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Real-time dynamic simulation of the Cassini spacecraft using DARTS. Part 2: Parallel/vectorized real-time implementationPart 1 of this paper presented the requirements for the real-time simulation of Cassini spacecraft along with some discussion of the DARTS algorithm. Here, in Part 2 we discuss the development and implementation of parallel/vectorized DARTS algorithm and architecture for real-time simulation. Development of the fast algorithms and architecture for real-time hardware-in-the-loop simulation of spacecraft dynamics is motivated by the fact that it represents a hard real-time problem, in the sense that the correctness of the simulation depends on both the numerical accuracy and the exact timing of the computation. For a given model fidelity, the computation should be computed within a predefined time period. Further reduction in computation time allows increasing the fidelity of the model (i.e., inclusion of more flexible modes) and the integration routine.
Document ID
19940010166
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Fijany, A.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Roberts, J. A.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
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
94N14639
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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