• DocumentCode
    2081324
  • Title

    To reduce initial control magnitude in backstepping: A continuous predictive approach

  • Author

    Hou, Mingzhe ; Duan, Guangren ; Liang, Xiaoling ; Deng, Zongquan

  • Author_Institution
    Center for Control Theory and Guidance Technology, Harbin Institute of Technology, Harbin, Heilongjiang Province, China 150001
  • fYear
    2015
  • fDate
    May 31 2015-June 3 2015
  • Firstpage
    1
  • Lastpage
    6
  • Abstract
    In this paper, a novel backstepping control algorithm is proposed by adopting the nonlinear continuous predictive approach. An optimization performance index containing the weighted tracking error and control input is introduced to obtain the actual control law. By adjusting the weighting matrix, the control magnitude in the initial stage can be reduced. In addition, when the weighting matrix imposing on input vector vanishes, the control law just coincides with the traditional backstepping control law. The proposed approach is further applied to the control of aircrafts. The simulation results show the effectiveness and advantage of our method.
  • Keywords
    Aerospace control; Aircraft; Backstepping; Closed loop systems; Nonlinear systems; Optimization; Performance analysis; aircraft control; backstepping control; continuous predictive approach; control magnitude;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Conference (ASCC), 2015 10th Asian
  • Conference_Location
    Kota Kinabalu, Malaysia
  • Type

    conf

  • DOI
    10.1109/ASCC.2015.7244374
  • Filename
    7244374