• DocumentCode
    2917672
  • Title

    Fault tolerant control of an octorotor using LPV based sliding mode control allocation

  • Author

    Alwi, Halim ; Edwards, Chris

  • Author_Institution
    Dept. of Eng., Univ. of Leicester, Leicester, UK
  • fYear
    2013
  • fDate
    17-19 June 2013
  • Firstpage
    6505
  • Lastpage
    6510
  • Abstract
    This paper presents an LPV based sliding mode fault tolerant controller for an octorotor. The scheme utilizes a combination of sliding mode methods and 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 coverage of operating conditions. The proposed scheme uses control allocation to take full advantage of the `redundant´ rotors to redistribute the control signals to the healthy rotors when faults/failures occur. Simulation results on the nonlinear model for various fault/failure scenarios show no visible difference in comparison to the nominal fault free performance.
  • Keywords
    aircraft control; autonomous aerial vehicles; fault tolerance; helicopters; mobile robots; rotors; stability; telerobotics; variable structure systems; LPV based sliding mode control allocation; UAV; baseline sliding mode controller design; control signal redistribution; fault free performance; multirotor unmanned aerial vehicle; nonlinear model; octorotor; redundant rotors; rotor fault-failure; sliding mode fault tolerant controller; stability analysis; Actuators; Equations; Fault tolerance; Mathematical model; Resource management; Rotors; Uncertainty;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference (ACC), 2013
  • Conference_Location
    Washington, DC
  • ISSN
    0743-1619
  • Print_ISBN
    978-1-4799-0177-7
  • Type

    conf

  • DOI
    10.1109/ACC.2013.6580859
  • Filename
    6580859