DocumentCode
2896093
Title
Neural Adaptive Controller Design for Missile Systems with Input Unmodeled Dynamics
Author
Xiao, Zhi-Cai ; Jin, Yu-Qiang ; Shi, Xian-Jun
Author_Institution
Dept. of Autom. Control, Naval Aeronaut. Eng. Inst., Yantai
fYear
2006
fDate
13-16 Aug. 2006
Firstpage
3162
Lastpage
3166
Abstract
A neural adaptive inverse compensator design method was proposed for a class of nonlinear systems with input unmodeled dynamics based on RBF neural networks. The compensator was designed using two neural networks, one to estimate the input unmodeled dynamics and another to provide adaptive inverse compensation to the input unmodeled dynamics. The method relaxes some rigorous demands to unmodeled dynamics such as relative degree zero, satisfying the small gain assumption and so on. The controller was designed using backstepping control techniques. Lyapunov theory was used to derive the tuning laws for the weight vectors of the neural networks and proved that the close-loop system is gradually stable. The proposed method is applied to design the missile control systems with input unmodeled dynamics in pitch channel. The simulation results show the effectiveness of the proposed control method
Keywords
Lyapunov methods; adaptive control; closed loop systems; control system synthesis; missile control; neurocontrollers; nonlinear systems; radial basis function networks; Lyapunov theory; RBF neural networks; backstepping control techniques; close-loop system; input unmodeled dynamics; missile control system; missile system; neural adaptive controller design; neural adaptive inverse compensator design method; Adaptive control; Aerodynamics; Backstepping; Control systems; Missiles; Neural networks; Nonlinear control systems; Nonlinear dynamical systems; Nonlinear systems; Programmable control; Adaptive Inverse; Backstepping; Input unmodeled Dynamics; Nonlinear Systems;
fLanguage
English
Publisher
ieee
Conference_Titel
Machine Learning and Cybernetics, 2006 International Conference on
Conference_Location
Dalian, China
Print_ISBN
1-4244-0061-9
Type
conf
DOI
10.1109/ICMLC.2006.258411
Filename
4028610
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