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
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