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System Simulation by Recursive Feedback: Coupling a Set of Stand-Alone Subsystem SimulationsConventional construction of digital dynamic system simulations often involves collecting differential equations that model each subsystem, arran g them to a standard form, and obtaining their numerical gin solution as a single coupled, total-system simultaneous set. Simulation by numerical coupling of independent stand-alone subsimulations is a fundamentally different approach that is attractive because, among other things, the architecture naturally facilitates high fidelity, broad scope, and discipline independence. Recursive feedback is defined and discussed as a candidate approach to multidiscipline dynamic system simulation by numerical coupling of self-contained, single-discipline subsystem simulations. A satellite motion example containing three subsystems (orbit dynamics, attitude dynamics, and aerodynamics) has been defined and constructed using this approach. Conventional solution methods are used in the subsystem simulations. Distributed and centralized implementations of coupling have been considered. Numerical results are evaluated by direct comparison with a standard total-system, simultaneous-solution approach.
Document ID
20020000781
Acquisition Source
Marshall Space Flight Center
Document Type
Technical Publication (TP)
Authors
Nixon, D. D.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Date Acquired
September 7, 2013
Publication Date
October 1, 2001
Subject Category
Mathematical And Computer Sciences (General)
Report/Patent Number
NASA/TP-2001-211331
NAS 1.60:211331
M-1032
Report Number: NASA/TP-2001-211331
Report Number: NAS 1.60:211331
Report Number: M-1032
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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