DocumentCode :
2210685
Title :
Adaptive backstepping with magnitude, rate, and bandwidth constraints: aircraft longitude control
Author :
Farrell, Jay ; Polycarpou, Marios M. ; Sharma, Manu
Author_Institution :
Dept. of Electr. Eng., California Univ., Riverside, CA, USA
Volume :
5
fYear :
2003
fDate :
4-6 June 2003
Firstpage :
3898
Abstract :
This article presents an adaptive backstepping approach to the longitudinal (γ, α, Q) control of an aircraft that directly accommodates magnitude, rate, and bandwidth constraints on the aircraft states and the actuator signals. The article includes design of the control law, Lyapunov analysis of the stability properties of the closed loop system, and simulation based analysis of the performance.
Keywords :
Lyapunov methods; adaptive control; aircraft control; closed loop systems; control nonlinearities; control system analysis; control system synthesis; Lyapunov analysis; actuator signals; adaptive backstepping approach; aircraft longitude control; bandwidth constraint; closed-loop system; control law; longitudinal control; magnitude constraint; rate constraint; stability properties; Actuators; Adaptive control; Aerospace control; Aircraft; Backstepping; Bandwidth; Control system analysis; Performance analysis; Programmable control; Stability analysis;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 2003. Proceedings of the 2003
ISSN :
0743-1619
Print_ISBN :
0-7803-7896-2
Type :
conf
DOI :
10.1109/ACC.2003.1240444
Filename :
1240444
Link To Document :
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