• DocumentCode
    2044116
  • Title

    Redesign implementation of a nonlinear sampled-data controller for a 3-DOF model helicopter

  • Author

    Takamuku, K. ; Ishitobi, M. ; Kumada, T. ; Nishi, M. ; Kunimatsu, S.

  • Author_Institution
    Dept. of Mech. Syst. Eng., Kumamoto Univ., Kumamoto, Japan
  • fYear
    2011
  • fDate
    13-18 Sept. 2011
  • Firstpage
    1014
  • Lastpage
    1018
  • Abstract
    This paper considers redesign implementation of a nonlinear sampled-data controller for a 3-DOF model helicopter. To improve the control performance, an emulation input is modified by an additional signal. The previous method is based on the Euler approximate model, and the improvement of the control performance cannot be expected. It is shown that the improved Euler model can achieve a better control performance. Since the 3-DOF model helicopter is not decouplable via static state feedback, dynamic state feedback is introduced and a further modification to the redesign input is given.
  • Keywords
    aircraft control; control system synthesis; helicopters; nonlinear control systems; sampled data systems; state feedback; 3DOF model helicopter; Euler approximate model; control performance; dynamic state feedback; nonlinear sampled-data controller redesign; redesign input; static state feedback; Control systems; Emulation; Equations; Helicopters; Mathematical model; Numerical models; Helicopter; Nonlinear systems; Redesign; Sampled-data control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    SICE Annual Conference (SICE), 2011 Proceedings of
  • Conference_Location
    Tokyo
  • ISSN
    pending
  • Print_ISBN
    978-1-4577-0714-8
  • Type

    conf

  • Filename
    6060657