• DocumentCode
    2255425
  • Title

    A vortex-ring-state-avoiding descending control strategy for multi-rotor UAVs

  • Author

    Chenglong, Li ; Zhou, Fang ; Jiafang, Wang ; Xiang, Zhang

  • Author_Institution
    School of Aeronautics and Astronautics, Zhejiang University, Hangzhou 310027
  • fYear
    2015
  • fDate
    28-30 July 2015
  • Firstpage
    4465
  • Lastpage
    4471
  • Abstract
    The vortex ring state (VRS) is a dangerous phenomenon that may typically arise in rotorcraft descent process. In VRS, the rotor will lose lift and get into a wobbling state. As a kind of rotorcraft, multi-rotor UAV(Unmanned Aerial Vehicle) also encounters the same problems in descending flight. So in this paper, we propose a VRS-avoiding control strategy for multi-rotor UAVs. The real phenomenon of multi-rotor in vortex ring state is described through experiments. Based on test data, a VRS alarm and recovery strategy is proposed for vertical landing. To meet the demand of rapid descending, a spiraling down control strategy is devised to make the multi-rotor avoid entering into the VRS based on Gao and Xin´s criterion. Using the developed simple model, this control strategy has been proved effective in hardware-in-loop simulation test, where larger than 4 m/s stable descending is realized.
  • Keywords
    Aerodynamics; Aerospace control; Blades; Helicopters; Mathematical model; Rotors; Multi-rotor UAV; rapid descending control; vortex ring state;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Conference (CCC), 2015 34th Chinese
  • Conference_Location
    Hangzhou, China
  • Type

    conf

  • DOI
    10.1109/ChiCC.2015.7260330
  • Filename
    7260330