DocumentCode
1585374
Title
Design of fuzzy sliding mode controller for supersonic anti-ship missile
Author
Zhang, Yifei ; Deng, Fanglin ; Shi, Xusheng
Author_Institution
Dept. of Autom., The Second Artillery Eng. Acad., Xi´´an, China
Volume
6
fYear
2004
Firstpage
5402
Abstract
Supersonic anti-ship missile flies with the special trajectory that initially cruises at high altitude, and cruises at low altitude at the end of its trajectory. As the difference of aerodynamic parameters between high altitude and low altitude is great, the missiles´ control performance must be very good. Sliding mode control can strengthen system´s robustness and sensitivity, so it is appropriate to control missile´s flight trajectory. But the chattering caused by SMC may badly affect system´s stabilization. To overcome the shortcoming, a fuzzy sliding mode controller combined fuzzy control with SMC was designed. Not only the controller keeps good robustness and sensitivity, but also it can efficiently reduce the chattering. Simulation results show that the method is effective.
Keywords
control system synthesis; fuzzy control; missile control; position control; stability; variable structure systems; fuzzy control; missile control; sliding mode controller; supersonic antiship missile; Aerodynamics; Control systems; Design engineering; Fuzzy control; Missiles; Robust control; Sliding mode control;
fLanguage
English
Publisher
ieee
Conference_Titel
Intelligent Control and Automation, 2004. WCICA 2004. Fifth World Congress on
Print_ISBN
0-7803-8273-0
Type
conf
DOI
10.1109/WCICA.2004.1343760
Filename
1343760
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