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Staggered solution procedures for multibody dynamics simulationThe numerical solution procedure for multibody dynamics (MBD) systems is termed a staggered MBD solution procedure that solves the generalized coordinates in a separate module from that for the constraint force. This requires a reformulation of the constraint conditions so that the constraint forces can also be integrated in time. A major advantage of such a partitioned solution procedure is that additional analysis capabilities such as active controller and design optimization modules can be easily interfaced without embedding them into a monolithic program. After introducing the basic equations of motion for MBD system in the second section, Section 3 briefly reviews some constraint handling techniques and introduces the staggered stabilized technique for the solution of the constraint forces as independent variables. The numerical direct time integration of the equations of motion is described in Section 4. As accurate damping treatment is important for the dynamics of space structures, we have employed the central difference method and the mid-point form of the trapezoidal rule since they engender no numerical damping. This is in contrast to the current practice in dynamic simulations of ground vehicles by employing a set of backward difference formulas. First, the equations of motion are partitioned according to the translational and the rotational coordinates. This sets the stage for an efficient treatment of the rotational motions via the singularity-free Euler parameters. The resulting partitioned equations of motion are then integrated via a two-stage explicit stabilized algorithm for updating both the translational coordinates and angular velocities. Once the angular velocities are obtained, the angular orientations are updated via the mid-point implicit formula employing the Euler parameters. When the two algorithms, namely, the two-stage explicit algorithm for the generalized coordinates and the implicit staggered procedure for the constraint Lagrange multipliers, are brought together in a staggered manner, they constitute a staggered explicit-implicit procedure which is summarized in Section 5. Section 6 presents some example problems and discussions concerning several salient features of the staggered MBD solution procedure are offered in Section 7.
Document ID
19950025781
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Park, K. C.
(Colorado Univ. Boulder, CO, United States)
Chiou, J. C.
(Colorado Univ. Boulder, CO, United States)
Downer, J. D.
(Colorado Univ. Boulder, CO, United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1990
Subject Category
Structural Mechanics
Report/Patent Number
NAS 1.26:199034
CU-CSSC-90-07
NASA-CR-199034
Report Number: NAS 1.26:199034
Report Number: CU-CSSC-90-07
Report Number: NASA-CR-199034
Accession Number
95N32202
Funding Number(s)
CONTRACT_GRANT: NAG1-756
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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