• DocumentCode
    581603
  • Title

    Nonlinear backstepping control of reentry warhead with hybrid actuators

  • Author

    Wang Zhen ; Wu Zhong

  • Author_Institution
    Sch. of Instrum. Sci. & Opto-Electron. Eng., Beijing Univ. of Aeronaut. & Astronaut., Beijing, China
  • fYear
    2012
  • fDate
    25-27 July 2012
  • Firstpage
    557
  • Lastpage
    561
  • Abstract
    A novel set of hybrid actuators with single control moment gyoscopes(SGCMGs) and moving masses are proposed to control a reentry warhead attitude, Since the hybrid actuators are both mounted inside the warhead directly, the ablation of them can be prevented and the aerodynamic shape can be preserved. Considering of the nonlinear and strong coupling characteristic of the reentry warhead dynamic model, A nonlinear attitude control system is designed based on backstepping method which has structured and systematic advantages. This controller has strong robustness, can achieved the two-loop control of the warhead attitude angular velocity and attitude angle. Simulation results demonstrate that the attitude controller has a high control precision and is effective.
  • Keywords
    actuators; aerodynamics; aircraft control; angular velocity control; attitude control; explosives; gyroscopes; military aircraft; nonlinear control systems; vehicle dynamics; SGCMG; ablation; aerodynamic shape; backstepping method; hybrid actuators; moving masses; nonlinear attitude control system; nonlinear backstepping control; nonlinear coupling characteristic; reentry warhead attitude control; reentry warhead dynamic model; single control moment gyoscopes; strong coupling characteristic; two-loop warhead attitude angle control; two-loop warhead attitude angular velocity control; Actuators; Aerodynamics; Attitude control; Backstepping; Educational institutions; Electronic mail; Vehicle dynamics; Backstepping Control; Control moment gyroscopes; Moving Mass; Nonlinear; Reentry warhead;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Conference (CCC), 2012 31st Chinese
  • Conference_Location
    Hefei
  • ISSN
    1934-1768
  • Print_ISBN
    978-1-4673-2581-3
  • Type

    conf

  • Filename
    6389991