• DocumentCode
    3158345
  • Title

    Linear model of a powered paraglider and observer design

  • Author

    Watanabe, Masahito ; Ochi, Yoshimasa

  • Author_Institution
    Dept. of Aerosp. Eng., Nat. Defense Acad., Yokosuka
  • fYear
    2008
  • fDate
    20-22 Aug. 2008
  • Firstpage
    2135
  • Lastpage
    2141
  • Abstract
    From analysis of a nonlinear model of a powered paraglider (PPG), it has been found that there exists poor damping of attitude oscillation similar to that of a pendulum due to wind disturbance. Hence, a state feedback control system with an observer of state variables and wind disturbance is necessary to improve the damping characteristics to take a picture of a ground circumstance clearly. This study presents analysis results such as controllability, observability, etc. of a linear model of the PPG, which is linearized from a nonlinear model. Furthermore, an outline of a state feedback system with a Kalman filter designed using the linear model is described.
  • Keywords
    Kalman filters; attitude control; controllability; damping; linear systems; nonlinear control systems; observers; state feedback; Kalman filter; attitude oscillation; damping characteristics; linear model; nonlinear model; observer design; pendulum; powered paraglider; state feedback control system; wind disturbance; Attitude control; Control systems; Controllability; Damping; Electronic mail; Nonlinear equations; Observability; Payloads; Power system modeling; State feedback; UAV; linear model; observer; parafoil;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    SICE Annual Conference, 2008
  • Conference_Location
    Tokyo
  • Print_ISBN
    978-4-907764-30-2
  • Electronic_ISBN
    978-4-907764-29-6
  • Type

    conf

  • DOI
    10.1109/SICE.2008.4655016
  • Filename
    4655016