DocumentCode :
1585907
Title :
A study of chattering avoidance in slide mode control guidance law for interceptor
Author :
Cai, Peng ; Wang, Yue ; Wang, Qingchao
Author_Institution :
Astronautics Sch., Harbin Inst. of Technol., China
Volume :
6
fYear :
2004
Firstpage :
5491
Abstract :
This paper engages to study the chattering problem in slide mode control guidance law (SMCGL). Applying the adaptive ability of slide mode control to system instability, a typical 3-D SMCGL based on line-of-sight (LOS) is presented and then developed by using fuzzy logic to smooth the signal function. Base on above study, adaptive active actor is designed to online adjust the parameters of the fuzzy rules used by above guidance law. In the numerical simulation, it is obviously that the proposed guidance law reduces the chattering phenomenon and is superior to typical SMCGL in terms of miss distance.
Keywords :
control nonlinearities; fuzzy control; fuzzy logic; missile guidance; variable structure systems; chattering avoidance; fuzzy control; fuzzy logic; slide mode control guidance law; Adaptive control; Control systems; Educational institutions; Fuzzy control; Fuzzy logic; Numerical simulation; Paper technology; Programmable control; Space technology;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Intelligent Control and Automation, 2004. WCICA 2004. Fifth World Congress on
Print_ISBN :
0-7803-8273-0
Type :
conf
DOI :
10.1109/WCICA.2004.1343783
Filename :
1343783
Link To Document :
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