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NASA NTRS ยท 19840047753

Optimal quasi-static shape control for large aerospace antennae

Abstract

In this paper, an on-line control approach which will adjust the steady-state shape of a large antenna arbitarily close to any achievable desired profile is proposed. The method makes use of distributed parameter system theory and allows refocusing using a limited number of control actuators and sensors. The controller gains are calculated by approximating the solution to an infinite-dimensional optimal quasi-static control problem. A very general convergence result for such quasi-static controllers is proved and applied to the antenna controller to show convergence, using any Galerkin (finite-element) approximation method.

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BibTeXRIS

Balas, M. J.. 1984-01-01. Optimal quasi-static shape control for large aerospace antennae. https://ntrs.nasa.gov/citations/19840047753

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