• DocumentCode
    2858979
  • Title

    Nonlinear aircraft modeling and controller design for target tracking

  • Author

    Rizwan, Y. ; Waslander, S.L. ; Nielsen, C.

  • Author_Institution
    Dept. of Me chanical & Mechatron. Eng., Univ. of Waterloo, Waterloo, ON, Canada
  • fYear
    2011
  • fDate
    June 29 2011-July 1 2011
  • Firstpage
    3191
  • Lastpage
    3196
  • Abstract
    In order to provide a novel perspective for videography of high speed sporting events, a highly capable trajectory tracking control methodology is developed for small scale Unmanned Aerial Vehicles (UAVs). The proposed controller combines dynamic inversion with linear tracking control using the internal model approach, and relies on a trajectory generating exosystem generated from available target training data. Three different aircraft models are presented each with increasing levels of complexity, in an effort to identify the simplest controller that yields acceptable performance. The dynamic inversion and linear tracking control laws are derived for each model, and simulation results are presented for tracking of elliptical and periodic trajectories.
  • Keywords
    aerospace robotics; aircraft control; control system synthesis; mobile robots; nonlinear control systems; periodic control; position control; remotely operated vehicles; sport; target tracking; UAV; controller design; dynamic inversion; elliptical trajectory; high speed sporting event; internal model approach; linear tracking control; nonlinear aircraft modeling; periodic trajectory; small scale unmanned aerial vehicle; target tracking; trajectory generating exosystem; trajectory tracking control; videography; Aerodynamics; Aerospace control; Aircraft; Atmospheric modeling; Mathematical model; Target tracking; Trajectory;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference (ACC), 2011
  • Conference_Location
    San Francisco, CA
  • ISSN
    0743-1619
  • Print_ISBN
    978-1-4577-0080-4
  • Type

    conf

  • DOI
    10.1109/ACC.2011.5991514
  • Filename
    5991514