• DocumentCode
    1587457
  • Title

    Environmental adaptive yaw control autonomous unmannedhelicopter and bifurcation of maneuvering in turning

  • Author

    Nakanishi, Hiroaki ; Kanata, Sayaka ; Sawaragi, Tetsuo

  • Author_Institution
    Yoshida Honmachi, Kyoto Univ., Kyoto, Japan
  • fYear
    2010
  • Firstpage
    1
  • Lastpage
    6
  • Abstract
    Adaptation to the environmental changes, such as wind, has very important role to improve the reliability of an autonomous unmanned helicopter. In this paper, we propose an adaptive yaw (heading) control for an autonomous helicopter. The control structure is based on a hierarchal scheme utilizing an inner yaw feedback control loop plus an outer feedback loop, which estimates the direction of the airspeed using roll angle and roll angular rate. Stable coupling in yaw and roll motion is induced by the proposed controller to improve the stabitity of the helicopter´ flight. Turning utilizing the proposed adaptive control system is discussed in particular. Results of flight experiments showed bifurcation of the helicopter´s maneuvering in turning occurs depending on the airspeed.
  • Keywords
    helicopters; mobile robots; remotely operated vehicles; state feedback; autonomous helicopter control; autonomous unmanned helicopter; control structure; environmental adaptive yaw control autonomous unmanned helicopter; feedback control loop; helicopter flight; maneuvering bifurcation; roll angle; roll angular rate; Autonomous Unmanned Helicoptera; Bifurcation of Maneuvering; Environmental Adaptive Flight Control; Turing; Yaw control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    World Automation Congress (WAC), 2010
  • Conference_Location
    Kobe
  • ISSN
    2154-4824
  • Print_ISBN
    978-1-4244-9673-0
  • Electronic_ISBN
    2154-4824
  • Type

    conf

  • Filename
    5665345