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Low-authority control synthesis for large space structuresThe control of vibrations of large space structures by distributed sensors and actuators is studied. A procedure is developed for calculating the feedback loop gains required to achieve specified amounts of damping. For moderate damping (Low Authority Control) the procedure is purely algebraic, but it can be applied iteratively when larger amounts of damping are required and is generalized for arbitrary time invariant systems.
Document ID
19830002171
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Aubrun, J. N.
(Lockheed Missiles and Space Co. Palo Alto, CA, United States)
Margulies, G.
(Lockheed Missiles and Space Co. Palo Alto, CA, United States)
Date Acquired
September 4, 2013
Publication Date
September 1, 1982
Publication Information
Publisher: NASA
Subject Category
Structural Mechanics
Report/Patent Number
NAS 1.26:3495
NASA-CR-3495
Report Number: NAS 1.26:3495
Report Number: NASA-CR-3495
Accession Number
83N10441
Funding Number(s)
CONTRACT_GRANT: NAS1-14887
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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