DocumentCode
2392409
Title
Dual control of supersonic missiles with simplified linear model
Author
Liu, Wei ; Meng, Wanjing ; Yang, Zhiyong ; Lei, Junwei
Author_Institution
91980 Unit, Office of Equip., PLA, China
fYear
2012
fDate
19-20 May 2012
Firstpage
140
Lastpage
142
Abstract
Considering the simplified pitch channel model of supersonic missile, a novel dual control strategy is proposed. It is a kind of hybrid control method. Both the traditional PID control and the backstepping method are used. And the two methods are integrated with a dual control structure which is very skillful. Also dual control mode is a very mature method which is widely applied in process control engineering, but it is the first time to be applied in a supersonic missile.
Keywords
missile control; three-term control; PID control; backstepping method; dual control mode; dual control structure; hybrid control; process control engineering; simplified linear model; simplified pitch channel model; supersonic missiles; Adaptive systems; Backstepping; Control systems; Educational institutions; Missiles; Nonlinear systems; Time varying systems; Dual Control; Missile; Uncertainty;
fLanguage
English
Publisher
ieee
Conference_Titel
Systems and Informatics (ICSAI), 2012 International Conference on
Conference_Location
Yantai
Print_ISBN
978-1-4673-0198-5
Type
conf
DOI
10.1109/ICSAI.2012.6223303
Filename
6223303
Link To Document