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
Link To Document :
بازگشت