DocumentCode :
815976
Title :
Control design for robust eigenstructure assignment in linear uncertain systems
Author :
Wilson, Robert F. ; Cloutier, James R. ; Yedavalli, R.K.
Author_Institution :
Armament Directorate of Wright Lab., Eglin, AFB, FL, USA
Volume :
12
Issue :
5
fYear :
1992
Firstpage :
29
Lastpage :
34
Abstract :
A generalized eigenstructure assignment procedure for designing a controller that has the best eigenstructure achievable while simultaneously maintaining stability robustness to time-varying parametric variations is presented. The approach taken is the constrained minimization of the difference between the actual and desired eigenstructure. The minimization is made subject to the constraints of the eigenstructure equation and the closed-loop Lyapunov equation. The capability of the formulation is illustrated in the design of a mode-decoupling roll-yaw autopilot for a generic, non-axisymmetrical airframe.<>
Keywords :
Lyapunov methods; aircraft control; closed loop systems; control system synthesis; eigenvalues and eigenfunctions; linear systems; minimisation; stability; aircraft control; closed-loop Lyapunov equation; constrained minimization; control system synthesis; linear uncertain systems; mode-decoupling roll-yaw autopilot; nonaxisymmetrical airframe; robust eigenstructure assignment; robustness; stability; time-varying parametric variations; Control design; Eigenvalues and eigenfunctions; Equations; Output feedback; Robust control; Robust stability; Robustness; State feedback; Time varying systems; Uncertain systems;
fLanguage :
English
Journal_Title :
Control Systems, IEEE
Publisher :
ieee
ISSN :
1066-033X
Type :
jour
DOI :
10.1109/37.158895
Filename :
158895
Link To Document :
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