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)