DocumentCode
3042901
Title
Research on fire algorithm of pulse thrusters for interceptor missile
Author
Yin, Yongxin ; Ou, Zhongming ; Shi, Wen
Author_Institution
China Acad. of Aerosp. Aerodynamics, Beijing, China
fYear
2010
fDate
8-10 June 2010
Firstpage
1005
Lastpage
1008
Abstract
In order to ensure the control precision of lateral thrust for interceptor missile, a new fire algorithm of pulse thrusters is presented. With a view to defect of lateral thrust from spinning interceptor missile, a method to search fire direction and fire quantity of pulse thrusters is presented. And improved genetic algorithm is given. In this improved genetic algorithm, the genetic operation is amended to overcome the local optimization in simple genetic algorithm. According to an improved genetic algorithm, the fire quantity of pulse thrusters is optimized, and the track error of fire command is compensated to ensure the control precision of lateral thrust. Simulation results show that this fire algorithm can implement efficiently control mission of lateral thrust for interceptor missile as well as preferable performance.
Keywords
genetic algorithms; missile control; control mission; control precision; fire algorithm; fire command; fire direction; fire quantity; genetic algorithm; lateral thrust; pulse thrusters; spinning interceptor missile; track error; Accuracy; Fires; Firing; Force; Force control; Genetics; Missiles;
fLanguage
English
Publisher
ieee
Conference_Titel
Systems and Control in Aeronautics and Astronautics (ISSCAA), 2010 3rd International Symposium on
Conference_Location
Harbin
Print_ISBN
978-1-4244-6043-4
Electronic_ISBN
978-1-4244-7505-6
Type
conf
DOI
10.1109/ISSCAA.2010.5633143
Filename
5633143
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