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An improved output feedback control of flexible large space structuresA special output feedback control design technique for flexible large space structures is proposed. It is shown that the technique will increase both the damping and frequency of selected modes for more effective control. It is also able to effect integrated control of elastic and rigid-body modes and, in particular, closed-loop system stability and robustness to modal truncation and parameter variation. The technique is seen as marking an improvement over previous work concerning large space structures output feedback control.
Document ID
19820042104
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Lin, Y. H.
(California Institute of Technology, Jet Propulsion Laboratory, Pasadena CA, United States)
Lin, J. G.
(Charles Stark Draper Laboratory, Inc. Cambridge, MA, United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1980
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: Conference on Decision and Control
Location: Albuquerque, NM
Start Date: December 10, 1980
End Date: December 12, 1980
Accession Number
82A25639
Funding Number(s)
CONTRACT_GRANT: NAS7-100
CONTRACT_GRANT: F30602-80-C-0096
Distribution Limits
Public
Copyright
Other

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