Sub-domain decomposition methods and computational controls for multibody dynamical systems
Abstract
This paper presents a concurrent methodology to simulate the dynamics of flexible multibody systems with a large number of degrees of freedom. A general class of open-loop structures is treated and a redundant coordinate formulation is adopted. A range space method is used in which the constraint forces are calculated using a preconditioned conjugate gradient method. By using a preconditioner motivated by the regular ordering of the directed graph of the structures, it is shown that the method is order N in the total number of coordinates of the system. The overall formulation has the advantage that it permits fine parallelization and does not rely on system topology to induce concurrency. It can be efficiently implemented on the present generation of parallel computers with a large number of processors. Validation of the method is presented via numerical simulations of space structures incorporating large number of flexible degrees of freedom.
- Publication:
-
Computing Systems in Engineering
- Pub Date:
- 1992
- Bibcode:
- 1992ComSE...3..189M
- Keywords:
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- Conjugate Gradient Method;
- Data Simulation;
- Equations Of Motion;
- Flexible Spacecraft;
- Parallel Computers;
- Spacecraft Control;
- Degrees Of Freedom;
- Dynamical Systems;
- Preconditioning;
- Spacecraft Design, Testing and Performance