DocumentCode :
2413618
Title :
Design of Missile Lateral Channel Controller Based on QFT
Author :
Shi, Zhen ; Wang, Fei ; Wang, Xiu-zhi
fYear :
2011
fDate :
21-23 Oct. 2011
Firstpage :
917
Lastpage :
920
Abstract :
QFT£ß(Quantitative Feedback Theory) indicators of MIMO system are derived, then QFT was applied to the MIMO missile attitude control system of lateral channel design, the lateral control system was simulated. The results show that, QFT can have the missile lateral channel robust stability, and can largely solve multi-channel decoupling problem.
Keywords :
Control systems; Indexes; MIMO; Mathematical model; Missiles; Robust stability; Sensitivity; MIMO system; QFT; decoupling; missile lateral channel control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Computational and Information Sciences (ICCIS), 2011 International Conference on
Conference_Location :
Chengdu, China
Print_ISBN :
978-1-4577-1540-2
Type :
conf
DOI :
10.1109/ICCIS.2011.128
Filename :
6086350
Link To Document :
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