• DocumentCode
    2241001
  • Title

    Adaptive backstepping trajectory tracking controller for a small-scaled helicopter

  • Author

    Zou, Yao ; Huo, Wei

  • Author_Institution
    The Seventh Research Division, Science and Technology on Aircraft Control Laboratory, Beihang University, Beijing 100190, P.R. China
  • fYear
    2015
  • fDate
    28-30 July 2015
  • Firstpage
    737
  • Lastpage
    742
  • Abstract
    An adaptive backstepping controller is proposed to achieve the trajectory tracking for a small-scaled helicopter. The helicopter model is first decomposed into a cascade structure between the position and attitude loops with uncertain dynamics. The backstepping technique is introduced to exploit the controller based on the decomposed model and the upper bounds of the unmodeled dynamics are compensated with the hyperbolic tangent function. The controller introduces a dynamic auxiliary system to obviate the singularity during the derivation of the command attitude; and criteria of controller parameters are developed to guarantee the bounded tracking. In addition, command filters are employed to ease complex derivative calculations. The stability analysis proves that the proposed controller realizes the ultimately bounded tracking of the helicopter system. Simulations verify the performance of the proposed controller.
  • Keywords
    Adaptation models; Backstepping; Helicopters; Quaternions; Rotors; Trajectory; Upper bound; Backstepping; Small-scaled helicopter; Trajectory tracking;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Conference (CCC), 2015 34th Chinese
  • Conference_Location
    Hangzhou, China
  • Type

    conf

  • DOI
    10.1109/ChiCC.2015.7259727
  • Filename
    7259727