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Approximation theory for LQG (Linear-Quadratic-Gaussian) optimal control of flexible structuresAn approximation theory is presented for the LQG (Linear-Quadratic-Gaussian) optimal control problem for flexible structures whose distributed models have bounded input and output operators. The main purpose of the theory is to guide the design of finite dimensional compensators that approximate closely the optimal compensator. The optimal LQG problem separates into an optimal linear-quadratic regulator problem and an optimal state estimation problem. The solution of the former problem lies in the solution to an infinite dimensional Riccati operator equation. The approximation scheme approximates the infinite dimensional LQG problem with a sequence of finite dimensional LQG problems defined for a sequence of finite dimensional, usually finite element or modal, approximations of the distributed model of the structure. Two Riccati matrix equations determine the solution to each approximating problem. The finite dimensional equations for numerical approximation are developed, including formulas for converting matrix control and estimator gains to their functional representation to allow comparison of gains based on different orders of approximation. Convergence of the approximating control and estimator gains and of the corresponding finite dimensional compensators is studied. Also, convergence and stability of the closed-loop systems produced with the finite dimensional compensators are discussed. The convergence theory is based on the convergence of the solutions of the finite dimensional Riccati equations to the solutions of the infinite dimensional Riccati equations. A numerical example with a flexible beam, a rotating rigid body, and a lumped mass is given.
Document ID
19890002382
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Gibson, J. S.
(California Univ. Los Angeles., United States)
Adamian, A.
(California Univ. Los Angeles., United States)
Date Acquired
September 5, 2013
Publication Date
August 1, 1988
Subject Category
Aircraft Stability And Control
Report/Patent Number
AD-A200257
NASA-CR-181705
ICASE-88-48
NAS 1.26:181705
Report Number: AD-A200257
Report Number: NASA-CR-181705
Report Number: ICASE-88-48
Report Number: NAS 1.26:181705
Accession Number
89N11753
Funding Number(s)
PROJECT: RTOP 505-90-21-01
CONTRACT_GRANT: NAS1-18107
CONTRACT_GRANT: NAS1-17070
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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