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Field-Programmable Gate Array Computer in Structural Analysis: An Initial Exploration PDF

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Paper Number: AIAA-2002-1761 FIELD-PROGRAMMABLE GATE ARRAY COMPUTER IN STRUCTURAL ANALYSIS: AN INITIAL EXPLORATION Robert C. Singleterry Jr., NASA Langley Research Center, Hampton, Virginia 1 Jaroslaw Sobieszczanski-Sobieski, AIAA F, NASA Langley Research Center, Hampton, Virginia Samuel Brown, Star Bridge Systems Inc., Midvale Utah Abstract 1. Introduction This paper reports on an initial assessment of using As in other areas of applied mechanics, structural aField-Programmable Gate Array (FPGA) analysis poses apersistent demand for faster computational device asanew tool for solving computing. This is particularly true in applications structural mechanics problems. A FPGA is an involving nonlinear behavior and in design optimization assemblage of binary gates arranged in logical blocks because of the repetitive analysis. Until recently, the that are interconnected via software in amanner computer hardware technology has responded to this dependent on the algorithm being implemented and can demand via a two-prong development of faster be reprogrammed thousands of times per second. In processors and concurrent processing with an effect, this creates acomputer specialized for the increasing number of processors packaged either in a problem that automatically exploits all the potential for single machine or distributed in a network. parallel computing intrinsic in an algorithm. This The Field Programmable Gate Array (FPGA) is a inherent parallelism is the most important feature of the relatively new addition to the above technology of FPGA computational environment. It is therefore Massively Concurrent and Distributed Processing. important that if aproblem offers achoice of different Relatively few engineers and scientists have had an solution algorithms, an algorithm of ahigher degree of opportunity to explore the FPGA computers. This inherent parallelism should be selected. paper reports on an initial assessment of the utility of It is found that in structural analysis, an "analog the FPGA machine and its graphic programming computer" style of programming, which solves language illustrated by a few simple examples in problems by direct simulation of the terms in the structures and dynamics. A variety of commercially governing differential equations, yields a more available FPGA systems now exist. They are supplied favorable solution algorithm than current solution either as separate boards or as complete, turnkey methods. This style of programming is facilitated by a systems. The information reported herein was obtained "drag-and-drop" graphic programming language that is at the NASA Langley Research Center by using one supplied with the particular type of FPGA computer such turnkey system containing 20 FPGA's called reported in this paper. Simple examples in structural HAL-30 Hypercomputer TM (Reference [3]), dynamics and statics illustrate the solution approach programmed with a graphic language VIVA ® used. The FPGA system also allows linear scalability (Reference [2]), both from Star Bridge Systems ®. The in computing capability. As the problem grows, the assessment includes a simplified description of the number of FPGA chips can be increased with no loss of salient features that distinguish the FPGA computer computing efficiency due to data flow or algorithmic from single or multiple processor computers. The latency that occurs when a single problem is distributed current merits and demerits of the FPGA computer and among many conventional processors that operate in its future potential are discussed. parallel. This initial assessment finds the FPGA hardware 2. Conventional CPU vs FPGA and software to be in their infancy in regard to the user conveniences; however, they have enormous potential The kernel of most current computer architectures for shrinking the elapsed time of structural analysis is the general purpose Central Processing Unit (CPU), solutions if programmed with algorithms that exhibit programmed individually or in networked groups. The inherent parallelism and linear scalability. This CPU itself consists of a large number of gates that work potential warrants further development of FPGA- as on-off switches and are permanently wired in a tailored algorithms for structural analysis. variety of fixed circuits that implement, in a binary- logic framework, the whole gamut of functions needed 1Corresponding author: Robert C. Singleterry, Jr.; NASA Langley Research Center, MS 188B, Hampton VA 23681; 757-864-1437; r.c.singleterry @larc.nasa.gov This paper is declared a work of the U.S. Government and is not subject to copyright protection in the United States 1 American Institute of Aeronautics and Astronautics for its operation. At any particular time, only a small equals the number of gates supplied in the array. This fraction of the total number of gates may be gainfully "inherently parallel" attribute allows all M operations to employed, while the idle gates consume power and be executed at the same time, so that the maximum M is generate heat. For engineers, the ability to generate only a function of the size and number of FPGAs floating-point results is essential; therefore, some CPUs available. have multiple floating-point units. In a massively parallel environment that employs many CPUs, the 3. Graphic Programming of FPGA number of floating-point results that can be generated simultaneously is limited by the number of the CPUs, To make the multitude of gates available to the user without performing machine-language level the communication speed, and the memory capability, all combined with the solution algorithm programming for each application, high-level languages characteristics. exist, such as, HANDEL-C TM (Reference [1]), and VIVA ®(Reference [2]), the latter having been used as a In an FPGA, a command to execute a particular basis for this report. function is interpreted by the resident operating system The authors' experiences to date indicate that the to interconnect "by software" as many gates as FPGA-based computers can benefit engineers in at least necessary to perform that particular function and only that function. The particular interconnection scheme two ways: exists only as long as the job executes and can be 1. They exploit inherent parallelism in the algorithm reconfigured to execute other functions many times per being executed, hence they have apotential to second. In effect, a "specialized CPU" is created for radically reduce the computation elapsed time. the job at hand. It isreminiscent of using an UV light 2. They may be programmed in an analog computer source to burn-in the inter-gate conduits to implement a style that bypasses the need to develop solution particular logic circuit, an operation known as algorithms to the equations that govern the programming by "firmware". However, the result of problem. this firmware programming is irreversible, while the These two points are illustrated by an introduction to FPGA program can be changed by the user in the field - the VIVA language using simple examples. -hence "Field" in FPGA. The VIVA language hides the tailoring of a If the algorithm being implemented offers an specialized CPU from the amorphous supply of gates opportunity to do M number of operations specifically for the job at hand under a veneer of a simultaneously, then M specialized CPUs are being graphic language that enables coding by drawing what created in the FPGA computer. In the extreme, the looks like a wiring diagram. In this regard, VIVA specialized CPUs might all be different in terms of the extends to the FPGA machines the same approach that number of gates and their interconnection logic if the languages such as MATLAB Simulink (Reference [4]) functions to be executed are different. Some of these implemented on a conventional, single or multiple specialized CPUs could operate simultaneously and processor computers. some could operate sequentially as required by the logic The essence of the VIVA graphic program is of the algorithm being executed. Thus, the set of gates illustrated in Figure 1by the simple example of computing a2for a given value of a. available in an FPGA computer is viewed as aresource for creating a computer tailored to the job at hand. In VIVA has a library of processing tools available in principle, if the job is not large enough to use all the adisplay on right the margin of the screen. The tools gates available, another unrelated job might be executed needed to execute the example problem are simultaneously. Also, the hardware executes the entire 1. Input a from the user, illustrated by a horn on the left algorithm at once unless a sequencing step is part of the algorithm, e.g., when the algorithm involves iterations. 2. Multiply (a *a), illustrated by the box with × To illustrate the computational parallelism afforded 3. Output a2to the user, illustrated by the horn on the right by a FPGA, consider the example of computing These objects are dragged and dropped onto the main a = b. c+ d. A conventional CPU needs two steps for screen area and the inputs and outputs are connected to this operation: first to calculate the product b. c and the multiply object. The resulting diagram is then to perform the sum because the steps are logically "compilea_' into an executable code that can accept any sequential. The FPGA potentially can complete both value of a as input. The entire diagram may be named, operations in one step provided the gates are properly saved, turned into another icon in the library of tools, configured. Furthermore, if the example is extended to and displayed. In this manner, one can develop a a = e. f + b. c + d, a FPGA still needs only one step complex code by building blocks forming many because it can engages more gates. This example can hierarchically related levels. These building blocks be extended in this manner while holding the execution to a single step until the number of gates employed 2 American Institute of Aeronautics and Astronautics workbesitfthealgorithmcanbemaderecursivine velocity, and translation as functions of time computed nature. by VIVA for an impulse force excitation are presented in Figure 6for a subcritical value of the damping 3.1 Equation Solution constant. Should the damping be set to a negative Now consider two algebraic equations with two value, a divergent behavior reminiscent of wing flutter unknowns y and z and six constants a, b, d, e, P, and M results. 3.3 Inclusion of non-linearitv adyy ++ebzz ==MP (1) A primary benefit of the analog computer programming style is that the handling of non-linearity One may program a VIVA solution using Cramer's becomes almost trivial. For example, should the right rule: hand side of the first equation in Eq. (1) depend Pe-Mb nonlinearly on the solution for y, Eq. (1) becomes y= ae-db (2) Ma- Pd ay +bz = P- ky2 (4) Z-" dy + ez = M ae -db and the diagram in Figure 2 changes by the simple and as in the previous example execute it in one step. addition of the "Two DOF NL term" object shown in However, expansion of the system of simultaneous Figure 7. The numerical solution is obtained by equations to larger number of variables causes recording the output values ofy and z as the system nonlinear explosion in the number of terms and converges to a steady state. In effect the usual operations that would quickly exhaust the FPGA approach of devising a solution to the equations and capacity and make the VIVA program exceedingly then programming the solution is replaced by complex. Therefore, a better method in VIVA is a programming an iterative solution by directly fixed-point iteration solution, as in Figure 2, simulating the terms of the governing equations and corresponding to their connectivity. Table 1shows the results of the above iterations along with results from a double Yi = P- bzi-1 precision FORTRAN program, which agrees to six a (3) significant figures. zi = M-dyi-1 e 3.4 Concurrent computing To see the concurrent computing capability in the Upon initialization, the system represented by the above application, consider alinear equation with only diagram in Figure 2 converges to the fixed-point one unknown whose iterative solution may be written as (y=,Zoo) solution as the iterations are stepped through. The need to iterate (with arate of convergence that (Xi_l)2-1 depends on the properties of the matrix of coefficients) Xi "- (5) 3 is the penalty for the solution simplicity. The flow of execution within one cycle is: all the "divide" operators and the corresponding VIVA diagram in Figure 8. The first, all the "multiply" operators next, followed by all reduced diagram amounts to one half of the diagram for the "subtraction" operators. the system of two equations as in Eq. (1) shown in Figure 2 (top left inset) and, yet, the execution time per 3.2 Analog programmin_ style iteration for the full system would be the same as for The diagram in Figure 2is strikingly similar to a the reduced system because of the concurrent processing. wiring diagram one would have developed for this problem when using an analog computer. The similarity is more than superficial. It implies a style of 4. Initial Assessment of Experience with Statics and programming based entirely on the now nearly Dynamics forgotten analog computer methods. In fact, for a case The next step is the application of alarger number of a spring-mass vibrating system with damping shown of degrees of freedom. Figure 9depicts asystem of in Figure 3, one may revert to an analog computer two vibrating masses with three springs, three dampers, diagram from a more than 30-year-old reference [5, and two governing, coupled differential equations. The Figure 2-9] rendered in Figure 4 and derive from it the corresponding analog computer wiring diagram is VIVA diagram shown in Figure 5. The acceleration, illustrated in Figure 10. A VIVA program based on 3 American Institute of Aeronautics and Astronautics that diagram is shown in Figure 11with the program's labor and the amount of memory required to hold the output shown in Figure 12. Again, if there were anon- intermediate results. This complexity stems from the linearity in the system, for example, the k2 spring phenomenon of the sparse matrix filling-in with stiffness were proportional to the spring elongation x2- nonzero terms in the direct solution process. The xl, a simple modification shown by the inset in Figure number of the new, fill-in entries created in the process 10 would implement that non-linearity. of a sparse [K] matrix solution is, typically, of the A cantilever beam in Figure 13provides an order of 10 to 20 times the original number of nonzero example of a static analysis case with multiple degrees entries. of freedom. This simple case suggests a conclusion of In general, the filling-in pattern cannot be precisely general significance. The conclusion is that to use predicted but reordering the degrees of freedom and the FPGA's efficiently, one needs to select among the associated reshuffling of the rows and columns in the solution algorithms available, one that affords the matrix can mitigate its detrimental effect on both the largest degree of inherent parallelism. For the case at amount of numerical labor and memory utilization. hand, three possible algorithms to choose from are: The graphic programming in VIVA does not lend itself 1. Forming the Load-Deflection equations easily to the large, sparse matrix reordering. Even if it [K]{u} = {P} and solving them by one of the did, that approach would still be unattractive because direct solution methods, e.g., the Cholesky the experience shows that when the algorithms based on decomposition algorithm. that approach are implemented on a multiprocessor 2. Solving the Load-Deflection equations by an computer, the interprocessor communication time iterative method as in Figure 2. grows relative to the computing time. The resulting 3. Treating the beam as a quasi-dynamic system that loss of scalability brings in the law of diminishing asymptotically tends to a solution corresponding to returns that limits the number of processors that may be the static state. used efficiently to well below 100 (Reference [7]). For The above alternative algorithms have the following these reasons, Alternative 1does not appear to be the merits and demerits. best choice for an FPGA programmed by a pictorial 4.1 Direct solution methods language considering the currently available information. The direct solution approach is the least advantageous in FPGA programming because it is a 4.2 Iterative solution methods procedure, which consists mostly of the array An iterative scheme has an obvious advantage of bookkeeping that exploits the [K] matrix sparseness. avoiding the filling-in phenomenon completely. In Considering that in a large problem, only a few percent principle, one could assign a separate processor to each of the [K] matrix entries may be nonzero, the equation, or even to each... + a_i*u i ... term in the exploitation of sparseness is a necessity in problems of equations so that they all would be evaluated any significance because processing of all the elements concurrently. That leaves the sparsity intact but does including the null ones requires the number of generate data transfers that consume significant time. arithmetical operations that is of order N3. On the other Furthermore, a separate and complete fixed-point hand, that number reduces radically to order Nb2if one iterative process needs to be converged for each loading exploits a banded structure of the matrix with the case whose number in practical applications may be in bandwidth b. Exploitation of an irregular sparsity, thousands. Focusing on the positive, one iteration of a measured by S equal to the ratio of the number of the [K] matrix, NxN, with sparseness S requires that the nonzero elements in the matrix to N2,generates number of floating point multiplications be proportional comparable or greater reduction. For example, for an to SN 2and all of them could be performed in the time acoustic analysis reported in Reference [8] involving required by a single multiplication if a sufficient millions of equations, it was observed that the growth in number of processors is available. the number of arithmetical operations was reduced to On the other hand, if the number of iterations to N4/3owing to the sparsity of the equation system. convergence is M and the number of loading cases isL, However, that reduction is too problem dependent to be the total number of multiplications grows to SN2ML expressed by a simple formula in terms of N and S. and the total elapsed time to execute them in an ideally Elaborate schemes have been created to exploit concurrent processing grows in proportion to ML. It efficiently the bandedness or irregular sparsity on single follows that the advantage of the iterative solution in and multiprocessor computers (Reference [6]). These terms of the elapsed time decreases with the increase of schemes although efficient and effective on today's the product ML and may vanish beyond a certain computers are also complex as they employ critical threshold of that product. The value of M is sophisticated bookkeeping and elaborate if-trees to find problem-dependent but should be expected to be large a compromise between the minimum of the numerical because the [K] matrix conditioning that governs M is 4 American Institute of Aeronautics and Astronautics knowntobepoor.ForexampleR,eferenc[6e]citesa that the FPGA hardware capacity develops to that level, casewith N = 16000 that required M = 50000 for L =1. programming the FPGA using Alternative 3has a It appears that implementation of an iterative potential for near perfect linear scalability of the solution a large system of equations with exploitation of equation solution stage in static and dynamic structural irregular sparsity is possible on a FPGA using VIVA. analysis. As abonus, this alternative is amenable to the The language supports matrix operations by treating a simple implementation of a non-linearity as illustrated matrix as one long vector and keeping track of the by inset in Figure 14. element location indices. Therefore, the foregoing assessment of the iterative solution, Alternative 2, 4.4 Computing time for operations other than implemented on a multiprocessor computer applies to solving the load-deflection equations FPGA as well. Therefore, one should consider Regardless of the load-deflection equation solution Alternative 2, an iterative solution, as a viable one for method, the total elapsed time of astructural analysis in FPGA up to a limit imposed by the product ML. any particular case is asum of the equation solution time discussed above and the times consumed by the 4.30uasi-dynamic, step-by-step solution method other stages in the total analysis process: In Alternative 3, a structure such as the example of 1. development of afinite element model, a cantilever beam represented by two finite element 2. assembly of the [K] matrix, and portrayed in Figure 13 is treated as a dynamic system 3. interpretation of results. solved by a step-by-step algorithm in time domain the The time of stage 1is primarily the human labor. To same as the one used for the dynamic cases depicted in make aradical reduction using an FPGA based system, Figures 3 and 9. To use that approach, one converts the the conventional finite element analysis would have to structure to a dynamic system by adding inertia and be rewritten, starting from the very fundamentals and damping. In case of the beam in Figure 13, that is tailoring the solution to the FPGA architecture. accomplished by assuming fictitious mass and moment Regarding stage 3,the FPGA is being used for of inertia associated with each of the unsupported visualization of voluminous data in non-engineering degrees of freedom. Similarly, fictitious translational applications, so it is conceivable that it may assist at and rotational dampers are attached to these degrees of that stage. For stage 2, the now-routine technique of freedom. The magnitudes of the fictitious quantities are assembling the [K] matrix consists of selective not important, except that for asymptotic convergence summing and placing the entries of the elemental the damping coefficient values should be close to the stiffness matrices in the framework of [K]. That critical ones. technique does not lend itself to efficient The dynamic equation for the system so modified implementation in VIVA for the same reasons that were reads previously discussed in conjunction with Alternative 1. That leaves an option of assembling [K] by the [M]{ii} +[D]{u} + [K]{u} ={P(t)} (6) textbook operation. where matrices [M], [D], and [K] represent inertia, [K] = [A]T[kdiag ] [A] (7) damping, and stiffness. Using amatrix-vector capability in VIVA the where [A] stands for the 0-1 connectivity matrix and solution diagram for Eq. (6) shown in Figure 14 looks [k_ag] is the block-diagonal matrix of the unassembled the same as one for asingle degree of freedom system structure. VIVA supports matrix operations so it could except that the matrix operations replace the scalar execute Eq. (7); however, because the matrices ones. When the loading {P(t)} advances in small involved aremostly zeros, it would be mandatory to implement azero-bypass capability in the VIVA increments from zero to {P(t)} in fictitious time the language. system converges to the static state of the displacement Eventually, the FPGA capability may prove to be a and stress under {P(t)}. strong enough motivator for development of non- Further experimentation is needed to determine conventional solution methods. One example of such whether the number of increments for {P(t)} does not emerging methods whose intrinsic parallelism makes them anatural match for FPGA is the cellular automata have to grow with N for good convergence. If it does method that has been demonstrated effective in not, then the solution elapsed time would grow only with the number of loading cases L and Alternative 3 structural analysis (Reference [9]) and in both analysis would become better than Alternative 2 up to alimit and optimization in Reference [10]. governed by L and by the size of the FPGA. The pictorial programming in VIVA has the Furthermore, the L limit can also be overcome if obvious advantage of being very intuitive. In computer science community, there is no consensus whether that the FPGA is large enough to carry the solution of Eq. advantage can be sustained when the volume of detail (6) for many loading cases simultaneously. Assuming 5 American Institute of Aeronautics and Astronautics tobeseenbegintsoexceeodfwhaat singlescreemnay developed in the past for the single processor, displayT. heauthoresxperientcoedatereinforcewdith sequential computing. The FPGA-based system is one thegrowinguseofgraphicasyl stemssuchasReference type of a computer on that path, and the methods [4],indicatethsattheabilitytocollapsaesinglescreen tailored to its architecture now will grow in their diagramintoasingleicontobeusedasabuilding effectiveness as the FPGA technology develops. The blockinanothesrcreeinseffectivienkeepintghe first exploratory step reported herein has but scratched visuaclodecomplexituyndecrontrolI.tisroughly the surface of the potential for this class of computers equivalentotthegeneralalycceptegdoodpractice and solution methods. principleofstructurepdrogrammitnogkeepa subroutinleengthtoonepage. 6. References 1. HANDEL-C at www.celoxica.com 5. Concluding Remarks 2. VIVA at www.starbridgesystems.com and are Initial exploratory experience to date with a marks of Star Bridge Systems, Copyright 1998- particular FPGA system, the VIVA/HAL-30 2001 by Star Bridge Systems, Inc. software/hardware combination, has been reported and 3. HAL-15 at www.starbridgesystems.com and are its merits and demerits assessed. Tentatively, on the marks of Star Bridge Systems, Copyright 1998- negative side one should point to the lack of 2001 by Star Bridge Systems, Inc. informative error messages, an effective debugger, and 4. SIMULINK at www.mathworks.com absence of textual or graphic output rendering to a disk. 5. Michael G. Rekoff, Jr., Analog Computer Considering that this FPGA technology is now in its Programming, Charles E. Merrill Books, Inc, infancy, one may expect that these shortcomings will be Columbus, Ohio, 1967. addressed as the VIVA product matures. On the 6. Nguyen, D. T.: Parallel-vector Equation Solvers for positive side, the FPGA hardware/software system fully Finite Element Engineering Applications; Kluwer exploits the solution algorithm's inherent parallelism, Academic Publ., 2002. and no engineering time needs to be spent on devising 7. Storaasli, O.O.; Nguyen, D.T.; Baddourah, M.A.; solutions to the governing equations. The problems of and Qin, J.: Computational Mechanics Analysis scaling, precision, and stability faced by the analog Tools for Parallel Vector Supercomputers; computer user in the past are absent owing to the digital Computing Systems in Engineering, Vol.4, N0:4-6, accuracy and repeatability. However, the careful pp.349-354, Elsevier Publ. 1993. choice of the time step in dynamic applications to stay 8. Watson, W.R.; and Storaasli, O.O.: Application of within the problem's time scale is still required. NASA general purpose solver to large-scale The analog programming style realizes best the computations in aeroacoustics; Advances in FPGA potential in structural analysis. It offers a Engineering Software, No.31, pp.555-561. potential to reduce the equation solving elapsed time, , Kim, P.; and Hajela, P.: Elastic Element Based and an easy way to implement non-linearities. Cellular Automata Models in Structural Design; 4th Extension of the FPGA utility to all the phases of a World Congress on Structural and complete structural analysis process, will require Multidisciplinary Optimization, Dalian, China, redevelopment from the ground up tailored to the June 2001. FPGA architecture. 10. Abdalla, M.; and Gurdal, Z.: Structural Design There is no doubt that computing technology has Using Optimality Based Cellular Automata; Paper embarked on a path of inherent parallelism in AIAA-2002-1676; 43rdAIAA Structures, processing that in due course will likely supplant many Dynamics, and Materials Conference; Denver, CO, of the engineering physics solutions that were April 2002. Table 1: Results of Fixed Point Iterations with Zo=3, Yo=2, a=P=l, b=d=0.5, M=0.0001 FORTRAN VIVA K (double " " - 10-13) (non-lineari: Y= Z= Iterations y= Z= 1.3332667 -0.66653333 47 1.333267 -0.6665334 1.1553033 -0.57755163 69 1.155303 -0.5775517 6 American Institute of Aeronautics and Astronautics asau,ared !i!_iii!Z:ii!!::ii_i!iii:!!iii:i!iiiiii!: Figure 1: Viva Algorithm to Calculate f(a) = a2 (Features left not explained are internal VIVA C housekeeping details beyond the scope of this report) k 1 [cY_+ kx + f(t)] m Figure 3: Frictionless Mass and Spring with Damper 7 American Institute of Aeronautics and Astronautics d2 dt2 X f(t) multiplier (amplifier) integrator adder -critical damping coefficient; natural vibration circular (,On - frequency; Figure 4: Analog Computer Diagram corresponding to the System in Figure 3; It is Directly Translatable into the Viva Algorithm in Figure 5 :_i_-_;&,; ----:_i-.......= _"-_:i::E__i::::.__i •:..::.:::..::::._._................... 15 Xo = Vo= to= 0 dt = 0.125 -- Position II Step infirst dt -- Velocity Impluse =125.0 iiil ;i'::i:!!:i!"'.::i 10 _k-......Damplng=O.5 ....................................... -- A_cceleration ...... = . Arbitrary 0 -lO :i:/iii:i/:i:i!. 0 2 4 Time 6 8 10 Figure 5: Viva Algorithm to Solve the Mass and Spring with Dampers from Figure 3 Figure 6: Plotted Output from the Viva Algorithm in Figure 5 8 American Institute of Aeronautics and Astronautics !i:!ii%iiii!ii i!iii!:i!!!ii!:_i Figure 8: Viva Algorithm to Solve Equation (5) Via the Fixed Point Algorithm for One Degree of Freedom Figure 7: Viva Algorithm to Solve Equation (4) Via the Fixed Point Algorithm with a Non-linearity X C1 C2 C3 k k2 k3 1 [C2X 2 -_- k2x 2 -- (C1 -_- C2)X 1 -(k 1 + k2)Xl] m 1 1 [C2X 1 "_"k2x 1 -- (C2 -[- C3)'X 2 -- (k2 + k3)x2] m 2 Figure 9: Two Masses Connected by Three Springs with Three Dampers on a Frictionless Surface 9 American Institute of Aeronautics and Astronautics 1/(ml) .f(t) w'! > J c2 1/(m2) Figure 10: Analog Equivalent Wiring Diagram to Solve System in Figure 9 =_ __',H _o4 / _w _ I__: Figure 11: Viva Algorithm to Implement Figure 10 10 American Institute of Aeronautics and Astronautics

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