 is 123.36 1418.64\n9% of 1542 is 138.78 1403.22\n10% of 1542 is 154.2 1387.8\n11% of 1542 is 169.62 1372.38\n12% of 1542 is 185.04 1356.96\n13% of 1542 is 200.46 1341.54\n14% of 1542 is 215.88 1326.12\n15% of 1542 is 231.3 1310.7\n16% of 1542 is 246.72 1295.28\n17% of 1542 is 262.14 1279.86\n18% of 1542 is 277.56 1264.44\n19% of 1542 is 292.98 1249.02\n20% of 1542 is 308.4 1233.6\n21% of 1542 is 323.82 1218.18\n22% of 1542 is 339.24 1202.76\n23% of 1542 is 354.66 1187.34\n24% of 1542 is 370.08 1171.92\n25% of 1542 is 385.5 1156.5\n26% of 1542 is 400.92 1141.08\n27% of 1542 is 416.34 1125.66\n28% of 1542 is 431.76 1110.24\n29% of 1542 is 447.18 1094.82\n30% of 1542 is 462.6 1079.4\n31% of 1542 is 478.02 1063.98\n32% of 1542 is 493.44 1048.56\n33% of 1542 is 508.86 1033.14\n34% of 1542 is 524.28 1017.72\n35% of 1542 is 539.7 1002.3\n36% of 1542 is 555.12 986.88\n37% of 1542 is 570.54 971.46\n38% of 1542 is 585.96 956.04\n39% of 1542 is 601.38 940.62\n40% of 1542 is 616.8 925.2\n41% of 1542 is 632.22 909.78\n42% of 1542 is 647.64 894.36\n43% of 1542 is 663.06 878.94\n44% of 1542 is 678.48 863.52\n45% of 1542 is 693.9 848.1\n46% of 1542 is 709.32 832.68\n47% of 1542 is 724.74 817.26\n48% of 1542 is 740.16 801.84\n49% of 1542 is 755.58 786.42\n50% of 1542 is 771 771\n51% of 1542 is 786.42 755.58\n52% of 1542 is 801.84 740.16\n53% of 1542 is 817.26 724.74\n54% of 1542 is 832.68 709.32\n55% of 1542 is 848.1 693.9\n56% of 1542 is 863.52 678.48\n57% of 1542 is 878.94 663.06\n58% of 1542 is 894.36 647.64\n59% of 1542 is 909.78 632.22\n60% of 1542 is 925.2 616.8\n61% of 1542 is 940.62 601.38\n62% of 1542 is 956.04 585.96\n63% of 1542 is 971.46 570.54\n64% of 1542 is 986.88 555.12\n65% of 1542 is 1002.3 539.7\n66% of 1542 is 1017.72 524.28\n67% of 1542 is 1033.14 508.86\n68% of 1542 is 1048.56 493.44\n69% of 1542 is 1063.98 478.02\n70% of 1542 is 1079.4 462.6\n71% of 1542 is 1094.82 447.18\n72% of 1542 is 1110.24 431.76\n73% of 1542 is 1125.66 416.34\n74% of 1542 is 1141.08 400.92\n75% of 1542 is 1156.5 385.5\n76% of 1542 is 1171.92 370.08\n77% of 1542 is 1187.34 354.66\n78% of 1542 is 1202.76 339.24\n79% of 1542 is 1218.18 323.82\n80% of 1542 is 1233.6 308.4\n81% of 1542 is 1249.02 292.98\n82% of 1542 is 1264.44 277.56\n83% of 1542 is 1279.86 262.14\n84% of 1542 is 1295.28 246.72\n85% of 1542 is 1310.7 231.3\n86% of 1542 is 1326.12 215.88\n87% of 1542 is 1341.54 200.46\n88% of 1542 is 1356.96 185.04\n89% of 1542 is 1372.38 169.62\n90% of 1542 is 1387.8 154.2\n91% of 1542 is 1403.22 138.78\n92% of 1542 is 1418.64 123.36\n93% of 1542 is 1434.06 107.94\n94% of 1542 is 1449.48 92.52\n95% of 1542 is 1464.9 77.1\n96% of 1542 is 1480.32 61.68\n97% of 1542 is 1495.74 46.26\n98% of 1542 is 1511.16 30.84\n99% of 1542 is 1526.58 15.42\n100% of 1542 is 1542 0\n\n### Here's How to Calculate 36% of 1542\n\nLet's take a quick example here:\n\nYou have a Target coupon of \\$1542 and you need to know how much will you save on your purchase if the discount is 36 percent.\n\nSolution:\n\nAmount Saved = Original Price x Discount in Percent / 100\n\nAmount Saved = (1542 x 36) / 100\n\nAmount Saved = 55512 / 100\n\nIn other words, a 36% discount for a purchase with an original price of \\$1542 equals \\$555.12 (Amount Saved), so you'll end up paying 986.88.\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 %" ]
[ null ]
{"ft_lang_label":"__label__en","ft_lang_prob":0.91458464,"math_prob":0.9864803,"size":6898,"snap":"2021-04-2021-17","text_gpt3_token_len":2618,"char_repetition_ratio":0.22497824,"word_repetition_ratio":0.039412674,"special_character_ratio":0.55552334,"punctuation_ratio":0.16309255,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9998326,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2021-01-21T12:21:16Z\",\"WARC-Record-ID\":\"<urn:uuid:91ab27ce-65e8-4aa5-8afc-ccf21c67a2c5>\",\"Content-Length\":\"47886\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:272ffc00-e995-4b2f-a594-c5aa20d345b5>\",\"WARC-Concurrent-To\":\"<urn:uuid:8af7a185-6f72-4e16-b721-9089e829998e>\",\"WARC-IP-Address\":\"209.42.195.149\",\"WARC-Target-URI\":\"https://percent-of.com/calculate/what-is-36-of-1542/\",\"WARC-Payload-Digest\":\"sha1:G5UH4MOAZXE7AOEA4QIGWXYGMHCYUAIU\",\"WARC-Block-Digest\":\"sha1:7XGBNFMSIH46XO3O5RK2VLYR35EWWHKT\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2021/CC-MAIN-2021-04/CC-MAIN-2021-04_segments_1610703524743.61_warc_CC-MAIN-20210121101406-20210121131406-00273.warc.gz\"}"}
http://eqworld.ipmnet.ru/eqarchive/view.php?id=51
[ "", null, "EqWorld The World of Mathematical Equations", null, "", null, "EqArchive: Add Equation/Solution > View Equation English only\n\n## View Equation\n\nThe database contains 327 equations (14 equations are awaiting activation).\n\nEquation data\nCategory:2. First-Order Partial Differential Equations\nSubcategory:2.3. Nonlinear Equations\nEquation(s):[can not create temporary dvi file]\nSolution(s),\nTransformation(s),\nIntegral(s)\n:\n[can not create temporary dvi file]\nRemarks:[can not create temporary dvi file]\nNovelty:Material has been fully published elsewhere\nReferences:Akulenko, L.D. (1987) Asymptotic Methods of Optimal Cotrol. Nauka, Moscow.\nAuthor/Contributor's Details\nLast name:Zhurov\nFirst name:Alexei\nCountry:Russia\nStatistic information\nSubmission date:Sun 17 Dec 2006 06:13\nEdits by author:0\n\nEdit (Only for author/contributor)\n\nThe EqWorld website presents extensive information on solutions to various classes of ordinary differential equations, partial differential equations, integral equations, functional equations, and other mathematical equations.\n\nCopyright © 2006-2011 Andrei D. Polyanin, Alexei I. Zhurov and Alexander L. Levitin" ]
[ null, "http://eqworld.ipmnet.ru/images/eqworld-logo-small.gif", null, "http://eqworld.ipmnet.ru/images/ipmlogo24b.gif", null, "http://counter.rambler.ru/top100.cnt", null ]
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https://stackoom.com/question/1zAkZ
[ "# 如果没有其他的话,Ocaml会嵌套Ocaml nested if without else\n\n``````let rec move_helper b sz r = match b with\n[] -> r\n|(h :: t) ->\nif h = 0 then\nif h - 1 = sz then h - 1 ::r\nif h + 1 = sz then h + 1 ::r\nelse move_helper t sz r\n;;\n\nlet move_pos b =\nmove_helper b 3 r\n;;\n\nlet g = move_pos [0;8;7;6;5;4;3;2;1]\n``````\n\n## 2 个回复2\n\n### #1楼 票数:4 已采纳\n\n``````let f x =\nif x land 1 <> 0 then print_string \"1\";\nif x land 2 <> 0 then print_string \"2\";\nif x land 4 <> 0 then print_string \"4\"\n``````\n\n### #2楼 票数:1\n\n``````(if test then f else g) 1\n``````\n\n``````let rec move_helper b sz r = match b with\n| [] -> r\n| h :: t ->\nif h = 0 then\nif h - 1 = sz then (h - 1) :: r\nelse if h + 1 = sz then (h + 1) :: r\nelse (* What do you want to return here? *)\nelse move_helper t sz r\n``````", null, "3回复\n\n2回复\n\n1回复\n\n1回复\n\n1回复\n\n1回复\n\n1回复\n\n1回复" ]
[ null, "https://stackoom.com/img/dash.png", null ]
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https://www.onlinemathlearning.com/statistics-lecture-2.html
[ "# Statistics Lectures: Variables\n\nA series of free Statistics Lectures with lessons, examples & solutions in videos.\n\nThis is the second page of the series of free video lessons, “Statistics Lectures”. These lectures introduce the concepts of variables, independent and dependent variables and discuss measurement scales.\n\nDescriptive statistics summarizes a sample, giving us some ideas about the mean and spread of the data, etc. Inferential statistics use a sample or samples to describe what the population is like; in other words, infering the characteristics of the population from the sample/s.\n\n### Statistics - Lecture 3: Types Of Variables\n\nA variable is a property that can take on many values.\nTwo kinds of variable:\n\n• Quantitative Variable\n• Qualitative/Categorical Variables.\n\nQuantitative variables are measured numerically. With measurements of quantitative variables you can do things like add, subtract, multiply and divide, and get a meaningful result.\nThere are two kinds of quantitative variables:\n\n• Discrete variables\n• Continuous Variables.\n\nA Discrete Variable is a quantitative variable with a finite number of values.\n\nA Continuous Variable is a quantitative variable with an infinite number of values.\n\nQualitative/Categorical variables allow for classification based on some characteristic.\n\n### Statistics - Lecture 4: Independent And Dependent Variables\n\nAn independent variable is any variable that is being manipulated.\nA dependent variable is any variable that is being measured.\n\n### Statistics - Lecture 5: Variable Measurement Scales\n\nThere are four data types of measured variables:\n\n• Nominal\n• Ordinal\n• Interval\n• Ratio\n\nNominal data (also known as qualitative/categorical data) is data that is split into categories.\nOrdinal data is data where order matters, but distance between values does not.\nInterval data is data where order matters, and distances between values are equal and meaningful, and a natural zero is not present. Ratio data is data where order matters, distances between values are equal and meaningful, and a natural zero is present.", null, "" ]
[ null, "https://www.onlinemathlearning.com/objects/default_image.gif", null ]
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https://www.gradesaver.com/textbooks/math/algebra/elementary-and-intermediate-algebra-concepts-and-applications-6th-edition/chapter-12-exponential-functions-and-logarithmic-functions-12-3-logarithmic-functions-12-3-exercise-set-page-803/73
[ "## Elementary and Intermediate Algebra: Concepts & Applications (6th Edition)\n\n$\\log_{z}6=m$\nSince $b^y=x$ is equivalent to $y=\\log_bx,$ the given equation, $z^m=6 ,$ is equivalent to \\begin{array}{l}\\require{cancel} \\log_{z}6=m .\\end{array}" ]
[ null ]
{"ft_lang_label":"__label__en","ft_lang_prob":0.81853193,"math_prob":0.99996364,"size":435,"snap":"2019-26-2019-30","text_gpt3_token_len":122,"char_repetition_ratio":0.09976798,"word_repetition_ratio":0.0,"special_character_ratio":0.26436782,"punctuation_ratio":0.08988764,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9999523,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2019-07-17T22:46:03Z\",\"WARC-Record-ID\":\"<urn:uuid:7badf8ee-0302-426d-a894-d468f0427a40>\",\"Content-Length\":\"129103\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:522166c5-4a87-49cf-ac63-8e6caf7c9001>\",\"WARC-Concurrent-To\":\"<urn:uuid:65b466c0-4c02-426b-ab4e-732e4400502b>\",\"WARC-IP-Address\":\"54.210.251.76\",\"WARC-Target-URI\":\"https://www.gradesaver.com/textbooks/math/algebra/elementary-and-intermediate-algebra-concepts-and-applications-6th-edition/chapter-12-exponential-functions-and-logarithmic-functions-12-3-logarithmic-functions-12-3-exercise-set-page-803/73\",\"WARC-Payload-Digest\":\"sha1:2GSOS45W2W6ZVQVIT2RHNI253WAJ4SQ2\",\"WARC-Block-Digest\":\"sha1:2H4P6H4WUXJRDCQLICLIMCRICOKYCVYH\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2019/CC-MAIN-2019-30/CC-MAIN-2019-30_segments_1563195525414.52_warc_CC-MAIN-20190717221901-20190718003901-00157.warc.gz\"}"}
https://au.mathworks.com/help/simbio/ref/simdata.getdata.html
[ "# getdata\n\nGet simulation data from `SimData` object\n\n## Syntax\n\n``[t,x,names] = getdata(simdata)``\n``sdOut = getdata(simdata)``\n``___ = getdata(simdata,format)``\n\n## Description\n\nexample\n\n````[t,x,names] = getdata(simdata)` returns the simulation time points `t`, the simulation data `x`, and corresponding `names` for the data columns.```\n````sdOut = getdata(simdata)` returns the simulation results as a `SimData` object `sdOut`.```\n\nexample\n\n````___ = getdata(simdata,format)` returns the simulation data in the specified `format`.```\n\n## Examples\n\ncollapse all\n\n`sbioloadproject('gprotein.sbproj');`\n\nSimulate the model.\n\n```sdObj = sbiosimulate(m1); sbioplot(sdObj);```", null, "The plot shows all the states together. Plot each state separately on its own axes in a subplot.\n\nFirst, extract the simulation data from the `SimData` object.\n\n`[time,data,names] = getdata(sdObj);`\n\nCalculate the number of rows and columns needed for the subplot.\n\n```sqrtnames = sqrt(numel(names)); nrows = round(sqrtnames); ncolumns = ceil(sqrtnames);```\n\nCreate a subplot and plot each state on its own axes.\n\n```figure for(i = 1:numel(names)) subplot(nrows,ncolumns,i) plot(time,data(:,i)); title(names(i)); end```", null, "## Input Arguments\n\ncollapse all\n\nSimulation data, specified as a `SimData` object or array of `SimData` objects.\n\nSimulation data format, specified as a character vector or string. Some formats require you to specify only one output argument. The valid formats follow.\n\n• `'num'` — This format returns simulation time points and simulation data in numeric arrays and the names of quantities and sensitivities as a cell array. This format is the default when you run `getdata` with multiple output arguments.\n\n• `'nummetadata'` — This format returns a cell array of metadata structures instead of the names of quantities and sensitivities as the third output argument.\n\n• `'numqualnames'` — This format returns qualified names in the third output argument to resolve ambiguities.\n\nYou must specify only one output argument for the following formats.\n\n• `'simdata'` — This format returns data in a new `SimData` object or an array of `SimData` objects. This format is the default when you specify a single output argument.\n\n• `'struct'` — This format returns a structure or structure array that contains both data and metadata.\n\n• `'ts'` — This format returns data as a cell array.\n\n• If `simdata` is scalar, the cell array is an m-by-1 array, where each element is a `timeseries` object. m is the number of quantities and sensitivities logged during the simulation.\n\n• If `simdata` is not scalar, the cell array is k-by-1, where each element of the cell array is an m-by-1 cell array of `timeseries` objects. k is the size of `simdata`, and m is the number of quantities or sensitivities in each `SimData` object in `simdata`. In other words, the function returns an individual time series for each state or column and for each `SimData` object in `simdata`.\n\n• `'tslumped'` — This format returns the data as a cell array of `timeseries` objects, combining data from each `SimData` object into a single time series.\n\n## Output Arguments\n\ncollapse all\n\nSimulation time points, returned as a numeric vector or cell array. If `simdata` is scalar, `t` is an n-by-1 vector, where n is the number of time points. If `simdata` is an array of objects, `t` is a k-by-1 cell array, where k is the size of `simdata`.\n\nSimulation data, returned as a numeric matrix or cell array. If `simdata` is scalar, `x` is an n-by-m matrix, where n is the number of time points and m is the number of quantities and sensitivities logged during the simulation. If `simdata` is an array of objects, `x` is a k-by-1 cell array, where k is the size of `simdata`.\n\nNames of quantities and sensitivities logged during the simulation, returned as a cell array. If `simdata` is scalar, `names` is an m-by-1 cell array. If `simdata` is an array of objects, `names` is a k-by-1 cell array, where k is the size of `simdata`.\n\nSimulation results, returned as a `SimData` object.", null, "" ]
[ null, "https://au.mathworks.com/help/examples/simbio/win64/ExtractDataFromSimDataObjectExample_01.png", null, "https://au.mathworks.com/help/examples/simbio/win64/ExtractDataFromSimDataObjectExample_02.png", null, "https://au.mathworks.com/images/responsive/supporting/apps/doc_center/bg-trial-arrow.png", null ]
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https://easystats.github.io/performance/reference/r2_efron.html
[ "Calculates Efron's pseudo R2.\n\n## Usage\n\nr2_efron(model)\n\n## Arguments\n\nmodel\n\nGeneralized linear model.\n\nThe R2 value.\n\n## Details\n\nEfron's R2 is calculated by taking the sum of the squared model residuals, divided by the total variability in the dependent variable. This R2 equals the squared correlation between the predicted values and actual values, however, note that model residuals from generalized linear models are not generally comparable to those of OLS.\n\nEfron, B. (1978). Regression and ANOVA with zero-one data: Measures of residual variation. Journal of the American Statistical Association, 73, 113-121." ]
[ null ]
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https://www.whirldatascience.com/2019/03/27/segnet-applicability-in-single-object-detection-with-low-resolution-images/
[ "We thank Madhusudhan B A, Ara Ramalingam and Muthupandian Thangarajan for their guidance and support towards making this paper a reality\n\nAbstract\n\nWe implemented the SegNet neural network architecture to detect strays of transparent and colored plastic on a conveyor belt containing paper from recycled garbage at a recycling / sorting facility in California and to determine whether this architecture was suitable for single object detection. We have also analyzed the performance of the model generated during the different stages of training on our test set to identify patterns if any.\n\nSegNet was designed to be an efficient architecture for pixel-wise semantic segmentation and it was our opinion that a pixel-wise semantic segmentation will aide in detecting the contours of plastic. FCN1 is also a popular architecture for pixel-wise segmentation but we chose SegNet as the authors of SegNet claim that their architecture was more efficient in terms of memory, accuracy, computation time compared to FCN and also used fewer trainable parameters.\n\nAn alternate was to try the faster R-CNN2. Since one of our initial requirements was to identify contours of the plastic, we did not consider Faster R-CNN as it would have only provided us with bounding boxes.\n\n1.Introduction", null, "Our aim was to do identify strays of transparent plastic on a moving conveyor belt containing mostly paper at a garbage sorting facility using SegNet and to determine if it is the right method to solve our problem. SegNet is a deep fully convolutional neural network for pixel-wise segmentation. The main challenge we faced was that, even visually, it was not possible to identify plastic in certain cases.\n\nFigure 1 and 2 serves as an example. Figure 1 can be clearly concluded as plastic while in Figure 2 it is unclear.\n\n2.Architecture\n\nThis SegNet architecture was derived from the deep FCN.", null, "It consists of two parts – an encoder and a decoder. The encoder is similar to the VGG163, but without the fully connected layer thus making the model smaller. The decoder consists of the deconvolutional network which is used for the upsampling process. This upsampling is done for accurate pixel-wise classication and to increase the resolution of the downsampled feature maps. Every decoder has a corresponding encoder.\n\nThe decoder makes use of the max-pooling indices which is obtained from the corresponding encoder to perform upsampling of the feature maps from the encoder.", null, "The reusing of max-pooling indices helps in reducing the training parameters and also improves the boundary delineation. We have made use of the SegNet – Basic architecture. This consists of four convolutional layers in encoder coupled with batch normalization and ReLu followed by a maxpooling layer. Decoder consists of the same but instead of the max-pooling layer an upsampling layer is present. The architecture of FCN and SegNet-Basic have been shown in Figure 3 and Figure 4 respectively.\n\n3.Dataset preparation\n\nStep 1: Dataset Collection & Preparation\n\nOur source data was a video shot through an entry level mobile phone camera. We collected the images by cutting frames from the video. The images were resized as our model takes an input of 480px of width and 360px of height. Then we took a total of 1,000 images such that 750 images contained plastic and 250 images were just paper without any plastic. Allotted a total of 600 images of plastic and 150 images without plastic to the training set and the rest to the validation set.\n\nStep 2: Dataset Ground Truth\n\nWe annotated the dataset using SegNet-annotate-tool4 . The annotation tool produces an output in a format which is not readily acceptable by the SegNet algorithm. We were able to suitably handengineer and automate the conversion process so that the output format was acceptable.\n\nStep 3: Weight Calculation\n\nThe weights5 have to be calculated using the train set. These weights are used to calculate the loss during the training process. According to the SegNet paper, when there is a large variation in the number of pixels in each class in the training set there is a requirement to weight the loss differently. This is known as class balancing.\n\n4.Training the model", null, "The process of training involves passing batches of the train images to the network using a concept of input pipeline. This input pipeline involves the use of two main queues, filename queue and example queue. Filename queue collects the filenames, which are passed through a decoder and enqueued to the example queue where the images are dequeued and passed to the network in batches and the training process starts. Figure 5 illustrates this process, this process is called input pipelining.\n\nWe used an input of 360 x 480 on an NVIDIA GeForce GTX 1050Ti with cuDNN6 v6 acceleration. There are two variants of the SegNet architecture – first the standard SegNet and second the SegNet Basic.\n\nThe rst variant being standard SegNet architecture makes use of 13 convolutional layers in both encoder and decoder networks. We tried this on our 4GB GTX 1050Ti GPU, but, encountered a CUDA7 out of memory error.\n\nSince all the images which we pass to the network in batches are stored in the GPU memory, the more layers we use the more memory gets utilized and thus we encountered this CUDA out of memory error. Then we tried reducing the layersby half to six layers and still encountered the same problem. Then we tried the second variant SegNet – Basic which makes use of four convolutional layers in both encoder and decoder networks as shown in Figure 4. This ran smoothly on our GPU and thus we made use of the egNet-Basic architecture. Figure 5 Input Pipeline to pass images to the network\n\nAt each step of the training process the mean Intersection over Union (mIoU), loss and accuracy is calculated for the the batch of training set.\n\n4.1.The mIoU is calculated by using the following formula :", null, "Where : True Positive[TP] is the number of pixels correctly classified as positive, False Positive[FP] is the number of pixels wrongly classified as positive, False Negative[FN] is the number of pixels wrongly classified as negative\n\n4.2.The accuracy value is calculated using the following formula:", null, "Where: True Negative [TN] is the number of pixels [n(px)] correctly classified as negative. The loss is calculated by using the the ground truth image as well as the SegNet networks output using the pixel values (These images are gray images). At every 100 steps the mean Intersection over Union, loss and accuracy is calculated for the validation set. The graphs for the above process is maintained in a TensorBoard8 and the values are maintained in a csv. At every 1,000 steps the models checkpoint file (which consists of model weights to test our model) will be saved.\n\n5.Hyper-parameter settings\n\nWe first set the maximum steps to 30,000. The validation loss started increasing approximately from the 6,000th step but when it reached the 15,000th step it started increasing at a faster rate thus we chose the maximum steps to be 15,000. Batch size is the number of images passed to the network at every step of the training process. The higher the batch size the more sooner the training would complete. We chose three values for our batch size and they are as follows:\n\n5.1.Training with batch size 6\n\nBatch-size = 6, Learning rate = 0.001, min-after-dequeue9 = 0.4 X (Size of training set), max-steps = 15,000 When we used batch size of 6 we encountered the CUDA out of memory error which we have mentioned about earlier.\n\n5.2.Training with batch size 5\n\nBatch-size = 5,\n\nLearning rate = 0.001,\n\nmin-after-dequeue = 0.4 X (Size of training set), max-steps = 15,000\n\nThis ran smoothly without any errors.\n\n5.3.Training with batch size 4\n\nBatch-size = 4,\n\nLearning rate = 0.001,\n\nmin-after-dequeue = 0.4 X (Size of training set), max-steps = 15000\n\nWe tried the same using batch size 4 to check if this hyperparameter(batch-size) has a significant impact on the performance and accuracy. Repeated the training five times for both batch size 4 and batch size 5.\n\n5.4.Steps and epochs\n\nAt every step, x number of images are passed to the network where x is the batch size. Thus one epoch is completed once all the images in our training set have been passed on to the network.", null, "Where ts is the training set and bs is the batch size.\n\nExample: Since we have used a batch size of 4, 1 epoch will be completed in approximately 188 steps. In that case 15000 steps would correspond to almost 80 epochs.\n\n6.Analysis of the training process\n\nThe TensorBoard results for validation accuracy and validation loss for both the batch sizes are shown below.\n\n6.1.Batch Size 4", null, "The validation loss in the case of batch 4 reached a minimum of 0.2450 at the 5,800th step and from there on it started increasing. The figures 6a and 6b illustrate this.\n\n6.2.Batch Size 5", null, "The same kind of behaviour was observed in the case of batch 5, only difference was that the increase in loss started at the 4,900th step with a loss of 0.2258 which is shown in Figure 7a and 7b. The training loss in both the cases of batch size were gradually decreasing. But there was a sudden increase in the validation loss while the training loss continued to decrease from which we concluded that the model was overfitting.\n\nNext we created a test set of 150 images with 101 of them having plastic and 49 without plastic. We used every checkpoint of the model to test on our test set. The reason for using all the checkpoints was to analyze the differences in the model’s result at different steps. Since we maintained a checkpoint le every 1,000 steps we had a total of 15 checkpoints. We found that the batch size 5 model performed slightly better than batch size 4 model.\n\n7. Results from the model\n\n7.1.Pass Cases", null, "", null, "", null, "7.2.Failed Cases\n\nThe results were not perfect and to analyze the results we created our own set of categories to classify the results to compare the performance between different checkpoint files.", null, "We first tried to obtain a single number metric to categorize the results but this was not possible as the predicted results were not confined to a fixed number of cases. Example: Some cases involved the predicted plastic to be correctly located but the size of the blob varied from the ground truth. Another case where the plastic was detected correctly but extra non existent plastics were also detected along with it. To overcome this, we came up with a total of 6 unique categories for the images with plastic as shown Table 1. Our test set contained 101 images with plastic and 49 without plastic. We maintained a separate table for both. The main reason we considered the columns B (Table 1) as true positive is because our aim was to make sure the model detects all plastic regardless of the paper detected along with it. If our aim were to detect plastic without detecting a single paper we would have to consider the columns B (Table 1) as False Negative. The images without plastic have two categories either True Negative or False Positive as shown in Table 2. Table 1 gives a brief explanation of each category, for Table 2 the True Negative are those cases where there is no plastic in the image and the model also predicted the same, whereas False Positive are those cases where there is no plastic 6 in image but the model has predicted some non existent plastic.\n\n7.3.An excerpt of the sheet we maintained:\n\nThe categories which are significant in defining the performance of our model are in columns A (Table 1)\n\nTable 1: Images with plastic", null, "1 – Location of the detected plastics and size of it are perfect matched with the visual appearance\n2 – Locations are precise, but difference in the size of the plastics\n3 – Plastic locations and size are correct, but predicted plastics at additional locations.\n4 – Plastic locations precise with different sizes, also predicted plastics at additional locations\n5 – Not detected any plastics but showing ones where it doesn’t exist\n6 – No plastic detected\n\nTable 2: Images without plastics", null, "A common pattern that we observed during our analysis of test set on different checkpoint files (for both batch size 4 and 5) was that the number of extra non-existent plastic decreased whereas the number of null predictions increased as the steps increased.\n\n8.Increasing the Size of the Dataset\n\nWe found that a common reason for overfitting is usually due to a small dataset where the model usually tends to memorize the training images along with its corresponding labels and the model settings would be very specific to the train set. Then we increased the dataset from 1000 images to 2000 images of which we allotted 1500 images to train set and the rest to validation set. The graph of validation loss was no different (gradual decrease with a sudden increase) expect for the fact that the validation loss reduced, and the increased datasets model performed much better and got more True positives compared to the one we trained with 750 image.\n\nTable 3: Comparison of true Positives between 1000 and 2000 datasets", null, "From the above Table 3 it is clear that, the number of True Positives (TP) are higher at every stage for the 2,000 images dataset. And then, we made use of the same 2,000 images and considered 1,750 images as the training set and 250 images as the validation set. The result of this training gave a significant decrease in the loss to 0.1848 at the 9,300th step and started increasing from there on. Thus from the above results, we concluded the size of the dataset has a significant impact on the accuracy and validation loss value.\n\n9.Dropout inclusion", null, "The most efficient way to avoid the problem of overfitting is to include a dropout layer, but, when we ran the code with the included dropout on our NVIDIA GeForce GTX 1050 Ti, we once again encountered the CUDA out of memory error. To solve this problem, we ran the same code on Google Colab10 on a 12GB GPU with the 2,000 images dataset and the result of the validation loss graph showed no sudden increase as in the previous runs. The dropout layer significantly reduced the problem of overfitting but the loss value did not go below 0.1840. The graphs have been shown below in Figure 14a and 14b.\n\n10.Challenges\n\nIt was very dificult to segregate the images with plastic and without plastic visually. We found it dificult to find a single valued metric for classifying the test results but came up with a fixed set of categories to categorize them as explained earlier.", null, "We did not get the required accuracy for the plastic dataset. We assumed that the dataset might have been too small for such a complex network like SegNet which involves the use of lot of parameters. To check, if this holds true we took a smaller dataset of 1,000 images of T-shirts compared to our 2,000 images of plastic. We had an idea to make the process of purchasing shirts more engaging and interactive by which users could select the t-shirt they like on a screen and this would be correctly placed on the body of the user, which can be viewed on the same screen below. To accomplish this task, we required the Tshirt which a person was wearing, to be correctly segmented out. SegNet was the perfect architecture as it was capable of delineating the boundaries by which the exact shape of the shirt could be extracted. For this we downloaded images of people wearing t-shirts from the internet. We took this new dataset to see, if the image quality also had a significant impact on the detection results.", null, "We took a total of 1,045 images allotted 900 as the training set and the rest as the validation set. We used an input of 360 X 480 on an NVIDIA GeForce GTX 1050Ti with cuDNN v6 acceleration. The labeling of these images were easy for us compared to the plastic labeling. The images were of high quality compared to the plastic dataset which was mediocre. We trained the model with the following hyperparameters: Batch-size=5, Learning rate=0.001, min-after-dequeue= 0.4 x (Size of training set), max-steps= 20000 Once the training of the t-shirts completed, we observed that there was a gradual decrease without any sudden increase in the validation loss value. The curve that we were expecting from our plastic dataset. The validation loss reached a minimum of 0.05 which was significantly better (Figure 15a & 15b).\n\n12.Sample results of the t-shirt dataset", null, "We succeeded in segmenting out the t-shirts a person is wearing, which is clear from the above results. From this additional process, we learnt that a small dataset was sufficient to obtain a good accuracy with minimal loss. We also found that increasing the dataset may not have a significant impact on accuracy and loss as proved by the plastic dataset, unless the image quality is good. Thus we identified that the required result could be achieved using a small dataset provided that we have a clear or unambiguous dataset.", null, "From this we could conclude that the dataset size is not a limiting factor for accuracy and the quality of images do play a vital role in obtaining a good accuracy.\n\n13.Quantitative comparison\n\nTable 4: 1000 Dataset-plastic (750-train, 250-validation)", null, "Table 5: 2000 Dataset-plastic (1500-train, 500-validation)", null, "BOOK A FREE CONSULTATION" ]
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{"ft_lang_label":"__label__en","ft_lang_prob":0.9466666,"math_prob":0.94668114,"size":16926,"snap":"2019-51-2020-05","text_gpt3_token_len":3611,"char_repetition_ratio":0.1396407,"word_repetition_ratio":0.03876774,"special_character_ratio":0.21357675,"punctuation_ratio":0.07970343,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9586108,"pos_list":[0,1,2,3,4,5,6,7,8,9,10,11,12,13,14,15,16,17,18,19,20,21,22,23,24,25,26,27,28,29,30,31,32,33,34,35,36,37,38,39,40,41,42,43,44,45,46],"im_url_duplicate_count":[null,2,null,2,null,2,null,2,null,2,null,2,null,2,null,2,null,2,null,2,null,2,null,2,null,2,null,2,null,2,null,2,null,2,null,2,null,2,null,2,null,2,null,2,null,2,null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2020-01-22T02:01:11Z\",\"WARC-Record-ID\":\"<urn:uuid:ac20d19d-247a-4081-b26e-9f4adcbccc20>\",\"Content-Length\":\"72542\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:bf8c333b-4522-4b70-b1ad-f3e9b3e1585a>\",\"WARC-Concurrent-To\":\"<urn:uuid:40d5f968-138c-48d7-9661-ce20779a6138>\",\"WARC-IP-Address\":\"35.226.14.252\",\"WARC-Target-URI\":\"https://www.whirldatascience.com/2019/03/27/segnet-applicability-in-single-object-detection-with-low-resolution-images/\",\"WARC-Payload-Digest\":\"sha1:D42TUR5QGGTF7GTSCERWFY3HQQXTFRVX\",\"WARC-Block-Digest\":\"sha1:4WNKARAPIJ3F7TEQYVX6ZFIIHXZ7PGZP\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2020/CC-MAIN-2020-05/CC-MAIN-2020-05_segments_1579250606269.37_warc_CC-MAIN-20200122012204-20200122041204-00016.warc.gz\"}"}
https://www.systutorials.com/docs/linux/man/3-slassq.f/
[ "# slassq.f (3) - Linux Manuals\n\nslassq.f -\n\n## SYNOPSIS\n\n### Functions/Subroutines\n\nsubroutine slassq (N, X, INCX, SCALE, SUMSQ)\nSLASSQ updates a sum of squares represented in scaled form.\n\n## Function/Subroutine Documentation\n\n### subroutine slassq (integerN, real, dimension( * )X, integerINCX, realSCALE, realSUMSQ)\n\nSLASSQ updates a sum of squares represented in scaled form.\n\nPurpose:\n\n``` SLASSQ returns the values scl and smsq such that\n\n( scl**2 )*smsq = x( 1 )**2 +...+ x( n )**2 + ( scale**2 )*sumsq,\n\nwhere x( i ) = X( 1 + ( i - 1 )*INCX ). The value of sumsq is\nassumed to be non-negative and scl returns the value\n\nscl = max( scale, abs( x( i ) ) ).\n\nscale and sumsq must be supplied in SCALE and SUMSQ and\nscl and smsq are overwritten on SCALE and SUMSQ respectively.\n\nThe routine makes only one pass through the vector x.\n```\n\nParameters:\n\nN\n\n``` N is INTEGER\nThe number of elements to be used from the vector X.\n```\n\nX\n\n``` X is REAL array, dimension (N)\nThe vector for which a scaled sum of squares is computed.\nx( i ) = X( 1 + ( i - 1 )*INCX ), 1 <= i <= n.\n```\n\nINCX\n\n``` INCX is INTEGER\nThe increment between successive values of the vector X.\nINCX > 0.\n```\n\nSCALE\n\n``` SCALE is REAL\nOn entry, the value scale in the equation above.\nOn exit, SCALE is overwritten with scl , the scaling factor\nfor the sum of squares.\n```\n\nSUMSQ\n\n``` SUMSQ is REAL\nOn entry, the value sumsq in the equation above.\nOn exit, SUMSQ is overwritten with smsq , the basic sum of\nsquares from which scl has been factored out.\n```\n\nAuthor:\n\nUniv. of Tennessee\n\nUniv. of California Berkeley" ]
[ null ]
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http://num.bubble.ro/d/49/4000/
[ "Division table for N = 49 / 3999÷4000\n\n49 / 3999 = 0.0123 [+]\n49 / 3999.01 = 0.0123 [+]\n49 / 3999.02 = 0.0123 [+]\n49 / 3999.03 = 0.0123 [+]\n49 / 3999.04 = 0.0123 [+]\n49 / 3999.05 = 0.0123 [+]\n49 / 3999.06 = 0.0123 [+]\n49 / 3999.07 = 0.0123 [+]\n49 / 3999.08 = 0.0123 [+]\n49 / 3999.09 = 0.0123 [+]\n49 / 3999.1 = 0.0123 [+]\n49 / 3999.11 = 0.0123 [+]\n49 / 3999.12 = 0.0123 [+]\n49 / 3999.13 = 0.0123 [+]\n49 / 3999.14 = 0.0123 [+]\n49 / 3999.15 = 0.0123 [+]\n49 / 3999.16 = 0.0123 [+]\n49 / 3999.17 = 0.0123 [+]\n49 / 3999.18 = 0.0123 [+]\n49 / 3999.19 = 0.0123 [+]\n49 / 3999.2 = 0.0123 [+]\n49 / 3999.21 = 0.0123 [+]\n49 / 3999.22 = 0.0123 [+]\n49 / 3999.23 = 0.0123 [+]\n49 / 3999.24 = 0.0123 [+]\n49 / 3999.25 = 0.0123 [+]\n49 / 3999.26 = 0.0123 [+]\n49 / 3999.27 = 0.0123 [+]\n49 / 3999.28 = 0.0123 [+]\n49 / 3999.29 = 0.0123 [+]\n49 / 3999.3 = 0.0123 [+]\n49 / 3999.31 = 0.0123 [+]\n49 / 3999.32 = 0.0123 [+]\n49 / 3999.33 = 0.0123 [+]\n49 / 3999.34 = 0.0123 [+]\n49 / 3999.35 = 0.0123 [+]\n49 / 3999.36 = 0.0123 [+]\n49 / 3999.37 = 0.0123 [+]\n49 / 3999.38 = 0.0123 [+]\n49 / 3999.39 = 0.0123 [+]\n49 / 3999.4 = 0.0123 [+]\n49 / 3999.41 = 0.0123 [+]\n49 / 3999.42 = 0.0123 [+]\n49 / 3999.43 = 0.0123 [+]\n49 / 3999.44 = 0.0123 [+]\n49 / 3999.45 = 0.0123 [+]\n49 / 3999.46 = 0.0123 [+]\n49 / 3999.47 = 0.0123 [+]\n49 / 3999.48 = 0.0123 [+]\n49 / 3999.49 = 0.0123 [+]\n49 / 3999.5 = 0.0123 [+]\n49 / 3999.51 = 0.0123 [+]\n49 / 3999.52 = 0.0123 [+]\n49 / 3999.53 = 0.0123 [+]\n49 / 3999.54 = 0.0123 [+]\n49 / 3999.55 = 0.0123 [+]\n49 / 3999.56 = 0.0123 [+]\n49 / 3999.57 = 0.0123 [+]\n49 / 3999.58 = 0.0123 [+]\n49 / 3999.59 = 0.0123 [+]\n49 / 3999.6 = 0.0123 [+]\n49 / 3999.61 = 0.0123 [+]\n49 / 3999.62 = 0.0123 [+]\n49 / 3999.63 = 0.0123 [+]\n49 / 3999.64 = 0.0123 [+]\n49 / 3999.65 = 0.0123 [+]\n49 / 3999.66 = 0.0123 [+]\n49 / 3999.67 = 0.0123 [+]\n49 / 3999.68 = 0.0123 [+]\n49 / 3999.69 = 0.0123 [+]\n49 / 3999.7 = 0.0123 [+]\n49 / 3999.71 = 0.0123 [+]\n49 / 3999.72 = 0.0123 [+]\n49 / 3999.73 = 0.0123 [+]\n49 / 3999.74 = 0.0123 [+]\n49 / 3999.75 = 0.0123 [+]\n49 / 3999.76 = 0.0123 [+]\n49 / 3999.77 = 0.0123 [+]\n49 / 3999.78 = 0.0123 [+]\n49 / 3999.79 = 0.0123 [+]\n49 / 3999.8 = 0.0123 [+]\n49 / 3999.81 = 0.0123 [+]\n49 / 3999.82 = 0.0123 [+]\n49 / 3999.83 = 0.0123 [+]\n49 / 3999.84 = 0.0123 [+]\n49 / 3999.85 = 0.0123 [+]\n49 / 3999.86 = 0.0123 [+]\n49 / 3999.87 = 0.0123 [+]\n49 / 3999.88 = 0.0123 [+]\n49 / 3999.89 = 0.0123 [+]\n49 / 3999.9 = 0.0123 [+]\n49 / 3999.91 = 0.0123 [+]\n49 / 3999.92 = 0.0123 [+]\n49 / 3999.93 = 0.0123 [+]\n49 / 3999.94 = 0.0123 [+]\n49 / 3999.95 = 0.0123 [+]\n49 / 3999.96 = 0.0123 [+]\n49 / 3999.97 = 0.0123 [+]\n49 / 3999.98 = 0.0123 [+]\nNavigation: Home | Addition | Substraction | Multiplication | Division       Tables for 49: Addition | Substraction | Multiplication | Division\n\nOperand: 1 2 3 4 5 6 7 8 9 10 20 30 40 50 60 70 80 90 100 200 300 400 500 600 700 800 900 1000 2000 3000 3991 3992 3993 3994 3995 3996 3997 3998 3999 4000 4001 4002 4003 4004 4005 4006 4007 4008 4009 5000 6000 7000 8000 9000\n\nDivision for: 1 2 3 4 5 6 7 8 9 10 20 30 40 41 42 43 44 45 46 47 48 49 50 60 70 80 90 100 200 300 400 500 600 700 800 900 1000 2000 3000 4000 5000 6000 7000 8000 9000" ]
[ null ]
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https://www.gkkv.com/113_113015/
[ "# 你是我的命中注定\n\n《你是我的命中注定》最新章节(提示:已启用缓存技术,最新章节可能会延时显示,登录书架即可实时查看。)\n\nChapter101. 你是我的命中注定\nChapter99.沈靖情况危急。\nChapter100. 危机重重。\nChapter97. 失望的心。\nChapter98. 沈靖病情暴露。\n《你是我的命中注定》正文\nChapter1. 其实,并不坚强。\nChapter2. 你若安好 便是晴天\nChapter3. 假如时光倒流。\nChapter4. 天不遂人愿。\nChapter5. 扰乱了谁的心。\nChapter6. 一波未平一波又起。\nChapter7.直播秀风波四起。\nChapter8.泰宇出现了。\nChapter9. 遇见,是最美的年华。\nChapter10. 物是人非事事休。\nChapter11. 隐形的心动。\nChapter12. 误会加深。\nChapter13.交友不慎。\nChapter14. 沈若溪的报复计划。\nChapter15.为伊消得人憔悴\nChapter16. 自作孽不可活。\nChapter17. 谢谢你的出现。\nChapter18. 不期而遇。\nChapter19. 滚蛋吧,人渣。\nChapter20. 逝去的美好。\nChapter21.爱情是上瘾的毒药\nChapter22. 你真的能忘了我吗?\nChapter23. 看清自己的心。\nChapter24. 越在乎,越忐忑。\nChapter25. 我一定要见到你。\nChapter26. 原来,只是局外人。\nChapter27. 要的只是一个结果。\nChapter28. 感受你的温度。\nChapter29.升级矛盾。\nChapter30. 女人心海底针。\nChapter31. 等着你上钩。\nChapter32. 突然的告白。\nChapter33. 解开心结。\nChapter34.你是我的专属天使。\nChapter35. 困扰不断。\nChapter36. 沈若溪回沈家。\nChapter37.惊天秘密。\nChapter38.泰宇出手救沈若溪。\nChapter39.智闯沈氏武馆。\nChapter40.藏起来的秘密。\nChapter41.误中圈套。\nChapter42.姜成勋识破诡计。\nChapter43.游艇爆炸。\nChapter44. 命运的捉弄。\nChapter45. 遗失的美好。\nChapter46. 分我一半的眼泪。\nChapter47. 意外发生。\nChapter48. 针锋相对。\nChapter49. 斗志盎然。\nChapter50. 时光荏苒,岁月匆匆\nChapter51. 解梦。\nChapter52. 奋不顾身靠近你。\nChapter53. 唯恐天下不乱。\nChapter54.若溪,是道不明的情愫\nChapter55. 我的眼里只有你。\nChapter56. 请你离我越远越好。\nChapter57. 一场闹剧。\nChapter58. 背道而驰。\nChapter59. 关于秘密,太入人心\nChapter60. 离别意味重逢。\nChapter61. 毛里求斯的惊喜。\nChapter62.毛里求斯的惊喜2.\nChapter63. 惹恼沈若溪。\nChapter64. 隐藏的心。\nChapter65. 回到武馆。\nChapter66.带不走的思念。\nChapter67.任务空降。\nChapter68. 龙潭虎穴。\nChapter69.两人再次相遇。\nChapter70. 父爱如山。\nChapter71.令人窒息的见面。\nChapter72.沈若溪落入险境。\nChapter73.触不及防的吻。\nChapter74.任务成功。\nChapter75.暗生情愫。\nChapter76. 意外得知秘密。\nChapter77. 一尘不染的真心\nChapter78. 慢慢靠近彼此。\nChapter79. 如果爱下去。\nChapter80. 隐藏的感情。\nChapter81. 好戏上演。\nChapter82.自己挖的坑,自己跳。\nChapter83. 热泪盈眶。\nChapter84. 你是卧底?\nChapter85. 怦然心动。\nChapter86.沈若溪,服从命令。\nChapter87.爱情萌芽的初期。\nChapter88. 我承认,我喜欢你。\nChapter89. 忘不掉的悲伤。\nChapter90. 突然,想爱你。\nChapter91. 触动心的失望。\nChapter92.生不如死。\nChapter93.关于毛里求斯的秘密。\nChapter94.心有了暖的温度。\nChapter95. 泰宇避而不见。\nChapter96. 痛声大哭。\nChapter97. 失望的心。\nChapter98. 沈靖病情暴露。\nChapter99.沈靖情况危急。\nChapter100. 危机重重。\nChapter101. 你是我的命中注定" ]
[ null ]
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https://edurev.in/course/quiz/attempt/17630_Olympiad-Test-Pattern-1-/f04f2b78-94b1-4939-8e3e-34ad7a2de09b
[ "# Olympiad Test: Pattern - 1\n\nTest Description\n\n## 15 Questions MCQ Test Science Olympiad Class 7 | Olympiad Test: Pattern - 1\n\nOlympiad Test: Pattern - 1 for Class 7 2023 is part of Science Olympiad Class 7 preparation. The Olympiad Test: Pattern - 1 questions and answers have been prepared according to the Class 7 exam syllabus.The Olympiad Test: Pattern - 1 MCQs are made for Class 7 2023 Exam. Find important definitions, questions, notes, meanings, examples, exercises, MCQs and online tests for Olympiad Test: Pattern - 1 below.\n 1 Crore+ students have signed up on EduRev. Have you?\nOlympiad Test: Pattern - 1 - Question 1\n\n### ​Directions: Choose the appropriate number which follow the given pattern.", null, "Detailed Solution for Olympiad Test: Pattern - 1 - Question 1\n\n7 × 5 + 6 = 41\n8 × 7 + 5 = 61\n6 × 7 + 9 = 51\n\nOlympiad Test: Pattern - 1 - Question 2\n\n### ​​Directions: Choose the appropriate number which follow the given pattern.", null, "Detailed Solution for Olympiad Test: Pattern - 1 - Question 2\n\n7 × 4 + 3 × 5 = 28 + 15 = 43\n6 × 2 + 6 × 4 = 12 + 24 = 36\n9 × 3 + 5 × 7 = 27 + 35 = 62\n\nOlympiad Test: Pattern - 1 - Question 3\n\n### ​​Directions: Choose the appropriate number which follow the given pattern.", null, "Detailed Solution for Olympiad Test: Pattern - 1 - Question 3\n\n84 ÷ 7 + 42 ÷ 2 = 12 + 21 = 33\n117 ÷ 13 + 96 ÷ 16 = 9 + 6 = 15\n153 ÷ 17 + 63 ÷ 3 = 9 + 21 = 30\n\nOlympiad Test: Pattern - 1 - Question 4\n\nDirections: Choose the appropriate number which follow the given pattern.", null, "Detailed Solution for Olympiad Test: Pattern - 1 - Question 4\n\n5 × 2 – 1 = 9\n9 × 2 + 1 = 19\n19 × 2 – 1 = 37\n37 × 2 + 1 = 75\n75 × 2 – 1 = 149\n149 × 2 + 1 = 299\n299 × 2 – 1 = 597\n\nOlympiad Test: Pattern - 1 - Question 5\n\n​​​​Directions: Choose the appropriate number which follow the given pattern.", null, "Detailed Solution for Olympiad Test: Pattern - 1 - Question 5\n\n3 × 7 + 6 × 9 = 21 + 54 = 75\n8 × 3 + 11 × 5 = 24 + 55 = 79\n9 × 4 + 8 × 7 = 36 + 56 = 92\n\nOlympiad Test: Pattern - 1 - Question 6\n\n​​​​Directions: Choose the appropriate number which follow the given pattern.", null, "Detailed Solution for Olympiad Test: Pattern - 1 - Question 6\n\n(46 + 18) ÷ 8 = 64 ÷ 8 = 8\n(62 + 34) ÷ 8 = 96 ÷ 8 = 12\n(57 + 15) ÷ 8 = 72 ÷ 8 = 9\n\nOlympiad Test: Pattern - 1 - Question 7\n\n​​​​​Directions: Choose the appropriate number which follow the given pattern.", null, "Detailed Solution for Olympiad Test: Pattern - 1 - Question 7\n\n(13 – 5)2 + (7 – 3)2 = 64 + 16 = 80\n(23 – 17)2 + (8 – 1)2 = 36 + 49 = 85\n(25 – 12)2 + (5 – 2)2 = 169 + 9 = 178\n\nOlympiad Test: Pattern - 1 - Question 8\n\n​​​​​Directions: Choose the appropriate number which follow the given pattern.​", null, "Detailed Solution for Olympiad Test: Pattern - 1 - Question 8\n\n(31 + 17) – (17 + 8) = 48 – 25 = 23\n(47 + 35) – (24 + 7) = 82 – 31 = 51\n(67 + 12) – (19 + 8) = 79 – 27 = 52\n\nOlympiad Test: Pattern - 1 - Question 9\n\n​​​​​Directions: Choose the appropriate number which follow the given pattern.​", null, "Detailed Solution for Olympiad Test: Pattern - 1 - Question 9", null, "", null, "Olympiad Test: Pattern - 1 - Question 10\n\n​​​​​​Directions: Choose the appropriate number which follow the given pattern.​", null, "Detailed Solution for Olympiad Test: Pattern - 1 - Question 10", null, "Olympiad Test: Pattern - 1 - Question 11\n\n​​​​​​Directions: Choose the appropriate number which follow the given pattern.​", null, "Detailed Solution for Olympiad Test: Pattern - 1 - Question 11", null, "Olympiad Test: Pattern - 1 - Question 12\n\n​​​​​​Directions: Choose the appropriate number which follow the given pattern.​", null, "Detailed Solution for Olympiad Test: Pattern - 1 - Question 12\n\n(8 × 7) + (9 × 3) = 56 + 27 = 83\n(13 × 5) + (8 × 4) = 65 + 32 = 97\n(17 × 4) + (7 × 9) = 68 + 63 = 131\n\nOlympiad Test: Pattern - 1 - Question 13\n\n​​​​​​Directions: Choose the appropriate number which follow the given pattern.​", null, "Detailed Solution for Olympiad Test: Pattern - 1 - Question 13", null, "Olympiad Test: Pattern - 1 - Question 14\n\n​​​​​​Directions: Choose the appropriate number which follow the given pattern.​", null, "Detailed Solution for Olympiad Test: Pattern - 1 - Question 14", null, "Olympiad Test: Pattern - 1 - Question 15\n\n​​​​​​Directions: Choose the appropriate number which follow the given pattern.​", null, "Detailed Solution for Olympiad Test: Pattern - 1 - Question 15\n\n(12 + 52 + 42 + 32) × 10 = 510\n(22 + 72 + 62 + 42) × 10 = 1050\n(52 + 32 + 82 + 92)  × 10 = 1790" ]
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https://www.sanfoundry.com/electric-drives-questions-answers-three-phase-half-wave-ac-dc-conversion-resistive-loads/
[ "# Electric Drives Questions and Answers – Solid-State Switching Circuits – Three Phase, Half-Wave, AC/DC Conversion for Resistive Loads\n\nThis set of Electric Drives Multiple Choice Questions & Answers (MCQs) focuses on “Solid-State Switching Circuits – Three Phase, Half-Wave, AC/DC Conversion for Resistive Loads”.\n\n1. Calculate the Vo(avg) for the 3-Φ phase Half-wave uncontrolled rectifier if the supply value is 440 V.\na) 297.25 V\nb) 298.15 V\nc) 298.11 V\nd) 300.15 V\n\nExplanation: The Vo(avg) for the 3-Φ phase Half-wave uncontrolled rectifier is 3Vml÷2π. The value of output voltage is 3Vml÷2π=3×√2×440÷6.28=297.25 V.\n\n2. Calculate the pulse number if the supply frequency is 2π and the output frequency is 2π÷3.\na) 4\nb) 5\nc) 6\nd) 3\n\nExplanation: The pulse number can be calculated using the ratio of input frequency to the output frequency. The value of pulse number (P) is 2π÷(2π÷3)=3. It is a three-pulse converter or 3-Φ phase Half-wave uncontrolled rectifier.\n\n3. Calculate the average value of current for the 3-Φ phase Half-wave uncontrolled rectifier if the supply value is 400 V and resistive load value is 5 Ω.\na) 54.04 A\nb) 57.26 A\nc) 51.64 A\nd) 58.15 A\n\nExplanation: The Io(avg) for the 3-Φ phase Half-wave uncontrolled rectifier is 3Vml÷2πR. The value of output voltage is 3Vml÷2πR=3×√2×440÷6.28×5=54.04 A.\n\n4. In 3-Φ Fully controlled rectifier calculate the average value of the voltage if the supply is 400 V and firing angle is 45°.\na) 381.15 V\nb) 382.16 V\nc) 383.19 V\nd) 384.25 V\n\nExplanation: In 3-Φ Fully controlled rectifier, the average value of the voltage is 3Vml(cos(∝))÷π=3×400×√2(cos(45°))÷3.14=382.16 V.\n\n5. Calculate the Vo(r.m.s) (Highly inductive load) for the 3-Φ phase Half-wave uncontrolled rectifier if the supply value is 441 V.\na) 297.25 V\nb) 298.15 V\nc) 298.11 V\nd) 300.15 V\n\nExplanation: The Vo(r.m.s) for the 3-Φ phase Half-wave uncontrolled rectifier is 3Vml÷2π. The value of output voltage is 3Vml÷2π=3×√2×441÷6.28=297.25 V.\n\n6. Calculate the Vo(avg) for the 3-Φ phase Half-wave controlled rectifier if the supply value is 364 V and the value of firing angle is 2°.\na) 247.62 V\nb) 245.76 V\nc) 214.26 V\nd) 233.26 V\n\nExplanation: The Vo(avg) for the 3-Φ phase Half-wave controlled rectifier is 3Vmlcos(α)÷2π. The value of output voltage is 3Vmlcos(α)÷2π=3×√2×364×(.99)÷6.28=245.76 V.\n\n7. Calculate the value of the Input power factor for 3-Φ Fully controlled rectifier if the firing angle value is 16°.\na) .96\nb) .91\nc) .93\nd) .94\n\nExplanation: The value of the input power factor for 3-Φ Fully controlled rectifier is .95cos(16°)=.91. The input power factor is a product of distortion factor and displacement factor.\n\n8. In 3-Φ Semi-controlled rectifier calculate the average value of the voltage if the supply is 299 V and firing angle is 56.15°.\na) 311.26 V\nb) 304.26 V\nc) 314.51 V\nd) 312.45 V\n\nExplanation: In 3-Φ Semi-controlled rectifier, the average value of the voltage is 3Vml(1+cos(∝))÷2π=3×299×√2(1+cos(56.15°))÷6.28=314.51 V.\n\n9. Calculate the circuit turn-off time for 3-Φ Fully controlled rectifier if the firing angle is 13° and supply frequency is 49.5 Hz.\na) 730.2 msec\nb) 740.8 msec\nc) 754.5 msec\nd) 755.1 msec\n\nExplanation: The circuit turn-off time for 3-Φ Fully controlled rectifier is (240°-α)÷ω. The value of circuit turn-off time for ∝ < 60° is (240°-13°)÷6.28×49.5=730.2 msec.\n\n10. Calculate the circuit turn-off time for 3-Φ Fully controlled rectifier if the firing angle is 170° and supply frequency is 50.5 Hz.\na) 32.4 msec\nb) 35.2 msec\nc) 39.3 msec\nd) 31.5 msec\n\nExplanation: The circuit turn-off time for 3-Φ Fully controlled rectifier is (180°-α)÷Ω. The value of circuit turn-off time for ∝ ≥ 60° is (180°-170°)÷6.28×50.5=31.5 msec.\n\n11. Calculate the form factor if V(r.m.s)=45 V, V(avg)=15 V.\na) 2\nb) 5\nc) 3\nd) 8\n\nExplanation: The form factor is defined as the ratio of the Vr.m.s÷Vavg=45÷15=3. The r.m.s value is three times of average value Vavg.\n\n12. Calculate the Vo(avg) for the 3-Φ phase Half-wave controlled rectifier if the supply value is 480 V and the value of firing angle is 92°.\na) 264.02 V\nb) 487.26 V\nc) 858.26 V\nd) 248.25 V\n\nExplanation: The Vo(r.m.s) for the 3-Φ phase Half-wave controlled rectifier is 3Vm(1+cos(α))÷2π. The value of output voltage is 3Vm(1+cos(α+30))÷2π=3×480×√3×√2(1+cos(92))÷2π=264.02 V.\n\n13. Full form of SCR is ____________\na) Silicon controlled rectifier\nb) State-controlled rectifier\nc) State cover rectifier\nd) State-controlled reset\n\nExplanation: SCR stands for silicon controlled rectifier. It is a semi-controlled, bipolar, uni-directional switch. It is a high power rating than other power electronic devices.\n\n14. Full form of TRIAC is __________\na) Triode for Alternating current\nb) Tri for Alternating current\nc) Triode for Alternating counter\nd) Tri for Alternating counters\n\nExplanation: TRIAC stands for Triode for Alternating current. It is a bipolar, bidirectional switch. It is used in fan regulators to control the speed of fans.\n\n15. TRIAC is a unipolar switch.\na) True\nb) False\n\nExplanation: TRIAC stands for Triode for Alternating current. It is a bipolar, bidirectional switch. It is used in fan regulators to control the speed of fans.\n\nSanfoundry Global Education & Learning Series – Electric Drives.\n\nTo practice all areas of Electric Drives, here is complete set of 1000+ Multiple Choice Questions and Answers.", null, "" ]
[ null, "data:image/svg+xml,%3Csvg%20xmlns=%22http://www.w3.org/2000/svg%22%20viewBox=%220%200%20150%20150%22%3E%3C/svg%3E", null ]
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https://answers.everydaycalculation.com/subtract-fractions/30-10-minus-8-6
[ "Solutions by everydaycalculation.com\n\n## Subtract 8/6 from 30/10\n\n1st number: 3 0/10, 2nd number: 1 2/6\n\n30/10 - 8/6 is 5/3.\n\n#### Steps for subtracting fractions\n\n1. Find the least common denominator or LCM of the two denominators:\nLCM of 10 and 6 is 30\n2. For the 1st fraction, since 10 × 3 = 30,\n30/10 = 30 × 3/10 × 3 = 90/30\n3. Likewise, for the 2nd fraction, since 6 × 5 = 30,\n8/6 = 8 × 5/6 × 5 = 40/30\n4. Subtract the two fractions:\n90/30 - 40/30 = 90 - 40/30 = 50/30\n5. After reducing the fraction, the answer is 5/3\n6. In mixed form: 12/3\n\n#### Subtract Fractions Calculator\n\n-\n\nUse fraction calculator with our all-in-one calculator app: Download for Android, Download for iOS" ]
[ null ]
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https://www.codetd.com/article/6804477
[ "## qbzt day2 晚上(竟然还有晚上)\n\nA*\n\ng 当前点到根节点的深度\n\nh 当前点到终点理想的最优情况需要走几步\n\nf  f=g+h\n\nA*就是把所有的f从小到大排序\n\ng*(x) : S x 的理论最近距离\n\ng(x) : S x 对于 g*(x) 的估计\n\nf*(x) : x T 的理论最近距离,F*(x)=g*(x)+h*(x)\n\nf(x) : x T 对于 f*(x) 的估计,F(x)=g(x)+h(x)", null, "BFS 几乎一样,只是每次都弹出当前局面中f(x)最小的那个局面进行扩展\n\n——故需要维护一个优先队列(小根堆)\n\n——使用系统的priority_queue<>即可\n\nf(x) = g(x) + h(x) h(x) = 0 即失去了启发式函数,则变为Breath First Search\n\nf(x) = g(x) + h(x) g(x) = 0 则变为 Best First Search", null, "", null, "", null, "IDA*\n\ng:从根节点往下几步\n\nh:步数\n\ng+h>d return\n\nh(x)>h*(x)?\n\nh(x)越接近h*(x)跑得越快", null, "x 对一个数 p 有逆元当且仅当 (x, p) = 1\n\n……,等等,岂不是 ax == 1 (mod p)", null, "", null, "", null, "", null, "P = p1 * p2 * ... * pn\n\nPi = P / pi\n\nQi = Pi pi 的逆元\n\nx = sigma(ai * Pi * Qi)", null, "" ]
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https://www.skyneel.com/sumif-and-sumifs-function
[ "Categories\n\n# What is Difference between SUMIF and SUMIFS Function\n\nSUMIF function allows you to conditionally sum the values which match the given single criteria, While SUMIF is used to conditionally sum the values which match the multiple criteria. Most of the person little bit confused during using these functions. Today we have to discuss what is the difference between the SUMIF and SUMIFS function in Excel.\n\n## Difference between SUMIF and SUMIFS Function\n\nSUMIF and SUMIFS are both important functions which are located in the Math and Trig category. SUMIF function is designed to work with only one criteria and return the result which match the given condition. SUMIFS function is used to get the conditional total which match the given more than one criteria in active worksheet.\n\n### SUMIF Function in Excel\n\nSUM is an important function used to get the total of selected range of cells. But sometime we need to sum selected range of cells which match the given condition. In that situation you have to use SUMIF function at the place of SUM function in Excel. SUMIF is an important function of Excel which is located in the Mathematical and Trig category. This function is used to conditionally sum the specified range values which match the given condition.", null, "SUMIF(range, criteria, [sum_range])\n\nrange: It the range of continuous cells that you want to evaluated by the given criteria.\n\ncriteria: It is a condition which specifies that which items you want to add that match the given criteria in the range.\n\nsum_range: It is an optional argument which specifies which cells to be added. If “sum_range” argument is omitted then “range” is used as a “sum_range”.\n\nStep 1: First you have to prepare the given table in new worksheet.\n\nStep 2: If you want to get the total units only for “North 1” region then you have to apply the given SUMIF function.\n\n=SUMIF(B27:B35, “North 1”, C27:C35)\n\nIf you want to get the total units for all those cells which date is greater than “31-12-2016” then you have to apply the given SUMIF function.\n\n=SUMIF(A27:A35,”>31-12-2016″,C27:C35)\n\n### SUMIFS Function in Excel\n\nSUMIFS is an important Excel function which is found in Mathematical and Trig category. This function allows you to add the continuous range of cells which is specified by a given set of conditions or criteria in active worksheet. If you have more than one conditions or criteria then you have to use SUMIFS function. If you have Excel 2007 or upper version then you have to use SUMIF function on active worksheet. But if you don’t Excel 2003 or lower version then you are not able to use this function in active worksheet.", null, "SUMIFS(sum_range, criteria_range1, criteria1, [criteria_range2, criteria2], …)\n\nsum_range – It is the range of cells which you want to add which match the given conditions. All blank and text values are ignored.\n\ncriteria_range1 – It is the first range which is evaluated by the first specified criteria.\n\ncriteria1 – It is the first condition that must be matched in the criteria_range 1.\n\ncriteria_range2, criteria2, … – These are additional ranges and criteria which you can associated with them as per your need. It is an optional part. You have to specified up to 127 range or criteria as per your requirement during using the SUMIFS function.\n\nStep 1: Create the following given table in new worksheet.\n\nStep 2: If you want to get the total units only for “North 1” region which date is greater than “31-12-2016” then you have to apply following given formula.\n\n=SUMIFS(C27:C35,B27:B35,”North 1″,A27:A35,”>31-12-2016″)\n\nIf you want to get the total units only for “North 2” region which date is greater than “31-12-2016” then you have to apply following given formula.\n\n=SUMIFS(C27:C35,B27:B35,”North 2″,A27:A35,”>31-12-2016″)\n\nIf you want to get the total units of “North 1” & “North 2” region which date is greater than “31-12-2016” then you have to apply following given formula.\n\n=SUM(SUMIFS(C27:C35,B27:B35,{“North 1″,”North 2″},A27:A35,”>31-12-2016″))\n\nI hope after reading this difference between SUMIF and SUMIFS Function article, you can understand what is the difference between the SUMIF and SUMIFS function in Excel. If you have any suggestion regarding this guide then please write us in the comment box. Thanks to all." ]
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https://www.yuheng.tech/page/37/
[ "原SDAU暑假训练第18天做题(2018816)\n\nHDU一直关着,很烦。做了几个洛谷的题,挑了几个题解发我新博客上了,点击查看\n\nCodeforces Round 48 (Rated for Div. 2)", null, "", null, "", null, "大意:输入字符串s和t、各自的长度和q个询问,询问由第l到r个字母构成的s的子串中,包含t的个数\n\n#include <iostream>\n#include <string>\n#include <cstdio>\nusing namespace std;\nint n,m,w,sum=0;\nstring s,t;\nint main()\n{\nint n,m,q;\nscanf(\"%d%d%d\",&n,&m,&q);//s长度,n长度,q次数\ns.resize(1200);\nt.resize(1200);\nscanf(\"%s%s\",&s,&t);//s串,t串\nint l,r,ans=0;\nwhile(q--)\n{\nans=0;\nscanf(\"%d%d\",&l,&r);\nif(r-l+1>=m)\n{\nfor(int i=l-1;i+m-1<r;i++)\n{\nstring temp=s.substr(i,m);\nif(s.substr(i,m)==t.substr(0,m)) ans++;\n}\n}\nprintf(\"%d\\n\",ans);\n\n}\n}\n\n后来采用了类似打表的思想过了。\n\n#include<iostream>\n#include<cstdio>\n#include<string>\nusing namespace std;\nint a;\nint main()\n{\nint n,m,k,q,l,r,ans;\nstring s,t;\ncin>>n>>m>>q;\ncin>>s>>t;\nfor(int i=0; i<=n-m; i++)\nif(s.substr(i,m)==t)\na[i]=1;\nwhile(q--)\n{\nans=0;\ncin>>r>>l;\nfor(int i=r-1; i<=l-m; i++)\nif(a[i])\nans++;\ncout<<ans<<endl;\n}\nreturn 0;\n}\n\n别人家的题解:\n\n#include<cstdio>\n#include<cstring>\n#include<string>\n#include<iostream>\n#include<algorithm>\nusing namespace std;\nint main()\n{\nint n,m,q,i,j,l,r,len;\nint counts;\nint vis;\nstring s1,s2;\ncin>>n>>m>>q;\ncin>>s1>>s2;\nlen=s2.size();\nmemset(vis,0,sizeof(vis));\nstring::size_type pos=0;\nwhile((pos=s1.find(s2,pos))!=string::npos)\n{\nvis[pos+1]=pos+1;\npos++;\n}\nfor(i=1;i<=q;i++)\n{\ncounts=0;\nscanf(\"%d%d\",&l,&r);\nfor(j=l;j<=r;j++)\n{\nif(vis[j]!=0&&vis[j]+len-1<=r)\n{\ncounts++;\n}\n}\nprintf(\"%d\\n\",counts);\n}\nreturn 0;\n}\n\n还有前缀数组的大佬:\n\n#include <bits/stdc++.h>\nusing namespace std;\nint n,m,q;\nstring s,t;\nint l,r;\nint hay,shay;\nint main()\n{\ncin>>n>>m>>q;\ncin>>s>>t;\ns=\" \"+s;\nt=\" \"+t;\nfor(int i=1;i<=n-m+1;i++)\n{\nhay[i]=1;\nfor(int j=0;j<m;j++)\n{\nif(s[i+j]!=t[1+j])\n{\nhay[i]=0;\nbreak;\n}\n}\nshay[i]=shay[i-1]+hay[i];\n}\n\nwhile(q--)\n{\ncin>>l>>r;\nr=r-m+1;\nif(r<l) cout<<\"0\"<<endl;\nelse cout<<shay[r]-shay[l-1]<<endl;\n}\nreturn 0;\n}\n\n原【模拟】NewBuildingforSIS", null, "", null, "题意:给你n个相邻的建筑(从左到右编号1到n),每个建筑有h层,每个建筑的a层到b层中任意一层c层可以花一秒通过连廊直接到隔壁建筑的c层。上下楼1层需要1秒。求q次查询(建筑a,层a)到(建筑b,层b)的最短时间。\n\n#include <iostream>\n#include <cmath>\n#include <cstdio>\nusing namespace std;\nint main()\n{\nint n,h,a,b,k;\nscanf(\"%d%d%d%d%d\",&n,&h,&a,&b,&k);\nwhile(k--)\n{\nint ta,fa,tb,fb;long long ans=0;\nscanf(\"%d%d%d%d\",&ta,&fa,&tb,&fb);\nif(ta==tb)\nans+=abs(fb-fa);//同楼层\nif(ta!=tb)\n{\nans+=abs(tb-ta);//计算横向移动时间\nif(fa>=a&&fa<=b)\n{\nans+=abs(fb-fa);//如果都处于连廊直接通过的楼层,附加纵向距离\n}\nelse\n{\nint temp1=0,temp2=0;\ntemp1+=abs(fa-a);//temp1代表如果从最下层连廊走\ntemp1+=abs(fb-a);\ntemp2+=abs(fa-b);//temp1代表如果从最上层连廊走\ntemp2+=abs(fb-b);\nans+=min(temp1,temp2);//取最短距离\n}\n}\ncout<<ans<<endl;\n}\nreturn 0;\n}" ]
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https://www.textbook.ds100.org/ch/23/classification_log_model.html
[ "import warnings\n# Ignore numpy dtype warnings. These warnings are caused by an interaction\n# between numpy and Cython and can be safely ignored.\n# Reference: https://stackoverflow.com/a/40846742\nwarnings.filterwarnings(\"ignore\", message=\"numpy.dtype size changed\")\nwarnings.filterwarnings(\"ignore\", message=\"numpy.ufunc size changed\")\n\nimport numpy as np\nimport matplotlib.pyplot as plt\nimport pandas as pd\nimport seaborn as sns\n%matplotlib inline\nimport ipywidgets as widgets\nfrom ipywidgets import interact, interactive, fixed, interact_manual\nimport nbinteract as nbi\n\nsns.set()\nsns.set_context('talk')\nnp.set_printoptions(threshold=20, precision=2, suppress=True)\npd.options.display.max_rows = 7\npd.options.display.max_columns = 8\npd.set_option('precision', 2)\n# This option stops scientific notation for pandas\n# pd.set_option('display.float_format', '{:.2f}'.format)\n\ndef df_interact(df, nrows=7, ncols=7):\n'''\nOutputs sliders that show rows and columns of df\n'''\ndef peek(row=0, col=0):\nreturn df.iloc[row:row + nrows, col:col + ncols]\nif len(df.columns) <= ncols:\ninteract(peek, row=(0, len(df) - nrows, nrows), col=fixed(0))\nelse:\ninteract(peek,\nrow=(0, len(df) - nrows, nrows),\ncol=(0, len(df.columns) - ncols))\nprint('({} rows, {} columns) total'.format(df.shape, df.shape))\n\ndef jitter_df(df, x_col, y_col):\nx_jittered = df[x_col] + np.random.normal(scale=0, size=len(df))\ny_jittered = df[y_col] + np.random.normal(scale=0.05, size=len(df))\nreturn df.assign(**{x_col: x_jittered, y_col: y_jittered})\n\nlebron = pd.read_csv('lebron.csv')\n\n\n# 23.2. The Logistic Model¶\n\nIn this section, we introduce the logistic model, a regression model that we use to predict probabilities.\n\nRecall that fitting a model requires three components: a model that makes predictions, a loss function, and an optimization method. For the by-now familiar least squares linear regression, we select the model:\n\n\\begin{aligned} f_\\hat{\\boldsymbol{\\theta}} (\\textbf{x}) &= \\hat{\\boldsymbol{\\theta}} \\cdot \\textbf{x} \\end{aligned}\n\nAnd the loss function:\n\n\\begin{split} \\begin{aligned} L(\\boldsymbol{\\theta}, \\textbf{X}, \\textbf{y}) &= \\frac{1}{n} \\sum_{i}(y_i - f_\\boldsymbol{\\theta} (\\textbf{X}_i))^2\\\\ \\end{aligned} \\end{split}\n\nWe use gradient descent as our optimization method. In the definitions above, $$\\textbf{X}$$ represents the $$n \\times p$$ data matrix ($$n$$ is the number of data points and $$p$$ is the number of attributes), $$\\textbf{x}$$ represents a row of $$\\textbf{X}$$, and $$\\textbf{y}$$ is the vector of observed outcomes. The vector $$\\boldsymbol{\\hat{\\theta}}$$ contains the optimal model weights whereas $$\\boldsymbol{\\theta}$$ contains intermediate weight values generated during optimization.\n\n## 23.2.1. Real Numbers to Probabilities¶\n\nObserve that the model $$f_\\hat{\\boldsymbol{\\theta}} (\\textbf{x}) = \\hat{\\boldsymbol{\\theta}} \\cdot \\textbf{x}$$ can output any real number $$\\mathbb{R}$$ since it produces a linear combination of the values in $$\\textbf{x}$$, which itself can contain any value from $$\\mathbb{R}$$.\n\nWe can easily visualize this when $$x$$ is a scalar. If $$\\hat \\theta = 0.5$$, our model becomes $$f_\\hat{\\theta} (\\textbf{x}) = 0.5 x$$. Its predictions can take on any value from negative infinity to positive infinity:\n\nxs = np.linspace(-100, 100, 100)\nys = 0.5 * xs\nplt.plot(xs, ys)\nplt.xlabel('$x$')\nplt.ylabel(r'$f_\\hat{\\theta}(x)$')\nplt.title(r'Model Predictions for $\\hat{\\theta} = 0.5$');", null, "For classification tasks, we want to constrain $$f_\\hat{\\boldsymbol{\\theta}}(\\textbf{x})$$ so that its output can be interpreted as a probability. This means that it may only output values in the range $$[0, 1]$$. In addition, we would like large values of $$f_\\hat{\\boldsymbol{\\theta}}(\\textbf{x})$$ to correspond to high probabilities and small values to low probabilities.\n\n## 23.2.2. The Logistic Function¶\n\nTo accomplish this, we introduce the logistic function, often called the sigmoid function:\n\n\\begin{aligned} \\sigma(t) = \\frac{1}{1 + e^{-t}} \\end{aligned}\n\nFor ease of reading, we often replace $$e^x$$ with $$\\text{exp}(x)$$ and write:\n\n\\begin{aligned} \\sigma (t) = \\frac{1}{1 + \\text{exp}(-t)} \\end{aligned}\n\nWe plot the sigmoid function for values of $$t \\in [-10, 10]$$ below.\n\nfrom scipy.special import expit\nxs = np.linspace(-10, 10, 100)\nys = expit(xs)\nplt.plot(xs, ys)\nplt.title(r'Sigmoid Function')\nplt.xlabel('$t$')\nplt.ylabel(r'$\\sigma(t)$');", null, "Observe that the sigmoid function $$\\sigma(t)$$ takes in any real number $$\\mathbb{R}$$ and outputs only numbers between 0 and 1. The function is monotonically increasing on its input $$t$$; large values of $$t$$ correspond to values closer to 1, as desired. This is not a coincidence—the sigmoid function may be derived from a log ratio of probabilities, although we omit the derivation for brevity.\n\n## 23.2.3. Logistic Model Definition¶\n\nWe may now take our linear model $$\\hat{\\boldsymbol{\\theta}} \\cdot \\textbf{x}$$ and use it as the input to the sigmoid function to create the logistic model:\n\n\\begin{aligned} f_\\hat{\\boldsymbol{\\theta}} (\\textbf{x}) = \\sigma(\\hat{\\boldsymbol{\\theta}} \\cdot \\textbf{x}) \\end{aligned}\n\nIn other words, we take the output of linear regression—any number in $$\\mathbb{R}$$— and use the sigmoid function to restrict the model’s final output to be a valid probability between zero and one.\n\nTo develop some intuition for how the logistic model behaves, we restrict $$x$$ to be a scalar and plot the logistic model’s output for several values of $$\\hat{\\theta}$$.\n\ndef flatten(li): return [item for sub in li for item in sub]\n\nthetas = [-2, -1, -0.5, 2, 1, 0.5]\nxs = np.linspace(-10, 10, 100)\n\nfig, axes = plt.subplots(2, 3, sharex=True, sharey=True, figsize=(10, 6))\nfor ax, theta in zip(flatten(axes), thetas):\nys = expit(theta * xs)\nax.plot(xs, ys)\nax.set_title(r'$\\hat{\\theta} =$' + str(theta))\n\n# add a big axes, hide frame\nfig.add_subplot(111, frameon=False)\n# hide tick and tick label of the big axes\nplt.tick_params(labelcolor='none', top='off', bottom='off',\nleft='off', right='off')\nplt.grid(False)\nplt.xlabel('$x$')\nplt.ylabel(r'$f_\\hat{\\theta}(x)$')\nplt.tight_layout()", null, "We see that changing the magnitude of $$\\hat{\\theta}$$ changes the sharpness of the curve; the further away from $$0$$, the sharper the curve. Flipping the sign of $$\\hat{\\theta}$$ while keeping magnitude constant is equivalent to reflecting the curve over the y-axis.\n\n## 23.2.4. Summary¶\n\nWe introduce the logistic model, a new prediction function that outputs probabilities. To construct the model, we use the output of linear regression as the input to the nonlinear logistic function." ]
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https://www.olympiadsuccess.com/courses/sof/international-mathematics-olympiad
[ "International Mathematics Olympiad(IMO) IMO Preparation Materials and Sample Papers for class 3,4,5,6,7,8,9,10\n\n#### Unified Council", null, "We are providing complete preparation guide for SOF IMO exams through multiple sample papers, practice papers & mock test papers for classes 1, 2, 3, 4, 5, 6, 7, 8, 9 and 10.\n\nBuy Level 1 & 2 Practice Papers\n\nOne of the popular Math Olympiad, conducted by SOF, the IMO is conducted at two levels\n\nLevel 1: The first level of the exam is organized in the respective schools of the participants during school hours only.\n\n• The Level 1 exam is an objective-type test having duration of 60 minutes comprising of 35 objective-type questions for classes 1 to 4 and 50 objective-type questions for classes 5 to 12.\n\n• The exam consists of four sections:\n\n• Section-1: Logical Reasoning\n\n• Section-2: Mathematical Reasoning\n\n• Section-3: Everyday Mathematics\n\n• Section-4: Achievers Section\n\n• There are separate question papers for each and every class.\n\n• The medium of the exam is English.\n\n• CBSE, ICSE/ISC and other State Board syllabus is followed for the setting of test papers.\n\n• The exam is conducted during school hours only\n\nLevel 2: The Level 2 is conducted for students of classes 3 to 12. The qualifiers to second round would include the following:\n\n• Top 5% of candidates class wise that appear for the 1st level exam. Due weightage to marks scored in different sections will be given. Each section is accorded with a separate weightage.\n• Zone wise top 25 rank holders class wise.\n• Class topper where at least 10 students from a class appear in the exam & have scored 50% qualifying marks.\n\nSOF IMO Syllabus and Marking Scheme\n\n Class Section No. of Questions Marks/Question Total Marks 1 to 4 Logical Reasoning 10 1 10 Mathematical Reasoning 10 1 10 Everyday Mathematics 10 1 10 Achievers Section 5 2 10 Grand Total 35 40 5 to 12 Logical Reasoning 15 1 15 Mathematical Reasoning 20 1 20 Everyday Mathematics 10 1 10 Achievers Section 5 3 15 Grand Total 50 60\n\nLearn How to Prepare for IMO\n\nSOF IMO Schedule for 2019-2020 examination\n\nThe exam will be held on 5th & 17th December 2019.\n\nBenefits\n\n• SOF IMO build some, but far from all, of the skills required to master at mathematical research.\n• SOF IMO make participants into very sharp-minded and so they are able to solve clever problems (which, perhaps, have some advantages in some contexts in research).\n\nCheck Class-wise Syllabus here:\n\n#### Class 1\n\nSection – 1 : Patterns, Odd One Out, Measuring Units, Geometrical Shapes, Spatial Understanding, Grouping, Analogy, Ranking Test, Problems based on Figures.\n\nSection – 2 : Numerals, Number names, Number Sense (2 digit numbers), Addition, Subtraction, Lengths, Weights and Comparisons, Time, Money, Geometrical Shapes and Solids, Patterns.\n\nSection – 3 : Syllabus as per Section–1 and 2.\n\nSection – 4 : Higher Order Thinking Questions - Syllabus as per Section–1 and 2.\n\nWhat we Offer?\n\n• Comprehensive Test Series: 60+ worksheets + 10+ mock test papers\n• Mock Test Series: 10+ mock test papers (IMO Mock Test Papers are based on Previous Year question papers for Class 1)\n\n* 20+ logical reasoning worksheets complimentary for every subscriber\n\n#### Class 2\n\nSection – 1 : Patterns, Odd One Out, Measuring Units, Geometrical Shapes, Analogy, Ranking Test, Grouping of Figures, Embedded Figures, Coding-Decoding.\n\nSection – 2 : Numerals, number names and Number Sense (3-Digit Numbers), Computation Operations, Length, Weight, Capacity, Time, Temperature, Money, Lines, Shapes and Solids, Pictographs, Patterns.\n\nSection – 3 : Syllabus same as Section 2.\n\nSection – 4 : Higher Order Thinking Questions - Syllabus as per Section 2.\n\nWhat we Offer?\n\n• Comprehensive Test Series: 60+ worksheets + 10+ mock test papers\n• Mock Test Series: 10+ mock test papers (IMO Mock Test Papers are based on Previous Year question papers for Class 2)\n\n* 20+ logical reasoning worksheets complimentary for every subscriber\n\n#### Class 3\n\nSection – 1 : Patterns, Analogy and Classification, Alphabet Test, Coding-Decoding, Ranking Test, Grouping of Figures and Figure Matrix, Mirror Images, Geometrical Shapes, Embedded Figures, Days and Dates & Possible Combinations.\n\nSection – 2 : Numerals, Number names and Number Sense (4-digit numbers), Computation Operations, Fractions, Length, Weight, Capacity, Temperature, Time, Money, Geometry, Data Handling.\n\nSection – 3 : The Syllabus of this section will be based on the Syllabus of Mathematical Reasoning.\n\nSection – 4 : Higher Order Thinking Questions - Syllabus as per Section – 2.\n\nWhat we Offer?\n\n• Comprehensive Test Series: 60+ worksheets + 10+ mock test papers\n• Mock Test Series: 10+ mock test papers (IMO Mock Test Papers are based on Previous Year question papers for Class 3)\n\n* 20+ logical reasoning worksheets complimentary for every subscriber\n\n#### Class 4\n\nSection – 1 : Patterns, Alphabet Test, Coding-Decoding, Ranking Test, Mirror Images, Geometrical Shapes and Solids, Embedded Figures, Direction Sense Test, Days and Dates & Possible Combinations, Analogy and Classification.\n\nSection – 2 : Numerals and Number Names, Number Sense (5-digit numbers), Computation Operations, Fractions, Length, Weight, Capacity, Time, Money, Geometry, Perimeter of Various Shapes, Symmetry, Conversions, Data Handling\n\nSection – 3 : The Syllabus of this section will be based on the Syllabus of Mathematical Reasoning.\n\nSection – 4 : Higher Order Thinking Questions - Syllabus as per Section 2.\n\nWhat we Offer?\n\n• Comprehensive Test Series: 60+ worksheets + 10+ mock test papers\n• Mock Test Series: 10+ mock test papers (IMO Mock Test Papers are based on Previous Year question papers for Class 4)\n\n* 20+ logical reasoning worksheets complimentary for every subscriber\n\n#### Class 5\n\nSection – 1 : Patterns, Analogy and Classification, Geometrical Shapes, Mirror and Water Images, Direction Sense Test, Ranking Test, Alphabet Test, Logical Sequence of Words, Puzzle Test, Coding-Decoding.\n\nSection – 2 : Numerals, Number names and Number Sense (7 and 8 digit numbers), Computation Operations, Fractions and Decimals, Measurement of Length, Weight, Capacity, Volume, Time, Temperature and Money, Conversions, Geometrical Shapes and Solids, Angles, Perimeter of Various Shapes & Area of Rectangle and Square, Symmetry, Data Handling\n\nSection – 3 : The Syllabus of this section will be based on the Syllabus of Mathematical Reasoning.\n\nSection – 4 : Higher Order Thinking Questions - Syllabus as per Section 2.\n\nWhat we Offer?\n\n• Comprehensive Test Series: 60+ worksheets + 10+ mock test papers\n• Mock Test Series: 10+ mock test papers (IMO Mock Test Papers are based on Previous Year question papers for Class 5)\n\n* 20+ logical reasoning worksheets complimentary for every subscriber\n\n#### Class 6\n\nSection – 1 : Verbal and Non-Verbal Reasoning.\n\nSection – 2 : Knowing our Numbers, Whole Numbers, Playing with Numbers, Basic Geometrical Ideas, Understanding Elementary Shapes, Integers, Fractions, Decimals, Data Handling, Mensuration, Algebra, Ratio And Proportion, Symmetry, Practical Geometry\n\nSection – 3 : The Syllabus of this section will be based on the syllabus of Mathematical Reasoning.\n\nSection – 4 : Higher Order Thinking Questions - Syllabus as per Section – 2.\n\nWhat we Offer?\n\n• Comprehensive Test Series: 60+ worksheets + 10+ mock test papers\n• Mock Test Series: 10+ mock test papers (IMO Mock Test Papers are based on Previous Year question papers for Class 6)\n\n* 20+ logical reasoning worksheets complimentary for every subscriber\n\n#### Class 7\n\nSection – 1 : Verbal and Non-Verbal Reasoning.\n\nSection – 2 : Integers, Fractions and Decimals, Exponents and Powers, Algebraic Expressions, Simple Linear Equations, Lines and Angles, Comparing Quantities, The Triangle and its Properties, Symmetry, Congruence of Triangles, Rational Numbers, Perimeter and Area,  Data Handling, Visualizing Solid Shapes, Practical Geometry.\n\nSection – 3 : The Syllabus of this section will be based on the syllabus of Mathematical Reasoning.\n\nSection – 4 : Higher Order Thinking Questions - Syllabus as per Section – 2.\n\nWhat we Offer?\n\n• Comprehensive Test Series: 60+ worksheets + 10+ mock test papers\n• Mock Test Series: 10+ mock test papers (IMO Mock Test Papers are based on Previous Year question papers for Class 7)\n\n* 20+ logical reasoning worksheets complimentary for every subscriber\n\n#### Class 8\n\nSection – 1 : Verbal and Non-Verbal Reasoning.\n\nSection – 2 : Rational Numbers, Squares and Square Roots, Cubes and Cube Roots, Exponents and Powers, Comparing Quantities, Algebraic Expressions and  Identities, Linear Equations in One Variable, Understanding Quadrilaterals, Constructions, Mensuration, Visualizing Solid Shapes, Data Handling, Direct and Inverse Variations, Factorization, Introduction to Graphs, Playing with Numbers.\n\nSection – 3 : The Syllabus of this section will be based on the syllabus of Mathematical Reasoning.\n\nSection – 4 : Higher Order Thinking Questions - Syllabus as per Section – 2.\n\nWhat we Offer?\n\n• Comprehensive Test Series: 60+ worksheets + 10+ mock test papers\n• Mock Test Series: 10+ mock test papers (IMO Mock Test Papers are based on Previous Year question papers for Class 8)\n\n* 20+ logical reasoning worksheets complimentary for every subscriber\n\n#### Class 9\n\nSection – 1 : Verbal and Non-Verbal Reasoning.\n\nSection – 2 : Number Systems, Polynomials, Coordinate Geometry, Linear Equations in Two Variables, Introduction to Euclid’s Geometry, Lines and Angles, Triangles, Quadrilaterals, Areas of Parallelograms and Triangles, Circles, Constructions, Heron’s Formula, Surface Areas and Volumes, Statistics, Probability.\n\nSection – 3 : The syllabus of this section will be based on the syllabus of Mathematical Reasoning and Quantitative Aptitude.\n\nSection – 4 : Higher Order Thinking Questions - Syllabus as per Section – 2.\n\nWhat we Offer?\n\n• Comprehensive Test Series: 60+ worksheets + 10+ mock test papers\n• Mock Test Series: 10+ mock test papers (IMO Mock Test Papers are based on Previous Year question papers for Class 9)\n\n* 20+ logical reasoning worksheets complimentary for every subscriber\n\n#### Class 10\n\nSection – 1 : Verbal and Non-Verbal Reasoning.\n\nSection – 2 : Real Numbers, Polynomials, Pair of Linear Equations in Two Variables, Quadratic Equations, Arithmetic Progressions, Triangles, Coordinate Geometry, Introduction to Trigonometry, Some Applications of Trigonometry, Circles, Constructions, Areas Related to Circles, Surface Areas and Volumes, Statistics, Probability.\n\nSection – 3 : The Syllabus of this section will be based on the syllabus of Mathematical Reasoning and Quantitative Aptitude.\n\nSection – 4 : Higher Order Thinking Questions - Syllabus as per Section – 2.\n\nWhat we Offer?\n\n• Comprehensive Test Series: 60+ worksheets + 10+ mock test papers\n• Mock Test Series: 10+ mock test papers (IMO Mock Test Papers are based on Previous Year question papers for Class 10)\n\n* 20+ logical reasoning worksheets complimentary for every subscriber" ]
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http://www.softmath.com/math-com-calculator/radical-inequalities/lowest-common-denominator.html
[ "English | Español\n\n# Try our Free Online Math Solver!", null, "Online Math Solver\n\n Depdendent Variable\n\n Number of equations to solve: 23456789\n Equ. #1:\n Equ. #2:\n\n Equ. #3:\n\n Equ. #4:\n\n Equ. #5:\n\n Equ. #6:\n\n Equ. #7:\n\n Equ. #8:\n\n Equ. #9:\n\n Solve for:\n\n Dependent Variable\n\n Number of inequalities to solve: 23456789\n Ineq. #1:\n Ineq. #2:\n\n Ineq. #3:\n\n Ineq. #4:\n\n Ineq. #5:\n\n Ineq. #6:\n\n Ineq. #7:\n\n Ineq. #8:\n\n Ineq. #9:\n\n Solve for:\n\n Please use this form if you would like to have this math solver on your website, free of charge. Name: Email: Your Website: Msg:\n\nSearch Engine visitors came to this page yesterday by using these math terms :\n\nEquations with restrictions, maths test bbc yr.8, simplifying quadratics + square roots, subtracting worksheets fifth grade, write 0.89 as a fraction.\n\nSimplifying cube roots, mcdougal littell algebra 1 answers free, how do you solve problems with a little x and y on a calculator.\n\nTrinomials math homework help, FREE BOOKS MATLAB 7, \"Penny Doubled\" mathematical formula, Free Math Solver, explanation add and subtract exponents, prentice hall answers.\n\nHow to graph ellipses in a scientific calculator, 2 different kinds of examples of linear programing for solving of everyday problems, help with hyperbolas.\n\nCompatible numbers and third grade math, binomial equations, square root fraction solver, pythagoras+programma+ti 84, how to solve a fraction equation with variables, algebra 2 probability hands on.\n\nBbc bitesize worksheets, worksheet about add and subtract 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[ null, "http://www.softmath.com/images/video-pages/solver-top.png", null ]
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https://www.tensorflow.org/versions/r2.1/api_docs/python/tf/keras/losses/SquaredHinge?hl=he
[ "# tf.keras.losses.SquaredHinge\n\nComputes the squared hinge loss between `y_true` and `y_pred`.\n\n`loss = square(maximum(1 - y_true * y_pred, 0))`\n\n`y_true` values are expected to be -1 or 1. If binary (0 or 1) labels are provided we will convert them to -1 or 1.\n\n#### Usage:\n\n``````sh = tf.keras.losses.SquaredHinge()\nloss = sh([-1., 1., 1.], [0.6, -0.7, -0.5])\n\n# loss = (max(0, 1 - y_true * y_pred))^2 = [1.6^2 + 1.7^2 + 1.5^2] / 3\n\nprint('Loss: ', loss.numpy()) # Loss: 2.566666\n``````\n\nUsage with the `compile` API:\n\n``````model = tf.keras.Model(inputs, outputs)\nmodel.compile('sgd', loss=tf.keras.losses.SquaredHinge())\n``````\n\n## Methods\n\n### `from_config`\n\nView source\n\nInstantiates a `Loss` from its config (output of `get_config()`).\n\nArgs\n`config` Output of `get_config()`.\n\nReturns\nA `Loss` instance.\n\nView source\n\n### `__call__`\n\nView source\n\nInvokes the `Loss` instance.\n\nArgs\n`y_true` Ground truth values. shape = `[batch_size, d0, .. dN]`\n`y_pred` The predicted values. shape = `[batch_size, d0, .. dN]`\n`sample_weight` Optional `sample_weight` acts as a coefficient for the loss. If a scalar is provided, then the loss is simply scaled by the given value. If `sample_weight` is a tensor of size `[batch_size]`, then the total loss for each sample of the batch is rescaled by the corresponding element in the `sample_weight` vector. If the shape of `sample_weight` is `[batch_size, d0, .. dN-1]` (or can be broadcasted to this shape), then each loss element of `y_pred` is scaled by the corresponding value of `sample_weight`. (Note on`dN-1`: all loss functions reduce by 1 dimension, usually axis=-1.)\n\nReturns\nWeighted loss float `Tensor`. If `reduction` is `NONE`, this has shape `[batch_size, d0, .. dN-1]`; otherwise, it is scalar. (Note `dN-1` because all loss functions reduce by 1 dimension, usually axis=-1.)\n\nRaises\n`ValueError` If the shape of `sample_weight` is invalid.\n\n[{ \"type\": \"thumb-down\", \"id\": \"missingTheInformationINeed\", \"label\":\"Missing the information I need\" },{ \"type\": \"thumb-down\", \"id\": \"tooComplicatedTooManySteps\", \"label\":\"Too complicated / too many steps\" },{ \"type\": \"thumb-down\", \"id\": \"outOfDate\", \"label\":\"Out of date\" },{ \"type\": \"thumb-down\", \"id\": \"samplesCodeIssue\", \"label\":\"Samples / code issue\" },{ \"type\": \"thumb-down\", \"id\": \"otherDown\", \"label\":\"Other\" }]\n[{ \"type\": \"thumb-up\", \"id\": \"easyToUnderstand\", \"label\":\"Easy to understand\" },{ \"type\": \"thumb-up\", \"id\": \"solvedMyProblem\", \"label\":\"Solved my problem\" },{ \"type\": \"thumb-up\", \"id\": \"otherUp\", \"label\":\"Other\" }]" ]
[ null ]
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https://math.answers.com/Q/What_is_the_volume_of_50_cm_25cm_and_16_cm
[ "", null, "", null, "", null, "", null, "0\n\n# What is the volume of 50 cm 25cm and 16 cm?\n\nUpdated: 9/26/2023", null, "Wiki User\n\n6y ago\n\nBe notified when an answer is posted", null, "Earn +20 pts\nQ: What is the volume of 50 cm 25cm and 16 cm?\nSubmit\nStill have questions?", null, "", null, "Related questions\n\n### What is the volume of a cube with 25 cm sides?\n\nVolume = length*width*height, which for the 25cm cube are all 25 cm. Vol = 25cm * 25cm * 25cm = 15625 cubic cm = 15.625 cubic decimetres = 15.625 litres.\n\n### What is the volume of a block 50 cm long 25 cm high and 16 cm wide?\n\nVolume of block: 50*25*16 = 20,000 cubic cm\n\n### What is the volume of a sphere with the diameter of 25 cm?\n\nThe volume of a sphere with a diameter of 25cm is about 8181.2cm3\n\n### Which is longer 25cm or 200mm?\n\n25cm is longer than 200mm which equals 20cm\n\n### How do you find the height of a box when the volume is 100 cm and the area of the bottom is 50 square cm?\n\nVolume = area x height volume is 100 cm cubed height = volume/area = 100/50 = 2 cm\n\n25cm\n\n15625 cubic cm\n\n### 0.5m plus 25cm equals cm?\n\nHalf a meter is equal to 50 centimeters. 50 centimeters plus 25 centimeters is equal to 75 centimeters.\n\n15625 cubic cm\n\n### How many cm in a 0.25 meters?\n\nOne meter is 100cm so a quarter of that is 25cm. There is 25cm in 0.25m.\n\n### What is the volume of a box that has 50 cm sq anda base of 35 cm?\n\nIf the box had a 50 cm square transverse section and the third dimension were 35 cm, the volume would be:50 &times; 50 &times; 35 = 87500 cubic centimeters or eighty seven and a half liters\n\n~35.36 cm" ]
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https://stats.stackexchange.com/questions/566994/glrt-of-exponential-distribution-and-critical-region/567011
[ "# GLRT of exponential distribution and critical region\n\nFind the Generalized likelihood ratio test (GLRT) for $$H_0: \\lambda = \\lambda_0$$ when $$H_A: \\lambda \\ne \\lambda_0$$ for $$X_1 ... X_n$$ taken from $$X \\sim Exp(\\lambda;x)$$, with a test size of $$0.06$$, obtain the critical region.\n\nHere's what I have tried:\n\n$$L(\\lambda_0;x) = \\prod_{i=1}^nf(x_i;\\lambda_0) = \\prod_{i=1}^n\\lambda_0 e^{-\\lambda_0 x_i}=\\lambda_0^ne^{-\\lambda_0 \\sum_{i=1}^nx_i}$$\n\n$$\\mathbf{L}(\\lambda_0;x) = \\log L(\\lambda_0;x) = n\\log(\\lambda_0) - \\lambda_0\\sum_{i=1}^nx_i$$\n\n$$\\frac{\\partial\\mathbf{L}(\\lambda_0;x)}{\\partial\\lambda_0} = \\frac{n}{\\lambda_0}-\\sum_{i=1}^nx_i \\implies \\frac{n}{\\lambda_0}-\\sum_{i=1}^nx_i=0 \\implies \\lambda_0 = \\frac{1}{\\bar{x}}$$\n\n$$\\mathbf{L}(\\hat{\\lambda};x) = \\left(\\frac{1}{\\bar{x}}\\right)^ne^{-\\left(\\frac{1}{\\bar{x}} \\right) \\sum_{i=1}^nx_i}$$\n\nThen applying the likelihood ratio:\n\n$$\\Lambda :=\\frac{L(\\lambda_0;x)}{\\mathbf{L}(\\hat{\\lambda};x)} = \\frac{\\lambda_0 ^ne^{-\\lambda_0 \\sum_{i=1}^nx_i}}{\\left(\\frac{1}{\\bar{x}}\\right)^ne^{-\\left(\\frac{1}{\\bar{x}} \\right) \\sum_{i=1}^nx_i}}= \\left(\\bar{x}\\lambda_0 e^{1-\\lambda_0\\bar{x}} \\right)^n$$\n\nWe can find the critical region by:\n\n\\begin{align} C &= \\{x : \\lambda \\le k\\} \\\\ &= \\{x : \\left(\\bar{x}\\lambda_0 e^{1-\\lambda_0\\bar{x}} \\right)^n \\le k\\} \\\\ \\end{align}\n\nHowever, I am unsure on how to proceed from here to obtain the critical region/\n\nEdit:\n\nI have been doing further reading and it seems that the critical region can be found by the following, Wilks Theorem $$-2\\log(\\Lambda) \\approx \\chi^2_{1, 1-\\alpha}$$\n\nAnd as such: \\begin{align} -2\\log(\\Lambda) &= -2n\\log\\left(\\bar{x}\\lambda_0 e^{1-\\lambda_0\\bar{x}} \\right) \\\\ &= -2n \\left(\\log(\\bar{x})+\\log(\\lambda_0) + 1-\\lambda_0\\bar{x} \\right) \\le \\chi^2_{1, 0.94} = 0.2571744 \\\\ &= \\log(\\bar{x})+\\log(\\lambda_0) + 1-\\lambda_0\\bar{x} \\ge -\\frac{\\chi^2_{1, 0.94}}{2n} \\end{align}\n\n[Not enough reputation to comment, so I write in an answer]\n\nHint: consider the function $$g(y)=y\\lambda_0e^{1-\\lambda_0 y}$$ for $$y>0$$. Take the derivative to help draw the curve. You'll find a region of $$y$$ such that $$g(y)\\le k^{1/n}$$ by drawing a horizontal line intersecting the curve. After getting a form of the region based on $$y$$, you can forget about $$k$$, and determine the boundary (intersection points of the horizontal line and the curve) using the distribution of $$y$$. Here $$y$$ is your $$\\bar{x}$$.\n\nBy the way, $$\\lambda_0$$ is a specific value of $$\\lambda$$ and it's generally not recommended to write $$\\hat{\\lambda}_0$$, because there is nothing unknown to estimate. Instead, I'll write $$\\hat{\\lambda}$$ as the value that maximizes your log-likelihood function $$\\mathbf{L}(\\lambda;x)$$. The likelihood ratio has nothing to do with the parameter $$\\lambda$$ of the exponential distribution, so I'll suggest using another letter, say $$\\Lambda := \\frac{L(\\lambda_0;x)}{L(\\hat{\\lambda};x)}$$, where the denominator is the likelihood function evaluated at $$\\hat{\\lambda}$$, not $$\\mathbf{L}(\\hat{\\lambda};x)$$.\n\n• Thanks for the hint, I'll look into it some further. I have edited my post from a reading, not sure if you're familiar with it? I might have got it totally wrong though. Also, thanks for the tips on notation also. I'll make an update later today on your hint and will upload it to my post for progress. Mar 8 at 16:24\n• I have taking the first derivative and I get $e^{1-\\lambda_0 y}(2-\\lambda_0 y)$ by setting this equal to $0$ I find that I get $\\bar{x} = y = \\frac{2}{\\lambda_0}$ how do I proceed from here? Mar 8 at 16:36\n• @dollarbill Are you familiar with drawing the function curve with the help of derivatives? You got the first derivative, which contains some important information about the function. The first part, $e^{1-\\lambda_0y}$, is always positive, so the sign of $g'$ is solely determined by the second part, $2-\\lambda_0 y$, where $\\lambda_0>0$. Then you can see that $g'(y)>0$ for all $0<y<2/\\lambda_0$, and $g'(y)\\le 0$ otherwise. What do these tell you about the shape of $g$?\n– Min\nMar 9 at 7:01\n• @dollarbill About your update. That is the asymptotic distribution of $-2\\log\\Lambda$, which approximately holds when you have a finite sample. In this case, actually, you can derive an exact distribution, which is true for any finite sample size.\n– Min\nMar 9 at 7:04\n• @dollarbill In addition, you may confuse a distribution itself with critical values under a distribution. $-2\\log\\Lambda\\overset{approx.}{\\sim} \\chi^2_1$, where $\\sim$ means the random variable on the left side follows a distribution whose name is indicated on the right, and the critical region is the set of all viable values of $\\bar{x}$ such that $-2\\log\\Lambda\\ge \\chi^2_{1,\\alpha}$.\n– Min\nMar 9 at 7:15" ]
[ null ]
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https://drmf-beta.wmflabs.org/wiki/Formula:KLS:01.13:15
[ "# Formula:KLS:01.13:15\n\n${\\displaystyle{\\displaystyle{\\displaystyle\\qHyperrphis{2}{1}@@{q^{-n},b}{c}{q}% {z}=\\frac{\\left(b;q\\right)_{n}}{\\left(c;q\\right)_{n}}q^{-n-\\binomial{n}{2}}(-z% )^{n}\\ \\qHyperrphis{2}{1}@@{q^{-n},c^{-1}q^{1-n}}{b^{-1}q^{1-n}}{q}{\\frac{cq^{% n+1}}{bz}}}}}$", null, "## Proof\n\nWe ask users to provide proof(s), reference(s) to proof(s), or further clarification on the proof(s) in this space." ]
[ null, "https://drmf-beta.wmflabs.org/index.php", null ]
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https://socratic.org/questions/find-the-function-values-of-cos-tan-sec-csc-and-cot#551189
[ "# Find the function values of cos θ, tan θ, sec θ, csc θ and cot θ ?\n\n## If sin θ = −(4)/(5) and cos θ < 0, in which quadrant is θ? Find the function values of cos θ, tan θ, sec θ, csc θ and cot θ.\n\nFeb 13, 2018\n\nGiven that, sin θ = (−4)/(5)\n\napplying the identity, ${\\sin}^{2} \\theta + {\\cos}^{2} \\theta = 1$\n\n${\\cos}^{2} \\theta = 1 - {\\sin}^{2} \\theta$\n\n${\\cos}^{2} \\theta = 1 - {\\left(\\frac{- 4}{5}\\right)}^{2}$\n\n${\\cos}^{2} \\theta = 1 - \\frac{16}{25} = \\frac{9}{25}$\n\n$\\cos \\theta = \\sqrt{\\frac{9}{25}} = \\pm \\frac{3}{5}$\n\nits given that, cos θ < 0 ; color(magenta)(costheta =(-3)/5\nSince, both $\\sin \\theta$ and $\\cos \\theta$ are negative, $\\theta$ lies in the $\\textcolor{red}{\\text{third quadrant}}$.\n\n$\\tan \\theta = \\sin \\frac{\\theta}{\\cos} \\theta$\n=(-4)/5 xx 5/(-3) => color(magenta)(tantheta= 4/3\n\nsec θ = 1/costheta => color(magenta)(sec theta=(-5)/3\n\ncsc θ = 1/sintheta => color(magenta)(csctheta = (-5)/4\n\ncottheta = costheta/sintheta = 1/tantheta => color(magenta)(cottheta=3/4" ]
[ null ]
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https://moam.info/biomedical-engineering-online-biomedsearch_5c5cae76097c478d4f8b4594.html
[ "## BioMedical Engineering OnLine - BioMedSearch\n\nOct 27, 2005 - Open Access. Research. Reliability of old and new ventricular fibrillation detection ... http://www.biomedical-engineering-online.com/content/4/1/60. Page 2 of 15 ...... \"BioMed Central will be the most significant development for.\n\nBioMedical Engineering OnLine\n\nBioMed Central\n\nOpen Access\n\nResearch\n\nReliability of old and new ventricular fibrillation detection algorithms for automated external defibrillators Anton Amann*1, Robert Tratnig2 and Karl Unterkofler*2 Address: 1Innsbruck Medical University, Department of Anesthesia and General Intensive Care, Anichstr. 35, A-6020 Innsbruck, Austria and Department of Environmental Sciences, ETH-Hönggerberg, CH-8093 Zürich, Switzerland and 2Research Center PPE, FH-Vorarlberg, Achstr. 1, A6850 Dornbirn, Austria Email: Anton Amann* - [email protected]; Robert Tratnig - [email protected]; Karl Unterkofler* - [email protected] * Corresponding authors\n\nPublished: 27 October 2005 BioMedical Engineering OnLine 2005, 4:60\n\ndoi:10.1186/1475-925X-4-60\n\nReceived: 06 May 2005 Accepted: 27 October 2005\n\nventricular fibrillation detectionautomated external defibrillator (AED)ventricular fibrillation (VF)sinus rhythm (SR)ECG analysis\n\nAbstract Background: A pivotal component in automated external defibrillators (AEDs) is the detection of ventricular fibrillation by means of appropriate detection algorithms. In scientific literature there exists a wide variety of methods and ideas for handling this task. These algorithms should have a high detection quality, be easily implementable, and work in real time in an AED. Testing of these algorithms should be done by using a large amount of annotated data under equal conditions. Methods: For our investigation we simulated a continuous analysis by selecting the data in steps of one second without any preselection. We used the complete BIH-MIT arrhythmia database, the CU database, and the files 7001 – 8210 of the AHA database. All algorithms were tested under equal conditions. Results: For 5 well-known standard and 5 new ventricular fibrillation detection algorithms we calculated the sensitivity, specificity, and the area under their receiver operating characteristic. In addition, two QRS detection algorithms were included. These results are based on approximately 330 000 decisions (per algorithm). Conclusion: Our values for sensitivity and specificity differ from earlier investigations since we used no preselection. The best algorithm is a new one, presented here for the first time.\n\nBackground Sudden cardiac arrest is a major public health problem and one of the leading causes of mortality in the western world. In most cases, the mechanism of onset is a ventricular tachycardia that rapidly progresses to ventricular fibrillation . Approximately one third of these patients\n\ncould survive with the timely employment of a defibrillator. Besides manual defibrillation by an emergency paramedic, bystander defibrillation with (semi-)automatic external defibrillators (AEDs) has also been recommended for resuscitation. These devices analyze the\n\nPage 1 of 15 (page number not for citation purposes)\n\nelectrocardiogram (ECG) of the patient and recognize whether a shock should be delivered or not, as, e.g., in case of ventricular fibrillation (VF). It is of vital importance that the ECG analysis system used by AEDs differentiates well between VF and a stable but fast sinus rhythm (SR). An AED should not deliver a shock to a collapsed patient not in cardiac arrest. On the other hand, a successfully defibrillated patient should not be defibrillated again. The basis of such ECG analysis systems of AEDs is one or several mathematical ECG analysis algorithms. The main purpose of this paper is to compare various old and new algorithms in a standardized way. To gain insight into the quality of an algorithm for ECG analysis, it is essential to test the algorithms under equal conditions with a large amount of data, which has already been commented on by qualified cardiologists. Commonly used annotated databases are Boston's Beth Israel Hospital and MIT arrhythmia database (BIH-MIT), the Creighton University ventricular tachyarrhythmia database (CU), and the American Heart Association database (AHA). We used the complete CU and BIH-MIT arrhythmia database, and the files 7001 – 8210 of the AHA database, , [3,4]. For each algorithm approximately 330 000 decisions had been calculated. No preselection of certain ECG episodes was made, which mimics the situation of a bystander more accurately. In this investigation we analyzed 5 well-known standard and 5 new ventricular fibrillation detection algorithms. In addition, two QRS detection algorithms were included. The results are expressed in the quality parameters Sensitivity and Specificity. In addition to these two parameters, we calculated the Positive Predictivity and Accuracy of the investigated algorithms. Furthermore, the calculation time in comparison to the duration of the real data was calculated for the different algorithms. The calculation times were obtained by analyzing data from the CU database only. The quality parameters were obtained by comparing the VF/no VF decisions suggested by the algorithm with the annotated decisions suggested by cardiologists. The cardiologists' decisions are considered to be correct. We distinguished only between ventricular fibrillation and no ventricular fibrillation, since the annotations do not include a differentiation between ventricular fibrillation and ventricular tachycardia. The closer the quality parameters are to 100%, the better the algorithm works. Since an AED has to differentiate between VF and no VF, the sensitivity and specificity are the appropriate parameters. To represent the quality of an algorithm by its sensitivity and specificity bears some problems. A special algorithm can\n\nhttp://www.biomedical-engineering-online.com/content/4/1/60\n\n100\n\n80 Sensitivity / per cent\n\nBioMedical Engineering OnLine 2005, 4:60\n\n60\n\n40\n\n20\n\n0\n\n0\n\n20\n\n40\n\n60\n\n80\n\n100\n\n(1−Specificity) / per cent\n\nFigureof Receiver plexity length measure\" 1operating 8s described characteristic in the for introduction, the algorithm for a\"comwindow Receiver operating characteristic for the algorithm \"complexity measure\" described in the introduction, for a window length of 8 s. The calculated value for the area under the curve, IROC, is 0.87.\n\nhave a high sensitivity, but a low specificity, or conversely. Which one is better? To arrive at a common and single quality parameter, we use the receiver operating characteristic (ROC). The sensitivity is plotted in dependence of (1 - specificity), where different points in the plot are obtained by varying the critical threshold parameter in the decision stage of the algorithm. By calculating the area under the ROC curve (we call this value \"integrated receiver operating characteristic\", and denote it by IROC), it is possible to compare different algorithms by one single value. Figure 1 shows a typical example of an ROC curve. Section 1 provides the necessary background for the algorithms under investigation. Section 2 describes the methods of evaluation and represents our results in Table 1, 2, 3 and Figure 5 and 6. A discussion of the results follows in Section 3. Appendix A recalls the basic definitions of the quality parameters Sensitivity, Specificity, Positive Predictivity, Accuracy, and ROC curve. In Appendix B we provide more details on one of the new algorithms.\n\n1 Methods The ventricular fibrillation detection algorithms considered here are partly taken from the scientific literature, five of them are new. Some of them have been evaluated in and . For all algorithms we used the same prefiltering process. First, a moving average filter of order 5 is applied to the\n\nPage 2 of 15 (page number not for citation purposes)\n\nBioMedical Engineering OnLine 2005, 4:60\n\nhttp://www.biomedical-engineering-online.com/content/4/1/60\n\nTable 1: >Quality of ventricular fibrillation detection algorithms (sensitivity (Sns), specificity (Spc), integrated receiver operating characteristic (IROC)) in per cent, rounded on 3 significant digits, wl = window length in seconds. (*) ... no appropriate parameter exists.\n\nData Source\n\nMIT DB\n\nParameter\n\nwl\n\nTCI TCI ACF95 ACF99 VF VF SPEC CPLX STE MEA SCA WVL1 WVL2 LI TOMP\n\n3 8 8 8 4 8 8 8 8 8 8 8 8 8 8\n\nSns. 82.5 74.5 33.2 59.4 36.7 29.4 23.1 6.3 54.5 62.9 72.4 28.7 81.1 3.1 68.5\n\nCU DB\n\nSpc. 78.1 83.9 45.9 30.1 100 100 100 92.4 83.4 80.8 98.0 99.9 89.0 95.1 40.6\n\nSns. 73.5 71.0 38.1 54.7 32.2 30.8 29.0 56.4 52.9 60.1 67.7 26.2 61.0 7.5 71.3\n\nAHA DB\n\nSpc. 62.6 70.5 58.9 49.3 99.5 99.5 99.3 86.6 66.6 87.5 94.9 99.4 72.1 94.8 48.4\n\nSns. 75.2 75.7 51.5 71.5 17.6 16.9 29.2 60.2 49.6 49.8 71.7 26.8 73.5 9.3 95.9\n\noverall result\n\nSpc. 78.3 86.9 52.2 40.3 99.9 100 99.8 91.9 81.0 88.6 99.7 99.5 89.6 92.0 39.7\n\nSns. 75.0 75.1 49.6 69.2 19.6 18.8 29.1 59.2 50.1 51.2 71.2 26.7 72.0 9.0 92.5\n\nSpc.\n\nIROC\n\n77.5 84.4 49.0 35.0 99.9 100 99.9 92.0 81.7 84.1 98.5 99.7 88.4 93.9 40.6\n\n82 82 49 49 85 87 89 87 67 82 92 80 (*) 58 67\n\nTable 2: Quality of ventricular fibrillation detection algorithms (positive predictivity (PP), accuracy (Ac), calculation time(ct)) for a window length of 8 seconds. Positive predictivity and accuracy in per cent, rounded on 3 digits; calculation time in per cent of the real time of the data, rounded on 2 digits, wl = window length in seconds.\n\nData Source\n\nMIT DB\n\nParameter\n\nwl\n\nTCI TCI ACF95 ACF99 VF VF SPEC CPLX STE MEA SCA WVL1 WVL2 LI TOMP\n\n3 8 8 8 4 8 8 8 8 8 8 8 8 8 8\n\nPP. 0.6 0.8 0.1 0.1 91.3 82.4 60.6 0.1 0.5 0.5 5.6 38.9 1.2 0.1 0.2\n\nCU DB\n\nAc. 78.1 83.9 45.9 30.2 99.9 99.9 99.8 92.3 83.4 80.8 97.9 99.8 88.9 94.9 40.6\n\nPP. 33.9 38.9 19.7 22.2 94.0 94.5 92.0 52.7 29.5 56.0 77.8 92.1 36.6 27.5 26.7\n\nAHA DB\n\nAc. 64.8 70.6 54.5 50.4 85.5 85.2 84.6 80.3 63.8 81.8 89.2 84.1 69.8 76.5 53.2\n\nsignal. (Note 1: Fixing the order of 5 seems to bear a problem. Data with different frequencies (AHA, CU ... 250 Hz, BIH-MIT ... 360 Hz) are filtered in a different way. But this is neglectable, when the Butterworth filter is applied afterwards.) This filter removes high frequency noise like inter-\n\nPP. 41.7 54.4 18.2 19.9 98.0 98.9 97.3 60.7 35.1 47.5 98.0 91.8 59.3 19.4 24.8\n\noverall result\n\nAc. 77.8 84.9 52.1 45.7 85.8 85.7 87.7 86.5 75.6 81.9 94.9 87.0 86.8 77.8 49.4\n\nPP. 23.7 31.1 8.3 9.1 97.0 97.7 96.1 40.8 20.4 23.2 81.6 90.5 36.8 12.1 12.7\n\nAc. 77.2 83.6 49.0 37.9 93.1 93.0 93.8 89.2 79.0 81.3 96.2 93.5 87.0 86.6 45.0\n\nct. 1.5 2.1 3.6 3.6 1.4 1.9 1.9 2.5 1.9 2.5 5.9 1.9 40 15 0.84\n\nspersions and muscle noise. Then, a drift suppression is applied to the resulting signal. This is done by a high pass filter with a cut off frequency of one Hz. Finally, a low pass Butterworth filter with a limiting frequency of 30 Hz is applied to the signal in order to suppress needless high-\n\nPage 3 of 15 (page number not for citation purposes)\n\nBioMedical Engineering OnLine 2005, 4:60\n\nhttp://www.biomedical-engineering-online.com/content/4/1/60\n\nTable 3: Sensitivity of ventricular fibrillation detection algorithms in per cent, wl = window length in seconds.\n\nSns. if Spc. = 95\n\nSns. if Spc. = 99\n\nTCI TCI ACF95 ACF99 VF VF SPEC CPLX STE MEA SCA WVL1 LI TOMP\n\n3 8 8 8 4 8 8 8 8 8 8 8 8 8\n\n15.0 25.3 3.0 3.0 71.0 73.4 69.8 38.8 29.4 7.0 79.0 56.7 7.3 9.1\n\n1.0 1.3 0.6 0.6 59.2 59.7 58.9 5.8 10.8 0.5 66.4 35.2 1.4 1.8\n\nfrequency information even more. This filtering process is carried out in a MATLAB routine. It uses functions from the \"Signal Processing Toolbox\". (Note 2: We used MATLAB R13 – R14 and \"Signal Processing Toolbox\" version 6.1 – 6.3 on a Power Mac G5, 2 GHz.) In order to obtain the ROC curve we have to change a parameter which we call \"critical threshold parameter\" below. TCI algorithm The threshold crossing intervals algorithm (TCI) operates in the time domain. Decisions are based on the number and position of signal crossings through a certain threshold.\n\nFirst, the digitized ECG signal is filtered by the procedure mentioned above. Then a binary signal is generated from the preprocessed ECG data according to the position of the signal above or below a given threshold. The threshold value is set to 20% of the maximum value within each one-second segment S and recalculated every second. Subsequent data analysis takes place over successive one-second stages. The ECG signal may cross the detection threshold one or more times, and the number of pulses is counted. For each stage, the threshold crossing interval TCI is the average interval between threshold crossings and is calculated as follows\n\nTCI =\n\n1000 (N − 1) +\n\nt2 t1 +t 2\n\n+\n\nt3 t3 +t4\n\n[ms].\n\nFigure 2 illustrates the situation.\n\n(1)\n\nACF95 STE MEA WVL1\n\n80 Sensitivity / per cent\n\nwl\n\nLI TOMP\n\n60\n\n40\n\n20\n\n0\n\n0\n\n20\n\n40\n\n60\n\n80\n\n100\n\n(1−Specificity) / per cent\n\nROC Figure TOMP curve 5 for the algorithms ACF, STE, MEA, WVL1, LI, ROC curve for the algorithms ACF, STE, MEA, WVL1, LI, TOMP.\n\n100 TCI 8s VF 8s SPEC CPLX SCA\n\n80 Sensitivity / per cent\n\nParameter\n\n100\n\n60\n\n40\n\n20\n\n0\n\n0\n\n20\n\n40\n\n60\n\n80\n\n100\n\n(1−Specificity) / per cent\n\nFigure ROC curve 6 for the algorithms TCI, VF, SPEC, CPLX, SCA ROC curve for the algorithms TCI, VF, SPEC, CPLX, SCA.\n\nHere, N is the number of pulses in S. t1 is the time interval from the beginning of S back to the falling edge of the preceding pulse. t2 is the time interval from the beginning of S to the start of the next pulse. t3 is the interval between the end of the last pulse and the end of S and t4 is the time from the end of S to the start of the next pulse. If TCI ≥ TCI0 = 400 ms, SR is diagnosed. Otherwise sequential hypothesis testing is used to separate ventricular tachycardia (VT) from VF. As stated above, the original algorithm works with single one-second time segments, (see , page 841). To achieve this the algorithm picks a 3-second episode. The first second and the third second are used to determine t1 and t4. The 2nd second yields the value for TCI. When picking an\n\nPage 4 of 15 (page number not for citation purposes)\n\nBioMedical Engineering OnLine 2005, 4:60\n\nhttp://www.biomedical-engineering-online.com/content/4/1/60\n\n@ I @\n\n\u0012 @ @\n\nN=2\n\n\u001b t1 -\u001b t2 -\n\n\u001b\n\nt3\n\n\u001b\n\nS (1 second interval)\n\nt4-\u001b -\n\nBinary Figuresignal 2 with 2 pulses in threshold crossing intervals algorithm Binary signal with 2 pulses in threshold crossing intervals algorithm.\n\n8-second episode we can hence evaluate 6 consecutive TCI values. Final SR decision is taken if diagnosed in four or more segments otherwise the signal is classified as VF. The critical threshold parameter to obtain the ROC is TCI0. ACF algorithm The autocorrelation algorithms ACF95 (Note 3: Probability of 95% in the Fisher distribution → α = 0.05 in F(α, k1, k2) with k1 = 1, k2 = 5) and ACF99 (Note 4: Probability of 99% in the Fisher distribution → α = 0.01 in F(α, k1, k2) with k1 = 1, k2 = 5) analyze the periodicities within the ECG. Given a discrete signal x(m), the short-term autocorrelation function (ACF) of x(m) with a rectangular window is calculated by\n\nR(k) =\n\nN −1−k\n\nm =0\n\nx(m)x(m + k), 0 ≤ k ≤ N − 1.\n\n(2)\n\nHere, this technique is used to separate VT and SR from VF. It is assumed that VF signals are more or less aperiodic and SR signals are approximately periodic. This assumption is however questionable since VF signals may have a cosine like shape. Compare this assumption with the assumption made by the algorithm in the next subsection.\n\nNote that the autocorrelation function of a function f is connected to the Power Spectrum of | f |2 by the \"WienerKhinchin Theorem\". The detection algorithm performs a linear regression analysis of ACF peaks. An order number i is given to each peak according to its amplitude. So, the highest peak is called P0, etc., ranged by decreasing amplitudes. In a SR signal, which is considered to be periodic or nearly periodic, a linear relationship should exist between the peaks lag and their index number i. No such relationship should exist in VF signals. The linear regression equation of the peak order and its corresponding lag of m peaks in the ACF is described as yi = a + bxi,\n\n(3)\n\nwhere xi is the peak number (from 0 to (m - 1)), and yi is the lag of Pi.\n\nx=\n\n1 m 1 m xi , y = ∑ i =1 yi , ∑ i = 1 m m\n\nb = ∑ i =1( xi − x )yi m\n\n(∑\n\nm (x i =1 i\n\n− x )2\n\n)\n\n−1\n\n.\n\n(4)\n\na = y − bx , In this study, m = 7. The variance ratio VR is defined by\n\nPage 5 of 15 (page number not for citation purposes)\n\nBioMedical Engineering OnLine 2005, 4:60\n\nhttp://www.biomedical-engineering-online.com/content/4/1/60\n\nThe critical threshold parameter to obtain the ROC is the leakage l0.\n\nm\n\nVR =\n\nb∑ ( xi − x )yi i =1\n\nR /(m − 2)\n\n,\n\n( 5)\n\nSpectral algorithm The spectral algorithm (SPEC) works in the frequency domain and analyses the energy content in different frequency bands by means of Fourier analysis.\n\nwhere m\n\nR = ∑ (yi − y − b( xi − x ))2 . i =1\n\nIf VR ≥ VR0 is greater than the Fisher statistics for degrees of freedom k1 = 1 and k2 = m - 2 = 5 with 95% (99%) probability, the rhythm is classified by ACF95 (ACF99) to be SR, otherwise it is VF. The critical threshold parameter to obtain the ROC is VR0, (VR0 ≈ 6.61(16.3) at 95% (99%)). VF filter algorithm The VF filter algorithm (VF) applies a narrow band elimination filter in the region of the mean frequency of the considered ECG signal.\n\nAfter preprocessing, a narrow band-stop filter is applied to the signal, with central frequency being equivalent to the mean signal frequency fm. Its calculated output is the \"VF filter leakage\". The VF signal is considered to be approximately of sinusoidal waveform.\n\nThe ECG of most normal heart rhythms is a broadband signal with major harmonics up to about 25 Hz. During VF, the ECG becomes concentrated in a band of frequencies between 3 and 10 Hz (cf. [11,12], with particularly low frequencies of undercooled victims). After preprocessing, each data segment is multiplied by a Hamming window and then the ECG signal is transformed into the frequency domain by fast Fourier transform (FFT). The amplitude is approximated in accordance with ref. by the sum of the absolute value of the real and imaginary parts of the complex coefficients. (Note 5: Normally one would take the modulus of complex amplitudes.) Let Ω be the frequency of the component with the largest amplitude (called the peak frequency) in the range 0.5 – 9 Hz. Then amplitudes whose value is less than 5% of the amplitude of Ω are set to zero. Four spectrum parameters are calculated, the normalized first spectral moment M\n\nThe number N of data points in an average half period N = T/2 = 1/(2fm) is given by −1    m  m  1  N = π  ∑| Vi |   ∑| Vi − Vi −1 |  +  ,     2   i =1     i =1\n\n(6)\n\nwhere Vi are the signal samples, m is the number of data points in one mean period, and Q...N denotes the floor function. The narrow band-stop filter is simulated by combining the ECG data with a copy of the data shifted by a half period. The VF-filter leakage l is computed as  m l =  ∑| Vi + Vi − N   i =1\n\n  m |   ∑ (| Vi | + | Vi − N |)      i =1 \n\n−1\n\n.\n\n(7)\n\nIn the original paper this algorithm is invoked only if no QRS complexes or beats are detected. This is done by other methods. Since we employ no prior QRS detection, we use the thresholds suggested by . If the signal is higher than a third of the amplitude of the last by the VFfilter detected QRS complex in a previous segment and the leakage is smaller than l0 = 0.406, VF is identified. Otherwise the leakage must be smaller than l0 = 0.625 in order to be classified as VF.\n\njmax\n\n1 M= Ω\n\naj w j\n\nj =1 jmax\n\nj =1\n\n,\n\n(8)\n\naj\n\njmax being the index of the highest investigated frequency, and A1, A2, A3. Here wj denotes the j-th frequency in the FFT between 0 Hz and the minimum of (20Ω, 100 Hz) and aj is the corresponding amplitude. A1 is the sum of amplitudes between 0.5 Hz and Ω/2, divided by the sum of amplitudes between 0.5 Hz and the minimum of (20Ω, 100 Hz). A2 is the sum of amplitudes between 0.7Ω and 1.4Ω divided by the sum of amplitudes between 0.5 Hz and the minimum of (20Ω, 100 Hz). A3 is the sum of amplitudes in 0.6 Hz bands around the second to eighth harmonics (2Ω – 8Ω), divided by the sum of amplitudes in the range of 0.5 Hz to the minimum of (20Ω, 100 Hz). VF is detected if M ≤ M0 = 1.55, A1 80% our current investigations indicate a promising good performance for new algorithms based on other methods coming from chaos theory which are currently under development. When finished these algorithms will be presented elsewhere.\n\nTable 2 shows the values for the positive predictivity, the accuracy and the calculation time of the investigated algorithms. Table 3 shows the values for the sensitivity of the investigated algorithms, if, due to an appropriate adaption of the threshold parameters, the specificity were 95% and 99%, respectively. Figure 5 and 6 show the ROC curves for all algorithms. For the computation of the ROC curves, we used 64 nodes. Since some critical threshold parameters are discrete the points of the ROC curve are not equidistant.\n\n3 Discussion and Conclusion In real applications of AEDs the specificity is more important than the sensitivity, since no patient should be defibrillated due to an analysis error which might cause cardiac arrest. Therefore, a low number of false positive decisions should be achieved, even if this process makes the number of false negative decisions higher. But one has to distinguish between our calculated values for specificity and sensitivity and the values in . Our values were determined for the basic mathematical algorithms, whereas this paper gives recommendations for whole ECG analysis systems. It also does not consider an analysis without preselection. Our results show that no algorithm achieves its proclaimed values for the sensitivity or specificity as described in the original papers or in and when applied to an arbitrary ECG episode. The main reason for this is the following: Whereas all other researchers made a preselection of signals, we simulated the situation of a bystander, who is supposed to use an AED, more accurately. Hence no preselection of ECG episodes were made. The best algorithm SCA, which yields the best value for the integrated receiver operating characteristic (IROC) is a new algorithm followed by the algorithms SPEC and VF. Studying the ROC curves in Figure 5 and Figure 6 we see that the relevant part of the ROC curves lies at the left side. The ROC curve also enables us to compare different algorithms given a specified specificity.\n\nAppendix A: Sensitivity, Specificity, Positive Predictivity, Accuracy, and ROC Sensitivity is the ability (probability) to detect ventricular fibrillation. It is given by the quotient\n\ndetected cases of VF TP = , all cases of VF TP + FN\n\n( 24 )\n\nwith TP being the number of true positive decisions, FN the number of false negative decisions. Specificity is the probability to identify \"no VF\" correctly. It is given by the quotient\n\ndetected cases of \"no VF\" TN = , all cases of \"no VF\" TN + FP\n\n( 25 )\n\nwhere TN is the number of true negative decisions, and FP is the number of false positive decisions. This means that if a defibrillator has a sensitivity of 90% and a specificity of 99%, it is able 90% of the time to detect a rhythm that should be defibrillated, and 99% of the time to recommend not shocking when defibrillation is not indicated. Remark: a trivial algorithm which classifies every ECG episode as \"no VF\" will reach a specificity of 100%, but will have sensitivity 0%. On the other hand, a trivial algorithm which classifies every ECG episode as VF will reach a sensitivity of 100%, but will have specificity 0%. The ROC curve (see below) describes this inherent tradeoff between sensitivity and specificity. Furthermore, we calculated the Positive Predictivity and the Accuracy of the investigated algorithms. Positive predictivity is defined by\n\nAll other algorithms yielded only mixed results in our simulations. We also conclude that algorithms developed for QRS detection, like LI and TOMP, are not suitable for VF detection even when the thresholds are suitably adapted.\n\ndetected cases of \"VF\" TP = . m as \"VF\" TP + FP all cases classified by the algorithm\n\n( 26 )\n\nPositive predictivity is the probability, that classified VF is truly VF:\n\nPage 12 of 15 (page number not for citation purposes)\n\nhttp://www.biomedical-engineering-online.com/content/4/1/60\n\n4\n\n4\n\n3\n\n3\n\n2\n\n2\n\nvoltage / a.u.\n\nvoltage / a.u.\n\nBioMedical Engineering OnLine 2005, 4:60\n\n1\n\n1\n\n0\n\n0\n\n−1\n\n−1\n\n−2 0\n\n2\n\n4\n\n6\n\n8\n\ntime / s\n\n2\n\n4\n\n6\n\n8\n\ntime / s\n\nFigure ECG applying signal 7step with 1 ofrelative Signal maxima Comparison (indicated Algorithm by stars (SCA) left) after ECG signal with relative maxima (indicated by stars left) after applying step 1 of Signal Comparison Algorithm (SCA). This ECG episode is annotated as no VF, a.u. ... arbitrary units.\n\nAccuracy is defined by\n\nall true decisions TP + TN = . all decisions TP + FP + TN + FN\n\n−2 0\n\n( 27 )\n\nAccuracy is the probability to obtain a correct decision. Specificity and sensitivity always depend on the chosen critical threshold parameters which depend, on the other hand, on the databases used for evaluation (see Note 7). To get rid of at least of the dependence on the chosen critical threshold parameter one uses the ROC curve. The sensitivity is plotted in dependence of (1 - specificity), where different points in the plot are obtained by varying the critical threshold parameter in the decision stage of an algorithm. The ROC curves enables us to compare different algorithms when choosing a specified specificity. For more information on ROC curves see [20,21].\n\nAppendix B: Algorithm details: Signal Comparison Algorithm (SCA) Here we describe the search for relative maxima and the appropriate choice among them, used in Section 1 in more detail.\n\nFigure ECG applying signal 8step with 2 ofrelative Signal maxima Comparison left (indicated Algorithmby(SCA) stars) after ECG signal with relative maxima left (indicated by stars) after applying step 2 of Signal Comparison Algorithm (SCA).\n\nAn offset is added to the ECG signal to make its mean value to zero. We construct a set Z containing the values aj and temporal positions tj of this new signal, i.e., Z = {(tj, aj)|aj is the value of the ECG signal at time tj}. All further steps are executed both with the set Z and the set -Z, where -Z = {(tj, bj)|bj = -aj is the value of the negative ECG signal at time tj} with the help of the reference signals rECGᐍ, ᐍ being VF, SR1, SR2 or SR3, or, equivalently, ᐍ = 0,1, 2, 3. Note, that the maxima of Z correspond to the minima of -Z. So we get 2 * 4 = 8 tests to find out whether a signal is VF or SR. If any of the 8 tests yields SR, the signal is considered to be SR. Step 1 All relative maxima aj of Z and their corresponding times tj are determined. The resulting set is called M0, i.e., M0 = {(tj, aj)|aj is a local maximum}, so M0 ⊂ Z. All aj in M0, that are smaller than A, where A = ∆·max(aj) and ∆ is a threshold, are deleted. The threshold ∆ is set to 0.1 for the VF reference signal and to 0.2 for the SR reference signals. We call the reduced set M1. In Figure 7 we see an ECG episode from the CU database (cu21, from t = 148 s until t = 156 s) together with its selected relative maxima according to the status after processing step 1.\n\nNow, we introduce an index l and set it to l = 1.\n\nPage 13 of 15 (page number not for citation purposes)\n\nhttp://www.biomedical-engineering-online.com/content/4/1/60\n\n4\n\n4\n\n3\n\n3\n\n2\n\n2\n\nvoltage / a.u.\n\nvoltage / a.u.\n\nBioMedical Engineering OnLine 2005, 4:60\n\n1\n\n1\n\n0\n\n0\n\n−1\n\n−1\n\n−2 0\n\n2\n\n4\n\n6\n\n8\n\n−2 0\n\n2\n\n4\n\ntime / s\n\nFigure ECG applying signal 9step with 4 ofrelative Signal Comparison maxima (indicated Algorithm by stars) (SCA) after ECG signal with relative maxima (indicated by stars) after applying step 4 of Signal Comparison Algorithm (SCA).\n\n8\n\nFigure ECG applying signal 11 step with 6 ofrelative Signal maxima Comparison and SR Algorithm reference(SCA) signal after ECG signal with relative maxima and SR reference signal after applying step 6 of Signal Comparison Algorithm (SCA).\n\ninterval are equal or smaller than amax and larger than 0.2amax. All pairs (aj, tj) except (amax, tmax) in Ml, that are referred to the found interval Il, are deleted. We get a set that we call Ml+1. This procedure is repeated with all untreated aj in Ml, until every aj has been considered and afterwards either been deleted or kept. After each step, l is increased by 1. This means, first we consider M1, then M2 = M1\\I1, then M3 = M1\\{I1 ∪ I2} and so on, until we reach a highest l, called lmax. In the end, we get a set that we call\n\n4 3 2 voltage / a.u.\n\n6\n\ntime / s\n\n1 0 −1\n\nl\n\nM, with M = M1 \\{∪ jmax =1\n\n−1\n\nI j} .\n\n−2 −3 −4 0\n\n2\n\n4\n\n6\n\n8\n\ntime / s\n\nFigure ECG applying signal 10 step with 6 ofrelative Signal maxima Comparison and VF Algorithm reference(SCA) signal after ECG signal with relative maxima and VF reference signal after applying step 6 of Signal Comparison Algorithm (SCA).\n\nIn the end, the aj in M are the relative maxima in Z, that are higher than A and are the only ones in certain subintervals of Z. Two different aj in M can only be neighbors in Z, if they are separated by a valley that is deeper than 20% of the higher peak of the two. In Figure 8 we again see the ECG episode, together with its newly selected relative maxima according to the status after processing step 2. Step 3 A value Ω is calculated from M. The frequency Ω of \"peaks\" is given by\n\nStep 2 Ml is reduced further: The maximum aj in Ml is searched. Here, we call it amax. amax has a corresponding temporal position tmax. Then, the largest possible temporal interval Il in Z around tmax is searched, so that all values aj in this\n\nΩ=\n\n60N M t max − t min\n\n[min−1],\n\n( 28 )\n\nwhere NM is the number of points in M and tmax - tmin is the maximum temporal range of the elements in M.\n\nPage 14 of 15 (page number not for citation purposes)\n\nBioMedical Engineering OnLine 2005, 4:60\n\nhttp://www.biomedical-engineering-online.com/content/4/1/60\n\nStep 4 Now, if two different elements (ai, ti) and (aj, tj) of M are\n\n12.\n\n24 , Ω the element with the smaller a is deleted from M. This final set is called X. In Figure 9 we again see the ECG episode as in the figures above and together with its newly selected relative maxima according to the status after processing step 4.\n\n13.\n\nseparated by a temporal distance |ti - tj| smaller than\n\nStep 5 Ω is recalculated by Equation (28) with the help of the recalculated set X. If Ω > 280, r is set to 2, if Ω < 180, r is set to 0.9, else r is set to 1. Step 6 The decision is calculated by Equation (16). VRF is calculated for the ventricular fibrillation reference signal, VRS for the sinus rhythm reference signal.\n\n14. 15. 16. 17. 18. 19.\n\n20. 21.\n\nMurray A, Campbell R, Julian D: Characteristics of the ventricular fibrillation waveform. In Proc. Computers in Cardiology Washington, DC: IEEE Computer Society Press; 1985:275-278. Zhang X, Zhu Y, Thakor N, Wang Z: Detecting ventricular tachycardia and fibrillation by complexity measure. IEEE Trans Biomed Eng 1999, 46(5):548-55. Lempel A, Ziv J: On the complexity of finite sequences. IEEE Trans Inform Theory 1976, 22:75-81. Louis A, Maaß P, Rieder A: Wavelets Stuttgart: Teubner; 1998. Li C, Zheng C, Tai C: Detection of ECG characteristic points using wavelet transforms. IEEE Trans Biomed Eng 1995, 42:21-8. Hamilton P, Tompkins W: Quantitative investigation of QRS detection rules using the MIT/BIH arrhythmia database. IEEE Trans Biomed Eng 1986, 33(12):1157-65. Pan J, Tompkins W: A real-time QRS detection algorithm. IEEE Trans Biomed Eng 1985, 32(3):230-6. Kerber R, Becker L, Bourland J, Cummins R, Hallstrom A, Michos M, Nichol G, Ornato J, Thies W, White R, Zuckerman B: Automatic External Deflbrillators for Public Access Defibrillation: Recommendations for Specifying and Reporting Arrhythmia Analysis Algorithm Performance, Incorporating New Waveforms, and Enhancing Safety. Circulation 1997, 95:1677-1682. Swets J, Pickett R: Evaluation of diagnostic systems: Methods from signal detection theory New York: Academic Press; 1992. The magnificent ROC [http://www.anaesthetist.com/mnm/stats/ roc/]\n\nIn Figure 10 we see the ECG episode together with the corresponding VF reference signal. In Figure 11 we see the ECG episode together with the first corresponding SR reference signal. c1 is set to 2/r, c2 is set to 1.\n\nAcknowledgements We are indebted to the referees for numerous helpful suggestions. A. A. gratefully appreciates continuous support by the Bernhard-Lang Research Association.\n\nReferences 1. 2. 3. 4. 5. 6. 7. 8. 9. 10.\n\n11.\n\nZheng Z, Croft J, Giles W, Mensah G: Sudden cardiac death in the United States, 1989 to 1998. Circulation 2001, 104(18):2158-63. American Heart Association, AHA database [http:// www.americanheart.org] Massachusetts Institute of Technology, MIT-BIH arrhythmia database [http://www.physionet.org/physiobank/database/mitdb] Massachusetts Institute of Technology, CU database [http:// www.physionet.org/physiobank/database/cudb] Clayton R, Murray A, Campbell R: Comparison of four techniques for recognition of ventricular fibrillation from the surface ECG. Med Biol Eng Comput 1993, 31(2):111-7. Jekova I: Comparison of five algorithms for the detection of ventricular fibrillation from the surface ECG. Physiol Meas 2000, 21(4):429-39. Thakor N, Zhu Y, Pan K: Ventricular tachycardia and fibrillation detection by a sequential hypothesis testing algorithm. IEEE Trans Biomed Eng 1990, 37(9):837-43. Chen S, Thakor N, Mower M: Ventricular fibrillation detection by a regression test on the autocorrelation function. Med Biol Eng Comput 1987, 25(3):241-9. Kuo S, Dillman R: Computer Detection of Ventricular Fibrillation. Computers in Cardiology, IEEE Computer Society 1978:347-349. Barro S, Ruiz R, Cabello D, Mira J: Algorithmic sequential decision-making in the frequency domain for life threatening ventricular arrhythmias and imitative artefacts: a diagnostic system. J Biomed Eng 1989, 11(4):320-8. Clayton R, Murray A, Campbell R: Changes in the surface ECG frequency spectrum during the onset of ventricular fibrillation. In Proc. Computers in Cardiology 1990 Los Alamitos, CA: IEEE Computer Society Press; 1991:515-518.\n\nPublish with Bio Med Central and every scientist can read your work free of charge \"BioMed Central will be the most significant development for disseminating the results of biomedical researc h in our lifetime.\" Sir Paul Nurse, Cancer Research UK\n\nYour research papers will be: available free of charge to the entire biomedical community peer reviewed and published immediately upon acceptance cited in PubMed and archived on PubMed Central yours — you keep the copyright\n\nBioMedcentral" ]
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https://www.victorvaquero.me/publication/vvaquero2017ecmr/
[ "", null, "# Deconvolutional Networks for Point-Cloud Vehicle Detection and Tracking in Driving Scenarios\n\n### Abstract\n\nVehicle detection and tracking is a core ingredient for developing autonomous driving applications in urban scenarios. Recent image-based Deep Learning (DL) techniques are obtaining breakthrough results in these perceptive tasks. However, DL research has not yet advanced much towards processing 3D point clouds from lidar range-finders. These sensors are very common in autonomous vehicles since, despite not providing as semantically rich information as images, their performance is more robust under harsh weather conditions than vision sensors. In this paper we present a full vehicle detection and tracking system that works with 3D lidar information only. Our detection step uses a Convolutional Neural Network (CNN) that receives as input a featured representation of the 3D information provided by a Velodyne HDL-64 sensor and returns a per-point classification of whether it belongs to a vehicle or not. The segmented point cloud is then geometrically processed to generate observations for a multi-object tracking system implemented via a number of Multi-Hypothesis Extended Kalman Filters (MH-EKF) that estimate the position and velocity of the surrounding vehicles. The system is thoroughly evaluated on the KITTI tracking dataset, and we show the performance boost provided by our CNN-based detector over the standard geometric approach. Our lidar-based approach uses about 4% a fraction of the data needed for an image-based detector with similarly competitive results\n\nType\nPublication\nEuropean Conference on Mobile Robotics\nDate", null, "## Paper Summary", null, "We introduce a novel CNN-based vehicle detector on 3D range data. The proposed model is fed with an encoded representation of the point cloud and computes for each 3D point its probability of belonging to a vehicle. The classified points are then clustered generating trustworthy observations that are fed to our MH-EKF based tracker. Note: Bottom left RGB image is shown here only for visualization purposes.\n\n### Lidar Data Representation", null, "To obtain a useful input for our CNN-based vehicle detector, we project the 3D point cloud raw data to a featured image-like representation containing ranges and reflectivity information by means of $G(\\cdot)$. In this way, we first project the 3D Cartesian point cloud to spherical coordinates $sph(p_i)~=~{\\phi_i,\\theta_i, \\rho_i}$. According to the Velodyne HDL-64 specifications, elevation angles $\\theta$ are represented as a $H \\in \\mathbb{R}^{64}$ vector with a resolution $\\Delta\\theta$ of 13 degrees for the upper laser rays and 12 degrees the lower half respectively. Moreover, $G(\\cdot)$ needs to restrict the azimuth field of view, $\\phi \\in [-40.5,40.5]$ to avoid the presence of unlabelled vehicle points, as the Kitti tracking benchmark has labels only for the front camera viewed elements. The azimuth resolution was set to a value of $\\Delta\\phi=0.18$ degrees according to the manufacturer, and hence lying in $W \\in \\mathbb{R}^{451}$. Each $H,W$ pair encodes the range ($\\rho$) and reflectivity of each projected point, so finally our input data representation lies in an image-like space $G(\\mathcal{P}) \\in \\mathbb{R}^{64 \\times 451 \\times 2}$.\n\nGround-truth for learning the proposed classification task is obtained by first projecting the image-based Kitti tracklets over the 3D Velodyne information, and then applying again $G(\\cdot)$ over the selected points.\n\n### Network Used", null, "Our network encompasses only convolutional and deconvolutional blocks followed by Batch Normalization (BN) and ReLu (RL) non-linearities. The first three blocks conduct the feature extraction step controlling, according to our vehicle detection objective, the size of the receptive fields and the feature maps generated. The next three deconvolutional blocks expanse the information enabling the point-wise classification. After each deconvolution, feature maps from the lower part of the network are concatenated (CAT) before applying the normalization and non-linearities, providing richer information and better performance.\n\nDuring training, three losses are calculated at different network points, as shown in the bottom part of the graph:\n\n$\\mathcal{L}(\\hat{\\mathcal{Y}}, \\mathcal{Y})$ = $\\sum_{r=1}^{3}$ $\\lambda_r \\mathcal{L}_r (\\hat{\\mathcal{Y}_r}, {\\mathcal{Y}_r})$ ,\n\nwhere $r$ represents the intermediate loss-control positions, $\\lambda_{r}$ are regularization weights for the loss at each resolution, and $\\hat{\\mathcal{Y}}, \\mathcal{Y}$ are respectively the predictions and ground-truth classes at those resolutions.\n\nIn our approach, $\\mathcal{L}_r$ is a multi-class Weighted Cross Entropy loss (WCE) defined as:\n\n$\\mathcal{L}_r^{WCE}$ = $-\\sum_{i,j,k}^{H_r,W_r,K_r}$ $\\omega(\\mathcal{Y}_{i,j})$ $\\textit{Id}_{[\\mathcal{Y}_{i,j}]}$ $\\text{log}(\\hat{\\mathcal{Y}}_{i,j,k})$ ,\n\nwhere $\\textit{Id}_{[x’]}(x)$ is an index function that selects the probability associated to the expected ground truth class and $\\omega(k)$ is the previously mentioned class-imbalance regularization weight computed from the training set statistics.\n\n### Results", null, "", null, "Acknowledgements: This work has been supported by the Spanish Ministry of Economy and Competitiveness projects ROBINSTRUCT (TIN2014-58178-R) and COL- ROBTRANSP (DPI2016-78957-R), by the Spanish Ministry of Education FPU grant (FPU15/04446), the Spanish State Research Agency through the Marı́a de Maeztu Seal of Excellence to IRI (MDM-2016-0656) and by the EU H2020 project LOGIMATIC (H2020-Galileo-2015-1-687534). The authors also thank Nvidia for hardware donation under the GPU grant program.", null, "" ]
[ null, "https://www.victorvaquero.me/publication/vvaquero2017ecmr/featured_hu21f3d1329605c8ee2cdbdc2bc3ddf02f_551899_1600x400_fill_q90_box_smart1_2.png", null, "https://www.victorvaquero.me/publication/vvaquero2017ecmr/ECMR_17_DeepLidar.jpg", null, "https://www.victorvaquero.me/publication/vvaquero2017ecmr/ecmr_17_fig1.png", null, "https://www.victorvaquero.me/publication/vvaquero2017ecmr/ecmr_17_fig2.png", null, "https://www.victorvaquero.me/publication/vvaquero2017ecmr/ecmr_17_fig3.png", null, "https://www.victorvaquero.me/publication/vvaquero2017ecmr/ecmr_17_finalFigure.jpg", null, "https://www.victorvaquero.me/publication/vvaquero2017ecmr/ecmr_17_results.png", null, "https://www.victorvaquero.me/img/vvaquero_truck.png", null ]
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https://wordpress.stackexchange.com/questions/342409/update-existing-post-times-to-random-times
[ "# Update existing post times to random times?\n\nI have found a code here that will randomize the date of all posts to a random date. Here is the code that someone has posted:\n\n``````<?php\n/**\n* Plugin Name: WPSE 259750 Random Dates\n* Description: On activation, change the dates of all posts to random dates\n*/\n\n//* We want to do this only once, so add hook to plugin activation\nregister_activation_hook( __FILE__ , 'wpse_259750_activation' );\nfunction wpse_259750_activation() {\n\n//* Get all the posts\n\\$posts = get_posts( array( 'numberposts' => -1, 'post_status' => 'any' ) );\nforeach( \\$posts as \\$post ) {\n\n//* Generate a random date between January 1st, 2015 and now\n\\$random_date = mt_rand( strtotime( '1 January 2015' ), time() );\n\\$date_format = 'Y-m-d H:i:s';\n\n//* Format the date that WordPress likes\n\\$post_date = date( \\$date_format, \\$random_date );\n\n//* We only want to update the post date\n\\$update = array(\n'ID' => \\$post->ID,\n'post_date' => \\$post_date,\n'post_date_gmt' => null,\n);\n\n//* Update the post\nwp_update_post( \\$update );\n}\n}\n``````\n\nHow would you do the same, but only randomize the time without randomizing the date of the post. So, the posts should keep the same date they currently have, but only randomize the time of the day they were posted.\n\nI tried changing the post_date to post_time and changing the random_date to time() only. Then of course changing the date_format to 'H:i:s' however it did nothing.\n\nThis is the part that is responsible for random date:\n\n``````//* Generate a random date between January 1st, 2015 and now\n\\$random_date = mt_rand( strtotime( '1 January 2015' ), time() );\n``````\n\nSo you need to change it. And if you want to randomize only the time part, then this is one way to achieve that:\n\n``````\\$random_date = strtotime( date( 'Y-m-d 00:00:00', strtotime(\\$post->post_date) ) ) + mt_rand(0, 24*60*60);\n``````\n\nThis line will:\n\n• take the date of post\n• get only day part of it\n• concert it to time\n• add random number of seconds to it\n\nSo it will randomize the time of publication.\n\n• This code does exactly what I've asked. Thank you so much for your prompt answer. Jul 9, 2019 at 14:15\n\nhow can I set up a cronjob for this? My website has 10k post and I want to setup a cronjob to random date for 10k post each day?\n\n• This does not really answer the question. If you have a different question, you can ask it by clicking Ask Question. To get notified when this question gets new answers, you can follow this question. Once you have enough reputation, you can also add a bounty to draw more attention to this question. - From Review Aug 15 at 21:50" ]
[ null ]
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https://trading-market.org/what-is-pip-value/
[ "The meaning of pip value can vary between currencies, but as most major currency pairs are priced to four decimal places, a pip is usually equal to the fourth figure after the decimal point. Calculating the value of pips, especially for cross currency pairs that do not include the U.S. dollar as one of the currencies, can be time consuming and difficult. For that reason, there are pip value calculators that will do the job for you. With a pip value calculator, you simply input your account base currency and the calculator will let you know the value of a pip for the standard lot , mini lot and micro lot . This can save you a lot of time and since it can update in real time you will always easily know what your potential profit or loss is. In addition, since forex transactions are typically leveraged, the pip value of positions gets multiplied by the amount of leverage used. By knowing the pip value of a currency pair, you can use money management techniques to calculate the ideal position size for any trade within the limits of the size of your account and your risk tolerance.", null, "The value of a pip is calculated by multiplying the amount of the trade in lots by one pip in decimal form, and then dividing it by the current exchange rate of the quote currency in your pair. However, we often find market forward points to be slightly different to the theoretical implied forward points. In this example, the current market tradeable forward point is 86 pips. The difference is called cross currency basis and it is driven by relative supply and demand between currencies. To do so they purchase USD in the spot market while selling USD in the forward market to return the USD to their native currency. This dynamic – excess demand to buy USD today but also to sell USD in the future – pushes USD forward rates down below levels implied from interest rate differentials.\n\n## Try A Demo Account\n\nThis one pip movement would equal a shift in value of \\$0.10 on a micro lot of 1,000 euros, \\$1 on a mini lot of 10,000 euros and \\$10 for a full lot of 100,000 euros. Those would be your pip values when trading in a U.S. dollar denominated account. If you trade in an account denominated in a specific currency, the pip value for currency pairs that do not contain your accounting currency are subject to an additional exchange rate. This is due to the fact that you need to convert pip value into your accounting currency to compare it with the pip value of your other positions. If we keep the EUR, in a year’s time with interest rate being -0.5%, we will have EUR 995,000. If we keep the money in USD, with interest rate 0.2%, it will become USD 1,202,400. Dividing USD 1,202,400 by EUR 995,000 gives us an implied forward rate of 1.2084.\n\nMost currency pairs are priced out to four decimal places and the pip change is the last decimal point. Most other currency pairs have the U.S. dollar as the base currency, such as USD/JPY and USD/CAD, for example, and they have different pip values. To calculate the pip value where the USD is the base currency when trading in a U.S. dollar-denominated account, you need to divide the position size by the exchange rate. Currencies must be exchanged to facilitate international trade and business.\n\n## Fractional Pip\n\nThe effect that a one-pip change has on the dollar amount, or pip value, depends on the number of euros purchased. If an investor buys 10,000 euros with U.S. dollars, the price paid will be US\\$12,908.22 ([1/0.7747] x 10,000). If the exchange rate for this pair experiences a one-pip increase, the price paid would be \\$12,906.56 ([1/0.7748] x 10,000). Forex pairs are used to disseminate exchange quotes through bid and ask quotes that are accurate to four decimal places.\n\nFor pairs in which the euro isn’t the quote currency, you would divide the usual pip value by the exchange rate between the euro and the quote currency. When trading in the foreign exchange market, it’s hard to underestimate the importance of pips. A pip, which stands for either “percentage in point” or “price interest point,” represents the basic movement a currency pair can make in the market.\n\n## What Is A Pip?\n\nThe currency you used to open your forex trading account will determine the pip value of many currency pairs. Those pip values would change only if the value of the U.S. dollar rose or fell significantly—by more than 10%. Most forex brokers allow a very high leverage ratio, or, to put it differently, have very low margin requirements.\n\n• Those pip values would change only if the value of the U.S. dollar rose or fell significantly—by more than 10%.\n• The pip value is defined by the currency pair being traded, the size of the trade and the exchange rate of the currency pair.\n• Then, multiply that figure by your lot size, which is the number of base units that you are trading.\n• To calculate pip value, divide one pip (usually 0.0001) by the current market value of the forex pair.\n\nFor most currency pairs—including, for example, the British pound/U.S. dollar (GBP/USD)—a pip is equal to 1/100 of a percentage point, or one basis point, and pips are counted in the fourth place after the decimal in price quotes. For currency pairs involving the Japanese yen, a pip is one percentage point, and pips are counted in the second place after the decimal in price quotes. Electronic trading platforms have brought greater price transparency and price competition to the foreign exchange markets. Several trading platforms have extended the quote precision for most of the major currency pairs by an additional decimal point; the rates are displayed in 1/10 pip. Pip is an acronym for “percentage in point” or” price interest point.” A pip is the smallest price move that an exchange rate can make based on forex market convention.\n\nThis is why profits and losses vary greatly in forex trading even though currency prices do not change all that much — certainly not like stocks. Stocks can double or triple in price, or fall to zero; currency never does.\n\nThe pip value is defined by the currency pair being traded, the size of the trade and the exchange rate of the currency pair. To calculate pip value, divide one pip (usually 0.0001) by the current market value of the forex pair. Then, multiply that figure by your lot size, which is the number of base units that you are trading. This means that the value of a pip will be different between currency pairs, due to the variations in exchange rates. However, when the quote currency is the US dollar, the value of a pip is always the same – if the lot size is 100,000, the pip will equal \\$10.\n\n## Example Of Pip Value\n\nThe forex market is where such transactions happen—along with bets made by speculators who hope to make money off of price moves in pairs of currencies. Pips are used in calculating the rates participants in the forex market pay when carrying out currency trades. Since most currency pairs are quoted to a maximum of four decimal places, the smallest change for these pairs is 1 pip. The value of a pip can be calculated by dividing 1/10,000 or 0.0001 by the exchange rate. In addition to determining costs, tracking the change of pips is important for traders in determining the potential profit, or loss, that might be made on a trade. As exchange rates vary throughout trading, traders can make or lose money depending on whether the bid and ask prices change enough, and in the right direction, to offset any costs imposed by the spread. Basically, the movement of a currency pair such as EUR/USD from 1.2000 to 1.2001 would represent a one pip rise in the exchange rate, so the pip size in EUR/USD is 0.0001.\n\nBecause currency prices do not vary substantially, much lower margin requirements are less risky than it would be for stocks. Note, however, that there is considerable risk in forex trading, so you may be subject to margin calls when currency exchange rates change rapidly. If your account is funded with a currency other than the U.S. dollar, the same pip value amounts apply when that currency is the quote currency. For example, for a euro-denominated account, the pip value will be 10 euros for a standard lot, 1 euro for a mini lot, and 0.10 euro for a micro lot when the euro is the second currency in the pair.\n\n## Performance Improvement Project (pip) Library\n\nThe implied forward points based on interest rate differential are 0.0084 . A pip refers to the last decimal place quoted for a currency pair. Most currency pairs are priced to 4 decimal places, so a pip will be the same as 0.01%, or a basis point, in those cases. The exact value of a pip depends on the currency pair and the quoting convention. For example, a pip in USD-JPY denotes the second decimal place, whereas a pip in EUR-CZK denotes the third decimal place. The pip value is the price attributed to a one-pip move in a forex trade – it is often used when referencing a position’s losses or gains.\n\nWithout this knowledge, you might wind up taking either too much or too little risk on a trade. If your account is funded with U.S. dollars and the dollar isn’t the quote currency, you would divide the usual pip value by the exchange rate between the dollar and the quote currency. For example, if the U.S. dollar/Canadian dollar (USD/CAD) exchange rate is 1.33119, the pip value for a standard lot is \\$7.51 (\\$10 / 1.3319)." ]
[ null, "data:image/svg+xml,%3Csvg%20xmlns='http://www.w3.org/2000/svg'%20viewBox='0%200%20395%20296'%3E%3C/svg%3E", null ]
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https://casestudysolution.xyz/get-help-search-engine-optimization-scope.html
[ "", null, "At Emineo Marketing our Core Values are the foundation of our program. We attract and recruit the finest people in the Las Vegas Valley. We build our organization from within, promoting and rewarding people without regard to any difference unrelated to performance. We act on the conviction that the men and women of Emineo Marketing will always be our most important asset.\nPaid channel marketing is something you’ve probably come across in some form or another. Other names for this topic include Search Engine Marketing (SEM), online advertising, or pay-per-click (PPC) marketing. Very often, marketers use these terms interchangeably to describe the same concept — traffic purchased through online ads. Marketers frequently shy away from this technique because it costs money. This perspective will put you at a significant disadvantage. It’s not uncommon for companies to run PPC campaigns with uncapped budgets. Why? Because you should be generating an ROI anyway. This chapter walks through the basics of how.\nAnother reason to achieve quality backlinks is to entice visitors to come to your website. You can't build a website, and then expect that people will find your website without pointing the way. You will probably have to get the word out there about your site. One way webmasters got the word out used to be through reciprocal linking. Let's talk about reciprocal linking for a moment.\n!function(n,t){function r(e,n){return Object.prototype.hasOwnProperty.call(e,n)}function i(e){return void 0===e}if(n){var o={},u=n.TraceKit,s=[].slice,a=\"?\";o.noConflict=function(){return n.TraceKit=u,o},o.wrap=function(e){function n(){try{return e.apply(this,arguments)}catch(e){throw o.report(e),e}}return n},o.report=function(){function e(e){a(),h.push(e)}function t(e){for(var n=h.length-1;n>=0;--n)h[n]===e&&h.splice(n,1)}function i(e,n){var t=null;if(!n||o.collectWindowErrors){for(var i in h)if(r(h,i))try{h[i].apply(null,[e].concat(s.call(arguments,2)))}catch(e){t=e}if(t)throw t}}function u(e,n,t,r,u){var s=null;if(w)o.computeStackTrace.augmentStackTraceWithInitialElement(w,n,t,e),l();else if(u)s=o.computeStackTrace(u),i(s,!0);else{var a={url:n,line:t,column:r};a.func=o.computeStackTrace.guessFunctionName(a.url,a.line),a.context=o.computeStackTrace.gatherContext(a.url,a.line),s={mode:\"onerror\",message:e,stack:[a]},i(s,!0)}return!!f&&f.apply(this,arguments)}function a(){!0!==d&&(f=n.onerror,n.onerror=u,d=!0)}function l(){var e=w,n=p;p=null,w=null,m=null,i.apply(null,[e,!1].concat(n))}function c(e){if(w){if(m===e)return;l()}var t=o.computeStackTrace(e);throw w=t,m=e,p=s.call(arguments,1),n.setTimeout(function(){m===e&&l()},t.incomplete?2e3:0),e}var f,d,h=[],p=null,m=null,w=null;return c.subscribe=e,c.unsubscribe=t,c}(),o.computeStackTrace=function(){function e(e){if(!o.remoteFetching)return\"\";try{var t=function(){try{return new n.XMLHttpRequest}catch(e){return new n.ActiveXObject(\"Microsoft.XMLHTTP\")}},r=t();return r.open(\"GET\",e,!1),r.send(\"\"),r.responseText}catch(e){return\"\"}}function t(t){if(\"string\"!=typeof t)return[];if(!r(j,t)){var i=\"\",o=\"\";try{o=n.document.domain}catch(e){}var u=/(.*)\\:\\/\\/([^:\\/]+)([:\\d]*)\\/{0,1}([\\s\\S]*)/.exec(t);u&&u===o&&(i=e(t)),j[t]=i?i.split(\"\\n\"):[]}return j[t]}function u(e,n){var r,o=/function ([^(]*)\\(([^)]*)\\)/,u=/['\"]?([0-9A-Za-z\\$_]+)['\"]?\\s*[:=]\\s*(function|eval|new Function)/,s=\"\",l=10,c=t(e);if(!c.length)return a;for(var f=0;f0?u:null}function l(e){return e.replace(/[\\-\\[\\]{}()*+?.,\\\\\\^\\$|#]/g,\"\\\\\\$&\")}function c(e){return l(e).replace(\"<\",\"(?:<|<)\").replace(\">\",\"(?:>|>)\").replace(\"&\",\"(?:&|&)\").replace('\"','(?:\"|\")').replace(/\\s+/g,\"\\\\s+\")}function f(e,n){for(var r,i,o=0,u=n.length;or&&(i=u.exec(o[r]))?i.index:null}function h(e){if(!i(n&&n.document)){for(var t,r,o,u,s=[n.location.href],a=n.document.getElementsByTagName(\"script\"),d=\"\"+e,h=/^function(?:\\s+([\\w\\$]+))?\\s*\\(([\\w\\s,]*)\\)\\s*\\{\\s*(\\S[\\s\\S]*\\S)\\s*\\}\\s*\\$/,p=/^function on([\\w\\$]+)\\s*\\(event\\)\\s*\\{\\s*(\\S[\\s\\S]*\\S)\\s*\\}\\s*\\$/,m=0;m]+)>|([^\\)]+))\\((.*)\\))? 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A poorer user experience would send your site hurtling down the rankings. This appeared to come as a shock to many in the SEO community and despite assurances that content was still king – many seemed to feel that this ...", null, "```\n\n## So, as you build a link, ask yourself, \"am I doing this for the sake of my customer or as a normal marketing function?\" If not, and you're buying a link, spamming blog comments, posting low-quality articles and whatnot, you risk Google penalizing you for your behavior. This could be as subtle as a drop in search ranking, or as harsh as a manual action, getting you removed from the search results altogether!\n\nSo, for example, a short-tail keyphrase might be “Logo design”. Putting that into Google will get you an awful lot of hits. There’s a lot of competition for that phrase, and it’s not particularly useful for your business, either. There are no buying signals in the phrase – so many people will use this phrase to learn about logo design or to examine other aspects of logo design work.\nIf you're not using internet marketing to market your business you should be. An online presence is crucial to helping potential clients and customer find your business - even if your business is small and local. (In 2017, one third of all mobile searches were local and local search was growing 50% faster than mobile searches overall.) Online is where the eyeballs are so that's where your business needs to be." ]
[ null, "https://casestudysolution.xyz/marketing-solution-Denver.jpg", null, "https://www.oastl.com/Portals/2535/iStock_60494472_MEDIUM.jpg", null ]
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https://de.webqc.org/molecularweightcalculated-180324-64.html
[ "", null, "#### Chemical Equations Balanced on 03/24/18\n\n Molecular weights calculated on 03/23/18 Molecular weights calculated on 03/25/18\nCalculate molecular weight\n 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 65 66 67 68 69 70 71 72 73 74 75 76 77 78 79 80 81 82 83 84 85 86 87 88 89 90 91 92 93 94 95\nMolar mass of MgI2 is 278,11394\nMolar mass of NaCH3CO2*3H2O is 136.07962928\nMolar mass of NaS2O4 is 151,11736928\nMolar mass of h2o2 is 34.01468\nMolar mass of C4H18 is 66,18572\nMolar mass of Cu is 63.546\nMolar mass of KMnO4 is 158.033945\nMolar mass of NO3 is 62.0049\nMolar mass of FeO is 71,8444\nMolar mass of NaOH is 39,99710928\nMolar mass of NO is 30,0061\nMolar mass of SO4 is 96.0626\nMolar mass of HCl is 36,46094\nMolar mass of Li4Ti2VCrS8 is 482.9556\nMolar mass of H2SO4 is 98,07848\nMolar mass of (NO)3 is 90.0183\nMolar mass of CO2 is 44,0095\nMolar mass of SO4 is 96.0626\nMolar mass of KCl is 74.5513\nMolar mass of PbClO34 is 786.6326\nMolar mass of CH3COONa is 82,03378928\nMolar mass of CaCl2*2H2O is 147.01456\nMolar mass of NaC6H5CO2 is 144.10316928\nMolar mass of Ca3(PO4)2 is 310,176724\nMolar mass of o is 15,9994\nMolar mass of NaOH SHCl is 108,52304928\nMolar mass of SO3 is 80,0632\nMolar mass of CH4 is 16,04246\nMolar mass of h2o is 18.01528\nMolar mass of H2O is 18.01528\nMolar mass of K2CO3 is 138,2055\nMolar mass of (NO)3 is 90.0183\nMolar mass of F2Ba5 is 724.6318064\nMolar mass of Ca(BrO4)2 is 327,8812\nMolar mass of NH4ClO4 is 117,48906\nMolar mass of CO2 is 44,0095\nMolar mass of HCl is 36,46094\nMolar mass of FeO is 71,8444\nMolar mass of CH4 is 16,04246\nMolar mass of CO2 is 44,0095\nMolar mass of Cu3P(PO4) is 316.583124\nMolar mass of CH3CH3 is 30.06904\nMolar mass of C2H2 is 26,03728\nMolar mass of Cu3(PO4) is 285.609362\nMolar mass of H2O is 18.01528\nMolar mass of CH2CH2CH2CH2 is 56,10632\nMolar mass of CH2CHCH2CH2CH2CH3 is 84,15948\nMolar mass of H2O2 is 34.01468\nMolar mass of CH3CH2CH(CH3)CH(CH2CH3)CH2CH2CH3 is 142,28168\nMolar mass of Cu(NO)3 is 153.5643\n 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 65 66 67 68 69 70 71 72 73 74 75 76 77 78 79 80 81 82 83 84 85 86 87 88 89 90 91 92 93 94 95\nCalculate molecular weight\n Molecular weights calculated on 03/23/18 Molecular weights calculated on 03/25/18\nMolecular masses on 03/17/18\nMolecular masses on 02/22/18\nMolecular masses on 03/24/17\nMit der Benutzung dieser Webseite akzeptieren Sie unsere Allgemeinen Geschäftsbedingungen und Datenschutzrichtlinien.\n© 2020 webqc.org Alle Rechte vorbehalten.\n Periodensystem der Elemente Einheiten-Umrechner Chemie Werkzeuge Chemie-Forum Chemie FAQ Konstanten Symmetrie Chemie Links Link zu uns Kontaktieren Sie uns Eine bessere Übersetzung vorschlagen? Wählen Sie eine SpracheDeutschEnglishEspañolFrançaisItalianoNederlandsPolskiPortuguêsРусский中文日本語한국어 Wie zitieren? WebQC.Org Online-Schulung kostenlose Hausaufgabenhilfe Chemie Probleme Fragen und Antworten" ]
[ null, "https://de.webqc.org/images/logo.png", null ]
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https://www.fatalerrors.org/a/common-methods-of-finding-the-greatest-common-divisor.html
[ "# greatest common divisor\n\nThe common method to solve the greatest common divisor and the least common multiple is factorization by short division, then the greatest common divisor is the product of all the common factors, and the least common multiple is the product of all the factors.", null, "In essence, finding the least common multiple is finding the most common multiple: x=m*a, y=m*b; M is the greatest common divisor, and the least common multiple is m*a*b. So we can get the relationship between the greatest common divisor and the least common multiple\n\nLCM(A,B)×GCD(A,B)=A×BLCM(A,B)×GCD(A,B)=A×B\n\nWhere LCM is the least common multiple and GCD is the greatest common divisor\n\nIt is represented by code\n\n``` // LCM:least common multiple\n// GCD:greatest common divisor\nint LCM(int a, int b) {\nint gcd = GCD(a, b);\nreturn a * b / gcd;\n}123456\n```\n\nSo the point is to find the greatest common divisor.\n\nThe common methods of finding the greatest common divisor are\n\n• Factorization method\n• Division by rotation\n• Phase change method\n• Stein algorithm\n\nThe extended Euclidean algorithm is added later. It is not only to solve the problem of finding the greatest common divisor, it should not have been added. Because this paper introduces the Euclidean algorithm, after weighing the pros and cons, we will also talk about the extended Euclidean algorithm.\n\n## Properties of common divisor\n\nBefore introducing the algorithm, we need to understand several important properties of the common divisor. These properties will be used in the following algorithms (we will prove them when we use them, so as to avoid the headache of those who are not familiar with Mathematics)\n\nIf B is the common divisor of A and B, then:\n\n• b is also the divisor of A+B, that is, b is the common divisor of A,B,A+B\n• B is also a divisor of A-B, that is, B is the common divisor of A,B,A-B\n• More generally, for any integer x, y, b is also a divisor of Ax+By, that is, b is the common divisor of A,B,Ax+By\n• According to the above property, r = A - kB = A mod B, so A mod B is also a divisor of A+B, mod is a complement operation, that is, b is the common divisor of A,B,A mod B\n\nWrite it in a formula\n\n```gcd(A,B) = gcd(B,A) = gcd(A,A+B) = gcd(A,A-B) = gcd(A,Ax+By) = gcd(A,A mod B)\n```\n\n## 1. Factorization\n\nObviously, factorization is not a good method. If you look at the following implementation code, you can see that it consumes a lot of performance, and it can't handle 0.\n\n```// greatest common divisor\nint GCD(int a, int b) {\nassert(a != 0);\nassert(b != 0);\nint min = a < b ? a : b;\nint accumulate = 1;\n\n// Break it down by 2. If 0 comes in, it's a dead loop\nwhile ((a & 1) == 0 && (b & 1) == 0) {\naccumulate *= 2;\na >>= 1;\nb >>= 1;\n}\n// Decompose by a number greater than or equal to 3\nfor (int i = 3; i <= min; i += 2) {\nwhile ((a % i) == 0 && (b % i) == 0) {\naccumulate *= i;\na /= i;\nb /= i;\n}\n}\n// Take the product of all common factors as the return value\nreturn accumulate;\n}\n```\n\nAlthough the brute force method has long code and low performance, it still has reference significance for the following algorithms.\n\n## 2. Phase change\n\ndefinition:\n\nThe original purpose of the modified subtraction method is to reduce the number of points: the number that can be divided into half and half, the number that cannot be divided into half, the number of sub denominators and sub denominators, so as to reduce the number of sub denominators and sub denominators. It's about equal numbers.\n\n1: Any given two positive integers; Judge whether they are all even numbers. If it is, it is reduced by 2; If not, perform the second step.\n\n2: Subtract the smaller number from the larger number, then compare the difference with the smaller number, and subtract the decimal from the larger number. Continue this operation until the resulting subtraction and difference are equal.\n\nThe product of some 2 in the first step and the number in the second step is the greatest common divisor, which is equivalent to not using the first step.\n\nChange to the formula:\n\n```If A > B,be gcd(A,B) = gcd(B,A-B)\nIf A < B,be gcd(A,B) = gcd(A,B-A)12\n```\n\nHere's the picture Wikipedia But in fact, this graph does not directly calculate the remainder, but subtracting the two, which is the same as the more subtractive method.", null, "prove:\n\nLet a > b, let the greatest common divisor of a and B be X, so A=aX, B=bx, where a and B are positive integers, tangent a > B.\n\nC = A-B, then there are:\n\n>C=aX−bX=(a−b)X>>C=aX−bX=(a−b)X>\n\nBecause a and B are positive integers, C can also be divided by X, that is, the greatest common divisor of a, B and C is X\n\nSo gcd(A,B) = gcd(B,A-B)\n\ncode\n\n```int GCD(int a, int b) {\nwhile (a != b) {\nif (a > b)\na = a - b;\nelse\nb = b - a;\n}\nreturn a;\n}\n```\n\n## 3. Division by rotation\n\nDivision by rotation (Chinese name) is also called Euclidean algorithm (foreign name).\n\nThe definition of the algorithm is as follows: the greatest common divisor of two positive integers A and B is equal to the greatest common divisor of the remainder divided by the smaller value.\n\nThe formula is as follows:\n\n```gcd(A, B) = gcd(B, A mod B) among:A > B1\n```\n\nprove\n\nLet a > b, let the greatest common divisor of a and B be X, so A=aX, B=bX, where a and B are positive integers and a > B.\n\nThe remainder of A divided by B: R = A - k*B, where k is A positive integer and is the quotient of A divided by B, so:\n\n>R=A−k∗B=aX−kbX=(a−kb)X>>R=A−k∗B=aX−kbX=(a−kb)X>\n\nBecause a, k and b are all positive integers, R can also be divisible by X\n\nThat is, the common divisors of A, B and R are the same, so gcd(A, B) = gcd(B, A mod B)\n\nThe least common multiple can be obtained by calculating the greatest common factor first and then quoting the formula.\n\nThe least common multiple can be obtained by many methods. The most direct method is enumeration. From small to large, the multiple of one number (such as the maximum number) can be listed. When this multiple is also the multiple of another number, the least common multiple can be obtained. Another method is to use the formula [if the external link picture transfer fails, the source station may have an anti-theft chain mechanism, so it is recommended to save the picture and upload it directly (img-ftrfvvlr-1622980225052)( https://wikimedia.org/api/rest_ Then we need to know their greatest common factor. The greatest common factor can be obtained by short division.\n\n```//recursion\nint GCD(int a, int b)\n{\nreturn b == 0 ? a : GCD(b, a%b);\n}\n//Reduce recursion to cycle\nint gcd(int m,int n)\n{\nwhile(m % n != 0)\n{\nint r = m % n;\nm = n;\nn = r;\n}\nreturn n;\n}\n```\n\n## 4. Testing\n\n```/**< Test several algorithms for finding the greatest common divisor */\n#include <stdio.h>\n#include <stdlib.h>\n\nint gcdOri(const int a, const int b);\nint gcdEA(const int a, const int b);\nint gcdMD(const int a, const int b);\nint gcdBEST(const int a, const int b);\n\nint main()\n{\nint a, b;\nscanf(\"%d %d\", &a, &b);\nprintf(\"Common algorithm: %d\\n\", gcdOri(a, b));\nprintf(\"Euclidean algorithm: %d\\n\", gcdEA(a, b));\nprintf(\"More derogation algorithm: %d\\n\", gcdMD(a, b));\nprintf(\"Best algorithm: %d\\n\", gcdBEST(a, b));\nprintf(\"Hello world!\\n\");\nsystem(\"pause\");\n}\n\n/** The most violent algorithm traverses from 2 to the smaller half of a and b\n* The efficiency is the lowest and the time complexity is O(n/2);\n*/\nint gcdOri(const int a, const int b)\n{\nint smallnum = a<b?a:b;\nint bignum = a>b?a:b;\nint i, rlt;\nif(bignum%smallnum == 0)\nrlt = smallnum;\nelse\n{\nfor(i=2; i<=smallnum/2; i++)\n{\nif((bignum%i==0) && (smallnum%i==0))\n{\nrlt = i;\n}\n}\n}\nreturn rlt;\n}\n\n/** Division by rotation, also known as Euclidean algorithm\n* Theorem: two positive integers a and B (a > b), their greatest common divisor is equal to the greatest common divisor between c and B, the remainder of a divided by B.\n* For example, 10 and 25, 25 divided by 10 quotient 2 and 5, then the greatest common divisor of 10 and 25 is equal to the greatest common divisor of 10 and 5.\n* However, when a and b are larger, the performance of a%b modular operation is lower\n*/\nint gcdEA(const int a, const int b)\n{\nint rlt;\nint smallnum = a<b?a:b;\nint bignum = a>b?a:b;\nif(bignum%smallnum == 0)\nrlt = smallnum;\nelse\n{\nrlt = gcdEA(smallnum, bignum%smallnum);\n}\nreturn rlt;\n}\n\n/** It comes from the ancient Chinese nine chapter arithmetic\n* Two positive integers a and B (a > b), their greatest common divisor is equal to the difference c of a-b and the greatest common divisor of the smaller fraction B.\n* For example, if the difference between 10 and 25 is 15, then the greatest common divisor of 10 and 25 is equal to the greatest common divisor of 10 and 15.\n* In addition, subtraction arithmetic depends on the difference between two numbers to recurse, and the number of operations must be much greater than the modular method of division\n* For example, if you calculate 1000 and 1, you have to recurse 999 times\n*/\nint gcdMD(const int a, const int b)\n{\nint rlt;\nint smallnum = a<b?a:b;\nint bignum = a>b?a:b;\nif(bignum%smallnum == 0) /**< It should be the same as bignum==smallnum */\nrlt = smallnum;\nelse\n{\nrlt = gcdMD(smallnum, (bignum-smallnum));\n}\nreturn rlt;\n}\n\n/** The best method is to combine the advantages of division and subtraction, and use shift operation on the basis of subtraction\n* For the given positive integers a and B, it is not difficult to get the following conclusion. Where gcb(a,b) means the greatest common divisor function of a,b:\n* When a and B are even, GCB (a, b) = 2 * GCB (A / 2, B / 2) = 2 * GCB (a > > 1, b > > 1)\n* When a is even and B is odd, GCB (a, b) = GCB (A / 2, b) = GCB (a > > 1, b)\n* When a is odd and B is even, GCB (a, b) = GCB (a, B / 2) = GCB (a, b > > 1)\n* When both a and B are odd numbers, gcb(a,b) = gcb(b, a-b), then A-B must be even, and the shift operation can be continued.\n*/\n\nint gcdBEST(const int a, const int b)\n{\nint rlt = 0;\nint smallnum = a<b?a:b;\nint bignum = a>b?a:b;\nif(bignum%smallnum == 0)\nrlt = smallnum;\nelse\n{\nif(!(bignum&1) && !(smallnum&1)) /**< '&1'And 1 operation means that the end and 1 in the binary system do \"and\" operation, and the result is the same as 1 but different from 0. Therefore, it can be used to judge the parity, and return 1 as odd and 0 as even */\n{\nrlt = gcdBEST(bignum>>1, smallnum>>1) << 1;\n/**< Shift right operation > > 1 is equivalent to even number / 2, on the contrary, shift left operation is equivalent to * 2 */\n}\nelse if(!(bignum&1) && smallnum&1)\n{\nrlt = gcdBEST(bignum>>1, smallnum);\n}\nelse if(bignum&1 && !(smallnum&1))\n{\nrlt = gcdBEST(bignum, smallnum>>1);\n}\nelse if(bignum&1 && smallnum&1)\n{\nrlt = gcdBEST(smallnum, bignum-smallnum);\n}\n}\nreturn rlt;\n}\n```\n\n## 5. The comparison between the two methods\n\n(1) Both of them are the methods to calculate the greatest common factor. Division is the main method to calculate the number of times, and subtraction is the main method to calculate the number of times.\n\n(2) From the form of the result, the result of division by rotation is obtained when the remainder of division is 0, while the result of subtraction is obtained when the subtraction is equal to the difference.\n\n## 6.Stein algorithm\n\nEuclidean algorithm is a traditional algorithm to calculate the greatest common divisor of two numbers, which is very efficient both theoretically and practically. However, there is a fatal defect. This defect is usually not felt when the prime number is small, and only appears when the prime number is large: in general, the integer in practical application rarely exceeds 64 bits (128 bits are allowed now). For such an integer, it is very simple to calculate the modulus between two numbers. For a 32-bit platform, only one instruction cycle is needed to compute the moduli of two integers no more than 32 bits, and only a few cycles are needed to compute the moduli of integers less than 64 bits. But for larger prime numbers, such a calculation process has to be designed by the user. In order to calculate the module of two integers with more than 64 bits, the user may have to adopt the trial and error method similar to the manual calculation process of multi digit division. This process is not only complex, but also consumes a lot of CPU time. For modern cryptographic algorithms, it is common to calculate more than 128 prime numbers, for example RSA encryption algorithm At least 500 bit key length is required, so it is urgent to design such a program to abandon division and modulus.\n\nThe Stein algorithm solves the defect of Euclidean algorithm. The Stein algorithm only has integer shift and addition and subtraction. Let's talk about the principle of Stein algorithm\n\n• If both a and b are even numbers, record the common divisor 2, and then divide them by 2 (i.e. shift 1 bit to the right);\n• If one of the numbers is even, divide the even number by 2, because 2 can't be the common divisor of the two numbers\n• If both are odd, then a = |a-b | and b = min(a,b), because if d is the common divisor of a and B, then d is also the common divisor of | a-b | and min(a,b).\n\nIt may be difficult to understand the third sentence. Here is a simple proof:\n\nLet odd numbers A > b, the common divisor of A and B be X, that is, A=jX, B=kX, where J and k are positive integers and j > k.\n\n>A−B=(j−k)X>>A−B=(j−k)X>\n\nBecause j and k are integers, X is also the common divisor of A-B.\n\nmin(A,B)=B\n\nSo the common divisor of A-B and min(A,B) is the same, because a and B are odd numbers, so A-B must be even, and even numbers can be divided and shifted.\n\n## Code implementation:\n\nThe following code takes int as the parameter,\n\n```int SteinGCD(int a, int b) {\nif (a < b) { int t = a; a = b; b = t; }\nif (b == 0) return a;\nif ((a & 1) == 0 && (b & 1) == 0)\nreturn SteinGCD(a >> 1, b >> 1) << 1;\nelse if ((a & 1) == 0 && (b & 1) != 0)\nreturn SteinGCD(a >> 1, b);\nelse if ((a & 1) != 0 && (b & 1) == 0)\nreturn SteinGCD(a, b >> 1);\nelse\nreturn SteinGCD(a - b, b);\n}123456789101112\n```\n\n## Reduce recursion to cycle\n\n```int SteinGCD(int a, int b) {\nint acc = 0;\nwhile ((a & 1) == 0 && (b & 1) == 0) {\nacc++;\na >>= 1;\nb >>= 1;\n}\nwhile ((a & 1) == 0) a >>= 1;\nwhile ((b & 1) == 0) b >>= 1;\nif (a < b) { int t = a; a = b; b = t; }\nwhile ((a = (a - b) >> 1) != 0) {\nwhile ((a & 1) == 0) a >>= 1;\nif (a < b) { int t = a; a = b; b = t; }\n}\nreturn b << acc;\n}\n```\n\nPosted by kk5595 at Jun 06, 2021 - 3:14 PM" ]
[ null, "https://www.fatalerrors.org/images/blog/60e5e9f8b54b7c98d9c1190dfcbcb5ba.jpg", null, "https://www.fatalerrors.org/images/blog/47cda2f6e168f08aa61b20f22ded25cc.jpg", null ]
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https://www.rdocumentation.org/packages/spatstat/versions/1.27-0/topics/smooth.ppp
[ "# smooth.ppp\n\n0th\n\nPercentile\n\n##### Spatial smoothing of observations at irregular points\n\nPerforms spatial smoothing of numeric values observed at a set of irregular locations. Uses Gaussian kernel smoothing and least-squares cross-validated bandwidth selection.\n\nKeywords\nmethods, smooth, spatial\n##### Usage\nsmooth.ppp(X, ..., weights = rep(1, npoints(X)), at=\"pixels\")\nmarkmean(X, ...)\nmarkvar(X, ...)\n##### Arguments\nX\nA marked point pattern (object of class \"ppp\").\n...\nArguments passed to bw.smoothppp and density.ppp to control the kernel smoothing and the pixel resolution of the result.\nweights\nOptional weights attached to the observations.\nat\nString specifying whether to compute the smoothed values at a grid of pixel locations (at=\"pixels\") or only at the points of X (at=\"points\").\n##### Details\n\nThe function smooth.ppp performs spatial smoothing of numeric values observed at a set of irregular locations. The functions markmean and markvar are wrappers for smooth.ppp which compute the spatially-varying mean and variance of the marks of a point pattern.\n\nSmoothing is performed by Gaussian kernel weighting. If the observed values are $v_1,\\ldots,v_n$ at locations $x_1,\\ldots,x_n$ respectively, then the smoothed value at a location $u$ is (ignoring edge corrections) $$g(u) = \\frac{\\sum_i k(u-x_i) v_i}{\\sum_i k(u-x_i)}$$ where $k$ is a Gaussian kernel. This is known as the Nadaraya-Watson smoother (Nadaraya, 1964, 1989; Watson, 1964). By default, the smoothing kernel bandwidth is chosen by least squares cross-validation (see below). The argument X must be a marked point pattern (object of class \"ppp\", see ppp.object). The points of the pattern are taken to be the observation locations $x_i$, and the marks of the pattern are taken to be the numeric values $v_i$ observed at these locations.\n\nThe marks are allowed to be a data frame (in smooth.ppp and markmean). Then the smoothing procedure is applied to each column of marks. The numerator and denominator are computed by density.ppp. The arguments ... control the smoothing kernel parameters and determine whether edge correction is applied. The smoothing kernel bandwidth can be specified by either of the arguments sigma or varcov which are passed to density.ppp. If neither of these arguments is present, then by default the bandwidth is selected by least squares cross-validation, using bw.smoothppp.\n\nThe optional argument weights allows numerical weights to be applied to the data. If a weight $w_i$ is associated with location $x_i$, then the smoothed function is (ignoring edge corrections) $$g(u) = \\frac{\\sum_i k(u-x_i) v_i w_i}{\\sum_i k(u-x_i) w_i}$$\n\nAn alternative to kernel smoothing is inverse-distance weighting, which is performed by idw.\n\n##### Value\n\n• If X has a single column of marks:\n• Ifat=\"pixels\"(the default), the result is a pixel image (object of class\"im\"). Pixel values are values of the interpolated function.\n• Ifat=\"points\", the result is a numeric vector of length equal to the number of points inX. Entries are values of the interpolated function at the points ofX.\nIf X has a data frame of marks:\n• Ifat=\"pixels\"(the default), the result is a named list of pixel images (object of class\"im\"). There is one image for each column of marks. This list also belongs to the classlistof, for which there is a plot method.\n• Ifat=\"points\", the result is a data frame with one row for each point ofX, and one column for each column of marks. Entries are values of the interpolated function at the points ofX.\nThe return value has attributes \"sigma\" and \"varcov\" which report the smoothing bandwidth that was used.\n\n##### References\n\nNadaraya, E.A. (1964) On estimating regression. Theory of Probability and its Applications 9, 141--142.\n\nNadaraya, E.A. (1989) Nonparametric estimation of probability densities and regression curves. Kluwer, Dordrecht.\n\nWatson, G.S. (1964) Smooth regression analysis. Sankhya A 26, 359--372.\n\ndensity.ppp, bw.smoothppp, ppp.object, im.object.\n\nSee idw for inverse-distance weighted smoothing. To perform interpolation, see also the akima package.\n\n• smooth.ppp\n• markmean\n• markvar\n##### Examples\n# Longleaf data - tree locations, marked by tree diameter\ndata(longleaf)\n# Local smoothing of tree diameter (automatic bandwidth selection)\nZ <- smooth.ppp(longleaf)\n# Kernel bandwidth sigma=5\nplot(smooth.ppp(longleaf, 5))\n# mark variance\nplot(markvar(longleaf, sigma=5))\n# data frame of marks: trees marked by diameter and height\ndata(finpines)\nplot(smooth.ppp(finpines, sigma=2))\nDocumentation reproduced from package spatstat, version 1.27-0, License: GPL (>= 2)\n\n### Community examples\n\nLooks like there are no examples yet." ]
[ null ]
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https://baylor.kattis.com/courses/CSI4144/22f/assignments/pdrqoq/problems/golombrulers
[ "Hide\n\n# Problem CGolomb Rulers\n\nA ‘Golomb ruler’ is a set of unique positive integers (called ‘marks’) which can be used to measure distances by using the difference between pairs of marks. Golomb rulers are useful in designing radio antennae and in cryptography. It’s helpful to think of the marks as being measurement marks on a real ruler. For example, $\\{ 0, 1, 3\\}$ is a Golomb ruler which can be used to measure distances of $1$ (by using $1 - 0$), $2$ (by using $3 - 1$), and $3$ (by using $3 - 0$). One extra constraint on a Golomb ruler is that there is at most one unique way to measure a given distance. So $\\{ 0, 1, 2\\}$ is not a Golomb ruler, because there are two ways to measure the distance $1$: $1-0=1$, and $2-1=1$. Another Golomb ruler is $\\{ 0, 1, 4, 6\\}$, and the distances that it can measure are\n\n$\\begin{array}{ccc} 1 = 1 - 0, & 2 = 6 - 4, & 3 = 4 - 1, \\\\ 4 = 4 - 0, & 5 = 6 - 1, & 6 = 6 - 0 \\end{array}$\n\nwhich are visually demonstrated as the arrows above the ruler in Figure 1.", null, "Figure 1: Measurements (arrows with associated lengths) that are possible with the Golomb ruler $\\{ 0,1,4,6\\}$ (marks on the bottom line).\n\nIf a Golomb ruler can be used to measure all distances from $1$ to $n$ (where $n$ is the largest mark), then it is called perfect. If the largest mark in a Golomb ruler is as small as possible for all rulers with the same number of marks, then the ruler is called optimal. The rulers above are each both perfect and optimal.\n\nFor this problem, you need to determine whether some set of numbers make a Golomb ruler, and if that Golomb ruler is perfect.\n\n## Input\n\nEach line of input contains a list of at least two but at most $25$ space-separated distinct integers in the range $[0, 2\\, 000]$. Each list of numbers includes $0$. There are at most $1\\, 000$ lines of input. Input ends at the end of file.\n\n## Output\n\nFor each input line, if the numbers given make a perfect Golomb ruler, output ‘perfect’. If they make a Golomb ruler that is not perfect, output ‘missing’ followed by a space-separated list of numbers that are missing from the ruler in the range $1$ to the largest mark, in increasing order. If the numbers do not make a Golomb ruler, output ‘not a ruler’.\n\nSample Input 1 Sample Output 1\n0 1 2\n0 3 1\n0 5\n0 1 4 9 10\n0 1 4 9 11\n\nnot a ruler\nperfect\nmissing 1 2 3 4\nnot a ruler\nmissing 6\n\nCPU Time limit 2 seconds\nMemory limit 1024 MB\nStatistics Show" ]
[ null, "https://baylor.kattis.com/problems/golombrulers/file/statement/en/img-0001.png", null ]
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https://lecturenotes.in/notes/24124-note-for-network-analysis-na-by-manjunatha-parameshwarappa
[ "×\nA DAY WITHOUT LEARNING IS A DAY WASTED\n\n# Note for Network Analysis - NA By Manjunatha Parameshwarappa\n\n• Network Analysis - NA\n• Note\n• 37 Views\nPage-1\n\n#### Note for Network Analysis - NA By Manjunatha Parameshwarappa\n\nTopic:", null, "/ 15\n\n0 User(s)\n\n#### Text from page-1\n\n0.1. NODE ANALYSIS 0.1 Node Analysis Q 2) In the circuit shown in Figure 3 determine all branch currents and the voltage across the 5 Ω resistor Steps to find a current flowing in a circuit using Node by node analysis. Analysis 3Ω 1. Identify nodes in a circuit and Label all the nodes. 2Ω +50V 2. Select one of node as reference node. +25V 5Ω 6Ω 3. Apply KCL to each node. 8Ω Figure 3 4. Solve the resulting simultaneous linear equations for the unknown node voltages using Cramer’s Solution: The circuit is labeled by nodes which is as shown in Rule. Figure 4 5. Branch currents can be calculated using node 3Ω V1 2Ω voltages +50V Q 1) In the circuit shown in Figure 1 determine all branch currents by node analysis. 6Ω +42V 4Ω +42V 4Ω 8Ω +25V 2 (Ref) 6Ω Figure 4 +- 8Ω 5Ω 10V Apply KCL to node V1 \u0014 \u0015 V1 − 50 V1 − 25 1 Figure 1 + + = 0 3+6 2+8 5 Solution: The circuit is labeled by nodes which is [0.111 + 0.1 + 0.2] V1 − 5.556 − 2.5 = 0 as shown in Figure 2 [0.4111] V1 = 8.056 8Ω V1 6Ω V1 = 19.59 +10V Current through 5 Ω resistor is 2 (Ref) I5 = Figure 2 Apply KCL to node V1 \u0015 \u0014 V1 − 42 1 V1 + 10 + + = 0 8 4 6 [0.125 + 0.25 + 0.167] V1 − 5.25 + 1.67 = 0 [0.5416] V1 = 3.58 V1 = 6.61 8.056 = 3.918A 5 Voltage across 5 Ω resistor is V = I5 × 5 = 3.918 × 5 = 19.59V Q 3) In the circuit shown in Figure 6 determine all branch currents and the voltage across the 5 Ω resistor by node analysis. 1Ω 2Ω Current through 8 Ω resistor is I8 = 10 V +- 42 − 6.61 = 4.42A 8 10 + 6.61 = 2.77A 6 Current through 4 Ω resistor is I4 = 2A Figure 5 Current through 6 Ω resistor is I6 = 10Ω 5Ω Solution: 1Ω V1 10 V +- 6.61 = 1.65A 4 Dr. Manjunatha P Professor Dept of ECE, JNN College of Engineering, Shivamogga 2Ω 5Ω V2 10Ω 2A 3 (Ref) 1\n\n#### Text from page-2\n\n0.1. NODE ANALYSIS Figure 6 Apply KCL at node V1 \u0014 \u0015 V1 − 10 V1 V1 − V2 = 0 + + 1 5 2 V1 [1 + 0.2 + 0.5] − 10 − 0.5V2 = 0 V1 [1 + 0.2 + 0.5] − 0.5V2 = 10 1.7V1 − 0.5V2 = 10 Apply KCL at node V2 \u0015 \u0014 V2 V2 − V1 + −2 = 0 10 2 −0.5V1 + V2 [0.1 + 0.5] = 2 Apply KCL at node V1 \u0014 \u0015 V1 − V2 V1 − V3 +3+8 = 0 + 3 4 V1 [0.25 + 0.333] − 0.25V2 − 0.0.25V3 + 11 = 0 0.583V1 − 0.333V2 − 0.25V3 = −11 Apply KCL at node V2 \u0014 \u0015 V2 − V1 V2 − V3 V2 = 0 + + 3 2 1 −0.333V1 + V2 [0.5 + 0.333 + 1] − 0.5V3 + 11 = 0 −0.333V1 + 1.833V2 − 0.5V3 = 0 Apply KCL at node V3 \u0014 \u0015 V3 − V1 V3 − V2 V3 + (−25) = 00 + + 4 2 5 −0.25V1 − 0.5V2 + V3 [0.25 + 0.5 + 0.2] = 25 −0.5V1 + 0.6V2 = 2 The simultaneous equations are −0.25V1 − 0.5V2 + V2 + 0.95V3 = 25 1.7V1 − 0.5V2 = 10 The simultaneous equations are −0.5V1 + 0.6V2 = 2 1.7 −0.5 = 1.02 − .25 = 0.25 = 0.77 ∆= −0.5 0.6 10 −0.5 2 0.6 6+1 V1 = = = 9.09 ∆ 0.77 1.7 10 −0.5 2 3.4 + 5 V2 = = = 10.91 ∆ 0.77 V1 is the voltage across 5 Ω resistor which is 9.09 V 0.583V1 − 0.333V2 − 0.25V3 = −11 −0.333V1 + 1.833V2 − 0.5V3 = 0 −0.25V1 − 0.5V2 + V2 + 0.95V3 = 0.583 −0.333 −0.25 −0.5 ∆ = −0.33 1.833 −0.25 −0.5 0.95 = 0.583[1.741 − .25] + 0.333[−0.313 − .125] −0.25[.165 + .458] = 0.583[1.491] + 0.333[−0.438] − 0.25[0.623] = 0.87 − 0.1458 − 0.155 = 0.5692 −11 −0.333 −0.25 0 1.833 −0.5 25 −0.5 0.95 V1 = ∆ Q 4) In the circuit shown in Figure 8 determine number of nodes and its voltages. 4Ω -3A −11[1.74 − 0.25] + 0.333[12.5] − 0.25[45.82] 0.5692 −16.39 + 4.1625 − 11.45 −23.677 = = = −41.43 0.5692 0.5692 Q 5) In the circuit shown in Figure 9 determine the current Ix 2Ω = 3Ω -8A -25A 5Ω 1Ω Figure 7 4Ω 8A -3A V1 -8A 25 V2 2Ω V3 b 3Ω 1Ω 5Ω 8Ω c I x 2Ω e +100V Solution: Figure 8 10Ω -25A a Dr. Manjunatha P Professor Dept of ECE, JNN College of Engineering, Shivamogga 3Ω 4Ω d g f 5Ω h 2\n\n#### Text from page-3\n\n0.1. NODE ANALYSIS Figure 9 Figure 11 Solution: Solution: V1 For the given circuit there is current source, to apply KCL current source has to be converted into voltage source, the modified circuit is as shown in Figure 10 +- +100V 3Ω 5Ω 3i1 2Ω 3Ω V2 15 A 4Ω i1 1Ω 8Ω V1 I x 2Ω V2 10Ω 80V + Vx - Figure 10 3 (Ref) \u0015 \u0014 V1 − 100 V1 V1 − V2 = 0 + + 8 4 2 [0.125 + 0.25 + 0.5] V1 − 12.5 − 0.5V2 = 0 0.875V1 − 0.5V2 = 12.5 \u0015 1V2 V2 − 80 V2 − V1 + + = 0 3 15 2 −0.5V1 + [0.33 + 0.067 + 0.5] V2 − 5.33 = 0 \u0014 Figure 12 Applying KCL to mesh V1 V1 − V2 V1 + − 15 = 0 1 2 (1 + 0.5)V1 − V2 = 15 1.5V1 − V2 = 15 −0.5V1 + 0.897V2 = 5.33 The simultaneous equations are i1 = 0.875V1 − 0.5V2 = 12.5 −0.5V1 + 0.897V2 = 5.33 0.875 −0.5 = 0.7848 − .25 = 0.5348 ∆= −0.5 0.897 12.5 −0.5 5.33 0.897 11.212 + 2.665 = V1 = ∆ 0.5348 13.877 = = 25.94V 0.5348 0.875 12.5 −0.5 5.33 4.66 + 6.25 10.91 V2 = = = = 20.4V ∆ 0.5348 0.5348 V1 − V2 25.94 − 20.4 = = 2.77A 2 2 Q 6) Find the loop currents i1 , i2 , i3 in the circuit shown in Figure 11 Ix = i1 1Ω 3Ω 15 A 3i1 + Vx - 2Ω V1 2 Applying KCL to mesh V2 V2 − V1 V2 + − 3i1 = 0 1 3 −V1 + [1 + 0.333]V2 − 3i1 = 0 −V1 + 1.333V2 − 3i1 = 0 −V1 + 1.333V2 − 3(0.5V1 ) = 0 −2.5V1 + 1.333V2 = 0 1.5V1 − V2 = 15 −2.5V1 + 1.333V2 = 0 1.5 −1 = 2 − 2.5 = −0.5 ∆ = −2.5 1.333 15 1 0 1.333 20 = = −40V V1 = ∆ −0.5 1.5 15 −2.5 0 37.5 V2 = = = −75V ∆ −0.5 Power delivered by dependent current source is i1 = V1 −40 = = −20 2 2 Dr. Manjunatha P Professor Dept of ECE, JNN College of Engineering, Shivamogga 3\n\n#### Text from page-4\n\n0.1. NODE ANALYSIS 2.786 − 50.6 + 1.6626 − 56.3 0.2826 − 62.79 1.764 − j2.148 + 0.922 − j1.38 = 0.2826 − 62.79 4.436 − 52.7 2.686 − j3.528 = = 0.2826 − 62.79 0.2826 − 62.79 = 15.876 10.01 V2 × 3i1 = −75 × 3 × −20 = 4.5kW = Q 7) In the network shown in Figure ?? find the current I by node voltage method. 5Ω 30∠0o V A 2+j3 Ω B 4Ω j5 Ω 6Ω 20∠0o V I 15.876 10.01 VB = = 2.646 10.01A 6 6 Q 8) In the network shown in Figure 14 find the value of E2 such that current through the 8+j8Ω is zero. I= Figure 13 Solution: Applying KCL to node V1 10 Ω VA − 306 0 VA − VB VA + + 5 2 + j3 j5 \u0014 \u0015 \u0015 \u0014 1 30 1 1 1 − VB − + + VA 5 j5 2 + j3 2 + j3 5 \u0015 \u0014 6 VB 1 30 0 VA − .2 − j0.2 + − 3.66 56.3 3.66 56.3 5 [.2 − j.2 + .2776 − 56.3] VA − .2776 − 56.3VB B 15 Ω = 0 j10 Ω 50∠0o V 10 Ω = 0 E2 = 0 = 6 [.2 − j.2 + .153 − j.23] VA − .2776 − 56.3VB = 6 [.353 − j.43] VA − .2776 − 56.3VB = 6 [.5566 − 50.6] VA − .2776 − 56.3VB = 6 Figure 14 Solution: It is given that current through the 8+j8Ω is zero this is possible only when VA = VB i., VA − VB = 0 Applying KCL to node VA Applying KCL to node V2 VB − 206 0 VB − VA VB + + 4 2 + j3 6 \u0015 \u0014 \u0015 \u0014 1 1 206 1 1 + + − VA − VB 6 4 2 + j3 2 + j3 4 \u0014 \u0015 1 VA 206 0 .16 + .25 + VA − − 3.66 56.3 3.66 56.3 4 6 6 [.16 + .25 + .277 − 56.3] VB − .277 − 56.3VA VA − 50 VA + = 0 10 j10 \u0014 \u0015 1 1 50 + VA − = 0 10 j10 10 [0.1 − j0.1] VA = 5 = 0 = 0 0.1416 − 45VA = 5 = 0 VA = 35.466 45 = 5 −.2776 − 56.3VA + [.16 + .25 + .153 − j.23] VB = 6 −0.2776 − 56.3VA + [0.563 − j0.23] VB = 5 Applying KCL to node VB −0.2776 − 56.3VA + 0.66 − 22.3VB = 5 0.5566 − 50.6VA − 0.2776 − 56.3V2 = 6 −0.2776 − 56.3VA + 0.66 − 22.3VB = 5 0.5566 − 50.6 −0.2776 − 56.3 ∆ = −0.2776 − 56.3 0.66 − 22.3 8+j8 Ω A VB − E2 VB + 15\u0015 10 \u0014 1 1 E2 + VB − 10 15 15 E2 [0.1 + 0.066] VB − 15 E2 15 E2 = 0 = 0 = 0 = 0.166VB = 2.5VB = 0.3366 − 72.9 − 0.0766 − 112.6 0.1−j0.321+0.029+j0.07 = 0.129−j0.251 = 0.2826 −62.79 0.5566 − 50.6 66 0 −0.2776 − 56.3 56 0 VB = = ∆ VA = VB E2 = 2.5 × 35.466 45 E2 = 88.656 45 Dr. Manjunatha P Professor Dept of ECE, JNN College of Engineering, Shivamogga 4" ]
[ null, "https://lecturenotes.in/assets/img/scroll-down-book.gif", null ]
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https://www.leadtools.com/help/sdk/dh/pc/histogramcommand-channel.html
[ " Channel Property (HistogramCommand) | Leadtools.ImageProcessing.Color | Raster, Medical, Document Help\n←Select platform\nIn This Topic ▼\n\n# Channel Property\n\nSummary\nGets or sets a flag that indicates the channel for which to get the histogram and the bits to use in calculating the histogram.\nSyntax\nC#\nObjective-C\nC++/CLI\nJava\nPython\n``public HistogramCommandFlags Channel { get; set; } ``\n``@property (nonatomic, assign) LTHistogramCommandFlags channel; ``\n````public int getChannel(); `\n`public void setChannel( `\n` int intValue `\n`); ````\n````public: `\n`property HistogramCommandFlags Channel { `\n` HistogramCommandFlags get(); `\n` void set ( HistogramCommandFlags ); `\n`} ````\n``Channel # get and set (HistogramCommand) ``\n\n#### Property Value\n\nValue that indicates the channel for which to get the histogram and the bits to use in calculating the histogram.\n\nRemarks\n\nIn order to speed up widely used image processing filters in LEADTOOLS, the grayscale value (master channel) of a colored image is calculated using the following formulas:\n\n````#define CalcGrayValue(r, g, b) ((L_UCHAR)(((L_UCHAR) (((2 * (L_UINT) (r)) + (5 * (L_UINT) (g)) + (L_UINT) (b) + 4) / 8)))) `\n`#define CalcGrayValue16(r, g, b) ((L_UINT16) (((2 * (L_UINT32) (r)) + (5 * (L_UINT32) (g)) + (L_UINT32) (b) + 4) / 8)) `\n`#define CalcGrayValue32(r, g, b) ((L_UINT32) (((2 * (L_UINT32) (r)) + (5 * (L_UINT32) (g)) + (L_UINT32) (b) + 4) / 8)) ````\nExample\nC#\n````using Leadtools; `\n`using Leadtools.Codecs; `\n`using Leadtools.ImageProcessing.Color; `\n` `\n` `\n`public void HistogramCommandExample() `\n`{ `\n` // Load an image `\n` RasterCodecs codecs = new RasterCodecs(); `\n` codecs.ThrowExceptionsOnInvalidImages = true; `\n` `\n` RasterImage image = codecs.Load(Path.Combine(LEAD_VARS.ImagesDir, \"Master.jpg\")); `\n` `\n` // Prepare the command `\n` HistogramCommand command = new HistogramCommand(); `\n` long[] histogramValues; `\n` //Create the red-channel histogram. `\n` command.Channel = HistogramCommandFlags.Red | HistogramCommandFlags.AllBits; `\n` command.Run(image); `\n` codecs.Save(image, Path.Combine(LEAD_VARS.ImagesDir, \"Result.jpg\"), RasterImageFormat.Jpeg, 24); `\n` histogramValues = command.Histogram; `\n` `\n`} `\n` `\n`static class LEAD_VARS `\n`{ `\n` public const string ImagesDir = @\"C:\\LEADTOOLS22\\Resources\\Images\"; `\n`} ````\nRequirements" ]
[ null ]
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https://deepai.org/publication/a-frequency-domain-characterization-of-optimal-error-covariance-for-the-kalman-bucy-filter
[ "DeepAI\n\n# A Frequency-Domain Characterization of Optimal Error Covariance for the Kalman-Bucy Filter\n\nIn this paper, we discover that the trace of the division of the optimal output estimation error covariance over the noise covariance attained by the Kalman-Bucy filter can be explicitly expressed in terms of the plant dynamics and noise statistics in a frequency-domain integral characterization. Towards this end, we examine the algebraic Riccati equation associated with Kalman-Bucy filtering using analytic function theory and relate it to the Bode integral. Our approach features an alternative, frequency-domain framework for analyzing algebraic Riccati equations and reduces to various existing related results.\n\n07/23/2022\n\n### Low-Complexity Acoustic Echo Cancellation with Neural Kalman Filtering\n\nThe Kalman filter has been adopted in acoustic echo cancellation due to ...\n12/06/2017\n\n### A Kalman Filter Approach for Biomolecular Systems with Noise Covariance Updating\n\nAn important part of system modeling is determining parameter values, pa...\n03/16/2021\n\n### SymPKF: a symbolic and computational toolbox for the design of parametric Kalman filter dynamics\n\nRecent researches in data assimilation lead to the introduction of the p...\n06/16/2020\n\n### On the Mathematical Theory of Ensemble (Linear-Gaussian) Kalman-Bucy Filtering\n\nThe purpose of this review is to present a comprehensive overview of the...\n03/08/2016\n\n### Frequency estimation in three-phase power systems with harmonic contamination: A multistage quaternion Kalman filtering approach\n\nMotivated by the need for accurate frequency information, a novel algori...\n03/24/2020\n\n### On the Complexity and Approximability of Optimal Sensor Selection and Attack for Kalman Filtering\n\nGiven a linear dynamical system affected by stochastic noise, we conside...\n11/12/2021\n\n### Neural optimal feedback control with local learning rules\n\nA major problem in motor control is understanding how the brain plans an...\n\n## I Introduction\n\nThe Kalman–Bucy filter is the optimal state estimator for linear continuous-time systems with white Gaussian noises. It is well known that the optimal state estimation error covariance attained by the Kalman–Bucy filter in steady state satisfies the algebraic Riccati equation [2, 3, 4], which, however, does not provide an analytical expression of the error covariance. Over the years, various upper bounds and lower bounds have been obtained for the error covariance (see, e.g., and the references therein). Meanwhile, nonrecursive algebraic solutions have been obtained as well (see, e.g., [6, 3, 7] and the references therein).\n\nIn this paper, we develop an alternative approach towards this problem from the viewpoint of the Bode integral . Bode integral was the first and arguably the best known result to analyze the fundamental limitations of feedback control systems using analytic function theory [9, 10, 11, 12, 13, 14, 15]. In particular, the Bode integral is implied by the Poisson–Jensen formula . This line of research has been of continuing interest to the control community [17, 18], and was related to information theory in recent years as well [19, 20, 21, 22, 23, 24, 25, 26, 27]; such results together with inspired us to reexamine the Kalman–Bucy filter (in steady-state) using analytic function theory, e.g., the Poisson–Jensen formula, which will be seen to play an essential role in our analysis.\n\nIn particular, we first develop from the Poisson–Jensen formula a counterpart of Jensen’s formula, based on which we obtain an analytical expression of the trace of the division of the optimal output estimation error covariance over the noise covariance by the Kalman–Bucy filter; this is given in terms of the plant dynamics, e.g., the unstable poles, and the noise statistics in a frequency-domain integral characterization. The analysis mainly concerns examining the algebraic Riccati equation associated with the Kalman–Bucy filter using analytic function theory.\n\nWe compare our result with the existing related results in [29, 30, 31, 32, 33], and our integral characterization is seen to be the most generic and reduces to all of them. Specifically, the case when the plant is stable and the plant output is a scalar process was considered in . The authors of then analyzed the case when the plant output is scalar but the plant is not necessarily stable. The following results in \n\nconsidered the case when the process noise is relatively small in variance (and in the limit, zero) compared with the observation noise. Most recently, the case when the plant output is a vector process while the observation noise is with an identity covariance matrix was investigated in\n\n. In addition, discussions on the dual problem in control can be found in [30, 32].\n\nThe remainder of the paper is organized as follows. Section II introduces the technical preliminaries. Section III introduces a counterpart of Jensen’s formula. In Section IV, we examine the Kalman–Bucy filter using algebraic function theory and presents an integral characterization of the optimal output estimation error covariance. Relevant discussions and interpretations are also presented. Concluding remarks are given in Section IV.\n\nFor analysis and discussions on the discrete-time Kalman filters, see our parallel work presented in\n\n.\n\n## Ii Preliminaries\n\nIn this section, we introduce some relevant notions from stochastic processes, and briefly review the basic properties of the Kalman–Bucy filter.\n\n### Ii-a Notations and Basic Concepts\n\nIn this paper, we consider real-valued continuous zero-mean random variables and vectors, as well as continuous-time stochastic processes. We denote random variables and vectors using boldface letters. The logarithm\n\nis defined with base , and all functions are assumed to be measurable.\n\nA zero-mean stochastic process is said to be (asymptotically) stationary if for any , the (asymptotic) correlation matrix\n\nexists. The (asymptotic) power spectrum of is then defined as\n\n Φx(ω)=∫∞−∞Rx(τ)e−jωτdτ.\n\nIt can be verified that is positive semidefinite. In the scalar case, we denote by . For the inversion,\n\n Rx(τ) =limt→∞E[x(t+τ)xT(t)] =12π∫∞−∞Φx(ω)ejωτdω.\n\nMoreover, the (asymptotic) covariance matrix of is given by\n\n Σx=limt→∞E[x(t)xT(t)]=Rx(0)=12π∫∞−∞Φx(ω)dω.\n\nIn the scalar case, reduces to (asymptotic) variance . Moreover, if is (asymptotically) white, then is a constant for all , and\n\nwhere is the Dirac delta function.\n\n### Ii-B The Kalman–Bucy Filter\n\nConsider the continuous-time Kalman–Bucy filtering system depicted in Fig. 1, where the system is linear time-invariant (LTI) with state-space model given by\n\n {˙x(t)=Ax(t)+w(t),y(t)=Cx(t)+v(t),\n\nwhere is the state to be estimated, is the system output, is the process noise, and is the measurement noise. The system matrices are and , and is assumed to be detectable. Suppose that and are white Gaussian with covariance matrices\n\n E[w(t+τ)wT(t)]=Wδ(τ), W≥0,\n\nand\n\n E[v(t+τ)vT(t)]=Vδ(τ), V>0,\n\nrespectively, and that the initial state is Gaussian with covariance satisfying . Furthermore, , , and are assumed to be mutually uncorrelated.\n\nThe Kalman–Bucy filter is given by\n\nwhere , , , and . Herein, denotes the Kalman gain, which is given by\n\n K(t)=P(t)CTV−1, (1)\n\nwhere denotes the state estimation error covariance matrix as\n\n P(t)=E[[x(t)−¯¯¯x(t)][x(t)−¯¯¯x(t)]T].\n\nHerein, is obtained using the Riccati equation\n\n ˙P(t)=AP(t)+P(t)AT+W−P(t)CTV−1CP(t),\n\nwith\n\nIt is known that the Kalman–Bucy filtering system converges, i.e., the estimator is asymptotically stable, the state estimation error and the output estimation error are asymptotically stationary, and is asymptotically white, under the assumption that the system is detectable. Moreover, in steady state, the optimal state estimation error covariance matrix\n\nattained by the Kalman–Bucy filter satisfies the algebraic Riccati equation\n\n AP+PAT+W−PCTV−1CP=0, (2)\n\nwhereas the steady-state Kalman gain is given by\n\n K=PCTV−1. (3)\n\nIn addition, the optimal steady-state output estimation error covariance matrix is found to be\n\n Σz−¯¯¯y =limt→∞E[[z(t)−¯¯¯y(t)][z(t)−¯¯¯y(t)]T] =CPCT, (4)\n\nwhere denotes the true value of the system output (in comparison, denotes the measured value of the system output). Moreover, when , (II-B) reduces to\n\n σ2z−¯¯¯y=limt→∞E[[z(t)−¯¯¯y(t)]2].\n\nIt is also worth mentioning that\n\n limt→∞E[e(t+τ)eT(t)]=Vδ(τ).\n\n## Iii A Counterpart of Jensen’s Formula\n\nIn this section, we first examine the Poisson–Jensen formula (see, e.g., Appendix C of ) for a special class of analytic functions, and obtain a formula that will be essential for the rest of the paper.\n\n###### Proposition 1\n\nLet\n\n f(s)=p(s)q(s) (5)\n\nbe a rational transfer function for which the numerator polynomial and denominator polynomial are both of order . Suppose that all the poles of are stable and that has no zeros on the imaginary axis. In addition, suppose that\n\n lims→∞f(s)=1. (6)\n\nThen,\n\n 12π∫∞−∞ln|f(jω)|dω=lims→∞12sln|f(s)|+m∑i=1max{0,R[φi]}, (7)\n\nwhere denote the zeros of .\n\nSee Appendix A.\n\nNote that in the discrete-time case (for the unit disk), Jensen’s formula is a consequence of the more general Poisson–Jensen formula . Likewise in the continuous-time case (for the half plane), (7) is also a consequence of the more general Poisson–Jensen formula (39). As such, (7) as well as the subsequent (2) may be viewed as the continuous-time (half-plane) counterparts of the discrete-time (unit-disk) Jensen’s formula.\n\nMore generally, when not necessarily all the poles of are stable, we can obtain the following result based on Proposition 1.\n\n###### Proposition 2\n\nLet\n\n f(s)=p(s)q(s) (8)\n\nbe a rational transfer function for which the numerator polynomial and denominator polynomial are both of order . Suppose that has no zeros on the imaginary axis and that\n\n lims→∞f(s)=1. (9)\n\nThen,\n\n 12π∫∞−∞ln|f(jω)|dω =lims→∞12sln|f(s)|+∑imax{0,R[φi]} −∑jmax{0,R[ηj]}, (10)\n\nwhere denote the zeros of and denote its poles.\n\nSee Appendix B.\n\n## Iv Optimal Error Covariance by the Kalman–Bucy Filter\n\nWe now study the optimal output estimation error covariance matrix by the continuous-time Kalman–Bucy filter, which is determined by the plant dynamics and the noise statistics in an integral characterization.\n\n###### Theorem 1\n\nThe optimal output estimation error covariance matrix by the Kalman–Bucy filter satisfies\n\n tr(Σz−¯¯¯yV−1) =tr(CPCTV−1) =12π∫∞−∞ln[detΦy(ω)detV]dω +2m∑i=1max{0,R[λi(A)]}, (11)\n\nwhere\n\n Φy(ω)=C(jωI−A)−1W(−jωI−A)−TCT+V, (12)\n\nand\n\ndenote the eigenvalues of\n\n.\n\nSee Appendix C.\n\nOn the right-hand side of (1), the term\n\n m∑i=1max{0,R[λi(A)]} (13)\n\nquantifies the instability of the system [36, 37]. Moreover, when is stable, i.e., when all the eigenvalues of matrix satisfy , is stationary and thus\n\n C(jωI−A)−1W(−jωI−A)−TCT+V (14)\n\ndenotes the power spectrum of ; in general, however, needs not to be stable, and hence the function\n\n C(sI−A)−1W(−sI−A)−TCT+V (15)\n\nis a Popov function (see, e.g., , for a detailed discussion).\n\nNote that an alternative proof of (V-C) is given by as\n\n 12π∫∞−∞ln∣∣∣det[I+C(jωI−A)−1K]−1∣∣∣2dω =12π∫∞−∞ln∣∣det[I−C[jωI−(A−KC)]−1K]∣∣2dω =−tr(CK)+2m∑i=1max{0,R[λi(A−KC+KC)]} =−tr(CPCTV−1)+2m∑i=1max{0,R[λi(A)]}. (16)\n\nOne may refer to Appendix A of for further details on this.\n\n### Iv-a Interpretation from the Viewpoint of Bode Integral\n\nEquation (V-C) in the proof of Theorem 1, in particular,\n\n 12π∫∞−∞ln∣∣∣det[I+C(jωI−A)−1K]−1∣∣∣dω =−12tr(CPCTV−1)+m∑i=1max{0,R[λi(A)]}, (17)\n\ncan also be obtained as a consequence of the (continuous-time) Bode integral ; it is interesting to discover that such a relation exists between these two top equations , namely algebraic Riccati equation and Bode integral, of the control field. Specifically, the estimator may be viewed as a feedback system, and thus the Bode integral can be obtained for its sensitivity from to (see Fig. 1). Indeed, if we denote\n\n L(s)=C(sI−A)−1K, (18)\n\nthen (IV-A) can be rewritten as\n\n 12π∫∞−∞ln∣∣det[I+L(jω)]−1∣∣dω=−lims→∞12strL(s)+m∑i=1max{0,R[λi]}, (19)\n\nwhere denote the poles of . Herein, we have used the fact that\n\n m∑i=1max{0,R[λi]}=m∑i=1max{0,R[λi(A)]}, (20)\n\nwhich holds since the system is detectable (all the unstable modes of the system are observable) and thus the unstable poles of correspond to the eigenvalues of with real parts larger than zero. It is also worth mentioning that when it is further assumed that , (19) reduces to\n\n 12π∫∞−∞ln∣∣∣11+L(jω)∣∣∣dω=−lims→∞12sL(s)+m∑i=1max{0,R[λi]}. (21)\n\nOn the other hand, it can be verified that the Bode integrals given in (19) and (21) are implied by (7) by letting and , respectively. In addition, note that one common instance for\n\n lims→∞s{ln∣∣det[I+L(s)]−1∣∣}=0 (22)\n\nto hold is that all the entries of have at least two more poles than zeros, which is not satisfied in the case of Kalman–Bucy filtering as discussed in this paper.\n\n### Iv-B A More Explicit Expression of (1)\n\nUsing (2), we can obtain a more explicit form for the formula in (1).\n\n###### Theorem 2\n\nEquality (1) can be rewritten as\n\n tr(Σz−¯¯¯yV−1) =tr(CPCTV−1) =∑jmax{0,R[φj]}−∑kmax{0,R[ηk]} +2m∑i=1max{0,R[λi(A)]}, (23)\n\nwhere denote the zeros of and denote its poles.\n\nBy invoking (2), it holds that\n\n 12π∫∞−∞ln[detΦy(ω)detV]dω =12π∫∞−∞lndet[Φy(ω)V−1]dω =lims→∞12s{lndet[Φy(s)V−1]}+∑jmax{0,R[φj]} −∑kmax{0,R[ηk]}.\n\nSince\n\n Φy(s)V−1=C(sI−A)−1W(−sI−A)−TCTV−1+I,\n\nit follows from (Appendix A) that\n\n lims→∞12s{lndet[Φy(s)V−1]}=0,\n\nNoting also (1), (2) follows by simple substitution.\n\nConcerning the terms in (2), it holds in general that\n\n ∑kmax{0,R[ηk]}≤2m∑i=1max{0,R[λi(A)]}, (24)\n\nsince the unstable poles of must belong to the set of eigenvalues with real parts larger than zero, while not all such eigenvalues of may be present in the set of unstable poles of . Note that this is different from the case of , as discussed in the proof of Theorem 1; in such a case, since the system is detectable (all the unstable modes of the system are observable), the set of unstable poles of is exactly the same as the set of eigenvalues of with real parts larger than zero.\n\n### Iv-C Some Straightforward Corollaries\n\nUsing the fact that\n\n λ––(CTV−1C)trP ≤tr(CPCTV−1) =tr(V−12CPCTV−12) ≤¯¯¯λ(CTV−1C)trP, (25)\n\nwe could obtain lower and upper bounds on based on (1) as\n\n trP +2m∑i=1max{0,R[λi(A)]}}, (26)\n\nand\n\n trP +2m∑i=1max{0,R[λi(A)]}}. (27)\n\nOne might also compare our bounds with those in, e.g., , which, however, goes beyond the scope of this paper.\n\nWe now consider some special cases of Theorem 1.\n\n###### Corollary 1\n\nIf , and suppose that and are white Gaussian with covariance matrix and variance , respectively, then\n\n σ2z−¯¯¯y=CPCT =σ2v2π∫∞−∞ln[Sy(ω)σ2v]dω+2σ2vm∑i=1max{0,R[λi(A)]}, (28)\n\nwhere\n\n Sy(ω)=C(jωI−A)−1W(−jωI−A)−TCT+σ2v. (29)\n###### Corollary 2\n\nIf , and suppose that and are white Gaussian with variances and , respectively, then\n\n P =1C2{σ2v2π∫∞−∞ln[C2∣∣∣1jω−A∣∣∣2σ2wσ2v+1]dω +2σ2vmax{0,R[A]}}. (30)\n\n### Iv-D Relation to Existing Results\n\nWe now present a list of comparisons with existing results in the related works. It will be seen that our result in (1) is the most generic and reduces to all the listed ones, although they have adopted different approaches.\n\n• When and is stable, is stationary and\n\n C(jωI−A)−1W(−jωI−A)−TCT (31)\n\ndenotes its power spectrum . Hence, (1) reduces to\n\n (32)\n\nThis coincides with the result in .\n\n• When , , and , where , (1) reduces to\n\n σ2z−¯¯¯y =CPCT =12π∫∞−∞ln[∣∣C(jωI−A)−1B∣∣2+1]dω +2m∑i=1max{0,R[λi(A)]}. (33)\n\nThis coincides with the conclusion in .\n\n• When , , and , (1) reduces to\n\n σ2z−¯¯¯y =CPCT =12π∫∞−∞ln[ε2C2∣∣∣1jω−A∣∣∣2+1]dω +2m∑i=1max{0,R[A]}. (34)\n\nThis coincides with the corresponding result in .\n\n• When , , and , (1) reduces to\n\n σ2z−¯¯¯y=CPCT=2m∑i=1max{0,R[λi(A)]}. (35)\n\nThis also coincides with conclusion in .\n\n• When , (1) reduces to\n\n trΣz−¯¯¯y =tr(CPCT) =12π∫∞−∞lndetΦy(ω)dω +2m∑i=1max{0,R[λi(A)]}, (36)\n\nwhere\n\n Φy(ω)=C(jωI−A)−1W(−jωI−A)−TCT+I. (37)\n\nThis coincides with the result in .\n\nDiscussions on the dual problem in control can be found in, e.g., [30, 32].\n\nIndeed, equation (32) is referred to as the Yovits–Jackson formula in . In a broad sense, the Yovits–Jackson formula can be viewed as the continuous-time counterpart of the Kolmogorov–Szegö formula [4, 35, 41, 42, 43] in the discrete-time case. For the multiple-input multiple-output (MIMO) case, when is stationary ( is stable), (1) reduces to\n\n tr(Σz−¯¯¯yV−1) =tr(CPCTV−1) =12π∫∞−∞ln[detΦy(ω)detV]dω =12π∫∞−∞ln{det[Φz(ω)+V]detV}dω, (38)\n\nwhich may be viewed as the as the continuous-time counterpart of the Wiener–Masani formula [44, 41, 43].\n\nAs we pointed out in , our formula therein generalizes the Kolmogorov–Szegö formula and the Wiener–Masani formula to the non-stationary case, and correspondingly in this paper, we have generalized the Yovits–Jackson formula to the MIMO case as well as the non-stationary case.\n\n## V Conclusion\n\nIn this paper, we have shown that the trace of the division of the optimal output estimation error covariance over the noise covariance attained by the Kalman–Bucy filter can be explicitly expressed in terms of the plant dynamics and noise statistics in a frequency-domain integral characterization. We have also discussed the relation of our integral characterization to the Bode integral. Possible future research directions include analysis of other classes of algebraic Riccati equations.\n\n## Appendix\n\n### V-a Proof of Proposition 1\n\nIt follows from the Poisson–Jensen formula for the half plane that for every point , ,\n\n 1π∫∞−∞σ0σ20+(ω−ω0)2ln|f(jω)|dω=ln|f(s0)|−∑iln∣∣∣s0−zis0+z∗i∣∣∣, (39)\n\nwhere denote the nonminimum-phase zeros of and denote the complex conjugate of . Hence, taking , we have\n\n 1π∫∞−∞σ0σ20+ω2ln|f(jω)|dω=ln|f(σ0)|−∑iln∣∣∣σ0−ziσ0+z∗i∣∣∣. (40)\n\nAs such,\n\n limσ0→∞σ0[12π∫∞−∞σ0σ20+ω2ln|f(jω)|dω] =limσ0→∞[12σ0ln|f(σ0)|] (41)\n\nIt is known that\n\n limσ0→∞σ0[12π∫∞−∞σ0σ20+ω2ln|f(jω)|dω] =limσ0→∞[12π∫∞−∞σ20σ20+ω2ln|f(jω)|dω] =12π∫∞−∞ln|f(jω)|dω,\n\nand\n\n −limσ0→∞(12σ0∑iln∣∣∣σ0−ziσ0+z∗i∣∣∣) =∑iR[zi] =m∑i=1max{0,R[φi]}.\n\nWe finally consider the remaining term in (V-A):\n\n limσ0→∞[12σ0ln|f(σ0)|]. (42)\n\nDenote , and . Since , we have . In addition, as , we have\n\n f(s) =p(s)q(s)=pmsm+pm−1sm−1+⋯+p1s+p0qmsm+qm−1sm−1+⋯+q1s+q0 =1+pm−1pm1s+pm−2pm1s+⋯+p1pm1sm−1+p0pm1sm1+qm−1qm1s+qm−2qm1s+⋯+q1qm1sm−1+q0qm1sm =1+(pm−1pm−qm−1qm)1s+O(1s2).\n\nHence,\n\n limσ0→∞[12σ0ln|f(σ0)|] =limσ0→∞{12σ0ln[1+(pm−1pm−qm−1qm)1σ0+O(1σ20)]} =limσ0→∞{12[(pm−1pm−qm−1qm)+O(1σ0)]} =12(pm−1pm−qm−1qm).\n\nIt thus follows that the limit (42) always exists; it is always finite, although it can be when . This completes the proof.\n\n### V-B Proof of Proposition  2\n\nRewrite\n\n f(s)=p(s)q(s)=p(s)l(s)l(s)q(s),\n\nwhere is chosen as a polynomial of satisfying the following conditions:\n\n• is with the same order as those of and ;\n\n• all the zeros of are nonminimum phase;\n\n• there is no pole-zero cancellation between and or between and ; and\n\n• the following relation holds:\n\n lims→∞p(s)l(s)=lims→∞l(s)q(s)=1.\n\nTherefore, the zeros of are given by the zeros of , while the poles of are given by the zeros of . On the other hand, the poles of both and are stable. Then, using Proposition 1, we arrive at\n\n 12π∫∞−∞ln|f(jω)|dω =12π∫∞−∞ln∣∣∣p(jω)l(jω)∣∣∣dω−12π∫∞−∞ln∣∣∣q(jω)l(jω)∣∣∣dω =lims→∞12sln∣∣∣p(s)l(s)∣∣∣+∑imax{0,R[φi]} −lims→∞12sln∣∣∣q(s)l(s)∣∣∣−∑jmax{0,R[ηj]} =lims→∞12sln∣∣∣p(s)q(s)∣∣∣+∑imax{0,R[φi]} −∑jmax{0,R[ηj]} =lims→∞12sln|f(s)|+∑imax{0,R[φi]} −∑jmax{0,R[ηj]}.\n\nThis completes the proof.\n\n### V-C Proof of Theorem 1\n\nFor all , it holds that\n\n AP+PAT=(A−sI)P+P(A+sI)T.\n\nHence, (2) can be rewritten as\n\n (A−sI)P+" ]
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https://weather.meta5.us/Abbreviations.html
[ "", null, "#### GFS And NAM Abbreviations\n\n• DT = The day of the month, denoted by the standard three or four letter abbreviation\n• HR = Hour of the day in UTC time. This is the hour at which the forecast is valid, or if the forecast is valid for a period, the end of the forecast period.\n• N/X = nighttime minimum/daytime maximum surface temperatures.\n• TMP = surface temperature valid at that hour.\n• DPT = surface dewpoint valid at that hour.\n• CLD = forecast categories of total sky cover valid at that hour.\n• CL - clear;\n• FW - > 0 to 2 octas of total sky cover;\n• SC - > 2 to 4 octas of total sky cover;\n• BK - > 4 to < 8 octas of total sky cover;\n• OV - 8 octas of total sky cover or totally obscured.\n• WDR = forecasts of the 10-meter wind direction at the hour, given in tens of degrees.\n• WSP = forecasts of the 10-meter wind speed at the hour, given in knots.\n• P06 = probability of precipitation (PoP) during a 6-h period ending at that time.\n• P12 = PoP during a 12-h period ending at that time.\n• Q06 = quantitative precipitation forecast (QPF) category for liquid equivalent precipitation amount during a 6-h period ending at that time.\n• 0 = no precipitation expected;\n• 1 = 0.01 - 0.09 inches;\n• 2 = 0.10 - 0.24 inches;\n• 3 = 0.25 - 0.49 inches;\n• 4 = 0.50 - 0.99 inches;\n• 5 = > 1.00 inches.\n• Missing forecasts are denoted by 9.\n• Q12 = QPF category for liquid equivalent precipitation amount during a 12-h period ending at the indicated time.\n• 0 = no precipitation expected;\n• 1 = 0.01 - 0.09 inches;\n• 2 = 0.10 - 0.24 inches;\n• 3 = 0.25 - 0.49 inches;\n• 4 = 0.50 - 0.99 inches;\n• 5 = 1.00 - 1.99 inches;\n• 6 = > 2.00 inches.\n• Missing forecasts are denoted by 9.\n• SNW = snowfall categorical forecasts during a 24-h period ending at the indicated time.\n• 0 = no snow or a trace expected;\n• 1 = > a trace to < 2 inches expected;\n• 2 = 2 to < 4 inches;\n• 4 = > 4 to < 6 inches;\n• 6 = > 6 to < 8 inches;\n• 8 = > 8 inches.\n• A missing forecast is denoted by 9; forecasts are disseminated only for the period of September 1 - May 31.\n• T06 = probability of thunderstorms/conditional probability of severe thunderstorms during the 6-hr period ending at the indicated time.\n• T12 = probability of thunderstorms/conditional probability of severe thunderstorms during the 12-hr period ending at the indicated time.\n• POZ = conditional probability of freezing pcp occurring at the hour.\n• POS = conditional probability of snow occurring at the hour.\n• TYP = conditional precipitation type at the hour.\n• S = pure snow or snow grains\n• Z = freezing rain/drizzle, ice pellets, or anything mixed with freezing precip\n• R = pure rain/drizzle or rain mixed with snow\n• CIG = ceiling height categorical forecasts at the hour.\n• 1 = ceiling height of < 200 feet;\n• 2 = ceiling height of 200 - 400 feet;\n• 3 = ceiling height of 500 - 900 feet;\n• 4 = ceiling height of 1000 - 1900 feet;\n• 5 = ceiling height of 2000 - 3000 feet;\n• 6 = ceiling height of 3100 - 6500 feet;\n• 7 = ceiling height of 6600 - 12,000 feet;\n• 8 = ceiling height of > 12,000 feet or unlimited ceiling.\n• VIS = visibility categorical forecasts at the hour.\n• 1 = visibility of < 1/2 mi;\n• 2 = visibility of 1/2 - < 1 mi;\n• 3 = visibility of 1 to < 2 mi;\n• 4 = visibility of 2 to < 3 mi;\n• 5 = visibility of 3 to 5 mi;\n• 6 = visibility of 6 mi;\n• 7 = visibility of > 6 mi.\n• OBV = obstruction to vision categorical forecasts at the hour.\n• N = none of the following;\n• HZ = haze, smoke, dust;\n• BR = mist (fog with visibility > 5/8 mi);\n• FG = fog or ground fog (visibility < 5/8 mi);\n• BL = blowing dust, sand, snow.\n\n#### NBH Abbreviations\n\n• UTC = forcast valid hour (in UTC) (date as in line 1, unless past 23Z - then the following date is valid)\n• TMP = temperature, degrees F\n• TSD* = standard deviation of temperature, degrees F\n• DPT = dew point temperature, degrees F\n• DSD* = dew point temperature standard deviation, degrees F\n• SKY = sky cover, percent\n• SSD* = sky cover standard deviation, percent\n• WDR = wind direction, nearest tens degrees (northerly=36; easterly=9; calm=00)\n• oceanic-only stations only have WDR for cycles=0,7,12,19\n• WSP = wind speed, knots\n• WSD* = wind speed standard deviation, knots\n• GST = wind gust, knots\n• GSD* = wind gust standard deviation, knots\n• P01 = 1-hour PoP, percent\n• P06 = 6-hour PoP, percent\n• Q01 = 1-hour QPF, 1/100 inches\n• T01 = 1-hour thunderstorm probability, percent\n• PZR = conditional probability of freezing rain, percent\n• PSN = conditional probability of snow, percent\n• PPL = conditional probability of sleet / ice pellets, percent\n• PRA = conditional probability of rain, percent\n• S01 = 1-hour snow amount, 1/10 inches\n• SLV = snow level, 100s feet MSL\n• I01 = 1-hour ice amount, 1/100 inches\n• CIG* = ceiling height, 100s feet (>5000 ft reported to the nearest 1000 ft; -88=unlimited)\n• MVC* = probability of ceiling MVFR flight conditions (ceiling <= 3000 ft), percent\n• IFC* = probability of ceiling IFR flight conditions (ceiling < 1000 ft), percent\n• LIC* = probability of ceiling LIFR flight conditions (ceiling < 500 ft), percent\n• LCB** = lowest cloud base, 100s feet (>5000 ft reported to the nearest 1000 ft; -88=unlimited)\n• VIS = visibility, 1/10th miles (rounded to nearest mile for values >= 1 mile) [Note: values before approx. 2019-06-01 are in full miles]\n• MVV* = probability of visibility MVFR flight conditions (visibility <= 5 miles), percent\n• IFV* = probability of visibility IFR flight conditions (visibility < 3 miles), percent\n• LIV* = probability of visibility LIFR flight conditions (visibility < 1 mile), percent\n• MHT = mixing height, 100s feet MSL\n• TWD = transport wind direction, nearest tens degrees (northerly=36; easterly=9; calm=00)\n• TWS = transport wind speed, knots (<0.5 knots will be listed as 0 (calm))\n• HID = Haines Index (unitless)\n• SOL** = instantaneous solar radiation, 10s W/m2 (ex: 8=80 W/m2; non-zero values < 10=1)\n\n#### NBS Abbreviations\n\n• DT (or blank) = forcast valid date (in UTC)\n• UTC = forcast valid hour (in UTC)\n• FHR = model forecast hour (number of hours forward from forecast date/cycle)\n• TXN** = (formerly X/N or N/X) = 18-hour maximum and minimum temperatures, degrees F.\n• Min is between 00Z-18Z and reported at 12Z (except Guam)\n• Max is between 12z(current day)-06Z(next day) and reported at 00z(following day) (except Guam)\n• Guam stations report Tmax at 12z and Tmin at 00z.\n• XND* = standard deviation of maximum or minimum temperature, degrees F\n• TMP = temperature, degrees F\n• TSD* = standard deviation of temperature, degrees F\n• DPT = dew point temperature, degrees F\n• DSD* = dew point temperature standard deviation, degrees F\n• SKY = sky cover, percent\n• SSD* = sky cover standard deviation, percent\n• WDR = wind direction, nearest tens degrees (northerly=36; easterly=9; calm=00)\n• oceanic-only stations only have WDR for cycles=0,7,12,19\n• WSP = wind speed, knots (<0.5 knots will be listed as 0 (calm))\n• WSD* = wind speed standard deviation, knots\n• GST = wind gust, knots\n• GSD* = wind gust standard deviation, knots\n• P06 = 6-hour PoP, percent\n• P12 = 12-hour PoP, percent\n• Q06 = 6-hour QPF, 1/100 inches\n• Q12 = 12-hour QPF, 1/100 inches\n• DUR = Duration of precipitation, hours\n• T03 = 3-hour thunderstorm probability, percent\n• T06* = 6-hour thunderstorm probability, percent\n• T12 = 12-hour thunderstorm probability, percent\n• PZR = conditional probability of freezing rain, percent\n• PSN = conditional probability of snow, percent\n• PPL = conditional probability of sleet / ice pellets, percent\n• PRA = conditional probability of rain, percent\n• S06 = 6-hour snow amount, 1/10 inches\n• SLV** = snow level, 100s feet MSL (rounded to nearest 1000 ft for values > 10,000 ft)\n• I06 = 6-hour ice amount, 1/100 inches\n• CIG** = ceiling height, 100s feet (>5000 ft reported to the nearest 1000 ft; -88=unlimited)\n• IFC* = probability of ceiling IFR flight conditions (ceiling < 1000 ft), percent\n• LCB** = lowest cloud base, 100s feet (>5000 ft reported to the nearest 1000 ft; -88=unlimited)\n• VIS** = visibility, 1/10th miles up to 10 miles (rounded to nearest mile for values >= 1 mile; VIS > 10 miles = 100)\n• IFV* = probability of visibility IFR flight conditions (visibility < 3 miles), percent\n• MHT = mixing height, 100s feet MSL\n• TWD = transport wind direction, nearest tens degrees (northerly=36; easterly=9; calm=00)\n• TWS = transport wind speed, knots (<0.5 knots will be listed as 0 (calm))\n• HID = Haines Index (unitless)\n• SOL** = instantaneous solar radiation, 10s W/m2 (ex: 8=80 W/m2; non-zero values < 10 = 1)\n• SWH = significant wave height, feet (marine and some near-water stations only)\n\n#### Notes for National Blend of Models Reports\n\n• New elements have been added. New elements are marked with an asterisk (*).\n• Some elements have changed format, position, and/or name. These elements are marked with a double asterisk(**).\n\n#### LAMP Abbreviations\n\nDocumentation on the Localized Aviation MOS Program abbreviations is available at https://vlab.noaa.gov/web/mdl/lamp-card-2.3.0." ]
[ null, "https://weather.meta5.us/noaa_nws.png", null ]
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https://www.exceltip.com/custom-functions/return-unique-items-using-vba-in-microsoft-excel.html?replytocom=994
[ "# Return unique items using VBA in Microsoft Excel\n\nIn this article, we will create a macro to extract unique values from the defined range.\n\nRaw data for this example consists of duplicate entries of country names in the range A7:A21.", null, "We have created “FindUniqueValues” macro to extract unique values from the defined range. This macro can be run by clicking the “Submit” button. Before clicking the “Submit” button, we have to specify the address of the range which contains duplicate data in the cell H9 and address of the destination where output should appear.", null, "Logic explanation\n\n“FindUniqueValues” macro takes two range objects as input parameters. First parameter defines the range which contains the duplicate data and second parameter defines the position of the starting cell which will contain the output. This macro cannot be called directly as we have to specify the parameters, so we have created second macro “MacroRunning” to call the macro.\n\n“MacroRunning” macro calls the “FindUniqueValues” macro with the parameter input by the user.\n\nCode explanation\n\nCopyToRange:=TargetCell, Unique:=True\n\nAdvancedFilter method of Range object is used to filter or copy data from the range based on a certain criteria. To copy only the unique values, we have to set Unique parameter of AdvancedFilter to True.\n\n```\nOption Explicit\n\nSub FindUniqueValues(SourceRange As Range, TargetCell As Range)\n\n'Using advance filter for extacting unique items in the source range\nCopyToRange:=TargetCell, Unique:=True\n\nEnd Sub\n\nSub MacroRunning()\n\n'Calling FindUniqueValues macro\nCall FindUniqueValues(Range(Range(\"H9\").Value), Range(Range(\"H10\").Value))\n\nEnd Sub\n\n```\n\nWe would love to hear from you, do let us know how we can improve our work and make it better for you. Write to us at [email protected]\n\n1.", null, "\"This function was missing from my previous post:\n\nFunction ArrayDimensionCount(InputArray As Variant) As Long\n' returns the number of dimensions of InputArray\nDim i As Long, d As Long\nIf Not TypeName(InputArray) Like \"\"*()\"\" Then Exit Function ' return 0\nOn Error Resume Next\ni = 0\nDo\ni = i + 1\nd = UBound(InputArray, i)\nLoop Until Err 0\nErr = 0\nOn Error GoTo 0\nArrayDimensionCount = i - 1 ' return the dimension count\nEnd Function \"\n\n2.", null, "\"There are many possibilities here. One solutions is the following:\n\nSub ExampleMultipleRanges()\n' returnes the unique items from A1:A10;C1:C10 to E1 and downwards\nDim varArray As Variant\nvarArray = ReturnUniqueItems(True, Range(\"\"A1:A10\"\"), Range(\"\"C1:C10\"\"))\nArrayToRange varArray, Range(\"\"E1\"\")\nErase varArray\nEnd Sub\n\nFunction ReturnUniqueItems(blnReturnItems As Boolean, ParamArray InputRange()) As Variant\n' returns the unique items or the count of unique items from a single range or multiple ranges\nDim c As Collection, i As Long, cl As Range, arrResult() As Variant\nReturnUniqueItems = CVErr(xlErrNA)\nSet c = New Collection\nFor i = LBound(InputRange) To UBound(InputRange)\nFor Each cl In InputRange(i)\nIf Len(cl.Text) > 0 Then\nOn Error Resume Next\nc.Add cl.Value, cl.Text ' ignores duplicates\nOn Error GoTo 0\nEnd If\nNext cl\nSet cl = Nothing\nNext i\nIf blnReturnItems Then ' return each unique item\nIf c.Count > 0 Then\nReDim arrResult(0 To c.Count - 1)\nFor i = 1 To c.Count\narrResult(i - 1) = c(i)\nNext i\nEnd If\n'ReturnUniqueItems = arrResult ' return data as a single row\nReturnUniqueItems = Application.Transpose(arrResult) ' return data as a single column\n' the transpose function can handle up to 5461 items\nErase arrResult\nElse ' return the count of unique items\nReturnUniqueItems = c.Count\nEnd If\nSet c = Nothing\nEnd Function\n\nSub ArrayToRange(InputArray As Variant, UpperLeftCell As Range)\n' fills the content of InputArray into a cell range starting at UpperLeftCell\nDim d As Long, r As Long, c As Long\nIf UpperLeftCell Is Nothing Then Exit Sub\nIf Not TypeName(InputArray) Like \"\"*()\"\" Then Exit Sub\nd = ArrayDimensionCount(InputArray)\nIf d 2 Then Exit Sub\nSelect Case d\nCase 1 ' 1-dimensional array\nr = UBound(InputArray, 1)\nc = 1\nCase 2 ' 2-dimensional array\nr = UBound(InputArray, 1)\nc = UBound(InputArray, 2)\nEnd Select\nUpperLeftCell.Resize(r, c).Formula = InputArray\nEnd Sub \"\n\n3.", null, "What about taking this further and finding unique items from multiple ranges\n\n4.", null, "\"SourceRange and TargetCell can be on different worksheets, e.g. like this:\nFindUniqueValues Worksheets(1).Range(\"\"A2:A100\"\"), Worksheets(2).Range(\"\"C1\"\") \"\n\n5.", null, "A good way of getting a unique list, but note that SourceRange and TargetCell must be on the same worksheet.\n\n6.", null, "\"This function was missing from my previous post:\n\nFunction ArrayDimensionCount(InputArray As Variant) As Long\n' returns the number of dimensions of InputArray\nDim i As Long, d As Long\nIf Not TypeName(InputArray) Like \"\"*()\"\" Then Exit Function ' return 0\nOn Error Resume Next\ni = 0\nDo\ni = i + 1\nd = UBound(InputArray, i)\nLoop Until Err 0\nErr = 0\nOn Error GoTo 0\nArrayDimensionCount = i - 1 ' return the dimension count\nEnd Function \"\n\n7.", null, "\"There are many possibilities here. One solutions is the following:\n\nSub ExampleMultipleRanges()\n' returnes the unique items from A1:A10;C1:C10 to E1 and downwards\nDim varArray As Variant\nvarArray = ReturnUniqueItems(True, Range(\"\"A1:A10\"\"), Range(\"\"C1:C10\"\"))\nArrayToRange varArray, Range(\"\"E1\"\")\nErase varArray\nEnd Sub\n\nFunction ReturnUniqueItems(blnReturnItems As Boolean, ParamArray InputRange()) As Variant\n' returns the unique items or the count of unique items from a single range or multiple ranges\nDim c As Collection, i As Long, cl As Range, arrResult() As Variant\nReturnUniqueItems = CVErr(xlErrNA)\nSet c = New Collection\nFor i = LBound(InputRange) To UBound(InputRange)\nFor Each cl In InputRange(i)\nIf Len(cl.Text) > 0 Then\nOn Error Resume Next\nc.Add cl.Value, cl.Text ' ignores duplicates\nOn Error GoTo 0\nEnd If\nNext cl\nSet cl = Nothing\nNext i\nIf blnReturnItems Then ' return each unique item\nIf c.Count > 0 Then\nReDim arrResult(0 To c.Count - 1)\nFor i = 1 To c.Count\narrResult(i - 1) = c(i)\nNext i\nEnd If\n'ReturnUniqueItems = arrResult ' return data as a single row\nReturnUniqueItems = Application.Transpose(arrResult) ' return data as a single column\n' the transpose function can handle up to 5461 items\nErase arrResult\nElse ' return the count of unique items\nReturnUniqueItems = c.Count\nEnd If\nSet c = Nothing\nEnd Function\n\nSub ArrayToRange(InputArray As Variant, UpperLeftCell As Range)\n' fills the content of InputArray into a cell range starting at UpperLeftCell\nDim d As Long, r As Long, c As Long\nIf UpperLeftCell Is Nothing Then Exit Sub\nIf Not TypeName(InputArray) Like \"\"*()\"\" Then Exit Sub\nd = ArrayDimensionCount(InputArray)\nIf d 2 Then Exit Sub\nSelect Case d\nCase 1 ' 1-dimensional array\nr = UBound(InputArray, 1)\nc = 1\nCase 2 ' 2-dimensional array\nr = UBound(InputArray, 1)\nc = UBound(InputArray, 2)\nEnd Select\nUpperLeftCell.Resize(r, c).Formula = InputArray\nEnd Sub \"\n\n8.", null, "What about taking this further and finding unique items from multiple ranges\n\n9.", null, "\"SourceRange and TargetCell can be on different worksheets, e.g. like this:\nFindUniqueValues Worksheets(1).Range(\"\"A2:A100\"\"), Worksheets(2).Range(\"\"C1\"\") \"\n\n10.", null, "A good way of getting a unique list, but note that SourceRange and TargetCell must be on the same worksheet.\n\nTerms and Conditions of use\n\nThe applications/code on this site are distributed as is and without warranties or liability. In no event shall the owner of the copyrights, or the authors of the applications/code be liable for any loss of profit, any problems or any damage resulting from the use or evaluation of the applications/code." ]
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https://help.algebrakit.com/pages/810-geometry-and-graphs-construction/
[ "# Geometrical constructions\n\n## Introduction\n\nThis section will teach you how to build mathematical constructions from geometrical elements. These constructions are dynamic, meaning students can drag points and see how this affects the whole construction.\n\nLive example: Inscribed circle of a triangle. You can drag the vertices of the triangle.\n\n## Construction Canvas and Element Panel\n\nClick on the Geometry and Graphs icon and then on the Geometry icon to get to the authoring panel. The rectangular area at the top left is the Construction Canvas, where you will build your construction. The Element Panel on the right shows all elements and their properties.", null, "Figure: The canvas and element panel.\n\n## Adding elements to the canvas\n\nYou can build your construction using the tools from the toolbar. The two tools on the left allow you to select or remove elements. The other tools correspond to the mathematical elements you can add to the canvas.", null, "Figure: The tools panel.\n\nSome buttons represent a group of tools. For example, the line button represents line, ray, segment, and vector tools. Click any one of these subtypes to activate it. Next, click on the canvas to create the elements.\n\n### Free, glider, and intersection points\n\nPoints are the most fundamental elements of any construction for two reasons:\n\n1. All other elements rely on points for their definition. For example, you define a line segment through its endpoints. A circle is defined by a midpoint and a point on the circle.\n2. Dragging points is what makes construction dynamic.\n\nPoints exist in three different types, depending on their freedom to move around:\n\n• Free points are points that can move without restrictions. You create them by placing a point on an empty part of the canvas.\n• Glider points can move along another element, such as a line, circle, or graph. If you place a point on a line, it will automatically snap to the line and become a glider point. A glider point cannot leave the element it is constrained to.\n• Intersection points cannot be dragged and have their position completely defined by other elements. A point placed on the intersection of two lines is an example of a dependent point.\n\nThe example below illustrates Thales' theorem and uses all three point categories. Points $M$ and $B$ are free. Point $C$ is a glider point on the circle. Point $A$ is a dependent point constrained to the intersection of the line and the circle.\n\nLive example: Points with different degrees of freedom.\n\n### Element dependencies\n\nThe live example above reveals that some elements depend on other elements. For instance, glider point $C$ lives on the circle, and the circle is defined through points $M$ and $B$. If you drag point $B$, all elements that depend on it will also move. If you delete point $B$, the line, circle, glider point $C$, and dependent point $A$ will also disappear.\n\nNote\n\nIt is important to be aware of dependency when you create your construction. Which points must students be able to move? These are the free points, and you should add these to the canvas first.\n\n## Changing properties in the element panel\n\nThe element panel shows a list of all elements you created. Click on an element to reveal its properties.", null, "Figure: The Element Panel.\n\nDepending on the element, you can configure all or some of the following types of properties:\n\n• Style properties, such as color, line style, and line thickness.\n• The element label. You can also hide the label.\n• Element visibility. You can hide an element from the canvas. Invisible elements still exist, and visual elements can depend on invisible elements.\n• A fixed point cannot be dragged.\n• The element ID is not visible for students but allows you to refer to elements from other elements or evaluation criteria.\n\n## Making tools available to students\n\nIf you run an exercise, you will notice the toolbar is not present. Students have access to only the tools you made available.\n\nClick on the Settings bar to expand it. Select the buttons you want to be included in the student toolbar.", null, "Figure: Adding tools to the student toolbar.\n\n## Other element types\n\nBesides basic elements like points, lines, and circles, you can use many other element types to build your constructions.\n\n### Polygon element", null, "Figure: Creating a polygon.\n\nA polygon is a figure made up of line segments. You create a polygon by creating a sequence of points in the canvas. Close the loop by clicking the first point again.\n\n### Construction elements\n\nConstruction elements are special lines that can be constructed with a ruler and compass.\n\n• A Perpendicular line is a line through a point and perpendicular to another line. Create the perpendicular line by clicking on a line and a point.\n\n• A Parallel line is a line through a point and parallel to another line. Create the parallel line by clicking on a line and a point.\n\n• An Angle bisector is a line that divides an angle into two equal angles. You create the angle bisector by selecting the three points that define an angle.\nFor example, to define the angle bisector for an angle $\\angle ABC$, you select the points $A$, $B$, and $C$.", null, "Figure: Creating an angle bisector.\n\n• A Perpendicular bisector of two points is the line at an equal distance to these points. Create the perpendicular bisector by selecting the two points.\n\nThe live example below shows the construction elements in a triangle. Use the dropdown to select the demo.\n\nLive example of construction elements in a triangle. Drag the triangle points to see how the construction elements move accordingly.\n\n### Transformation elements\n\nTransformations create image points of existing points. To create a transformation, you first click the point of which you want to make the image point. Next, you click the element that defines the transformation. Based on the type of transformation, this can be a point, line, or vector.\n\n• Reflection with respect to a line. Click the point first and then the reflection line.\n• Reflection with respect to a point. Click the point first and then the reflection point.\n• Translation is defined by a vector, so add a vector element to the canvas first. To create the translation, click the point first, then the vector.\n• Dilation. First click the point, then the point that will act as the origin of the dilation. An input dialog appears for the dilation factor. You can later change the dilation factor in the element panel.\n• Rotation. First click the point, then the point that will act as the origin of the rotation. An input dialog appears for the rotation angle. You can later change the rotation angle in the element panel.\n\nThe live example below shows all transformation elements. Use the dropdown to select the transformation demo.\n\nLive example of transformation elements. You can drag the points of the triangle and the red elements.\n\n### Angle elements\n\nThe Geometry & Graphs question type offers two tools for angles. One to indicate existing angles and one to create fixed angles of a given size.\n\nLive example with two angle indicators and one angle fixed to 60 degrees. Drag points $A, B$, and $C$ to see these tools in action.\n\nAngle indicators mark angles with a small circle segment. You can configure in the element panel whether the angle label or the angle size should be visible. You create the angle indicator by clicking three points that define the angle.\n\nYou can create a fixed angle by clicking on two points that define one leg of the angle and entering the angle size in the dialogue box. A new point will be added to the canvas such that the three points mark the desired angle.", null, "Figure: Creating a fixed angle.\n\n### Graph element\n\nThe Graph tool allows you to draw smooth graphs through a set of points.", null, "To create the graph, enable the Graph tool and click on the canvas to create the consecutive points. Finalize the graph by clicking outside the canvas or pressing enter or escape.\n\nYou can drag the points after the graph is created. You can also add new points to an existing graph by selecting the graph first and then adding the new points.\n\nYou can remove existing points from a graph by clicking the point again.\n\nLive example: Use the Graph tool to create a graph. The second example shows a graph with points that are constrained to a line segment.\n\n### Graph Edge element\n\nYou can use Geometry & Graphs to create graphs of vertices and edges instead of a function graph. Use the Edge Tool to connect points (vertices).\n\n• Click a point twice to create a loop\n• Select a line and drag the center point to bend the edge\n• Select a line and use the toolbar above the canvas to configure the label or hatch mark.\n\nLive example: A graph with vertices and edges.\n\n### Text element\n\nUsing the Text Tool, you can add text or math expressions to the canvas. Click in the canvas and enter the formula in the dialog.\n\nThe text element can be anchored to an existing point to make it move with that point. You can select the anchor point by clicking on that point when you create the expression or by entering the point ID in the properties in the element panel.\n\nNote that you can also use point labels to add math content. Use the Text Tool for more flexibility regarding where to position the content." ]
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https://www.colorhexa.com/0c5561
[ "# #0c5561 Color Information\n\nIn a RGB color space, hex #0c5561 is composed of 4.7% red, 33.3% green and 38% blue. Whereas in a CMYK color space, it is composed of 87.6% cyan, 12.4% magenta, 0% yellow and 62% black. It has a hue angle of 188.5 degrees, a saturation of 78% and a lightness of 21.4%. #0c5561 color hex could be obtained by blending #18aac2 with #000000. Closest websafe color is: #006666.\n\n• R 5\n• G 33\n• B 38\nRGB color chart\n• C 88\n• M 12\n• Y 0\n• K 62\nCMYK color chart\n\n#0c5561 color description : Very dark cyan.\n\n# #0c5561 Color Conversion\n\nThe hexadecimal color #0c5561 has RGB values of R:12, G:85, B:97 and CMYK values of C:0.88, M:0.12, Y:0, K:0.62. Its decimal value is 808289.\n\nHex triplet RGB Decimal 0c5561 `#0c5561` 12, 85, 97 `rgb(12,85,97)` 4.7, 33.3, 38 `rgb(4.7%,33.3%,38%)` 88, 12, 0, 62 188.5°, 78, 21.4 `hsl(188.5,78%,21.4%)` 188.5°, 87.6, 38 006666 `#006666`\nCIE-LAB 32.783, -16.21, -12.968 5.557, 7.438, 12.451 0.218, 0.292, 7.438 32.783, 20.759, 218.659 32.783, -22.99, -14.919 27.272, -11.354, -7.979 00001100, 01010101, 01100001\n\n# Color Schemes with #0c5561\n\n• #0c5561\n``#0c5561` `rgb(12,85,97)``\n• #61180c\n``#61180c` `rgb(97,24,12)``\nComplementary Color\n• #0c6143\n``#0c6143` `rgb(12,97,67)``\n• #0c5561\n``#0c5561` `rgb(12,85,97)``\n• #0c2b61\n``#0c2b61` `rgb(12,43,97)``\nAnalogous Color\n• #61430c\n``#61430c` `rgb(97,67,12)``\n• #0c5561\n``#0c5561` `rgb(12,85,97)``\n• #610c2b\n``#610c2b` `rgb(97,12,43)``\nSplit Complementary Color\n• #55610c\n``#55610c` `rgb(85,97,12)``\n• #0c5561\n``#0c5561` `rgb(12,85,97)``\n• #610c55\n``#610c55` `rgb(97,12,85)``\nTriadic Color\n• #0c6118\n``#0c6118` `rgb(12,97,24)``\n• #0c5561\n``#0c5561` `rgb(12,85,97)``\n• #610c55\n``#610c55` `rgb(97,12,85)``\n• #61180c\n``#61180c` `rgb(97,24,12)``\nTetradic Color\n• #04191d\n``#04191d` `rgb(4,25,29)``\n• #062d34\n``#062d34` `rgb(6,45,52)``\n• #09414a\n``#09414a` `rgb(9,65,74)``\n• #0c5561\n``#0c5561` `rgb(12,85,97)``\n• #0f6978\n``#0f6978` `rgb(15,105,120)``\n• #127d8e\n``#127d8e` `rgb(18,125,142)``\n• #1491a5\n``#1491a5` `rgb(20,145,165)``\nMonochromatic Color\n\n# Alternatives to #0c5561\n\nBelow, you can see some colors close to #0c5561. Having a set of related colors can be useful if you need an inspirational alternative to your original color choice.\n\n• #0c6158\n``#0c6158` `rgb(12,97,88)``\n• #0c615f\n``#0c615f` `rgb(12,97,95)``\n• #0c5c61\n``#0c5c61` `rgb(12,92,97)``\n• #0c5561\n``#0c5561` `rgb(12,85,97)``\n• #0c4e61\n``#0c4e61` `rgb(12,78,97)``\n• #0c4761\n``#0c4761` `rgb(12,71,97)``\n• #0c4061\n``#0c4061` `rgb(12,64,97)``\nSimilar Colors\n\n# #0c5561 Preview\n\nText with hexadecimal color #0c5561\n\nThis text has a font color of #0c5561.\n\n``<span style=\"color:#0c5561;\">Text here</span>``\n#0c5561 background color\n\nThis paragraph has a background color of #0c5561.\n\n``<p style=\"background-color:#0c5561;\">Content here</p>``\n#0c5561 border color\n\nThis element has a border color of #0c5561.\n\n``<div style=\"border:1px solid #0c5561;\">Content here</div>``\nCSS codes\n``.text {color:#0c5561;}``\n``.background {background-color:#0c5561;}``\n``.border {border:1px solid #0c5561;}``\n\n# Shades and Tints of #0c5561\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, #01090a is the darkest color, while #f7fdfe is the lightest one.\n\n• #01090a\n``#01090a` `rgb(1,9,10)``\n• #03181b\n``#03181b` `rgb(3,24,27)``\n• #06272d\n``#06272d` `rgb(6,39,45)``\n• #08363e\n``#08363e` `rgb(8,54,62)``\n• #0a4650\n``#0a4650` `rgb(10,70,80)``\n• #0c5561\n``#0c5561` `rgb(12,85,97)``\n• #0e6472\n``#0e6472` `rgb(14,100,114)``\n• #107484\n``#107484` `rgb(16,116,132)``\n• #128395\n``#128395` `rgb(18,131,149)``\n• #1592a7\n``#1592a7` `rgb(21,146,167)``\n• #17a1b8\n``#17a1b8` `rgb(23,161,184)``\n• #19b1ca\n``#19b1ca` `rgb(25,177,202)``\n• #1bc0db\n``#1bc0db` `rgb(27,192,219)``\nShade Color Variation\n• #26c9e4\n``#26c9e4` `rgb(38,201,228)``\n• #37cee6\n``#37cee6` `rgb(55,206,230)``\n• #49d2e8\n``#49d2e8` `rgb(73,210,232)``\n• #5ad6eb\n``#5ad6eb` `rgb(90,214,235)``\n• #6cdbed\n``#6cdbed` `rgb(108,219,237)``\n• #7ddfef\n``#7ddfef` `rgb(125,223,239)``\n• #8fe3f1\n``#8fe3f1` `rgb(143,227,241)``\n• #a0e7f3\n``#a0e7f3` `rgb(160,231,243)``\n• #b1ecf5\n``#b1ecf5` `rgb(177,236,245)``\n• #c3f0f8\n``#c3f0f8` `rgb(195,240,248)``\n• #d4f4fa\n``#d4f4fa` `rgb(212,244,250)``\n• #e6f9fc\n``#e6f9fc` `rgb(230,249,252)``\n• #f7fdfe\n``#f7fdfe` `rgb(247,253,254)``\nTint Color Variation\n\n# Tones of #0c5561\n\nA tone is produced by adding gray to any pure hue. In this case, #363737 is the less saturated color, while #045b69 is the most saturated one.\n\n• #363737\n``#363737` `rgb(54,55,55)``\n• #323a3b\n``#323a3b` `rgb(50,58,59)``\n• #2e3d3f\n``#2e3d3f` `rgb(46,61,63)``\n• #294044\n``#294044` `rgb(41,64,68)``\n• #254348\n``#254348` `rgb(37,67,72)``\n• #21464c\n``#21464c` `rgb(33,70,76)``\n• #1d4950\n``#1d4950` `rgb(29,73,80)``\n• #194c54\n``#194c54` `rgb(25,76,84)``\n• #144f59\n``#144f59` `rgb(20,79,89)``\n• #10525d\n``#10525d` `rgb(16,82,93)``\n• #0c5561\n``#0c5561` `rgb(12,85,97)``\n• #085865\n``#085865` `rgb(8,88,101)``\n• #045b69\n``#045b69` `rgb(4,91,105)``\nTone Color Variation\n\n# Color Blindness Simulator\n\nBelow, you can see how #0c5561 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://discourse.julialang.org/t/function-for-creating-a-neural-network-with-n-hidden-layers-in-flux/75589
[ "# Function for creating a neural network with n hidden layers in Flux\n\nHi,\n\nI want to create a function, where I can set the number of hidden layers with an argument. One option that kinda works is\n\n``````using Flux\nfunction make_nn(length_in = 80, length_out = 1, nodes = 128, hid_lay = 3, act_fun = relu, act_fun_last = sigmoid)\nq = Dense(length_in, nodes, act_fun)\nfor i in 1:hid_lay-1\nq = Chain(q, Dense(nodes, nodes, act_fun))\nend\nq = Chain(q, Dense(nodes, length_out, act_fun_last))\nend\n``````\n\nbut the output is a nested Chain which is not particular beautiful to me:\n\n``````Chain(\nChain(\nChain(\nDense(80, 128, relu), # 10_368 parameters\nDense(128, 128, relu), # 16_512 parameters\n),\nDense(128, 128, relu), # 16_512 parameters\n),\nDense(128, 1, σ), # 129 parameters\n)\n``````\n\nIs there a better way to do this in Flux?\n\nBest regards.\n\nYou could create the layers first and then stack them, something like this maybe\n\n``````using Flux\n\nfunction make_nn(length_in = 80, length_out = 1, nodes = 128, hid_lay = 3, act_fun = relu, act_fun_last = sigmoid)\nfirst_layer = Dense(length_in, nodes, act_fun)\nintermediate_layers = [Dense(nodes,nodes,act_fun) for _ in 1:hid_lay-1]\nlast_layer = Dense(nodes, length_out, act_fun_last)\n\nreturn Chain(\nfirst_layer,\nintermediate_layers...,\nlast_layer\n)\nend\n``````\n2 Likes" ]
[ null ]
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https://www.semanticscholar.org/paper/Gravitational-waveforms-from-inspiralling-compact-Blanchet-Iyer/79b9438bbfbdc0c26e5e6f874aa396c0fdb5a322
[ "# Gravitational waveforms from inspiralling compact binaries to second-post-Newtonian order\n\n```@article{Blanchet1996GravitationalWF,\ntitle={Gravitational waveforms from inspiralling compact binaries to second-post-Newtonian order},\nauthor={Luc Blanchet and Bala R. Iyer and Clifford M. Will and ALAN G. Wiseman},\njournal={Classical and Quantum Gravity},\nyear={1996},\nvolume={13},\npages={575-584}\n}```\nThe two independent 'plus' and 'cross' polarization waveforms associated with the gravitational waves emitted by inspiralling, non-spinning, compact binaries are presented, ready for use in the data analysis of signals received by future laser interferometer gravitational-wave detectors such as LIGO and VIRGO. The computation is based on a recently derived expression of the gravitational field at the second-post-Newtonian approximation of general relativity beyond the dominant (Newtonian… Expand\n198 Citations\nGravitational waveforms from a Lense-Thirring system\n• Physics\n• 2006\nThe construction of ready to use templates for gravitational waves from spinning binaries is an important challenge in the investigation of detectable gravitational wave signals. Here we present aExpand\nSpin effects on gravitational waves from inspiraling compact binaries at second post-Newtonian order\n• Physics\n• 2013\n(Dated: May 3, 2014) We calculate the gravitational waveform for spinning, precessing compact binary inspirals through second post-Newtonian order in the amplitude. When spins are collinear with theExpand\nGravitational-wave amplitudes for compact binaries in eccentric orbits at the third post-Newtonian order: Memory contributions\n• Physics\n• Physical Review D\n• 2019\nWe compute the non-linear memory contributions to the gravitational-wave amplitudes for compact binaries in eccentric orbits at the third post-Newtonian (3PN) order in general relativity. TheseExpand\nGravitational Radiation from Post-Newtonian Sources and Inspiralling Compact Binaries\n• L. Blanchet\n• Physics, Medicine\n• Living reviews in relativity\n• 2014\nThe current state of the art on post-Newtonian methods as applied to the dynamics and gravitational radiation of general matter sources (including the radiation reaction back onto the source) and inspiralling compact binaries is presented. Expand\nGravitational-wave amplitudes for compact binaries in eccentric orbits at the third post-Newtonian order: Tail contributions and postadiabatic corrections\n• Physics\n• Physical Review D\n• 2019\nWe compute the tail contributions to the gravitational-wave mode amplitudes for compact binaries in eccentric orbits at the third post-Newtonian order of general relativity. We combine them with theExpand\nPhasing of gravitational waves from inspiralling eccentric binaries\n• Physics\n• 2005\nWe develop a method for analytically constructing highly accurate post-Newtonian (PN) templates for gravitational-wave signals emitted by compact binaries moving in inspiralling eccentric orbits.Expand\nThe third post-Newtonian gravitational wave polarizations and associated spherical harmonic modes for inspiralling compact binaries in quasi-circular orbits\n• Physics\n• 2008\nThe gravitational waveform (GWF) generated by inspiralling compact binaries moving in quasi-circular orbits is computed at the third post-Newtonian (3PN) approximation to general relativity. OurExpand\nInspiraling Compact Binaries\nIn this contribution we review several astrophysical properties of inspiraling compact binaries which make these systems unique, and very important as potential sources of gravitational radiation toExpand\nBounding the mass of the graviton with gravitational waves: effect of higher harmonics in gravitational waveform templates\n• Physics\n• 2009\nObservations by laser interferometric detectors of gravitational waves from inspiraling compact binary systems can be used to search for a dependence of the waves' propagation speed on wavelength,Expand\nGravitational waveforms for finite mass binaries\n• Physics\n• 2007\nOne of the promising sources of gravitational radiation is a binary system composed of compact stars. It is an important question of how the rotation of the bodies and the eccentricity of the orbitExpand" ]
[ null ]
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https://formulasearchengine.com/wiki/Outer_product
[ "Outer product\n\nFor \"outer product\" in geometric algebra, see Exterior algebra.\n\nIn linear algebra, the term outer product typically refers to the tensor product of two vectors. The result of applying the outer product to a pair of coordinate vectors is a matrix. The name contrasts with the inner product, which takes as input a pair of vectors and produces a scalar.\n\nThe outer product of vectors can be also regarded as a special case of the Kronecker product of matrices.\n\nSome authors use the expression \"outer product of tensors\" as a synonym of \"tensor product\". The outer product is also a higher-order function in some computer programming languages such as R, APL, and Mathematica.\n\nDefinition (matrix multiplication)\n\n{{#invoke:main|main}}\n\nThe outer product uv is equivalent to a matrix multiplication uvT, provided that u is represented as a m × 1 column vector and v as a n × 1 column vector (which makes vT a row vector). For instance, if m = 4 and n = 3, then\n\n${\\mathbf {u} }\\otimes {\\mathbf {v} }={\\mathbf {u} }{\\mathbf {v} }^{\\mathrm {T} }={\\begin{bmatrix}u_{1}\\\\u_{2}\\\\u_{3}\\\\u_{4}\\end{bmatrix}}{\\begin{bmatrix}v_{1}&v_{2}&v_{3}\\end{bmatrix}}={\\begin{bmatrix}u_{1}v_{1}&u_{1}v_{2}&u_{1}v_{3}\\\\u_{2}v_{1}&u_{2}v_{2}&u_{2}v_{3}\\\\u_{3}v_{1}&u_{3}v_{2}&u_{3}v_{3}\\\\u_{4}v_{1}&u_{4}v_{2}&u_{4}v_{3}\\end{bmatrix}}.$", null, "Or in index notation:\n\n$(\\mathbf {u} \\mathbf {v} ^{\\mathrm {T} })_{ij}=u_{i}v_{j}$", null, "For complex vectors, it is customary to use the conjugate transpose of v (denoted vH):\n\n${\\mathbf {u} }\\otimes {\\mathbf {v} }={\\mathbf {u} }{\\mathbf {v} }^{\\mathrm {H} }.$", null, "Contrast with inner product\n\nIf m = n, then one can take the matrix product the other way, yielding a scalar (or 1 × 1 matrix):\n\n$\\left\\langle \\mathbf {u} ,\\mathbf {v} \\right\\rangle =\\mathbf {u} ^{\\mathrm {T} }\\mathbf {v}$", null, "which is the standard inner product for Euclidean vector spaces, better known as the dot product. The inner product is the trace of the outer product.\n\nRank of an outer product\n\nIf u and v are both nonzero then the outer product matrix uvT always has matrix rank 1, as can be easily seen by multiplying it with a vector x:\n\n$(\\mathbf {u} \\mathbf {v} ^{\\mathrm {T} })\\mathbf {x} =\\mathbf {u} (\\mathbf {v} ^{\\mathrm {T} }\\mathbf {x} )$", null, "which is just a scalar vTx multiplied by a vector u.\n\n(\"Matrix rank\" should not be confused with \"tensor order\", or \"tensor degree\", which is sometimes referred to as \"rank\".)\n\nDefinition (vectors and tensors)\n\nVector multiplication\n\nGiven the vectors\n\n$\\mathbf {u} =(u_{1},u_{2},\\dots ,u_{m})$", null, "$\\mathbf {v} =(v_{1},v_{2},\\dots ,v_{n})$", null, "their outer product uv is defined as the m × n matrix A obtained by multiplying each element of u by each element of v:\n\n${\\mathbf {u} }\\otimes {\\mathbf {v} }={\\mathbf {A} }={\\begin{bmatrix}u_{1}v_{1}&u_{1}v_{2}&\\dots &u_{1}v_{n}\\\\u_{2}v_{1}&u_{2}v_{2}&\\dots &u_{2}v_{n}\\\\\\vdots &\\vdots &\\ddots &\\vdots \\\\u_{m}v_{1}&u_{m}v_{2}&\\dots &u_{m}v_{n}\\end{bmatrix}}.$", null, "For complex vectors, the complex conjugate of v (denoted v or ). Namely, matrix A is obtained by multiplying each element of u by the complex conjugate of each element of v.\n\nTensor multiplication\n\nThe outer product on tensors is typically referred to as the tensor product. Given a tensor a of order q with dimensions (i1, ..., iq), and a tensor b of order r with dimensions (j1, ..., jr), their outer product c is of order q + r with dimensions (k1, ..., kq+r) which are the i  dimensions followed by the j  dimensions. It is denoted in coordinate-free notation using ⊗ and components are defined index notation by:\n\n${\\mathbf {c} }={\\mathbf {a} }\\otimes {\\mathbf {b} },\\quad c_{ij}=a_{i}b_{j}$", null, "similarly for higher order tensors:\n\n${\\mathbf {T} }={\\mathbf {a} }\\otimes {\\mathbf {b} }\\otimes {\\mathbf {c} },\\quad T_{ijk}=a_{i}b_{j}c_{k}$", null, "For example, if A is of order 3 with dimensions (3, 5, 7) and B is of order 2 with dimensions (10, 100), their outer product c is of order 5 with dimensions (3, 5, 7, 10, 100). If A has a component A[2, 2, 4] = 11 and B has a component B[8, 88] = 13, then the component of C formed by the outer product is C[2, 2, 4, 8, 88] = 143.\n\nTo understand the matrix definition of outer product in terms of the definition of tensor product:\n\n1. The vector v can be interpreted as an order-1 tensor with dimension M, and the vector u as an order-1 tensor with dimension N. The result is a order-2 tensor with dimension (M, N).\n2. The order of the result of an inner product between two tensors of order q and r is the greater of q + r − 2 and 0. Thus, the inner product of two matrices has the same order as the outer product (or tensor product) of two vectors.\n3. It is possible to add arbitrarily many leading or trailing 1 dimensions to a tensor without fundamentally altering its structure. These 1 dimensions would alter the character of operations on these tensors, so any resulting equivalences should be expressed explicitly.\n4. The inner product of two matrices V with dimensions (d, e) and U with dimensions (e, f) is $\\sum _{j=1}^{e}V_{ij}U_{jk}$", null, ", where i = 1, 2, ..., d and k = 1, 2, ..., f. For the case where e = 1, the summation is trivial (involving only a single term).\n5. The outer product of two matrices V with dimensions (m, n) and U with dimensions (p, q) is $C_{st}=V_{ij}U_{hk}$", null, ", where s = 1, 2, ..., mp − 1, mp and t = 1, 2, ..., nq − 1, nq.\n\nDefinition (abstract)\n\nLet V and W be two vector spaces, and let W be the dual space of W. Given a vector xV and yW, then the tensor product yx corresponds to the map A : W → V given by\n\n$w\\mapsto y^{*}(w)x.$", null, "Here y(w) denotes the value of the linear functional y (which is an element of the dual space of W) when evaluated at the element wW. This scalar in turn is multiplied by x to give as the final result an element of the space V.\n\nIf V and W are finite-dimensional, then the space of all linear transformations from W to V, denoted Hom(W, V), is generated by such outer products; in fact, the rank of a matrix is the minimal number of such outer products needed to express it as a sum (this is the tensor rank of a matrix). In this case Hom(W, V) is isomorphic to WV." ]
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https://edurev.in/course/quiz/attempt/12127_RRB-NTPC-Mock-Test-19--English-/ed54208d-4189-40f0-b35e-793060c95e54
[ "Courses\n\n# RRB NTPC Mock Test - 19 (English)\n\n## 120 Questions MCQ Test RRB NTPC - Mock Tests Papers 2020 | RRB NTPC Mock Test - 19 (English)\n\nDescription\nThis mock test of RRB NTPC Mock Test - 19 (English) for Railways helps you for every Railways entrance exam. This contains 120 Multiple Choice Questions for Railways RRB NTPC Mock Test - 19 (English) (mcq) to study with solutions a complete question bank. The solved questions answers in this RRB NTPC Mock Test - 19 (English) quiz give you a good mix of easy questions and tough questions. Railways students definitely take this RRB NTPC Mock Test - 19 (English) exercise for a better result in the exam. You can find other RRB NTPC Mock Test - 19 (English) extra questions, long questions & short questions for Railways on EduRev as well by searching above.\nQUESTION: 1\n\nSolution:\nQUESTION: 2\n\nSolution:\nQUESTION: 3\n\n### Which country uses maximum amount of fertilizer ?\n\nSolution:\nQUESTION: 4\n\nTornado is related to which country?\n\nSolution:\nQUESTION: 5\n\nWhich two countries are separated by Gibraltar strait ?\n\nSolution:\nQUESTION: 6\n\nThe official language of Nagaland is :-\n\nSolution:\nQUESTION: 7\n\nWhere is “Asiatic Society” situated ?\n\nSolution:\nQUESTION: 8\n\nTwo numbers are respectively 20% and 60% of a third number. The first number is how much percent of the second number ?\n\nSolution:\n\nLet third number is 100.\n\n∴ first number = 20\n\nsecond number = 60", null, "QUESTION: 9\n\nMatch the following :\n\nColumn I                    Column II\n\n(A) Earthquake               1. Ammeter\n\n(B) Height                      2. Seismograph\n\n(C) Electric current       3. Altimeter\n\n(D) Resistance               4. Ohm\n\nSolution:\nQUESTION: 10\n\nWhich among the following is strongest oxidizing agent ?\n\nSolution:\nQUESTION: 11\n\nSea horse is an example of which class?\n\nSolution:\nQUESTION: 12\n\nIf the cost price is 95% of selling price. What is the profit percent ?\n\nSolution:\n\nLet selling price = Rs. 100\n\n∴ Cost price = Rs. 95", null, "QUESTION: 13\n\nWhich among the following pairs is mismatched regarding Nobel Prize Winners and their related work in specific field ?\n\nSolution:\nQUESTION: 14\n\nIn which field Dronacharya award is given ?\n\nSolution:\nQUESTION: 15\n\nThe marked price of an article is Rs.1500. A discount of 20% is given on the marked price. What additional % discount must be offered to the customer to bring the net price Rs. 1104?\n\nSolution:", null, "QUESTION: 16\n\nWhat is the name of autobiography of Mahatma Gandhi ?\n\nSolution:\nQUESTION: 17\n\nWhat is the reason behind heart attack ?\n\nSolution:\nQUESTION: 18\n\nWhich is called \"Black Death\"?\n\nSolution:\nQUESTION: 19\n\nA tradesman  gives 4% discount on the marked price and gives 1 article free for buying every 5 articles and thus gains 25%. How much percent is the marked price more than the cost price?\n\nSolution:", null, "QUESTION: 20\n\nExamine the following sentences :\n\n1. Dehydrated sodium carbonate is commonly known as pure soda.\n\n2. Bleaching powder is produced in Hasenclever Plant\n\n3. Pure soda is used in manufacturing fire extinguisher.\n\nOn the basis of above statements, which of the following is true ?\n\nSolution:\nQUESTION: 21\n\nA sum of money at simple interest amount to 1012 in", null, "year and to Rs. 1067.20 in 4 years. What is the rate of interest per annum?\n\nSolution:", null, "QUESTION: 22\n\nWhat will be the next number in the series :\n\n5, 7, 14, 16, 32, 34, ........\n\nSolution:", null, "QUESTION: 23\n\nThe average age of a team of  9 members is 23 years. If the age of the team leader be included then the average increases by 3 months. What is the age of the team leader ?\n\nSolution:", null, "QUESTION: 24\n\nComplete the given series 5, 30, 15, 90, 45, 270 ................?\n\nSolution:", null, "QUESTION: 25\n\nRs. 31450 is divided among A, B and C in the ratio of", null, ". What is the difference between the smallest and greatest part?\n\nSolution:", null, "QUESTION: 26\n\nIf 3x – 3x–1 = 54 then find the value of 2x2 + 4x + 3\n\nSolution:\n\n3x – 3x – 1 = 54\n\nx = 4\n\n∴ 2x2 + 4x + 3 = 2 × (4)2 + 4 × 4 + 3 = 51\n\nQUESTION: 27\n\nIn a certain language, NEAREST is coded as LAUIGWZ, how is SUBJECT coded in that code ?\n\nSolution:", null, "QUESTION: 28\n\nThree men can complete a piece of work in 6 days. Two days after they started the work 3 more men joined them. How many days will they take to complete the remaining work ?\n\nSolution:", null, "QUESTION: 29\n\nWhich of the following tribes of India follows polyandry ?\n\n1. Gond\n\n2. Naga\n\n3. Jaunsari\n\n4. Toda\n\nCode :\n\nSolution:\nQUESTION: 30\n\nA man goes from a place A to B at a speed of 30 km/hr and returns at a speed of 20 km/hr. What is the average speed for the whole journey?\n\nSolution:", null, "QUESTION: 31\n\nFrom which of the mountain range Konkan Railways passes ?\n\nSolution:\nQUESTION: 32\n\nWho established Ahmedabad ?\n\nSolution:\nQUESTION: 33\n\nThe smallest five digit number which is divisible by 12, 18, and 21 is:\n\nSolution:\n\nLCM of 12, 18 & 21 = 252\n\nSmallest number of five digit = 10000\n\n∴ Required number = 10000 + 80  = 10080\n\nQUESTION: 34\n\nWho led English forces in the Battle of Plassey (1757) ?\n\nSolution:\nQUESTION: 35\n\nThe value of", null, "Solution:", null, "QUESTION: 36\n\nJay Prakash Narayan was associated with which party ?\n\nSolution:\nQUESTION: 37\n\nUnder which article of the Indian Constitution the President is bound to follow the advice of union cabinet ?\n\nSolution:\nQUESTION: 38\n\nWhen financial emergency was declared by the president of India ?\n\nSolution:\nQUESTION: 39\n\nIf (2a – 1)2 + (4b – 3)2 + (4c + 5)2 = 0 then the value of", null, "Solution:", null, "QUESTION: 40\n\nOn which basis the judges of the Supreme Court can be impeached ?\n\nSolution:\nQUESTION: 41\n\nWho is credited for creating World Wide Web ?\n\nSolution:\nQUESTION: 42\n\nWhich sector was given priority in first five year plan ?\n\nSolution:\nQUESTION: 43\n\nWhich is the longest run train of India that covers longest distance (4283 km) ?\n\nSolution:\nQUESTION: 44\n\nIf x : y = 2 : 3  then the value of", null, "Solution:\nQUESTION: 45\n\nIf AT = 33, BAT = 58, then RAT = ?\n\nSolution:\n\nGiven code is the sum of the positions of English alphabets from reverse.\n\nAT = 26 + 7 = 33, BAT = 26 + 7 + 25 = 58\n\nRAT = 9 + 26 + 7 = 42\n\nQUESTION: 46\n\nIf P means '×', Q means '+', R means '÷' and S means '–', then what is the value of : 1 Q 9 R 7 P 7 Q 3 S 5 ?\n\nSolution:\n\n1 Q 9 R 7 P 7 Q 3 S 5\n\n= 1 + 9 ÷ 7 × 7 + 3 – 5\n\n= 8\n\nQUESTION: 47\n\nChoose the figure which is different from the other three figures ?\n\nSolution:\n\nFigures except (C) are divided into four equal parts.\n\nQUESTION: 48\n\nFraction between", null, "Solution:\n\n3/7 = 0.42\n\nQUESTION: 49\n\nWhere is the head – quarter of newly constituted North – Western zone (NWR) of railways ?\n\nSolution:\nQUESTION: 50\n\nThe main constituent of LPG is :\n\nSolution:\nQUESTION: 51\n\nCryogenic liquid is :\n\nSolution:\nQUESTION: 52\n\nWho gets maximum benefit from inflation ?\n\nSolution:\nQUESTION: 53\n\nWhere is the headquarter of World Meteorological Organization ?\n\nSolution:\nQUESTION: 54\n\nIn this question find out the alternative which will replace the question mark ?\n\nBus : Depo : : Train : ?\n\nSolution:\nQUESTION: 55\n\nIn this question find out the alternative which will replace the question mark ?\n\nDTP : IAY : : JMY : ?\n\nSolution:", null, "QUESTION: 56\n\nIn this question find out the alternative which will replace the question mark ?\n\n1 : 1 : : 25 : ?\n\nSolution:", null, "QUESTION: 57", null, "Solution:", null, "QUESTION: 58\n\nThe average of 5 consecutive even numbers is 50. Then the difference between \"product of the largest and the smallest number\" and \"product of fourth and second number\" is\n\nSolution:\n\nNumbers = 46     48    50    52     54\n\n∴ Difference = 48 × 52 – 46 × 54\n= 2496 – 2484\n= 12\n\nQUESTION: 59\n\n'A' runs form his home towards East. After that he turns his left and runs again. Again he turns his right and runs. And finally he turns his left and runs and reached his office.In which direction A runs in last and what is the direction of A's office from his home ?\n\nSolution:", null, "QUESTION: 60\n\nP goes 5 km in North direction. After that he moves his right and goes 4 km. After that he turns again his right and goes 10 km and finally reached Park.\n\nWhat is direction from starting point to park and what is the distance between starting point to park ?\n\nSolution:", null, "", null, "QUESTION: 61\n\nIf x = 511 then find the value of", null, "Solution:", null, "QUESTION: 62\n\nIf A + B means A is the mother of B ; A – B means A is the brother of B ; A % B means A is the father of B and A × B means A is the sister of B, which of the following shows that P is the maternal uncle of Q ?\n\nSolution:", null, "QUESTION: 63\n\nThe elevation of the top of a tower from a point on the ground is 45°. On travelling 60 m from the point towards the tower the elevation of the top becomes 60°. What is the height of the tower?\n\nSolution:", null, "", null, "", null, "QUESTION: 64\n\nIf a : b = 2 : 1 and b : c = 3 : 2 then find the value of a : b : c\n\nSolution:", null, "QUESTION: 65\n\nThe population of town increases by 5% every year. If the present population is 9261 then what was the population 3 years ago ?\n\nSolution:", null, "QUESTION: 66\n\nRead the statements and conclusions and answer the questions from the alternatives given below.\n\nStatements :\n\nI. Every year world's population increases.\n\nII. World's food problem increases every year due to population explosion.\n\nConclusions :\n\nI. Population control will minimize food problem in the world.\n\nII. Increase in population needs Production of more food.\n\nSolution:\nQUESTION: 67\n\nIf 30% of A = 0.25 of B = 1/5 of C then A : B : C is equal to:\n\nSolution:", null, "QUESTION: 68\n\nThe percentage of loss when an article is sold at Rs. 80 is the same as that of the profit when it is sold at Rs. 110. What is the percentage profit or loss on the article?\n\nSolution:", null, "QUESTION: 69\n\nIn how many years will a sum of money double itself at 12% per annum simple interest ?\n\nSolution:", null, "QUESTION: 70\n\nChoose the box that is similar to the box formed from the given sheet of paper (✕)", null, "", null, "", null, "", null, "", null, "Solution:\n\nWhen a cube is formed by folding the sheet shown in figure (✕), then the two half – shaded faces lies opposite to each other and one of three blank faces to the face bearing a dot.\n\nSo clearly each one of the four cube shown in figure (1), (2), (3) and (4) can be formed.\n\nQUESTION: 71\n\nIn a 40 L mixture of milk and water the ratio of milk to water is 7 : 1. In order to make the ratio of milk and water 3 : 1, the quantity of water that should be added to the mixture will be:\n\nSolution:\n\nLet added quantity of water is x L.", null, "QUESTION: 72\n\nTwo positions of a dice are shown below. When 3 points are at the bottom, how many points will be at the top ?", null, "Solution:\nQUESTION: 73\n\nA ranks fifth in a class. P is eighth from the last. If T is sixth after A and just in the middle of A and P, then how many students are there in the class ?\n\nSolution:", null, "QUESTION: 74\n\nHow many sides does a regular polygon have whose interior and exterior angles are in the ratio 2 : 1 ?\n\nSolution:", null, "QUESTION: 75\n\nA and B together can do a piece of work in 12 days. B alone can finish it in 30 days. In how many days A alone can complete the work ?\n\nSolution:", null, "QUESTION: 76\n\nIn a line of boys P's rank is 10th from the end. Seven boys are sitting between P and Q. R's rank is 8th from the begening of line and Q is 10th after R. What will be the minimum number of boys in the line ?\n\nSolution:", null, "QUESTION: 77\n\nA constable follows a thief who is 400 m ahead of the constable. If the constable and the thief run at speed of 8 km/hr and 7 km/hr respectively, the constable would catch the thief in:\n\nSolution:", null, "QUESTION: 78\n\n\"Won\" is the currency of :\n\nSolution:\nQUESTION: 79\n\nRohit is the brother of Sumit and Mukul is father of Rohit. Jayesh is brother of Sneha and Sneha is daughter of Sumit. Who is the uncle of Jayesh ?\n\nSolution:", null, "QUESTION: 80\n\nSelf - dependence was the main objective of which five – year plan ?\n\nSolution:\nQUESTION: 81\n\nWhat causes structural unemployment ?\n\nSolution:\nQUESTION: 82\n\nChoose odd number pair :\n\n(18 – 45), (16 – 40), (14 – 28), (8 – 20)\n\nSolution:\n\nIInd number is = Ist number × 2.5\n\nQUESTION: 83\n\nWhich is equal to one micron ?\n\nSolution:\nQUESTION: 84\n\nA tree increases annually by", null, "of its height. By how much will it increase after 2 years, if it stands, today 128 cm?\n\nSolution:", null, "QUESTION: 85\n\nThe speed of light is maximum in\n\nSolution:\nQUESTION: 86\n\nWhich Indian city has hosted the 2016 National Children Film Festival ?\n\nSolution:\nQUESTION: 87\n\nFind the odd one out :\n\nSolution:\nQUESTION: 88\n\nWhat will come in place of question mark :", null, "Solution:", null, "QUESTION: 89\n\nWhich planets are situated on both sides of Earth ?\n\nSolution:\nQUESTION: 90\n\nWhich of the followings diagram indicates the best relation between :\n\nPlayer, Cricket player, Female\n\nSolution:\nQUESTION: 91\n\nWhich of the followings diagram indicates the best relation between :\n\nMinister, Prime minister, Counsil of ministers\n\nSolution:\n\nAll the ministers including prime minister constitute the council of ministers.\n\nQUESTION: 92\n\nWhich state has become the first cash less state of India ?\n\nSolution:\nQUESTION: 93\n\nMitochondria is related to\n\nSolution:\nQUESTION: 94\n\nFrom which part of cotton plant, cotton fibre is obtained ?\n\nSolution:\nQUESTION: 95\n\nIf 4 @ 5 = 41 and 6 @ 7 = 85, then 8 @ 9 = ?\n\nSolution:\n\n4 @ 5 = (4)2 + (5)2 = 41\n\n6 @ 7 = (6)2 + (7)2 = 85\n\n8 @ 9 = (8)2 + (9)2 = 145\n\nQUESTION: 96\n\nOn which river bank is Jabalpur located ?\n\nSolution:\nQUESTION: 97\n\nFrom which Indian State tropic of cancer does not pass ?\n\nSolution:\nQUESTION: 98\n\n___________is known as Nightingle of India\n\nSolution:\nQUESTION: 99\n\nIn which state India's first \"Green Rail\" corridor is launched ?\n\nSolution:\nQUESTION: 100\n\nWho wrote \"Geet Govind\" ?\n\nSolution:\nQUESTION: 101\n\nWhich country has the oldest monarchy in the world ?\n\nSolution:\nQUESTION: 102\n\nConservation of linear momentum is equal to\n\nSolution:\nQUESTION: 103\n\nWho was the father of Maratha warrior Shivaji ?\n\nSolution:\nQUESTION: 104\n\nFrom the given alternatives, select that alternative whose word cannot be formed by using letters of the word 'SIGNATURE' ?\n\nSolution:\n\n'SIGNATURE' has no 'H'.\n\nQUESTION: 105\n\nThe square root of (2722 – 1282) is :\n\nSolution:", null, "QUESTION: 106\n\nFind total prime factor in the product of {(16)4 × (27)5 × (125)2 × (343)3}\n\nSolution:\n\n{(16)4 × (27)5 × (125)2 × (343)3}   =   24×4 × 33×5 × 53×2 × 73×3\n\n{(16)4 × (27)5 × (125)2 × (343)3}   =   216 × 315  × 5 × 79\n\n∴ Total Prime Factors = 16 + 15 + 6 + 9 = 46\n\nQUESTION: 107\n\nRead the information carefully and answer the following question.\n\nSix boys are sitting in a circle facing towards the centre of the circle. They are Prakash, Nikhil, Rohan, Suresh, Tarun and Vikram. Nikhil and Suresh are adjacent to each other but Nikhil is not to the right of Suresh. Prakash is next to the left of Vikram. Rohan is 4th to the right of Prakash.\n\nWho sits to the left of Tarun ?\n\nSolution:", null, "QUESTION: 108\n\nRead the information carefully and answer the following question.\n\nSix boys are sitting in a circle facing towards the centre of the circle. They are Prakash, Nikhil, Rohan, Suresh, Tarun and Vikram. Nikhil and Suresh are adjacent to each other but Nikhil is not to the right of Suresh. Prakash is next to the left of Vikram. Rohan is 4th to the right of Prakash.\n\nWhat is Vikram's position with respect to Rohan's ?\n\nSolution:", null, "QUESTION: 109\n\nRead the information carefully and answer the following question.\n\nSix boys are sitting in a circle facing towards the centre of the circle. They are Prakash, Nikhil, Rohan, Suresh, Tarun and Vikram. Nikhil and Suresh are adjacent to each other but Nikhil is not to the right of Suresh. Prakash is next to the left of Vikram. Rohan is 4th to the right of Prakash.\n\nIf Nikhil and Tarun interchange their position, then which of the following pair will sit between them ?\n\nSolution:", null, "QUESTION: 110\n\nBy using formula of mean proportional and third proportional, find the ratio of third proportional to 8 & 20 and mean proportional between 4 & 9.\n\nSolution:", null, "QUESTION: 111\n\nStudy the following table carefully to solve the given question.\n\nNumber of mobile phones manufactured by three companies in different years.", null, "What is the average number of mobile phones manufactured by Company B?\n\nSolution:", null, "QUESTION: 112\n\nStudy the following table carefully to solve the given question.\n\nNumber of mobile phones manufactured by three companies in different years.", null, "The number of mobile phones manufactured by company B in 2011 is approximately how much percent of mobile phones manufactured by company C in 2013?\n\nSolution:", null, "QUESTION: 113\n\nA man can row boat at 5 km/hr in still water. If the speed of current is 1 km/hr and he takes 1 hour to row to a place and come back, how far is the place ?\n\nSolution:", null, "QUESTION: 114\n\nIf in a certain language LOVELY is coded as OLEVOB, how FUTILE will be coded in that language ?\n\nSolution:", null, "QUESTION: 115\n\nWhich of the following set of letters when placed sequencially complete the given series ?\n\nGFE _ IG _ EII _ FEI _ GF _ II\n\nSolution:\n\nThe series will be : GFEII / GFEII / GFEII / GFEII.\n\nQUESTION: 116\n\nArrange the following words as per dictionary and select the correct option :\n\nI. Ascent, II. Assert, III. Ascend, IV. Assent\n\nSolution:\n\nCorrect order of the words is : Ascend, Ascent, Assent, Assert.\n\nQUESTION: 117\n\nIn a certain code language RADICAL is written as 2437645, how can the word DARE be written in that language ?\n\nSolution:", null, "QUESTION: 118\n\nSelect the combination of number so that the letters arranged accordingly will form a meaningful word :\n\nL   C   A   M    P   I   O    R\n\n1    2    3    4    5   6   7    8\n\nSolution:\n\nThe meaningful word will be PROCLAIM.\n\nQUESTION: 119\n\nConsidering the given statements true, decide which of the following conclusion(s) follow(s) definitely.\n\nStatements :\n\nI. All books are pens.\n\nII. Some pens are pencils.\n\nConclusion :\n\nI. All pens are books.\n\nII. Some pencils are books\n\nSolution:", null, "QUESTION: 120\n\n10 : 1100 : : ?\n\nSolution:\n\n1100 = (10)2 × 11\n\nSimilarly,\n\n576 = (8)2 × 9" ]
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https://us.metamath.org/mpeuni/pm5.41.html
[ "", null, "Metamath Proof Explorer < Previous   Next > Nearby theorems Mirrors  >  Home  >  MPE Home  >  Th. List  >  pm5.41 Structured version   Visualization version   GIF version\n\nTheorem pm5.41 382\n Description: Theorem *5.41 of [WhiteheadRussell] p. 125. (Contributed by NM, 3-Jan-2005.) (Proof shortened by Wolf Lammen, 12-Oct-2012.)\nAssertion\nRef Expression\npm5.41 (((𝜑𝜓) → (𝜑𝜒)) ↔ (𝜑 → (𝜓𝜒)))\n\nProof of Theorem pm5.41\nStepHypRef Expression\n1 imdi 381 . 2 ((𝜑 → (𝜓𝜒)) ↔ ((𝜑𝜓) → (𝜑𝜒)))\n21bicomi 216 1 (((𝜑𝜓) → (𝜑𝜒)) ↔ (𝜑 → (𝜓𝜒)))\n Colors of variables: wff setvar class Syntax hints:   → wi 4   ↔ wb 198 This theorem was proved from axioms:  ax-mp 5  ax-1 6  ax-2 7  ax-3 8 This theorem depends on definitions:  df-bi 199 This theorem is referenced by: (None)\n Copyright terms: Public domain W3C validator" ]
[ null, "https://us.metamath.org/mpeuni/mm.gif", null ]
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https://deepai.org/publication/reconfigurable-inverted-index
[ "", null, "# Reconfigurable Inverted Index\n\nExisting approximate nearest neighbor search systems suffer from two fundamental problems that are of practical importance but have not received sufficient attention from the research community. First, although existing systems perform well for the whole database, it is difficult to run a search over a subset of the database. Second, there has been no discussion concerning the performance decrement after many items have been newly added to a system. We develop a reconfigurable inverted index (Rii) to resolve these two issues. Based on the standard IVFADC system, we design a data layout such that items are stored linearly. This enables us to efficiently run a subset search by switching the search method to a linear PQ scan if the size of a subset is small. Owing to the linear layout, the data structure can be dynamically adjusted after new items are added, maintaining the fast speed of the system. Extensive comparisons show that Rii achieves a comparable performance with state-of-the art systems such as Faiss.\n\n## Code Repositories\n\n### rii\n\nFast and memory-efficient ANN with a subset-search functionality\n\n##### This week in AI\n\nGet the week's most popular data science and artificial intelligence research sent straight to your inbox every Saturday.\n\n## 1. Introduction\n\nIn recent years, the approximate nearest neighbor search (ANN) has received increasing attention from various research communities (Gudmundsson et al., 2018)\n\n. Typical ANN systems operate in two stages. In the offline phase, database vectors are stored in the ANN system. These vectors may be converted to other forms, such as compact codes, for fast searching and efficient memory usage. In the online querying phase, the system receives a query vector. Similar items to the query are retrieved from the stored database vectors. Their identifiers (and optionally their distances to the query) are then returned. To handle large datasets, this search should be not only fast and accurate, but also memory efficient.\n\nAlthough many ANN methods have already been proposed, there are two critical problems of practical importance that have not received sufficient attention from the research community (Fig. 3).\n\n• [leftmargin=15pt]\n\n• Subset search (Fig. (a)a): Once database vectors are stored, modern ANN systems can run a search efficiently for the whole database. Surprisingly, however, almost no systems can run a search over a subset of the database111 For example, the state-of-the-art systems Faiss (Jégou et al., 2018) and Annoy (Bernhardsson, 2018) do not provide this functionality. See discussion at https://github.com/facebookresearch/faiss/issues/322, https://github.com/spotify/annoy/issues/263 . For example, let us consider an image search problem, where the search is formulated as an ANN search over feature vectors. We assume that each image also has a corresponding shooting date. Given a query image, an ANN system can easily find similar images from the whole dataset. However, it is not trivial to find similar images that were taken on a target date (say, May 28 1987). Here, the search should not be conducted over the whole dataset, but rather over a subset of the dataset, where the subset is specified by identifiers of target images. The straightforward solution is to run the search and check whether or not the results were taken on May 28, but this post-checking can be drastically slow, especially if the size of the subset is small. Current ANN systems cannot provide a clear solution to this problem.\n\n• Performance degradation via data addition (Fig. (b)b): So far, the manner in which the search performance degrades when items are newly added has not been discussed. The number of database items is typically assumed to be provided when an ANN system is built. Parameters of the system are usually optimized by taking this number into consideration. However, in a practical scenario, new items might be often added to the system. Although the performance does not change while the number of new items is small, we can ask whether the system remains efficient even after items are newly added. To put this another way, suppose that one would like to develop a search system that can handle 1,000,000 vectors in the future, but only has 1,000 vectors in the initial stage. In such a case, is the search fast even for 1,000 vectors?\n\nWe develop an ANN system that solves the above two problems, namely reconfigurable inverted index (Rii). The key idea is extremely simple: storing the data linearly. Based on the well-known inverted file with product quantization (PQ) approach (IVFADC) (Jégou et al., 2011a), we design the data layout such that an item can be fetched by its identifier with a cost of . This simple but critical modification enables us to search over a subset of the dataset efficiently by switching to a linear PQ scan if the size of the subset is small. Owing to this linear layout, the granularity of a coarse assignment step can easily be controlled by running clustering again over the dataset whenever the user wishes. This means that the data structure can be adjusted dynamically after new items are added.\n\nAn extensive comparison with state-of-the-art systems, such as Faiss (Jégou et al., 2018), Annoy (Bernhardsson, 2018), Falconn (Razenshteyn and Schmidt, 2018), and NMSLIB (Naidan et al., 2018), shows that Rii achieves a comparable performance. For subset searches and data-addition problems for which the existing approaches do not perform well, we demonstrate that Rii remains fast in all cases.\n\nOur contributions are summarized as follows.\n\n• [leftmargin=15pt]\n\n• Rii enables efficient searching over a subset of the whole database, regardless of the size of the subset.\n\n• Rii remains fast, even after many new items are added, because the data structure is dynamically adjusted for the current number of database items.\n\n## 2. Related Work\n\nWe review existing work that is closely related to our approach.\n\n#### Locality-sensitive-hashing\n\nLocality-sensitive-hashing (LSH) (Datar et al., 2004)\n\ncan be considered as one of the most popular branches of ANN. Hash functions are designed such that the probability of collision is higher for close points than for points that are widely separated. Using these functions with hash tables, nearest items can be found efficiently. Although it has been said that LSH requires a lot of memory and is not accurate compared to data-dependent methods, a recent well-tuned library (FALCONN\n\n(Andoni et al., 2015; Razenshteyn and Schmidt, 2018)) using multi-probe technology (Lv et al., 2007) has achieved a reasonable performance.\n\n#### Projection/tree-based approach\n\nSpace partitioning using a projection or tree constitutes another significant branch of ANN. Especially in the computer vision community, one of the most widely employed methods is FLANN\n\n(Muja and Lowe, 2014). Recently, the random projection forest-based method Annoy (Bernhardsson, 2018) achieved a good performance for million-scale data.\n\n#### Graph traversal\n\nBenchmark scores (Aumüller et al., 2017; Bernhardsson et al., 2018) show that graph traversal-based methods (Malkov et al., 2014; Malkov and Yashunin, 2016) achieve the current best performance (the fastest with a fixed recall) when the number of database items is around one million. These methods first create a graph where each node corresponds to a database item, which is called a navigable small world. Given a query, the algorithm starts from a random initial node. The graph is traversed to the node that is the closest to the query. In particular, the hierarchical version HNSW (Malkov and Yashunin, 2016) with the highly optimized implementation NMSLIB (Boytsov and Naidan, 2013) represents the current state-of-the-art. The drawback is that it tends to consume memory space, with a long runtime for building the data structure.\n\n#### Product quantization\n\nProduct quantization (PQ) (Jégou et al., 2011a) and its extensions (Ge et al., 2014; Norouzi and Fleet, 2013; Babenko and Lempitsky, 2014; Martinez et al., 2016; Zhang et al., 2014, 2015; Babenko and Lempitsky, 2015b; Douze et al., 2016; Heo et al., 2014; Jain et al., 2016; Babenko and Lemitsky, 2017; Wang et al., 2015) are popular approaches to handling large-scale data. Our proposed Rii method also follows this line. PQ-based methods compress vectors into short memory-efficient codes. The Euclidean distance between an original vector and compressed code can be efficiently approximated using a lookup table. Current billion-scale search systems are usually based on PQ methods, especially combined with an inverted index-based architecture (Babenko and Lempitsky, 2015a; Kalantidis and Avrithis, 2014; Matsui et al., 2018b; Iwamura et al., 2013; Heo et al., 2016; Spyromitros-Xioufis et al., 2014; Xia et al., 2013). Hardware-based acceleration has also recently been discussed (André et al., 2015, 2017; Blalock and Guttag, 2017; Wieschollek et al., 2016; Johnson et al., 2017; Zhang et al., 2018; Liu et al., 2017). An efficient implementation proposed by the original authors is Faiss (Johnson et al., 2017; Jégou et al., 2018). An extensive survey is given in (Matsui et al., 2018a).\n\n## 3. Background: Product Quantization\n\nIn this section, we will review product quantization (PQ) (Jégou et al., 2011a). PQ compresses vectors into memory efficient short codes. The squared Euclidean distance between an input vector and the compressed code can be approximated efficiently. Owing to its memory-efficient form, PQ played a central role in large-scale ANN systems.\n\nWe first describe how to encode a vector. A -dimensional input vector is split into sub-vectors. Each -dimensional sub-vector is compared to pre-trained code words, and the identifier (an integer in ) of the closest one is recorded. Using this, is encoded as , which is a tuple of integers:\n\n (1) x↦¯x=[¯x1,…,¯xM]⊤∈{1,…,Z}M,\n\nwhere the th sub-vector in is quantized into . We refer to as a PQ-code for . Note that is represented by bits, and we set to 256 in order to represent each code using bytes.\n\nNext, we show how to search over the PQ-codes given a query vector . First, a distance table is computed online by comparing the query to the code words. Here, is the squared Euclidean distance between the th part of and th code word from the th codebook. The squared Euclidean distance between the query and the database vector can be approximately computed using the PQ-code , as follows:\n\n (2) d(q,x)2∼dA(q,¯x)2=M∑m=1A(m,¯xm).\n\nThis is called an asymmetric distance computation (ADC) (Jégou et al., 2011a), and can be performed efficiently, because only fetches are required on . A search over PQ-codes requires .\n\n## 4. Reconfigurable Inverted Index\n\nNow, we introduce our proposed approach: reconfigurable inverted index (Rii). Let us define a query vector , database vectors , and target identifiers . The subset-search problem is defined to find the similar items to the query from the subset of specified by :\n\n (3) R\\mathchar45argmins∈S∥q−xs∥22,\n\nwhere the operator finds the arguments for which an objective function attains (sorted) smallest values. The exact solution can be obtained by a time-consuming direct linear scan. Our goal is to approximately find nearest items in a fast and memory-efficient manner. Note that the problem turns out to be a usual ANN search if the whole database is set as the subset: .\n\n### 4.1. Data Structure\n\nFirst, input database vectors are encoded as PQ-codes , where each . These PQ-codes are stored linearly, meaning that they are stored in a single long array. Given an identifier , fetching requires a computational cost of .\n\nThe PQ-codes are clustered into groups for inverted indexing. First, coarse centers are created by running the clustering algorithm (Matsui et al., 2017) on (or its subset). Note that each coarse center is also a PQ-code . Using these coarse centers, the database PQ-codes are clustered into groups. The resulting assignments are stored as posting lists , where each is a set of identifiers of the database vectors whose nearest coarse center is the th one:\n\n (4) Wk={n∈{1,…,N}|a(n)=k}.\n\nNote that is an assignment function, that is defined as , where is a symmetric distance function that measures the distance between two PQ-codes (Jégou et al., 2011a; Matsui et al., 2017). Finally, we store , , and as a data structure for Rii. The total theoretical memory usage is bits if an integer is represented by 32 bits. We will show in Sec. 5.5 that this theoretical value is almost the same as the measured value.\n\nNote that in a typical implementation of the original IVFADC (Jégou et al., 2011a) system, PQ-codes are stored in posting lists (not a single array). That is, are chunked for each and then stored. This would enhance the locality of the data, and improve the cache efficiency when traversing a posting list. However, the experimental results (Sec. 5.5) showed that this difference is not serious.\n\n### 4.2. Search\n\nWe explain how to search for similar vectors using the data structure explained above. Our system provides two search methods: PQ-linear-scan and inverted-index. The former is fast when the size of a target subset is small, and the latter is fast when the size is large. Depending on the size, the faster method is automatically selected.\n\nA search over a subset of a database is defined as a search on target PQ-codes denoted by the target identifiers . Note that we assume that the elements of are sorted222 A set is denoted by calligraphic font, such as , and implemented by a single array. . This is a slightly strong but reasonable assumption. Because is sorted, it can be checked whether or not an item is contained in a set () with a cost of using a binary search, where is the number of elements in . Note again that a search over the whole dataset is available by setting .\n\n#### PQ-linear-scan\n\n: Because the database PQ-codes are stored linearly, we can simply pick up target PQ-codes and evaluate the distances to the query. We call this a PQ-linear-scan. This is essentially fast if is small, because only a fraction of vectors are compared. The pseudocode is presented in Alg. 1.\n\nAs inputs, the system accepts a query vector , database PQ-codes , the number of returned items , and the target identifiers . First, a distance table is created by comparing a query to code words333 We intentionally omitted the code words from the pseudocode, for simplicity. (L1). This is an online pre-processing step, required for all PQ-based methods. To store the results, an array of tuples is prepared (L2). Each tuple consists of (1) an identifier of an item and (2) the distance between the query and the item. For each target identifier , the asymmetric distance to the query is computed (L4). This distance is then stored in the result array with its identifier , where the PushBack function is used to append an element to an array (L5). After all target items have been evaluated, the result array is sorted by the distance (L6). As we require only the top results, we use a partial sort algorithm. Finally, the top elements are returned, where the Take function simply picks up the first several elements (L7). Note that and are not required for the search.\n\nLet us analyze the computational cost. The creation of a distance table requires , and a comparison to items requires . Partial sorting requires on average444 This cost comes from the heap sort-based implementation used in the partial_sort function in C++ STL. Another option is to pick up the smallest items and only sort these. This leads to . We used the former in this paper because we empirically determined that the former is faster in practice, especially when is small. . Their sum leads to a final average cost (Table 1). It is clear that the computation is efficient if is small. As the cost depends on linearly, a PQ-linear-scan becomes inefficient if is large. Note that if the search target is the whole dataset, is replaced by .\n\n#### Inverted-index\n\n: The other search method is inverted-index. Because the database items are preliminarily clustered as explained in Sec. 4.1, we can simply evaluate items that are in the same/close clusters to the query. This drastically boosts the performance if the number of the target identifiers is large.\n\nWe show the pseudo-code in Alg. 2. Inverted-index takes three additional inputs: posting lists , coarse centers , and the number of candidates . Note that candidates will be selected and evaluated in the final step. This means that is a runtime parameter that controls the trade-off between the accuracy and runtime.\n\nTo search, a distance table is first created in the same manner as for PQ-linear-scan (L1). The search steps consists of two blocks. First, the closest clusters to the query are found (L2-6). Then, the items inside the clusters are evaluated (L7-16).\n\nTo find the closest clusters, an array of tuples is created (L2). For each coarse center (, the distance from the query is computed (L4). The results are stored in the array (L5).\n\nNext, we run partial sort on the array to find the closest clusters to the query (L6). Here, the target number of the partial sort (the number of postings lists to be focused) is set as , which is determined as follows. Because the target identifiers are of size , where the total number of identifiers is , the probability of any item being a target identifier is on average. Because our purpose here is to select target items as candidates of the search, the required number of items to traverse is . To traverse items, we need to focus on posting lists, because the average number of items per posting list is . This implies that we need to select the nearest posting lists. Note that if , we simply replace the value by , because this performs a full sort of the array ().\n\nThe selected posting lists are then evaluated. A score array is prepared (L7). For each closest posting list (L8), identifiers in the posting list are traversed (L9). If an identifier is not included in the target identifier , then this item is simply ignored (L10-11). Note that if the search is for the whole dataset (), any item is always included in , thus we remove L10-11.\n\nFor a selected identifier , the identifier and the distance to the query are recorded in the same manner as for the PQ-linear-scan (L12-13). If the size of the score array () reaches the parameter , then the top results are selected and returned (L14-16).\n\nThe computational cost is summarized as follows. After the code creation with , the comparison to coarse centers requires . Partial sort requires . The number of items to be traversed is . We can check whether or not each item is included in using a binary search, requiring . This leads to in total. The number of items that are actually evaluated is , and so of the cost is required. Finally, the top are selected using the partial sort, requiring . Table 1 summarizes the computational cost. Inverted-index is fast when is sufficiently large, but is slow if is small. This is highlighted in the term , where this term becomes dominant if is small.\n\nNote that although there appear to be several input parameters for inverted-index, all of them except are usually decided deterministically. is the only parameter the user needs to decide. Our initial setting is the average length of a posting list, . This means that the system traverses one posting list on average. This is a fast setting, and users can change this if they require more accuracy, as .\n\n#### Selection\n\n: The final query algorithm is described in Alg. 3. Given inputs, the system automatically determines the query method as either PQ-linear-scan or inverted-index. This decision is based on the threshold value for the number of target identifiers (L1). Owing to this flexible switching, we can always achieve a fast search with a single Rii data structure (, , and ), regardless of the sizes of the target identifiers (). Fig. 4 highlights the relations among the three query algorithms.\n\nNote that it is not trivial to set the threshold deterministically, because it depends on several parameters, such as and . To find the best threshold, we simply run the search with several parameter combinations when the data structure is constructed. Based on the result, we fit a 1D line in the parameter space, and finally obtain the best threshold. See the supplementary material for more details. This works almost perfectly, as shown in Fig. 4. This thresholding does not require any additional runtime cost for the search phase.", null, "Figure 4. Comparison of PQ-linear-scan, inverted-index, and the final query algorithm. Runtime per query for the SIFT1M dataset with various sizes of target identifiers is plotted. Note that L=K=1000,R=1,θ=24743.\n\n### 4.3. Reconfiguration\n\nHere, we introduce a reconfigure function that enables us to search efficiently even if a large number of vectors are newly added. As discussed in Sec. 1, typical ANN systems are first optimized to achieve fast searching for items. If new items are added later, such systems might become slow. For example, IVFADC requires an initial decision on the number of space partitions . The selection of is sensitive and critical to the performance. A standard convention is to set . On the other hand, cannot be changed later. The system could become slower if changes significantly. In other words, we must decide even if the final database size is not known, which sometimes frustrates users.\n\nUnlike these existing methods, Rii provides a reconfigure function. If the search becomes slow because of newly added items, coarse centers and assignments are updated by simply running clustering again. The system is automatically optimized to achieve the fastest search for the current number of database items.\n\nLet us first explain how to add a new item. Given a new PQ-code , the database PQ-codes are updated using PushBack(, ). A corresponding posting list is also updated by PushBack(). Then, searching can be performed without any modifications, but it may be slower if many items are added. This is because the length of each posting list () can become too long, making the traversal inefficient.\n\n#### Reconfigure\n\nIf the search becomes slow, a reconfigure function can be called (Alg. 4). This function takes the database PQ-codes and a new number of coarse space partitions as inputs. Again, is typically set as for the new . The outputs are updated posting lists and coarse centers. First, the updated coarse centers are computed by running clustering over the PQ-codes using PQk-means (Matsui et al., 2017) (L1). PQk-means efficiently puts the input PQ-codes into several clusters, without decoding the codes for the original -dimensional vectors. Note that clustering can be run for a subset of to make this fast. We set the upper limit of the codes to be clustered as . After new coarse centers are obtained, the posting lists are created by simply finding the nearest center for each PQ-code (L2-4).\n\nThe advantage of the reconfigure function is that it can be called whenever the user wishes. The results are deterministic for , because this just runs the clustering over the codes. We will show in Sec. 5.4 that this reconfigure function is especially useful when the database size drastically changes. Another way of looking at this is that we do not need to know the final number of database items when the index structure is built. This is a clear advantage over IVFADC-based methods. In a practical scenario, it will often occur that the number of database items cannot be decided when the system is created. Even in such cases, IVFADC must decide the parameters. This would lead to a suboptimal performance.\n\nThe data structure proposed above is similar to the original IVFADC (Jégou et al., 2011a), but has the following fundamental differences.\n\n• [leftmargin=15pt]\n\n• In Rii, each vector is encoded directly, whereas IVFADC encodes a residual between an input vector and a coarse center. This makes the accuracy of Rii slightly inferior to that of IVFADC (see Sec. 5.5), but enables us to store PQ-codes linearly.\n\n• In Rii, PQ-codes are stored linearly, and their identifiers are stored in posting lists. In IVFADC, both PQ-codes and identifiers are stored in posting lists. This simple modification enables us to run the PQ-linear scan without any additional operations.\n\n• In IVFADC, coarse centers are a set of -dimensional vectors, whereas coarse centers in Rii are PQ-codes. The advantage of this is that the reconfigure steps become considerably fast with PQk-means. The limitation is that this might decrease the accuracy, but the experimental results show that this degradation is not serious (Sec. 5.5).\n\nThere exist advanced encoding methods for PQ, such as optimized product quantization (OPQ) (Ge et al., 2014; Norouzi and Fleet, 2013), additive quantization (AQ) (Babenko and Lempitsky, 2014; Martinez et al., 2016), and composite quantization (CQ) (Zhang et al., 2014, 2015). Although state-of-the-art accuracy has been achieved by AQ or CQ, it is widely known that they are more complex and time consuming. Therefore, we did not incorporate AQ and CQ in our system.\n\nOn the other hand, OPQ provides a reasonable trade-off (slightly slow but with a high accuracy). In OPQ, a rotation matrix is preliminarily trained to minimize the error. In the search phase, an input vector is first rotated with the matrix. The remaining process is exactly the same as PQ. We will show the results of OPQ in Sec. 5.5.\n\n## 5. Evaluations\n\nAll experiments were performed on a server with a 3.6 GHz Intel Xeon CPU (six cores, 12 threads) and 128 GB of RAM. For a fair comparison, we employed a single-thread implementation for the search. Rii is implemented by C++ with a Python interface, All source codes are publicly available\n\n### 5.1. Datasets\n\nThe various methods were evaluated using the following datasets:\n\n• [leftmargin=15pt]\n\n• SIFT1M (Jégou et al., 2011b) consists of 128D SIFT feature vectors extracted from several images. It provides 1,000,000 base, 10,000 query, and 100,000 training vectors.\n\n• GIST1M (Jégou et al., 2011b) consists of 960D GIST feature vectors extracted from several images. It provides 1,000,000 base, 1,000 query, and 500,000 training vectors.\n\n• Deep1B (Babenko and Lempitsky, 2016)\n\nconsists of 96D deep features extracted from the last FC layer of GoogLeNet\n\n(Szegedy et al., 2015) for one billion images. It provides 1,000,000,000 base, 10,000 query, and 1,000,000 (we used the top 1M from the whole training branch) training vectors.\n\nThe code words of Rii and Faiss were preliminarily trained using the training data. The search is conducted over the base vectors.\n\n### 5.2. Methods\n\nWe compare our Rii method with the following existing methods:\n\n• [leftmargin=15pt]\n\n• Annoy (Bernhardsson, 2018): A random projection forest-based system. Because Annoy is easy to use (fewer parameters, intuitive interface, no training steps, and easy IO with a direct mmap design), it is the baseline for million-scale data.\n\n• FALCONN (Razenshteyn and Schmidt, 2018): Highly optimized LSH (Andoni et al., 2015). FALCONN is regarded as a representative state-of-the-art LSH-based method.\n\n• NMSLIB (Naidan et al., 2018): Highly optimized ANN library with the support of non-metric spaces (Boytsov and Naidan, 2013). This library includes several algorithms, and we used Hierarchical Navigable Small World (HNSW) (Malkov et al., 2014; Malkov and Yashunin, 2016) in this study. NMSLIB with HNSW is the current state-of-the-art for million-scale data (Aumüller et al., 2017; Bernhardsson et al., 2018).\n\n• Faiss (Jégou et al., 2018): A collection of highly-optimized PQ-based methods. This library includes IVFADC (Jégou et al., 2011a), OPQ (Ge et al., 2014), inverted multi-index (Babenko and Lempitsky, 2015a), and polysemous codes (Douze et al., 2016). Some of these are implemented using the GPU as well (Johnson et al., 2017). In particular, we compared Rii with the basic IVFADC, which is one of the fastest options. Note that only Faiss and Rii can handle billion-scale data, because PQ-based methods are memory efficient.\n\n### 5.3. Subset Search\n\nWe first present the results for searching over a subset of the whole database. This is the main function that the proposed Rii method provides. The conclusion is that Rii always remains fast, whereas existing methods become considerably slower, especially if the size of the target subset is small. We first explain the task, and then introduce a post-checking module through which existing methods can conduct a subset search. Finally, we present the results.\n\nThe task is defined as follows. We randomly select integers from , sort them, and construct the target indices . For each query, we run the search and find the top- results. All the results must be members of . The runtime per query was reported with several combinations of and . The evaluation was conducted using the SIFT1M dataset (), with .\n\n#### Post-checking module\n\nBecause none of the existing methods provide a subset search functionality, we implemented a straightforward post-checking module in order to enable the existing methods to perform a subset search. Alg. 5 shows the pseudocode. This module takes a query function , a query vector , target identifiers , and the number of returned items as inputs. The query function returns the identifiers of the closest items, given and . This is an existing method such as Annoy. First, the output identifier set is prepared (L1). The number of returned items for each iteration, , is first initialized (L2). Then, the search begins with an infinite loop. The top- items are searched using , and the results are stored in the temporal buffer (L4). For each identifier in , if has already been checked, the loop continues (L6-7). This is actually achieved by starting a for loop with some offsets over , so that the first already-checked elements up to a certain number are not traversed. If is included in , we store it in the output set (L8-9). The algorithm finishes if the enough () items are found (L10-11). If an insufficient number of items are found, then is updated to a larger number by simply multiplying a constant value (L12). The search continues with the updated until items are found.\n\nWith this module, searching over a target subset is made available for the existing methods. Note that cannot always return items when is large. This depends on the design of the query function, and some methods have a limit on in order not to make the search too slow. We found that FALCONN and NMSLIB do not return items if is large. Therefore, we compared Rii with Annoy using the post-checking module (Annoy + PC).\n\n#### Results\n\nFig. 5 illustrates the results. We point out the following:\n\n• [leftmargin=15pt]\n\n• Rii was fast under all conditions (less than 2 ms/query). We can conclude that Rii was stable and effective for the subset-search.\n\n• As with IVFADC, Rii is robust against .\n\n• Annoy + PC became drastically slow for small , which is further highlighted when is large. This is an obvious result, because the while loop (L3 in Alg. 5) must be repeated several times for large . Here, can be even . ANN systems are usually not designed to handle such values.", null, "Figure 5. Subset search using the SIFT1M dataset over 10 queries. Note that K=L=1000,M=64.\n\n### 5.4. Robustness Against Data Addition\n\nWe describe the experiments for our other main function, reconfigure. The conclusion is that Rii becomes fast by using reconfigure, even after many new vectors are added. First, the task is explained, then the results are presented. Here, we used the Deep1B dataset to demonstrate the robustness against billion-scale data.\n\nThe index is first constructed using vectors with , and then the runtime is evaluated. Next, new items are added to the index, so that the final becomes . Then, the runtime is evaluated in two ways: (1) a search is performed with , and (2) the data structure is updated using the reconfigure function with , and then the search is conducted. We run this experiment with the final as , , and .\n\n#### Results\n\nFig. 6 illustrates the result. It is clear that the search becomes dramatically faster after the reconfigure function is called. For example, if the user keeps the same data structure after new items are added, the search takes an average of 3.9 ms. This can be made faster after applying the reconfigure function.\n\nMost importantly, because the data structure can be always adjusted for the new , the user need not face the burden of selecting when the system is constructed. This is a clear advantage over the other existing methods. Note that the runtime for adding vectors was 109 s, and that of the reconfigure function with was 111 s. These times can be considered moderate.", null, "Figure 6. The runtime performance with and without the reconfigure function over the Deep1B dataset, where R=1, M=8, and L=N/K.\n\n### 5.5. Comparison with Existing Methods\n\nFinally, we compare Rii (and its variant Rii-OPQ) with Annoy, FALCONN, NMSLIB (HNSW), and Faiss (IVFADC), using SIFT1M and GIST1M. The conclusion is that our Rii method achieved a comparable performance to the state-of-the-art system Faiss. Note that the searches were conducted over the whole datasets.\n\nThe accuracy was measured using Recall@1, which measures the fraction of queries for which the ground truth nearest neighbor is returned within the top-1 result. The average Recall@1 over the query set is reported. We evaluated the methods with several parameter combinations, and report the results with a fixed Recall@1 (0.65 for SIFT1M and 0.5 for GIST1M) for a fair comparison. Because the ranges of some parameters are discrete, we cannot achieve an exact target Recall@1. Thus, the target Recall@1 was selected as best as possible as a value that all methods can achieve.\n\nThe disk consumption of the index data structure is also reported. This was measured by storing the data structure on the disk and checking its size in bytes. Note that the runtime (peak-time) memory consumption is the more important measure, but measuring the peak-time memory usage is not always stable, and can vary depending on the computer. Thus, we report the disk space instead, which is reproducible and strongly related to the memory consumption. The runtime of building the data structure is also reported.\n\nTable 2 presents the results. We summarize our findings:\n\n• [leftmargin=15pt]\n\n• Rii was comparable with the state-of-the-art system Faiss. In particular, although our method is basically an approximation of IVFADC, the decrease in the accuracy is not significant.\n\n• Rii was the most memory efficient among the methods. The measured value is almost same as the theoretically predicted value (68 MB against 69 MB and 244 MB against 249 MB).\n\n• If we compare Rii and Rii-OPQ, Rii-OPQ was slightly slower but a little more accurate with the same parameter settings.\n\n• Annoy achieved the second fastest result. Because Annoy supports the direct memory map system, the construction required some time and consumed a relatively large disk space.\n\n• FALCONN achieved a comparable (or slightly slower) performance to Faiss/Rii. We note that the building cost of FALCONN is considerably smaller than for other methods. As FALCONN does not provide IO functions, we did not report the disk space.\n\n• As reported in the benchmark (Aumüller et al., 2017; Bernhardsson et al., 2018), NMSLIB achieved the fastest performance. On the other hand, the building time and memory consumption are inferior relative to Faiss/Rii.\n\n• The results for SIFT1M and GIST1M follow similar tendencies.\n\n## 6. Application\n\nWe present an application to highlight the subset search function of Rii. For this demonstration, we leverage the data of The Metropolitan Museum of Art (MET) Open Access. This dataset contains more than 420,000 items from MET, with both the image and extensive metadata for each item (Table 3). From this data, we select 201,998 items that are provided with the Creative Common license. For each image, we extracted a 1,920-dimensional activation of last average pooling layer of the DenseNet-201 (Huang et al., 2017)\n\narchitecture trained with ImageNet. The features are stored in Rii with\n\n. Several meta-information is stored in a table using Pandas, which is a popular on-memory data management system for Python.\n\nFig. 7 demonstrates the system, including Python codes and the search results. The metadata and DenseNet vectors are first read. Then, the search is conducted based on the metadata. Here, the items that were created before A.D. 500 in Egypt are specified. Next, the target identifiers are prepared. This is simply a set of IDs of the selected items. The image-based search is then conducted over them. The query here is Chinese tapestry. We can find similar items to the Chinese tapestry from the museum items in ancient Egypt.\n\nAs this demonstration reveals, the search using the target subset is a general problem setting. Rii can solve this type of problem easily. As Sec. 5.3 shows, existing methods using the late checking module do not perform well when is small. For example, in this case the result of the metadata search can have any number of items. Rii can handle a subset search for any size of .", null, "Figure 7. Demonstration of the subset search. The target items are first selected using metadata information. Then, an image-based search is conducted over the target items.\n\n## 7. Conclusions\n\nWe developed an approximate nearest neighbor search method, called Rii. Rii provides the two functions of searching over a subset and a reconfigure function for newly added vectors. Extensive comparisons showed that Rii achieved a comparable performance to state-of-the art systems, such as Faiss.\n\nNote that the latest systems incorporate HNSW for the coarse assignment of IVFADC (Baranchuk et al., 2018; Douze et al., 2018). Our Rii architecture can be combined to them, but that will be remained as a future work.\n\nAcknowledgments: This work was supported by JST ACT-I Grant Number JPMJPR16UO, Japan.\n\n## References\n\n• (1)\n• Andoni et al. (2015) Alexandr Andoni, Piotr Indyk, Thijs Laarhoven, Ilya Razenshteyn, and Ludwig Schmidt. 2015. Practical and Optimal LSH for Angular Distance. In Proc. NIPS.\n• André et al. (2015) Fabien André, Anne-Marie Kermarrec, and Nicolas Le Scouarnec. 2015. Cache Locality is Not Enough: High-performance Nearest Neighbor Search with Product Quantization Fast Scan. In Proc. VLDB.\n• André et al. (2017) Fabien André, Anne-Marie Kermarrec, and Nicolas Le Scouarnec. 2017. Accelerated Nearest Neighbor Search with Quick ADC. In Proc. ICMR.\n• Aumüller et al. (2017) Martin Aumüller, Erik Bernhardsson, and Alexander Faithfull. 2017. ANN-Benchmarks: A Benchmarking Tool for Approximate Nearest Neighbor Algorithms. In Proc. SISAP.\n• Babenko and Lemitsky (2017) Artem Babenko and Victor Lemitsky. 2017. AnnArbor: Approximate Nearest Neighbors Using Arborescence Coding. In Proc. IEEE ICCV.\n• Babenko and Lempitsky (2014) Artem Babenko and Victor Lempitsky. 2014. Additive Quantization for Extreme Vector Compression. In Proc. IEEE CVPR.\n• Babenko and Lempitsky (2015a) Artem Babenko and Victor Lempitsky. 2015a. The Inverted Multi-Index. IEEE TPAMI 37, 6 (2015), 1247–1260.\n• Babenko and Lempitsky (2015b) Artem Babenko and Victor Lempitsky. 2015b. Tree Quantization for Large-Scale Similarity Search and Classification. In Proc. IEEE CVPR.\n• Babenko and Lempitsky (2016) Artem Babenko and Victor Lempitsky. 2016. Efficient Indexing of Billion-Scale Datasets of Deep Descriptors. In Proc. IEEE CVPR.\n• Baranchuk et al. 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(2018) Matthijs Douze, Alexandre Sablayrolles, and Hervé Jégou. 2018. Link and code: Fast indexing with graphs and compact regression codes. In Proc. IEEE CVPR.\n• Ge et al. (2014) Tiezheng Ge, Kaiming He, Qifa Ke, and Jian Sun. 2014. Optimized Product Quantization. IEEE TPAMI 36, 4 (2014), 744–755.\n• Gudmundsson et al. (2018) Gylfi Þór Gudmundsson, Björn Þór Jónsson, Laurent Amsaleg, and Michael J. Franklin. 2018. Prototyping a Web-Scale Multimedia Retrieval Service Using Spark. ACM TOMM 14, 3s (2018), 65:1–65:24.\n• Heo et al. (2016) Jae-Pil Heo, Zhe Lin, Xiaohui Shen, Jonathan Brandt, and Sung-Eui Yoon. 2016.\n\nShortlist Selection With Residual-Aware Distance Estimator for K-Nearest Neighbor Search. In\n\nProc. IEEE CVPR.\n• Heo et al. (2014) Jae-Pil Heo, Zhe Lin, and Sung-Eui Yoon. 2014. Distance Encoded Product Quantization. In Proc. IEEE CVPR.\n• Huang et al. (2017) Gao Huang, Zhuang Liu, Laurens van der Maaten, and Kilian Q. Weinberger. 2017. Densely Connected Convolutional Networks. In Proc. IEEE CVPR.\n• Iwamura et al. (2013) Masakazu Iwamura, Tomokazu Sato, and Koichi Kise. 2013. What Is the Most Efficient Way to Select Nearest Neighbor Candidates for Fast Approximate Nearest Neighbor Search?. In Proc. IEEE ICCV.\n• Jain et al. (2016) Himalaya Jain, , Patrick Pérez, Rémi Gribonval, Joaquin Zepeda, and Hervé Jégou. 2016. Approximate Search with Quantized Sparse Representations. In Proc. ECCV.\n• Jégou et al. (2018) Hervé Jégou, Matthijs Douze, and Jeff Johnson. 2018. Faiss.\n• Jégou et al. (2011a) Hervé Jégou, Matthijis Douze, and Cordelia Schmid. 2011a. Product Quantization for Nearest Neighbor Search. IEEE TPAMI 33, 1 (2011), 117–128.\n• Jégou et al. (2011b) Hervé Jégou, Romain Tavenard, Matthijs Douze, and Laurent Amsaleg. 2011b. Searching in One Billion Vectors: Re-rank with Source Coding. In Proc. IEEE ICASSP.\n• Johnson et al. (2017) Jeff Johnson, Matthijs Douze, and Hervé Jégou. 2017. Billion-scale Similarity Search with GPUs. CoRR abs/1702.08734 (2017).\n• Kalantidis and Avrithis (2014) Yannis Kalantidis and Yannis Avrithis. 2014. Locally Optimized Product Quantization for Approximate Nearest Neighbor Search. In Proc. IEEE CVPR.\n• Liu et al. (2017) Yingfan Liu, Hong Cheng, and Jiangtao Cui. 2017. PQBF: I/O-Efficient Approximate Nearest Neighbor Search by Product Quantization. In Proc. CIKM.\n• Lv et al. (2007) Qin Lv, William Josephson, Zhe Wang, Moses Charikar, and Kai Li. 2007. Multi-Probe LSH: Efficient Indexing for High-Dimensional Similarity Search. In Proc. VLDB.\n• Malkov et al. (2014) Yury Malkov, Alexander Ponomarenko, Andrey Logvinov, and Vladimir Krylov. 2014. Approximate Nearest Neighbor Algorithm Based on Navigable Small World Graphs. Inf. Syst. 45 (2014), 61–68.\n• Malkov and Yashunin (2016) Yury A. Malkov and Dmitry A. Yashunin. 2016. Efficient and Robust Approximate Nearest Neighbor Search using Hierarchical Navigable Small World Graphs. CoRR abs/1603.09320 (2016).\n• Martinez et al. (2016) Julieta Martinez, Joris Clement, Holger H. Hoos, and James J. Little. 2016. Revisiting Additive Quantization. In Proc. ECCV.\n• Matsui et al. (2017) Yusuke Matsui, Keisuke Ogaki, Toshihiko Yamasaki, and Kiyoharu Aizawa. 2017. PQk-means: Billion-scale Clustering for Product-quantized Codes. In Proc. MM.\n• Matsui et al. (2018a) Yusuke Matsui, Yusuke Uchida, Hervé Jégou, and Shin’ichi Satoh. 2018a. A Survey of Product Quantization. ITE Transactions on Media Technology and Applications 6, 1 (2018), 2–10.\n• Matsui et al. (2018b) Yusuke Matsui, Toshihiko Yamasaki, and Kiyoharu Aizawa. 2018b. PQTable: Non-exhaustive Fast Search for Product-quantized Codes using Hash Tables. IEEE TMM 20, 7 (2018), 1809–1822.\n• Muja and Lowe (2014) Marius Muja and David G. Lowe. 2014.\n\nScalable Nearest Neighbor Algorithms for High Dimensional Data.\n\nIEEE TPAMI 36, 11 (2014), 2227–2240.\n• Naidan et al. (2018) Bilegsaikhan Naidan, Leonid Boytsov, Yury Malkov, David Novak, and Ben Frederickson. 2018. Non-Metric Space Library (NMSLIB).\n• Norouzi and Fleet (2013) Mohammad Norouzi and David J. Fleet. 2013.\n\nCartesian k-means. In\n\nProc. IEEE CVPR.\n• Razenshteyn and Schmidt (2018) Ilya Razenshteyn and Ludwig Schmidt. 2018. FALCONN - FAst Lookups of Cosine and Other Nearest Neighbors.\n• Spyromitros-Xioufis et al. (2014) Eleftherios Spyromitros-Xioufis, Symeon Papadopoulos, Ioannis (Yiannis) Kompatsiaris, Grigorios Tsoumakas, and Ioannis Vlahavas. 2014.\n\nA Comprehensive Study Over VLAD and Product Quantization in Large-Scale Image Retrieval.\n\nIEEE TMM 16, 6 (2014), 1713–1728.\n• Szegedy et al. (2015) Christian Szegedy, Wei Liu, Yangqing Jia, Pierre Sermanet, Scott Reed, Dragomir Anguelov, Dumitru Erhan, Vincent Vanhoucke, and Andrew Rabinovich. 2015. Going Deeper With Convolutions. In Proc. IEEE CVPR.\n• Wang et al. 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https://goodmancoaching.nl/does-infinity-exist-in-the-real-worldother-than-just-in-mathmatics/
[ "# Does infinity exist in the real world,other than just in mathmatics?\n\nContents\n\n## Does infinity exist outside of math?\n\nIn the context of a number system, in which “infinity” would mean something one can treat like a number. In this context, infinity does not exist.\n1 сент. 1997\n\n## Is there infinity in the real world?\n\nActual infinity does not exist. What we call infinite is only the endless possibility of creating new objects no matter how many exist already. ” H. Poincar e (1854-1912). “Every infinity is potential.” Aristotle (384 BC – 322 BC) “Actual infinity exists” Geprge Cantor (1845-1918) It is a very controversial question.\n\n## What is an example of infinity in real life?\n\nAnother good example of infinity is the number π or pi. Mathematicians use a symbol for pi because it’s impossible to write the number down. Pi consists of an infinite number of digits. It’s often rounded to 3.14 or even 3.14159, yet no matter how many digits you write, it’s impossible to get to the end.\n\n## Can humans understand infinity?\n\nFor many of us, it’s easy to understand the concept of infinity, but we can’t comprehend how “big” or “never-ending” it is, because our perception of time always has a beginning and an end — minutes, days, years, lifespans.\n\n## What is infinity in life?\n\nInfinity Symbol Meaning in Spirituality and Meditation\nLife is infinite. Our time on earth may be finite but our souls exist forever. In meditation, the symbol of infinity is used to remind us of balance, focus, harmony, peace, and oneness.\n\n## What is infinity in this world?\n\nInfinity is the idea of something that has no end. In our world we don’t have anything like it. So we imagine traveling on and on, trying hard to get there, but that is not actually infinity. So don’t think like that (it just hurts your brain!).\n\n## What is truly infinite?\n\n“For generally the infinite has this mode of existence: one thing is always being taken after another, and each thing that is taken is always finite, but always different.” — Aristotle, Physics, book 3, chapter 6.\n\n## What is beyond infinity?\n\nNot only is the infinity of decimals bigger than that of the counting numbers – there is no biggest infinity. Beyond infinity is another infinity, and beyond that is yet another… and even after you’ve reached an infinity of infinities, there’s still another infinity beyond that.\n\n## Why is infinity useful?\n\nIt is also useful in geometry (by analyzing infinitely close points) and inequalities (by analyzing the effect of an infinitely small change), as well as many other areas where the effects of an infinitely small change can be analyzed.\n\n## How many types of infinity are there?\n\nCantor defined two kinds of infinite numbers: ordinal numbers and cardinal numbers. Ordinal numbers characterize well-ordered sets, or counting carried on to any stopping point, including points after an infinite number have already been counted.\n\n## Who created infinity?\n\nmathematician John Wallis\n\ninfinity, the concept of something that is unlimited, endless, without bound. The common symbol for infinity, ∞, was invented by the English mathematician John Wallis in 1655. Three main types of infinity may be distinguished: the mathematical, the physical, and the metaphysical.\n\n## Where does infinity come from?\n\nInfinity is derived etymologically from the Latin, infinitas, which is a combination of in (meaning not) and finis (meaning end, boundary, limit, termination, etc.). In general, the word signifies the state or condition arising from an entity’s not having some sort of end, limit, termination, or determining factor.\n\n## Is infinity real philosophy?\n\nModern philosophical views\nModern discussion of the infinite is now regarded as part of set theory and mathematics. Contemporary philosophers of mathematics engage with the topic of infinity and generally acknowledge its role in mathematical practice." ]
[ null ]
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http://petsharelink.com/index.asp
[ "创造营2021", null, "[(2021.11.1)] 深耕细研踏歌行 齐心协力共提升\n\n[(2021.11.1)] 精诚团结共发展,教学研讨同提升\n\n[(2021.11.1)] 潜心专研,携手互助,共同成长!\n\n[(2021.11.1)] 同课异构展风采,教学研讨促成长\n\n[(2021.10.15)] 国庆新民俗,八中开好头\n\n[(2021.10.15)] 爱国 爱校 爱学习――八中东校区第一次表彰大..\n\n[(2021.10.2)] 军训生涯,不负韶华――驻马店市第八中学新生..\n\n[(2021.10.2)] 更上层楼山水阔 无边光景一时新\n\n[(2021.10.2)] 少年强则国强,吾辈当自强\n\n[(2021.7.19)] 一路同行,一路感恩!\n\n[(2021.7.19)] 青春拂晓 圆梦今朝―2021毕业典礼\n\n[(2021.6.1)] 红旗飘扬党百年,诗词盛会颂华章\n\n[(2021.5.23)] 特色办学立潮头,教研教改八中行\n\n[(2021.5.23)] 同读百年党史,悦享万卷书香\n\n[(2021.5.1)] 共商共研 精准备考\n\n(2015.4.23) 品味橡皮章[图]\n\n(2013.5.2) 理化生实验课[图]\n\n(2013.5.2) 理化生实验[图]\n\n(2013.5.2) 理化生实验[图]\n\n(2013.5.2) 理化生实验[图]\n\n(2013.4.27) 纪念革命烈士 弘扬民族精神主题班会[图]\n\n(2013.4.27) 美术社团活动[图]\n\n(2013.4.27) 美术社团活动[图]\n\n(2013.4.27) 雷锋精神主题班会[图]\n\n(2013.4.26) 建团九十周年手抄报[图]\n\n(2013.4.26) 收看感动中国刘伟事迹[图]\n\n(2013.4.26) 收看禁毒知识片[图]\n\n(2013.4.26) 艺术节展版[图]\n\n(2013.4.26) 艺术节展版[图]\n\n(2013.4.26) 艺术节展版[图]\n\n(2013.4.26) 艺术节展版[图]\n\n(2013.4.26) 篮球绕杆跑[图]\n\n[(2013.4.26)] 《驻马店日报》报道我校举办英语演讲比赛\n\n[(2013.4.26)] 《驻马店日报》报道我校骨干教师到山东潍坊五..\n\n[(2013.4.26)] 《天中晚报》报道九年级学生备考中招体育考试..\n\n[(2013.4.26)] 《天中晚报》报道我校深入推进课程改革情况\n\n[(2013.4.26)] 《河南经济报》大幅报道我校特色办学纪实\n\n[(2013.4.26)] 《天中晚报》大幅版面报道我校特色课改纪实\n\n[(2013.4.26)] 高效实效,向幸福教育出发------河南卫视走进..\n\n[(2013.4.24)] 《驻马店日报》报道我校举办向道德模范看齐活..\n\n[(2013.4.24)] 《驻马店日报》报道我校交通安全知识讲座\n\n[(2013.4.24)] 中国新闻网深入我校采访\n\n[(2013.4.24)] 河南卫视再次走进八中\n\n[(2013.5.21)] 《七色光》第二期\n\n[(2013.5.21)] 《七色光》第一期\n\n[(2013.5.21)] 《七色光》第三期\n\n[(2013.5.21)] 《七色光》第二期\n\n[(2013.4.24)] 《七色光》第一期\n\n[(2013.4.24)] 驻马店市第八中学校报工作实施细则\n\n[(2013.4.24)] 驻马店市第八中学校报编辑出版的相关规定", null, "联系方式\n\n电话:0396-2123817 地址:驻马店文明路与丰泽路交叉口向西50米路北\u0007\u0006\b。\n\n学生风采", null, "", null, "", null, "" ]
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https://intlpress.com/site/pub/pages/journals/items/cis/content/vols/0008/0001/a001/index.php
[ "# Communications in Information and Systems\n\n## Volume 8 (2008)\n\n### Computation of curvatures using conformal parameterization\n\nPages: 1 – 16\n\nDOI: https://dx.doi.org/10.4310/CIS.2008.v8.n1.a1\n\nJeffrey Kwan\n\nLok Ming Lui\n\nYalin Wang\n\nShing-Tung Yau\n\n#### Abstract\n\nCurvatures on the surface are important geometric invariants and are widely used in different area of research. Examples include feature recognition, segmentation, or shape analysis. Therefore, it is of interest to develop an effective algorithm to approximate the curvatures accurately. The classical methods to compute these quantities involve the estimation of the normal and some involve the computation of the second derivatives of the 3 coordinate functions under the param- eterization. Error is inevitably introduced because of the inaccurate approximation of the second derivatives and the normal. In this paper, we propose several novel methods to compute curva- tures on the surface using the conformal parameterization. With the conformal parameterization, the conformal factor function $\\lambda$ can be defined on the surface. Mean curvature (H) and Gaussian curvatures (K) can then be computed with the conformal Factor ($\\lambda$). It involves computing only the derivatives of the function $\\lambda$, instead of the 3 coordinate functions and the normal. We also introduce a technique to compute H from K and vice versa, using the parallel surface.\n\n#### Keywords\n\nMean curvature; Gaussian curvature; normal; conformal parameterization; conformal factor\n\nPublished 1 January 2008" ]
[ null ]
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https://topic.alibabacloud.com/a/download-and-decryption-of-source-code-article-1-of-2048-game-font-classtopic-s-color00c1degamesfont-with-more-than-font-classtopic-s-color00c1de10font-million-downloads_1_21_32599005.html
[ "Source: Internet\nAuthor: User\n\nA picture tells you how hot 2048 is.\n\nTragedy of small 3There will be one or two games in each phase of the phone, whether on a public car, on a bed, on a toilet or before going to bed or before dinner, you will always have the desire to open your cell phone. Most people are overwhelmed by Flappy bird and cannot take care of themselves. At this time of crisis, a digital puzzle game named the legend of little 3 appeared in our field of view. The game is simple, complex, simple, and ever-changing, it's hard to stop people! But the story is like this. Two developers of legend 3 spent nearly a year and a half before developing the core gameplay of this game, however, it was copied by \"1024\" only 21 days after the appstore was launched. In 2048, the 19-year-old Gabriel Cirulli used only one week to adapt the first two games, but he achieved the greatest success, while little 3 was not known; from its launch to the present, the downloads of such games, whether in the app store or android Market, have far exceeded 10 million. There are various online versions;\n\nCocosEditor open source Edition\nThe author took a night, finally completed the cocos2d-js open source version, encoding is easy, creative is not easy, and the line and cherish;\nThis version contains various popular online versions. It includes nearly 10 versions including the original version, dynasty version, Jin Yong version, constellation, and luxury cars. The code is open-source, and readers are expected to make various versions based on open source code for full-name entertainment;\nCocosEditor must be configured to run the demo. Other tools are not supported. Demo is cross-platform, can be transplanted to run android, ios, html5 web pages, code is based on javascript language, cocos2d-x game engine, CocosEditor mobile game development tools to complete.\n\nThis article consists of two parts: the first one is the original version, and the second one is the analysis of various versions. This code is for reference only. If you have better implementation methods, you can comment on it;\n\nReleased apk demo\nSeveral hours of development, one-day review and launch, which is the speed at which CocosEditor develops games\n\nGithub version management-https://github.com/makeapp/cocoseditor-2048\n\nIn Github, Daniel provides versions in various languages.\nIncluding (java, css, shell, python, objective-c and so on), readers can download the https://github.com/search on their own? Q = 2048 & ref = terraform\n\nFor different platforms:\n\nWindows\n\nHtml5 webpage\n\nAndroid platform (various theme versions)\n\nCode Analysis:\n\n1 initialization; enter the game, initialize 4*4 tables, and randomly generate two 2;\n\n# Two-dimensional array this. tables Table stores data cyclically\n\n# Four random numbers random1, random2, random11, and random22 can determine the xy positions of two 2;\n\n# In the newNumber method, a new number can be determined based on location I, j, and level num; the digital label cellLabel on the Background cell and cell is created; and the cellLabel is determined based on num; finally, associate the cell with a data. In particular, the number: num here is not the number above the genie but the level of the genie. For example, if number = 11, the number is 1024.\n\n`MainLayer. prototype. onEnter = function () {// version this. versionNum = indexVersions; this. indexVersion = VERSIONS [this. versionNum]; this. title. setString (this. indexVersion. name + \"target:\" + this. indexVersion. array [this. indexVersion. array. length-1] + \"\"); var random1 = getRandom (4); var random2 = getRandom (4); while (random1 = random2) {random2 = getRandom (4);} var random11 = getRandom (4); var random22 = getRandom (4); this. tables = new Array (4); for (var I = 0; I <4; I ++) {var sprites = new Array (4); for (var j = 0; j <4; j ++) {if (I = random1 & j = random11) {sprites [j] = this. newNumber (I, j, 1);} else if (I = random2 & j = random22) {sprites [j] = this. newNumber (I, j, 1);} else {sprites [j] = this. newNumber (I, j, 0) ;}} this. tables [I] = sprites;} this. totalScore = 0 ;}; MainLayer. prototype. newNumber = function (I, j, num) {var cell = cc. mySprite. create (this. rootNode, \"5.png\", this. getPosition (I, j), 1); var cellLabel = cc. mySprite. createLabel (cell, \"\"); if (num> 0) {cell. setColor (COLOR [num]); cellLabel. setVisible (true); cellLabel. setString (this. indexVersion. array [num]); cellLabel. setFontSize (this. indexVersion. labelFontSize);} else {cellLabel. setVisible (false);} cell. data = {col: I, row: j, numberLabel: cellLabel, number: num}; return cell ;};`\n\nTwo Algorithms in four directions. When you play a game, you can touch the four directions, and the table will merge the algorithms in four directions: leftCombineNumber, rightCombineNumber, downCombineNumber, and upCombineNumber. The algorithms of the four methods and functions are the same, I only analyze one leftCombineNumber;\n\nStep 1: overlap the same data:\n\n# J increases from left to right, And I increases from bottom to top; that is, the initial position is the lower left corner;\n\n# If the cell level is not empty, cell. data. number! = 0;\n\n# Var k = I + 1 from the right; loop traversal while (k <4) {k ++ };\n\n# If the traversal to the cell level is not an empty background if (nextCell. data. number! = 0) End of traversal k = 4; break ;;\n\n# And if the two units have the same level, if (cell. data. number = nextCell. data. number)\n\n# Level data number refresh changes\n\nCell. data. number + = 1;\n\nNextCell. data. number = 0;\n\nStep 2 fill in empty data;\n\n# Similarly, the first step is to traverse while (k <4) {k ++} cyclically if the background is empty if (cell. data. number = 0 };\n\n# If the traversal to the cell level is not an empty background if (nextCell. data. number! = 0), empty background to get the data of the cell, and the cell is set to empty background;\n\nCell. data. number = nextCell. data. number;\nNextCell. data. number = 0;\n\n`//direction leftMainLayer.prototype.leftCombineNumber = function () { for (var j = 0; j < 4; j++) { for (var i = 0; i < 4; i++) { var cell = this.tables[i][j]; if (cell.data.number != 0) { var k = i + 1; while (k < 4) { var nextCell = this.tables[k][j]; if (nextCell.data.number != 0) { if (cell.data.number == nextCell.data.number) { cell.data.number += 1; nextCell.data.number = 0; this.totalScore += SCORES[cell.data.number]; } k = 4; break; } k++; } } } } for (j = 0; j < 4; j++) { for (i = 0; i < 4; i++) { cell = this.tables[i][j]; if (cell.data.number == 0) { k = i + 1; while (k < 4) { nextCell = this.tables[k][j]; if (nextCell.data.number != 0) { cell.data.number = nextCell.data.number; nextCell.data.number = 0; k = 4; } k++; } } } } this.refreshNumber();};//direction rightMainLayer.prototype.rightCombineNumber = function () { for (var j = 0; j < 4; j++) { for (var i = 3; i >= 0; i--) { var cell = this.tables[i][j]; if (cell.data.number != 0) { var k = i - 1; while (k >= 0) { var nextCell = this.tables[k][j]; if (nextCell.data.number != 0) { if (cell.data.number == nextCell.data.number) { cell.data.number += 1; nextCell.data.number = 0; this.totalScore += SCORES[cell.data.number]; } k = -1; break; } k--; } } } } for (j = 0; j < 4; j++) { for (i = 3; i >= 0; i--) { cell = this.tables[i][j]; if (cell.data.number == 0) { k = i - 1; while (k >= 0) { nextCell = this.tables[k][j]; if (nextCell.data.number != 0) { cell.data.number = nextCell.data.number; nextCell.data.number = 0; k = -1; } k--; } } } } this.refreshNumber();};MainLayer.prototype.downCombineNumber = function () { for (var i = 0; i < 4; i++) { for (var j = 0; j < 4; j++) { var cell = this.tables[i][j]; if (cell.data.number != 0) { var k = j + 1; while (k < 4) { var nextCell = this.tables[i][k]; if (nextCell.data.number != 0) { if (cell.data.number == nextCell.data.number) { cell.data.number += 1; nextCell.data.number = 0; this.totalScore += SCORES[cell.data.number]; } k = 4; break; } k++; } } } } for (i = 0; i < 4; i++) { for (j = 0; j < 4; j++) { cell = this.tables[i][j]; if (cell.data.number == 0) { k = j + 1; while (k < 4) { nextCell = this.tables[i][k]; if (nextCell.data.number != 0) { cell.data.number = nextCell.data.number; nextCell.data.number = 0; k = 4; } k++; } } } } this.refreshNumber();};//touch upMainLayer.prototype.upCombineNumber = function () { for (var i = 0; i < 4; i++) { for (var j = 3; j >= 0; j--) { var cell = this.tables[i][j]; if (cell.data.number != 0) { var k = j - 1; while (k >= 0) { var nextCell = this.tables[i][k]; if (nextCell.data.number != 0) { if (cell.data.number == nextCell.data.number) { cell.data.number += 1; nextCell.data.number = 0; this.totalScore += SCORES[cell.data.number]; } k = -1; break; } k--; } } } } for (i = 0; i < 4; i++) { for (j = 3; j >= 0; j--) { cell = this.tables[i][j]; if (cell.data.number == 0) { k = j - 1; while (k >= 0) { nextCell = this.tables[i][k]; if (nextCell.data.number != 0) { cell.data.number = nextCell.data.number; nextCell.data.number = 0; k = -1; } k--; } } } } this.refreshNumber();};`\n\n3. Refresh the data and color;\n\nThe above algorithm is complete, but the data in the data of the genie has changed, but there is no visual change, so you need to refresh the data and color\n\n# Create an empty background array emptyCellList;\n\n# This. tables\n\n# Obtain the text label and level cellNumber of the cell.\n\n# If it is not an empty background cellNumber! = 0. The label displays and sets the text content and size. If it is detected to be the highest level, the game ends successfully.\n\n# If the background is empty, label hides emptyCellList and adds this element emptyCellList. push (cell );;\n\n# After obtaining an emptyCellList, if the size of the array is found to be empty, a number 2 cannot be generated, and the game is over;\n\n# If the array size is not empty, set randomCell to a random location, set the data level to 0, number to 2, and play the scaling animation runAction;\n\n`MainLayer. prototype. refreshNumber = function () {var emptyCellList = []; for (var I = 0; I <4; I ++) {var numbers = \"\"; for (var j = 0; j <4; j ++) {var cell = this. tables [I] [j]; var label = cell. data. numberLabel; var cellNumber = cell. data. number; if (cellNumber! = 0) {cell. setColor (COLOR [cellNumber]); label. setString (this. indexVersion. array [cellNumber] + \"\"); label. setFontSize (this. indexVersion. labelFontSize); label. setVisible (true); if (cellNumber = (this. indexVersion. array. length-1) {// check success var toast = cc. toast. create (this. rootNode, \"successfully arrived:\" + this. indexVersion. array [cellNumber], 2); toast. setColor (cc. c3b (255, 0, 0); this. rootNode. schedul EOnce (function () {cc. builderReader. runScene (\"\", \"MainLayer\") ;}, 2) }} else {cell. setColor (COLOR [cellNumber]); label. setVisible (false); emptyCellList. push (cell);} numbers + = \"\" + cellNumber;} cc. log (\"numbers =\" + numbers);} // score this. scoreLabel. setString (\"score:\" + this. totalScore); if (emptyCellList. length <1) {// check fail var toast = cc. toast. create (this. rootNode, \"failed! \", 2); toast. setColor (cc. c3b (255, 0, 0); this. rootNode. scheduleOnce (function () {cc. builderReader. runScene (\"\", \"MainLayer\") ;}, 2)} else {// create random cell var randomCell = emptyCellList [getRandom (emptyCellList. length)]; randomCell. data. number = 1; randomCell. data. numberLabel. setVisible (true); randomCell. data. numberLabel. setString (VERSIONS [this. versionNum]. array + \"\"); randomCell. data. numberLabel. setFontSize (this. indexVersion. labelFontSize); randomCell. setColor (COLOR ); randomCell. runAction (cc. sequence. create (cc. scaleTo. create (0, 0.8), cc. scaleTo. create (0.5, 1 )));}};`\n\n4. Touch to detect two touch points this. pEnded this. pBegan determine the direction based on x y, and then determine the left and right and top and bottom based on the distance;\n\n`MainLayer.prototype.onTouchesEnded = function (touches, event) { this.pEnded = touches.getLocation(); if (this.pBegan) { if (this.pEnded.x - this.pBegan.x > 50) { this.rightCombineNumber(); } else if (this.pEnded.x - this.pBegan.x < -50) { this.leftCombineNumber(); } else if (this.pEnded.y - this.pBegan.y > 50) { this.upCombineNumber(); } else if (this.pEnded.y - this.pBegan.y < -50) { this.downCombineNumber(); } }};`\n\nThe idea is clear and simple, but the game is simple and not simple;\n\nCocos2d-x cross-platform game engine\nCocos2d-x is a world-renowned game engine, engine in the world has a large number of developers, covering all well-known game developers at home and abroad. At present, Cocos2d-x engine has been achieved across ios, Android, Bada, MeeGo, BlackBerry, Marmalade, Windows, Linux and other platforms. Write once, run everywhere, divided into two versions of cocos2d-c ++ and cocos2d-html5 this article uses the latter; cocos2d-x Official Website: http://cocos2d-x.org/cocos2d-x data download http://cocos2d-x.org/download\n\nCocosEditor development tool:\n\nCocosEditor, it is the development of cross-platform mobile game tools, run Windows/mac system, javascript scripting language, based on cocos2d-x cross-platform game engine, set code editing, Scene Design, animation production, font design, as well as particle, physical system, MAP and so on, and easy debugging, and real-time simulation;\n\nCocosEditor blog: http://blog.makeapp.co /;\n\n2048 series of articles\n\n2048 source code decryption and download (first analysis of the original version)\n\nFlappy bird game source code exposure and download follow-up-porting to android real machine\n\nFlappy bird game source code exposure and download follow-up-porting to html5 Web Browser\n\nSource code download, analysis, and cross-platform migration for PopStar games-Article 1 (UI)\n\nDownload, analyze, and port the game source code across platforms-Article 2 (algorithm)\n\nDownload, analyze, and port the game source code across platforms-Article 3 (score)\n\nDownload, analyze, and port the game source code across platforms-Article 4 (checkpoints)\n\nAuthor's note:\n\nFor more information, please go to the official blog. The latest blog and code will be launched on the official blog. Please stay tuned for more CocosEditor game source code coming soon;\n\nContact me: [email protected] (Mailbox) QQ group: 232361142\n\nAppendix:\n\nSort out various versions of 2048 online games and get up;\n\n1. Original Version 2048\nHttp://gabrielecirulli.github.io/2048/\n2. 2048 advanced edition (features of multiplication and continuous playback)\n3. 2048 Chinese Version 1: A, B, and C\nHttp://tiansh.github.io/2048/zhong/\n4. 2048 Chinese Version 2: Shang Zhou Qin and Han Dynasties\nHttp://oprilzeng.github.io/2048/\n5. 2048 meow version: weak color and careful\nHttp://hczhcz.github.io/2048/20mu/\n6. 2048 mourning version: 8*8\nHttp://cyberzhg.github.io/2048/\n7. 2048flappy\nHttp://hczhcz.github.io/Flappy-2048/\n8. 2048 hexagonal Edition\nHttp://baiqiang.github.io/2048-hexagon/\n9. 2048cross\nHttp://baiqiang.github.io/2048-cross/\nVersion 10 and 2048double\nHttp://baiqiang.github.io/2048-double/\n11. 2048 philosophy Edition\nHttp://learn.tsinghua.edu.cn: 8080/2013310744/philosopher2048/\n\n12. 2048 one-step Installation\nHttp://jennypeng.me/2048/\n13. 2048 Fibonacci Series\nHttp://mike199515.free3v.com/1597/2.htm\n14. 2048 dual combat Edition\nHttp://emils.github.io/2048-multiplayer/\n15. 2048 changed to Version 2\nHttps://www.prism.gatech.edu /~ Hli362/\n2048 line edition\nHttp://tiansh.github.io/2048/\nHttp://baiqiang.github.io/2048-3d/\n18. A collection of 2048:\nHttp://get2048.com/\n\nRelated Keywords:\nRelated Article\n\nThe content source of this page is from Internet, which doesn't represent Alibaba Cloud's opinion; products and services mentioned on that page don't have any relationship with Alibaba Cloud. If the content of the page makes you feel confusing, please write us an email, we will handle the problem within 5 days after receiving your email.\n\nIf you find any instances of plagiarism from the community, please send an email to: [email protected] and provide relevant evidence. A staff member will contact you within 5 working days.\n\n## A Free Trial That Lets You Build Big!\n\nStart building with 50+ products and up to 12 months usage for Elastic Compute Service\n\n• #### Sales Support\n\n1 on 1 presale consultation\n\n• #### After-Sales Support\n\n24/7 Technical Support 6 Free Tickets per Quarter Faster Response\n\n• Alibaba Cloud offers highly flexible support services tailored to meet your exact needs." ]
[ null ]
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http://lemonlilyfestival.com/fun-3rd-grade-math-worksheets/
[ "", null, "Printables\n\nFun 3rd Grade Math Worksheets\n\n1000 images about worksheets for homework on pinterest 3rd grade math and times tables. Math 3rd grade and worksheets on pinterest. Fun multiplication worksheets to 10x10 sheet 2. Math puzzle worksheets 3rd grade fun newtons crosses 3. Simple worksheets and division on pinterest math coloring pages 3rd grade color by number worksheet education com.", null, "1000 images about worksheets for homework on pinterest 3rd grade math and times tables", null, "Math 3rd grade and worksheets on pinterest", null, "Fun multiplication worksheets to 10x10 sheet 2", null, "Math puzzle worksheets 3rd grade fun newtons crosses 3", null, "Simple worksheets and division on pinterest math coloring pages 3rd grade color by number worksheet education com", null, "Fun multiplication worksheets to 10x10 5x5 sheet 4 answers", null, "The ojays products and worksheets on pinterest fun multiplication fourth grade multiplying by 8", null, "Fun third grade math worksheets coffemix printable 3rd worksheets", null, "Fun multiplication worksheets to 10x10 free sheets 5x5 1", null, "Free printable coloring math worksheets for 3rd grade pages graders 1st students", null, "Easy to color 3rd grade math printable worksheets free fall rounding hundreds woo jr kids activities", null, "Fun 3rd grade math worksheets syndeomedia worksheet pichaglobal", null, "Fun third grade math worksheets coffemix activities for 3rd frankie s bingo fun", null, "1000 ideas about 3rd grade math worksheets on pinterest 2nd coloring pages color by number division worksheet education com", null, "Football fun 2nd grade math worksheets jumpstart free worksheet", null, "Math 3rd grade worksheets and on pinterest fun multiplication worksheet to 10x10 sheets", null, "More numbers make it fun addition printable for 4th grade free worksheet 3rd grade", null, "Fun multiplication worksheets to 10x10 sheet 7", null, "Fun 3rd grade math worksheets syndeomedia division for 4th graders thousands of worksheet math", null, "Worksheets fun math for 3rd grade laurenpsyk free printable", null, "Add total 1st grade math worksheets jumpstart total", null, "3rd grade math worksheets penny candy puzzles polygons worksheets", null, "Money math and activities on pinterest", null, "Math mystery picture worksheets addition worksheet picture", null, "1000 images about math worksheets on pinterest place value follow the leader and number worksheets", null, "Related Posts\n\nMath Printable Worksheets 3rd Grade", null, "" ]
[ null, "https://s-media-cache-ak0.pinimg.com/originals/f5/6d/65/f56d6585e18a81ba2f5b85aae7b2f737.gif", null, "https://s-media-cache-ak0.pinimg.com/originals/f5/6d/65/f56d6585e18a81ba2f5b85aae7b2f737.gif", null, "https://s-media-cache-ak0.pinimg.com/236x/14/69/26/1469265468fc07363a857f2c05dba927.jpg", null, "http://www.math-salamanders.com/images/math-worksheets-printable-fun-multiplication-to-10x10-2.gif", null, "http://www.math-salamanders.com/image-files/fun-math-worksheets-newtons-crosses-puzzle-3.gif", null, "https://s-media-cache-ak0.pinimg.com/236x/5b/ec/f2/5becf225055b28c20bfe523fb4685a74.jpg", null, "http://www.math-salamanders.com/images/multiplication-fun-worksheets-multiplication-to-5x5-4ans.gif", null, "https://s-media-cache-ak0.pinimg.com/236x/0c/a6/4d/0ca64d6809ebd41755ac69de93a84114.jpg", null, "http://www.woojr.com/wp-content/uploads/2009/08/xfall-math-addition-workshee.gif.pagespeed.ic.HlUFc5D53X.png", null, "http://www.math-salamanders.com/images/free-multiplication-sheets-fun-multiplication-to-5x5-1.gif", null, "https://s-media-cache-ak0.pinimg.com/564x/fe/b6/bb/feb6bb48d1c130fbab620c846669e906.jpg", null, "http://www.pipress.net/wp-content/uploads/2016/07/free-fall-math-worksheets-rounding-hundreds-woo-jr-kids-activities.gif", null, "http://ceanntrahomes.com/jojo/Math%20Fun%20Worksheet_4.jpg", null, "https://s-media-cache-ak0.pinimg.com/originals/60/e0/2c/60e02c06b1090700f812ce6afe5d16cd.jpg", null, "https://s-media-cache-ak0.pinimg.com/736x/5b/ec/f2/5becf225055b28c20bfe523fb4685a74.jpg", null, "http://m.jumpstart.com/JumpstartNew/uploadedFiles/sne/small-screenshots/football-fun.jpg", null, "https://s-media-cache-ak0.pinimg.com/236x/8b/cd/16/8bcd16040aaf17d2071750631a39ee0c.jpg", null, "http://m.mathblaster.com/Mathblaster/uploaded-files/small-screenshots/more-numbers-make-it-fun.jpg", null, "http://www.math-salamanders.com/images/printable-multiplication-sheets-fun-multiplication-to-10x10-7.gif", null, "http://www.damprat.com/i/2016/12/grade-math-free-worksheets-kids-maths-worksheet-wednesday-popsicle-paging.jpg", null, "http://ikidspad.com/math/mathGames/images/Math%20puzzle%20worksheets%20273.png", null, "http://m.jumpstart.com/JumpstartNew/uploadedFiles/sne/small-screenshots/add-total.jpg", null, "https://candymathgamesworksheets.files.wordpress.com/2011/04/math-word-search-puzzles.png", null, "https://s-media-cache-ak0.pinimg.com/236x/c5/d5/6b/c5d56beb239bc35668ff506980dadd9d.jpg", null, "https://www.superteacherworksheets.com/thumbnails/math-mystery-picture/addition-math-mystery-picture-worksheet.jpg", null, "https://s-media-cache-ak0.pinimg.com/originals/c7/2a/95/c72a9506773bfa90f67ec33803b6d0b2.jpg", null, "https://s-media-cache-ak0.pinimg.com/564x/58/e6/33/58e6330ddbf0de792f49cc42d46acd71.jpg", null, "http://www.ziggityzoom.com/sites/default/files/styles/activity_full/public/Pattern_Sequence1.gif", null ]
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https://ecstasyshots.wordpress.com/category/physics/electrodynamics/
[ "# Jackson’s Laplacian in spherical Coordinates\n\nIf you took a look at one of the previous posts on how to remember the Laplacian in different forms by using a metric,  you will notice that the form of  the Laplacian that we get is:", null, "$\\nabla^2 \\psi = \\frac{1}{r^2} \\frac{\\partial}{\\partial r} \\left( r^2 \\frac{\\partial \\psi}{\\partial r} \\right) + \\frac{1}{r^2 \\sin(\\theta)} \\frac{\\partial}{\\partial \\theta} \\left( sin(\\theta) \\frac{\\partial \\psi}{\\partial \\theta} \\right) + \\frac{1}{r^2 \\sin^2(\\theta)} \\frac{\\partial^2 \\psi}{\\partial \\phi^2}$\n\nBut in Jackson’s Classical Electrodynamics, III edition he notes the following:", null, "This is an interesting form of the Laplacian that perhaps not everyone has encountered. This can obtained from the known form by making the substitution", null, "$u = r \\psi$ and simplifying. The steps to which have been outlined below:", null, "", null, "# Prof.Ghrist at his best!", null, "To understand why this is true, we must start with the Fundamental Theorem of Vector calculus. If", null, "$F$ is a conservative field ( i.e", null, "$F = \\nabla \\phi$ ), then", null, "$\\int\\limits_{A}^{B} F.dr = \\int\\limits_{A}^{B} \\nabla\\phi .dr = \\phi_{A} - \\phi_{B}$\n\nWhat this means is that the value is dependent only on the initial and final positions. The path that you take to get from A to B is not important.", null, "Now if the path of integration is a closed loop, then points A and B are the same, and therefore:", null, "$\\int\\limits_{A}^{A} F.dr = \\int\\limits_{A}^{A} \\nabla\\phi .dr = \\phi_{1} - \\phi_{1} = 0$\n\nNow that we are clear about this, according to Stokes theorem the same integral for a closed region can be represented in another form:", null, "$\\int_{C} F.dr = \\int\\int_{A} (\\nabla X F) .\\vec{n} dA = 0$\n\nFrom this we get that Curl =", null, "$\\nabla X F = 0$ for a conservative field (i.e", null, "$F = \\nabla \\phi$). Therefore when a conservative field is operated on by a curl operator (", null, "$\\nabla X$), it yields 0.\n\nBravo Prof.Ghrist! Beautifully said 😀\n\n# Solving the Laplacian in Spherical Coordinates (#1)\n\nIn this post, let’s derive a general solution for the Laplacian in Spherical Coordinates. In future posts, we shall look at the application of this equation in the context of Fluids and Quantum Mechanics.", null, "", null, "$x = rsin\\theta cos\\phi$", null, "$y = rsin\\theta cos\\phi$", null, "$z = rcos\\theta$\n\nwhere", null, "$0 \\leq r < \\infty$", null, "$0 \\leq \\theta \\leq \\pi$", null, "$0 \\leq \\phi < 2\\pi$\n\nThe Laplacian in Spherical coordinates in its ultimate glory is written as follows:", null, "$\\nabla ^{2}f ={\\frac {1}{r^{2}}}{\\frac {\\partial }{\\partial r}}\\left(r^{2}{\\frac {\\partial f}{\\partial r}}\\right)+{\\frac {1}{r^{2}\\sin \\theta }}{\\frac {\\partial }{\\partial \\theta }}\\left(\\sin \\theta {\\frac {\\partial f}{\\partial \\theta }}\\right)+{\\frac {1}{r^{2}\\sin ^{2}\\theta }}{\\frac {\\partial ^{2}f}{\\partial \\phi ^{2}}} = 0$\n\nTo solve it we use the method of separation of variables.", null, "$f = R(r)\\Theta(\\theta)\\Phi(\\phi)$\n\nPlugging in the value of", null, "$f$ into the Laplacian, we get that :", null, "$\\frac{\\Theta \\Phi}{r^2} \\frac{d}{dr} \\left( r^2\\frac{dR}{dr} \\right) + \\frac{R \\Phi}{r^2 sin \\theta} \\frac{d}{d \\theta} \\left( sin \\theta \\frac{d\\Theta}{d\\theta} \\right) + \\frac{\\Theta R}{r^2 sin^2 \\theta} \\frac{d^2 \\Phi}{d\\phi^2} = 0$\n\nDividing throughout by", null, "$R\\Theta\\Phi$ and multiplying throughout by", null, "$r^2$, further simplifies into:", null, "$\\underbrace{ \\frac{1}{R} \\frac{d}{dr} \\left( r^2\\frac{dR}{dr} \\right)}_{h(r)} + \\underbrace{\\frac{1}{\\Theta sin \\theta} \\frac{d}{d \\theta} \\left( sin \\theta \\frac{d\\Theta}{d\\theta} \\right) + \\frac{1}{\\Phi sin^2 \\theta} \\frac{d^2 \\Phi}{d\\phi^2}}_{g(\\theta,\\phi)} = 0$\n\nIt can be observed that the first expression in the differential equation is merely a function of", null, "$r$ and the remaining a function of", null, "$\\theta$ and", null, "$\\phi$ only. Therefore, we equate the first expression to be", null, "$\\lambda = l(l+1)$ and the second to be", null, "$-\\lambda = -l(l+1)$. The reason for choosing the peculiar value of", null, "$l(l+1)$ is explained in another post.", null, "$\\underbrace{ \\frac{1}{R} \\frac{d}{dr} \\left( r^2\\frac{dR}{dr} \\right)}_{l(l+1)} + \\underbrace{\\frac{1}{\\Theta sin \\theta} \\frac{d}{d \\theta} \\left( sin \\theta \\frac{d\\Theta}{d\\theta} \\right) + \\frac{1}{\\Phi sin^2 \\theta} \\frac{d^2 \\Phi}{d\\phi^2}}_{-l(l+1)} = 0$ (1)\n\nThe first expression in (1) the Euler-Cauchy equation in", null, "$r$.", null, "$\\frac{d}{dr} \\left( r^2\\frac{dR}{dr} \\right) = l(l+1)R$\n\nThe general solution of this has been in discussed in a previous post and it can be written as:", null, "$R(r) = C_1 r^l + \\frac{C_2}{r^{l+1}}$\n\nThe second expression in (1) takes the form as follows:", null, "$\\frac{sin \\theta}{\\Theta} \\frac{d}{d \\theta} \\left( sin \\theta \\frac{d\\Theta}{dr} \\right)+ l(l+1)sin^2 \\theta + \\frac{1}{\\Phi} \\frac{d^2 \\Phi}{d\\phi^2} = 0$\n\nThe following observation can be made similar to the previous analysis", null, "$\\underbrace{\\frac{sin \\theta}{\\Theta} \\frac{d}{d \\theta} \\left( sin \\theta \\frac{d\\Theta}{dr} \\right)+ l(l+1)sin^2 \\theta }_{m^2} + \\underbrace{\\frac{1}{\\Phi} \\frac{d^2 \\Phi}{d\\phi^2}}_{-m^2} = 0$ (2)\n\nThe first expression in the above equation (2) is the Associated Legendre Differential equation.", null, "$\\frac{sin \\theta}{\\Theta} \\frac{d}{d \\theta} \\left( sin \\theta \\frac{d\\Theta}{dr} \\right)+ l(l+1)sin^2 \\theta = m^2$", null, "$sin \\theta \\frac{d}{d \\theta} \\left( sin \\theta \\frac{d\\Theta}{dr} \\right)+ \\Theta \\left( l(l+1)sin^2 \\theta - m^2 \\right) = 0$\n\nThe general solution to this differential equation can be given as:", null, "$\\Theta(\\theta) = C_3 P_l^m(cos\\theta) + C_4 Q_l^m(cos\\theta)$\n\nThe solution to the second term in the equation (2) is a trivial one:", null, "$\\frac{d^2 \\Phi}{d\\phi^2} = m^2 \\Phi$", null, "$\\Phi(\\phi) = C_5 e^{im\\phi} + C_6 e^{-im\\phi}$\n\nTherefore the general solution to the Laplacian in Spherical coordinates is given by:", null, "$R\\Theta\\Phi = \\left(C_1 r^l + \\frac{C_2}{r^{l+1}} \\right) \\left(C_3 P_l^m(cos\\theta) + C_4 Q_l^m(cos\\theta \\right) \\left(C_5 e^{im\\phi} + C_6 e^{-im\\phi}\\right)$\n\n# Mars: Red Planet, Blue sunset?\n\nMars has always been an interesting planet to us earthlings. The possibility of life, rovers leaving no stone unturned(literally), it’s demanding reddish appearance and now those breathtaking sunsets.Mesmerizing isn’t it ? But,\n\n## Why are martian sunsets blue?\n\nHere on earth, sunsets are bright with Yellow, Orange and Red colors dazzling in the sky. During sunsets, the light from the sun has to travel a longer distance in our atmosphere to reach the earth.\n\nConsequently, all the blue and violet light is scattered( thrown in various directions) by the particles in our atmosphere leaving behind only shades of yellow, orange and red, which is what you see. This phenomenon is known as Rayleigh scattering.\n\nOn mars, the reverse effect occurs. The martian dust is smaller and more abundant than on earth and it incidentally happens to be just the right size that it absorbs the blue light whilst scattering the red ones across the sky. This makes martian sunsets blue :).\n\nStay tuned, there is more space stuff coming your way." ]
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https://www.indiabix.com/non-verbal-reasoning/analogy/004003
[ "# Non Verbal Reasoning - Analogy\n\n### Exercise :: Analogy - Section 2\n\nEach of the following questions consists of two sets of figures. Figures A, B, C and D constitute the Problem Set while figures 1, 2, 3, 4 and 5 constitute the Answer Set. There is a definite relationship between figures A and B. Establish a similar relationship between figures C and D by selecting a suitable figure from the Answer Set that would replace the question mark (?) in fig. (D).\n\n11.\n\nSelect a suitable figure from the Answer Figures that would replace the question mark (?).", null, "(A)     (B)      (C)     (D)                  (1)      (2)      (3)      (4)      (5)\n\n A. 1 B. 2 C. 3 D. 4 E. 5\n\nExplanation:\n\nThe complete figure rotates through 180o and the element that reaches the RHS position rotates further by 90oCW.\n\n12.\n\nSelect a suitable figure from the Answer Figures that would replace the question mark (?).", null, "(A)     (B)      (C)     (D)                  (1)      (2)      (3)      (4)      (5)\n\n A. 1 B. 2 C. 3 D. 4 E. 5\n\nExplanation:\n\nThe middle and the inner elements get enlarged to become the outer and the middle elements respectively. The outer element gets reduced in size and becomes the inner element.\n\n13.\n\nSelect a suitable figure from the Answer Figures that would replace the question mark (?).", null, "(A)     (B)      (C)     (D)                  (1)      (2)      (3)      (4)      (5)\n\n A. 1 B. 2 C. 3 D. 4 E. 5\n\nExplanation:\n\nThe number of arcs in the central element increases by one; the number of small ellipses increases by one and these ellipses shift to the inner side of the central element.\n\n14.\n\nSelect a suitable figure from the Answer Figures that would replace the question mark (?).", null, "(A)     (B)      (C)     (D)                  (1)      (2)      (3)      (4)      (5)\n\n A. 1 B. 2 C. 3 D. 4 E. 5\n\nExplanation:\n\nThe two elements at the ends of the line segment, move to the centre of the line segment.\n\n15.\n\nSelect a suitable figure from the Answer Figures that would replace the question mark (?).", null, "(A)     (B)      (C)     (D)                  (1)      (2)      (3)      (4)      (5)\n\n A. 1 B. 2 C. 3 D. 4 E. 5" ]
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https://www.netexplanations.com/30-2-1-2020-class-10-math-standard-question-paper-solution/
[ "# 30 / 2 / 1 2020 Class 10 Math Standard Question Paper Solution\n\n## 30 / 2 / 1 2020 Class 10 Math Standard Question Paper Solution", null, "Section – A\n\nQuestion numbers 1 to 10 are multiple choice questions of 1 mark each. Select the correct option.\n\n(1) The sum of exponents of prime factors in the prime-factorisation of 196 is\n\n(a) 3\n\n(b) 4\n\n(c) 5\n\n(d) 2\n\nSolution: 4\n\n(2) Euclid’s division Lemma states that for two positive integers a and b, there exists unique integer q and r satisfying a = bq + r, and\n\n(a) 0 < r < b\n\n(b) 0 < r < b\n\n(c) 0 < r < b\n\n(d) 0 < r < b\n\nSolution: 0 ≤ r < b\n\n(3) The zeroes of the polynomial x 2 – 3x – m (m + 3) are\n\n(a) m, m + 3\n\n(b) –m, m + 3\n\n(c) m, –(m + 3)\n\n(d) –m, –(m + 3)\n\nSolution: –m, m + 3\n\n(4) The value of k for which the system of linear equations x + 2y = 3, 5x + ky + 7 = 0 is inconsistent is\n\n(a) – 14/ 3\n\n(b) 2/ 5\n\n(c) 5\n\n(d) 10\n\nSolution: 10\n\n(5) The roots of the quadratic equation x 2 – 0.04 = 0 are\n\n(a) + 0.2\n\n(b) + 0.02\n\n(c) 0.4\n\n(d) 2\n\nSolution: ± 0.2\n\n(6) The common difference of the A.P. 1/ p , 1 – p/ p , 1 – 2p/ p , …… is\n\n(a) 1\n\n(b) 1/ p\n\n(c) –1\n\n(d) – 1/ p\n\nSolution: –1\n\n(7) The nth term of the A.P. a, 3a, 5a, …… is\n\n(a) na\n\n(b) (2n – 1) a\n\n(c) (2n + 1) a\n\n(d) 2na\n\nSolution: (2n – 1)a\n\n(8) The point P on x-axis equidistant from the points A(–1, 0) and B(5, 0) is\n\n(a) (2, 0)\n\n(b) (0, 2)\n\n(c) (3, 0)\n\n(d) (2, 2)\n\nSolution: (2, 0)\n\n(9) The co-ordinates of the point which is reflection of point (–3, 5) in x-axis are\n\n(a) (3, 5)\n\n(b) (3, –5)\n\n(c) (–3, –5)\n\n(d) (–3, 5)\n\nSolution: (–3, –5)\n\n(10) If the point P (6, 2) divides the line segment joining A(6, 5) and B(4, y) in the ratio 3 : 1, then the value of y is\n\n(a) 4\n\n(b) 3\n\n(c) 2\n\n(d) 1\n\nSolution: 1 mark be awarded to everyone\n\n(11) In Q. Nos. 11 to 15, fill in the blanks. Each question is of 1 mark. In fig. 1, MN || BC and AM : MB = 1 : 2, then Are(D AMN)/ar(D ABC) = _________.", null, "Solution: 1/9\n\n(12) In given Fig. 2, the length PB = _________ cm.", null, "Solution: 4\n\n(13) In  D ABC, AB = 6 √  3 cm, AC = 12 cm and BC = 6 cm, then <B = ……..\n\nSolution: 90°\n\nOR\n\nTwo triangles are similar if their corresponding sides are ……..\n\nSolution: proportional\n\n(14) The value of (tan 1º tan 2º …… tan 89º) is equal to _________.\n\nSolution: 1\n\n(15) In fig. 3, the angles of depressions from the observing positions O1 and O2 respectively of the object A are _________, _________.", null, "Solution: 30°, 45°\n\nQ.Nos. 16 to 20 are short answer type questions of 1 mark each.\n\n(16) If sin A + sin2 A = 1, then find the value of the expression (cos2 A + cos4 A).\n\nSolution: sin A =1- sin2 A\n\nSin A = cos2 A\n\nCos2 A + cos4 A = sin A + Sin2 A = 1\n\n(17) In Fig. 4 is a sector of circle of radius 10.5 cm. Find the perimeter of the sector. (Take π = 22/7)", null, "Solution: Perimeter = 2r + πr θ/ 1800\n\n= 2 x 10. 5 + 22 / 7 x 10.5 x 600/ 1800\n\n= 21 + 11 = 32 cm\n\n(18) If a number x is chosen at random from the numbers –3, –2, –1, 0, 1, 2, 3, then find the probability of x2 < 4.\n\nSolution: Number of Favourable outcomes = 3 i.e., { – 1, 0, 1} ∴ p(x2 <4) = 3/7\n\nOR\n\nWhat is the probability that a randomly taken leap year has 52 Sundays?\n\nSolution: P(52 Sundays) = 5/7\n\n(19) Find the class-marks of the classes 10-25 and 35-55.\n\nSolution:\n\nClass Marks 10 + 25/2 = 17.5; 35 + 55/2 = 45\n\n(20) A die is thrown once. What is the probability of getting a prime number.\n\nSolution: Number of prime numbers = 3 i.e. ; {2, 3, 5}\n\nP(Prime Number) = 3/6 or 1/2\n\nSECTION – B\n\nQ.Nos. 21 to 26 carry 2 marks each\n\n(21) A teacher asked 10 of his students to write a polynomial in one variable on a paper and then to handover the paper. The following were the answers given by the students:\n\n2x + 3, 3x2 + 7x + 2, 4x3 + 3x2 + 2, x3 + √3x + √7, 7x + 7 , 5x3 – 7x + 2,\n\n2x2 + 3 – 5/ x , 5x – 1/ 2 , ax3 + bx2 + cx + d, x + 1/ x .\n\n(i) How many of the above ten, are not polynomials?\n\n(ii) How many of the above ten, are quadratic polynomials?\n\nSolution:\n\n(i) 3\n\n(ii) 1\n\n(22) In Fig. 5, ABC and DBC are two triangles on the same base BC. If AD intersects BC at O, show that\n\nar (△ ABC)/ ar (△ DBC) = AO/DO", null, "Solution:", null, "Draw AX ⊥ BC, DY ⊥ BC\n\nΔAOX ~ ΔDOY\n\nAX/DY = AO/DO …… (i)\n\nar (Δ ABC)/ar (Δ DBC) = 1/2 X BC X AX/ 1/2 X BC X DY\n\nAX/DY = AO/DO (From) (1)\n\nOR\n\nIn Fig. 6, if AD BC, then prove that AB2 + CD2 = BD2 + AC2 .", null, "Solution: In rt ΔABD\n\nAB2 + CD2 = BD2 + AC2\n\nAB2 = BD2 + AD2 … (i)\n\nCD2 = AC2 – AD2 … (ii)\n\n(23) Prove that 1 + cot α/ 1 + cos ec α = cos ec α\n\nSolution: L.H.S = 1 + cos ec2 α 1/ 1+ cos ec α\n\n= 1 +  (cos ec α -1) (co sec α + 1)/ co sec α + f\n\n= cosec α = R.H.S\n\nOR\n\nShow that tan4 θ + tan2 θ = sec4 θ – sec2 θ\n\nSolution: L.H.S = tan4 θ + tan2 θ\n\n= tan2 θ (tan2 θ + 1)\n\n= (sec2 θ – 1) (sec2 θ) = sec4 θ – sec2 θ = R.H.S\n\n(24) The volume of a right circular cylinder with its height equal to the radius is  25 1/ 7 cm3 . Find the height of the cylinder. (Use π = 22/7)\n\nSolution: Let height and radius of cylinder = x cm\n\nV = 176/ 7 cm3\n\n22/7 x x2 X x = 176/7\n\nX3 = 8 ⇒ x = 2\n\n∴ height of cylinder = 2 cm\n\n(25) A child has a die whose six faces show the letters as shown below:\n\n A B C D E A\n\nThe die is thrown once. What is the probability of getting (i) A, (ii) D?\n\nSolution: (i) P(A) = 2/6 or 1/3\n\n(ii) P(D) = 1/6\n\n(26) Compute the mode for the following frequency distribution:\n\n Size of items (in cm) 0-4 4-8 8-12 12-16 16-20 20-24 24-28 Frequency 5 7 9 17 12 10 6\n\nSolution: l = 12 f0 = 9 f1 = 17 f2 = 12 h = 4\n\nMode = 12 + 17 – 9/ 34 – 9 – 12 x 4 = 14.46 cm (Approx)\n\nSECTION – C\n\nQuestion numbers 27 to 34 carry 3 marks each.\n\n(27) If 2x + y = 23 and 4x – y = 19, find the value of (5y – 2x) and (y/x – 2)\n\nSolution: 2x + y = 23 , 4x – y = 19\n\nSolving, we get x = 7, y = 9\n\n5y – 2x = 31, y/x – 2 = -5/7\n\nOR\n\nSolve for x: 1/ x + 4 – 1/ x + 7= 11/30, x # – 4, 7\n\nSolution: 1/x + 4 – 1/x – 7 = 11/30 ⇒ -11/(x + 4) (x – 7) = 11/30\n\n⇒ x2 – 3x + 2 = 0\n\n⇒ (x – 2) (x – 1) = 0\n\n⇒ x =2, 1\n\nThe Following solution should also be accepted\n\n1/x + 4 – 1/x + 7 = 11/30 ⇒ x + 7 – x – 4/ (x + 4) (x – 7) = 11/30\n\n⇒ 11 x2 + 121x + 218 = 0\n\nHere, D = 5049\n\nX = -121 ± √5049/22\n\n(28) Show that the sum of all terms of an A.P. whose first term is a, the second term is b and the last term is c is equal to (a + c) (b + c – 2a)/ 2(b –a)\n\nSolution: Here d = b – a\n\nLet c be the nth term\n\n∴ c = a + (n – 1) (b – a)\n\n⇒ n = c+b – 2a/ b – a\n\n⇒ Sn = c+ b – 2a/ 2(b – a) (a+c)\n\nOR\n\nSolve the equation : 1 + 4 + 7 + 10 + … + x = 287.\n\nSolution: Let sum of n terms = 287\n\nn/2[2 x1 + (n – 1) 3] = 287\n\n3n2 – n – 574 = 0\n\n(3n + 41) (n – 14) =0\n\nn = 14 ( Reject n = -41/3)\n\nx = a14 = 1 + 13 x 3 = 40\n\n(29) In a flight of 600 km, an aircraft was slowed down due to bad weather. The average speed of the trip was reduced by 200 km/hr and the time of flight increased by 30 minutes. Find the duration of flight.\n\nSolution: Let actual speed = x km/hr A.T.Q\n\n600/ x – 200 – 600 / x = 1/2\n\nX2 – 200x – 240000 = 0\n\n(x – 600) (x + 400) = 0\n\nX = 600 (x = -400 Rejected)\n\nDuration of flight = 600/600 = 1hr\n\n(30) If the mid-point of the line segment joining the points A(3, 4) and B(k, 6) is P (x, y) and x + y – 10 = 0, find the value of k.\n\nSolution:", null, "X = 3 + k/2 y = 5\n\nX + y – 10 = 0 ⇒ 3 + k / 2 + 5 – 10 = 0\n\n⇒ k = 7\n\nOR\n\nFind the area of triangle ABC with A (1, –4) and the mid-points of sides through A being (2, –1) and (0, –1).\n\nSolution:", null, "B(3, 2), C(–1, 2)\n\nArea = 1/2 / 1 (2 – 2) + 3 (2 + 4 – 1 (-4 – 2)/ = 12 sq. units\n\n(31) In Fig. 7, if ΔABC ~ ΔDEF and their sides of lengths (in cm) are marked along them, then find the lengths of sides of each triangle.", null, "Solution: As ΔABC ~ ΔDEF\n\n2x – 1/18 = 3x/ 6x\n\nX = 5\n\nAB = 9 cm\n\nBC = 12 cm\n\nCA = 15 cm\n\nDE = 18 cm\n\nEF = 24 cm\n\nFD = 30 cm\n\n(32) If a circle touches the side BC of a triangle ABC at P and extended sides AB and AC at Q and R, respectively, prove that AQ = 1/2 (BC + CA + AB)\n\nSolution:", null, "Correct Fig\n\nAQ = 1 /2 (2AQ)\n\n= 1/ 2 (AQ + AQ)\n\n= 1 / 2 (AQ + AR)\n\n= 1 / 2 (AB + BQ + AC + CR)\n\n= 1/ 2 (AB + BC + CA)\n\n∵ [BQ = BP, CR = CP]\n\n(33) If sin θ + cos θ = √2 , prove that tan θ + cot θ = 2.\n\nSolution: sin θ + cos θ = √2\n\ntan θ + 1 = √2 sec θ\n\nSq. both sides\n\ntan2 θ + 1 + 2 tan θ = 2sec2 θ\n\ntan2 θ + 1 + 2 tan θ = 2(1 + tan2 θ)\n\ntan2 θ + 1 + 2 tan θ = 2 + 2tan2 θ\n\n2 tan θ = tan2 θ +1\n\n2 = tan θ + cot θ\n\n(34) The area of a circular play ground is 22176 cm2 . Find the cost of fencing this ground at the rate of  ₹50 per metre.\n\nSolution: Let the radius of playground be r cm\n\nπ r2 = 22176 cm2\n\nr = 84 cm\n\nCircumference = 2πr = 2 x 22/7 x 84 = 528 cm\n\nCost of fencing = 50/100 x 528 = ₹ 264\n\nSECTION – D\n\nQuestion numbers 35 to 40 carry 4 marks each.\n\n(35) Prove that √5 is an irrational number.\n\nSolution: Let √5 be a rational number.\n\n√5= p/q, p & q are coprimes & q ≠ 0\n\n5q2 = p2 ⇒ 5 divides p2 ⇒ 5 divides p also Let p = 5a, for some integer a\n\n5q2 = 25a2 ⇒ q2 = 5a2 ⇒ 5 divides q2 ⇒ 5 divides q also\n\n∴ 5 is a common factor of p, q, which is not possible as p, q are coprimes.\n\nHence assumption is wrong √5 is irrational no.\n\n(36) It can take 12 hours to fill a swimming pool using two pipes. If the pipe of larger diameter is used for four hours and the pipe of smaller diameter for 9 hours, only half of the pool can be filled. How long would it take for each pipe to fill the pool separately?\n\nSolution: Let time taken by pipe of larger diameter to fill the tank be x hr Let time taken by pipe of smaller diameter to fill the tank be y hr\n\nA.T.Q\n\n1/x + 1/y = 1/12, 4/x + 9/y = 1/2\n\nSolving we get x = 20 hr y = 30 hr\n\n(37) Draw a circle of radius 2 cm with centre O and take a point P outside the circle such that OP = 6.5 cm. From P, draw two tangents to the circle.\n\nSolution: Correct construction of circle of radius 2 cm\n\nCorrect construction of tangents.\n\nOR\n\nConstruct a triangle with sides 5 cm, 6 cm and 7 cm and then construct another triangle whose sides are 3/ 4 times the corresponding sides of the first triangle.\n\nSolution: Correct construction of given triangle Construction of Similar triangle\n\n(38) From a point on the ground, the angles of elevation of the bottom and the top of a tower fixed at the top of a 20 m high building are 45° and 60° respectively. Find the height of the tower.\n\nSolution:", null, "Let height of tower = h m\n\nIn rt. ΔBCD tan 45° = BC/CD\n\n1 = 20/CD\n\nCD = 20 m\n\nIn rt. ΔACD tan 60° = AC/CD\n\n√3 = 20 + h/ 20\n\nh = 20 (√3 – 1) m\n\n(39) Find the area of the shaded region in Fig. 8, if PQ = 24 cm, PR = 7 cm and O is the centre of the circle.", null, "Solution: ∠P = 90° RQ = √(24)2 + 72 = 25 cm, r = 25/2 cm\n\nArea of shaded portion = Area of semi circle – ar (Δ PQR)\n\n= 1/2 X 22/7 X (25/2)2 – 84\n\n= 161 . 54 cm2\n\nOR\n\nFind the curved surface area of the frustum of a cone, the diameters of whose circular ends are 20 m and 6 m and its height is 24 m.\n\nSolution: R = 10 m r = 3 m h = 24 m\n\nl = √(24)2 + (10 – 3)2 = 25 cm\n\nCSA = π (10 + 3) 25 = 325 π m2\n\n(40) The mean of the following frequency distribution is 18. The frequency f in the class interval 19 – 21 is missing. Determine f.\n\n Class interval 11- 13 13 – 15 15 – 17 17 – 19 19 – 21 21 – 23 23 – 25 Frequency 3 6 9 13 f 5 4\n\nSolution:\n\n C.I f x xf 11 – 13 3 12 36 13 – 15 6 14 84 15 – 17 9 16 144 17 – 19 13 18 234 21 – 23 5 22 110 23 – 25 4 24 96 40 + f 704 + 20 f\n\nMean =  Σ xf/ Σ f ⇒ 18 = 704 + 20 f/ 40 + f ⇒ f = 8\n\nOR\n\nThe following table gives production yield per hectare of wheat of 100 farms of a village:\n\n Production yield 40 – 45 45 – 50 50 – 55 55 – 60 60 – 65 65 – 70 No. of farms 4 6 16 20 30 24\n\nChange the distribution to a ‘more than’ type distribution and draw its ogive.\n\nSolution:\n\n Production yield Number of farms More than or equal to 40   More than or equal to 45   More than or equal to 50   More than or equal to 55   More than or equal to 60   More than or equal to 65 100   96   90   74   54   24\n\nPlotting of points (40, 100) (45, 96) (50, 90) (55, 74) (60, 54) (65, 24) join to get ogive." ]
[ null, "https://i0.wp.com/www.netexplanations.com/wp-content/uploads/2022/07/30-2-1.jpg", null, "data:image/svg+xml,%3Csvg%20xmlns='http://www.w3.org/2000/svg'%20width='130'%20height='116'%20viewBox='0%200%20130%20116'%3E%3C/svg%3E", null, "data:image/svg+xml,%3Csvg%20xmlns='http://www.w3.org/2000/svg'%20width='130'%20height='120'%20viewBox='0%200%20130%20120'%3E%3C/svg%3E", null, "data:image/svg+xml,%3Csvg%20xmlns='http://www.w3.org/2000/svg'%20width='213'%20height='126'%20viewBox='0%200%20213%20126'%3E%3C/svg%3E", null, "data:image/svg+xml,%3Csvg%20xmlns='http://www.w3.org/2000/svg'%20width='115'%20height='106'%20viewBox='0%200%20115%20106'%3E%3C/svg%3E", null, "data:image/svg+xml,%3Csvg%20xmlns='http://www.w3.org/2000/svg'%20width='155'%20height='114'%20viewBox='0%200%20155%20114'%3E%3C/svg%3E", null, "data:image/svg+xml,%3Csvg%20xmlns='http://www.w3.org/2000/svg'%20width='126'%20height='111'%20viewBox='0%200%20126%20111'%3E%3C/svg%3E", null, "data:image/svg+xml,%3Csvg%20xmlns='http://www.w3.org/2000/svg'%20width='200'%20height='88'%20viewBox='0%200%20200%2088'%3E%3C/svg%3E", null, "data:image/svg+xml,%3Csvg%20xmlns='http://www.w3.org/2000/svg'%20width='222'%20height='59'%20viewBox='0%200%20222%2059'%3E%3C/svg%3E", null, "data:image/svg+xml,%3Csvg%20xmlns='http://www.w3.org/2000/svg'%20width='136'%20height='106'%20viewBox='0%200%20136%20106'%3E%3C/svg%3E", null, "data:image/svg+xml,%3Csvg%20xmlns='http://www.w3.org/2000/svg'%20width='217'%20height='84'%20viewBox='0%200%20217%2084'%3E%3C/svg%3E", null, "data:image/svg+xml,%3Csvg%20xmlns='http://www.w3.org/2000/svg'%20width='198'%20height='121'%20viewBox='0%200%20198%20121'%3E%3C/svg%3E", null, "data:image/svg+xml,%3Csvg%20xmlns='http://www.w3.org/2000/svg'%20width='152'%20height='179'%20viewBox='0%200%20152%20179'%3E%3C/svg%3E", null, "data:image/svg+xml,%3Csvg%20xmlns='http://www.w3.org/2000/svg'%20width='116'%20height='98'%20viewBox='0%200%20116%2098'%3E%3C/svg%3E", null ]
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https://forumgeom.fau.edu/FG2009volume9/FG200918index.html
[ "David Graham Searby, On three circles,\nForum Geometricorum, 9 (2009) 181--193.\n\nAbstract:  The classical Three-Circle Problem of Apollonius requires the construction of a fourth circle tangent to three given circles in the Euclidean plane. For circles in general position this may admit as many as eight solutions or even no solutions at all.  Clearly, an ``experimental\" approach is unlikely to solve the problem,  but, surprisingly, it leads to a more general theorem. Here we consider the case of a chain of circles which, starting from an arbitrary point on one of the three given circles defines (uniquely, if one is careful) a tangent circle at this point and a tangency point on another  of the given circles. Taking this new point as a base we construct a circle tangent to the second circle at this point and to the third circle, and repeat the construction  cyclically. For any choice of the three starting circles, the tangency points are concyclic and the chain can contain at most six circles. The figure reveals unexpected connections with many classical theorems of projective geometry, and it admits the Three-Circle Problem of Apollonius as a particular case.\n\n[ps file][pdf]" ]
[ null ]
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https://cleaninside.pl/08-05_formulae-of-the-ionic-compounds-that-will-form-in-iceland.html
[ "# formulae of the ionic compounds that will form in iceland\n\n### SIMPLE IONIC - SIMPLE IONIC Which one of the …\n\nView Homework Help - SIMPLE IONIC from CHEMI 101 at College of DuPage. SIMPLE IONIC Which one of the following pairs will form an ionic compound with a 1:1 ratio between\n\n### Ionic compounds | Teaching Resources\n\nIncluded: levelled tasks, questions & answeres explanations and step by step instructions how to work out the formula of an ionic compound. Explanations of compound ions are also included. covers in edexcel additional science, chemistry topic 2.3-2.5. This lesson\n\n### 1B5 Ionic Compounds - Chemistry\n\nIonic compounds are electrically neutral, so there must be a balance of ions and anions in a compound. When coining, positive ions collect enough negative ions to offset their charge. In any compound, the nuer of atoms of a ion depends on the ion it is\n\n### Ion - Wikipedia\n\nHistory of discovery The word ion comes from the Greek word ἰόν, ion, \"going\", the present participle of ἰέναι, ienai, \"to go\".This term was introduced (after a suggestion by the English polymath William Whewell ) by English physicist and chemist Michael Faraday in 1834 for the then-unknown species that goes from one electrode to the other through an aqueous medium.\n\n### For each of the following pairs of ions, write the formula …\n\n4/5/2015· Textbook solution for Chemistry by OpenStax (2015-05-04) 1st Edition Klaus Theopold Chapter 2 Problem 50E. We have step-by-step solutions for your textbooks written by\n\n### /a>\n\n26/10/2017· 9. Why do ionic compounds tend to be hard? bonds 10.Almost all ion compounds are called s structure. and have a ll.ln a solid state (crystalline form), does an ionic compound conduct electricity? Why? No, / ons Can''* move- 12.1n a liquid or molten form does\n\n### CH150: Chapter 3 – Ions and Ionic Compounds – Chemistry\n\nCH150: Chapter 3 – Ions and Ionic Compounds This content can also be downloaded as an printable PDF, adobe reader is required for full functionality. This text is published under creative commons licensing, for referencing and adaptation, please click here. 3.1\n\n### Metallacycle · Nomenclature of Ionic Compounds\n\nOne nice way to gain familiarity and exposure to ionic compounds is to study the system of nomenclature used to assign unique names to them. Converting from a molecular formula to a name will help you learn how to communie the identity of substances clearly in words—a very important problem as the diversity and complexity of known substances continues to increase!\n\n### Ionic Compounds6.pdf - QUESTION Decide whether …\n\nView Ionic Compounds6.pdf from CHEMISTRY 1110 at Weber State University. QUESTION Decide whether each pair of elements in the table below will form an ionic compound. If\n\n### University High School Chemistry: Ionic Nomenclature\n\nIonic compounds form ionic crystal lattices rather than molecules. Ionic compounds have very high melting and boiling points. Ionic compounds tend to be brittle solids. Ionic compounds are generally soluble in water, and the resulting solutions will conduct\n\n### Why do some coinations of ionic compounds form …\n\nSome coination of ionic compound forms precipitates while others do not because precipitate will form only in that case where the salt is insoluble See full answer below.\n\n### 2 Formulas for compounds are balanced so that the …\n\nFormulas for compounds are balanced so that the total positive ionic charge is equal to the total negative ionic charge + - 3 Al 2 O 3 2 3 Total positive = +6 Total negative = -6 C. Sizes of Ions 1. Anions are larger than the parent atom 2. ions are smaller than\n\n### Solved: 2. Predict The Formula Of The Ionic Compounds …\n\n2. Predict the formula of the ionic compounds formed from the following pairs of elements using Lewis syols. Name the compounds. a. Al and I b. Rb andS 3. Rank the following in order of increasing bond length and bond strength. a. Si-F Si-C; Si-o 4. Calculate\n\n### Write the empirical formula for at least four ionic …\n\nQuestion: Write the empirical formula for at least four ionic compounds that could be formed from the following ions: {eq}Fe^{2+}, CO_{3}^{2-}, Fe^{3-}, SO_{4}^{2-}{/eq} Empirical Formulas\n\n### Ionic Compounds7.pdf - QUESTION Decide whether …\n\nQUESTION Decide whether each pair of elements in the table below will form an ionic compound. If they will, write the empirical formula of the compound formed in the space provided. EXPLANATION When a compound is made from only two elements, we call it a binary compound. compound.\n\n### What is the formula for the ionic compound of …\n\nFormula: [K+][I-]The chemical formula for potassium iodide is KI. When Potassium and bromine react to form an ionic compound they form a compound called? Potassium bromide.\n\n### Practice Problems Ionic Compounds Answers\n\n4 answer b cuso 4 answer c cacl 2 practice naming ionic compounds when given the formula practice youve mastered them the next step is predicting whether two species will form ionic or covalent bonds naming ionic compounds worksheet name the\n\n### aluminum and nitrogen form an ionic compound with …\n\n8/5/2010· aluminum and nitrogen form an ionic compound with the formula? A. AL2N3 B. AL3N2 C. ALN D. ALN3 Source(s): aluminum nitrogen form ionic compound formula : 1 1 dabdoub Lv 4 4 years ago Aluminum Nitride Formula Source(s): 0 0\n\n### Ions and Ionic Compounds – Introductory Chemistry – …\n\nThe naming of ionic compounds that contain polyatomic ions follows the same rules as the naming for other ionic compounds: simply coine the name of the ion and the name of the anion. Do not use numerical prefixes in the name if there is more than one polyatomic ion; the only exception to this is if the name of the ion itself contains a numerical prefix, such as dichromate or triiodide.\n\n### Ionic bonding - IGCSE Chemistry Revision\n\n7/1/2013· The ions form a regular lattice in which the ionic bonds act in all directions. Dot-and-cross diagrams You need to be able to draw dot-and-cross diagrams to show the ions in some common ionic compounds .\n\n### What are the main properties of ionic compounds? | …\n\n2/10/2014· There are many properties. Here is a short list of main properties: They form crystals. Ionic compounds form crystal lattices rather than amorphous solids. They have higher enthalpies of fusion and vaporization than molecular compounds. They are hard. They are brittle. They have high melting points and also high boiling points. They conduct electricity but only when they are dissolved in water\n\n### Ionic Bonding | Chemical Bonding | Siyavula\n\nIonic compounds have a nuer of properties: Ions are arranged in a lattice structure Ionic solids are crystalline at room temperature The ionic bond is a strong electrostatic attraction. This means that ionic compounds are often hard and have high melting and\n\n### Simple Binary Ionic Compounds - Appoquinimink High School\n\n18/3/2015· Remeer that ionic compounds must be neutral. In order to yield a neutral compound, two chlorides must bond to the calcium ion: (+2) + 2(-1) = 0 So, the formula for this salt is CaCfe. Nomenclature: When naming ionic compounds, simply write the element\n\n### Ionic and Molecular Compounds | Infinite Essays\n\n1. Name each of the following molecular compounds a. CO2 b. N2O c. P2O5 d. N2S3 e. CF4 2. Write the formula of the following molecular compound a. Carbon tetrachloride b. Sulfur dioxide c. Phosphorus pentafluoride d. Dinitrogen tetroxide e. Chlorine dioxide 3. Classify each of the following as ionic or molecular and give its […]\n\n### Solved: Fill In The Name And Empirical Formula Of Each …\n\nFill in the name and empirical formula of each ionic compound that could be formed from the ions in this table: Some ionic compounds ionanionempirical formula name of compound Ba2+ Cr3+ Mg2+ Get more help from Chegg Get 1:1 help now from expert" ]
[ null ]
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https://gsebsolutions.com/gseb-solutions-class-9-maths-chapter-4-ex-4-4/
[ "# GSEB Solutions Class 9 Maths Chapter 4 Linear Equations in Two Variables Ex 4.4\n\nGujarat Board GSEB Solutions Class 9 Maths Chapter 4 Linear Equations in Two Variables Ex 4.4 Textbook Questions and Answers.\n\n## Gujarat Board Textbook Solutions Class 9 Maths Chapter 4 Linear Equations in Two Variables Ex 4.4\n\nQuestion 1.\nGive the geometric representations of y = 3 as an equation\n(i) in one variable.\n(ii) in two variables\nSolution:\nThe given equation is y = 3\n(i) In one variable, y = 3\nRepresentation of y = 3 on a number line\nreflects a point. For this, we draw a vertical number line and locate the point.", null, "", null, "(ii) In two variables, y = 3 can be expressed as o.x + 1.y = 3", null, "This is a linear equation in two variables x and y which is represented by a line. All the values of x are permissible because 0.x is always 0. whereas y satisfies the relation y = 3. Therefore two solutions of the given equation are x = 0, y = 3 and x = 2, y = 3.\nHence the graph AB is a line parallel to x-axis at the distance of 3 units above the origin.", null, "Question 2.\nGive the geometric representations of 2x + 9 = 0 as an equation\n(i) in one variable (ii) in two variables\nSolution:\nThe given equation is 2x + 9 = 0 on the number line is shown below.", null, "(ii) In one variable", null, "2x + 9 = 0\n2x + 0.y + 9 = 0\nThis is a linear equation in two variables x andy which is represented by a line. Hence all the values of y are permissible because 0.y is always 0. Whereas x must satisfies the relation 2x + 9 = 0 i.e., x = $$\\frac {-9}{2}$$\nHence two solutions of given equation are, x = $$\\frac {-9}{2}$$ , y = 0, and x = $$\\frac {-9}{2}$$ , y = 2\nHence AB is a line parallel to the y-axis and at a distance of $$\\frac {9}{2}$$ units to the left of origin O.", null, "" ]
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http://www.jmchemsci.com/article_135204.html
[ "Document Type : Original Article\n\nAuthor\n\nM.V. Lomonosov Institute of Fine Chemical Technologies, MIREA - Russian Technological University, Vernadskogo pr., 86, Moscow, 119571, Russia\n\nAbstract\n\nComputer chemistry is a field of science appearing at the intersection of chemistry, mathematics and informatics. For the solution of any task in this field some mathematical representation of chemical structures is need. The most widely used approach to description of molecular structure is based on its representation as a graph G with vertices and edges corresponding to atoms and bonds of molecule. However, there may be other ways of describing the molecular structure. In this paper a number of methods to present the molecular structures of organic compounds (hydrocarbons) as hypergraphs Hk (k=1,2,…) of special type is suggested. Some results of comparison of graph and hypergraph molecular models are also given. Construction of Hk is defined by neighborhoods of k-th order for all vertices in a graph G corresponding to the carbon skeleton of molecule (k=1,2,…). Besides, analytical formulae, expressing the adjacency matrices of Hk throw adjacency matrix of corresponding graph G are obtained (k=1,2,…). The comparison of traditional graph model G and suggested hypergraph models Hk (k=1,2,…) is made by definite quantitative parameters, characterizing the efficiency of their applications in some tasks of computer chemistry. Some 4 different sets of structural formulae of hydrocarbons and 30 different quantitative parameters are used for these investigations. It is shown, that in 97% of all considered 120 cases the model H1 is superior to the model G, and in other cases these models are equivalent. However, the models Hk for k ≥ 2 are worse than G and H1. It is also shown on concrete examples, that in some cases, H1-models may be useful in constructing the structure-property correlations, since their use allows us to obtain more precise correlations than for G-models (in 75% of considered cases).\n\nGraphical Abstract", null, "Keywords\n\n###### ##### Full Text\n\nIntroduction\n\nComputer chemistry is a field of science appearing at the intersection of chemistry, mathematics and informatics. The basic problems of computer chemistry are, in particular, the problems of computer generation of possible reactions between given reagents, the construction of mathematical models connecting the structures and different properties of chemical compounds and prediction the properties of new compounds using this models, computer generation of chemical compounds with prescribed properties, etc. [1-6].\n\nHowever, for the solution of any task, considered in this field, chemical compounds must be as some mathematical objects represented. Therefore, in computer chemistry, there is a number of special tasks, which deal with constructing the mathematical models of chemical compounds, investigating the properties of these models, elaborating the different algorithms (combinatorial, optimization, etc.) operating with selected mathematical objects.\n\nThere are many different types of molecular models; they describe the molecular structure with different level of detailing and reflect certain peculiarities of molecule. However, the most widespread mathematical models of molecules are graphs. These graphs are usually called “molecular graphs”. A molecular graph is a weighted (or labeled) graph with vertices corresponding to atoms of molecule, and with edges corresponding to chemical bonds in it. The weights (or labels) of vertices and edges code atoms and bonds of different chemical nature (see, for example, ).   This graph can be described by matrix A = (aij), where aii is a weight of vertex i, and aij for i ≠ j is a weight of edge (i, j). It is usually supposed that aij = 0 for non-adjacent vertices i and j. For molecules of hydrocarbons, as a rule, simple graphs representing only carbon skeleton of molecule are used. In this case it is assumed that aii = 0, aij = 1 for adjacent vertices i and j, aij = 0 for non-adjacent vertices i and j, and then matrix A is the adjacency matrix of corresponding graph [8, 9].\n\nFor each molecular structure, different invariants of its molecular graph may be calculated, that is, the numbers defined by graph, which are independent of numbering the graph vertices. The examples of simple graph invariants are the numbers of vertices, edges, cycles in a graph, determinant of its adjacency matrix, etc. The graph invariants are widely used as so-called molecular descriptors in mathematical models of relation between the structure and properties of chemical compounds; these models are often called Quantitative Structure-Property Relationships or QSPR [8, 10, and 11]. However, graph invariants are not only used in QSPR-analysis, they may be also applied in procedures of coding, ordering, searching for chemical compounds in chemical data bases. Therefore, the problem of search for graph invariants with little degeneration degree (or with big discrimination ability) is of great importance. The investigations of degeneration degrees of graph invariants and comparison of invariants by this parameter on some particular sets of graphs are usually fulfilled (see, for example, ).\n\nFor the solution of some problems of computer chemistry the local vertex invariants (LVI) are also used; for example, in the searching the canonical numbering the molecular graph vertices, or in the searching the symmetry group of a graph, or in establishing the graph isomorphism (see, for example, [13, 14]). All methods of solutions of these problems are based on exhaustive search with using some criteria for rejection of unsuitable variants. As a rule, these criteria are formulating in terms of some LVI. For effective solutions of such tasks, it is important to find LVI, which can quantitatively distinguish non-equivalent vertices of a graph; that is, vertices belonging to different orbits of symmetry group of a graph. Therefore, the problem of searching the LVI having the greatest ability to distinguish non-equivalent vertices is actual one. Note that there are other possible applications of LVI, for example, constructing on their base new graph invariants or graph codes, that is, sequences of ordered LVI .\n\nAs it is known, a generalization of a notion “graph” is a notion of “hypergraph” [15-20]. A hypergraph H = (V, E) is a pair of some sets V = {v1,…,vn} and E = {e1,…,ep}, where V is a set of vertices, E is a set of hyperedges; any hyperedge ei is some non-empty subset of set V, which can contain any number of elements. Thus, the graph G is a particular case of a hypergraph H, when any hyperedge ei consists of two vertices, and called by edge. In the picture of hypergraph, their hyperedges are indicated with help of closed curve, inside of which place the corresponding vertices; for hyperedge with two vertices these vertices by a segment of strait line are connected. A hypergraph H may be given by its incidence matrix B = (bij) of dimension nxp, where bij = 1, if vertex vi belongs to hyperedge ej, and bij = 0 in otherwise. The example of hypergraph Н with vertices v1,…, v4 and hyperedges e1 = {v1}, e2 = {v2,v3}, e3 = {v1,v2,v4} and its incidence matrix B is given in Figure 1.\n\nFor a hypergraph H the adjacency matrix A = (aij) can be also defined: An element aij for  is equal to a number of hyperedges, containing the pair of vertices i and j, and aii = 0. The definitions of invariants or LVI for a hypergraph are similar to definitions of these notations for a graph. Besides, invariants and LVI for hypergraph one can calculate using some their matrices and known algorithms elaborated for ordinary graphs. It should be noted, that, as a rule, hypergraphs with simple hyperedges are considered; that is, each set ei in this construction is taking into account only once.", null, "Figure 1: Example of hypergraph Н and its incidence matrix В\n\nHypergraphs are also applying in computer chemistry. Ordinary graphs do not adequately describe chemical compounds of non-classical structures; for example, molecules with delocalized polycentric bonds, in particular, organometallic compounds. In a number of works for description of structures of such compounds the hypergraphs were suggested (see, for example, [19-23]). In a previous study , for very large set of compounds with non-classical structures the graph models and hypergraph models were considered; for these molecular graphs and hypergraphs some known invariants of the same name were calculated and it was shown, that invariants of hypergraphs were essentially less degenerative than analogous invariants of graphs. Some advantages of hypergraph representation of such molecules were also noted. However, in literature any results concerning the using the hypergraph invariants in QSPR-analysis are absent.\n\nTo perceive isomorphic hypergraphs, the sanctioned types of rate grids are to be found. The calculation for development of standard rate network of hypergraph is proposed. Some substance issues managing the hypergraph hypothesis are talked about .\n\nDiagram hypothetical ideas are valuable for the portrayal and investigation of communications and connections in organic frameworks .\n\nThe consequences of this investigation showed that the affectability of most lists is higher in the hypergraph model. The absolute number of no correlated files additionally increments in the last model .\n\nIt should be noted that amount of works devoted to applications of hypergraphs in chemistry is very little, compared with amount of works deals with applications of graphs in chemistry [29, 30]. Besides, the hypergraphs for the description of compounds with classical structures were not used. The main reason of this is that the structural formula of molecule already is a labeled graph, which allows construct on its base other different molecular graphs. Another possible reason of little using of hypergraphs in chemistry is the complexity of visual perception of such graphical constructions.\n\nMaterial and methods\n\nNote that in all graph models of molecules, two vertices are connected by an edge if and only if there is a chemical bond between the corresponding atoms, indicated in structural formula. However, there is some interaction between atoms, which are not connected by such bonds; in this case, the force of atom interaction depends on distance between atoms. These reasons lead us to idea to assume that “are connected” not two, but a few atoms, which are arranged nearly from each other (by some criteria of nearness) and to use the hypergraphs for description of classical molecular structures. For example, one can assume, that “are connected” all atoms arranged in neighborhood of the 1-st order of fixed atom or all four atoms arranged on a chain of three sequential chemical bonds. Thus, new models of structures of classical compounds arise; these models are hypergraphs and they based on definite interpretation of notion “connectedness of atoms”. The obtained models one can to compare with traditional graph models by some parameters, as this was done, for example, in a series of works [19-23] for the non-classical structures, and to conclude about their appropriateness and usefulness in computer chemistry.\n\nThe main goals of the present work were as follows:\n\n1) To elaborate a number of ways of molecular structure description for organic compounds (hydrocarbons) in terms of hypergraphs using for this purpose different interpretations of the notion “connectedness of atoms”;\n\n2) To deduce a general analytical formula, expressing the adjacency matrices of obtained molecular hypergraphs throw the adjacency matrices of corresponding molecular graph;\n\n3) To compare the efficiencies of using the traditional graph model and suggested hypergraph models of molecules in some special tasks of computer chemistry, mentioned above; and,\n\n4) To investigate the usefulness of hypergraph models in constructing the structure-property correlations.\n\nLet us now list briefly the main results of this article.\n\n1) A number of ways of constructing the hypergraph models of organic compounds (hydrocarbons of some classes) are suggested.\n\n2) The general analytical formulae connecting the adjacency matrices of obtained hypergraphs and adjacency matrix of initial molecular graph are deduced.\n\n3) A comparison of traditional graph model of hydrocarbons and suggested hypergraph models is by definite quantitative parameters, characterizing the efficiency of their applications in some tasks of computer chemistry. For this comparison, some 4 different sets of hydrocarbons and 30 different quantitative parameters were used. It was found, that one of the suggested hypergraph models in 97% considered cases is superior to the graph model, and in other cases these models are equivalent.\n\n4) It is shown, that in some cases the hypergraph models may be useful in constructing the structure-property correlations, since their use in this process allows us to obtain more precise correlations than for graph models.\n\nResult and Dissection\n\nA set of all 80 structural formulae of saturated hydrocarbons with 6, 7, 8 carbon atoms from , and a set of all 22 structural formulae of alkyl benzenes with 10 carbon atoms from were used in aforementioned investigations. Molecular graphs of carbon skeletons of all these compounds are given in Figures 2-6. The vertices of pictured graphs correspond to atoms in molecule, and the edges - to chemical bonds between these atoms. We denote these graphs by letter G.", null, "Figure 2:  Compounds 1-24 used for construction and investigation of hypergraph molecular models", null, "Figure 3: Compounds 25-44 used for construction and investigation of hypergraph molecular models", null, "Figure 4: Compounds 45-64 used for construction and investigation of hypergraph molecular models", null, "Figure 5: Compounds 65-80 used for construction and investigation of hypergraph molecular models", null, "Figure 6: Compounds 81-102 used for construction and investigation of hypergraph molecular models\n\nLet us describe a procedure of constructing Hk-models (k ≥ 1) of aforementioned compounds by initial molecular graphs G, derived from the structural formulae of molecules. Let G = (V (G), E (G)) be a graph with n vertices numbered arbitrarily by numbers 1,…, n. We construct a hypergraph Hk = (V (Hk), E (Hk)), k ≥ 1, by a graph G, using the following rules:\n\nV(Hk )=V(G), E(Hk )={e1,…,ep }, ei={set of vertices j: d(i,j)≤k},                                                                        (1)\n\nWhere d (i,j) is the distance between vertices i and j. In other words, hyperedge ei is a neighbor of k-th order of vertex i (i = 1,…, n).\n\nThe examples of graph G, hypergraph H = H1, their adjacency matrices A(G), A(H) and their incident matrices B(G), B(H) are given in Figure 7. In this case G = (V (G), E (G)) and H = (V (H), E (H)), where:\n\nV(G) = {1,2,3,4},E(G)={h1, h2, h3},                           (2)\n\nh1 = {1,2}, h2 = {2,3}, h3={3,4};\n\nV(H) = {1,2,3,4}, E(H)={e1, e2, e3 },\n\ne1={1,2}, e2={1,2,3}, e3={2,3,4}, e4={3,4}", null, "Figure 7: Graph G and corresponding hypergraph H = H1 and their matrices A (G), A (H), B (G), B (H)\n\nIt should be noted, that if k ≥ D(G), where D(G) is the diameter of a graph G, then all hyperedges of constructed hypergraph Hk will be identical and will coincide with the set V(G). In this case, all elements of matrix B (Hk) will be equal to unit, and all elements of matrix A (Hk) will be equal to n. Thus, all information about a graph structure will be lost and Hk-model will be senseless.\n\nSince in our investigations we compare graph model G and hypergraph models Hk by a number of characteristics of the same name, calculated by their adjacency matrices A (G) and A (Hk), a deduction of analytical relations between A (G) and A (Hk) is interesting.\n\nLet us introduce the following notations: E - identity matrix of dimension n; D (m) = (dij(m)) - symmetrical matrix of dimension nxn, where dij(m) = 1, if dij = m and dij(m) = 0 in otherwise, m = 1,2,…, k; V = (vii) - diagonal matrix of dimension nxn, where", null, "vi - degree of vertex I in graph G.\n\nStatement   The following formula, connecting matrices A (G) and A (Hk), k ≥ 1, is true:", null, "Proof It is known, that for any hypergraph H (in particular, for any graph G) the following formula takes place: A = BB*-V.  Here A is the adjacency matrix of H (or G), B is the incident matrix of H (or G), B* is the matrix, transposed to B, V = (vii) is the diagonal matrix, vii is the degree of vertex i in H (that is, vii is the number of hyperedges, to which vertex i belongs). In considered case B = B*, hence BB* = B2. Besides, A (G) = D (1) and", null, "Where vi is the degree of vertex i in a graph G. Thus,\n\n B =E +D(1)+ D(2)+…+ D(k) = E+A(G)+ D2+ D(k) (6)\n\nThe required formula follows from this relation. In particular, for k = 1:\n\nA(H) = (E+A(G))2-V = E+2A(G) +A2(G)-V                (7)\n\nWhere V is diagonal matrix with diagonal elements, which are equal to vi + 1, where vi is the degree of vertex i in graph G.\n\nLet us define a number of simple local vertex invariants (LVI) of graph and hypergraph, based on their adjacency matrices A.  Let A2 = (aij(2)) be a square of adjacency matrix A of graph G (or hypergraph H). Let us consider the following five LVI:", null, "Note, that for graph G the number wi(1) is equal to degree of vertex i, and wi(1) = wi(2) = wi(3). Besides, let us consider 4 following sets of compounds (or corresponding molecular graphs), formed on the base of the set of initial data, consisting of:\n\n• all saturated hydrocarbons with 6 and 7 carbon atoms (№№ 1-41 in Figure 2(a),(b); the number of such compounds is equal to N = 41);\n• all saturated hydrocarbons with 8 carbon atoms (№№ 42-80 in Figure 2 (b)-(d); the number of such compounds is equal to N = 39);\n• All saturated hydrocarbons with 6, 7, 8 carbon atoms (№№ 1-80 in Figure 2(a)-(d); the number of such compounds is equal to N = 80).\n• All alkyl benzenes with 10 carbon atoms (№№ 81-102 in Figure 2(e); the number of such compounds is equal to N =22).\n\nLet us compare LVI of the same name by their capacities to distinguish non-equivalent vertices in initial molecular graphs. For this purpose, two quantitative characteristics of this capacity, N1 and N2, are introduced. The number N1 is a fraction of structures in considered set, in which there are indistinguishable non-equivalent vertices. It is easily to see, that 0 ≤ N1 ≤ 1, and N1 = 0 for the best case, when all non-equivalent vertices in all considered structures are distinguishable, and N1 = 1 for the worst case, when in all structures all non-equivalent vertices are indistinguishable.\n\nLet us now define the second characteristics, N2. At first, we find in each graph G all non-equivalent vertices, which are indistinguishable by considered LVI; these vertices will belong to different classes of equivalence and will have the same values of LVI. Then, we find the minimal number of vertices in this set satisfying the following condition: If we change, by some way, the values of their LVI, then all non-equivalent vertices in a given graph will be distinguishable. Let N2 is a total number of such vertices in all graphs of considered set, M is total number of vertices in these graphs, N is total number of graphs in considered set. It is easily to see, that 0 ≤ N2M-N. Define N2 by the following way:", null, "Evidently, 0 ≤ N2 ≤ 1, and for the best case N2 = 0, and for the worst case N2 = 1, when all vertices in a graph have the same values of LVI, and it is takes place for any graph in considered set). It is natural to accept that the best model from several ones is that which has the least value of N1 (or N2).\n\nIn Tables 1 and 2, the obtained values of N1 and N2 are given for all 5 variants of LVI for 4 sets of compounds (1)-(4), for G and H = H1. From these tables, it follows that in 38 considered cases (from 40 ones) H1-model is better than G-model; that is, the values of N1 and N2 for H1 are less than corresponding values for G; and in 2 cases these models are equivalent. However, for considered sets of compounds Hk-models for k > 1 are worse than H1-model and G-model.", null, "Let us define codes Kj(G) and Kj(H) (j = 1,…,5) for graphs and hypergraphs as the sequences of LVI wi(j) (j = 1,…,5) arranged in ascending order. For example, K1(G) = {1,1,1,2,3,4}, K1(H) = {4,5,5,9,10,11} for graph G and hypergraph H, as shown in Figure 3.\n\nLet us compare these codes by their degeneration degrees. For this purpose, we introduce the quantitative characteristics of degeneration degree of a code, N3 = N3’/N, where N3is the number of different codes for given set of structures. Evidently, 1/N ≤ N3 ≤ 1, and in the best case N3 = 1, in the worst case N3 = 1/N. In Table 3 obtained values of N3 for the sets of molecular graphs (1)-(4) for H1- and G-models are given.", null, "It follows from these data that in 18 cases (from 20 ones) H1-model is better than G-model (that is, N3 for H1-model is more than N3 for G-model); in 2 cases both models are equivalent (values of N3 for both models are the same). Besides, H1-model in 11 cases gives “ideal” result (N3 = 1). However, for considered structures Hk-models for k > 1 are worse than H1 -and G-models.\n\nLet us consider the following 15 simple invariants for graphs and hypergraphs, constructed on the bases of LVI introduced above and on the base of spectral characteristics of adjacency matrix A:\n\nI1 = min wi(1) I2 = max wi(1), I3 = min wi(3), I4 = max wi(3),\n\nI5 = min wi(4),  I6 = max wi(4), I7 = min wi(5), I8 = max wi(5),\n\nI9 = S1 = Σ wi(1)I10  = S2 = Σ (wi(1))2,\n\nI11 = λmax ─ maximal eigenvalue of matrix A,\n\nI12 = λmin  ─ minimal eigenvalue of matrix A,\n\nI13 =  λmax - λminI14 = detA ─ determinant of matrix A,  I15 =  λmax + λmin\n\nLet us compare the degeneration degrees of these invariants on the sets (1)-(4). For this purpose, we will use quantitative characteristic N3 (see subsection 3.2). In Tables 4-6 the obtained values of N3 for the sets (1)-(4) and all 15 described above invariants for G and H = H1 are given.", null, "It follows from these data that in all 60 cases H1-model is better than G-model (that is, N3 for H1-model is more than N3 for G-model). Besides, H1-model in 11 cases gives “ideal” result (N3 = 1).  However, for considered structures Hk-models for k > 1 are worse than H1- and G-models.\n\nIn this section we consider the set of 22 alkylbenzenes (structures  Compounds 81-102, Figure 2(e)) with known values of a number of physico-chemical properties (boiling point, bp (°C); density, d (g×cm-3); refractive index, nD20; heat of combustion, DHc (kcal×mol-1)), given in Table 7 . Using these data, we will analyze the usefulness of H-models in constructing the structure-property correlations.\n\nThe values of invariants I1-I15 (see subsection 3.3) for these structures were earlier calculated for G -models and H-models. Let us denote by symbols {I(G)}and {I(H)}the sets of obtained invariants, that is {I(G)}={I1(G),…,I15(G)} and  {I(H)}={I1(H),…,I15(H)}. We construct for each property under consideration the structure-property correlations with the best 2, 3, 4 parameters, choosing them independently from the one with the following 3 sets:\n\na){I(G)};        b) {I(H)};      c) {I(G)}U{I(H)}.\n\nFor each correlation, we found mean square deviation s and correlation coefficient R; we will further use these parameters to estimate the quality of correlations and to compare one correlation with another. In Tables 8-11 the best 2, 3, 4 parameters for all these cases and corresponding s and R are given.", null, "", null, "Let us analyze the obtained results for all 12 correlations, comparing s and R for correlations for the sets a), b), c) in analogous cases. As we can see, in 9 cases from 12 ones (that is, in 75% of all considered cases) the use of invariants of hypergraphs allows us to obtained more precise correlations than correlations with invariants from the set {I(G)} only.\n\nThus, in a number of cases the hypergraph models may be useful in constructing the structure-property correlations.\n\nConclusion\n\nIn the present paper, a number of ways of constructing the hypergraph models Нk (k ≥ 1) of organic compounds (hydrocarbons of some classes) are described. The vertices of Нk correspond to carbon atoms in molecule, and each hyper edge in Нk is defined as a set of vertices belonging to the neighborhood of k-th order of some fixed vertex for constructing the hyper edges all vertices are considered.\n\nBesides, the analytical formulae connecting the adjacency matrices of obtained hypergraphs Нk (k ≥ 1) and adjacency matrix of initial molecular graph G are deduced; these dependences are nonlinear ones.\n\nA comparison of traditional graph model G and suggested hypergraph models Нk (k ≥ 1) is made by definite quantitative parameters, characterizing the efficiency of their applications in some tasks of computer chemistry. For this comparison, some 4 different sets of hydrocarbons, presented by their structural formulae, and 30 different quantitative parameters are used. It is shown that in 116 cases from considered 120 ones the model H1 is superior to the model G (that is, in 97% of all cases), and in other cases these models are equivalent.  However, for considered sets of structures, the models Hk for k > 1 are worse than the models H1 and G; the reason for this, probably, is relatively small sizes of considered molecules.  Analyzing the results obtained, we can conclude that the hypergraph molecular models can be successfully used in computer chemistry instead traditional graph models.\n\nIt is also shown on concrete examples, that in some cases, the hypergraph models may be useful in constructing the structure-property correlations; since their use in this process allows us to obtain more precise correlations than for G-models; this takes place in 75% of all considered cases.\n\nFunding\n\nThis research did not receive any specific grant from funding agencies in the public, commercial, or not-for-profit sectors.\n\nAuthors' contributions\n\nAll authors contributed toward data analysis, drafting and revising the paper and agreed to be responsible for all the aspects of this work.\n\nConflict of Interest\n\nWe have no conflicts of interest to disclose.\n\nMaria Skvortsova. Molecular Graphs and Molecular Hypergraphs of Organic Compounds: Comparative Analysis, J. Med. Chem. Sci., 2021, 4(5) 452-465\n\nDOI: 10.26655/JMCHEMSCI.2021.5.6\n\n###### ##### References\n1. Marsili M., Computer Chemistry. CRC Press, Boca Raton. 1990 [Crossref], [Google scholar], [Publisher]\n2. Solov’ev M.E., Solov’ev M.M., Computer Chemistry. SOLON-Press, Moscow. 2005 [Google scholar]\n3. Basak S.C., Restrepo J., Villaveces J.L., Advances in Mathematical Chemistry and Applications. Elsevier-Bentham, Sharjah. 2014 [Crossref], [Google scholar], [Publisher]\n4. Wagner S., Wang H., Introduction to Chemical Graph Theory. Chapman and Hall/CRC, London. 2018 [Crossref], [Google scholar], [Publisher]\n5. Bonchev D., Rouvray D.H., Chemical Graph Theory: Introduction and Fundamentals. Routledge, London. 1991 [Google scholar], [Publisher]\n6. Kerber A., Laue R., Meringer M., Rücker C., Schymanski E., Mathematical Chemistry and Chemoinformatics. 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https://www.teachoo.com/8481/2101/Ex-6.4--6/category/Ex-6.4/
[ "Ex 6.4\n\nChapter 6 Class 8 Squares and Square Roots\nSerial order wise", null, "", null, "Get live Maths 1-on-1 Classs - Class 6 to 12\n\n### Transcript\n\nEx 6.4, 6 Find the length of the side of a square whose area is 441 𝑚^2.Given area of the square plot = 441 𝑚^2 Let side of the square = 𝑥 We know that, Area of square = Side2 ∴ Area of square = 𝑥^2 441 = 𝑥^2 𝑥^2 = 441 𝑥 = √441 ∴ Side = √441 Finding square root of 2304 by Long Division :- ∴ Square root of 441 = 21 Thus, Side of the square plot = 21 m", null, "" ]
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https://www.groundai.com/project/application-of-cross-correlations-between-cmb-and-large-scale-structure-to-constraints-on-the-primordial-non-gaussianity/
[ "Application of cross correlations between CMB and large scale structure to constraints on the primordial non-Gaussianity\n\n# Application of cross correlations between CMB and large scale structure to constraints on the primordial non-Gaussianity\n\nYoshitaka Takeuchi Department of Physics, Nagoya University, Chikusa-ku, Nagoya, 464-8602, Japan    Kiyotomo Ichiki Department of Physics, Nagoya University, Chikusa-ku, Nagoya, 464-8602, Japan    Takahiko Matsubara Kobayashi-Maskawa Institute for the Origin of Particles and the Universe, Nagoya University, Chikusa-ku, Nagoya, 464-8602, Japan\nJuly 27, 2019\n###### Abstract\n\nThe primordial non-Gaussianity of local type affects the clustering of dark matter halos, and the planned deep and wide photometric surveys are suitable for examining this class of non-Gaussianity. In our previous paper, we investigated the constraint from the cross correlation between CMB lensing potential and galaxy angular distribution on the primordial non-Gaussianity, without taking into account redshift slicing. To improve our previous analysis, in this paper, we add the galaxy lensing shear into our analysis and take into account redshift slicing to follow the redshift evolution of the clustering. By calculating 81 power spectra and using the Fisher matrix method, we find that the constraint on the primordial non-Gaussianity can be improved from to by including the galaxy-galaxy lensing shear cross correlations expected from the Hyper Suprime-Cam survey (HSC), in comparison with the constraint without any cross correlations. Moreover, the constraint can go down to by including the galaxy-CMB lensing cross correlations from the ACTPol and Planck experiments.\n\n###### pacs:\n98.80.-k, 98.62.Sb, 98.65.-r\n\n## I Introduction\n\nPrimordial non-Gaussianities have been intensively discussed, because any detection of them offers an important window into the early Universe. Standard single-field slow-roll inflation models predict small non-Gaussianity Mukhanov and Chibisov (1981); Allen et al. (1987); Gangui et al. (1994); Maldacena (2003); Acquaviva et al. (2003), so that the detection of large non-Gaussianity may turn down the standard model and suggest physics beyond the standard model. The most popular method to hunt for primordial non-Gaussianities is to measure higher order correlation functions of the cosmic microwave background (CMB) anisotropies such as the the three-point correlation function (bispectrum) and the four-point one (trispectrum). Non-vanishing signals of these higher order correlations may predict the presence of primordial non-Gaussianities. Komatsu et al. (2003); Spergel et al. (2007); Creminelli et al. (2007); Komatsu et al. (2009); Smith et al. (2009); Komatsu et al. (2011a).\n\nRecently, many studies have revealed that the primordial non-Gaussianity of local type affects the large-scale structure (LSS) through the clustering of dark matter halos, and shown the modification of the halo mass function Lo Verde et al. (2008); Matarrese et al. (2000); Verde et al. (2001); D’Amico et al. (2011); Grossi et al. (2009); Yokoyama et al. (2011) and the halo bias Slosar et al. (2008); Dalal et al. (2008); Afshordi and Tolley (2008); Matarrese and Verde (2008); Yokoyama (2011); Gong and Yokoyama (2011); Desjacques et al. (2009), both by numerical simulations and by analytic calculations. Among several types of primordial non-Gaussianities, the local-type non-Gaussianity induces strong scale-dependence of the halo bias Slosar et al. (2008); Dalal et al. (2008); Afshordi and Tolley (2008); Matarrese and Verde (2008). This scale-dependent bias is also powerful tool to constrain the primordial non-Gaussianity from the observations of LSS independently of the method with CMB higher order correlation functions.\n\nUsing this scale-dependent feature in the halo bias, some measurements of the primordial non-Gaussianity have been done in Refs. Slosar et al. (2008); Afshordi and Tolley (2008); Xia et al. (2011). It is expected that future wide and deep surveys, such as Subaru Hyper Suprime-Cam (HSC) survey Miyazaki et al. (2006), Dark Energy Survey (DES) The Dark Energy Survey Collaboration (2005), Large Synoptic Survey Telescope (LSST) LSST Science Collaborations et al. (2009), and so on, will put tighter constraints on the primordial non-Gaussianity, which are expected to be comparable to those from the future CMB observations or more (e.g., Carbone et al. (2008, 2010); Oguri and Takada (2011); Cunha et al. (2010)).\n\nTo get a tighter constraint on the primordial non-Gaussianity, it is important to distinguish the signature of the primordial non-Gaussianity from the other effects more precisely, especially from the linear bias in the limited survey area. Thus, it is better for this purpose to combine unbiased observables which are sensitive to the matter power spectrum in the near Universe, such as weak gravitational lensing of CMB and galaxy lensing shear.\n\nCross correlations with complementary probes are expected to provide additional information on top of their respective auto correlations. The cross correlation between CMB and LSS is known to give information about the integrated Sachs-Wolfe (ISW) effect of CMB temperature anisotropy, which generates the secondary anisotropies due to the time variation of the gravitational potential Sachs and Wolfe (1967). Moreover, CMB lensing also has a correlation with LSS since the gravitational lensing of CMB is induced by the gravitational potential produced by LSS, and the galaxy lensing shear as well Jeong et al. (2009).\n\nSince the effects of the CMB lensing are imprinted on small scales, the Wilkinson Microwave Anisotropy Probe (WMAP) satellite has not detected the CMB lensing directly. Recent ground based CMB experiments such as Atacama Cosmology Telescope (ACT), announced the detection of the CMB lensing signal, and an ongoing CMB observation by Planck The Planck Collaboration (2006) or various ground based experiments are expected to detect this signal more precisely. Therefore, we can be sure that the observation of CMB lensing will increase its accuracy and play an important role in observational cosmology in near future surveys.\n\nIn this paper we consider prospects for constraining the primordial non-Gaussianity through the scale-dependent bias from the near future surveys taking into account all auto and cross correlations among CMB, galaxy distribution and galaxy lensing shear. We shall show that galaxy-CMB lensing and galaxy-galaxy lensing cross correlations are particularly fruitful and allow us to improve the constraints on the primordial non-Gaussianity.\n\nThis paper is organized as follows. In section II we briefly review the effects of the primordial non-Gaussianity for large-scale structure and show the modifications to the mass function and bias of dark matter halos. In section III we summarize the observables employed in our analysis and describe the angular power spectra of the cross correlations between CMB and LSS. In section IV we mention the survey design and photometric redshift systematics employed in our analysis. In section V we explain the method and the setup of our analysis. In section VI we show the results particularly focusing on the constraints on the primordial non-Gaussianity. In section VII we discuss the effects of the photometric redshift systematics and the massive neutrino on the constraints. Then we assess the contribution of the cross correlations for the constraints. Moreover, we compare the constraints from some different surveys. Finally, in section VIII we summarize our conclusions. Through this paper we assume a spatially flat Universe for simplicity.\n\n## Ii Primordial non-Gaussianity\n\nDeviations from Gaussian initial conditions are commonly parameterized in terms of the dimensionless parameter and the primordial non-Gaussianity of the local form is described as Komatsu and Spergel (2001); Verde et al. (2000); Gangui et al. (1994)\n\n Φ=ϕ+fNL(ϕ2−⟨ϕ2⟩), (1)\n\nwhere is the curvature perturbation and is a Gaussian random field. On the subhorizon scale, is related to the Newtonian gravitational potential as .\n\nThe existence of the primordial non-Gaussianity, , indicates that the initial density field is positively or negatively skewed. Furthermore, the fact that the non-Gaussianity affects the clustering of dark matter halos or galaxies allows us to constrain on the non-Gaussianity from large-scale structure surveys. In particular, the local-type non-Gaussianity described by Eq. (1) induces a scale-dependent enhancement of the halo/galaxy power spectrum.\n\nIn the presence of the primordial non-Gaussianity, the mass function of clustering halos is modified and we adopt a non-Gaussian correction factor of the halo mass function based on the Edgeworth expansion Lo Verde et al. (2008):\n\n dn/dMdnG/dM=1+σMS36(ν2−3ν)−16d(σMS3)dlnν(ν−1ν), (2)\n\nwhere is the skewness of the density field which is proportional to , is the rms of the linear density field smoothed on mass scale , is defined as and is the critical linear overdensity. is the mass function in the non-Gaussian case and is the one in the Gaussian case. For the Gaussian one, we adopt a model of Warren Warren et al. (2006).\n\nRecent studies have shown that the local-type primordial non-Gaussianity produces a scale-dependent enhancement of the clustering of halo on large-scales,\n\n Pg(M,z,k)=b2G(M,z)P(k,z)→[bG+Δb(M,z,k)]2P(k,z), (3)\n\nwhere is the galaxy power spectrum, is the matter power spectrum, is the bias in the Gaussian case and is the non-Gaussian correction of the halo bias described as Desjacques et al. (2009)\n\n Δb(M,z,k)=3Ωm,0H20k2T(k)D(z)fNLδc(bG(M,z)−1)−νδcddν(dn/dMdnG/dM). (4)\n\nHere, and are the matter energy density normalized by the critical density and the Hubble parameter at present, is the linear growth rate normalized to the scale factor in the matter-dominant era and is the transfer function of linear matter density fluctuations. For the halo bias in the Gaussian case , we assumed the form presented by Sheth Sheth et al. (2001).\n\n## Iii Angular power spectrum\n\nHere we briefly review the auto and cross correlations of various cosmological observables and their angular power spectra. In this paper we take into account CMB temperature () anisotropies, -mode polarization () and CMB lensing potential () for CMB observables and galaxy distribution (g) and weak lensing shear () for LSS observables.\n\n### iii.1 Integrated Sachs-Wolfe (ISW) effect\n\nThe decay of the Newtonian potential due to the presence of dark energy produces a differential gravitational redshift, and this effect is called the late-time integrated Sachs-Wolfe (ISW) effect. In a flat Universe the presence of ISW effect is a signature of dark energy, and induces a non-vanishing cross correlation between CMB temperature and large-scale structure measurements, such as galaxy distribution, weak lensing field and so on.\n\nThe contribution of the ISW effect to the CMB temperature field can be written as\n\n ΘISW(^n)=ΔTISW(^n)TCMB=−2TCMB∫χ∗0dχ˙Φ(χ^n,χ), (5)\n\nwhere is the mean temperature of the CMB, is the direction to the line of sight, is the comoving distance and denotes the distance to the last scattering surface. is the gravitational potential and a dot denotes a derivative with respect to the conformal time.\n\nThe angular power spectrum of the cross correlation between CMB temperature through ISW effect and the other measurements can be written as\n\n CTXℓ=2π∫k2dkPΦ(k)ΔISWℓ(k)ΔXℓ(k), (6)\n\nwhere\n\n ΔISWℓ(k)=3Ωm,0H20∫z∗0dzddz{D(z)a(z)}T(k)jℓ(kχ(z)), (7)\n\nis the primordial power spectrum of as a function of the wave number and is the tilt of the primordial power spectrum. The functions and are the transfer function and the growth rate for linear matter density fluctuations, respectively, and is a spherical Bessel function. The kernel is for the other measurements, namely, CMB lensing potential, galaxy distribution and weak lensing shear in this paper; , respectively.\n\nThe noise spectra of CMB include detector noise and residual foreground contamination. Here, we assume the ideal condition that foreground contamination can be completely removable and include only Gaussian random detector noise of the form Knox (1995)\n\n NT,Pℓ=[∑ν{(θFWHMΔT,P)−2e−ℓ(ℓ+1)θFWHM/8ln2}]−1, (8)\n\nwhere is the spatial resolution of the beam and represents the sensitivity to the temperature and polarization per pixel, respectively. These values are given for each of the frequency bands of channels and we show the values for two CMB experiments such as Planck The Planck Collaboration (2006) and ACT with new polarization sensitive receiver (ACTPol) Niemack et al. (2010) in Table 1.\n\n### iii.2 CMB lensing potential\n\nCMB photons are deflected due to the gravitational potential produced by the large-scale structure on the way propagating to us (e.g., Ref. Lewis and Challinor (2006)). The relationship between the lensed temperature anisotropy and the unlensed one is given by the deflection angle as . The deflection is related to the line of sight projection of the gravitational potential as , where\n\n ψ(^n)=−2∫χ∗0dχχ∗−χχ∗χΨ(χ^n,χ). (9)\n\nHere, is the (effective) lensing potential.\n\nThe angular power spectrum of the lensing potential can be written as\n\n Cψℓ=2π∫k2dkPΦ(k)[Δψℓ(k)]2, (10)\n\nwhere\n\n Δψℓ(k)=3Ωm,0H20∫χ∗0dχχ∗−χχ∗χT(k)D(z(χ))a(χ)jℓ(kχ). (11)\n\nThe lensing potential can be reconstructed with quadratic statistics in the temperature and polarization data that are optimized to extract the lensing signal. To reconstruct the lensing potential, one needs to use the non-Gaussian nature imprinted into the lensed CMB statistics, and the noise of the lensing potential can be estimated as the reconstruction error Hu and Okamoto (2002); Okamoto and Hu (2003). In this paper, we estimate the noise spectrum of lensing potential following the technique developed in Okamoto and Hu (2003) optimally combining the temperature and polarization fields.\n\n### iii.3 Galaxy distribution\n\nThe luminous sources such as galaxies must be the most obvious tracers of the large-scale structure in the linear regime, and the projected density contrast of the galaxies can be written as\n\n δg,i(^n)=∫∞0dzbeff(z,k)ni(z)nAiδ(χ(z)^n,z), (12)\n\nwhere the subscript represents the -th redshift bin. represents the matter density fluctuation, and and are the galaxy redshift distribution and the total number of galaxies per steradian in the -th redshift bin. The function is the weighted effective halo/galaxy bias defined as\n\n beff(z,k)=[∫∞MobsdMdndM]−1∫∞MobsdMb(M,z,k)dndM, (13)\n\nwhere is the observable mass threshold, which is the minimum mass of the galaxy we can observe, and we take the value to be . The function and are the halo mass function and the halo bias in the case of the non-Gaussian initial condition defined in Eqs. (2) and (3), respectively. We show the dependence of on the redshift and the wave number with different mass thresholds and in Fig. 1.\n\nThe angular power spectrum of the galaxy distribution between -th and -th redshift bins can be written as\n\n Cgigjℓ=2π∫k2dkPΦ(k)Δgiℓ(k)Δgjℓ(k), (14)\n\nwhere\n\n Δgiℓ(k)=∫dzbeff(z,k)ni(z)nAiT(k)D(z)jℓ(kχ). (15)\n\nTo estimate the signal-to-noise ratios and errors in parameter determination for each survey, we need to describe the noise contribution due to the finiteness in the number of sources associated with source samples. We can write the noise spectra from the shot noise as\n\n Ngigjℓ=δij1¯ni, (16)\n\nwhere is the mean surface density of sources per steradian in the -th redshift bin.", null, "Figure 1: The effective weighted bias defined in Eq. (13) as a function of redshift z (Top) and as a function of wave number k (Bottom). (Top) We plot the Gaussian case (fNL=0) for the values logMobs=11.2,11.7,12.2, respectively, and the k dependence does not appear in this case. (Bottom) We plot the non-Gaussian case (fNL=50,100) at redshift z=0.5,1.0,2.0 as indicated, and the value logMobs is fixed to be logMobs=11.7.\n\n### iii.4 Weak lensing shear\n\nThe weak lensing shear (equivalently the convergence in the weak lensing limit) is a weighted integral of the density field of sources, which is directly related to the source galaxy redshift distribution. The average convergence of a light ray bundle from sources in the -th redshift bin is written as\n\n κi(^n)=∫∞0dχWi(χ)δ(χ^n,χ), (17)\n\nwhere is the convergence weight function of kernel defined as\n\n Wi(χ(z))=3Ωm,0H202χ(z)a(z)∫∞zdz′ni(z′)nAiχ(z′)−χ(z)χ(z′). (18)\n\nHere is the distance to the lens and is the one to the source.\n\nThe angular power spectra of the weak lensing shear between -th and -th redshift bins can be written as\n\n Cγiγjℓ=2π∫k2dkPΦ(k)Δγiℓ(k)Δγjℓ(k), (19)\n\nwhere\n\n Δγiℓ(k)=∫dzWi(z)T(k)D(z)jℓ(kχ). (20)\n\nThe measurement of the shear from galaxy images has some uncertainties, one of which mainly comes from the intrinsic shape ellipticities of galaxies. The galaxy shapes can be treated statistically through a shape noise contribution and the noise spectra can be written as\n\n Nγiγjℓ=δijσ2γ¯ni, (21)\n\nwhere is the intrinsic galaxy shear. In this paper, we assume the intrinsic galaxy shear to be as the empirically derived value Bernstein and Jarvis (2002) for all surveys.", null, "Figure 2: The angular power spectra for galaxy-CMB lensing (giψ; Top), galaxy-galaxy lensing (giγj; Middle), and CMB lensing-galaxy lensing (ψγi; Bottom). Here the subscripts i, j represent the redshift bin and we divided into 5 redshift bins for galaxy distribution (g) and cosmic shear (γ). The angular power spectra shown here are i=j=1,3,5 from left to right, respectively. The boxed bars are the errors of the power spectra assuming HSC, Planck and/or ACTPol, and we adopt the logarithmic binning for illustrative purpose. We also plot the angular power spectra in the non-Gaussian case, fNL=50,100 and Mobs[h−1M⊙]=1011.2,1012.2. For comparison, we plot the contribution of the photo-z error, σ(i)z=0.03 for each bin.\n\n### iii.5 Cross correlation angular power spectrum\n\nThe effect of the primordial non-Gaussianity stands out the most in the galaxy-galaxy auto correlation (gg) through the bias parameter. As many previous works show, almost all the constraints on the primordial non-Gaussianity come from the galaxy-galaxy power spectrum Slosar et al. (2008); Afshordi and Tolley (2008); Xia et al. (2010a, b, 2011). The cross correlation power spectra, e.g., CMB Temperature-galaxy cross correlation (g), however, provide extra information and improve the errors of the parameters.\n\nIn our previous analysis Takeuchi et al. (2010), we paid a particular attention to the CMB lensing-galaxy cross correlation (g), and estimated the contribution to the constraint on the primordial non-Gaussianity. Here, we improve our analysis by adding the galaxy lensing shear, which may also correlated with galaxy distribution and CMB lensing, and estimate the errors of determining cosmological parameters including any possible auto and cross correlations.\n\nFig. 2 shows an example of the cross correlation angular power spectra, for galaxy-galaxy lensing (g), galaxy-CMB lensing (g) and CMB lensing-galaxy lensing (). The boxes around the curve show the expected measurement errors for HSC- survey (for an illustrating purpose, we take the logarithmic binning, as ). For the cross correlations with CMB lensing, we show the errors for two cases that one is for Planck and the other is Planck with ACTPol.\n\n## Iv Survey design\n\nThe errors in determining cosmological parameters from observations of LSS depend a great deal on the survey design, such as the survey region, the mean redshift and photometric redshift errors. Here we summarize the survey design employed in our analysis.\n\n### iv.1 Redshift distribution of galaxies\n\nWe assume the redshift distribution of galaxy samples with a function of the form:\n\n n(z)=¯ngβΓ[(α+1)/β]zαzα+10exp[−(zz0)β], (22)\n\nwhere is the mean number density of source galaxies at all redshifts, , and are free parameters. We adopt , , and the parameter is related to the mean redshift as\n\n zm=∫dzzn(z)¯ng=z0Γ[(α+2)/β]Γ[(α+1)/β], (23)\n\nand is determined in such a way that the mean redshift fits the value in Table 2 for each survey. The normalization of the redshift distribution function is fixed by the total number density of galaxies:\n\n nA=∫∞0dzn(z). (24)\n\n### iv.2 Photometric redshift systematics\n\nIn the galaxy imaging survey whose observables are galaxy distribution and galaxy shear, we measure a large number of galaxies so that the systematic uncertainties play a correspondingly important role with statistical errors. Although systematics may include many effects and these effects depend on the details of the observations Bernstein (2009); Das et al. (2011), we include only the effect of photometric redshift errors.\n\nImperfect calibration of photometric redshifts induces a residual scatter and bias with respect to the true redshifts, and uncertainties in the redshifts distort the volume element. Following the photometric redshift model as described in Ma et al. (2006), the probability distribution of photometric redshift given the true redshift , is modeled as a Gaussian distribution\n\n p(zph|z)=1√2πσzexp[−(z−zph−zbias)22σ2z], (25)\n\nwhere and are the scatter and bias, respectively, which are arbitrary function of redshift .\n\nThe best-estimated distribution for objects in the -th photometric redshift bin with , , can be written as\n\n ni(z) = ∫z(i+1)phz(i)phdzphn(z)p(zph|z), (26) = 12n(z)[erf(xi+1)−erf(xi)],\n\nwhere is defined as\n\n xi≡(z(i)ph−z+zbias(z))/√2σz(z). (27)\n\nIn the same way as Eq. (24), the total number density of galaxies in the -th bin becomes\n\n nAi=∫∞0dzni(z). (28)\n\nWe assume a fiducial redshift scatter and bias following Das et al. (2011) as\n\n σz(z)=σ(i)z(1+z), (29) zbias(z)=z(i)bias(1+z), (30)\n\nwhere and are defined for each redshift bin. We set the fiducial values as , for each redshift bin and all surveys.\n\n## V Forecasts\n\nWe estimate the parameter errors using the Fisher matrix formalism. We summarize the Fisher matrix formalism taking into account the cross correlation between CMB and LSS, and we describe the setup for the CMB and LSS observables.\n\n### v.1 Fisher matrix formalism\n\nUnder the assumptions that the observables follow the Gaussian statistics, we can obtain the information on a set of parameters from the Fisher matrix written as Tegmark et al. (1997)\n\n Fℓ,ij=fskyℓmax∑ℓmin(2ℓ+1)2Tr[Cℓ,iC−1ℓCℓ,jC−1ℓ], (31)\n\nwhere is the sky coverage of the experiment, is the signal plus noise covariance matrix, and is the derivative of with respect to the parameter .\n\nFor CMB experiments, we consider two cases: that one is the constraint from Planck and the other is from Planck with ACTPol. It is well known that combining the results of the satellite CMB experiment with the ground based one can improve the constraints, e.g., combining WMAP with ACTDunkley et al. (2010), ACBARReichardt et al. (2009) or so on. For these two cases, we define the total Fisher matrix as below, respectively, under the assumption for the size of survey area as . Here , and are the sky coverage of the ACTPol, the LSS and the Planck surveys, respectively, and we define the overlap region between CMB experiments and LSS surveys as .\n\n• LSS + Planck:\n\n Fℓ,ij=fCrossskyℓLSSmax∑ℓmin=2FCrossℓ,ij+fPlanckskyℓCMBmax∑ℓLSSmax+1FCMBℓ,ij+(fPlancksky−fCrosssky)ℓLSSmax∑ℓmin=2FCMBℓ,ij, (32)\n• LSS + Planck + ACTPol:\n\n Fℓ,ij=fCrossskyℓLSSmax∑ℓmin=2FCrossℓ,ij∣∣ACTPol+fACTPolskyℓCMBmax∑ℓLSSmax+1FCMBℓ,ij∣∣ACTPol+(fLSSsky−fCrosssky)ℓLSSmax∑ℓmin=2FCrossℓ,ij∣∣Planck+(fPlancksky−fLSSsky)ℓLSSmax∑ℓmin=2FCMBℓ,ij∣∣Planck+(fPlancksky−fACTPolsky)ℓCMBmax∑ℓLSSmax+1FCMBℓ,ij∣∣Planck, (33)\n\nwhere\n\n FCrossℓ,ij = (2ℓ+1)2Tr[CCrossℓ,i(CCrossℓ)−1CCrossℓ,j(CCrossℓ)−1], (34) FCMBℓ,ij = (2ℓ+1)2Tr[CCMBℓ,i(CCMBℓ)−1CCMBℓ,j(CCMBℓ)−1],\n\nand different superscripts for and represent different observations or CMB experiments, e.g., and are the maximum multipole we can take for the CMB experiment and the LSS survey, respectively. Here is the minimum multipole we can take and we use in all cases. We summarize these values in Table 4.\n\nThe covariance matrix and each of its matrix elements is defined as\n\n [CCross,CMBℓ]XY = CXYℓ+NXYℓδXY, (36) where X,Y = {T,E,ψ,gi,γi(for Cross)T,E,ψ(for CMB),\n\nis the angular power spectrum and is the noise spectrum for each auto or cross correlation. We defined and as and in Eq. (8), and in Eqs. (16) and (21), respectively, and is the noise spectrum of CMB lensing potential we estimate following the technique developed in Okamoto and Hu (2003). Then we assume that there is no correlation of noises between the different observables and different redshift bins. Moreover, we assume that -mode polarization () has correlation only with temperature anisotropies () because -mode polarization can be generated through the Thomson scattering dominantly on the last scattering surface, .\n\nIncidentally the assumption that is not strictly correct Lewis et al. (2011) because the large-scale polarization -mode generated by scattering at reionization correlates with sources of CMB lensing potential over long distance. Moreover, if the galaxies are at high-redshift, the assumption that is also not correct Challinor and Lewis (2011). However the influence of these assumptions for our results, especially constraints on the primordial non-Gaussianity, can be small because sample galaxies in our analysis are at low redshift.\n\nHere we explain the detail of our Fisher matrices given in Eqs. (32) and (LABEL:eq:Fisher_II). In Eq. (32) the first term is responsible for the cross correlation between LSS and CMB, the second one is for CMB observables at the higher multipoles than the LSS survey can probe, and the last one is for CMB observables in the remaining survey area of CMB which does not overlap with the LSS survey. In Eq. (LABEL:eq:Fisher_II) the first term is responsible for the cross correlation between LSS and CMB with ACTPol, the second one is for CMB observables with ACTPol at the higher multipoles than the LSS survey can probe, the third one is for the cross correlation between LSS and CMB with Planck in the overlapping region which does not overlap with ACTPol, the forth one is for CMB observables with Planck in the region which does not overlap with the LSS survey, and the last one is for CMB observables with Planck at the higher multipoles than the LSS survey can probe in the region which does not overlap with ACTPol.\n\nIn our analysis, the total number of non-zero angular power spectra is 81 for the full cross correlation case (), while it is 5 for the only CMB case ().\n\n### v.2 Setup\n\nGiven the measurement design of the surveys, we can estimate the errors in determining the cosmological parameters using the Fisher matrix formalism. The formalism tells us how well the given surveys can measure the cosmological parameters around fiducial cosmological model. Therefore, the parameter forecasts by Fisher matrix formalism depend on the choice of the fiducial model and the number of free parameters.\n\nAs for our fiducial cosmological model, we assume a flat CDM model and we include the following 9 cosmological parameters, which is based on the WMAP seven-year results Komatsu et al. (2011b). The density parameters of cold dark matter, baryon and dark energy are , and , respectively; dark energy equation of state parameter is ; the optical depth at reionization is ; and the primordial power spectrum parameters are the spectrum tilt and the amplitude of the primordial power spectrum which is normalized at . We also include the primordial non-Gaussianity of local type modeled by the non-linear parameter . For specifying the galaxy bias, we include the minimum mass of halo hosting the galaxies, for which we can observe as a free parameter. The fiducial values are\n\n {100Ωbh2, Ωch2, ΩΛ, τ, nS, Δ2R, w, fNL, logMobs}={0.20, 0.1109, 0.72, 0.086, 0.96, 2.4×10−9, −1, 0, 11.7}. (37)\n\nThroughout this paper we assume a spatially flat Universe, and the Hubble parameter is adjusted to keep our Universe flat when we vary .\n\nTo calculate the angular power spectra including non-linear effects on the angular power spectrum of the galaxy distribution, cosmic shear and lensing potential, we use the CAMB code Lewis et al. (2000) and the HALOFIT code Smith et al. (2003). We, however, want to remove the burden of the uncertainty of the non-linear calculation as much as possible, so our estimation preferably is based on the information from large-scale for LSS where the linear prediction is reliable.\n\nIn our estimation, we include the information from temperature anisotropies (), -mode polarization () and reconstructed lensing potential () for CMB. The range of multipoles are and the survey area is taken as for Planck and for ACTPol, respectively. On the other hand, for the galaxy survey () and galaxy weak lensing survey (), the ranges of multipole are and the survey areas are for both of them with HSC. Furthermore we take into account all the cross correlation we can consider and we assume the optimal condition that there is no correlation between different patches, so that the area having a correlation between CMB and LSS corresponds to the overlapped survey area. We summarize the values we use in the following calculation in TABLE 4.\n\n## Vi Result\n\n### vi.1 Signal-to-Noise ratio\n\nTo see the errors in the cross correlation power spectra more quantitatively, we estimate the signal-to-noise ratio () for each -bin and the cumulative (). We define the for a cross correlation between X and Y, following Peiris and Spergel (2000), as\n\nfor each -bin:\n\n (SN)2(ℓ)≡fskyℓ(i)max∑ℓ(i)min(2ℓ+1)×(CXYℓ)2(CXXℓ+NXXℓ)(CYYℓ+NYYℓ)+(CXYℓ)2, (38)\n\nstacked :\n\n (SN)2(≤ℓmax)≡fskyℓmax∑ℓ=2(2ℓ+1)×(CXYℓ)2(CXXℓ+NXXℓ)(CYYℓ+NYYℓ)+(CXYℓ)2, (39)\n\nwhere and are the maximum and minimum multipoles of the -th multipole bin, respectively, and , are the fiducial and noise spectra, respectively. The index represents .\n\nFigure  3 shows an example of for each given by Eq. (38) and cumulative by Eq. (39), for the galaxy-galaxy lensing (g), galaxy-CMB lensing (g) and CMB lensing-galaxy lensing () cross correlations. For the galaxy-CMB lensing and CMB lensing-galaxy lensing with HSC-Planck experiments, the amplitude of decreases at high- bins and the stacked saturates due to the noise of CMB lensing at small scales. On the other hand, we can expect the lager at high- bins for the case with HSC-ACTPol. The amplitude of at low- bins where the signature of the primordial non-Gaussianity shines out is very low in all the cases. However, comparing galaxy-CMB lensing with galaxy-galaxy lensing signals, the amplitude of the former is larger than the latter in high-redshift bins and the difference becomes even greater for the with HSC-ACTPol.", null, "Figure 3: Signal-to-Noise ratio for some angular power spectra. We show the S/N for each bin (box) and stacked S/N (line), respectively. Top panels are for galaxy-CMB lensing (giψ) angular power spectra, Center ones are for galaxy-galaxy lensing (giγj), and Bottom ones are for CMB lensing-galaxy lensing (ψγj) based on the fiducial model of Fig. 2.", null, "Figure 4: Projected 1σ(68%) confidence constraints in some parameter spaces for the fν≠0 model. We show contours from CMB and galaxy distribution (black thick); from CMB, galaxy distribution and CMB lensing (red dashed); from CMB, galaxy distribution and galaxy lensing (green dot-dashed); and from all the observables (blue thin). All auto and cross correlations between these observables are taken into account for the constraints. Here we assume the HSC survey and Planck experiment (Left) or HSC and combination of Planck and ACTPol (Right).", null, "Figure 5: Projected 1σ(68%) confidence constraints in some parameter spaces from Planck and HSC experiments including auto and cross correlations between CMB, CMB lensing, galaxy distribution and galaxy lensing. We show the contours with or without the photometric redshift scatter for the ΛCDM model, the contours without the photometric redshift scatter for the fν≠0 model and the contour with the photometric redshift scatter for the fν=0 model.\n\n### vi.2 Constraints on the primordial non-Gaussianity\n\nWe estimate the errors in the determination of cosmological parameters for the HSC- survey using the Fisher matrix formalism, and show the main results, namely, the 1 confidence limit constraints in Fig. 4 and Table 5, in which we consider 10 cosmological parameters: the fraction of the massive neutrino density parameter to the matter density parameter in addition to the nine cosmological parameters defined in Sec. V.2.\n\nThe simplest case, which is from only galaxy clustering, puts the constraint on as , and the constraint can be improved to by combining the CMB-only result though CMB has no information about primordial non-Gaussianity on the level of the 2-point function without cross correlations with galaxy clustering. This is because the information from CMB helps to determine the galaxy bias by breaking degeneracies with other cosmological parameters, and then the degeneracy between and can be broken effectively. Hence the constraint on is also improved dramatically after combining CMB information, which can be seen in Table 5, and these tendencies have been seen in our previous analysis Takeuchi et al. (2010).\n\nWe show four cases to see the improvement by adding the different observables in Fig. 4. In the first case we use CMB and galaxy distribution (CMB + g); in the second case we add CMB lensing to the first case (CMB + g + ); in the third case we add shear to the first case (CMB + g + ); and in the last case we use all the information available. We take into account all the available power spectra. The selection of auto and cross correlations in Fig. 4 and Table 5 corresponds to each other in each case. We obtain the constraints on as with Planck and HSC. Moreover, we can improve the constraint by including ACTPol as , thanks to the galaxy-CMB lensing cross correlations.\n\n## Vii Discussion\n\n### vii.1 Selection of the fiducial model\n\nWe assume imaging surveys for the LSS galaxy surveys, and we have to take into account the influence of the various systematics, e.g.,, magnification effects due to gravitational lensing Namikawa et al. (2011), photometric redshift(photo-) errors Ma et al. (2006) and so on (see, for example, Bernstein (2009); Das et al. (2011)). Moreover, as mentioned in the previous section, the parameter forecasts by Fisher matrix formalism depend on the choice of the fiducial model and free parameters. In Fig. 5, we summarize the effects of selecting fiducial models.\n\n#### vii.1.1 Photometric redshift error\n\nFor the constraint on , any significant difference is not found between with and without the photometric redshift scatter systematics. This is because the redshift scatter changes the overall amplitude of the galaxy distribution (g) and cosmic shear () as shown in Fig. 2. On the other hand, the effect of non-Gaussianity, , emerges only at large angular scales, and it can be distinguishable. However, the effects of the photometric redshift error are significant for the parameters which are determined through the information about the redshift evolution such as and . Although the effect of the parameter is to change the bias parameter and is similar to the effect of the redshift scatter, a significant difference is not found in the figure.\n\n#### vii.1.2 Massive neutrino\n\nVarious experiments, such as ground based experiments of neutrino oscillation, predict the non-zero neutrino mass Schwetz et al. (2008); Maltoni et al. (2004). Therefore, we need to include the mass of neutrinos for a more accurate estimation of the cosmological parameters. There are, however, some debatable subtle arguments about taking the mass of neutrinos into account in models for the mass function and the halo bias. These models have been tested by N-body simulations without massive neutrinos and are not guaranteed enough for cosmological models with massive neutrinos. The analytic formula for the scale-dependent bias presented in Eq. (4) is also for models without massive neutrinos.\n\nFor the mass function, it is found that the influence of massive neutrinos is very small Ichiki and Takada (2011). Thus, we just assume that the halo mass function and halo bias models can be applied even if the massive neutrinos are included.\n\nComparing the results of and models in Fig. 5, a significant difference can be seen in the constraint on . The existence of massive neutrinos affects the large-scale structure formation through its large velocity dispersion and alter the amplitude of the matter power spectrum. This effect is similar to the effect from and these two parameters are strongly degenerated with each other as shown in Fig. 4. Note that the degrade of the constraint on in the case of the model comes from the strong degeneracy between them and we have confirmed that there is little change in the constraint if we fix the value of (and do not take it as a free parameter). For the constraints on itself, however, the difference of the fiducial models whether or not is not so significant.\n\nIn summary, focusing on the constraint of , the selection of the fiducial model makes little impact on the result. On the other hand, the constraints on some other parameters depend on the fiducial model, especially on the existence of neutrino mass and photometric redshift error.", null, "Figure 6: Same as Fig. 4 but we highlight the contribution from the cross correlations to the constraints. The base constraints are from CMB(TT,EE,TE), galaxy distribution (gg), CMB lensing (ψψ) and galaxy lensing (γγ) auto correlations (black thin line). The other contours show improvements by including cross correlation as indicated in the figure. Here we consider the HSC survey and Planck with and without ACTPol experiment (left and right panels, respectively).\n\n### vii.2 Contribution of cross correlations\n\nNow let us discuss the contribution from ACTPol experiment which will extract the information of CMB lensing more efficiently than Planck.\n\nAs shown Fig. 4 and Table 5, we find that almost all the constraints on each plane are determined through galaxy lensing information except for and . However, CMB lensing also gives important contributions if the ACTPol experiment is included. Focusing on the constraints on the - plane, both the CMB lensing and galaxy lensing signals improve the constrains slightly by including their cross correlations, though the most of the constraints are determined by the galaxy auto correlation.\n\nWe show how the cross correlations improve the constraints in Fig. 6 and Table 6. We find that most of the constraints are mainly determined through the auto correlations on each plane but we can still gain a little benefit from the cross correlations. By including all cross correlations among CMB, galaxy distribution and galaxy lensing shear, we can expect improvement for the constraint on with HSC and Planck, and improvement with HSC, Planck and ACTPol. In particular, the impact of the cross correlation between galaxy and galaxy lensing (g) is significant, especially in the - plane. This result is consistent with that obtained by Namikawa et al. (2011); Oguri and Takada (2011) and g will play a very important role in the constraint on dark energy parameters.\n\nFinally, to see the impact of cross correlations for the constraint on the primordial non-Gaussianity, let us focus on the constraints on the - plane in Fig. 6. We find that the cross correlation between galaxy and CMB lensing (g) will improve the constraint on when the Planck and ACTPol experiments are combined. However we have little benefit from the cross correlations if we use only Planck for the CMB experiment.\n\n### vii.3 Dependence on mass threshold Mobs\n\nThe parameter reflects the mass threshold we can observe as galaxy and relates to the galaxy bias through Eq. (13). We can interpret from Fig. 1 that the larger value of predicts the larger bias. We show the constraints for the different fiducial value of in Fig. 7. Only in this figure, we plot instead of for the purpose of illustrating the different fiducial models on the same planes.\n\nThe difference which comes from the different fiducial values of appears especially in the constraints on and , while the constraints on the other parameters are not altered so much. This is because the constraints on and come mainly from the galaxy distribution (g), while the constraints of the others come mainly from the other observables. As for the constraints on , the larger value of can lead to a tighter constraint on . The larger value of means picking out the higher mass objects. Because high mass objects exhibit a large bias, the non-Gaussian correction to the bias becomes large. Furthermore, the correction to the mass function also becomes large for high mass objects. For these reasons, the effect of the non-Gaussianity through the effective bias" ]
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https://zbmath.org/?q=an:1231.11030
[ "## On exponentials of exponential generating series.(English)Zbl 1231.11030\n\nThe shuffle product of two formal power series $$\\sum_{n=0}^{\\infty}{\\alpha_nX^n}$$ and $$\\sum_{n=0}^{\\infty}{\\beta_n X^n}$$ with coefficients in a field $$\\mathbb K$$ is defined by $\\sum_{n=0}^{\\infty}{\\gamma_nX^n}:=\\sum_{n=0}^{\\infty}{\\alpha_nX^n} \\operatorname{\\text Ш} \\sum_{n=0}^{\\infty}{\\beta_nX^n}$ where $\\gamma_n=\\sum_{n=0}^{\\infty}{\\binom{n}{k}\\alpha_k \\beta_{n-k}}.$ A result which goes back to Hurwitz shows that the additive group $$(X\\mathbb K [[X]],+)$$ and the shuffle group $$(1+X\\mathbb K [[X]], \\operatorname{\\text Ш} )$$ are isomorphe. The map which gives this isomorphism is the exponential map defined as follows. If $$A=\\sum_{n=1}^{\\infty}{\\alpha_n X^n}$$ and $$B=\\sum_{n=1}^{\\infty}{\\beta_n X^n}$$, then $\\exp_{!}(A):=1+B$ when $\\exp(\\sum_{n=1}^{\\infty}{\\frac{\\alpha_n}{n!} X^n})=1+\\sum_{n=1}^{\\infty}{\\frac{\\beta_n}{n!} X^n}.$\nIn this article, the author proves that the map $$\\exp_{!}$$ also induces a group isomorphism between the subgroup of rational (respectively algebraic) series of $$(X\\mathbb K [[X]], +)$$ and the subgroup of rational (respectively algebraic) series of $$(1+X\\mathbb K [[X]], \\operatorname{\\text Ш} )$$, if $$\\mathbb K$$ is a subfield of the algebraically closed field $$\\overline{\\mathbb F}_p$$ of positive characteristic $$p$$. The author also shows that this result is not true if the field is of characteristic zero.\n\n### MSC:\n\n 11B85 Automata sequences 11B73 Bell and Stirling numbers 11E08 Quadratic forms over local rings and fields 11E76 Forms of degree higher than two 22E65 Infinite-dimensional Lie groups and their Lie algebras: general properties\nFull Text:" ]
[ null ]
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https://papers.neurips.cc/paper/2017/file/4a8423d5e91fda00bb7e46540e2b0cf1-Reviews.html
[ "NIPS 2017\nMon Dec 4th through Sat the 9th, 2017 at Long Beach Convention Center\nPaper ID: 2519 Selective Classification for Deep Neural Networks\n\n### Reviewer 1\n\nThe paper proposes a practical scheme of adding selective classification capabilities to an existing neural network. The method consists of: 1. Choosing a score function that captures how confident the network is in its prediction, analysed are MC-dropout scores for networks trained with dropout and the maximum softmax score for networks with a softmax output with the second performing empirically better. 2. Defining the desired confidence level and error rate. 3. Running a binomial search to establish a score threshold such that with the desired confidence level the classifier will have an error rate smaller than the specified one on the samples it chooses to classify. The procedure uses an existing bound on the true error rate of a classifier based on a small sample estimate (Lemma 3.1) and uses binomial search with a Bonferroni correction on the confidence level (Algorithm 1) to find the score threshold. Experimental results validate the approach and show good agreement between the algorithm inputs (desired error rate) and observed empirical error rates on a test set. The strong points of the paper are the practical nature of it (with the softmax response score function the procedure can be readily applied to any pretrained neural network) and the ease of specifying the algorithm’s desired confidence level and error rate (which is modeled after ref ). While the paper builds on well known concepts, the careful verification of the concepts adds a lot of value. The paper lacks simple baselines, that could showcase the importance of using the binomial search and the bound on the classifier’s error rate. In particular, I would like to know what happens if one chooses the score threshold as the lowest value for which the error rate on a given tuning set is lower than e specified value- would the results be much more different than using the bound from Lemma 3.1? Knowing this baseline would greatly motivate the advanced techniques used in the paper (and would raise my score of this paper). Nitpicks: the Algorithm 1 uses an uninitialized variable r*\n\n### Reviewer 2\n\nSelective classification is the problem of simultaneously choosing which data examples to classify, and subsequently classifying them. Put another way, it’s about giving a classifier the ability to ignore certain data if it’s not confident in its prediction. Previous approaches have focused on assigning a small cost for abstaining. This paper proposes a post-hoc strategy where, if a classifier’s confidence can be accurately gauged, then this confidence is thresholded such that the classifier obtains a guaranteed error rate with high probability. The main novelty with this paper is the proposed SGR algorithm and associated theory. This relies on an ideal confidence function, which is not available in practice, so two methods, SR and MC-dropout are tested. The results are promising, obtaining a low test error with a reasonably high coverage. Getting into specifics: it’s not obvious how you solve Equation (4). I’m assuming it’s a simple line search in 1D, but it would be helpful to be explicit about this. Also, what is the complexity of this whole procedure? It looks like it’s mlog(m)? It’s interesting that mc-dropout performed worse on Imagenet, do you have any intuition as to why this might be the case? It may be helpful to visualize how the confidence functions differ for a given model. I suppose one can easily test both and take the one that works better in practice. As far as I know, there is no explicit validation set for CIFAR-10 and CIFAR-100. They each have 50,000 training points with a separate 10,000-point test-set. Did you split up the test-set into 5,000 points? Or did you use the last batch of the training set for Sm? I think a more proper way to evaluate this would be to use some portion of the last batch of the training sets as validation, and evaluate on the full test set. It would be helpful for you to mention what you did for Imagenet as well; it looks like you split the validation set up into two halves and tested on one half? Why not use the full test set, which I think has 100,000 images? There’s a typo in section 5.3 (mageNet). One point of weakness in the empirical results is that you do not compare with any other approaches, such as those based on assigning a small cost for abstaining. This cost could be tuned to get a desired coverage, or error rate. It’s not clear that a post-hoc approach is obviously better than this approach, although perhaps it is less expensive overall. Overall I like this paper, I think it’s a nice idea that is quite practical, and opens a number of interesting directions for future research.\n\n### Reviewer 3\n\nThe paper addresses the problem of constructing a classifier with the reject option that has a desired classification risk and, at the same time, minimizes the probability the \"reject option\". The authors consider the case when the classifiers and an associate confidence function are both known and the task is to determine a threshold on the confidence that determines whether the classifier prediction is used or rejected. The authors propose an algorithm finding the threshold and they provide a statistical guarantees for the method. Comments: - The authors should provide an exact definition of the task that they attempt to solve by their algorithm. The definition on line 86-88 describes rather the ultimate goal while the algorithm proposed in the paper solves a simpler problem: given $(f,\\kappa)$ find a threshold $\\theta$ defining $g$ in equation (3) such that (2) holds and the coverage is maximal. - It seems that for a certain values of the input arguments (\\delta,r^*,S_m,...) the Algorithm 1 will always return a trivial solution. By trivial solution I mean that the condition on line 10 of the Algorithm 1 is never satisfied and thus all examples will be at the end in the \"reject region\". It seems to me that for $\\hat{r}=0$ (zero trn error) the bound B^* solving equation (4) can be determined analytically as $B^* = 1-(\\delta/log_2(m))^{1/m}$. Hence, if we set the desired risk $r^*$ less than the number $B^* = 1-(\\delta/log_2(m))^{1/m}$ then the Algorithm 1 will always return a trivial solution. For example, if we set the confidence $\\delta=0.001$ (as in the experiments) and the number of training examples is $m=500$ then the minimal bound is $B^*=0.0180$ (1.8%). In turn, setting the desired risk $r^* < 0.018$ will always produce a trivial solution whatever data are used. I think this issue needs to be clarified by the authors. - The experiments should contain a comparison to a simple baseline that anyone would try as the first place. Namely, one can find the threshold directly using the empirical risk $\\hat{r}_i$ instead of the sophisticated bound B^*. One would assume that the danger of over-fitting is low (especially for 5000 examples used in experiments) taking into account the simple hypothesis space (i.e. \"threshold rules\"). Without the comparing to baseline it is hard to judge the practical benefits of the proposed method. - I'm missing a discussion of the difficulties connected to solving the numerical problem (4). E.g. which numerical method is suitable and whether there are numerical issues when evaluating the combinatorial coefficient for large m and j. Typos: - line 80: (f,g) - line 116: B^*(\\hat{r},\\delta,S_m) - line 221: \"mageNet\"" ]
[ null ]
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https://www.mvtec.com/doc/halcon/1805/en/toc_tools_geometry.html
[ "Operators\n\nGeometry\n\nList of Operators\n\nangle_ll\nCalculate the angle between two lines.\nangle_lx\nCalculate the angle between one line and the horizontal axis.\napply_distance_transform_xld\nDetermine the pointwise distance of two contours using an XLD distance transform.\nclear_distance_transform_xld\nClear a XLD distance transform.\ncreate_distance_transform_xld\nCreate the XLD distance transform.\ndeserialize_distance_transform_xld\nDeserialize an XLD distance transform.\ndistance_cc\nCalculate the distance between two contours.\ndistance_cc_min\nCalculate the minimum distance between two contours.\ndistance_cc_min_points\nCalculate the minimum distance between two contours and the points used for the calculation.\ndistance_contours_xld\nCalculate the pointwise distance from one contour to another.\ndistance_lc\nCalculate the distance between a line and one contour.\ndistance_lr\nCalculate the distance between a line and a region.\ndistance_pc\nCalculate the distance between a point and one contour.\ndistance_pl\nCalculate the distance between one point and one line.\ndistance_pp\nCalculate the distance between two points.\ndistance_pr\nCalculate the distance between a point and a region.\ndistance_ps\nCalculate the distances between a point and a line segment.\ndistance_rr_min\nMinimum distance between the contour pixels of two regions each.\ndistance_rr_min_dil\nMinimum distance between two regions with the help of dilation.\ndistance_sc\nCalculate the distance between a line segment and one contour.\ndistance_sl\nCalculate the distances between a line segment and a line.\ndistance_sr\nCalculate the distance between a line segment and one region.\ndistance_ss\nCalculate the distances between two line segments.\nget_distance_transform_xld_contour\nGet the reference contour used to build the XLD distance transform.\nget_distance_transform_xld_param\nGet the parameters used to build an XLD distance transform.\nget_points_ellipse\nCalculate a point of an ellipse corresponding to a specific angle.\nintersection_circle_contour_xld\nCalculate the intersection points of a circle or circular arc and an XLD contour\nintersection_circles\nCalculate the intersection points of two circles or circular arcs\nintersection_contours_xld\nCalculate the intersection points of two XLD contours\nintersection_line_circle\nCalculate the intersection points of a line and a circle or circular arc\nintersection_line_contour_xld\nCalculate the intersection points of a line and an XLD contour\nintersection_lines\nCalculate the intersection point of two lines\nintersection_segment_circle\nCalculate the intersection points of a segment and a circle or circular arc\nintersection_segment_contour_xld\nCalculate the intersection points of a segment and an XLD contour\nintersection_segment_line\nCalculate the intersection point of a segment and a line\nintersection_segments\nCalculate the intersection point of two line segments\nprojection_pl\nCalculate the projection of a point onto a line." ]
[ null ]
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https://answers.everydaycalculation.com/simplify-fraction/3276-2521
[ "Solutions by everydaycalculation.com\n\n## Reduce 3276/2521 to lowest terms\n\n3276/2521 is already in the simplest form. It can be written as 1.299484 in decimal form (rounded to 6 decimal places).\n\n#### Steps to simplifying fractions\n\n1. Find the GCD (or HCF) of numerator and denominator\nGCD of 3276 and 2521 is 1\n2. Divide both the numerator and denominator by the GCD\n3276 ÷ 1/2521 ÷ 1\n3. Reduced fraction: 3276/2521\nTherefore, 3276/2521 simplified is 3276/2521\n\nMathStep (Works offline)", null, "Download our mobile app and learn to work with fractions in your own time:" ]
[ null, "https://answers.everydaycalculation.com/mathstep-app-icon.png", null ]
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https://deque.blog/2017/06/25/alias-method-and-data-transformation/
[ "This post is dedicated to describing a wonderful and beautiful small algorithm that is not widely known. It allows to pick a random element among an enumerated distribution of elements, where each element is associated a weight.\n\nThis need is frequently encountered, for instance in property based testing libraries. In test.check, it correspond to the library function frequency which allows to select a random generator based on frequency of occurence (the weight).\n\nWe will first describe two classic methods to solve this problem before jumping to the Alias Method, a very efficient algorithm. We will describe how it works and give one possible implementation.\n\nWe will end this post by taking some distance and discuss the importance of data transformations to build efficient algorithms, and one reason that might explain why tend to fail to see these transformation so often in our everyday code.\n\n### Stating the problem\n\nAs input, we have a bunch of elements xs and each element is associated a weight. This weight is proportional to the probability of picking that element among xs. We call this kind of distribution an enumerated distribution.\n\nOur algorithm should output a random generator such that:\n\n• Each time we call it, it outputs an element from our elements xs\n• The probability of taking x from xs is P(x) = Weight(x) / TotalWeight\n• The TotalWeight is the sum of Weight(x) for all x of the elements xs\n\nWe will name the function that implements this algorithm (and returns the desired generator) enumerated-distribution-gen.\n\n### Usage example\n\nLet us take as input a map associating to the keyword :a the weight 1, to :b the weight 2 and to :c the weight 1. We expect our enumerated-distribution-gen function to output a random generator that will:\n\n• Output :a 25% of the time\n• Output :b 50% of the time\n• Output :c 25% of the time\n\nHere is how it would translate in term of Clojure code:\n\nWe will now go through different implementation of this algorithm.\n\n### Linear naive algorithm\n\nThe most naive algorithm consist in computing the sum of the weights, which we will name total-weight and to randomly pick a number between 0 and this total-weight (excluded). We then linearly scan the collection to find the appropriate match.\n\nFor instance, if we pick as input {:a 1, :b 2, :c 1}, we compute its total-weight, yielding 4. Each random generation will randomly generate an double d between 0 and 4, and scan the collection to find the correct match:\n\n• If d is in [0, 1), we output :a\n• If d is in [1, 3), we output :b\n• If d is in [3, 4), we output :c\n\n###### Implementation\n\nFinding the correct match is rather simple: we subtract to d the weight of each element. The first element that makes d strictly negative is the one we select.\n\nThis function makes use of the sum-weights helper function that sums the weight of our input elements:\n\nWe can run our function a few time to see how it behaves:\n\n###### Alternate implementations\n\nEquivalently, we can precompute the cumulative sum of the weights, and select the first cumulative weight that is higher than the number d we generate. In terms of algorithm complexity, these implementations are equivalent to the one provided above:\n\n• O(N) pre-processing time (summing the weights)\n• O(N) processing time at each rand (scanning)\n\nTwo implementations (from Rich Hickey and Stuart Halloway) of this variant of the naive algorithm are shown in this stack overflow thread.\n\n### Binary search\n\nThe implementation based on cumulative weights gives us some insight on how we can improve our algorithm. Since cumulative weights form an increasing sequence of weights, the weights are sorted and so we can binary search into it.\n\nBased, on binary search, we can improve our algorithm complexity to:\n\n• O(N) pre-processing time (summing the weights)\n• O(log N) processing time at each rand (binary search)\n\nIn case the random generator output by enumarated-distribution-gen is used a lot of times, this can yield some interesting performance boost. We will not delve further into this. The implementation is very similar to the previous one, and is left as an exercise for the reader.\n\n### Alias method\n\nWe will now cover the alias method, an algorithm that allows to randomly pick an element from an enumerated distribution in O(1), given a typical O(N log N) pre-processing time.\n\nIn this section, we will describe the algorithm, starting with an analogy with buckets of water, before moving to the implementation in the next section.\n\nLet us imagine a bucket of water of volume Vtotal, where Vtotal is the sum of the weights of the elements in the enumerated distribution. We fill this bucket such that each element x is associated with the volume Weight(x).\n\nThis bucket equivalent to our enumerated distribution. Our {:a 1, :b 2, :c 1} initial example can be viewed as as bucket of 4 litres capacity, filled with:\n\n• 1 litre of :a\n• 2 litres of :b\n• 1 litre of :c\n\nIn this view, picking one random element in our enumerated distribution is equivalent to randomly picking (with a uniform distribution) one random atom in the bucket.\n\n###### Splitting in several buckets\n\nThings start to be interesting when we split our single bucket of 4 litres into 2 buckets of 2 litres each, and fill them intelligently:\n\n• We can fill the first bucket with our 2 litres of :c\n• We can fill the second bucket with 1 litre of :a and 1 litre of :c\n\nTo randomly pick an element, we first randomly pick one bucket. The selected bucket is a new enumerated distribution, smaller than the initial one.\n\n###### A good split\n\nIt is important to note that we should divide our initial bucket of volume total-weight into buckets of equal volumes. This makes the random selection of one of the K bucket a simple uniform integer roll between 0 and K-1. Had we not do that, we would end up with an additional enumerated distribution to select our bucket.\n\nThe trick is then to choose our number of bucket K and the way we fill each of these buckets in such a way that each of the sub-problems are made so simple than they can be decided by a simple random roll. The Alias method is such a way.\n\n###### The Alias Method\n\nThe Alias Method gives us a way to split our probability volume into buckets, such that these buckets are filled with at most 2 elements of our initial enumerated distribution. This makes it possible to randomly pick an element in two random rolls:\n\n• One integer roll, to pick the bucket\n• One double roll, to pick an element from the bucket\n\nWe select our number of bucket K as being equal to the number of xs elements, denoted N, minus one. Each bucket has a volume Vbucket equal to Vtotal divided by N – 1.\n\nWe fill each bucket by picking an element with a weight W inferior to its volume Vbucket. This leaves Vremaining (VbucketW) as remaining volume to fill. We fill it with an element whose weight is higher than Vremaining (it exists by construction).\n\nThis process will completely drain one element at each iteration, and consume some of the volume of another element as well. We repeat this process until all the buckets are filled, at which point each of our elements are drained (by construction).\n\n###### Example\n\nLet us consider the following example: {:a 1, :b 4/3, :c 1, :d 2/3}:\n\n• The total volume Vtotal equal to 4\n• The number of bucket K equal to 3 (4 elements – 1)\n• Each bucket has a volume Vbucket equal to 4/3\n\n```Elements = {:a 1, :b 4/3, :c 1, :d 2/3}\nBucket 1 = Empty\nBucket 2 = Empty\nBucket 3 = Empty\n```\n\nStep 1: We fill the first bucket with :a whose volume 1 is inferior to Vbucket (4/3). There is still 1/3 litres to fill in this bucket. We take them from element :b:\n\n```Elements = {:b 1, :c 1, :d 2/3}\nBucket 1 = {:a 1, :b 1/3}\nBucket 2 = Empty\nBucket 3 = Empty\n```\n\nStep 2: We fill the second bucket with :c whose volume 1 is inferior to Vbucket (4/3). We complete the remaining 1/3 litres by taking them from our element :b again:\n\n```Elements = {:b 2/3, :d 2/3}\nBucket 1 = {:a 1, :b 1/3}\nBucket 2 = {:c 1, :b 1/3}\nBucket 3 = Empty\n```\n\nStep 3: We fill the third bucket, whose volume is 4/3, with the remaining 2/3 litres of :b and :d. This completes our distribution in buckets:\n\n```Elements = Empty\nBucket 1 = {:a 1, :b 1/3}\nBucket 2 = {:c 1, :b 1/3}\nBucket 3 = {:b 2/3, :d 2/3}\n```\n\nWe are now done. To randomly select an element, we pick a random bucket uniformly and then roll a double between 0 and 1. If the roll is higher than the ratio of the first element in the bucket, we pick the second element, else the first element.\n\nFor instance, we pick {:c 1, :b 1/3} by first rolling 1. Then we pick :b by rolling 0.9 which is higher than the ratio of :c in the bucket (3/4).\n\n### Implementing the Alias Method\n\nNow that we know how the Alias Method works, we will implement it. Since the Alias Method stays voluntarily vague on the order in which we can pick our elements to fill the buckets, there are several possible implementations available for us.\n\n###### Chosen implementation\n\nWe will use the nice semantics of sorted-set to help us. We will store each element and its associated weight as a key in a sorted set of pairs [weight value]. So the weight will act as primary attribute in the ordering: the elements will be sorted by increase weights.\n\nAs a consequence, by construction, the first element of the sorted set will have a weight inferior to the volume of a bucket, and the last element will have a weight superior to the remaining volume of the bucket.\n\nAt each iteration, we will therefore pick the first element of the set, drain it completely to fill the bucket as much as possible. We will then pick the last element of the set and drain enough of it to fill the remaining of the volume.\n\n###### High level Clojure code\n\nThe algorithm translates into the following Clojure code, in which we first check if the input collection has enough element:\n\n• If we have just a collection of one element to pick from, we short circuit and return a function that constantly returns the same number\n• Otherwise, we construct our vector of buckets with enum-dist->buckets, and implement our algorithm based on two uniform random rolls\n\n###### Clojure Code to create buckets\n\nThe construction of the buckets is based on the sorted-set collection of Clojure, and always picks the first and last element of the container to fill the current bucket:\n\nWhere fill-one-bucket is the function that implements the draining of the quantities to-verse into a bucket. It is the core of the algorithm:\n\nWe can test our fill-one-bucket function in the REPL and see how it implements one iteration of the Alias Method:\n\nWe can also test the enum-dist->buckets and check that it transforms our enumerated distribution into buckets correctly:\n\n### Conclusion: data transformation vs code tuning\n\nIn this post, we saw how to generate random number from an enumerated distribution containing N element, in constant time, given a pre-processing time of O(N log N).\n\n###### Simple yet effective data transformations\n\nAside from the algorithm itself, the fascinating bit about the Alias Method is how simple it ends up being: it is about transforming pairs of value and probabilities, into tuples of two elements and a probability.\n\nIt shows that switching between data representation can unlock unsuspected performance improvements, and also show that it does not systematically require complex data structure to speed up an algorithm tremendously.\n\n###### Failing to see these transformations\n\nThe Alias Method is pretty smart: it is not something we would naturally come up with. But it asks the question of how many data transformation we miss, that would improve our run-time efficiency tremendously, instead of focusing so much of our efforts on code tuning.\n\nIn my years doing professional development, I have seen plenty of simple yet missed opportunities of data transformation which would have improved the efficiency of the code by much. We do miss a lot of trivial ones, and it is not because they are hard.\n\nWe often simply do not look for them. Lots of what we learned in OOP books makes us think in terms of fixed entities, with one chosen representation, and very few incentives to actually copy data to transform it into another form (mapping it).\n\nWhile having several ways to represent the same data will certainly comes at a cost if introduced gratuitously, this might be the key to unlock better performance in our software as well, and not stay stuck in tuning a sub-optimal algorithms.\n\n###### Escaping the trap in our minds\n\nClojure (and Functional Programming in general) avoids us falling into the trap of the “one representation to rule them all” by making us love data transformation.\n\nAs shown in this post, we can leverage this love for data transformations to build smarter data structure for more efficient algorithm. And I will certainly work on doing it more often in the years to come." ]
[ null ]
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https://fahdshariff.blogspot.com/2010/01/interview-questions.html
[ "## Friday, January 15, 2010\n\n### Interview Questions\n\nHere are a few questions you may be asked if interviewing for a technology / developer role in an investment bank:\n\nJava:\n\n• What is object orientation?\n• State three fundamental concepts in object-oriented programming (e.g encapsulation, abstraction, inheritance)?\n• What is the super class of all classes?\n• State three methods of the `Object` class.\n• What is the difference between checked and unchecked exceptions?\n• Name the subclasses of `Throwable`.\n• What is the `Error` class?\n• Why are `hashcode()` and `equals()` important?\n• What is `hashcode()` used for in a `Hashmap`?\n• Write an equals method for a Person class which contains a `String` attribute called `name`.\n• List XML parsers and how would you decide if you should use SAX or DOM?\n• Discuss testing with JUnit.\nOracle:\n• Given an `Employee (name, dept_id)` table and a `Department (id, name)` table, write a query to display which department each employee belongs to and another query to list all departments which have exactly 10 employees.\n• What steps would you take to identify why a query is slow and how would you optimise it?\n• What kinds of Hints are there?\n• What is the difference between a normal index and a clustered index?\nProblem Solving:\n• You have 8 coins which look identical. However, one of them is heavier than the rest. You have a weighing scale. Find the heaviest coin using the scale the fewest times as possible.\nAnswer: Weigh coins 1,2,3 vs 4,5,6. If they weigh the same, weigh 7 vs 8 to get the heaviest. If they are not the same, pick the heaviest batch (e.g. 1,2,3) and weigh 1 vs 2,3 and so on.\n• In the diagram below, you have two lists. Change the ordering of the elements in the first list, so that they appear in the same order as the second list. You have a container which can hold only one element to help you.\n• ```A B\nB C\nC +--+ D\nD | | E\nE +--+ F\nF G\nG A\n```\nAnswer: Put A into the container. Shift all elements up by one. Move A into the vacant slot in the bottom of the list.\nRisk and PnL:\n• What is Real PnL?\n• What is attribution i.e. what attributes make this PnL?\n• What is explained and unexplained pnl?\n• What is Delta Risk and why is it important?\n• What market data do you need to calculate Delta Risk and how is it calculated?\n• What is a yield curve?\n• What is a volatility surface?\n• Real PnL: Profit and Loss compared to yesterday REAL_P+L = PVToday - PVYest\n• Attribution: What made this PnL such as The Greeks: Delta PnL, Gamma PnL, Theta PnL, Vega PnL, New deals, Dropped deals, Amended deals, Cash flows\n• PnL Explained: The addition of all these attributions that explains the Real PnL.\n• PnL Unexplained: The difference between the Real PnL and the Explained PnL.\n• The target is to get Unexplained as close to 0 as possible.\nRelated Posts:\n\n#### 1 comment:\n\n1.", null, "Anonymous8:43 PM\n\nbesides DOM and SAX, you may want to look at vtd-xml as the latest and most powerful XML parsing lib\n\nhttp://vtd-xml.sf.net" ]
[ null, "https://resources.blogblog.com/img/blank.gif", null ]
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https://iftm-pharo2005.org/non-invasive-detection-and-monitoring-of-lethal-illnesses-such-as-cancer-are/
[ "# Non-invasive detection and monitoring of lethal illnesses, such as cancer, are\n\nNon-invasive detection and monitoring of lethal illnesses, such as cancer, are considered as effective factors in treatment and survival. blue color appearance due to polymerization from the diacetylene devices. Table 1. PDA and Lipid compositions from the detector vesicles. 2.3. Chromatic Measurements: Fluorescence Spectroscopy Fluorescence was assessed on the Fluscan Ascent utilizing a 96-well microplate (Greiner dish Kitty# 655C180), using excitation of 544 emission and nm of 620 nm using LP filter systems with regular slits. Applying this excitation/emission set assured that the backdrop CTX 0294885 fluorescence from the detector vesicle solutions before addition from the examined serum was negligible. Examples for fluorescence measurements had been prepared by adding 5 L processed serum to 30 L of CTX 0294885 lipid/PDA detector vesicles followed by addition of 30 L 50 mM Tris buffer (pH is depicted at Table 1). The samples were incubated for 60 CTX 0294885 min at 27 C prior to measurements. Sixty min time point was chosen as the optimal time in which the chromatic response equilibrates (Figure S1). Fluorescent chromatic responses were calculated according to the formula: percentage fluorescent chromatic responses (%FCR) = [(Emi ? Emc)/(Emr ? Emc)] 100%, in which Emc is the background fluorescence of blue vesicles without addition of tested sample, Emi is the value obtained for the vesicle solution after incubation with tested sample and Emr is the maximal fluorescence value obtained for the red-phase vesicles (heating at 80 C for 2 min). The result taken for each serum sample-specific detector was the mean of the triplicate. 2.4. Statistical Analysis Experiments were performed in 96-well plates; a typical plate employed one type of detector vesicle and contained replicates of serum samples from each studied group as well as positive and negative color controls and identical aliquots of five standardization serum samples. Average %FCR per each sample was calculated based on the plate negative and positive color controls (see above, chromatic measurements: fluorescence spectroscopy). The %FCR ideals from different experimental plates had been standardized based on the results from the five standardization serum examples used in all experimental plates. To improve for experimental biases between different experimental plates further, a normalization stage was put on %FCR ideals in each experimental dish the following: the suggest %FCR from the experimental dish control serum samples was subtracted from each %FCR worth and the effect was divided by the typical deviation from the experimental dish control serum samples. This technique was repeated for every chromatic vesicle, and each normalized %FCR was utilized as an attribute in following classification tests. Classification was carried out using the support vector machine (SVM) technique having a linear kernel as applied in the LIBSVM CTX 0294885 collection [9,10]. Distinct machine learning tests were conducted for every pair of course organizations: Control Abdomen; Control Pancreas and Pancreas Abdomen. The examples had been split into teaching and tests subsets arbitrarily, maintaining the percentage of control instances to treatment instances analyzed in each test. For feature selection, all feasible subsets were regarded as. An SVM model originated for every feasible subset of features, and the best model was chosen based on its accuracy of predicting the class of the training subset samples. The accuracy of this model was evaluated over the remaining testing group, using the percent of accurate prediction (Accuracy) and Mathews Correlation Coefficient (MCC) as quality measures. This procedure was repeated five times, using different random partitions into training and test sets each time, and the quality measures (classification Accuracy and MCC) were calculated for all partitions. For a binary classification test, Sensitivity measures the proportion of actual positives which are correctly identified as such and Specificity measures the proportion of negatives which are properly identified. Accuracy may be the percentage of true outcomes (both accurate positives and accurate negatives) in the Rabbit Polyclonal to NPM (phospho-Thr199) populace. MCC can be used in machine learning like a measure of the grade of binary (two course) classifications and comes back a worth between ?1 and +1. A coefficient of +1 represents an ideal prediction, 0 the average arbitrary prediction and ?1 an inverse prediction. MCC is normally seen as a well balanced measure which may be utilized actually if the classes are of different sizes. 3.?Discussion and Results 3.1. Basic principles from the Reactomics Technique The hypothesis root the reactomics strategy can be that molecular variants of sera connected with tumor onset and development provide a chance for disease recognition and monitoring. The diagnostic concept CTX 0294885 and experimental concept are depicted in Figure 1 schematically. Shape 1(A) represents a common experiment where three sera are analyzed (sera iCiii), using." ]
[ null ]
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https://docs.appian.com/suite/help/20.4/fnc_mathematical_roundup.html
[ "roundup() Function\n\nRounds the number up to the specified digit.\n\n## Syntax\n\nroundup( number, num_digits )\n\nnumber: (Decimal) The number to be rounded.\n\nnum_digits: (Number) Determines the digit or place to which the number will be rounded up to the nearest 10^(-num_digits). 2 is default.\n\n## Returns\n\nDecimal\n\nTo round the number up to the nearest hundred, set num_digits equal to `-2`.\n\n## Examples\n\n`roundup(7.36819)` returns `7.37`\n\n`roundup(7.36819, 3)` returns `7.369`\n\n`roundup(7.36819, 4)` returns `7.3682`\n\nfixed(): Use this function with `roundup()` to display your desired output." ]
[ null ]
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https://garbagevalue.com/books-solutions/let-us-c/the-loop-control-structure/b-3/write-a-program-to-print-out-all-armstrong-numbers-between-1-and-500-if-the-sum-of-cubes-of-each-di
[ "# Write a program to print out all Armstrong numbers between 1 and 500. If the sum of cubes of each digit of the number is equal to the number itself, then the number is called an Armstrong number. For example, 153 = ( 1 * 1 * 1 ) + ( 5 * 5 * 5 ) + ( 3 * 3 * 3 )\n\nB\nSections\n5\nExercises\n\nA\n\nB\n\nC\n\nD\n\nE\n\n1\n\n2\n\n3\n\n4\n\n5\n\n6\n\n7\n\n8\n\n9\n\n``````#include<stdio.h>\n#include<conio.h>\n#include<math.h>\nint main()\n{\nint check = 0, i, k, ans;\nfor(i = 1; i <= 500; i++ )\n{\nk = i;\nans = 0;\nwhile(k)\n{\ncheck = k%10;\ncheck = pow(check, 3);\nans += check;\nk /= 10;\n}\nif(i == ans)\nprintf(\"%d, \", ans);\n}\nprintf(\"are the armstrong numbers between 1 and 500.\");\ngetch();\nreturn 0;\n}``````\n\n© 2020 Garbage Value", null, "" ]
[ null, "https://ik.imagekit.io/garbagevalue/garbagevalue_xFh4R6wZG.svg", null ]
{"ft_lang_label":"__label__en","ft_lang_prob":0.60809,"math_prob":0.9996941,"size":672,"snap":"2020-34-2020-40","text_gpt3_token_len":243,"char_repetition_ratio":0.12275449,"word_repetition_ratio":0.0,"special_character_ratio":0.4315476,"punctuation_ratio":0.17721519,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9989712,"pos_list":[0,1,2],"im_url_duplicate_count":[null,null,null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2020-09-25T12:38:10Z\",\"WARC-Record-ID\":\"<urn:uuid:5243fe68-af72-4135-94f6-ed815426bf2a>\",\"Content-Length\":\"81571\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:b231ca63-fbc9-4392-8193-49ebd01713de>\",\"WARC-Concurrent-To\":\"<urn:uuid:a4204bc2-b030-49a5-b8a7-c695fb5124f0>\",\"WARC-IP-Address\":\"104.24.116.209\",\"WARC-Target-URI\":\"https://garbagevalue.com/books-solutions/let-us-c/the-loop-control-structure/b-3/write-a-program-to-print-out-all-armstrong-numbers-between-1-and-500-if-the-sum-of-cubes-of-each-di\",\"WARC-Payload-Digest\":\"sha1:HPSE652AU2QNU5XQK2XMYAY2GKW4RCQY\",\"WARC-Block-Digest\":\"sha1:LWA6CFIF7JRVSK7OCL6PS7ZJCTVPN2UF\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2020/CC-MAIN-2020-40/CC-MAIN-2020-40_segments_1600400226381.66_warc_CC-MAIN-20200925115553-20200925145553-00121.warc.gz\"}"}
http://www.numbersaplenty.com/1022120
[ "Search a number\nBaseRepresentation\nbin11111001100010101000\n31220221002022\n43321202220\n5230201440\n633524012\n711454641\noct3714250\n91827068\n101022120\n11638a30\n12413608\n1329a308\n141c86c8\n15152cb5\nhexf98a8\n\n1022120 has 64 divisors (see below), whose sum is σ = 2643840. Its totient is φ = 352000.\n\nThe previous prime is 1022113. The next prime is 1022123. The reversal of 1022120 is 212201.\n\nAdding to 1022120 its reverse (212201), we get a palindrome (1234321).\n\nIt can be divided in two parts, 102 and 2120, that added together give a palindrome (2222).\n\n1022120 is digitally balanced in base 2, because in such base it contains all the possibile digits an equal number of times.\n\nIt is a Cunningham number, because it is equal to 10112-1.\n\nIt is a Harshad number since it is a multiple of its sum of digits (8).\n\nIt is a junction number, because it is equal to n+sod(n) for n = 1022098 and 1022107.\n\nIt is a congruent number.\n\nIt is not an unprimeable number, because it can be changed into a prime (1022123) by changing a digit.\n\nIt is a polite number, since it can be written in 15 ways as a sum of consecutive naturals, for example, 10070 + ... + 10170.\n\nIt is an arithmetic number, because the mean of its divisors is an integer number (41310).\n\n21022120 is an apocalyptic number.\n\n1022120 is a gapful number since it is divisible by the number (10) formed by its first and last digit.\n\nIt is an amenable number.\n\nIt is a practical number, because each smaller number is the sum of distinct divisors of 1022120, and also a Zumkeller number, because its divisors can be partitioned in two sets with the same sum (1321920).\n\n1022120 is an abundant number, since it is smaller than the sum of its proper divisors (1621720).\n\nIt is a pseudoperfect number, because it is the sum of a subset of its proper divisors.\n\n1022120 is a wasteful number, since it uses less digits than its factorization.\n\n1022120 is an evil number, because the sum of its binary digits is even.\n\nThe sum of its prime factors is 146 (or 142 counting only the distinct ones).\n\nThe product of its (nonzero) digits is 8, while the sum is 8.\n\nThe square root of 1022120 is about 1010.9995054400. Note that the first 3 decimals coincide. The cubic root of 1022120 is about 100.7319625692.\n\nThe spelling of 1022120 in words is \"one million, twenty-two thousand, one hundred twenty\"." ]
[ null ]
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http://hettingern.people.cofc.edu/Aes_Fall_2014/Expalnation_of_Final_Quiz_Score.html
[ "Explanation of quiz scores\n\nOn each quiz:\n\n**A check means you answered correctly and this is equal to a 4 =A (free quizzes are an automatic 4)\n\n**1/2 means I wasn't sure how much or if you read; this equals a 2 = C\n\n**A slash ------ means you did not answer correctly; it’s a 0 = F\n\nThere were 10 required quizzes. Add up the #s on your quizzes (using above key), including \"free quizzes,\" and divide by 10. This is the # that is on the front of your quizzes I returned.\n\nI use the College’s grading scale\n\nA 4.0\n\nA- 3.7\n\nB+ 3.3\n\nB 3.0\n\nB- 2.7\n\nC+ 2.3\n\nC 2.0\n\nC- 1.7\n\nD+ 1.3\n\nD 1.0\n\nD- 0.7\n\nF 0.0" ]
[ null ]
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http://aplicacionesblackberry.co/word-problem-lesson-plans-1st-grade/word-problem-lesson-plans-1st-grade-mixed-multiplication-and-division-word-problems-word-problem-lessons-for-first-grade/
[ "# Word Problem Lesson Plans 1st Grade Mixed Multiplication And Division Word Problems Word Problem Lessons For First Grade", null, "word problem lesson plans 1st grade mixed multiplication and division word problems word problem lessons for first grade.\n\nword problem lessons for first grade wow weekly lesson plan template plans,word problem lesson plans first grade lessons for free worksheets library download and print on,word problems problem lesson plans first grade lessons for ,word problem lesson plans first grade math step into lessons for, word problem lessons for first grade lesson plans problems,word problem lesson plans first grade lessons for guided math in the brown bag teacher, word problem lesson plans first grade lessons for plan template editable on google drive school bee,adding 3 numbers grade tutorials word problem lesson plans first lessons for,word problem lessons for first grade lesson plans kindergarten valentines day math problems multi step a ,word problem lessons for first grade second drama lesson plans ." ]
[ null, "http://aplicacionesblackberry.co/wp-content/uploads/2019/01/word-problem-lesson-plans-1st-grade-mixed-multiplication-and-division-word-problems-word-problem-lessons-for-first-grade.jpg", null ]
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https://education.vex.com/stemlabs/v5/stemlabs-v5/vision-sensor/prepare-for-the-vision-data-challenge-c?type=teacher
[ "", null, "", null, "STEMLabs V5\nVision Sensor Teacher\n\nTeacher Portal\n\n# Prepare for the Vision Data Challenge - C++", null, "Teacher Toolbox - The Purpose of this Activity\n\nThe Vision Sensor provides a variety of data that can then be used in projects. The Sensing instruction allows the user to have the project take snapshots, decide if the object exists, decide how many exist, determine the object's center X and Y coordinates within the Vision Sensor's snapshot, and determine the object's width and height in pixels within the snapshot. This activity will introduce all of the related instruction necessary for collecting that information in preparation for the Vision Data Challenge.\nThe following is an outline of Rethink's Vision Data Challenge:\n\n• Review a complete data set of information collected from the Vision Sensor's Sensing instruction.\n\n• Complete a partial data set of information collected from the Vision Sensor about a different snapshot.\n\n• Create a data set based on a snapshot and the Vision Sensor's Sensing instructions.\n\n### The Vision Sensor's Sensing Instructions\n\nVEXcode V5 has Sensing instruction for the Vision Sensor. The first two you already used in the Play section to take a snapshot and to check if the object exists.\n\nIn the figure below, you see that the snapshot captured the GREENBOX snapshot. The object, GREENBOX, was identified in the snapshot and so the answer of whether it exists is TRUE.\n\nLet's look at these other Sensing instructions and what their values tell us.", null, "• The object count instruction tells us how many GREENBOX objects are in the snapshot. Here, there is only 1 detected.\n\n• The center X value tells us whether the GREENBOX object is to the left or right of the robot's center point. Remember, the Vision Sensor should be mounted in the middle of the robot facing forward and so the snapshot's view is the robot's view.\n\n• If center X is greater than 157.5, the object is to the right of the robot's center point.\n\n• If center X is less than 157.5, the object is to the left of the robot's center point.\n\n• The center Y value tells us whether the GREENBOX is higher or lower than the robot's center point.\n\n• If center Y is greater than 105.5, the object is lower than the robot's center point.\n\n• If center Y is less than 105.5, the object is higher than the robot's center point.\n\n• The width and height values tell us how close the GREENBOX is to the robot.\n\n• The same-sized object will be larger in width and height as it gets closer to the robot.", null, "Teacher Toolbox - Why this reading?\n\nThe Help information within VEXcode V5 also provides information about the instructions but here, the data being collected are contextualized as to what they specifically tell the user about the object in the snapshot.\n\nNotes:\n\n• The centerX and centerY values of the entire snapshot are used for determining whether the object is to the left/right or above/below the robot's center point. They are calculated by dividing the total number of pixels on that axis by two (e.g., centerX of snapshot = 315 / 2 = 157.5).\n\nWe can assume the center point of the robot is the same as the center point of the Vision Sensor's snapshot because the Vision Sensor should be mounted in the center of the robot and facing forward. The position of the Vision Sensor on the robot's build and the degree to which the Vision Sensor might be angled downward need to be taken into account when judging the position of the object relative to the robot's (or Vision Sensor's) center point.\n\n• The Y values increase downward within the snapshot. Make sure students recognize that before moving on to the next part.\n\n### How are the center X and center Y values calculated?\n\nThe values are calculated based on the coordinates within the snapshot. The width and height of the object are already calculated.\n\nThe Vision Sensor tracks the X and Y values of the upper left corner of the object. Below, those coordinates are (84, 34).", null, "The center X and center Y values can be calculated based off of the coordinates of the upper left corner (84, 34), and the width (W 140) and height (H 142) values provided.", null, "• centerX = 140/2 + 84 = 154\n\n• centerX = half the width of the object added to its leftmost X coordinate\n\n• centerY = 142/2 + 34 = 105\n\n• centerY = half the height of the object added to its topmost Y coordinate", null, "Teacher Toolbox - Concluding this page\n\nMake sure that students understand the math involved in finding the center X and center Y values. They will need it for the activity on the next page.\n\nAsk how the (84, 34) and (W 140, H 142) values relate to the coordinates provided in the corners of the snapshot. Students should recognize that the entire snapshot is mapped onto a coordinate plane based on the number of pixels. The X values range from 0 to 315 (316 pixels wide) and the Y values range from 0 to 211 (212 pixels tall). The object's coordinates and size are based on how many pixels the object takes up along those axes." ]
[ null, "https://content.vexrobotics.com/vexheader/whiteCurrencyIcon.svg", null, "https://content.vexrobotics.com/vexheader/whiteDropDownArrow.svg", null, "https://education.vex.com/stemlabs/themes/custom/vexedu/assets/images/spark/icon-teacher-toolbox.png", null, "https://education.vex.com/xyleme_content/vision-sensor-v5/web-teacher/media/Activity%20Packs/V5%20Vision%20Sensor/image%20%281%29.png", null, "https://education.vex.com/stemlabs/themes/custom/vexedu/assets/images/spark/icon-teacher-toolbox.png", null, "https://education.vex.com/xyleme_content/vision-sensor-v5/web-teacher/media/Activity%20Packs/Vision%20Sensor/VisionSensorSnapshot2.png", null, "https://education.vex.com/xyleme_content/vision-sensor-v5/web-teacher/media/Activity%20Packs/V5%20Vision%20Sensor/four.PNG", null, "https://education.vex.com/stemlabs/themes/custom/vexedu/assets/images/spark/icon-teacher-toolbox.png", null ]
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https://www.positioniseverything.net/javascript-sort-array/
[ "# JavaScript Sort Array Functions: Sorting Arrays Effectively", null, "JavaScript sort array functions will help you quickly sort the elements within an array. If this is something that you’ve been looking for, in order to improve your array’s readability, then our article is for you!\n\nThis write-up teaches you how to sort array in js using the sort () method and reverse () function. Read on to understand how each one works through your array.\n\n## Sort Array in JavaScript: The Methods You Can Use\n\nYou may want to sort a given array in different formats; for example, you may wish that you display values in an array alphabetically. JavaScript offers inbuilt methods that you can use to sort elements in an array as you want.\n\nMoreover, the sort() method returns values alphabetically. However, if you want the values to be in the reverse order, you may use the reverse() function. Additionally, you can use the sort() function with a nested function if you want to create custom sorts.\n\nLet’s look at these and other methods in detail.\n\n## Using JavaScript Sort() Method\n\nThe sort method reads all the values in an array before returning them alphabetically. However, if values are integers or numbers, it returns them in ascending or descending order. By default, the method will convert each element in the array that requires sorting into a string.\n\n### – Code Examples Using Sort Method\n\n#### The sort() method sorts an array alphabetically:\n\n const fruits = [“Lemon”, “Orange”, “Banana”, “Mango”] fruits.sort();\n##### Returns:\n Banana, Lemon, Mango, Orange\n\n#### The sort() function sorts an array in ascending order:\n\n\n##### Returns:\n 1,2,3,8,9\n\n### – How the JavaScript Sort() Method Works: Sorting Objects\n\nIn a gist, the sort() function can be written as Array.sort(). Now, check out this code below:\n\n const bar = [5, 18, 32, new Set, { user: ‘John Smith’ }]; bar.sort(); // returns [ 18, 32, 5, { user: ‘John Smith’ }, Set {} ]\n\nIt is not logical that 32 comes before 5. However, it is logical in JavaScript because each element within an array is converted to a string, and in the Unicode order, 32 comes before 5.\n\n### – Code Example Noticing How Array.sort Function Changes Arrays it Sorts\n\nNote that the array.sort function changes or mutates the array it sorts, unlike many other JavaScript array functions.\n\nFor example:\n\n const baz = [‘My cat ate a book’, 17, 6, 5, 37]; baz.sort(); // baz array modified console.log(baz); // shows [ 37, 17, 5, 6, ‘My cat ate a book’ ]\n\nYou can prevent this by creating a new array instance to be sorted and modified instead. This is possible by using an array method that returns a copy of the array, e.g., Array.slice.\n\n#### Code example:\n\n const sortedBaz = baz.slice().sort(); // new instance of baz array is created and sorted\n\nAlternatively, you can use the spread operator if you like a new syntax for the same effect, as we did here:\n\n const sortedBaz = […baz].sort(); // creates and sorts a new instance of the baz array\n\nIn both cases, the output is the same:\n\n console.log(baz); // [‘My cat ate my homework’, 37, 9, 5, 17]; console.log(sortedBaz); // [ 17, 37, 5, 9, ‘My cat ate my book’ ]\n\nMoreover, in JavaScript sort array of objects using the array.sort() method alone is easy but might not be helpful. Thankfully, the method takes an optional parameter, compareFunction, that causes the sorting of the array elements as per its return value.\n\n## JavaScript Sort Array: Using The Compare Function\n\nIf you have two functions, compare them using the compare function. The compareFunction returns a negative, zero, or positive value, depending on the arguments:\n\nfunction(a, b){return a-b}\n\nSort () compares two values, sends the values to the compare function, and sorts the value based on returned value( negative, zero, positive). For instance, the sort() function sorts 40 as lower than 100. So, when comparing 40 and 100, sort() invokes the function (40,100). So, it will calculate 40 – 100, giving -60.\n\n### – Example\n\nTake, for example, you want to compare two elements, bar and foo using the compare function, you can set up the values as follows:\n\n• less than 0 — foo comes before bar\n• greater than 0  — bar comes before foo\n• equal to 0  — foo and bar remain unchanged concerning each other.\n\nHere is a code example to make you comprehend what we are talking about better:\n\n#### Ascending order:\n\n\n##### Output:\n 1,5,10,25,30,200\n\n#### Descending order\n\n\n##### Output\n 200,30,25,10,5,1\n\n## JavaScript Sort Array by Property\n\nYou can also sort an array of objects by their property values. Check out the code below which sorts an array by property name:\n\n### – Code Example: by Property\n\n // program to sort array by property name function compareName(x, y) { // converting to uppercase to have case-insensitive comparison const name1 = x.name.toUpperCase(); const name2 = y.name.toUpperCase(); let comparison = 0; if (name1 > name2) { comparison = 1; } else if (name1 < name2) { comparison = -1; } return comparison; } const students = [{name: ‘Jane’, age: 26},{name: ‘Sarah’, age: 22}, {name: ‘Smith’, age: 24}]; console.log(students.sort(compareName));\n\n#### Output:\n\n [{name: “Jane”, age: 26}, {name: “Sarah”, age: 22}, {name: “Smith”, age: 24}]\n\nThe code above uses the sort() method to sort an array by the name property of its object elements. Ideally, it sorts the elements according to values returned by a custom sort function, in this case, compareName.\n\nThe toUpperCase() method changes the property name to uppercase. The name order remains unchanged if comparing two names results in ‘0’ or ‘-1’. Otherwise, the order changes if comparing two names results in ‘1’.\n\n### – Code Example: by Property Age\n\nYou can also sort the array by property age:\n\n // program to sort array by property Age function compareAge(a, b) { return x.age – y.age; } const students = [{name: ‘Jane’, age: 26},{name: ‘Sarah’, age: 22}, {name: ‘Smith’, age: 24}]; console.log(students.sort(compareAge));\n\n#### Output:\n\n [{name: “Sarah”, age: 22}, {name: “Smith”, age: 24}, {name: “Jane”, age: 26}]\n\nTo compare the age property of two objects, you can simply subtract them. If you receive a negative value as the difference, the order is changed. Else, if the difference is positive, the order is unchanged.\n\n## JavaScript Bubble Sort: Sorting an Array Without Using the Sort() Function\n\nIf you have a list of values to sort and do not want to use the Sort() method, you might find real help in the JS Bubble Sort. The bubble sort, also called sinking sort, is a JavaScript function that compares adjacent elements in a given list and changes their positioning if their order is incorrect.\n\nSimply put, it is a sorting algorithm that compares a pair of adjacent elements in a list. If the order is incorrect, it swaps elements; otherwise, they remain as before. Typically, the bubble sort loops through a list and moves all larger values to the end, i.e., the larger values bubble up at the end of the list. The method works in both ascending and descending order.\n\nTwo bubble sort methods exist and they are named optimized and regular. A regular bubble sort will compare elements in all possible ways regardless of whether an array is sorted. Conversely, an optimized bubble sort stops execution after an iteration is complete if no swapping occurs.\n\n## How To Create a Bubble Sort in JavaScript\n\n### – Regular Bubble Sort\n\nIn JavaScript array sort numbers using bubble sort algorithm is quite straightforward, as you’ll notice by its syntax that we’ve provided below.\n\nThe JavaScript function for the regular bubble is:\n\n function sortItems(array) { for (let i = 0; i < array.length; i++) { for (let j = 0; j < array.length; j++) { if (array[j] > array[j + 1]) { let temp = array[j]; array[j] = array[j + 1]; array[j + 1] = temp; } } } return array; }\n\nThis JS function takes an array of numbers and sorts using the bubble sort algorithm. First, the algorithm creates a for loop that iterates through each item in the list. The code uses an array length attribute to calculate the length of the list and then declare another loop. This for loop compares each element in the list.\n\nFor each inner loop iteration, the code executes an if statement. The JS if statement checks if the number on the left is more significant than the number on the right. If it is true, the code swaps the numbers. Else, things remain unchanged.\n\n### – Coding Example\n\n var numbers = [13, 11, 15, 12, 16, 14, 17]; bubbleSort(numbers); console.log(numbers);\n\n#### Output:\n\n 11, 12, 13, 14, 15, 16, 17]\n\n[In the code above, you declare a variable ‘numbers’ containing the numbers you want to sort. Then, invoke the bubbleSort () method and pass the variable as a parameter. This sorts the list and prints the newly sorted list.\n\nNote that the code above sorts the list in ascending order. You can alter this behavior by replacing the “greater than” sign in our “if” statement with a “less than” sign:\n\n if (array[j] < array[j + 1]) {\n\n### – Optimized Bubble Sort\n\nThe optimized bubble sort introduces a new variable that tracks whether a swap occurs. If no swap occurs, the sort stops.\n\nYou can make your bubble sort more effective by replacing outer for loop with a while loop:\n\n function sortItems(array) { let swapped = true; do { swapped = false; for (let j = 0; j < array.length; j++) { if (array[j] > array[j + 1]) { let temp = array[j]; array[j] = array[j + 1]; array[j + 1] = temp; swapped = true; } } } while (swapped); return array; }\n\nThe while loop executes until swapped is false. So, in every iteration, set the value of swapped to false. If a swap occurs, the value returns to true, as it is the default value of swapped.\n\nThis action lets you track whether a swap is made in an iteration. If no swap is made, the list is sorted; hence you can stop the bubble sort.\n\n### – Coding Example\n\n var numbersToSort = [9, 3, 2, 11]; var sortedList = sortItems(numbersToSort); console.log(sortedList);\n\n#### Output:\n\n [2, 3, 9, 11]\n\n## JavaScript Array Sort(): Sort in Reverse Order\n\nTo sort an array in reverse order, JavaScript offers an inbuilt function, reverse(). This function reverses an array to make the first element become last and places the last element at the first position. Therefore, the reverse () method overwrites the array order. However, the method will not order an array in alphabetical descending order.\n\n### – Coding Example\n\n\n\n#### Output:\n\n Aeroplane, Ship, Bike, Car\n\nThe reverse() method modifies the order of items in the list. Keep in mind, however, that you cannot assign the results of a reverse() function to a new variable without modifying the original array.\n\n## Conclusion", null, "We have comprehensively explained how to sort elements in a JavaScript array using different methods. So now, you have learned how to sort numerical arrays, the array of objects, and sorting an array by property. This is enough for you to start sorting JavaScript arrays effectively today!" ]
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https://jp.mathworks.com/help/simulink/ref_extras/dflipflop.html
[ "# D Flip-Flop\n\nModel a positive-edge-triggered enabled D flip-flop\n\n• Library:\n• Simulink Extras / Flip Flops\n\n•", null, "## Description\n\nThe D Flip-Flop block models a positive-edge-triggered enabled D flip-flop. The D Flip-Flop block has three inputs:\n\n• D — data input\n\n• CLK — clock signal\n\n• !CLR — enable input signal\n\nOn the positive (rising) edge of the clock signal, if the block is enabled (!CLR is greater than zero), the output Q is the same as the input D. The truth table for the D Flip-Flop block follows.\n\nNote\n\nThe D Flip-Flop block treats a nonzero input as true (`1`).\n\nDQ!Q\n110\n001\n\nIf the block is not enabled on the rising edge of the clock signal, Q is reset to zero. When the clock signal is not rising, the block remains in the previous state.\n\n### Logic Signals as Boolean or Double Data Types\n\nThe Implement logic signals as boolean data (vs. double) configuration parameter setting affects the input and output data types of the D Flip-Flop block because the D Flip-Flop is a masked subsystem that uses the Logical Operator block. The Logical Operator block in the masked subsystem has the following parameter settings:\n\nBlock Parameter Setting\nOutput data type`Inherit: Logical`\nRequire all inputs and output to have the same data type`On`\n\nFor more information about the Implement logic signals as boolean data (vs. double) configuration parameter, see Implement logic signals as Boolean data (vs. double).\n\n## Ports\n\n### Input\n\nexpand all\n\nData input signal, specified as a scalar, vector, or matrix.\n\n#### Dependencies\n\nThe data types that the D Flip-Flop block accepts for the input D depend on the setting of the Implement logic signals as boolean data (vs. double) model configuration parameter. If this parameter is on, D must have data type `boolean`; if this parameter is off, D can have data type `boolean` or `double`.\n\nData Types: `double` | `Boolean`\n\nClock signal, specified as a scalar, vector, or matrix.\n\nData Types: `single` | `double` | `int8` | `int16` | `int32` | `uint8` | `uint16` | `uint32` | `Boolean` | `fixed point` | `enumerated` | `bus`\n\nEnable input signal, specified as a scalar, vector, or matrix.\n\nData Types: `single` | `double` | `int8` | `int16` | `int32` | `uint8` | `uint16` | `uint32` | `Boolean` | `fixed point` | `enumerated` | `bus`\n\n### Output\n\nexpand all\n\nOutput signal Q, with the same dimensions and data type as the input D.\n\nData Types: `double` | `Boolean`\n\nOutput signal !Q, with the same dimensions and data type as the input D.\n\nData Types: `double` | `Boolean`\n\n## Version History\n\nIntroduced in R2008b" ]
[ null, "https://jp.mathworks.com/help/simulink/ref_extras/d_flipflop_block_icon.png", null ]
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https://scirp.org/journal/paperinformation.aspx?paperid=65754
[ "Phonons near Peierls Structural Transition in Quasi-One-Dimensional Organic Crystals of TTF-TCNQ\n\nThe Peierls structural transition in quasi-one-dimensional organic crystals of TTF-TCNQ is investigated in the frame of a more complete physical model. The two most important electron-phonon interaction mechanisms are taken into account simultaneously. One is similar of that of deformation potential and the other is of polaron type. For simplicity, the 2D crystal model is considered. The renormalized phonon spectrum and the phonon polarization operator are calculated in the random phase approximation for different temperatures. The effects of interchain interaction on renormalized acoustic phonons and on the Peierls critical temperature are analyzed.\n\nShare and Cite:\n\nAndronic, S. and Casian, A. (2016) Phonons near Peierls Structural Transition in Quasi-One-Dimensional Organic Crystals of TTF-TCNQ. Advances in Materials Physics and Chemistry, 6, 98-104. doi: 10.4236/ampc.2016.64010.\n\nReceived 16 March 2016; accepted 19 April 2016; published 22 April 2016", null, "1. Introduction\n\nQuasi-one-dimensional (Q1D) organic materials have received much interest during the last years due to more diverse and often unusual properties manifested by them - . Besides, their properties can be easily manipulated and controlled by molecular chemistry methods. It has been also mentioned that the highly conducting Q1D organic crystals may have very prospective thermoelectric applications . The charge transfer compound TTF-TCNQ (tetrathiafulvalene-tetracyanoquinodimethane) is the most investigated Q1D organic crystal with the high electrical conductivity . Its structure consists of segregated chains or stacks of TTF and TCNQ molecules. The metallic properties are due to partial transfer of electrons from TTF to TCNQ molecules.\n\nWith the decrease of temperature, two processes undergo. From one side, the lattice distortion is favorable because it diminishes the electronic energy of the crystal, lowering the Fermi energy. From other side, the lattice distortion increases the elastic lattice energy. At some temperature, when the first process prevails over the second one, a Peierls structural transition undergoes.\n\nIt is established that in TTF-TCNQ at 54 K the Peierls transition takes place into interacting TCNQ stacks with the opening of a band gap in the electronic spectrum above the Fermi energy and a strong reducing of electrical conductivity. Although the development of the pre-transitional 1D structural fluctuations is observed on a large temperature range below 150 K , these fluctuations lead to modification of the phonon spectrum with the lowering temperature . If at some temperature, the renormalized phonon frequency becomes equal to zero, a periodic lattice distortion with the respective wave vector occurs and the Peierls structural transition is observed.\n\nIn the last time, the physical model of Q1D organic crystals was completed by an additional electron-phonon interaction mechanism. It takes into account the fluctuations due to acoustic longitudinal phonons of the polarization energy of molecules surrounding the conduction electron - . The molecules of TCNQ are relatively big and their polarizability is large too.\n\nIn , the Peierls structural transition in Q1D crystals of TTF-TCNQ type was investigated in this more complete physical model of the crystal, but in strictly 1D approximation. It was considered the case when the conduction band is half filled and Fermi dimensionless quasi momentum, kF = π/2. The Peierls critical temperature was determined.\n\nIn , the Peierls transition has been studied also in the 1D physical model. But now the renormalized acoustic phonon frequencies W(q) as functions of wave number q were calculated: 1) when the conduction band is half filled and the dimensionless Fermi momentum kF = π/2 and 2) when the concentration of conduction electrons is reduced and the band is filled up to a quarter of the Brillouin zone, kF = π/4. It was shown that a more detailed calculation considerably modifies the dependences W(q). In both cases, the critical temperature of transition was determined.\n\nThe 2D physical model for the real crystals of TTF-TCNQ was investigated in . The polarization operator as a function of temperature was calculated numerically for different values of the parameter d, which describes the ratio of the transfer energy in the direction transversal to conductive chains to the transfer energy along the chains. The Peierls critical temperature was determined in two cases: 1) when the dimensionless Fermi momentum is kF = 0.59 π/2, and 2) when the carrier’ concentration is slightly modified and the Fermi momentum kF = 0.59 π/2 ± δ, where δ represents the variation of the Fermi momentum. In this paper, the numerical modellings were performed for the values of the sound velocity at low temperatures taken from : vs1 = 3.4 × 105 cm/s along chains and vs2 = 5.25 × 105 cm/s in transversal direction. However, more exact calculations of the Peierls critical temperature in TCNQ chains have shown that in order to achieve the experimental result, it is necessary to choose vs2 = 0.5vs1. The last value has been used later on.\n\nThe aim of this paper is to present a detailed modeling of the Peierls transition in TTF-TCNQ crystals in the frame of above mentioned more complete physical model. The effects of interchain interaction on the dispersion of renormalized phonons and on Peierls critical temperature are analyzed. For the simplicity, we consider the 2D approximation.\n\n2. The Physical Model in 2D Approximation\n\nThe Hamiltonian of the 2D crystal in the tight binding and nearest neighbor approximations has the form:", null, ". (1)\n\nIn Equation (1) the first term represents the energy operator of free electrons in the periodic field of the lattice,", null, "are the creation and annihilation operators of such electron, where k is two-dimensional wave vector with projections (kx, ky). The carrier energy", null, "is measured from the bottom of conduction band.", null, "(2)\n\nwhere", null, "and", null, "are the transfer energies of a carrier from one molecule to another along the chain (x direction) and in perpendicular direction (y direction). In Equation (1)", null, "are creation and annihilation operators of an acoustic phonon with two-dimensional wave vector q and frequency", null, ". The second term in the Equation (1) is the energy of longitudinal acoustic phonons", null, "(3)\n\nwhere", null, "and", null, "are limit frequencies for oscillations in x and y directions. The third term in Equation (1) represents the electron-phonon interactions. Two interaction mechanisms are considered. The first interaction is determined by the fluctuations of transfer energies", null, "and", null, ", due to the intermolecular vibrations (acoustic phonons). This interaction is similar to that of deformation potential, and the coupling constants are proportional to the derivatives", null, "and", null, "of and with respect to the intermolecular distances, ,. The second interaction is of polaron type. This interaction is conditioned by the fluctuations of the polarization energy of the molecules surrounding the conduction electron. The coupling constant of this interaction is proportional to the average polarizability of the molecule. This interaction is important for crystals composed of large molecules such as TCNQ, so as is roughly proportional to the volume of molecule.\n\nThe square module of matrix element from Equation (1) has the following form:\n\n(4)\n\nwhere N is the number of molecules in the basic region of the crystal, M is the mass of the molecule;, parameters γ1 and γ2 have the sense of the amplitudes ratio of second electron-phonon interaction to the first one along chains and in transversal direction\n\n. (5)\n\nFrom exact series of perturbation theory for the phonon Green function we sum up the diagrams containing closed loops of two electron Green functions that make the most important contribution. This is the random phase approximation. We obtain for the Fourier component of the phonon Green function:\n\n(6)\n\nwhere\n\n(6a)\n\nis the free phonon Green function, δ → 0+ and Ω(q) is the renormalized phonon frequency. is the phonon polarization operator, q is the wave vector of longitudinal acoustic phonons. The real part of the dimensionless polarization operator is presented in the form:\n\n. (7)\n\nHere, is the number of elementary cells in the basic region of the crystal, the number of molecules is, where r = 2 is the number of molecules in the elementary cell, is the Planck constant. The temperature enters in our expressions only through the Fermi distribution functions and. Ω(q) is determined by the pole of function and is obtained from the transcendent dispersion equation\n\n. (8)\n\nThis equation can be solved only numerically.\n\n3. Results and Discussions\n\nThe calculations were performed for the following parameters: w1 = 0.125 eV, eV∙Å−1, a = 12.30 Å, b = 3.82 Å, kF = 0.59π/2 , vs1 = 3.4 × 105 cm/s, vs2 = 0.5vs1 cm/s, d = 0.015, M = 3.7 × 105me (me is the mass of the free electron), γ1 = 1.37, r = 2. The parameter γ2 is determined from the relation: γ2 = γ125b5/(a5d).\n\nFigure 1 and Figure 2 show the dependences of renormalized phonon frequencies Ω(qx) as functions of qx for different temperatures and different values of qy. The same dependences for initial phonon frequency ω(qx) are presented too. It is seen that the values of Ω(qx) are diminished in comparison with those of frequency ω(qx) in the absence of electron-phonon interaction. This means that the electron-phonon interaction diminishes the values of lattice elastic constants. In addition, it is observed that with a decrease of temperature T the curves change their form, and in dependencies Ω(qx) a minimum appears. This minimum becomes more pronounced at lower temperatures. After all, at certain temperature Ω(qx) attains zero for qx = 0.58π. At this temperature, the structural Peierls transition takes place. The deviation of Ω(qx) = 0 from qx = 2kF is caused by T ≠ 0 and kF ≠ π/2.\n\nFigure 1(a) shows the case, when qy = 0. At T = 59.7 K the transition occurs in TCNQ chains alone. The crystal lattice along TCNQ chains changes from the initial state with the lattice constant b to a new crystalline state with constant 4b, that is four times larger. At this temperature, the electrical conductivity is strongly diminished, so as a gap in the carrier spectrum is fully opened just above the Fermi energy. In addition, it is seen that the slope of Ω(qx) at small qx is diminished in comparison with that of ω(qx). This means that the electron-phonon interaction has reduced also the sound velocity in a large temperature interval.\n\nWhen the interaction between TCNQ chains is taken into account (qy ≠ 0), the Peierls critical temperature is diminished. Figure 1(b) and Figure 2 correspond to 2D physical model, qy ≠ 0. Figure 1(b) shows Ω(qx) for qy = π/4 and different temperatures. One can observe that Ω(qx) attains zero at T ~ 59 K, i.e. the transition takes place at this T.\n\nWhen qy = 2kF (Figure 2(a)), the Peierls critical temperature some more decreases and has a value of T ~ 56 K. Figure 2(b) shows the dependences of Ω(qx) on qx for qy = π and different temperatures. It is observed that the transition temperature decreases still more and equals T ~ 54 K. Note that this value agrees with the experimental data.\n\n(a) (b)\n\nFigure 1. Renormalized phonon spectrum Ω(qx) for γ1 = 1.37 and different temperatures. The dashed line is for the spectrum of free phonons. (a) qy = 0; (b) qy = π/4.\n\nFigure 3 shows clearly that with the increase of parameter qy, the Peierls critical temperature decrease. So, for qy = 0, T ~ 59.7 K; for qy = π/4, T ~ 59 K; for qy = 2kF, T ~ 56 K and for qy = π, T ~ 54 K. This means that Peierls transition begins at T ~ 59 ÷ 60 K in TCNQ chains alone, but when the interaction between TCNQ chains is taken into account in 2D approximation, Peierls transition occurs completely at T ~ 54 K. It is expected that 3D approximation will not introduce important modifications.\n\nFigure 4 shows the dependencies of the real part of dimensionless polarization operator as function of qx for different values of qy and different temperatures at Ω = 0. From the both graphs it is observed a very sharp peak near the value of unity.\n\n(a) (b)\n\nFigure 2. Renormalized phonon spectrum Ω(qx) for γ1 = 1.37 and different temperatures. The dashed line is for the spectrum of free phonons. (a) qy = 2k­F; (b) qy = π.\n\nFigure 3. Renormalized phonon spectrum Ω(qx) for γ1 = 1.37, different values of qy and different temperatures.\n\n(a) (b)\n\nFigure 4. Polarization operator as function of qx for: (a) qy = 0 and T = 59.7 K; (b) qy = π and T = 54 K.\n\nNote that in above calculations we have used the value of vs1 = 3.4 × 105 cm/s at low temperatures from , but for vs2 we have taken 0.5vs1 instead of vs2 = 5.25 × 105 cm/s measured in . If the last value of vs2 is applied, it results that a complete Peierls transition should undergo at T = 15 K. Such big deviation of critical temperature from the observed one at T = 54 K suggests, that the sound velocity in the transversal direction cannot be larger than in longitudinal to chains direction and the most probably vs2 ~ 0.5vs1, as demonstrate our calculations of transition temperature. In addition, due to the quasi-one-dimensionality of the crystal, the chemical bonds in transversal direction must be weaken. This fact also suggests that vs2 should be less than vs1.\n\n4. Conclusion\n\nThe behavior of phonons near Peierls transition has been studied in quasi-one-dimensional organic crystals of TTF-TCNQ in 2D approximation. A more complete crystal model is applied which takes into account the two most important electron-phonon interactions. One of them is of the deformation potential type. The coupling constants are proportional to the derivatives of the transfer energies and with respect to the intermolecular distances. The other interaction is similar to that of a polaron with the coupling constant proportional to the average polarizability of the molecule. The ratios of amplitudes of second electron-phonon interaction to the first one along chains and in transversal direction are noted by γ1 and γ2, respectively. Analytical expression for the polarization operator was obtained in random phase approximation. The numerical calculations for renormalized phonon spectrum, Ω(qx), for different temperatures are presented: 1) when qy = 0 and the interaction between TCNQ chains is neglected and 2) when qy ≠ 0 and interactions between the adjacent chains are considered. It has been established that Peierls transition begins at T ~ 59.7 K in TCNQ chains alone and reduces considerably the electrical conductivity. Due to interchain interaction, the transition is finished at T ~ 54 K. It is demonstrated that the electron-phonon interaction diminishes Ω(qx) with respect to initial frequency ω(qx) and reduces the sound velocity in a large temperature interval.\n\nConflicts of Interest\n\nThe authors declare no conflicts of interest.\n\n Jerome, D. (2004) Organic Conductors: From Charge Density Wave TTF-TCNQ to Superconducting (TMTSF) 2PF6. Chemical Reviews, 104, 5565-5592. http://dx.doi.org/10.1021/cr030652g Jerome, D. (2012) Organic Superconductors: When Correlations and Magnetism Walk. Journal of Superconductivity and Novel Magnetism, 25, 633. Pouget, J.P. (2012) Bond and Charge Ordering in Low-Dimensional Organic Conductors. Physica B, 407, 1762-1770. http://dx.doi.org/10.1016/j.physb.2012.01.025 Casian, A. (2006) Thermoelectric Properties of Electrically Conducting Organic Materials. In: Rowe, D.M., Ed., Thermoelectric Handbook, Macro to Nano, Chap. 36, CRC Press, Boca Raton, FL, 36-1-36-8. Casian, A.I., Pflaum, J. and Sanduleac, I.I. (2015) Prospects of Low Dimensional Organic Materials for Thermoelectric Applications. Journal of Thermoelectricity, 1, 16. Chernenkaya, A., et al. (2015) Nature of the Empty States and Signature of the Charge Density Wave Instability and Upper Peierls Transition of TTF-TCNQby Temperature-Dependent NEXAFS Spectroscopy. The European Physical Journal B, 88, 13. http://dx.doi.org/10.1140/epjb/e2014-50481-9 Kagoshima, S., Ishiguro, T. and Anzai, H. (1976) Observation of the Kohn Anomaly and the Peierls Transition in TTF-TCNQ by X-Ray Scattering. Journal of the Physical Society of Japan, 41, 2061. http://dx.doi.org/10.1143/JPSJ.41.2061 Khanna, S.K., Pouget, J.P., Comes, R., Garito, A.F. and Heeger, A.J. (1977) X-Ray Studies of 2kF and 4kF Anomalies in Tetrathiafulva-lene-Tetracyanoquinodimethane (TTF-TCNQ). Physical Review B, 16, 1468. http://dx.doi.org/10.1103/PhysRevB.16.1468 Reitschel, H. (1973) The Giant Kohn Anomaly in a Peierls Semiconductor. Solid State Communications, 13, 1859. Bulaevskii, L.N. (1975) Peierls Structure Transition in Quasi-One-Dimensional Crystals. Soviet Physics Uspekhi, 18, 131. http://dx.doi.org/10.1070/PU1975v018n02ABEH001950 Casian, A., Dusciac, V. and Coropceanu, Iu. (2002) Huge Carrier Mobilities Expected in Quasi-One-Dimensional Organic Crystals. Physical Review B, 66, Article ID: 165404. http://dx.doi.org/10.1103/PhysRevB.66.165404 Casian, A. (2010) Violation of Wiedemann-Franz Law in Quasi-One-Dimensional Organic Crystals. Physical Review B, 81, Article ID: 155415. http://dx.doi.org/10.1103/PhysRevB.81.155415 Sanduleac, I., Casian, A. and Pflaum, J. (2014) Thermoe-lectric Properties of Nanostructured Tetrathiotetracene Iodide Crystals in a Two-Dimensional Model. Journal of Nano-electronics and Optoelectronics, 9, 247-252. http://dx.doi.org/10.1166/jno.2014.1574 Casian, A. and Andronic, S. (2012) Phonons near Peierls Phase Transition in Quasi-One-Dimensional Organic Crystals. Proceedings of the 4th International Conference on Telecommunication, Electronics and Informatics, Chisinau, 17-20 May 2012, 258. (In Rumanian) Andronic, S. and Casian, A. (2013) Peierls Structural Transition in Quasi-One-Dimensional Organic Crystals. Modavian Journal of Physical Sciences, 12, 192. Andronic, S., Casian, A. and Dusciac, V. (2015) Peierls Structural Transition in Q1D Crystals of TTF-TCNQ Type for Different Values of Carrier Concentration. Materials Today: Proceedings, 2, 3829-3835. http://dx.doi.org/10.1016/j.matpr.2015.08.009 Tiedje, T., et al. (1977) Temperature Dependence of Sound Velocity in TTF-TCNQ. Solid State Communications, 23, 713. http://dx.doi.org/10.1016/0038-1098(77)90478-1", null, "" ]
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https://www.statology.org/covariance-matrix-excel/
[ "# How to Create a Covariance Matrix in Excel\n\nCovariance is a measure of how changes in one variable are associated with changes in a second variable. Specifically, it’s a measure of the degree to which two variables are linearly associated.\n\nThe formula to calculate the covariance between two variables, X and Y is:\n\nCOV(X, Y) = Σ(x-x)(y-y) / n\n\nA covariance matrix is a square matrix that shows the covariance between many different variables. This can be an easy, useful way to understand how different variables are related in a dataset.\n\nThe following example shows how to create a covariance matrix in Excel using a simple dataset.\n\n### How to Create a Covariance Matrix in Excel\n\nSuppose we have the following dataset that shows the test scores of 10 different students for three subjects: math, science, and history.\n\nTo create a covariance matrix for this dataset, click on the Data Analysis option in the top right of Excel under the Data tab.\n\nNote: If you don’t see the Data Analysis option, you need to first load the Data Analysis Toolpak.\n\nOnce you click this option, a new window will appear. Click on Covariance.\n\nIn the Input Range box, type “\\$A\\$1:\\$C\\$11”, since this is the range of cells where our dataset is located. Check the box that says Labels in first row to tell Excel that the labels for our variables are located in the first row. Then, in the Output Range box, type any cell where you would like the covariance matrix to appear. I chose cell \\$E\\$2. Then click OK.\n\nThe covariance matrix is automatically generated and appears in cell \\$E\\$2:\n\n### How to Interpret a Covariance Matrix\n\nOnce we have a covariance matrix, it’s rather simple to interpret the values in the matrix.\n\nThe values along the diagonals of the matrix are simply the variances of each subject. For example:\n\n• The variance of the math scores is 64.96\n• The variance of the science scores is 56.4\n• The variance of the history scores is 75.56\n\nThe other values in the matrix represent the covariances between the various subjects. For example:\n\n• The covariance between the math and science scores is 33.2\n• The covariance between the math and history scores is -24.44\n• The covariance between the science and history scores is -24.1\n\nA positive number for covariance indicates that two variables tend to increase or decrease in tandem. For example, math and science have a positive covariance (33.2), which indicates that students who score high on math also tend to score high on science. Likewise, students who score low on math also tend to score low on science.\n\nA negative number for covariance indicates that as one variable increases, a second variable tends to decrease. For example, math and history have a negative covariance (-24.44), which indicates that students who score high on math tend to score low on history. Likewise, students who score low on math tend to score high on history." ]
[ null ]
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https://numbermatics.com/n/459029/
[ "# 459029\n\n## 459,029 is a prime number. Like all primes greater than two, it is odd and has no factors apart from itself and one.\n\nWhat does the number 459029 look like?\n\nAs a prime, it is not composed of any other numbers and has no internal structure.\n\n459029 is a prime number. Like all primes (except two), it is an odd number.\n\n## Prime factorization of 459029:\n\n### 459029\n\nSee below for interesting mathematical facts about the number 459029 from the Numbermatics database.\n\n### Names of 459029\n\n• Cardinal: 459029 can be written as Four hundred fifty-nine thousand and twenty-nine.\n\n### Scientific notation\n\n• Scientific notation: 4.59029 × 105\n\n### Factors of 459029\n\n• Number of distinct prime factors ω(n): 1\n• Total number of prime factors Ω(n): 1\n• Sum of prime factors: 459029\n\n### Divisors of 459029\n\n• Number of divisors d(n): 2\n• Complete list of divisors:\n• Sum of all divisors σ(n): 459030\n• Sum of proper divisors (its aliquot sum) s(n): 1\n• 459029 is a deficient number, because the sum of its proper divisors (1) is less than itself. Its deficiency is 459028\n\n### Bases of 459029\n\n• Binary: 11100000001000101012\n• Base-36: 9U6T\n\n### Squares and roots of 459029\n\n• 459029 squared (4590292) is 210707622841\n• 459029 cubed (4590293) is 96720909405081389\n• The square root of 459029 is 677.5167894599\n• The cube root of 459029 is 77.1400722425\n\n### Scales and comparisons\n\nHow big is 459029?\n• 459,029 seconds is equal to 5 days, 7 hours, 30 minutes, 29 seconds.\n• To count from 1 to 459,029 would take you about five days.\n\nThis is a very rough estimate, based on a speaking rate of half a second every third order of magnitude. If you speak quickly, you could probably say any randomly-chosen number between one and a thousand in around half a second. Very big numbers obviously take longer to say, so we add half a second for every extra x1000. (We do not count involuntary pauses, bathroom breaks or the necessity of sleep in our calculation!)\n\n• A cube with a volume of 459029 cubic inches would be around 6.4 feet tall.\n\n### Recreational maths with 459029\n\n• 459029 backwards is 920954\n• 459029 is a twin prime! Its twin is 459031\n• The number of decimal digits it has is: 6\n• The sum of 459029's digits is 29\n• More coming soon!\n\nMLA style:\n\"Number 459029 - Facts about the integer\". Numbermatics.com. 2022. Web. 2 July 2022.\n\nAPA style:\nNumbermatics. (2022). Number 459029 - Facts about the integer. Retrieved 2 July 2022, from https://numbermatics.com/n/459029/\n\nChicago style:\nNumbermatics. 2022. \"Number 459029 - Facts about the integer\". https://numbermatics.com/n/459029/\n\nThe information we have on file for 459029 includes mathematical data and numerical statistics calculated using standard algorithms and methods. We are adding more all the time. If there are any features you would like to see, please contact us. Information provided for educational use, intellectual curiosity and fun!\n\nKeywords: Divisors of 459029, math, Factors of 459029, curriculum, school, college, exams, university, Prime factorization of 459029, STEM, science, technology, engineering, physics, economics, calculator, four hundred fifty-nine thousand and twenty-nine.\n\nOh no. Javascript is switched off in your browser.\nSome bits of this website may not work unless you switch it on." ]
[ null ]
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http://physics.oregonstate.edu/portfolioswiki/activities:guides:cfveffkin
[ "Navigate back to the activity.\n\n## Interpreting Effective Potential Plots: Instructor's Guide\n\n### Main Ideas\n\nUnderstanding how a graph of effective potential is connected to actual motion.\n\nEstimated Time: 15 minutes\n\nA student is invited to “act out” motion corresponding to a plot of effective potential vs. distance. The student plays the role of the “Earth” while the instructor plays the “Sun”.\n\n### Prerequisite Knowledge\n\n• An introduction to graphs of energy vs. distance.\n• An introduction to angular momentum and its conservation in orbital motion.\n\n### Props/Equipment\n\n• An energy graph (energy vs. distance) of the effective potential of a generic planetary orbit drawn on the blackboard.\n\n### Activity: Introduction\n\nWe typically begin this activity with a lecture about the classical equations of orbital motion, specifically a derivation that reformulates 2-D equations of orbital motion to 1-D by using the effective potential.\n\nJust before initiating the activity, the following plot is made on the board as a reference for the student. It may be useful to contrast this plot with one for the harmonic oscillator since that case is the most familiar potential energy plot.\n\nThis is an 8 minute video clip of the activity cfveffkin.wmv\n\n### Activity: Student Conversations\n\n• It is important to select the student “volunteer” carefully. It seems to work best when the volunteer is confident enough to be involved in a discussion in front of the class (without being overly embarrassed about making mistakes), but also will not immediately come to a correct answer. Avoid students with a strong interest in astronomy.\n• We often find that the student volunteer will initially act out the orbital motion based on the common knowledge that planets make elliptical orbits. The volunteer should be directed to explain how this motion is related to the graph. (You can ask, “Is that what the graph says?”).\n• Almost all students interpret the graph to be back-and-forth oscillatory motion - and laughter often accompanies this clearly inaccurate orbit.\n• The student volunteer should be specific about how the graph indicates how close/far he/she gets to the “sun”.\n• The student volunteer should be asked to identify where the “sun” is located on the energy graph. This helps the student to understand what it means to fully articulate the meaning of the graph.\n\n### Activity: Wrap-up\n\nNo separate wrap-up discussion is necessary, but the take home message should be that the plot of the effective potential has buried in it information about the angular momentum, and that the corresponding energy graph only tells you about the radial motion.\n\nIt is valuable to discuss the specific parts of the conservation of energy equation $$E = {{1}\\over{2}} \\mu \\dot{r}^2 + {{1}\\over{2}} {l^2 \\over \\mu r^2} - {k \\over r}$$ explicity identifying the effective potential ${{1}\\over{2}} {l^2 \\over \\mu r^2} - {k \\over r}$, the radial kinetic energy ${{1}\\over{2}} \\mu \\dot{r}^2$, and the $\\phi$ component of the kinetic energy ${{1}\\over{2}} {l^2 \\over \\mu r^2}$.\n\n### Extensions\n\nThis activity works particularly well when sequenced with other activities.\n\n##### Views\n\nNew Users\n\nCurriculum\n\nPedagogy\n\nInstitutional Change\n\nPublications\n\n##### Toolbox", null, "" ]
[ null, "http://physics.oregonstate.edu/portfolioswiki/lib/exe/indexer.php", null ]
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https://www.science20.com/alpha_meme/math_puzzle_column_science_20-105291
[ "Richard Mankiewicz, our man in Bangkok, also known as Red Man (see his profile – no no, not because of Bangkok’s red light district - that would be Stickman, not Red Man!) has started a Math Puzzle Column on Science2.0, first entry: Circles Stuck in a Triangle.\n\nRichard has another webpage where he proved to be able to come up with a lot more puzzles, so if we encourage him, he may well do a darn good job here, too - so go there and encourage him.\n\nHe asks … , well go over there and have a look already.  Here is my solution, but I only tell you hints about how to get it:\n\nConsider that the circles touch the base of the triangle, thus the heights a, b, and c (he demands a > b > c) all go straight up (right angles) from the base of the outer triangle to the circle’s centers.  Circles are everywhere tangential to their radius, therefore, when two circles touch, the radius of one circle, say a, is on the same line as that of the touching one, say b, so they make a longer line, here a + b.  This gives a bunch of right triangles to play with (Next picture provided by Derek Potter; below I used Mathematica5 for the images):", null, "The Pythagoras theorem applied to the red triangle is\n\n(a + b)2 = (a - b)2 + [x + y]2\n\nwhere x and y are lengths (both parallel to the base of the triangle whose area is asked) of another two such triangles (blue and green in Derek's picture), thus resulting in\n\n(a + b)2 = (a - b)2 + [2 (b*c)0.5 + 2 (a*c)0.5 ]2\n\nRed Man wants integer numbers, but there are square roots(!).  Thus, the integers should be already squares.  The first case would be c = 1 (= 1*1), which leaves b = 4 (= 2*2), which makes also a = b*c = 4, and a triangle cannot be had (or it would have infinite area):", null, "", null, "The second case is c = 4, so b = 9, which makes a = b*c = 36:", null, "", null, "But Richard explicitly demands the next case, namely c = 9.  This leaves b = 16, and thus a = b*c = 144:", null, "", null, "Now again, an outer triangle cannot be had (if it's base is to still touch all three circles), or in other words, the “triangle’s” area would be infinite, because it opens up instead of having a top.\n\nDon’t agree?  Well maybe I am just trolling.  Always think for yourself!  Look at the links below for more Didactic Challenges.\n\n-------------------\n\nUpdate: Red Man does in fact not quite agree, because that all circles touch the base of the triangle was not really a strict requirement, and so he would not have to be red-faced now (which is of course no longer an option for Red Man):", null, "" ]
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https://cosmolearning.org/courses/ap-statistics-lessons-from-mr-tarrou/video-lectures/
[ "", null, "", null, "# AP Statistics Lessons with Mr. Tarrou\n\n## Video Lectures\n\nDisplaying all 79 video lectures.\nI. Introduction; Displaying Data\nLecture 1", null, "Play Video\nStem Plots in Statistics\nAn introduction to the benefits, construction, and interpretation of stem plots.\nLecture 2", null, "Play Video\nHistograms in Statistics\nIntroducing the uses of histograms in statistics, how to construct them and interpret them.\nLecture 3", null, "Play Video\nMaking histograms, boxplots,and timeplots with a graphing calculator\nAn introduction to making histograms and boxplots with the TI-83 and TI-84.\nLecture 4", null, "Play Video\nCatagorical Graphs in Statistics\nAn introduction to pie charts and bar graphs. I talk about their construction and the pros and cons of each type of graph. Please excuse my grammatical error on the third bullet under pie charts...catagory's relation.\nII. Describing Distributions\nLecture 5", null, "Play Video\nDescribing Distributions in Statistics\nThe four key points are discussed when describing distributions in statistics...Shape, Center, Spread, and Outliers. Please forgive the misspelling of DESCRIBED in the video.TIP to identify Left & Right Skewness: (Thanks LeBadman:) Left: Mean is less than Median is less than Mode Symmetrical: Mean, Median and Mode are approximately equal Right: Mean is greater than Median is greater than ModeYou just take: Mean, Median, Mode If it's left skewed, you will see the inequalities pointing to the left. If it's right skewed, you will see the inequalities pointing to the right.\nLecture 6", null, "Play Video\nDetermining Skewness In Ogive Graphs\nI help you identify left skewness, right skewness, and bell curves in an Ogive graph. At 6:40 I said \"this is left skewed\"- that is incorrect. Skewness is determined by the direction of the tail. In the histogram, the tail tapers off to the right, so it is right skewed.\nLecture 7", null, "Play Video\nResistance, Mean, Median, 5 Number Summary and BoxPlots\nI start going over 5 number summary of distributions, define resistance, and box plots.\nIII. Density Curves & Normal Distributions\nLecture 8", null, "Play Video\nStandard Deviation Preview and IQR Test\nI overview the definition of standard deviaiton and introduce the IQR test in statistics.\nLecture 9", null, "Play Video\nDistribution Shapes, Ogive Graphs, and Time Plots\nA review of the shapes of distributions and the relationships between the three measures of center. Also included is an intro to the Ogive graph and Time Plots.\nLecture 10", null, "Play Video\nStandard Deviation and Linear Transformations\nAn introdution to Standard Deviation, it's properties, and the linear transformation process. LINEAR TRANSFORMATION AT 9:01\nLecture 11", null, "Play Video\nDensity Curves, Empirical Rule & Normality, Z-score Intro\nI define density curves. I also define Normality through the Empirical Rule. We then introduce the Z-score formula, which is a linear transformation, and show how is allows us to use the Standard Normal Distribution to find p-values. DENSITY CURVES 0:04 EMPERICAL RULE 3:48 Z-SCORE INTRO 6:50 EXAMPLE 11:01 I have no idea what happened to the end of my lesson.  If you need help finding area under a bell curve you can check out https://www.youtube.com/watch?v=_86q-hn_3DQ&list=PLC84780005...\nLecture 12", null, "Play Video\nNormal Probability Plots & the TI-84\nI show you how to make a Normal Probability Plot on your TI-83 or TI-84 calculator. We will see how this graph verifies normality and how it shows left and right skewness. You will also be reminded of how to view boxplots and histograms on the same screen shot to get used to comparing the two types of graphs.\nLecture 13", null, "Play Video\nz-score Calculations & Percentiles in a Normal Distribution\nI show you how to calculate Z-scores and find areas under the bell curve...p-values. I will also show you how to find statistics from areas under the curve...such as quartiles.You can find p-values with a calculator as well. This is what it looks like on a TI-NSPIRE TI-NSPIRE Z score to Pval & Pval to Zscore NormCDF invNorm https://www.youtube.com/watch?v=-kmJRVr-ZQ8\nLecture 14", null, "Play Video\nTI-NSPIRE Z score to Pval & Pval to Zscore NormCDF invNorm\nI show you how to get a p-value from a z score, and get a z score from a p-value using a TI-NSPIRE using the NormCDF(lower limit, upper limit, mean, standard deviation) command and invNorm(p-value, mean, standard deviation) command.\nIV. Scatter Plots & Linear Regression Model\nLecture 15", null, "Play Video\nScatter Plot Intro and Lurking Variables defined\nI introduce the structure of scatterplots and explain what characteristics you will need to use to intrepret them. I discuss how lurking variables can help to form the patterns that we see. I also go over the two type of outliers we may see in scatterplots.\nLecture 16", null, "Play Video\nIntro of Corellation \"r\" to measure linear strength\nI introduce correlation and how it measures the strength and direction of a linear relationship. I also discuss the many properties of correlation you must be familiar with. Coefficient of Determination is also defined.In the last example about MPG, r = -.8 and not positive .8 as written.\nLecture 17", null, "Play Video\nOutlier vs Influential Point\nI compare the affects of an outlier and an influencial point on the regression line with the help of a TI-NSpire\nLecture 18", null, "Play Video\nRegression lines, Residual plots, and Correlation with TI-NSpire\nI introduce the regression line and talk about some of it's key characteristics before showing you how to find it's equation with a TI-NSpire calculator.\nLecture 19", null, "Play Video\nLeast Squares Regression Line Notes\nI give notes of the concepts and properties of Least Squares Regression lines in Statistics, residuals, and preview minitab output.\nLecture 20", null, "Play Video\nRegression Lines and Correlation with TI-84\nI make a scatterplot, calculate the Least Squares Regression Line, find correlation, and then make a Residual Plot to verify the linearity of the scatter plot.\nLecture 21", null, "Play Video\nLog Transformation Part 1\nI introduce log transformations and show how to make curved exponential data linear so that we can analyze the data with a linear regression line. Part 2 is transforming data that follows a power function.\nLecture 22", null, "Play Video\nLog Transformations Part 2\nI finish my log transformation introduction by introducing notes for Power Functions.\nLecture 23", null, "Play Video\nLog Transformations with a TI-NSPIRE\nI create data from expontial and power equations, make scatter plots out of that data and then show you how to transform those plots so they are linear. This is known as log transformations in statistics.\nV. Using of Graphing Calculator\nLecture 24", null, "Play Video\nHistogram, Boxplot, Dot Plot, & Normal Prob Plot on TI-NSPIRE\nI show a quick video on entering univariate quantitative data in a TI-NSPIRE, and then I make a dot plot, histogram, box plot, and normal probability plot.\nLecture 25", null, "Play Video\nScatter Plot, Linear Reg, Correlation & Residuals with TI-NSPIRE\nI show you how to make a scatter plot, a least squares regression line, and a residual plot with a TI-NSPIRE\nLecture 26", null, "Play Video\nLog Transformations with TI-84\nLog transformation demonstration with TI-84/83. This video will also review how to find least squares regression lines and making residual plots. I will also show how to remove the log function from your linear regression line to make either an exponential or power model for the original data.\nVI. Introduction to Categorical Variables\nLecture 27", null, "Play Video\nI show an example of Simpson's Paradox. This is when an observed relationship is reversed when a third lurking variable is brought into the picture.Kidney Stone data referenced from: ^ C. R. Charig, D. R. Webb, S. R. Payne, O. E. Wickham (29 March 1986). \"Comparison of treatment of renal calculi by open surgery, percutaneous nephrolithotomy, and extracorporeal shockwave lithotripsy\". Br Med J (Clin Res Ed)\nLecture 28", null, "Play Video\nRelationship between catagorical variables in a 2 way table\nI show you how to analyze catagorical data in a 2 way table. We will find marginal distributions, conditional probabilities, and bar graphs.\nLecture 29", null, "Play Video\nLog Tranformation with TI-NSPIRE\nI go over how to to do a Log transformation with a TI-NSPIRE, explain how to determine the explanatory & response variable, and show how to remove the Log function to get a model for the original curved data.\nVII. Evidence of Causation\nLecture 30", null, "Play Video\nCausation Defined & 5 Key Checks for Signs of Causattion\nI defined causation, review the two types of lurking variables, and I go over the 5 checks for evidence of causation.\nVIII. Sampling Techniques and Experimental Design\nLecture 31", null, "Play Video\nSampling Techniques Part 1\nI define and discuss the differences of observational studies and experiments. I then discuss the difference between a sample and a census, then introduce two types of sampling techniques that yield biased results...Voluntary Response and Convenience Sampling.\nLecture 32", null, "Play Video\nSampling Techniques Part 2\nI continue to introduce sampling techniques. In this video I go over Stratified Random Samples, Stratified Random Sample, Cluster Samples, and Multistage Samples.\nLecture 33", null, "Play Video\nCautions about Sample Surveys, Causes of Bias, and Inference defined\nI finish my three part introduction of Sample Surveys. In this lecture I define Undercoverage, Non-Response, discuss causes of Biased Results, define Inference, and preview Sample Distributions.\nLecture 34", null, "Play Video\nSampling Techniques & Cautions (Full Length)\nI define and discuss the differences of observational studies and experiments. I then discuss the difference between a sample and a census. I introduce two types of sampling techniques that yield biased results...Voluntary Response and Convenience Sampling. I discuss Stratified Random Samples, Stratified Random Sample, Cluster Samples, and Multistage Samples. I finish by defining Undercoverage, Non-Response, discuss causes of Biased Results, define Inference, and preview Sample Distributions.\nLecture 35", null, "Play Video\nExperimental Design Part 1\nIn part one of this lecture I cover basic definitions related to experiments, the 3 Principles of Experimental Design, and define Statistical Significance.\nLecture 36", null, "Play Video\nExperimental Design Part 2\nI finish my lecture on Experimental Design with an introduction to Block Design, Matched Pairs Design, and Double Blind Experiments.\nLecture 37", null, "Play Video\nSimulation Notes for Statistics\nI introduce the concept of simulations and explain how they can be used to answer difficult statistcs questions, save money, or time.\nIX. Introduction to Probabilities\nLecture 38", null, "Play Video\nIntro to Probabilities in Statistics (Full Length)\nAn AP Statistics lecture introducing probabilities, randomness, Law of Large Numbers, Probability Model, Tree Diagram, 5 Rules of Probability,etc.\nLecture 39", null, "Play Video\nIntro to Probabilities Part 1\nAn AP Statistics lecture introducing probabilities, randomness, Law of Large Numbers, Probability Model, Tree Diagram, 5 Rules of Probability,etc.\nLecture 40", null, "Play Video\nIntro to Probabilities Part 2\nAn AP Statistics lecture introducing probabilities, randomness, Law of Large Numbers, Probability Model, Tree Diagram, 5 Rules of Probability,etc.\nLecture 41", null, "Play Video\nIntro to Probabilities Part 3\nAn AP Statistics lecture introducing probabilities, randomness, Law of Large Numbers, Probability Model, Tree Diagram, 5 Rules of Probability,etc.\nLecture 42", null, "Play Video\nGeneral Probability Rules (Full Length)\nI go over the General Addition and Multiplication Rules in Statistics. I show how a Venn diagram can help with the General Addition Rule. I also explain how we started to learn conditional probabilities when we did row and column percents in 2 way tables.\nLecture 43", null, "Play Video\nGeneral Probability Rules Part 2\nI go over the General Addition and Multiplication Rules in Statistics. I show how a Venn diagram can help with the General Addition Rule. I also explain how we started to learn conditional probabilities when we did row and column percents in 2 way tables.\nLecture 44", null, "Play Video\nGeneral Probability Rules Part 1\nI go over the General Addition and Multiplication Rules in Statistics. I show how a Venn diagram can help with the General Addition Rule. I also explain how we started to learn conditional probabilities when we did row and column percents in 2 way tables.\nX. Discrete & Continuous Variables\nLecture 45", null, "Play Video\nDiscrete & Continuous Random Variables (Full Length)\nI define and compare the two types of Random Variables in AP Statistics...Discrete & Continuous. The formulas for finding the mean and standard deviation of a discrete random variables are introduced, and I also review the old mean and standard deviation formulas that the calculators does when you do 1 Var Stats. Many old concepts are reviewed in this video such as probability models, z-scores, normality, degrees of freedom, etc.\nLecture 46", null, "Play Video\nDiscrete & Continuous Variables Part 1\nI define and compare the two types of Random Variables in AP Statistics...Discrete & Continuous. The formulas for finding the mean and standard deviation of a discrete random variables are introduced, and I also review the old mean and standard deviation formulas that the calculators does when you do 1 Var Stats. Many old concepts are reviewed in this video such as probability models, z-scores, normality, degrees of freedom, etc.\nLecture 47", null, "Play Video\nDiscrete & Continuous Variables Part 2\nI define and compare the two types of Random Variables in AP Statistics...Discrete & Continuous. The formulas for finding the mean and standard deviation of a discrete random variables are introduced, and I also review the old mean and standard deviation formulas that the calculators does when you do 1 Var Stats. Many old concepts are reviewed in this video such as probability models, z-scores, normality, degrees of freedom, etc.\nLecture 48", null, "Play Video\nTI-NSPIRE Discrete Random Variable Mean & Standard Deviation\nI show you how to find the mean and standard deviation of a discrete random variable with your TI-NSPIRE.\nXI. Combining Means and Variances\nLecture 49", null, "Play Video\nCombining Means and Variance in Statistics\nI review how linear transformations affect the mean, standard deviation, and the variance of data. I then introduce the rules for combining the means and variance of mutliple sets of data and finish with an example.\nLecture 50", null, "Play Video\nCombining Means and Variance Examples\nI do two examples of z- score calculations that involve combining means and variance. EXAMPLES AT 0:30 8:20\nXII. Binomial and Geometric Setting\nLecture 51", null, "Play Video\nBinomial Setting & Binomial Distribution in Statistics Pt 1\nIn a two part video I introduce the Binomial Setting and Distribution where x is defined as the number of successes. This lecture also includes the formulas and examples for of the Binomial Coefficient and the Binomial Probability Formula. I also go over how to use the binompdf(n,p,k) and binomcdf(n,p,k) commands in a calculator.\nLecture 52", null, "Play Video\nBinomial Setting & Binomial Distribution in Statistics Pt 2\nIn part 2 of my lecture about the Binomial Setting, I show how to set up a probability distribution function for a binomial variable when x is defined as the number of successes. I then introduce how to find probabilities of binomial events through Normal Approximation and compare this process with the exact values we get with binompdf and binomcdf from a calculator.\nLecture 53", null, "Play Video\nGeometric Setting & Distribution in Statistics\nI introduce the Geometric Setting & Distribution in statistics and compare it to the Binomial Setting. This video includes setting up a PDF, examples of finding probabilities, and a non-example of a geometric setting.\nXIII. One Sample Mean & Central Limit Theorem One Sample Proportions\nLecture 54", null, "Play Video\nCalculating 1-Var Statistics with a TI-NSPIRE\nI show you how to calculate mean, standard deviation, and find the 5-number summary with a TI-NSPIRE and the 1-Var Statistics command.\nLecture 55", null, "Play Video\nIntro to Sample Mean Distribution and Central Limit Theorem\nI introduce the Central Limit theorem and explain how it helps to set up the distribution of sample means. This video only discusses setting up the distribution of a one sample mean when given the population standard deviation. I hint of the upcoming topic of t-distributions\nLecture 56", null, "Play Video\n1 Sample Mean Z-Test Example\nI work through a 1 sample mean z-test. I include the required checks for working with means, preview how to make a hypothesis statement, and compare how a z-score with means compares to a z-score test with a single piece of data.\nLecture 57", null, "Play Video\nIntroduction of Sample Proportions\nA set of notes to help you understand the Binomial Setting and how to set up binomial proportions.\nLecture 58", null, "Play Video\nExample of 1 Sample Proportion Z-test\nI do multiple examples of Normal Approximation calculations of sample proportions. I also compare this process to using the binomcdf(n,p,k) commands in you calculator.\nLecture 59", null, "Play Video\nN-SPIRE 1 Proportion Z-Test Example\nI compare how to work 1 sample proportion z-tests with Normal Approximation and with the TI-NSPIRE calculator\nXIV. Understanding One Sample Confidence Intervals\nLecture 60", null, "Play Video\nIntro to Confidence Intervals & 1 Sample Mean z Interval\nI introduce the concept of confidence intervals and finish with an example of a one sample mean z interval. A note about Margin of Error: The Margin of Error accounts for random variability, NOT sampling errors, non-response, or undercoverage, etc. EXAMPLE AT 16:50\nLecture 61", null, "Play Video\n1 Sample Mean t-Confidence Interval\nI introduce the t-distribution and work through an example of a 1 Sample Mean t-Confidence Interval. EXAMPLE AT 9:34\nLecture 62", null, "Play Video\nMatched Pairs t Confidence Interval\nI do an example of setting up a Matched Pairs Mean t-Confidence Interval. The sixth student's score was mis-copied and should be a 95 instead of a 92. Sorry for the small copy error.\nLecture 63", null, "Play Video\n1 Sample Proportion z Confidence Interval\nI work through and example of setting up a 1 sample z confidence interval.\nXV. One Sample Significance Tests & Power\nLecture 64", null, "Play Video\nSignificance Hypothesis Test Intro & Matched Pairs t-Test\nI introduce the basics of setting up a significance test, such as defining a null and alternative hypothesis, checking conditions, etc. I finish by working through an example of a matched pairs t-test. EXAMPLE AT 19:00\nLecture 65", null, "Play Video\n2 Sided Hypothesis Tests & Confidence Intervals\nI explain the relationship between 2-sided significance tests and confidence intervals.\nLecture 66", null, "Play Video\nType 1 Error Type 2 Error Power 1 Sample Mean Hypothesis z-Test\nI define what Type 1 and Type 2 errors and do an example. I then introduce power and work through and example of finding the power of a 1 sample mean z-test and the probability of a Type 2 error. The x's in the first half of my Power example should have bars on top of them to represent sample means.\nLecture 67", null, "Play Video\nPower of a T Test 1 Sample Mean\nI explain the differences of finding Power of a t-Test compared to Power of a z-Test.\nLecture 68", null, "Play Video\nPower 1 Sample Proportion z-Test (2 Sided)\nI work through an example of finding power of a 1 sample proportion z test which is 2 sided.\nXVI. Two Sample Significance Tests & Confidence Intervals\nLecture 69", null, "Play Video\n2 Sample Mean t-test & Confidence Interval\nI introduce how to compare 2 means in statistics. I cover the goals of the comparison, the required conditions that need to be checked, robustness, how to combine means and variance, and give the formulas for z-test...t-test...and confidence intervals. I finish with a few examples. EXAMPLE begins at 22:48\nLecture 70", null, "Play Video\n2 Sample Mean Hypothesis t Test & Confidence Interval Example w/ TI-NSPIRE\nI work through a 2 sample mean t-test and a 2 sample mean t-interval using a TI-NSPIRE. The video starts with a description of the setting, hypothesis statement, and conditions check. Why? Because the numbers out of your calculator mean nothing if you can't do the test in the first place!!!\nLecture 71", null, "Play Video\n2 Proportions Pooled Hypothesis z-test & Confidence Intervals\nI introduce how to compare 2 sample proportions through the use of z-tests and confidence intervals. I finish with a 2 Sample Pooled z-test. EXAMPLES AT 11:09 21:28\nXVII. Chi-Square Test\nLecture 72", null, "Play Video\nChi Square Goodness of Fit Test\nI introduce the Chi Square Goodness of Fit test and finish with two examples. EXAMPLES AT 5:10 15:55\nLecture 73", null, "Play Video\nTI-NSPIRE Chi Square Goodness of Fit Test\nUsing an excerpt from a previous video I show you how to do a Chi Square Goodness of Fit test with the TI-NSPIRE.\nLecture 74", null, "Play Video\nChi Square Test for Independence & Homogeneity\nI introduce the concept of the Chi Square Test on 2 Way Tables. I work through 2 examples. 1) Chi Square Test for Homogeneity of Populations 2) Chi Square Test for Independence EXAMPLES AT 0:10 3:24 10:36\nLecture 75", null, "Play Video\nTI-NSPIRE Chi Square Test on 2 Way Tables\nI use an excerpt from a previous video to show you how to do a Chi Square Test on a 2 way table.\nLecture 76", null, "Play Video\nChi Square Calculation by Hand\nI work through a Chi Square test on a 2 way table without much aid from a calculator.\nXVIII. Linear Regression t-Test and Confidence\nLecture 77", null, "Play Video\nLinear Regression t test and Confidence Interval Corrected\nI introduce the Linear Regression t test and confidence intervals for the slope of a regression line.\nLecture 78", null, "Play Video\nLinear Regression t test and Confidence Interval\nCorrected Version for iPad Viewers at http://www.youtube.com/watch?v=vWgKDhki5Sw&feature=share&lis... introduce the Linear Regression t test and confidence intervals for the slope of a regression line. On the third screen I miscopied the denominator in the formula of Standard Error about the Least-Squares Line. The denominator should be n-2 and not n. I have an annotation correction, but you will not see it without Flash like on an iPad.\nLecture 79", null, "Play Video\nTI-NSPIRE Linear Regression t-test & Confidence Interval of slope\nI work through an example of doing a linear regression t-test with your TI-NSPIRE and making a confidence interval to estimate the true slope of a regression line. For some reason I didn't find it necessary to properly round the numbers on the screen as I read through my example of how to use this calculator." ]
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https://www.geeksforgeeks.org/array-copy-in-java/?ref=lbp
[ "# Array Copy in Java\n\n• Difficulty Level : Easy\n• Last Updated : 26 Oct, 2021\n\nGiven an array, we need to copy its elements in a different array, to a naive user below way comes into mind which is however incorrect as depicted below as follows:\n\n```// Java Program to Illustrate Wrong Way Of Copying an Array\n\n// Input array\nint a[] = { 1, 8, 3 };\n\n// Creating an array b[] of same size as a[]\nint b[] = new int[a.length];\n\n// Doesn't copy elements of a[] to b[], only makes\n// b refer to same location\nb = a;```\n\nOutput:", null, "Output Explanation: When we do “b = a”, we are actually assigning a reference to the array. Hence, if we make any change to one array, it would be reflected in other arrays as well because both a and b refer to the same location. We can also verify it with code as shown below as follows:\n\nExample:\n\n## Java\n\n `// A Java program to demonstrate that simply``// assigning one array reference is incorrect``public` `class` `Test {``    ``public` `static` `void` `main(String[] args)``    ``{``        ``int` `a[] = { ``1``, ``8``, ``3` `};` `        ``// Create an array b[] of same size as a[]``        ``int` `b[] = ``new` `int``[a.length];` `        ``// Doesn't copy elements of a[] to b[],``        ``// only makes b refer to same location``        ``b = a;` `        ``// Change to b[] will also reflect in a[]``        ``// as 'a' and 'b' refer to same location.``        ``b[``0``]++;` `        ``System.out.println(``\"Contents of a[] \"``);``        ``for` `(``int` `i = ``0``; i < a.length; i++)``            ``System.out.print(a[i] + ``\" \"``);` `        ``System.out.println(``\"\\n\\nContents of b[] \"``);``        ``for` `(``int` `i = ``0``; i < b.length; i++)``            ``System.out.print(b[i] + ``\" \"``);``    ``}``}`\n\nOutput\n\n```Contents of a[]\n2 8 3\n\nContents of b[]\n2 8 3 ```\n\nMethods:\n\nWe have seen internal working while copying elements and edge cases to be taken into consideration after getting through errors as generated above, so now we can propose out correct ways to copy array as listed below as follows:\n\n1. Iterating each element of the given original array and copy one element at a time\n2. Using clone() method\n3. Using arraycopy() method\n4. Using copyOf() method of Arrays class\n5. Using copyOfRange() method of Arrays class\n\nMethod 1: Iterating each element of the given original array and copy one element at a time. With the usage of this method, it guarantees that any modifications to b, will not alter the original array a, as shown in below example as follows:\n\nExample:\n\n## Java\n\n `// Java program to demonstrate copying by``// one by one assigning elements between arrays` `// Main class``public` `class` `GFG {` `    ``// Main driver method``    ``public` `static` `void` `main(String[] args)``    ``{``        ``// Input array a[]``        ``int` `a[] = { ``1``, ``8``, ``3` `};` `        ``// Create an array b[] of same size as a[]``        ``int` `b[] = ``new` `int``[a.length];` `        ``// Copying elements of a[] to b[]``        ``for` `(``int` `i = ``0``; i < a.length; i++)``            ``b[i] = a[i];` `        ``// Changing b[] to verify that``        ``// b[] is different from a[]``        ``b[``0``]++;` `        ``// Display message only``        ``System.out.println(``\"Contents of a[] \"``);` `        ``for` `(``int` `i = ``0``; i < a.length; i++)``            ``System.out.print(a[i] + ``\" \"``);` `        ``// Display message only``        ``System.out.println(``\"\\n\\nContents of b[] \"``);` `        ``for` `(``int` `i = ``0``; i < b.length; i++)``            ``System.out.print(b[i] + ``\" \"``);``    ``}``}`\n\nOutput\n\n```Contents of a[]\n1 8 3\n\nContents of b[]\n2 8 3 ```\n\nMethod 2: Using Clone() method\n\nIn the previous method we had to iterate over the entire array to make a copy, can we do better? Yes, we can use the clone method in Java\n\nExample:\n\n## Java\n\n `// Java program to demonstrate Copying of Array``// using clone() method` `// Main class``public` `class` `GFG {` `    ``// Main driver method``    ``public` `static` `void` `main(String[] args)``    ``{``        ``// Input array a[]``        ``int` `a[] = { ``1``, ``8``, ``3` `};` `        ``// Copying elements of a[] to b[]``        ``int` `b[] = a.clone();` `        ``// Changing b[] to verify that``        ``// b[] is different from a[]``        ``b[``0``]++;` `        ``// Display message for better readability``        ``System.out.println(``\"Contents of a[] \"``);` `        ``for` `(``int` `i = ``0``; i < a.length; i++)``            ``System.out.print(a[i] + ``\" \"``);` `        ``// Display message for better readability``        ``System.out.println(``\"\\n\\nContents of b[] \"``);` `        ``for` `(``int` `i = ``0``; i < b.length; i++)``            ``System.out.print(b[i] + ``\" \"``);``    ``}``}`\n\nOutput\n\n```Contents of a[]\n1 8 3\n\nContents of b[]\n2 8 3 ```\n\nMethod 3: Using arraycopy() method\n\nWe can also use System.arraycopy() Method. The system is present in java.lang package. Its signature is as :\n\n```public static void arraycopy(Object src, int srcPos, Object dest,\nint destPos, int length)```\n\nParameters:\n\n• src denotes the source array.\n• srcPos is the index from which copying starts.\n• dest denotes the destination array\n• destPos is the index from which the copied elements are placed in the destination array.\n• length is the length of the subarray to be copied.\n\nExample:\n\n## Java\n\n `// Java program to demonstrate array``// copy using System.arraycopy()` `// Main class``public` `class` `GFG {` `    ``// Main driver method``    ``public` `static` `void` `main(String[] args)``    ``{``        ``// Custom input array``        ``int` `a[] = { ``1``, ``8``, ``3` `};` `        ``// Creating an array b[] of same size as a[]``        ``int` `b[] = ``new` `int``[a.length];` `        ``// Copying elements of a[] to b[]``        ``System.arraycopy(a, ``0``, b, ``0``, ``3``);` `        ``// Changing b[] to verify that``        ``// b[] is different from a[]``        ``b[``0``]++;` `        ``// Display message only``        ``System.out.println(``\"Contents of a[] \"``);` `        ``for` `(``int` `i = ``0``; i < a.length; i++)``            ``System.out.print(a[i] + ``\" \"``);` `        ``// Display message only``        ``System.out.println(``\"\\n\\nContents of b[] \"``);` `        ``for` `(``int` `i = ``0``; i < b.length; i++)``            ``System.out.print(b[i] + ``\" \"``);``    ``}``}`\n\nOutput\n\n```Contents of a[]\n1 8 3\n\nContents of b[]\n2 8 3 ```\n\nMethod 4: Using copyOf() method of Arrays class\n\nIf we want to copy the first few elements of an array or a full copy of the array, you can use this method.\n\nSyntax:\n\n`public static int[] copyOf​(int[] original, int newLength) `\n\nParameters:\n\n• Original array\n• Length of the array to get copied.\n\nExample:\n\n## Java\n\n `// Java program to demonstrate array``// copy using Arrays.copyOf()` `// Importing Arrays class from utility class``import` `java.util.Arrays;` `// Main class``class` `GFG {` `    ``// Main driver method``    ``public` `static` `void` `main(String[] args)``    ``{``        ``// Custom input array``        ``int` `a[] = { ``1``, ``8``, ``3` `};` `        ``// Create an array b[] of same size as a[]``        ``// Copy elements of a[] to b[]``        ``int` `b[] = Arrays.copyOf(a, ``3``);` `        ``// Change b[] to verify that``        ``// b[] is different from a[]``        ``b[``0``]++;` `        ``System.out.println(``\"Contents of a[] \"``);` `        ``// Iterating over array. a[]``        ``for` `(``int` `i = ``0``; i < a.length; i++)``            ``System.out.print(a[i] + ``\" \"``);` `        ``System.out.println(``\"\\n\\nContents of b[] \"``);` `        ``// Iterating over array b[]``        ``for` `(``int` `i = ``0``; i < b.length; i++)``            ``System.out.print(b[i] + ``\" \"``);``    ``}``}`\n\nOutput\n\n```Contents of a[]\n1 8 3\n\nContents of b[]\n2 8 3 ```\n\nMethod 5: Using copyOfRange() method of Arrays class\n\nThis method copies the specified range of the specified array into a new array.\n\n`public static int[] copyOfRange​(int[] original, int from, int to)`\n\nParameters:\n\n• Original array from which a range is to be copied\n• Initial index of the range to be copied\n• Final index of the range to be copied, exclusive\n\nExample:\n\n## Java\n\n `// Java program to demonstrate array``// copy using Arrays.copyOfRange()` `// Importing Arrays class from utility package``import` `java.util.Arrays;` `// Main class``class` `GFG {` `    ``// Main driver method``    ``public` `static` `void` `main(String[] args)``    ``{``        ``// Custom input array``        ``int` `a[] = { ``1``, ``8``, ``3``, ``5``, ``9``, ``10` `};` `        ``// Creating an array b[] and``        ``// copying elements of a[] to b[]``        ``int` `b[] = Arrays.copyOfRange(a, ``2``, ``6``);` `        ``// Changing b[] to verify that``        ``// b[] is different from a[]` `        ``// Iterating over array a[]``        ``System.out.println(``\"Contents of a[] \"``);``        ``for` `(``int` `i = ``0``; i < a.length; i++)``            ``System.out.print(a[i] + ``\" \"``);` `        ``// Iterating over array b[]``        ``System.out.println(``\"\\n\\nContents of b[] \"``);``        ``for` `(``int` `i = ``0``; i < b.length; i++)``            ``System.out.print(b[i] + ``\" \"``);``    ``}``}`\n\nOutput\n\n```Contents of a[]\n1 8 3 5 9 10\n\nContents of b[]\n3 5 9 10 ```\n\nLastly, let us do discuss the overview of the above methods:\n\n• Simply assigning references is wrong\n• The array can be copied by iterating over an array, and one by one assigning elements.\n• We can avoid iteration over elements using clone() or System.arraycopy()\n• clone() creates a new array of the same size, but System.arraycopy() can be used to copy from a source range to a destination range.\n• System.arraycopy() is faster than clone() as it uses Java Native Interface\n• If you want to copy the first few elements of an array or a full copy of an array, you can use Arrays.copyOf() method.\n• Arrays.copyOfRange() is used to copy a specified range of an array. If the starting index is not 0, you can use this method to copy a partial array." ]
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http://www.ccodechamp.com/c-program-of-newton-backward-interpolation-formula/
[ "C program of Newton Backward Interpolation Formula\n\n# C program of Newton Backward Interpolation Formula\n\n23218\n12\nSHARE\n\nC program of Newton Backward Interpolation formula : Newton has proposed several methods of estimating the values of any number at certain point by learning the behavior of previous values. Newton’s Backward interpolation formula is one of them. Newton’s backward interpolation is based on interpolating the newton’s polynomial which is sometimes also referred as Newton’s divided differences interpolation polynomial because the coefficients of the polynomial are calculated using divided differences.\n\n(From Wikipedia) :Given a set of k + 1 data points", null, "where no two xj are the same, the interpolation polynomial in the Newton form is a linear combination of Newton basis polynomials", null, "with the Newton basis polynomials defined as", null, "for", null, "and", null, ". The coefficients are defined as", null, "where", null, "is the notation for divided differences.\n\nThus the Newton polynomial can be written as", null, "Now\n\nIf the nodes are reordered as", null, ", the Newton Polynomial becomes:", null, "If", null, "are equally spaced with x=", null, "and", null, "for", null, ",then,", null, "", null, "is called the Newton Backward Divided Difference Formula.\n\nNow Let us see how to implement above logic using . Below which takes number of values of x as input from user and then takes values of x and corresponding values of y. Then it asks user at which point he wish to estimate the value and the displays the output value of N(x) at that point.\n\n### C program of Newton Backward Interpolation Formula :\n\n```#include<stdio.h>\n#include<conio.h>\n#include<math.h>\n#include<process.h>\n#include<conio.h>\n#include<stdlib.h>\n\nint main()\n{\nint n;\nint i,j,k;\nfloat mx,my;\nfloat x,h,x0=0,fun=0,p;\nfloat y0,sum=0,diff;\nfloat y1,y2,y3,y4;\n\nprintf(\"----------------------------------------------------------------------\\n\");\nprintf(\"-------------------made by C code champ ------------------------------\\n\");\nprintf(\"----------------------------------------------------------------------\\n\");\nprintf(\"\\n\\n\\t!! NEWTON'S BACKWARD INTERPOLATION FORMULA !! \");\nprintf(\"\\n\\n Enter the values of x you want to enter -> \");\nscanf(\"%d\",&n);\n\nprintf(\"\\n\\n Enter the value in the form of x : \");\nfor(i=0;i<n;i++)\n{\nprintf(\"\\n Enter the value of x[%d] : \",i+1);\nscanf(\"%f\",&mx[i]);\n}\n\nprintf(\"\\n\\n Enter the value in the form of y : \");\nfor(i=0;i<n;i++)\n{\nprintf(\"\\n Enter the value of y[%d] : \",i+1);\nscanf(\"%f\",&my[i]);\n}\n\nprintf(\"\\n\\n Enter the value of x for which u want the value of y : \");\nscanf(\"%f\",&x);\n\n// Calculation and processing section.\nh=mx-mx;\nfor(i=0;i<n-1;i++)\ndiff[i]=my[i+1]-my[i];\n\nfor(j=2;j<=4;j++)\nfor(i=0;i<n-j;i++)\ndiff[i][j]=diff[i+1][j-1]-diff[i][j-1];\ni=0;\n\nwhile(!mx[i]>x)\ni++;\n\nx0=mx[i];\nsum=0;\n\ny0=my[i];\nfun=1;\n\np=(x-x0)/h;\nsum=y0;\n\nfor(k=1;k<=4;k++)\n{\nfun=(fun*(p-(k-1)))/k;\nsum=sum+fun*diff[i][k];\n}\n\n// Output\nprintf(\"\\n When x = %6.4f , y = %6.8f\\n\\n\",x,sum);\ngetch();\nsystem(\"pause\");\n}```\n\nWe hope you all have enjoyed the C program of Newton Backward Interpolation formula i.e. backward divided difference. If you have any issues with above code, ask us in form of comments.\n\nSHARE\nPrevious articleC program of Booth’s multiplication algorithm\nWell, I am software programmer and love to code. My hobbies is to do Hacking, Coding, Blogging, Web Designing and playing online games. Feel free to contact me at [email protected] or [email protected]" ]
[ null, "http://upload.wikimedia.org/wikipedia/en/math/5/c/e/5ce24ebcbf7048ddd470abb471aba925.png", null, "http://upload.wikimedia.org/wikipedia/en/math/5/c/5/5c51433ce778c70d220394d853d6dd0c.png", null, "http://upload.wikimedia.org/wikipedia/en/math/6/1/8/61892943bf8825cb5779f3f666e9a667.png", null, "http://upload.wikimedia.org/wikipedia/en/math/0/8/1/0818d4c096ad314ff59869c0e49256bd.png", null, "http://upload.wikimedia.org/wikipedia/en/math/3/8/f/38f26f4fbeb56919557f00562ae33156.png", null, "http://upload.wikimedia.org/wikipedia/en/math/b/4/9/b491d0408158e036e9d4e317aaee6e03.png", null, "http://upload.wikimedia.org/wikipedia/en/math/6/d/a/6daef1a01980a186b9c9b04125727b67.png", null, "http://upload.wikimedia.org/wikipedia/en/math/a/c/e/ace3f8ce40c2aded63771a4e8f791263.png", null, "http://upload.wikimedia.org/wikipedia/en/math/7/8/d/78d8d41465087c8f38ddde50299a3c76.png", null, "http://upload.wikimedia.org/wikipedia/en/math/b/2/4/b2467520a5f3d4388ba98c0a1c0482c4.png", null, "http://upload.wikimedia.org/wikipedia/en/math/a/3/6/a36d385c979e4b1946db0c50c7bcb11a.png", null, "http://upload.wikimedia.org/wikipedia/en/math/c/5/f/c5fb9f8035a8612da42aa673117229dc.png", null, "http://upload.wikimedia.org/wikipedia/en/math/b/7/f/b7ffd155af26c8355f15bb7bde06a3e4.png", null, "http://upload.wikimedia.org/wikipedia/en/math/a/a/f/aafdf44bc8739e7b53239a2e37171df3.png", null, "http://upload.wikimedia.org/wikipedia/en/math/5/5/8/558b3271b1189381d8662120c7bbdaa1.png", null, "http://upload.wikimedia.org/wikipedia/en/math/e/9/4/e9416ec60031dbb23241ce109bc9e1db.png", null ]
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https://blog.macuyiko.com/post/2021/does-it-make-sense-to-tune-the-cutoff-of-trees-in-a-random-forests.html
[ "Does It Make Sense to Tune the Cutoff of Trees in a Random Forests?\n\nTL;DR: very likely not.\n\nA student once asked me whether it would make sense to tune the probability cutoff (a.k.a. threshold) for random forests. Let’s explain first what we mean by that exactly. Assume a binary classification setting. Say we’ve trained a single decision tree. We know that the prediction is given by the leaf node, and that a probability P(y=1|x) can be assigned by the number of training examples in leaf node with positive outcome divided by the number of all training examples in leaf node (note that this is a fixed ratio for each leaf node and does not change once the tree is trained). This is not a well-calibrated probability, but does allow to rank predictions.\n\nGiven such a probability P(y=1|x), it is then possible to specify a threshold T so that if P(y=1|x) >= T, we assume the outcome to be 1, and 0 otherwise. We can then tune T (e.g. through cross-validation) to get an optimal cutoff point given a metric we desire to optimise (accuracy, F1, or something else…) 1.\n\nLet us now consider the case of a random forest: N trees are constructed which all provide their prediction for a given instance, after which the majority vote determines the final outcome. Again, a probability P(y=1|x) can be assigned as the number of trees which predicted y=1 divided by N.\n\nHowever, we’ve kind of forgotten about the fact that every tree member itself can output a probability as well. What if we would tune the individual trees with a threshold Tn, with n = 1..N? Would this lead to a better result? The answer is that it might, but only in very specific circumstances, and is hence probably not worth doing.\n\nFirst, most implementations of random forest construct non-pruned trees. E.g. each leaf node relates to one training example. This doesn’t lead to overfit thanks to bootstrapping and random feature subset selection. As such, the probability that P(y=1|x) is either 1 or 0 for each tree, and threshold tuning would not make sense here.\n\nSecond, many implementations (most notably scikit-learn) in fact deviate from the behavior of random forests as originally described. Instead of letting each tree vote and having the final probability of the ensemble equal P(y=1|x) = number of trees which predicted y=1 / N, they instead average the probabilistic predictions of all members, i.e. P(y=1|x) = Σ(for n = 1..N)[ Pn(y=1|x) ] / N. This also avoids the problem of individual tree tuning altogether.\n\nIf you’re curious, see this tech report by Leo Breiman. Using averaging gives smoother probabilities. Again, note that this doesn’t matter under the default assumption where we build trees all the way down.\n\nBut what happens if we do limit the depth of trees?\n\nThis is easily tested, e.g. by means of the following example churn data set:\n\n``````df = pd.read_csv(\"https://raw.githubusercontent.com/yhat/demo-churn-pred/master/model/churn.csv\")\ndf.drop(columns=['Phone', 'State'], inplace=True)\ndf['Int\\'l Plan'].replace({'no': 0, 'yes': 1}, inplace=True)\ndf['VMail Plan'].replace({'no': 0, 'yes': 1}, inplace=True)\ndf['Churn?'].replace({'False.': 0, 'True.': 1}, inplace=True)\n\nnp.unique(df['Churn?'], return_counts=True)\n# (array([0, 1], dtype=int64), array([2850, 483], dtype=int64))\n\nX, y = df.drop(columns=['Churn?']), df['Churn?']\nX_train, X_test, y_train, y_test = train_test_split(X, y, test_size=0.5)\n``````\n\nTraining a standard random forest with limited depth:\n\n``````rf = RandomForestClassifier(max_depth=2).fit(X_train, y_train)\nbase_score = roc_auc_score(\ny_test,\nrf.predict_proba(X_test)[:,1]\n)\n\nprint(\"RF AUC:\", base_score)\n# RF AUC: 0.8785843604842545\n``````\n\nWe can then implement our own predict function which accepts a threshold:\n\n``````def rf_predict_thresholded(model, X, average=True, tree_threshold=0.5):\n# tree_threshold is ignored if average=True\npreds = []\nfor estimator in rf.estimators_:\npreds.append(np.array(estimator.predict_proba(X)[:,1]))\nP = np.vstack(preds).T\nif average:\nV = np.mean(P, axis=1)\nelse:\nP[P >= tree_threshold] = 1; P[P < tree_threshold] = 0\nV = np.sum(P, axis=1) / len(rf.estimators_)\nreturn V\n``````\n\nAnd comparing it with the original score:\n\n``````auc_avg = roc_auc_score(y_test, rf_predict_thresholded(rf, X_test))\nauc_thr = roc_auc_score(y_test, rf_predict_thresholded(rf, X_test, average=False))\n\nprint(\"RF AUC (scikit-learn):\", base_score)\nprint(\"RF AUC (manual implementation):\", auc_avg)\nprint(\"RF AUC (0.5 threshold):\", auc_thr)\n\n# RF AUC (scikit-learn): 0.8785843604842545\n# RF AUC (manual implementation): 0.8785843604842545\n# RF AUC (0.5 threshold): 0.8740978140277726\n``````\n\nWe get the same result, and see that the majority voting approach even does slightly worse with a threshold of 0.5. We can in fact see that the average probabilities differ somewhat from the majority voted ones in this case:", null, "We can then tune the threshold (on the training set, to play it safe, but you’d normally cross-validate this):\n\n``````thresholds = np.linspace(0, 1, 30)\n\naucs = [roc_auc_score(\ny_train,\nrf_predict_thresholded(rf, X_train, average=False, tree_threshold=t)\n) for t in thresholds]\n\nbest_thres = thresholds[np.argmax(aucs)]\n\nprint(\"Best threshold:\", best_thres)\n# Best threshold: 0.10344827586206896\n\nplt.plot(thresholds, aucs)\n``````\n\nInterestingly enough, the best threshold appears to be around 0.10:", null, "With these final test set results:\n\n``````best_auc = roc_auc_score(\ny_test,\nrf_predict_thresholded(rf, X_test, average=False, tree_threshold=best_thres)\n)\n\nprint(\"RF AUC (scikit-learn):\", base_score)\nprint(\"RF AUC (manual implementation):\", auc_avg)\nprint(\"RF AUC (0.5 threshold):\", auc_thr)\nprint(f\"RF AUC (best threshold = {best_thres}):\", best_auc)\n\n# RF AUC (scikit-learn): 0.8951299611518283\n# RF AUC (manual implementation): 0.8951299611518283\n# RF AUC (0.5 threshold): 0.8782447377605374\n# RF AUC (best threshold = 0.10344827586206896): 0.8906157921536992\n``````\n\nAs can be seen, this best threshold comes close to our averaged value. When repeating the run with a different random seed, we can find cases where the best threshold does slightly better. So what to take from this?\n\n• Tuning the threshold of individual trees is most likely not worth it\n• Except when (for some reason) you’re using depth-limited trees and can not use an averaged ensemble prediction probability (but in which case it would be easier to implement that instead)\n• It might play a more important role when incorporating less trees in the ensemble\n• We’ve used the same threshold for every tree in the ensemble, but tuning this on a per-tree basis would lead even further down the rabbit hole (metalearning-like)\n\nSo in short: stick instead to the basics.\n\n1. Of course, it doesn’t matter that much when evaluating on e.g. AUROC, as this metric is threshold-independent (or rather, it incorporates all thresholds in a single metric)." ]
[ null, "https://blog.macuyiko.com/images/2021/trees1.png", null, "https://blog.macuyiko.com/images/2021/trees2.png", null ]
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https://customwritingreviews.com/math114n-week-7-discussion-solving-equations-using-square-roots-or-the-quadratic-formula/
[ "# Math114N Week 7 Discussion: Solving Equations using Square Roots or the Quadratic Formula\n\n## Math114N Week 7 Discussion: Solving Equations using Square Roots or the Quadratic Formula\n\nRequired Resources\n\nRead/review the following resources for this activity:\n\n• Lesson in Canvas\n• Assignments in Knewton\n• Solving Quadratic Equations Using the Square Root Property\n• Solving Quadratic Equations by Completing the Square\n• Solving Equations by using Quadratic Methods\n• Problem Solving with Quadratic Equations\n\nInitial Post Instructions\n\nFrom farmers to civil engineers, there are many jobs in which the quadratic equation could be utilized. To complete the Discussion activity, please do the following:\n\nWrite a paragraph (3-4 sentences) answering the following questions:\n\n1. What is one possible field or profession you may be considering?\n2. What are ways the quadratic equation could be used in this chosen profession?\n\nBe very specific and include a practical example.\n\nFollow-Up Post Instructions\n\nRespond to at least two peers in a substantive, content-specific way. Further the dialogue by providing more information and clarification.\n\nDo you need high quality Custom Essay Writing Services?" ]
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https://math.libretexts.org/Bookshelves/Combinatorics_and_Discrete_Mathematics/A_Spiral_Workbook_for_Discrete_Mathematics_(Kwong)/06%3A_Functions
[ "$$\\newcommand{\\id}{\\mathrm{id}}$$ $$\\newcommand{\\Span}{\\mathrm{span}}$$ $$\\newcommand{\\kernel}{\\mathrm{null}\\,}$$ $$\\newcommand{\\range}{\\mathrm{range}\\,}$$ $$\\newcommand{\\RealPart}{\\mathrm{Re}}$$ $$\\newcommand{\\ImaginaryPart}{\\mathrm{Im}}$$ $$\\newcommand{\\Argument}{\\mathrm{Arg}}$$ $$\\newcommand{\\norm}{\\| #1 \\|}$$ $$\\newcommand{\\inner}{\\langle #1, #2 \\rangle}$$ $$\\newcommand{\\Span}{\\mathrm{span}}$$\n\n# 6: Functions\n\n$$\\newcommand{\\vecs}{\\overset { \\rightharpoonup} {\\mathbf{#1}} }$$ $$\\newcommand{\\vecd}{\\overset{-\\!-\\!\\rightharpoonup}{\\vphantom{a}\\smash {#1}}}$$$$\\newcommand{\\id}{\\mathrm{id}}$$ $$\\newcommand{\\Span}{\\mathrm{span}}$$ $$\\newcommand{\\kernel}{\\mathrm{null}\\,}$$ $$\\newcommand{\\range}{\\mathrm{range}\\,}$$ $$\\newcommand{\\RealPart}{\\mathrm{Re}}$$ $$\\newcommand{\\ImaginaryPart}{\\mathrm{Im}}$$ $$\\newcommand{\\Argument}{\\mathrm{Arg}}$$ $$\\newcommand{\\norm}{\\| #1 \\|}$$ $$\\newcommand{\\inner}{\\langle #1, #2 \\rangle}$$ $$\\newcommand{\\Span}{\\mathrm{span}}$$ $$\\newcommand{\\id}{\\mathrm{id}}$$ $$\\newcommand{\\Span}{\\mathrm{span}}$$ $$\\newcommand{\\kernel}{\\mathrm{null}\\,}$$ $$\\newcommand{\\range}{\\mathrm{range}\\,}$$ $$\\newcommand{\\RealPart}{\\mathrm{Re}}$$ $$\\newcommand{\\ImaginaryPart}{\\mathrm{Im}}$$ $$\\newcommand{\\Argument}{\\mathrm{Arg}}$$ $$\\newcommand{\\norm}{\\| #1 \\|}$$ $$\\newcommand{\\inner}{\\langle #1, #2 \\rangle}$$ $$\\newcommand{\\Span}{\\mathrm{span}}$$\n\n• 6.1: An Introduction to Functions\nThe functions we studied in calculus are real functions, which are defined over a set of real numbers, and the results they produce are also real. In this chapter, we shall study their generalization over other sets. The definition could be difficult to grasp at the beginning, so we would start with a brief introduction.\n• 6.2: Definition of Functions\nA function from A to B is a rule that assigns to every element of A a unique element in B .\n• 6.3: One-to-One Functions\nWe distinguish two special families of functions: the one-to-one functions and the onto functions. We shall discuss one-to-one functions in this section.\n• 6.4: Onto Functions\nOne-to-one functions focus on the elements in the domain. We do not want any two of them sharing a common image. Onto functions focus on the codomain. We want to know if it contains elements not associated with any element in the domain.\n• 6.5: Properties of Functions\nIn this section, we will study some properties of functions.\n• 6.6: Inverse Functions\n• 6.7: Composite Functions" ]
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https://quartzcomponents.com/collections/resistors?page=2
[ "#### 33 ohm, 1/4 Watt Resistor with 5% tolerance (Pack of 10)\n\nRs. 5.00 (Exc. GST)\nQC0917\nThis is a set of 10, 33 ohm carbon film resistors with 1/4 Watt and 5% tolerance. Each resistor has strong leads and easy-to-read color coding for breadboarding....\n\n#### 82K ohm, 1/4 Watt Resistor with 5% tolerance (Pack of 10)\n\nRs. 5.00 (Exc. GST)\nQC0941\nThis is a set of 10, 82K ohm carbon film resistors with 1/4 Watt and 5% tolerance. Each resistor has strong leads and easy-to-read color coding for breadboarding....\n\n#### 39 ohm, 1/4 Watt Resistor with 5% tolerance (Pack of 10)\n\nRs. 5.00 (Exc. GST)\nQC0918\nThis is a set of 10, 39 ohm carbon film resistors with 1/4 Watt and 5% tolerance. Each resistor has strong leads and easy-to-read color coding for breadboarding....\n\n#### 82 ohm, 1/4 Watt Resistor with 5% tolerance (Pack of 10)\n\nRs. 5.00 (Exc. GST)\nQC0921\nThis is a set of 10, 82 ohm carbon film resistors with 1/4 Watt and 5% tolerance. Each resistor has strong leads and easy-to-read color coding for breadboarding....\n\n#### 240 ohm, 1/4 Watt Resistor with 5% tolerance (Pack of 10)\n\nRs. 5.00 (Exc. GST)\nQC0924\nThis is a set of 10, 240 ohm carbon film resistors with 1/4 Watt and 5% tolerance. Each resistor has strong leads and easy-to-read color coding for breadboarding....\n\n#### 1 Ohm, 2 Watt Resistor (Pack of 4)\n\nRs. 9.00 (Exc. GST)\nQC0203\nThis is a packet of four Carbon Film Resistors (CFR). The resistance of each is 1 Ohm and the rated power is 2W. The...\n\n#### 10 Ohm 2 Watt Resistor (Pack of 4)\n\nRs. 9.00 (Exc. GST)\nQC0204\nThis is a packet of four Carbon Film Resistors (CFR). The resistance of each is 10 Ohm and the rated power is 2W. The main function...\n\n#### 100 Ohm 2 Watt Resistor (Pack of 4)\n\nRs. 16.00 Rs. 10.00 (Exc. GST)\nQC0205\nThis is a packet of four Carbon Film Resistors (CFR). The resistance of each is 100 Ohm and the rated power is 2W. The main function...\n\n#### 1k ohm 2 Watt Resistor (Pack of 4)\n\nRs. 16.00 (Exc. GST)\nQC0206\nThis is a packet of four Carbon Film Resistors (CFR). The resistance of each is 1K Ohm and the rated power is 2W. The main function...\n\n#### 2.2k ohm 2 Watt Resistor (Pack of 4)\n\nRs. 9.00 (Exc. GST)\nQC0207\nThis is a packet of four Carbon Film Resistors (CFR). The resistance of each is 2.2K Ohm and the rated power is 2W. The main function...\n\n#### 4.7K ohm 2 Watt Resistor (Pack of 4)\n\nRs. 8.00 (Exc. GST)\nQC0208" ]
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https://gateoverflow.in/336697/nielit-2016-mar-scientist-b-section-c-44
[ "635 views\n\nFor a database relation $R(a,b,c,d)$ where the domains of $a,b,c,d$ include only atomic values, only the following functional dependencies and those that can be inferred from them hold:\n\n$a\\to c\\\\b\\to d$\n\nthe relation is in\n\n1. first normal form but not in second normal form.\n2. second normal form but not in third normal form.\n3. third normal form.\n4. none of these.\n\n### 1 comment\n\nOriginal Source of this question: GATE 1997\n\nThe candidate key for the relation is:  $ab$ ,  because  $ab^{+}=abcd$\n\nSince,  $a \\rightarrow c$  and  $b \\rightarrow d$ are partial dependencies which are not allowed in $2$NF, the relation is hence in $1$NF.\n\nOption A is correct.\nby\nA) first normal form but not in second normal form,\n\n( ab)+=abcd..so , ab is a candidate key, so, a→c and b→d both are partial dependencies...and in 2NF it is not Allowed...and in the question it is given that  domains of a,b,c,d include only atomic values...So it is in 1NF..\nANS: A\n\nCANDIATE KEY OF THIS RELATION IS AB\n\na→c\n\nb→d\n\nBOTH CONTAIN PARTIAL INDEPENDENCIES , AND IN 2ND NORMAL FORM PARTIAL INDEPENDENCIES IS NOT ALLOWED.\n\nSO GIVEN RELATION IS ONLY IN 1ST NORMAL FORM.\nby\n\n1\n601 views" ]
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