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
Link To Document :
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