• DocumentCode
    582306
  • Title

    Adaptive Trajectory Linearization Control for a model-scaled helicopter with uncertain inertial parameters

  • Author

    Bing, Zhu ; Wei, Huo

  • Author_Institution
    Seventh Res. Div., Beihang Univ., Beijing, China
  • fYear
    2012
  • fDate
    25-27 July 2012
  • Firstpage
    4389
  • Lastpage
    4395
  • Abstract
    An adaptive approach based on Trajectory Linearization Control (TLC) is introduced to achieve the trajectory tracking of model-scaled helicopter with constant or slow time-varying model uncertainties. In the procedure of the controller designing, estimated parameters are applied to compensate for the uncertain inertial parameters (such as the mass and the inertial matrix) of the helicopter. Stability of the adaptive control system is proved in both constant and time-varying cases. Performances of the closed-loop system are verified by simulation results.
  • Keywords
    adaptive control; aircraft control; closed loop systems; control system synthesis; helicopters; linearisation techniques; stability; time-varying systems; trajectory control; uncertain systems; adaptive trajectory linearization control; closed loop system; controller design; model scaled helicopter; stability; time-varying model uncertainty; trajectory tracking; uncertain inertial parameter estimation; Adaptation models; Attitude control; Helicopters; Mathematical model; Rotors; Trajectory; Uncertainty; Trajectory linearization control; adaptive control; helicopter control; nonlinear control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Conference (CCC), 2012 31st Chinese
  • Conference_Location
    Hefei
  • ISSN
    1934-1768
  • Print_ISBN
    978-1-4673-2581-3
  • Type

    conf

  • Filename
    6390697