• 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