• DocumentCode
    646229
  • Title

    Quadrotors flight formation control using a leader-follower approach

  • Author

    Mercado, D.A. ; Castro, R. ; Lozano, Rogelio

  • Author_Institution
    Dept. of Electr. Eng., CINVESTAV-IPN, Mexico City, Mexico
  • fYear
    2013
  • fDate
    17-19 July 2013
  • Firstpage
    3858
  • Lastpage
    3863
  • Abstract
    In this paper it is presented a control strategy to solve the trajectory tracking and flight formation problem, in horizontal plane, of multiple unmanned aerial vehicles (UAVs) kind quadrotor, by means of a leader-follower scheme. Time scale separation of the translational and rotational quadrotor dynamics is used to achieve trajectory tracking. A sliding mode controller is proposed for the translational dynamic and provides the desired orientation for the UAV, which is controlled by a linear PD control. Finally, from the formation error dynamics, a sliding mode control is used by the follower to preserve the formation with respect to a leader. Experimental results, using a virtual leader and a follower in formation, are shown to evaluate the proposed control law.
  • Keywords
    PD control; aircraft control; autonomous aerial vehicles; helicopters; linear systems; variable structure systems; vehicle dynamics; control law; flight formation problem; formation error dynamics; horizontal plane; leader-follower approach; linear PD control; multiple unmanned aerial vehicles; quadrotor flight formation control; rotational quadrotor dynamics; sliding mode controller; time scale separation; trajectory tracking; translational quadrotor dynamics; Attitude control; Equations; Lead; Trajectory; Uncertainty; Vectors; Vehicle dynamics;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Conference (ECC), 2013 European
  • Conference_Location
    Zurich
  • Type

    conf

  • Filename
    6669637