• DocumentCode
    2657826
  • Title

    A differential flatness approach for rotorcraft fault detection

  • Author

    Nan, Zhang ; Antoine, Drouin ; Andrei, Doncescu ; Félixo, Mora-Camin

  • Author_Institution
    Air Transp. Dept., ENAC, Toulouse
  • fYear
    2008
  • fDate
    16-18 July 2008
  • Firstpage
    237
  • Lastpage
    241
  • Abstract
    The purpose of this communication is to investigate the usefulness of the differential flatness theory of a non linear system such as a four rotor aircraft to design an efficient fault detection scheme. The flight dynamics equations of a four rotor aircraft as well as the dynamics of the engines controlling the rotors are introduced. Then the differential flatness of the rotorcraft flight dynamics is displayed and finally a fault detection scheme, based on the differential flatness property, is proposed.
  • Keywords
    aerospace engines; fault diagnosis; helicopters; vehicle dynamics; differential flatness approach; differential flatness theory; engine dynamics; fault detection scheme; flight dynamics equations; nonlinear system; rotorcraft fault detection; Aerodynamics; Air transportation; Aircraft propulsion; Clocks; Engines; Equations; Fault detection; Linear systems; Rotors; Sliding mode control; Differential flatness; Fault detection; Rotorcraft flight mechanics;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Conference, 2008. CCC 2008. 27th Chinese
  • Conference_Location
    Kunming
  • Print_ISBN
    978-7-900719-70-6
  • Electronic_ISBN
    978-7-900719-70-6
  • Type

    conf

  • DOI
    10.1109/CHICC.2008.4605023
  • Filename
    4605023
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=2657826