• DocumentCode
    3153779
  • Title

    Research on Control Method for Lateral Thrust Based on Interceptor in Aerosphere

  • Author

    Yin, Yongxin ; Yang, Ming ; Wang, Zicai

  • Author_Institution
    Control & Simulation Center Harbin
  • Volume
    1
  • fYear
    2006
  • fDate
    4-6 Oct. 2006
  • Firstpage
    713
  • Lastpage
    716
  • Abstract
    A method to control the lateral thrust is presented for combined control interceptor in aerosphere. The control command of the interceptor is divided into two commands: command of aerodynamic force and command of lateral thrust. A lateral thrust subsystem is constituted, lateral thrust from the pulse motor is presented, and detailed method to control the lateral thrust is designed. This method is useful to control the interceptor and is convenient for practical project. The simulation results show that this method tracks control command efficiently and accurately, economizes the quantity of pulse motors, and has satisfactory control precision, which shows the availability and advantage
  • Keywords
    aerodynamics; aerospace control; stepping motors; aerodynamic force; aerosphere; control interceptor; lateral thrust; pulse motor; switch control; Aerodynamics; Computational modeling; Control systems; Delay; Design methodology; Force control; Switches; Systems engineering and theory; Target tracking; Weight control; combined control; hybrid system; switch control; track command;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Computational Engineering in Systems Applications, IMACS Multiconference on
  • Conference_Location
    Beijing
  • Print_ISBN
    7-302-13922-9
  • Electronic_ISBN
    7-900718-14-1
  • Type

    conf

  • DOI
    10.1109/CESA.2006.4281745
  • Filename
    4281745