Marshall Technical Reports Server

System Simulation by Recursive Feedback: Coupling a Set of Stand-Alone Subsystem Simulations

NASA/TP-211331, Nixon, D.D., System Simulation by Recursive Feedback: Coupling a Set of Stand-Alone Subsystem Simulations, National Aeronautics and Space Administration, Washington, DC 20546-0001, George C. Marshall Space Flight Center Marshall Space Flight Center, AL 35812, Prepared for Vehicle and System Development Department, Space Transportation Directorate, October 2001, pp. 196, Format(s): PDF 130800k

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Conventional construction of digital dynamic system simulations often involves collecting differential equations that model each subsystem, arranging them to a standard form, and obtaining their numerical 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.
Keywords:system simulation, coupled subsystems, multidiscipline, high fidelity, recursive, feedback, dynamic
Subjects:Mathmatical and Computer Sciences: Mathmatical and Computer Sciences (General): Applied Mathmatics
ID Code:578
Deposited On:01 August 2002