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Optimization of Controlled StructuresA formulation is presented for the coupled optimal design of a structural system and its control by defining a composite objective function as a linear combination of two components: a structural objective and a control objective. For the case when the structural objective is a function of the structural design variables only, and when the control objective is represented by the quadratic functional of the response and control energy, one can analytically express the optimal control in terms of any set of admissible structural design variables. The expression for the optimal control is used recursively in an iterative Newton-Raphson search scheme, the goal of which is to determine a corresponding optimal set of structural design variables that minimize the composite objective function. A numerical example is given to illustrate the computational procedure.
Document ID
19850022873
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Salama, M.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Hamidi, M.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Demsetz, L.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, 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
85N31186
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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