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
Link To Document :
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