• DocumentCode
    3208925
  • Title

    The Switch Time Simulation of a Kind of Jet Element and its Effect on Control Precision

  • Author

    Ma, Wuju ; Yao, Xiaoxian ; Cheng, Jianwei

  • Author_Institution
    Sch. of Aerosp. Sci., Beijing Inst. of Technol., Beijing, China
  • Volume
    3
  • fYear
    2010
  • fDate
    11-12 May 2010
  • Firstpage
    1013
  • Lastpage
    1016
  • Abstract
    Rocket missile is an important weapon for saturation attack, which exist the problem of the precision. In order to improve the bad precision, the facility control is added. Jet element is the key actuating mechanism of the attitude control for rocket missile. The switch time of jet element is critical for control precision, in this paper the switch time is simulated and its effect on control precision is discussed. The right time when the control system produces control signal is given. Finally, the simulation of trajectory shows that trajectory correction with jet element in side direction is feasible.
  • Keywords
    attitude control; jets; missile control; position control; rockets; actuating mechanism; attitude control; control signal; jet element; precision control; rocket missile; saturation attack; switch time simulation; trajectory correction; Computational modeling; Control systems; Equations; Force control; Missiles; Plugs; Rockets; Spinning; Switches; Testing; Jet element; simulation and test; the switch time;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Intelligent Computation Technology and Automation (ICICTA), 2010 International Conference on
  • Conference_Location
    Changsha
  • Print_ISBN
    978-1-4244-7279-6
  • Electronic_ISBN
    978-1-4244-7280-2
  • Type

    conf

  • DOI
    10.1109/ICICTA.2010.204
  • Filename
    5523525