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Control design variable linking for optimization of structural/control systemsA method is presented to integrate the design space of structural/control system optimization problems in the case of linear state feedback control. Conventional structural sizing variables and elements of the feedback gain matrix are both treated as strictly independent design variables in optimization by extending design variable linking concepts to the control gains. Several approximation concepts including new control design variable linking schemes are used to formulate the integrated structural/control optimization problem as a sequence of explicit nonlinear mathematical programming problems. Examples which involve a variety of behavior constraints, including constraints on dynamic stability, damped frequencies, control effort, peak transient displacement, acceleration, and control force limits, are effectively solved by using the method presented.
Document ID
19930013638
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Jin, Ik Min
(California Univ. Los Angeles, CA, United States)
Schmit, Lucien A.
(California Univ. Los Angeles, CA, United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1993
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-4493
NAS 1.26:4493
Report Number: NASA-CR-4493
Report Number: NAS 1.26:4493
Accession Number
93N22827
Funding Number(s)
PROJECT: RTOP 505-63-10-02
CONTRACT_GRANT: NSG-1490
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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