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An Integrated Control and Minimum Mass Structural Optimization Algorithm for Large Space StructuresA new approach is discussed for solving dual structural control optimization problems for high-order flexible space structures, where reduced-order structural models are employed and minimum mass designs are sought. For a given initial structural design, a quadratic control cost is minimized subject to a constant-mass constraint. The sensitivity of the optimal control cost with respect to the structural design variables is then determined and used to obtain successive structural redesigns, using a constrained gradient optimization algorithm. This process is repeated until the constrained control cost sensitivity becomes negligible. The minimum mass design is obtained by solving a sequence of neighboring optimal constant mass designs, where the sequence of optimal performance indices has a minimum at the optimal minimum mass design. A numerical example is presented which demonstrates that this new approach effectively addresses the problem of dual optimization for potentially very high-order structures.
Document ID
19850022870
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Messac, A.
(Draper (Charles Stark) Lab., Inc. Cambridge, MA, United States)
Turner, J.
(Cambridge Research Belmont, Mass., United States)
Soosaar, K.
(Cambridge Research Belmont, Mass., 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
85N31183
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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