• DocumentCode
    183532
  • Title

    Using Linear Model Predictive Control via Feedback Linearization for dynamic encirclement

  • Author

    Hafez, A.T. ; Iskandarani, M. ; Givigi, Sidney N. ; Yousefi, Siamak ; Rabbath, C.A. ; Beaulieu, A.

  • Author_Institution
    Dept. of Electr. & Comput. Eng., Queens Univ., Kingston, ON, Canada
  • fYear
    2014
  • fDate
    4-6 June 2014
  • Firstpage
    3868
  • Lastpage
    3873
  • Abstract
    An Unmanned Aerial Vehicle (UAV) team formed from two or more UAVs is used in the autonomous encirclement of a stationary target in simulation. The encirclement tactic is defined as the situation in which a target is surrounded by a UAV team in formation. This tactic can be employed by a team of UAVs to neutralize a target by restricting its movement. A combination of Linear Model Predictive Control (LMPC) and Feedback Linearization (FL) is implemented on a team of UAVs in order to accomplish dynamic encirclement. The linear plant, representing each UAV, is found through System Identification then linearized using an FL technique. The contributions of this paper lay in the application of LMPC and FL to the problem of encirclement using an autonomous team of UAVs in simulation.
  • Keywords
    autonomous aerial vehicles; feedback; linearisation techniques; mobile robots; predictive control; robot dynamics; FL technique; LMPC; UAV team; autonomous encirclement; dynamic encirclement; encirclement tactic; feedback linearization; linear model predictive control; linear plant; stationary target; system identification; unmanned aerial vehicle team; Aerodynamics; Angular velocity; Equations; Mathematical model; Vectors; Vehicle dynamics; Vehicles; Feedback Linearization; Linear Model Predictive Control; Unmanned Aerial Vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference (ACC), 2014
  • Conference_Location
    Portland, OR
  • ISSN
    0743-1619
  • Print_ISBN
    978-1-4799-3272-6
  • Type

    conf

  • DOI
    10.1109/ACC.2014.6858619
  • Filename
    6858619