• DocumentCode
    661064
  • Title

    LPV sliding mode fault tolerant control of an octorotor using fixed control allocation

  • Author

    Alwi, Halim ; Edwards, Chris

  • Author_Institution
    Centre for Dynamics & Control, Univ. of Exeter, Exeter, UK
  • fYear
    2013
  • fDate
    9-11 Oct. 2013
  • Firstpage
    772
  • Lastpage
    777
  • Abstract
    This paper presents a fault tolerant control scheme for an octorotor using LPV based sliding mode control allocation. The scheme utilizes a combination of sliding mode methods and fixed control allocation in order to deal with rotor faults/failures. An LPV scheme has been used to design the baseline sliding mode controller and a stability analysis has been provided for a wide range of operating conditions. The proposed scheme takes full advantage of the `redundant´ rotors when faults/failures occur, without requiring any FDI (or any information about the faults/failures). Furthermore, the proposed scheme is simple as it does not require the baseline sliding mode controller to be reconfigured. To highlight the efficacy of the proposed scheme, simulation results on a nonlinear octorotor model for various fault/failure scenarios with gust conditions are presented.
  • Keywords
    aircraft control; control system synthesis; fault diagnosis; fault tolerant control; helicopters; nonlinear control systems; rotors (mechanical); stability; variable structure systems; LPV sliding mode fault tolerant control; fixed control allocation; gust conditions; linear parameter varying analysis; nonlinear octorotor model; octorotor; redundant rotors; rotor failures; rotor faults; sliding mode controller design; stability analysis; Uncertainty;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control and Fault-Tolerant Systems (SysTol), 2013 Conference on
  • Conference_Location
    Nice
  • Type

    conf

  • DOI
    10.1109/SysTol.2013.6693887
  • Filename
    6693887