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