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Computer-aided design and distributed system technology development for large space structuresProposed large space structures have many characteristics that make them difficult to analyze and control. They are highly flexible, with components mathematically modeled by partial differential equations or very large systems of ordinary differential equations. They have many resonant frequencies, typically low and closely spaced. Natural damping may be low and/or improperly modeled. Coupled with stringent operational requirements of orientation, shape control, and vibration suppression, and the inability to perform adequate ground testing, these characteristics present an unconventional identification and control design problem to the systems theorist. Some of the research underway within Langley's Spacecraft Control Branch, Guidance and Control Division aimed at developing theory and algorithms to treat large space structures systems identification and control problems is described. The research areas to be considered are computer-aided design algorithms, and systems identification and control of distributed systems.
Document ID
19870006609
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Armstrong, Ernest S.
(NASA Langley Research Center Hampton, VA, United States)
Joshi, Suresh M.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
November 1, 1986
Publication Information
Publication: NASA(DOD Control)Structures Interaction Technology, 1986
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
87N16042
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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