• DocumentCode
    3289808
  • Title

    Formation control of VTOL UAVs without linear-velocity measurements

  • Author

    Abdessameud, A. ; Tayebi, A.

  • Author_Institution
    Dept. of Electr. & Comput. Eng., Univ. of Western Ontario, London, ON, Canada
  • fYear
    2010
  • fDate
    June 30 2010-July 2 2010
  • Firstpage
    2107
  • Lastpage
    2112
  • Abstract
    We address the formation control problem without linear-velocity measurements for a group of Vertical Take-Off and Landing (VTOL) Unmanned Aerial Vehicles (UAV) with a fixed and undirected communication topology. The vehicles among the team are required to track a desired reference linear-velocity and maintain a desired formation. Our control design is achieved in two main steps. First, an intermediary control input is designed for the translational dynamics, from which we extract the desired system attitude and thrust achieving the formation objective. Then, the torque input for the rotational dynamics of each vehicle is designed to drive the actual attitudes to the desired ones. To obviate the need for linear-velocity, we use instrumental auxiliary variables in each step of the control design. The stability of the overall closed loop system is rigorously established. Simulation results are provided to show the effectiveness of the proposed control scheme.
  • Keywords
    aerospace control; closed loop systems; position control; remotely operated vehicles; robot dynamics; stability; velocity control; VTOL UAV; closed loop system stability; formation control; instrumental auxiliary variable; linear-velocity measurement; rotational dynamics; translational dynamics; unmanned aerial vehicle; vertical take-off and landing; Attitude control; Communication system control; Control design; Control systems; Instruments; Topology; Torque; Unmanned aerial vehicles; Vehicle driving; Vehicle dynamics;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference (ACC), 2010
  • Conference_Location
    Baltimore, MD
  • ISSN
    0743-1619
  • Print_ISBN
    978-1-4244-7426-4
  • Type

    conf

  • DOI
    10.1109/ACC.2010.5531323
  • Filename
    5531323