Research on Fire Algorithm of Pulse Thrusters for Interceptor Missile

摘要：

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.

作者: Yongxin Yin Zhongming Ou Wen Shi

作者单位: Doctor,Engineer at China Academy of Aerospace Aerodynamics,Beijing,China.Research interests include Researcher at China Academy of Aerospace Aerodynamics,Beijing,China.Research interests include fligh Researcher at China Academy of Aerospace Aerodynamics,Beijing,China.Research interests include fligh

会议类型: 国际会议

会议名称: The 3rd International Symposium on Systems and Control in Aeronautics and Astronautics(第三届航空航天系统与控制国际会议 ISSCAA 2010)

会议地点: 哈尔滨

会议语种:英文

页码: 1015-1018

在线出版日期: 2010-01-08（万方平台首次上网日期，不代表论文的发表时间）