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Optimization of the structural and control system for LSS with reduced-order modelThe objective is the simultaneous design of the structural and control system for space structures. The minimum weight of the structure is the objective function, and the constraints are placed on the closed loop distribution of the frequencies and the damping parameters. The controls approach used is linear quadratic regulator with constant feedback. A reduced-order control system is used. The effect of uncontrolled modes is taken into consideration by the model error sensitivity suppression (MESS) technique which modified the weighting parameters for the control forces. For illustration, an ACOSS-FOUR structure is designed for a different number of controlled modes with specified values for the closed loop damping parameters and frequencies. The dynamic response of the optimum designs for an initial disturbance is compared.
Document ID
19900011759
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Khot, N. S.
(Air Force Wright Aeronautical Labs. Wright-Patterson AFB, OH, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1989
Publication Information
Publication: NASA, Langley Research Center, NASA(DOD Controls-Structures Interaction Technology 1989
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
90N21075
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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