DocumentCode :
2869495
Title :
Achieving maximum regions of attraction for unstable linear systems with control constraints
Author :
Barbu, Corneliu ; Cheng, J.J. ; Freeman, Randy A.
Author_Institution :
Dept. of Electr. & Comput. Eng., California Univ., Santa Barbara, CA, USA
Volume :
1
fYear :
1997
fDate :
4-6 Jun 1997
Firstpage :
848
Abstract :
For unstable linear systems with actuator magnitude constraints, we present a method for designing smooth feedback control laws which yield maximal regions of attraction. The designed feedback control law produces a closed-loop region of attraction identical to the open-loop region of asymptotic null-controllability. We apply the result to the problem of stabilizing a statically unstable aircraft in the longitudinal direction
Keywords :
aircraft control; closed loop systems; control system synthesis; controllability; feedback; linear systems; stability; actuator magnitude constraints; asymptotic null-controllability; closed-loop region of attraction; control constraints; longitudinal direction; maximum regions of attraction; open-loop region; smooth feedback control laws; statically unstable aircraft; unstable linear systems; Aerospace control; Computer science; Control systems; Design engineering; Design methodology; Feedback control; Linear feedback control systems; Linear systems; Military aircraft; State feedback;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 1997. Proceedings of the 1997
Conference_Location :
Albuquerque, NM
ISSN :
0743-1619
Print_ISBN :
0-7803-3832-4
Type :
conf
DOI :
10.1109/ACC.1997.611924
Filename :
611924
Link To Document :
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