DocumentCode
3162643
Title
Research on fuzzy intelligent sliding mode control of BTT missile based on T-S model
Author
Hou, Hongqing ; Liu, Gang ; Wang, Minghao ; Zhao, Pengtao
Author_Institution
9rd Dept., Second Artillery Eng. Coll., Xi´´an, China
fYear
2011
fDate
8-10 Aug. 2011
Firstpage
4236
Lastpage
4239
Abstract
Adaptive fuzzy controller based on fuzzy T-S Model is designed to the question of BTT missile Control and guidance system nonlinear model uncertainties and fast variable time characterizes in this paper. Designed sliding mode controller using feedback linearization method. T-S fuzzy model approximation for the nonlinear part of the control system. Then, the Lyapunov stability theory is used to guarantee the closed-loop stability and proved that the asymptotic stability of nonlinear control system, and derive the adaptive rules. Finally, the results of simulation demonstrate the controller achieve excellent tracking performance.
Keywords
Lyapunov methods; adaptive control; asymptotic stability; closed loop systems; control system synthesis; feedback; fuzzy control; intelligent control; linearisation techniques; missile control; nonlinear control systems; variable structure systems; BTT missile; Lyapunov stability theory; adaptive fuzzy controller; asymptotic stability; closed loop stability; designed sliding mode controller; fast variable time; feedback linearization method; fuzzy T-S model; fuzzy intelligent sliding mode control; nonlinear control system; nonlinear model uncertainties; nonlinear part approximation; Adaptation models; Fuzzy control; Mathematical model; Missiles; Sliding mode control; Adaptive Control; Bank-to-Turn Missile; Sliding Mode Control; T-S Fuzzy Control;
fLanguage
English
Publisher
ieee
Conference_Titel
Artificial Intelligence, Management Science and Electronic Commerce (AIMSEC), 2011 2nd International Conference on
Conference_Location
Deng Leng
Print_ISBN
978-1-4577-0535-9
Type
conf
DOI
10.1109/AIMSEC.2011.6010013
Filename
6010013
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