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