• DocumentCode
    3550943
  • Title

    A model reference robust control and its application to autopilot control law design

  • Author

    Wenhan, Dong ; Xiuxia, Sun ; Yan, Lin ; Qingrong, Zhang

  • Author_Institution
    Inst. of Eng., Airforce Eng. Univ., Xi´´an, China
  • fYear
    2005
  • fDate
    8-10 June 2005
  • Firstpage
    2670
  • Abstract
    In this paper, a new model reference robust control (MRRC) scheme is proposed and is applied to autopilot control law design. By using our scheme, both the tracking performance and the control effort can be improved significantly. The simulation results of a pitch-attitude-hold autopilot design show that, even with the existence of plant uncertainty, nonlinear disturbance and unmodeled dynamics, the steady-state error of the step response is no more than 0.3 percent of the final value and, the amplitude of the control signal is only about 35 percent of that by using the traditional zero-pole placement control scheme.
  • Keywords
    aircraft control; attitude control; control nonlinearities; control system synthesis; robust control; step response; uncertain systems; autopilot control law design; model reference robust control; nonlinear disturbance; pitch-attitude-hold autopilot design; plant uncertainty; steady-state error; step response; unmodeled dynamics; Aerodynamics; Algorithm design and analysis; Automatic control; Control system synthesis; Design engineering; Nonlinear control systems; Robust control; Signal design; Sun; Uncertainty;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 2005. Proceedings of the 2005
  • ISSN
    0743-1619
  • Print_ISBN
    0-7803-9098-9
  • Electronic_ISBN
    0743-1619
  • Type

    conf

  • DOI
    10.1109/ACC.2005.1470371
  • Filename
    1470371