forked from gilbertgede/idetc-2013-paper
-
Notifications
You must be signed in to change notification settings - Fork 3
/
asme2e.tex
944 lines (869 loc) · 50.5 KB
/
asme2e.tex
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
96
97
98
99
100
101
102
103
104
105
106
107
108
109
110
111
112
113
114
115
116
117
118
119
120
121
122
123
124
125
126
127
128
129
130
131
132
133
134
135
136
137
138
139
140
141
142
143
144
145
146
147
148
149
150
151
152
153
154
155
156
157
158
159
160
161
162
163
164
165
166
167
168
169
170
171
172
173
174
175
176
177
178
179
180
181
182
183
184
185
186
187
188
189
190
191
192
193
194
195
196
197
198
199
200
201
202
203
204
205
206
207
208
209
210
211
212
213
214
215
216
217
218
219
220
221
222
223
224
225
226
227
228
229
230
231
232
233
234
235
236
237
238
239
240
241
242
243
244
245
246
247
248
249
250
251
252
253
254
255
256
257
258
259
260
261
262
263
264
265
266
267
268
269
270
271
272
273
274
275
276
277
278
279
280
281
282
283
284
285
286
287
288
289
290
291
292
293
294
295
296
297
298
299
300
301
302
303
304
305
306
307
308
309
310
311
312
313
314
315
316
317
318
319
320
321
322
323
324
325
326
327
328
329
330
331
332
333
334
335
336
337
338
339
340
341
342
343
344
345
346
347
348
349
350
351
352
353
354
355
356
357
358
359
360
361
362
363
364
365
366
367
368
369
370
371
372
373
374
375
376
377
378
379
380
381
382
383
384
385
386
387
388
389
390
391
392
393
394
395
396
397
398
399
400
401
402
403
404
405
406
407
408
409
410
411
412
413
414
415
416
417
418
419
420
421
422
423
424
425
426
427
428
429
430
431
432
433
434
435
436
437
438
439
440
441
442
443
444
445
446
447
448
449
450
451
452
453
454
455
456
457
458
459
460
461
462
463
464
465
466
467
468
469
470
471
472
473
474
475
476
477
478
479
480
481
482
483
484
485
486
487
488
489
490
491
492
493
494
495
496
497
498
499
500
501
502
503
504
505
506
507
508
509
510
511
512
513
514
515
516
517
518
519
520
521
522
523
524
525
526
527
528
529
530
531
532
533
534
535
536
537
538
539
540
541
542
543
544
545
546
547
548
549
550
551
552
553
554
555
556
557
558
559
560
561
562
563
564
565
566
567
568
569
570
571
572
573
574
575
576
577
578
579
580
581
582
583
584
585
586
587
588
589
590
591
592
593
594
595
596
597
598
599
600
601
602
603
604
605
606
607
608
609
610
611
612
613
614
615
616
617
618
619
620
621
622
623
624
625
626
627
628
629
630
631
632
633
634
635
636
637
638
639
640
641
642
643
644
645
646
647
648
649
650
651
652
653
654
655
656
657
658
659
660
661
662
663
664
665
666
667
668
669
670
671
672
673
674
675
676
677
678
679
680
681
682
683
684
685
686
687
688
689
690
691
692
693
694
695
696
697
698
699
700
701
702
703
704
705
706
707
708
709
710
711
712
713
714
715
716
717
718
719
720
721
722
723
724
725
726
727
728
729
730
731
732
733
734
735
736
737
738
739
740
741
742
743
744
745
746
747
748
749
750
751
752
753
754
755
756
757
758
759
760
761
762
763
764
765
766
767
768
769
770
771
772
773
774
775
776
777
778
779
780
781
782
783
784
785
786
787
788
789
790
791
792
793
794
795
796
797
798
799
800
801
802
803
804
805
806
807
808
809
810
811
812
813
814
815
816
817
818
819
820
821
822
823
824
825
826
827
828
829
830
831
832
833
834
835
836
837
838
839
840
841
842
843
844
845
846
847
848
849
850
851
852
853
854
855
856
857
858
859
860
861
862
863
864
865
866
867
868
869
870
871
872
873
874
875
876
877
878
879
880
881
882
883
884
885
886
887
888
889
890
891
892
893
894
895
896
897
898
899
900
901
902
903
904
905
906
907
908
909
910
911
912
913
914
915
916
917
918
919
920
921
922
923
924
925
926
927
928
929
930
931
932
933
934
935
936
937
938
939
940
941
942
943
944
%%%%%%%%%%%%%%%%%%%%%%%%%%% asme2e.tex %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
% Template for producing ASME-format articles using LaTeX %
% Written by Harry H. Cheng %
% Integration Engineering Laboratory %
% Department of Mechanical and Aeronautical Engineering %
% University of California %
% Davis, CA 95616 %
% Tel: (530) 752-5020 (office) %
% (530) 752-1028 (lab) %
% Fax: (530) 752-4158 %
% Email: [email protected] %
% WWW: http://iel.ucdavis.edu/people/cheng.html %
% May 7, 1994 %
% Modified: February 16, 2001 by Harry H. Cheng %
% Modified: January 01, 2003 by Geoffrey R. Shiflett %
% Use at your own risk, send complaints to /dev/null %
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
%%% use twocolumn and 10pt options with the asme2e format
\documentclass[twocolumn,10pt,final]{asme2e}
\special{papersize=8.5in,11in}
\usepackage{fancyvrb}
\usepackage{graphicx}
\usepackage{amsmath}
\usepackage{tikz}
\usepackage{pgf}
\usepackage{cite}
\usetikzlibrary{arrows}
\usetikzlibrary{snakes}
\renewcommand{\b}[1]{\mathbf{#1}}
\newcommand{\bs}[1]{\boldsymbol{#1} }
\newcommand{\uv}[1]{\hat{\mathbf{#1}}}
\newcommand{\drawpendulum}[6]{
\def \x {#1}
\def \y {#2}
\def \theta {#3}
\def \length {#4}
\def \m {#5}
\def \index {#6}
% Shift the origin to x, y
\pgftransformshift{\pgfpoint{\x}{\y}}
% Draw a dashed line from origin to -l
\draw[dashed] (0,0)--(0,-\length);
% Draw an arc from (0,-.75*l) that is theta degrees clockwise
\draw[->] (0,-0.75*\length) arc (-90:\theta-90:0.75*\length);
% Rotate to middle of arc and label it
\pgftransformrotate{\theta/2}
\node at (0,-0.90*\length) {$q_{\scriptscriptstyle\index}$};
% Rotate to end of arc
\pgftransformrotate{\theta/2}
% Draw the link
\draw [thick] (0,0)--(0,-\length);
% Label the link
\draw[snake=brace] (\m+1mm,0)--(\m+1mm,-\length);
\node at (\m+6mm,-0.5*\length) {$l_{\scriptscriptstyle\index}$};
% Draw the mass
\shade[ball color=black] (0,-\length) circle (\m);
% Label the mass
\pgftransformshift{\pgfpoint{0}{-\length}}
\pgftransformrotate{-\theta}
\node at (-\m/2-2mm, -\m/2-2mm) {$m_{\scriptscriptstyle\index}$};
\pgftransformrotate{\theta}
\pgftransformshift{\pgfpoint{0}{\length}}
% Reset the coordinates back to what they were prior to this command
\pgftransformrotate{-\theta}
\pgftransformshift{\pgfpoint{-\x}{-\y}}
}
%% The class has several options
% onecolumn/twocolumn - format for one or two columns per page
% 10pt/11pt/12pt - use 10, 11, or 12 point font
% oneside/twoside - format for oneside/twosided printing
% final/draft - format for final/draft copy
% cleanfoot - take out copyright info in footer leave page number
% cleanhead - take out the conference banner on the title page
% titlepage/notitlepage - put in titlepage or leave out titlepage
%
%% The default is oneside, onecolumn, 10pt, final
%%% Replace here with information related to your conference
\confshortname{IDETC/CIE 2013}
\conffullname{the ASME 2013 International Design Engineering Technical Conferences \&\\
Computers and Information in Engineering Conference}
%%%%% for date in a single month, use
%\confdate{24-28}
%\confmonth{September}
%%%%% for date across two months, use
\confdate{4-7}
\confdate{August}
\confyear{2013}
\confcity{Portland}
\confcountry{USA}
%%% Replace DETC2009/MESA-12345 with the number supplied to you
%%% by ASME for your paper.
\papernum{IDETC/CIE 2013-13470}
%%% You need to remove 'DRAFT: ' in the title for the final submitted version.
\title{Constrained Multibody Dynamics With Python: From Symbolic
Equation Generation to Publication}
%%% first author
\author{Gilbert Gede\thanks{Address all correspondence to this author}, Dale L.
Peterson, Angadh S. Nanjangud, Jason K. Moore, Mont Hubbard
\affiliation{
Sports Biomechanics Laboratory\\
Department of Mechanical and Aerospace Engineering\\
University of California\\
Davis, California 95616\\
Email: \{ggede, dlpeterson, asnanjangud, jkmoor, mhubbard\}@ucdavis.edu
}
}
\begin{document}
\maketitle
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
\begin{abstract}
% Context
\it Symbolic equations of motion (EOMs) for multibody systems are desirable
for simulation, stability analyses, control system design, and parameter
studies.
% Need (what we have and what we want)
Despite this, the majority of engineering software designed to analyze
multibody systems are numeric in nature (or present a purely numeric user
interface). To our knowledge, none of the existing software packages are 1)
fully symbolic, 2) open source, and 3) implemented in a popular, general,
purpose high level programming language.
% Task
In response, we extended SymPy (an existing computer algebra system implemented
in Python) with functionality for derivation of symbolic EOMs for constrained
multibody systems with many degrees of freedom.
% Object of the document
We present the design and implementation of the software and cover the basic
usage and workflow for solving and analyzing problems. The intended audience is
the academic research community, graduate and advanced undergraduate students,
and those in industry analyzing multibody systems.
% Findings
We demonstrate the software by deriving the EOMs of a N-link pendulum, show its
capabilities for \LaTeX\ output, and how it integrates with other Python
scientific libraries - allowing for numerical simulation, publication quality
plotting, animation, and online notebooks designed for sharing results.
% Conclusion
This software fills a unique role in dynamics and is attractive to academics
and industry because of its BSD open source license which permits open source
or commercial use of the code.
% TODO cite BSD license
% Perspectives
\end{abstract}
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
\section*{INTRODUCTION}
There are many dynamic systems which can be better or more effectively studied
when their EOMs are accessible in a symbolic form. For equations that may be
visually inspected (i.e., of reasonable length), symbolics are generally
preferable because the interrelations of the variables and constants can give
clear understanding to the nature of the problem without the need for numerical
simulation. Many classic problems fit this category, such as the
mass-spring-damper, double pendulum, rolling disc, rattleback, and tippy-top.
The benefits of symbolic equations of motion are not limited to these basic
problems though. Larger, more complicated multibody systems can also be studied
more effectively when the equations of motion are available symbolically.
Advanced simplification routines can sometimes reduce the length of the
equations such that they are human readable and the intermediate derivation
steps are often short enough that symbolic checks can be used to validate the
correctness. Furthermore, the symbolic form of the EOMs often evaluate much
faster than their numerical counterparts, which is a significant advantage for
real time computations. Problems in biomechanics, spacecraft dynamics, and
single-track vehicles have all been successfully studied using symbolic EOMs.
Having the symbolic equations of motion available permits numerical simulation,
but also allows for a more mathematical study of the system in question. System
behavior can be studied parametrically by examining coefficients in the
differential equations. This includes symbolic expressions for equilibria
points and symbolic conditions for the stability of these points. The symbolic
form also allows for more complicated tasks, such as analyzing how
infinitesimal changes in system parameters (masses, lengths, inertias) affect
the dynamics, studying lumped parameter discretization sizing, and analyzing
how coordinate choices affect problem complexity or configuration
singularities. It also becomes possible to share the equations of motion in a
``written'' form to other individuals for collaboration, validation, or
comparison reasons. This allows for the EOMs to be used with other software
packages, for multi-domain simulation, hardware-in-the-loop testing, or for use
in optimal control/optimization problems.
Before adequate computing technology was available, the equations of motion for
multibody dynamics problems were formed by hand. There are many methodologies
to obtain the correct equations of motion (Newton-Euler, Lagrange, Kane,
Hamilton, etc). But all methods are tedious and error-prone when derived by
hand, which limits the size and complexity of systems which can be studied. It
only takes a handful of unique orientations between a small set of rigid bodies
within the system to reach this point of complexity. The introduction of
computer algebra systems (CAS) has reduced the difficulty involved in forming
the equations of motion, but it has not completely eliminated these problems.
However, the details of the symbolic algebra, differentiation, and vector
calculus can be handled by a reliable CAS, eliminating the errors associated
with those operations, allowing the user to think more about the implications
of the dynamic equations.
The software presented herein addresses some of the limitations of hand
derivations and allows for the symbolic study of complex multibody dynamics
problems. There already exist software packages which similarly meet these
limited criteria (e.g. Autolev/MotionGenesis, AutoSim/VehicleSim). But when
developing our software, we also included these unique requirements:
\begin{enumerate}
\item The software should be open source with a liberal license, encourage
collaborative development, ensure continued project development, not be
limited by or rely on any individual or organization, and allow easy
integration and use by other projects.
\item The software should be written in a popular high level programming
language that balances efficient execution speed with efficient programmer
development time, and has a wide selection of scientific libraries (or can
conveniently interface with libraries written in other languages).
\item The software should be built on top of an existing full-featured
symbolic CAS that is also open source.
\item The software should easily export the equations in formats that are
publication friendly (i.e., \LaTeX) or are compatible with other popular
computing platforms and languages (i.e., Modelica, C/C++/Fortan, MATLAB).
\end{enumerate}
To meet these criteria, we selected Python as the programming language to
implement our software. Python is interactive, high level, easy to learn,
widely available, widely used, cross platform, open source, and has a large
scientific user base.
Our software is distributed as a sub-package of SymPy \cite{sympy2012}, which
is a full featured CAS written in Python. SymPy is part of the SciPy Stack
\cite{SciPyStackGithub} specification and is included with all scientific
Python distributions including Enthought, Sage, Anaconda, and Python(x,y).
SymPy is one of the more actively developed Python packages with a large number
of maintainers, ensuring a long future. The SymPy development model allows new
functionality to be easily added and allows for other users to view our code,
suggest additional features, and improve upon and add to what we have already
done, as well as ensure that the our code is constantly tested against any
changes or updates to the base symbolic functionality offered by SymPy.
In this paper, we discuss two main topics: 1) The interface to the EOM
generation sub-package sympy.physics.mechanics, and 2) the workflow for
studying multibody dynamic systems (from derivation to simulation and
visualization), which we call Python Dynamics (PyDy). We will explore these two
topics through an explanation of the software design and by demonstrating a
test problem which displays software functionality and usage, how our software
is incorporated into a workflow for analyzing dynamic systems, and the results
of these processes. We will then discuss a number of other features, internal
constructions within our software, and verification with benchmark examples.
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
\section*{DEMONSTRATION PROBLEM}
We now demonstrate the value of PyDy through the derivation of the $N$-pendulum
system shown in Figure \ref{fig:n_pendulum}. The system is defined by $N$
massless links of length $l_i$ with particles of mass $m_i$ fixed at one end.
We selected this problem because it illustrates the power and utility of having
EOM generation code available within a full-featured programming language. The
angular velocity of each and every link must be found, as well as the velocity
of each particle. The velocity of $i$-th particle is
\begin{align*}
%\omega_i &= u_i \cdot a_z\\
\bar{v}_i &= \bar{v}_{i-1} + \bar{\omega}_i \times
\bar{r}^i \qquad (i = 1,\dots,N)
\end{align*}
This nesting of velocities is best addressed with a loop, something that a
computer is well suited for (loop unrolling is difficult by hand when there are
many steps and $N$ is large). There are thirty-seven lines of source code
required to derive the dynamic equations of motion for the $N$ pendulum, where
$N$ is the number of links, is shown in Figure \ref{fig:n_pendulum_source}.
The script first imports necessary functions and classes, then declares a
number of symbolic variables that represent generalized coordinates,
generalized speeds, constant parameters, reference frames, points and
particles. A few empty lists are created before the for loop is entered; these
lists are filled by the loop. When the final iteration of the for loop is
complete, the kinematics and all active forces of the problem have been
completely specified. The last two lines of the script take this specification
of kinematics and dynamics and generate Kane's dynamical equations of motion
($F_r + F_r^* = 0$) in symbolic form. At this point, these equations may be
manipulated as fully symbolic variables for a variety of purposes. For example,
the command \verb|mlatex(fr)| generates \LaTeX\ code for the generalized active
force $F_r$, which renders as:
\begin{equation}
\left[\begin{smallmatrix}g l_{0} m_{0} \operatorname{sin}\left(q_{0}\right) + g l_{0} m_{1} \operatorname{sin}\left(q_{0}\right) + g l_{0} m_{2} \operatorname{sin}\left(q_{0}\right) + g l_{0} m_{3} \operatorname{sin}\left(q_{0}\right)\\g l_{1} m_{1} \operatorname{sin}\left(q_{1}\right) + g l_{1} m_{2} \operatorname{sin}\left(q_{1}\right) + g l_{1} m_{3} \operatorname{sin}\left(q_{1}\right)\\g l_{2} m_{2} \operatorname{sin}\left(q_{2}\right) + g l_{2} m_{3} \operatorname{sin}\left(q_{2}\right)\\g l_{3} m_{3} \operatorname{sin}\left(q_{3}\right)\end{smallmatrix}\right]
\end{equation}
with no further modification from the user.
\begin{figure}
\begin{center}
\begin{tikzpicture}[scale=1.0]
\draw [thick] (-2cm,3mm)--(2cm,3mm);
\draw [thick, rounded corners=1mm] (-3mm,3mm)--(0,-3mm)--(3mm,3mm);
\draw [->,thick] (5mm,0)--(10mm,0);
\node at (12mm,0) {$\hat{\mathbf{a}}_y$};
\draw [->,thick] (0,-21mm)--(0,-26mm);
\node at (0,-28mm) {$\hat{\mathbf{a}}_x$};
\draw [->,thick] (-10mm,-60mm)--(-10mm,-70mm);
\node at (-10mm,-72mm) {$g$};
%\drawpendulum{ x}{ y}{ deg}{ l}{ m}{i}
\drawpendulum{0cm}{0cm}{22.5}{2cm}{1mm}{0}
\drawpendulum{0.76536686cm}{-1.847759cm}{45}{3cm}{3mm}{1}
\node at (3cm,-5cm) {$\vdots$};
\node at (3cm,-5.5cm) {$\vdots$};
\drawpendulum{3.5cm}{-6cm}{22.5}{4cm}{2mm}{N-1}
\foreach \x in {-2cm,-1.5cm,-1.0cm,-0.5cm,0cm,0.5cm,1.0cm,1.5cm,2cm}
\draw[thick] (\x,3mm)--(\x-1mm,5mm);
\end{tikzpicture}
\end{center}
\caption{N-pendulum system, a sequence of massive links connected by revolute
joints subjected to a gravitational field.}
\label{fig:n_pendulum}
\end{figure}
\begin{figure*}
\fvset{frame=single}
\VerbatimInput{n_pends_minimal.py}
\caption{User Python script to derive equations of motion for N-pendulum}
\label{fig:n_pendulum_source}
\end{figure*}
There are other options besides \LaTeX\ output which are useful. Within a
console, commands to ``pretty print'' symbolic expressions can be performed
with \verb|mpprint|, which generates the output formatted just like the
\LaTeX\ equation above, but within the terminal.
Another part of studying dynamic systems is simulation and visualization of the
results. SymPy can only analytically solve simple ODEs, so the equations of
motion generated for more complex systems need to be passed to other numerical
integrators. Currently, sympy.physics.mechanics can make use of existing SymPy
translation functions, but more advanced options to generate compiled code are
being developed and guided by user demands. The SymPy translation function
\verb|lambdify| can convert symbolic expressions to a NumPy compatible
function. The code in Figure \ref{fig:numerical_code} (which is executed after
the previously written code) shows this method.
\begin{figure*}
\begin{Verbatim}[frame=single]
from pylab import *
from sympy import Dummy, lambdify
from scipy.integrate import odeint
parameters = [g] # Parameter Definitions
parameter_vals = [9.81] # First we define gravity
for i in range(n):
parameters += [l[i], m[i]] # Then each mass
parameter_vals += [1. / n, 0.01 / n] # and length
dummy_symbols = [Dummy() for i in q + u] # Necessary to translate
dummy_dict = dict(zip(q + u, dummy_symbols)) # out of functions of time
kds = kane.kindiffdict() # Need to eliminate qdots
mm_sym = kane.mass_matrix_full.subs(kds).subs(dummy_dict) # Substituting away qdots
fo_sym = kane.forcing_full.subs(kds).subs(dummy_dict) # and in dummy symbols
mm = lambdify(dummy_symbols + parameters, mm_sym) # The actual call that gets
fo = lambdify(dummy_symbols + parameters, fo_sym) # us to a NumPy function
def rhs(y, t, args): # Creating the rhs function
vals = hstack((y, args)) # States and parameters
sol = linalg.solve(mm_sym(*vals), fo_sym(*vals)) # Solving for the udots
return array(sol).T[0]
y0 = hstack((arange(n) * 0.01, arange(n) * 0)) # Initial conditions, q & u
t = linspace(0, 10, 1000) # Time vector
y = odeint(rhs, y0, t, args=(parameter_vals,)) # Actual integration
\end{Verbatim}
\caption{User input Python script to perform numerical integration}
\label{fig:numerical_code}
\end{figure*}
NumPy is an integral part of the larger Scientific Python ecosystem, focusing
primarily on numerical arrays and matrices and operations on these arrays and
matrices. SciPy is another part of this ecosystem that provides quick and
simple Python wrappers to a large library of legacy scientific code. The third
necessary component of this ecosystem is matplotlib, a Python plotting library
for visualization of the large datasets generated by NumPy and SciPy code.
Using these three Python packages, we can numerically integrate ODEs and plot
the results, which are shown in Figure \ref{fig:time_series}.
\begin{figure}
\includegraphics[width=\columnwidth]{four_link_pendulum_time_series}
\caption{Time history of generalized coordinates and speeds for a 4 link
pendulum.}
\label{fig:time_series}
\end{figure}
Using other Python packages, such as MayaVi, 3D animations can be created. Use
of human-interface-devices (with a sufficiently fast computer) allows for
real-time interaction between a user and a visualized simulation.
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
\section*{SOFTWARE VALIDATION}
Anytime new software is developed to generate equations of motion, the validity
and accuracy of the software comes into question. We have addressed these
concerns in three ways to ensure that our code does generate correct equations
of motion for arbitrarily complex systems. Firstly, the code is open source and
well documented. This allows anyone to review the code and check for bugs.
Linus's Law ``given enough eyeballs, all bugs are shallow'' \cite{Raymond1999}
applies, if true. Secondly, the code functionality is thoroughly checked with
unit testing; each piece of independent functionality in the code has a test
(known input/output) in place that guarantees correct functioning of each unit.
This ensures that not only the current code works as expected, but also that
future versions are automatically checked against the same expected behavior.
Thirdly, there are built in tests for well benchmarked problems in mutlibody
dynamics. There are many problems, both simple and complex, that have well
known symbolic solutions. We have chosen several benchmark problems that
include sequential rotations, configuration and motion constraints, and
examination of noncontributing forces. These problems are built into the test
suite for the package.
Built in tests which validate the equations of motion that are generated
include: varying degrees of freedom spring-mass-damper systems, various
pendulums, multiple rolling disc examples testing auxiliary and dependent
speeds, and an inverted-pendulum cart. These are all compared to results found
by hand (checked multiple times). The other parts of sympy.physics.mechanics
include hundreds of tests on other pieces of the overall functionality.
There are also some external (non-automated) tests which are more advanced.
Currently, the most complicated test validates the formulation of the equations
of motion for a bicycle (a system with configuration and velocity constraints),
symbolically linearizes it, and compares it (successfully) to benchmark values
presented in \cite{Meijaard2007}.
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
\section*{USAGE}
%%%%%%%%%%%% JASON BELOW HERE %%%%%%%%%%%%
This section deals with obtaining the software demonstrated in this paper and
the available resources for learning to use it. All of the software
demonstrated in this paper can be readily obtained for free and installed on
virtually any platform. Also, all of the packages are liberally licensed with a
BSD or compatible license and either stable releases or development branches
can be downloaded.
To obtain and use the core \verb|mechanics| package for symbolic equation of
motion generation, one must simply download and install Python version 2.5+ and
SymPy version 0.7.2+\footnote{One of the major requirements for code added to
SymPy is that every function and object has to be thoroughly tested and
documented. SymPy has over 88\% of its code tested by the automated unit-tests.
This ensures that no update causes regressions or breaks current functionality.
Generally, the SymPy development branch is more stable and contains fewer bugs
than the numbered releases.}. Download and installation instructions for each
can be found on the softwares' respective web sites, www.python.org and
www.sympy.org.
To run a full PyDy example from equation of motion generation to simulation and
visualization, Python and at least the Scientific Python stack (SciPy)
\cite{SciPyStackGithub} must be obtained. SciPy provides more comprehensive
installation instructions than space permits here, but we make use of these
packages in the SciPy stack in the previous demo problem:
%
\begin{itemize}
\item SymPy: http://sympy.org/
\item NumPy: http://www.numpy.org/
\item SciPy: http://www.scipy.org/
\item matplotlib: http://matplotlib.org/
\end{itemize}
Download and installation instructions for various platforms are available on
their respective web sites. But it is worth noting that these packages are part
of most of the widely used scientific Python distributions. Downloading a
distribution binary is generally the easiest method of installing \emph{all} of
the needed software for a user unfamiliar with Python. Popular scientific
distributions that provide the needed software are listed below:
%
\begin{itemize}
\item Enthought: http://www.enthought.com/
\item Sage: http://www.sagemath.org/
\item Anaconda: http://continuum.io/
\item Python(x,y): http://www.pythonxy.com
\end{itemize}
The first step in doing multibody dynamics with Python is to get familiar using
\verb|mechanics|\footnote{Some may prefer to learn Python and the SciPy Stack
first, but the authors do not think this is such a necessity. It boils down to
preference and learning style.}. The first stop is the SymPy documentation which
is available online \cite{SymPyDocs}. The documentation provides detailed
instructions on installation, has introductory tutorials, lists common
mistakes, details development procedures and the internal architecture, and
contains detailed documentation for all of the subpackages and modules. In
particular, the \verb|mechanics| documentation contains over 60 pages that aim
to provide an overview of using the package and a brief introduction to the
fundamentals dynamics. Several example classic dynamics problems are included
in the documentation and there are even more in the \verb|mechanics.tests|
package. Working through the material in the \verb|mechanics| documentation
will provide the basics of generating the symbolic equations of motion of
multibody systems.
Additionally, a wiki for PyDy is maintained at www.pydy.org. This is a
user-editable guide to solving dynamics problems in Python, and contains
numerous introductory examples that demonstrate the process from system
definition to simulation and visualization, examples of interfacing
\verb|mechanics| with various compiled languages, and more advanced use cases
to demonstrate capabilities. As the PyDy workflow is integrated into more
university courses, the goal is to allow professors, teaching assistants, and
students to utilize, refine, and expand the wiki.
Finally, each of the software packages listed above maintains email lists and
IRC channels for ``live'' help and the communities supporting the software are
quite amicable to beginners. The PyDy Google Group is a good place to start if
you have questions \cite{PyDyGoogleGroup}.
%
\section*{SOFTWARE DESIGN}
The software design for \verb|mechanics| is influenced by Python's object
oriented nature, the underlying SymPy data types, Kane's method for generating
equations of motion\cite{Kane1985} for multibody systems, and the proprietary
(now defunct) software, Autolev\cite{Kane2000}, which also implemented Kane's
method in a symbolic fashion.
Kane's method powers many of the dynamic system software packages available
\cite{Sayers1990, Enlighten2013} due to its detailed bookkeeping design and
ease of mapping to programming languages. Kane's method has influenced the
design of \verb|mechanics| a great deal, but the code is structured so that any
method for deriving the equations can be used. This is possible because we
separated the kinematic code from the equations of motion generation code. We
have recently included Lagrange's method to demonstrate that unique ability.
SymPy's symbolic manipulation library provides the core functionality for the
mechanics package. The majority of objects that are created when using SymPy
are expression objects, \verb|Expr|. Other symbolic objects in SymPy, such as
symbols, adds and muls, or exponentials are inherited from the \verb|Expr|
class. The \verb|mechanics| package is dependent on these objects, but not via
inheritance. \verb|mechanics| is made up of a number of classes and functions
spread out over several modules which are explained in the following list:
%
\begin{description}
\item[essential.py] contains the basic building blocks for working with
vector calculus and dynamic systems and includes the following classes and
functions:
\begin{description}
\item[ReferenceFrame] is a class that represent a rotational reference
frame in a dynamic system. \verb|ReferenceFrame| has three orthonormal
basis unit vectors and manages information about the frame's
orientation, angular velocity, and angular acceleration relative to
other reference frames through a direction cosine matrix and velocity
and acceleration vectors. It is closely interlinked to the
\verb|Vector| class, i.e. \verb|Vector|s have associated
\verb|ReferenceFrame|s and \verb|ReferenceFrames|s have associated
\verb|Vector|s.
\item[Vector] is a class that represents a generic three dimensional
vector built from components in multiple frames of reference. Vectors
support all of the common operations as one would expect such as
addition, subtraction, multiplication, division, dot products, cross
products, outer products, re-expression into different reference
frames, and frame dependent differentiation.
\item[Dyadic] is a class that represents a generic Dyadic. Dyadics are
used in this software as a basis independent method of defining an
inertia tensor. Dyadics support all of the common operations, similar to
the Vector class.
\item[dynamicsymbols] is a function that is used to facilitate the generation
of time dependent quantities and their derivatives. These variables are
created as SymPy \verb|Function|s of time, where the default time is
the symbols \verb|t|.
\end{description}
\item[point.py] contains the \verb|Point| class. This class manages
and tracks the location, velocity, and acceleration of a point in space
relative to another point. It also provides some convenience methods to set
velocities and accelerations via the one point and two point theories
\cite{Kane1985}.
\item[functions.py] contains an assortment of convenience functions. For
example there is a function for generating inertia dyadics from tensor
notation, a function that outputs kinematical differential equations for
various body or spaced fixed coordinates and speeds, functions to generate
linear and angular momenta or kinetic and potential energies for a general
system of particles and bodies, among others.
\item[particle.py] contains the \verb|Particle| class which functions as a
container class for a point and an associated mass. It also has methods for
computing momentum and energy.
\item[rigidbody.py] contains the \verb|RigidBody| is analogous to the
\verb|Particle| class but for rigid bodies and contains mass, mass center,
inertia, and a reference frame associated with the rigid body. It also has
methods for momentum and energy.
\item[kane.py] contains the \verb|KanesMethod| class which automates the
generation of a system's non-linear equations of motion using Kane's
method\cite{Kane1985} and linear equations of motion using the method
presented in \cite{Peterson2013}. A \verb|KanesMethod| object is initialized
with an inertial reference frame, set of particles and/or rigid bodies, a
set of forces and torques acting on the system, the desired kinematical
differential equations, the desired independent and dependent generalized
speeds, any configuration constraints, any velocity constraints, and any
auxiliary speeds needed to compute non-contributing forces.
\item[lagrange.py] contains the \verb|LagrangesMethod| class which automates
the generation of a system's non-linear equations of motion via the methods
of Lagrangian mechanics\cite{Crandall1968}. To derive the equations of
motion of a constrained system using Lagrange's equations, one requires the
configuration and velocity constraint equations, if any, before proceeding
to derive a complete set of dynamical equations that describe said system.
The \verb|LagrangesMethod| object is initialized with a Lagrangian and the
desired generalized coordinates and optionally forces acting on the system,
velocity constraints, and an inertial reference frame. If velocity
constraints are supplied, Lagrange multipliers are generated to account for
them and non-conservative forces are appropriately handled if they affect
the system.
\end{description}
\subsection*{ESSENTIAL}
As previously mentioned, the submodule essential.py (which is the core of
sympy.physics.mechanics) includes \verb|ReferenceFrame|, \verb|Vector|,
\verb|Dyadic|, and \verb|dynamicsymbols|, as well as some output functions.
These classes will be explained in some detail, to allow for a greater
understanding of how our software was written and how it functions.
Firstly, \verb|dynamicsymbols| will be explained - it is merely a shortcut to
producing quantities which are functions of time.
It is included for two reasons: specifics relating to Python
importing requirements, and because \verb|dynamicsymbols| defines the symbol
used to represent time (default ``\verb|t|'').
All of the vector calculus methods assume that functions of time define
rotations between \verb|ReferenceFrame|s; if basic symbols or expressions which
are not functions of time are supplied, they will be treated as constants when
differentiating with respect to time.
The relationship between \verb|ReferenceFrame| and \verb|Vector| is very
complex. Upon initialization, a \verb|ReferenceFrame| has three vectors
representing the orthonormal basis vectors of that reference frame. A
\verb|Vector| is made up of a list of segments per associated frame. For each
unique \verb|ReferenceFrame| involved in the definition of a vector, one
element in this list exists. Each element in the list contains the associated
\verb|ReferenceFrame| and a $3\times1$ SymPy matrix representing the measure
numbers for each frame. The basis vectors, which are created upon
\verb|ReferenceFrame| initialization, have a list of length 1 and are made up
of the \verb|ReferenceFrame| they are created in and a matrix that defines one
of the standard basis vectors (e.g. $[1, 0, 0]$).
As objects, both these basis vectors and other general vectors are instances of
the same \verb|Vector| class. More complicated \verb|Vector|s just consist of
longer lists and matrices. More frames can be introduced by adding vectors
together or performing more advanced vector and vector calculus operations.
The final two parts of \verb|Vector|'s design are in the users interaction with
these objects, i.e. creating and displaying them. Direct initialization of a
\verb|Vector| object by a user should never take place; more complicated
vectors will be formed out of basis vectors from the \verb|ReferenceFrame|s and
operations between \verb|Vector|s. When displaying a \verb|Vector| object to
the user, the complex implementation details of each instance are masked.
Instead, the user only sees something along the following lines:
\begin{verbatim}
3*A.x + 5*A.y + sin(theta)*C.z
\end{verbatim}
Each measure number and accompanying basis vector are printed out in a way that
the output can be copied and reentered to form the \verb|Vector| again. This
leaves our \verb|Vector| class as a symbolic object (although, not a subclass
of the main SymPy \verb|Expr| class) which users will interact with on a
symbolic/mathematical level. The complex initialization should never have to be
done by hand, thus making use of this class is easy for people not intimately
familiar with Python and SymPy.
In order to allow interactions between vectors defined in different reference
frames, information is stored which relates each reference frame to others.
The user defines how one frame is oriented to another, using a simple rotation
around an arbitrary axis, standard body- or space-fixed angles, quaternions, or
Euler parameters. Once this is defined, each of the involved
\verb|ReferenceFrame|s sets its internal dictionary, where a pointer to the
other frame and the generated direction cosine matrix are stored together
(transposing happens for one of the frames). When the orientation matrix
between two frames is requested, if it has not already been defined, the code
will search through all possible branches to find the other frame, and then
multiply all of the orientation matrices in order to generate the direction
cosine matrix between the two frames. After doing so, it will be saved so
future searching does not have to happen again.
Angular velocities between frames are set in a similar way.
When the user orients one frame relative to another, the angular velocity is
generated by taking the time derivative of the direction cosine matrix.
This is usually not desirable though, so the user is free to overwrite the
angular velocity vector between frames.
Again, setting this in one frame will set an equal and opposite vector in the
other frame, to ensure consistency.
Also, the same tree search occurs for angular velocities, except it involves
adding angular velocity vectors instead of multiplying direction cosine matrices.
One potential pitfall is the possibility of a user closing a loop of
\verb|ReferenceFrame|s.
In doing so, it is possible for the user to create internally inconsistent
rotations or angular velocities; in other terms, if they don't use the correct
value when closing the loop, the code does not detect this and incorrect
results might be generated.
Users are instructed to avoid doing this, and we feel it is an unlikely
scenario, as it requires extra, unneeded work on the user's part.
The \verb|Point| class functions in a similar manner to \verb|ReferenceFrame|,
in that it has a tree which links the position of this point to other points
and is searchable to find the position between two points which have not been
directly assigned.
However, the \verb|Point| class does not extend this functionality to
velocities; it only works for positions.
This limitation is due to the complexities of identifying bound/unbound vectors within
reference frames.
It has been more reliable to ask the user to find these velocities themselves
rather than attempting to do it automatically (and frequently incorrectly).
In order to help with this task, the \verb|Point| class has a number of methods
using the one point and two point theorems \cite{Kane1985} to make this step
easier.
The \verb|Dyadic| object has a similar construction approach as \verb|Vector|,
i.e. it is made up of a list of components.
However, for a dyadic, there are three parts of each list entry: a measure number,
the first basis vector, and the second basis vector.
The lists which compose a \verb|Dyadic| object look like:
\begin{verbatim}
[(J, A.x, A.x), (I, A.x, B.y)]
\end{verbatim}
which in turn is printed as:
\begin{verbatim}
J*(A.x|A.x) + I*(A.x|B.y)
\end{verbatim}
which again follows the SymPy convention that the displayed version of this
object can be copied and pasted in order to remake the object.
The vector math and calculus associated with \verb|Dyadic| is similar to that
in \verb|Vector|. The first or second basis vector is operated upon, depending
on whether pre or post dot and cross products are used.
For a user, once all kinematics and system parameters have been defined, the
next step is generating the equations of motion.
There are two included methods for generating EOM: Kane's and Lagrange's.
Both of these objects require the system's definition to be passed in using the
container classes \verb|Particle| and \verb|RigidBody|.
These objects (as described above) store the minimum amount of information for
a body that is needed to create the equations of motion.
\subsection*{KanesMethod Class}
Upon initialization, it takes in a number of properties which describe the
system: the inertial reference frame; independent and constrained generalized
coordinates; independent, auxiliary, and constrained (dependent) generalized
speeds; and configuration, velocity, and (optionally) acceleration constraint
equations. At this point, the relationships between the independent and
constrained speeds are found as in Kane's Method \cite{Kane1985}; this is shown
in equation (\ref{eq:Ars_forming}), where $f_v(q, u, t)$ is the list of
constraint equations and $u$ is the list of independent and dependent speeds.
\begin{align}
%\begin{subequations}
\mathbf{0} &= \mathbf{f_v}(q, u, t) \\
&= \nabla_u \mathbf{f_v}(q, u, t) \mathbf{u} \\
&= \mathbf{B} \mathbf{u} \\
&= \mathbf{B}_{ind} \mathbf{u}_{ind} + \mathbf{B}_{dep}
\mathbf{u}_{dep} \\
\implies \mathbf{u}_{dep} &= - \mathbf{B}_{dep}^{-1} \mathbf{B}_{ind} \mathbf{u}_{ind} \\
&= \mathbf{A} \mathbf{u}_{ind}
%\end{subequations}
\label{eq:Ars_forming}
\end{align}
The configuration constraints are used directly when forming the equations of
motion, but they do need to be supplied if the system is going to be linearized
\cite{Peterson2013}.
From here, the formulation of the term $\mathbf{F}_r$ follows what Kane
presented, with the advantage that all of the vector addition and
multiplication is carried out symbolically. If necessary, the unconstrained
generalized active forces can be transformed into the constrained generalized
active forces, where $n$ is the total number of generalized speeds, $p$ is the
number of independent speeds, leaving $m$ as the number of constrained speeds;
this is shown in equation (\ref{eq:uncon_to_con}).
\begin{equation}
\label{eq:uncon_to_con}
\tilde{\mathbf{F}}_{ind} = \mathbf{F}_{ind} + \mathbf{A}^{T}
\mathbf{F}_{dep}
\end{equation}
The formulation of the generalized inertia forces is more complicated.
First, we defined $\mathbf{F}_r^*$ differently, as in equation (\ref{eq:x}).
\begin{equation}
\mathbf{F}_r^* = \mathbf{M}_m \mathbf{\dot{u}} + \mathbf{M}_n
\label{eq:x}
\end{equation}
$\mathbf{M}_m$ is the mass matrix of the system and $\mathbf{M}_n$ is all the
terms in $\mathbf{F}_r^*$ which are not part of the mass matrix. The
construction of these terms will be shown for a particle, but the procedure for
rigid bodies is almost the same, albeit for the rotational components. If we
start by defining the velocity of a particle $P$ in the inertial frame $A$ as:
\begin{equation}
^{A}\bar{v}^{P} = \sum_{i=1}^{n} {} ^{A}\bar{v}_{r}^{P}
\end{equation}
the inertial force $R^*$ for that particle can be written as:
\begin{align}
%\begin{subequations}
\bar{R}^* &= -\frac{^{A} d}{dt}(m ^A\bar{v}^P) \\
&= -m \frac{^{A}d}{dt}^A\bar{v}^P - \dot{m} ^A\bar{v}^P \\
&= -\dot{m} ^A\bar{v}^P - m \frac{^{A}d}{dt}\left(\sum_{i=1}^{n}{} ^A
\bar{v}^P_i u_i \right) \\
&= -\dot{m} ^A\bar{v}^P - m \sum_{i=1}^{n} \left( ^A\bar{v}_i^P
\frac{d}{dt}u_i + u_i \frac{^{A}d}{dt} {}^A\bar{v}^P_i \right) \\
%\end{subequations}
\end{align}
We can then write:
\begin{align}
\mathbf{F^*}_r &= ^A\bar{v}^P_r \bar{R}^{*} \\
\mathbf{F^*}_r &= - \left[
^A\bar{v}^P_r \dot{m} ^A\bar{v}^P +
^A\bar{v}^P_r m \sum_{i=1}^{n} \left(
\dot{u}_i ^A\bar{v}^P_i + u_i
\frac{^{A}d}{dt} {}^A\bar{v}^P_i
\right)
\right]
\end{align}
From this equation, we can see that only the mass and partial velocity
terms multiply $\dot{u}$ terms, or that the mass matrix coefficients are made
up of the product of mass and the dot product between two partial velocities.
In fact, the location of the element in the mass matrix corresponds to the
index of each partial velocity (the order is not important as long as it is
consistent).
If we wanted to define this another way, we could write a vertical vector of
the partial velocities of particle $P$, $[^A\bar{v}^P_r]$, and then the
mass matrix would be:
\begin{equation}
\mathbf{M}_m = -m \left[^A\bar{v}_r^P\right] \left[^A\bar{v}_r^P \right]^T
\end{equation}
In either case, the non-mass matrix terms (which make up $M_n$) are the
collection of terms that do not involve $\dot{u}$'s.
As in Kane's method, the rotational and translational inertia forces and
torques are multiplied by the angular and translational partial velocities,
for each body/particle, summed across all bodies and particles.
To transform this for systems with nonholonomic constraints, we again
use equation (\ref{eq:uncon_to_con}), substituting $\mathbf{F}^*$ for
$\mathbf{F}$.
Using auxiliary speeds to bring noncontributing forces into evidence is
important to fully utilize Kane's method.
Upon initialization of a \verb|KanesMethod| object the user needs to supply
auxiliary speeds.
Assuming the auxiliary speeds were used correctly when forming velocities, the
user does not have to worry about these speeds again, and they will not show up
in any output equations.
When there are velocity constraints and auxiliary speeds, the relationship
between auxiliary speeds and constrained speeds needs to be found and
used in forming the equations.
To accomplish this, a second, internal \verb|KanesMethod| object is created
which has the same constraints and constrained speeds, but auxiliary speeds are
supplied as both independent and auxiliary speeds, leaving the rest of the math
the same.
More plainly, for any instance of \verb|KanesMethod|, auxiliary speeds are
removed from (set to 0) the accelerations and velocities that form
$\bar{R}, \bar{T}, \bar{R}^*$, and $\bar{T}^*$.
The only difference between the user's and the internal instance is which
generalized speeds are used to form the partial velocities: independent or
auxiliary.
The relationship between auxiliary speeds and constrained speeds is found
the same way as the relationship between the independent speeds and constrained
speeds, i.e. the matrix $\mathbf{A}$ is found to relate auxiliary and
constrained speeds.
The transformation from unconstrained auxiliary equations to the
constrained auxiliary equations ($\mathbf{F} + \mathbf{F}^*=0$ to
$\tilde{\mathbf{F}} + \tilde{\mathbf{F}}^* = 0$ is performed exactly the same
way, just using the matrix $\mathbf{A}$ that relates the auxiliary and
constrained speeds.
The entire process is transparent to the user.
As the constrained generalized speeds are not substituted out of the equations
generated, we will have fewer equations than independent and dependent speeds.
If we have $n$ total generalized speeds and $p$ independent speeds, we are left
with $m=n-p$ constrained speeds.
This means that we will have $p$ equations containing time derivatives of $n$
speeds, or not enough equations to solve for the $\dot{u}$'s.
We instead use the $m$ velocity constraint equations to generate the needed
equations.
When the velocity constraint equations are differentiated with respect to time,
we get $m$ equations (the additional number we needed) containing up to $n$
$\dot{u}$'s, giving the required information to solve for the time derivatives
of the generalized speeds.
We will only briefly discuss linearization here, as a more detailed description
of the linearization procedure used within \verb|KanesMethod| can be found
elsewhere \cite{Peterson2013}. The only complications that arise are when the
user has a constrained system, in which case relationships between dependent
and independent coordinates needs to be considered, as well as the relationship
between dependent speeds and independent speeds, independent coordinates, and
dependent coordinates. The important message for the user is
configuration constraints are not considered when forming the equations of
motion, but if they exist and are not supplied, the linear equations
generated will be incorrect.
\subsection*{LangrangesMethod Class}
In sympy.physics.mechanics, we assume that three basic sets of equations are
necessary to completely describe a system and obtain the symbolic equations
using \verb|LagrangesMethod|:
\begin{align}
\mathbf{0} &= \mathbf{m_{c}}(q, t) \dot{q} + \mathbf{f_{c}}(q, t) \label{eqn:lag_qd}\\
\mathbf{0} &= \mathbf{m_{dc}}(\dot{q}, q, t) \ddot{q} + \mathbf{f_{dc}}(\dot{q}, q,
t) \label{eqn:lag_qdd}\\
\mathbf{0} &= \mathbf{m_d}(\dot{q}, q, t) \ddot{q} + \Lambda_c(q, t)
\mathbf{\lambda} + \mathbf{f_d}(\dot{q}, q, t) \label{eqn:lag_eom}
\end{align}
where $q$ represents a vector of generalized coordinates, $\dot{q}$ and
$\ddot{q}$ are vectors of the first and second time derivatives of the
generalized coordinates, $\mathbf{\lambda}$ is a vector of the Lagrange
multipliers. $\mathbf{m_c}$, $\mathbf{m_{dc}}$, $\mathbf{m_d}$ and
$\Lambda_c$ are coefficient matrices.
Equation (\ref{eqn:lag_qd}) shows the constraint equations,
(\ref{eqn:lag_qdd}) shows the
first derivative of the constraint equations, and (\ref{eqn:lag_eom}) shows
the dynamical equations using Lagrange's equations. The
\verb|LagrangesMethod| class rearranges the equations of motion into the
following form:
\label{eqn:lag_rearr}
\begin{align}
\mathbf{M}(q, t) x = \mathbf{f}(q, \dot{q}, t)
\end{align}
where $\mathbf{M}$ is the 'mass matrix', and $x$ is a vector of the states,
namely the $\ddot{q}$'s and $\lambda$'s, if any.
The \verb|LagrangesMethod| class is initialized by suppliying properties that
describe a system: the Lagrangian, a list of the generalized coordinates,
holonomic and non-holonomic constraint equations (if any), the forces and/or
moments acting on the system, and the inertial reference frame.
The \verb|LagrangesMethod| class requires that holonomic constraint equation be
supplied after taking its first time derivative.
The forces supplied upon initialization are primarily to account for the
non-conservative forces acting on the system as the conservative forces are
accounted for in the computation of the Lagrangian.
Instead of the system's Lagrangian, the user may
supply the system's kinetic energy, and account for any conservative and/or
non-conservative forces in the force list.
Usage of the \verb|LagrangesMethod| class does not allow for bringing
non-contributing forces into evidence, or linearization functionality.
Otherwise, it provides mass matrix/forcing function outputs as in the
\verb|KanesMethod| class.
\section*{CONCLUSIONS}
We have presented a set of tools, PyDy, for forming the
equations of motion of a constrained dynamic system in an automated fashion.
The core of PyDy, the mechanics package within SymPy, is written in a
high-level programming language on top of a fully function computer algebra
system. We have demonstrated the use of our software, as well as how it fits
into the larger scientific Python ecosystem. We also detailed how our software
has been validated, why design decisions were made, and how its internal
architecture functions. All of the source code, including extra code which
generates a two dimensional animation of the N-link pendulum, are available
online \cite{SourceCode}.
\section*{ACKNOWLEDGEMENTS}
Three Google Summer of Code grants (2009, 2011, 2012) supported most of the
software development. This material is also partially based upon work supported
by the National Science Foundation under Grant No. 0928339. Any opinions,
findings, and conclusions or recommendations expressed in this material are
those of the author(s) and do not necessarily reflect the views of the National
Science Foundation.
\bibliographystyle{asmems4}
\bibliography{asme2e}
\end{document}