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Closed-form Grammians and model reduction for flexible space structuresAnalytical expression are derived for the Grammians of a model in modal coordinates for the dynamics of a flexible space structure (FSS). These exact results provide insight into the dynamics of such systems and reduce the known approximate expressions in the case of lightly damped, widely separated modes. A novel algorithm is outlined that uses these to compute a dominant reduced-order model for such a system in an efficient manner.
Document ID
19890041223
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Williams, Trevor
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1988
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: IEEE Conference on Decision and Control
Location: Austin, TX
Country: United States
Start Date: December 7, 1988
End Date: December 9, 1988
Accession Number
89A28594
Distribution Limits
Public
Copyright
Other

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