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A case study in nonlinear dynamics and control of articulated spacecraft: The Space Station Freedom with a mobile remote manipulator systemThe following topics are discussed: (1) modeling of articulated spacecraft as multi-flex-body systems; (2) nonlinear attitude control by adaptive partial feedback linearizing (PFL) control; (3) attitude dynamics and control for SSF/MRMS; and (4) performance analysis results for attitude control of SSF/MRMS.
Document ID
19940031372
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bennett, William H. (Techno-Sciences, Inc. Greenbelt, MD, United States)
Kwatny, Harry G. (Techno-Sciences, Inc. Greenbelt, MD, United States)
Lavigna, Chris (Techno-Sciences, Inc. Greenbelt, MD, United States)
Blankenship, Gilmer (Techno-Sciences, Inc. Greenbelt, MD, United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1994
Publication Information
Publication: NASA. Langley Research Center, NASA Workshop on Distributed Parameter Modeling and Control of Flexible Aerospace Systems
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
94N35879
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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