• DocumentCode
    575180
  • Title

    Experiment of height and attitude control using monorotor unmanned aerial vehicle

  • Author

    Fujita, Shohei ; Sekiguchi, Kazuma ; Sampei, Mitsuji

  • Author_Institution
    Dept. of Mech. & Control Syst. Eng., Tokyo Inst. of Technol., Tokyo, Japan
  • fYear
    2012
  • fDate
    20-23 Aug. 2012
  • Firstpage
    1986
  • Lastpage
    1990
  • Abstract
    This paper shows the usefulness of the nonlinear controller realizing periodic motion of monorotor UAV by experiments. Monorotor UAV has no equilibrium point. So, the control target is semi-hovering; a motion that passes desired non-equilibrium point at which height and attitude stop periodically. In order to achieve this control objective, we propose discontinuous and time-varying output zeroing controller which allows zero dynamics to be controlled. The numerical simulation and experiments show the validity of suggesting controller design method.
  • Keywords
    attitude control; autonomous aerial vehicles; nonlinear control systems; numerical analysis; time-varying systems; vehicle dynamics; attitude control; control objective; controller design method; discontinuous output zeroing controller; height control; monorotor UAV; monorotor unmanned aerial vehicle; non-equilibrium point; nonlinear controller; numerical simulation; periodic motion; time-varying output zeroing controller; Aerodynamics; Attitude control; Nonlinear dynamical systems; Propulsion; Robots; Trajectory; Nonlinear Control; Periodic Motion; UAV; Underactuated System; Zero Dynamics;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    SICE Annual Conference (SICE), 2012 Proceedings of
  • Conference_Location
    Akita
  • ISSN
    pending
  • Print_ISBN
    978-1-4673-2259-1
  • Type

    conf

  • Filename
    6318338