DocumentCode :
1752726
Title :
Robust Sliding Mode Control Guidance Law for Interceptor Based on Wavelet Neural Networks
Author :
Li, Da ; Wang, Qingchao
Author_Institution :
Dept. of Astronaut. Eng., Harbin Inst. of Technol.
Volume :
1
fYear :
0
fDate :
0-0 0
Firstpage :
2199
Lastpage :
2203
Abstract :
In this paper, a wavelet neural networks (WNN) sliding mode control guidance law with strong robustness is proposed for interceptor considering the dynamics of autopilot. Firstly, using the robust ability of sliding mode control to uncertainties in the control process, a typical three-dimensional sliding mode control guidance law (SMCGL) based on line-of-sight (LOS) is presented. And then wavelet neural networks are employed to predict the uncertain system dynamics on line to relax the requirement of uncertainty bound in the design of a traditional sliding mode controller. The adaptive learning algorithm of the WNN is derived from the sense of Lyapunov stability analysis. Numerical simulation results show that the dynamic behaviors of the proposed guidance law are superior to typical SMCGL in term of miss distance and obviously reduce the chattering phenomenon
Keywords :
Lyapunov methods; aerospace control; neurocontrollers; robust control; uncertain systems; variable structure systems; Lyapunov stability analysis; adaptive learning algorithm; chattering phenomenon; line-of-sight; robust sliding mode control guidance law; uncertain system dynamics; wavelet neural network; Algorithm design and analysis; Control systems; Lyapunov method; Neural networks; Numerical simulation; Process control; Robust control; Sliding mode control; Uncertain systems; Uncertainty; chattering; guidance law; sliding mode control; wavelet neural networks;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Intelligent Control and Automation, 2006. WCICA 2006. The Sixth World Congress on
Conference_Location :
Dalian
Print_ISBN :
1-4244-0332-4
Type :
conf
DOI :
10.1109/WCICA.2006.1712749
Filename :
1712749
Link To Document :
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