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Sub-Optimal Control of Nonlinear Flexible Space StructuresA simple yet effective method is presented for the on-line vibration control of nonlinear distributed parameter systems, with constant or time-varying properties, responding to a wide class of dynamic environments. The control procedure uses pulse generators located at selected positions throughout a given system. The degree of system oscillation near each controller determines the controller's activation time and pulse amplitude. The direct method of Liapunov is used to establish that the response of the controlled nonlinear system is Lagrange stable. Analytical and experimental studies of a wing-like plate demonstrate the feasibility, reliability, and robustness of the proposed vibration-suppression method.
Document ID
19850022877
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Dehghanyar, T. J.
(University of Southern California Los Angeles, CA, United States)
Masri, S. F.
(University of Southern California Los Angeles, CA, United States)
Miller, R. K.
(University of Southern California Los Angeles, CA, United States)
Bekey, G. A.
(University of Southern California Los Angeles, 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: JPL Proc. of the Workshop on Identification and Control of Flexible Space Struct., Vol. 2
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
85N31190
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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