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Nonrecursive formulations of multibody dynamics and concurrent multiprocessingSince the late 1980's, research in recursive formulations of multibody dynamics has flourished. Historically, much of this research can be traced to applications of low dimensionality in mechanism and vehicle dynamics. Indeed, there is little doubt that recursive order N methods are the method of choice for this class of systems. This approach has the advantage that a minimal number of coordinates are utilized, parallelism can be induced for certain system topologies, and the method is of order N computational cost for systems of N rigid bodies. Despite the fact that many authors have dismissed redundant coordinate formulations as being of order N(exp 3), and hence less attractive than recursive formulations, we present recent research that demonstrates that at least three distinct classes of redundant, nonrecursive multibody formulations consistently achieve order N computational cost for systems of rigid and/or flexible bodies. These formulations are as follows: (1) the preconditioned range space formulation; (2) penalty methods; and (3) augmented Lagrangian methods for nonlinear multibody dynamics. The first method can be traced to its foundation in equality constrained quadratic optimization, while the last two methods have been studied extensively in the context of coercive variational boundary value problems in computational mechanics. Until recently, however, they have not been investigated in the context of multibody simulation, and present theoretical questions unique to nonlinear dynamics. All of these nonrecursive methods have additional advantages with respect to recursive order N methods: (1) the formalisms retain the highly desirable order N computational cost; (2) the techniques are amenable to concurrent simulation strategies; (3) the approaches do not depend upon system topology to induce concurrency; and (4) the methods can be derived to balance the computational load automatically on concurrent multiprocessors. In addition to the presentation of the fundamental formulations, this paper presents new theoretical results regarding the rate of convergence of order N constraint stabilization schemes associated with the newly introduced class of methods.
Document ID
19940010159
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kurdila, Andrew J.
(Texas A&M Univ. College Station, TX, United States)
Menon, Ramesh
(Texas A&M Univ. College Station, TX, United States)
Date Acquired
September 6, 2013
Publication Date
February 15, 1993
Publication Information
Publication: JPL, Proceedings of the Fifth NASA(NSF)DOD Workshop on Aerospace Computational Control
Subject Category
Structural Mechanics
Accession Number
94N14632
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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