DocumentCode
438983
Title
Adaptive fuzzy sliding-mode controller for BTT missile
Author
Xu, Yuru ; Yu, Jinyong ; Yuan, Yuman ; Gu, Wenjin
Author_Institution
Dept. of Autom. Control, Naval Aeronaut. Eng. Inst., Yantai, China
Volume
2
fYear
2004
fDate
6-9 Dec. 2004
Firstpage
1222
Abstract
In this paper, a novel adaptive fuzzy sliding mode controller for BTT missile is proposed, which incorporates the auto-tuning fuzzy logic system to sliding-mode control, the influence of the uncertainty of parameters can be alleviated. Besides, Lyapunov stability theorem is used to prove the stability of the system and the adaptive laws are deduced which possess the characteristics of sliding-mode control. Finally, the correctness and effectiveness of the method have been verified by simulation using nonlinear overload model of pitch channel of some BTT missile.
Keywords
Lyapunov methods; adaptive control; fuzzy control; fuzzy logic; missile control; variable structure systems; BTT missile; Lyapunov stability; adaptive fuzzy sliding-mode control; auto-tuning fuzzy logic system; nonlinear overload model; pitch channel; Adaptive control; Control systems; Fuzzy control; Fuzzy logic; Fuzzy systems; Lyapunov method; Missiles; Programmable control; Sliding mode control; Uncertainty;
fLanguage
English
Publisher
ieee
Conference_Titel
Control, Automation, Robotics and Vision Conference, 2004. ICARCV 2004 8th
Print_ISBN
0-7803-8653-1
Type
conf
DOI
10.1109/ICARCV.2004.1469019
Filename
1469019
Link To Document