• DocumentCode
    3529588
  • Title

    Simultaneous low-order control of a nonlinear quadrotor model at four equilibria

  • Author

    Nanjangud, Akshay

  • Author_Institution
    Dept. of Mech. Eng., Univ. of Texas, Dallas, TX, USA
  • fYear
    2013
  • fDate
    10-13 Dec. 2013
  • Firstpage
    2914
  • Lastpage
    2919
  • Abstract
    Four equilibria of a nonlinear quadrotor model are considered as a problem for simultaneous stabilization. Linearizations at these equilibria represent the operating modes corresponding to hover, vertical translation with any constant velocity, and horizontal translations with either any constant roll angle tilt or any constant pitch angle tilt. The linearizations at hover and vertical translation give rise to linear time-invariant systems to be stabilized. Each setting of constant roll angle or pitch angle gives rise to a different linear time-invariant system to be stabilized. Any finite number of such systems are shown be simultaneously stabilizable by simple, low-order and decentralized controllers with integral-action. Synthesis procedure for such controllers is described.
  • Keywords
    autonomous aerial vehicles; control system synthesis; decentralised control; integral equations; linear systems; linearisation techniques; motion control; nonlinear control systems; rotors; stability; velocity control; constant pitch angle tilt; constant velocity; controller synthesis; decentralized controllers; finite number; four equilibria; horizontal translations; hover; integral-action; linear time-invariant systems; linearizations; low-order control; nonlinear quadrotor model; roll angle tilt; simultaneous stabilization; vertical translation; Aerodynamics; Aircraft; Backstepping; Force; Mathematical model; Military aircraft; Rotors;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Decision and Control (CDC), 2013 IEEE 52nd Annual Conference on
  • Conference_Location
    Firenze
  • ISSN
    0743-1546
  • Print_ISBN
    978-1-4673-5714-2
  • Type

    conf

  • DOI
    10.1109/CDC.2013.6760326
  • Filename
    6760326