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Optimal quasi-static shape control for large aerospace antennaeIn 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.
Document ID
19840047753
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Balas, M. J.
(Rensselaer Polytechnic Institute, Troy, NY, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1984
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AAS PAPER 83-326
Report Number: AAS PAPER 83-326
Accession Number
84A30540
Funding Number(s)
CONTRACT_GRANT: NSF ECS-80-16173
CONTRACT_GRANT: NAG1-171
CONTRACT_GRANT: AF-AFOSR-83-0124
Distribution Limits
Public
Copyright
Other

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