• DocumentCode
    720466
  • Title

    Quadrotor control in a wind field

  • Author

    Nguyen Khoi Tran ; Bulka, Eitan ; Nahon, Meyer

  • Author_Institution
    Dept. of Mech. Eng., McGill Univ., Montreal, QC, Canada
  • fYear
    2015
  • fDate
    9-12 June 2015
  • Firstpage
    320
  • Lastpage
    328
  • Abstract
    This paper investigates the ability of a quadrotor to maneuver in a wind field. A dynamic model of a quadrotor is presented to model its motion. The quadrotor model includes a wind effect model to quantify the effect of wind on the dynamics of a quadrotor. A proportional-integral-derivative (PID) controller is shown as a baseline controller typically used on quadrotors. A LQR controller is then shown as an alternative to a PID controller. These two controllers are compared in a simulation environment using the wind effect model and simulated wind disturbances. Both controllers are found to have similar performance in a wind field, though the LQR controller is found to be easier to tune.
  • Keywords
    aerodynamics; aircraft control; flow control; helicopters; linear quadratic control; motion control; three-term control; vehicle dynamics; wind; LQR controller; PID controller; linear quadratic regulator control; maneuver; motion modeling; proportional-integral-derivative controller; quadrotor control; quadrotor dynamic model; quadrotor model; wind disturbances; wind effect model; wind field; Atmospheric modeling; Force; Mathematical model; Predictive models; Propellers; Wind forecasting;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Unmanned Aircraft Systems (ICUAS), 2015 International Conference on
  • Conference_Location
    Denver, CO
  • Print_ISBN
    978-1-4799-6009-5
  • Type

    conf

  • DOI
    10.1109/ICUAS.2015.7152306
  • Filename
    7152306