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NASA NTRS · 19850022870

An Integrated Control and Minimum Mass Structural Optimization Algorithm for Large Space Structures

Abstract

A 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.

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BibTeXRIS

Messac, A., Turner, J., Soosaar, K.. 1985-04-01. An Integrated Control and Minimum Mass Structural Optimization Algorithm for Large Space Structures. https://ntrs.nasa.gov/citations/19850022870

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