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Stiffness control of large space structuresA method of using internal force producing dual element/actuators for vibration suppression of large space structures is proposed. This technique is applied to a vibrating string as well as a low order system. Response feedback control for the vibrating string and selected modal control are used for achieving the modal damping. The actuators used in this method may be electrically powered and are suitable for structures with extremely low rigidity.
Document ID
19860048516
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chen, J.-C.
(California Institute of Technology Jet Propulsion Laboratory, Pasadena, United States)
Fanson, J. L.
(California Institute of Technology Pasadena, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1985
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
86A33254
Distribution Limits
Public
Copyright
Other

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