• DocumentCode
    66754
  • Title

    Adaptive neural observer-based backstepping fault tolerant control for near space vehicle under control effector damage

  • Author

    Bin Jiang ; Dezhi Xu ; Peng Shi ; Cheng Chew Lim

  • Author_Institution
    Coll. of Autom. Eng., Nanjing Univ. of Aeronaut. & Astronaut., Nanjing, China
  • Volume
    8
  • Issue
    9
  • fYear
    2014
  • fDate
    June 12 2014
  • Firstpage
    658
  • Lastpage
    666
  • Abstract
    In this study, a theoretical framework for reconfigurable flight control is developed and applied to near space vehicle (NSV) attitude dynamics. First, NSV reentry mode is described. Second, an adaptive neural network observer is proposed, which ensures asymptotic convergence of the state observer error to zero under control effector damage and uncertainty. Next, a reconfigurable command-filter backstepping controller is designed based on the adaptive neural network observer. The authors focus is on the accommodation of the control effector damage, uncertainty and resulting disturbances. It is shown that the presented new control design results in asymptotic convergence of the attitude tracking error to zero. Finally, simulation results are given to demonstrate the effectiveness and potential of the proposed fault tolerant control scheme.
  • Keywords
    asymptotic stability; attitude control; control system synthesis; convergence; fault tolerant control; matrix algebra; observers; space vehicles; NSV; adaptive neural network observer; asymptotic convergence; attitude tracking error; backstepping fault tolerant control; control effector damage; near space vehicle attitude dynamics; reconfigurable command-filter backstepping controller design; reconfigurable flight control; state observer error;
  • fLanguage
    English
  • Journal_Title
    Control Theory & Applications, IET
  • Publisher
    iet
  • ISSN
    1751-8644
  • Type

    jour

  • DOI
    10.1049/iet-cta.2013.0404
  • Filename
    6842518