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Numerical simulation of actively controlled space structuresThe numerical simulation of large, actively controlled space structures is a problem that has received considerable attention. A new computational method is presented in this paper, which simulates the vibration suppression of a large space structure by a linear compensator. The structure is assumed to be modeled by a large linear finite element model. Nested circularly linked lists and the trapezoidal rule are key aspects of this algorithm. There is an emphasis on generality, while establishing an equivalence between numerical stability and system stability.
Document ID
19910055227
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Quan, Ralph
(Colorado Univ. Boulder, CO, United States)
Balas, Mark
(Colorado, University Boulder, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1990
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: NASA-UCLA Workshop on Computational Techniques in Identification and Control of Flexible Flight Structures
Location: Lake Arrowhead, CA
Country: United States
Start Date: November 2, 1989
End Date: November 4, 1989
Sponsors: NASA, ComCon Conference Board, University of California
Accession Number
91A39850
Distribution Limits
Public
Copyright
Other

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