• DocumentCode
    1794962
  • Title

    Design of servo system robust controller for multiple launcher

  • Author

    Changjun Xia ; Jinguo Tang ; Changjin Wang

  • Author_Institution
    Dept. of Airborne Vehicle Eng., Naval Aeronaut. & Astronaut. Univ.(NAAU), Yantai, China
  • fYear
    2014
  • fDate
    8-10 Aug. 2014
  • Firstpage
    845
  • Lastpage
    849
  • Abstract
    This paper designs a robust controller to ensure that the control tracking performance of the multiple launcher servo system maintain robustness under the influence of the parameter perturbation and uncertain disturbance. First the system differential dynamic model with parameter perturbation and disturbance is established, state equation of error between the reference model and the system is deduced. Second, robust controller is designed according to the system error, the robust control system is proved to be global stable by Lyapunov theorem. Last, the paper makes simulation, the simulation result of robust controller is compared with that of PID controller, and comparison shows robust controller has better robustness than PID controller for multiple launcher servo system.
  • Keywords
    Lyapunov methods; aerospace control; control system synthesis; robust control; servomechanisms; three-term control; Lyapunov theorem; PID controller; control tracking performance; global stable; multiple launcher servo system; parameter disturbance; parameter perturbation; reference model; robust control system; servo system robust controller design; state equation; system differential dynamic model; system error; Equations; Load modeling; Mathematical model; Missiles; Robust control; Robustness; Servomotors;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Guidance, Navigation and Control Conference (CGNCC), 2014 IEEE Chinese
  • Conference_Location
    Yantai
  • Print_ISBN
    978-1-4799-4700-3
  • Type

    conf

  • DOI
    10.1109/CGNCC.2014.7007319
  • Filename
    7007319