• DocumentCode
    2983404
  • Title

    Modeling and Control for a Six-Rotor Aerial Vehicle

  • Author

    Yin, Liangliang ; Shi, Jingkui ; Huang, Yimin

  • Author_Institution
    Res. Inst. of Flight Control, Nanjing Univ. of Aeronaut. & Astronaut., Nanjing, China
  • fYear
    2010
  • fDate
    25-27 June 2010
  • Firstpage
    1289
  • Lastpage
    1292
  • Abstract
    In this paper, we have derived the linear model of a six-rotor aerial vehicle and proposed a controller for hovering. Attitudes of the six-rotor vehicle are affected by various sources of disturbances such as wind, measurement noise and modeling uncertainty. For these reasons, we proposed a controller based on disturbance observer, which estimates and compensates disturbances. It is shown by simulation that the proposed controller effectively rejects disturbances.
  • Keywords
    aircraft control; attitude control; modelling; observers; uncertain systems; disturbance observer; hovering control; linear model; modeling uncertainty; six-rotor aerial vehicle control; six-rotor aerial vehicle modelling; Equations; Mathematical model; Noise; Observers; Propellers; Vehicle dynamics; Vehicles; disturbance observer; dynamic model; hovering control; six-rotor; unmanned aerial vehicles(UAVs);
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Electrical and Control Engineering (ICECE), 2010 International Conference on
  • Conference_Location
    Wuhan
  • Print_ISBN
    978-1-4244-6880-5
  • Type

    conf

  • DOI
    10.1109/iCECE.2010.320
  • Filename
    5630053