• DocumentCode
    1752679
  • Title

    Modeling and Simulation of Endo-atmospheric Mass Moment Control Interceptor

  • Author

    Wang, Zhongkui ; Deng, Zongquan

  • Author_Institution
    Res. Center of Space Navigation Mechanism & Control, Harbin Inst. of Technol.
  • Volume
    1
  • fYear
    0
  • fDate
    0-0 0
  • Firstpage
    1843
  • Lastpage
    1847
  • Abstract
    In order to research endo-atmospheric mass moment control interceptor with three moving mass actuators, dynamics equations of this system are derived in detail. The dynamics model with nine degrees-of-freedom is presented. Then the integrated simulation is performed using SIMULINK without neglecting any control parameters. The important factors of influencing the angle-of-attack and angle-of-sideslip are found and the influence of negligible parameters to the system error is analyzed. Simulation results validate the feasibility of the mass moment control technique; and this will provide the basis for simplifying equations and the design of control system and moving mass actuators
  • Keywords
    actuators; aerospace control; control system analysis computing; control system synthesis; vehicle dynamics; control system design; dynamics equations; dynamics model; endo-atmospheric mass moment control interceptor; integrated simulation; moving mass actuators; Actuators; Automation; Control system synthesis; Control systems; Equations; Error analysis; Intelligent control; Navigation; Space technology; Weight control; mass moment interceptor; modeling; simulation;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Intelligent Control and Automation, 2006. WCICA 2006. The Sixth World Congress on
  • Conference_Location
    Dalian
  • Print_ISBN
    1-4244-0332-4
  • Type

    conf

  • DOI
    10.1109/WCICA.2006.1712673
  • Filename
    1712673