• DocumentCode
    603444
  • Title

    Nonlinear Controllers Applied to Fixed-Wing UAV

  • Author

    Espinoza, T. ; Dzul, A. ; Garcia, Luis ; Parada, R.

  • Author_Institution
    Div. de Estudios de Posgrado e Investig., Inst. Tecnol. de la Laguna, Torreón, Mexico
  • fYear
    2012
  • fDate
    19-23 Nov. 2012
  • Firstpage
    243
  • Lastpage
    248
  • Abstract
    This article presents a comparison of controllers which have been applied to a fixed-wing UAV (Unmanned Aerial Vehicle). The comparison is realized between the following nonlinear controllers techniques: sliding modes, nested saturations and back stepping. These controllers are compared and analyzed for altitude, yaw and roll by using simulation tests.
  • Keywords
    aerospace components; autonomous aerial vehicles; nonlinear control systems; backstepping; fixed wing UAV; nested saturation; nonlinear controller technique; sliding mode controller; unmanned aerial vehicle; backstepping control; fixed-wing UAV; nested saturations control; sliding modes control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Electronics, Robotics and Automotive Mechanics Conference (CERMA), 2012 IEEE Ninth
  • Conference_Location
    Cuernavaca
  • Print_ISBN
    978-1-4673-5096-9
  • Type

    conf

  • DOI
    10.1109/CERMA.2012.46
  • Filename
    6524585
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=603444