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Stiffness Control of Large Space StructuresA technique for using internal force producing dual element/actuators for vibration suppression of large space structures is proposed. The method is applied to a low order system. Selective modal damping is achieved. The actuators used in this method may be electrically powered. The method is suitable for structures which are too slender or flimsy to permit the use of reaction jet-type actuators.
Document ID
19850022876
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Fanson, J. L. (California Inst. of Tech. Pasadena, United States)
Chen, J. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Caughey, T. K. (California Inst. of Tech. Pasadena, United States)
Date Acquired
August 12, 2013
Publication Date
April 1, 1985
Publication Information
Publication: Proc. of the Workshop on Identification and Control of Flexible Space Struct., Vol. 2
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
85N31189
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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IDRelationTitle19850022857Collected WorksProceedings of the Workshop on Identification and Control of Flexible Space Structures, Volume 2
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