DocumentCode :
1639766
Title :
Design for BTT Missile Controller Base on the RBF Neural Networks
Author :
Shengjie, Huang ; Zhuwei, Zhao ; Qi, Luo
Author_Institution :
Sci. & Technol. Univ., Nanjing
fYear :
2007
Firstpage :
91
Lastpage :
95
Abstract :
In this paper, adaptive RBF neural networks are present for nonlinear BTT missile controller. Considering the unknown smooth function vectors and the uncertainty of pneumatic parameter , we introduce RBF neural networks to simulate this nonlinear vectors. It overcomes some limitations of robust control. Furthurmore, a systematic backstepping design method has been used to ultimately guarantee semileptonically uniformly bounded of closed loop signals, and the output of system can converge to a small neighborhood of the actual trajectory. Finally, the simulation result is presented to demonstrate the validity of the approach.
Keywords :
closed loop systems; control system synthesis; missile control; neurocontrollers; nonlinear control systems; pneumatic systems; radial basis function networks; vectors; adaptive RBF neural networks; backstepping design method; closed loop signals; nonlinear BTT missile controller design; nonlinear vectors; pneumatic parameter uncertainty; smooth function vectors; Adaptive control; Angular velocity; Backstepping; Control systems; Missiles; Neural networks; Nonlinear control systems; Programmable control; Robust control; Uncertainty; Adaptive control; BBT missile control systems; RBF neural control; backstepping;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Conference, 2007. CCC 2007. Chinese
Conference_Location :
Hunan
Print_ISBN :
978-7-81124-055-9
Electronic_ISBN :
978-7-900719-22-5
Type :
conf
DOI :
10.1109/CHICC.2006.4346857
Filename :
4346857
Link To Document :
بازگشت