DocumentCode
337744
Title
Fixed-structure controller design for systems with actuator amplitude and rate nonlinearities
Author
Kapila, Vikram ; Haddad, Wassim M.
Author_Institution
Dept. of Mech. Aerosp. & Manuf. Eng., Polytech. Univ., Brooklyn, NY, USA
Volume
1
fYear
1998
fDate
1998
Firstpage
909
Abstract
In this paper we develop fixed-order (i.e., full- and reduced-order) dynamic output feedback compensators for systems with actuator amplitude and rate saturation constraints. The proposed design methodology employs a rate limiter as part of the controller architecture. The problem of simultaneous control amplitude and rate saturation is embedded within an optimization problem by constructing a Riccati equation whose solution guarantees closed-loop global asymptotic stability in the face of sector bounded actuator amplitude and rate nonlinearities. Application of the proposed framework is demonstrated via a numerical example
Keywords
Riccati equations; actuators; asymptotic stability; closed loop systems; control nonlinearities; control system synthesis; feedback; stability criteria; Riccati equation; actuator amplitude constraint; closed-loop global asymptotic stability; fixed-order dynamic output feedback compensators; fixed-structure controller design; full-order dynamic output feedback compensators; optimization problem; rate limiter; rate nonlinearities; rate saturation constraint; reduced-order dynamic output feedback compensators; sector bounded actuator amplitude nonlinearity; sector bounded actuator rate nonlinearity; simultaneous control amplitude; Actuators; Aerospace engineering; Control nonlinearities; Control systems; Design methodology; Force control; Military aircraft; Nonlinear control systems; Riccati equations; Stability;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 1998. Proceedings of the 37th IEEE Conference on
Conference_Location
Tampa, FL
ISSN
0191-2216
Print_ISBN
0-7803-4394-8
Type
conf
DOI
10.1109/CDC.1998.760809
Filename
760809
Link To Document