DocumentCode :
2841172
Title :
Robust adaptive controller design for missile with three-tunnel input unmodeled dynamics and uncertainties
Author :
Hu, Yunan ; Li, Jing
Author_Institution :
Dept. of Control Eng., Naval Aeronaut. Eng. Inst. Acad., Yantai, China
fYear :
2010
fDate :
26-28 May 2010
Firstpage :
4015
Lastpage :
4020
Abstract :
For a missile system with both input unmodeled dynamics and uncertainties, a robust adaptive controller based on RBF neural networks and backstepping technique is proposed. Two RBF neural networks are firstly designed to approximate the input unmodeled dynamics and its inversion. By introducing adaptive control technique, uncertainties are estimated by adaptive law. Then, adaptive tuning law of weight matrices and uncertain parameters are designed using Lyapunov stability theory based backstepping technique. The developed control scheme guarantees the global stability of the close-loop adaptive systems. Finally, 6DOF simulation results of missile are given to validate the correctness of the control scheme.
Keywords :
Lyapunov methods; adaptive control; closed loop systems; missile control; neurocontrollers; radial basis function networks; robust control; uncertain systems; Lyapunov stability theory; RBF neural networks; adaptive tuning law; backstepping technique; close-loop adaptive systems; missile system; robust adaptive controller design; three-tunnel input unmodeled dynamics; uncertain parameters; Adaptive control; Backstepping; Control systems; Lyapunov method; Missiles; Neural networks; Programmable control; Robust control; Stability; Uncertainty; Backstepping; Input Unmodeled Dynamics; RBF Neural Networks; Uncertainties;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control and Decision Conference (CCDC), 2010 Chinese
Conference_Location :
Xuzhou
Print_ISBN :
978-1-4244-5181-4
Electronic_ISBN :
978-1-4244-5182-1
Type :
conf
DOI :
10.1109/CCDC.2010.5498435
Filename :
5498435
Link To Document :
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