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Real-time dynamics simulation of the Cassini spacecraft using DARTS. Part 1: Functional capabilities and the spatial algebra algorithmThis paper describes the Dynamics Algorithms for Real-Time Simulation (DARTS) real-time hardware-in-the-loop dynamics simulator for the National Aeronautics and Space Administration's Cassini spacecraft. The spacecraft model consists of a central flexible body with a number of articulated rigid-body appendages. The demanding performance requirements from the spacecraft control system require the use of a high fidelity simulator for control system design and testing. The DARTS algorithm provides a new algorithmic and hardware approach to the solution of this hardware-in-the-loop simulation problem. It is based upon the efficient spatial algebra dynamics for flexible multibody systems. A parallel and vectorized version of this algorithm is implemented on a low-cost, multiprocessor computer to meet the simulation timing requirements.
Document ID
19940010165
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Jain, A.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Man, G. K.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 6, 2013
Publication Date
February 15, 1993
Publication Information
Publication: Proceedings of the Fifth NASA(NSF)DOD Workshop on Aerospace Computational Control
Subject Category
Computer Programming And Software
Accession Number
94N14638
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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