DocumentCode
2476406
Title
Adaptive fuzzy control of bank-to-turn missiles
Author
Lin, Chuan-Kai ; Wang, Sheng-De
Author_Institution
Dept. of Electr. Eng., Nat. Taiwan Univ., Taipei, Taiwan
Volume
1
fYear
1996
fDate
5-10 Aug 1996
Firstpage
596
Abstract
An adaptive fuzzy autopilot is developed for bank-to-turn (BTT) missiles. The BTT missile is a complex multi-input and multi-output (MIMO) system which has a nonminimum phase phenomenon. Fuzzy control is suitable for such a system since BTT missiles can be seen as an uncertain system with unmodeled dynamics. One feature of the proposed autopilot is to incorporate the terminal attractor controller into the autopilot to speed up the convergence rate. The stability analysis shows that the states and tracking errors of the BTT missile are uniformly bounded. Two simulation examples demonstrate the effectiveness of the proposed autopilot. The first example is to present the significant contribution of the terminal attractor controller to the convergence rate. Another simulation result is illustrated in our scenarios and shows the superior tracking performance under various flight conditions
Keywords
MIMO systems; adaptive control; fuzzy control; missile control; stability; tracking; uncertain systems; adaptive fuzzy autopilot; adaptive fuzzy control; bank-to-turn missiles; convergence rate; multi-input multi-output system; nonminimum phase phenomenon; simulation; stability analysis; superior tracking performance; terminal attractor controller; tracking errors; uncertain system; unmodeled dynamics; Acceleration; Adaptive control; Aerodynamics; Aerospace simulation; Aircraft; Convergence; Fuzzy control; Missiles; Optimal control; Programmable control;
fLanguage
English
Publisher
ieee
Conference_Titel
Industrial Electronics, Control, and Instrumentation, 1996., Proceedings of the 1996 IEEE IECON 22nd International Conference on
Conference_Location
Taipei
Print_ISBN
0-7803-2775-6
Type
conf
DOI
10.1109/IECON.1996.571023
Filename
571023
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