• DocumentCode
    529743
  • Title

    2DOF control system design for maneuverability matching and gust disturbance rejection in in-flight simulator MuPAL-α

  • Author

    Ebihara, Yoshio ; Fujiwara, Yoshinori ; Hagiwara, Tomomichi ; Sato, Masayuki

  • Author_Institution
    Dept. of Electr. Eng., Kyoto Univ., Kyoto, Japan
  • fYear
    2010
  • fDate
    18-21 Aug. 2010
  • Firstpage
    524
  • Lastpage
    528
  • Abstract
    Multipurpose aviation laboratory-α (MuPAL-α) is an experimental aircraft developed by the Japan aerospace exploration agency (JAXA). Its one of the most important functions is to realize in-flight simulation, i.e., to simulate maneuverability of other aircraft via practical flight experiments. To achieve the desired maneuverability matching under model uncertainty and gust disturbance, in this paper, we construct reference feedforward type 2DOF (RFF-2DOF) control system. We will show via numerical simulation that satisfactory results are obtained by constructing RFF-2DOF control system.
  • Keywords
    aerospace simulation; control system synthesis; feedforward; numerical analysis; 2DOF control system design; Japan aerospace exploration agency; gust disturbance rejection; in-flight simulator MuPAL-a; maneuverability matching; multipurpose aviation laboratory-α; numerical simulation; practical flight experiment; reference feedforward type 2DOF control system; Adaptive control; Aircraft; Aircraft manufacture; Atmospheric modeling; Control systems; Delay; Feedforward neural networks; 2DOF control system; In-flight simulation; disturbance rejection; maneuverability matching;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    SICE Annual Conference 2010, Proceedings of
  • Conference_Location
    Taipei
  • Print_ISBN
    978-1-4244-7642-8
  • Type

    conf

  • Filename
    5603120