• DocumentCode
    183942
  • Title

    Rotor state feedback in helicopter flight control: Robustness and fault tolerance

  • Author

    Panza, S. ; Lovera, M.

  • Author_Institution
    Dipt. di Elettron., Inf. e Bioingegneria, Politec. di Milano, Milan, Italy
  • fYear
    2014
  • fDate
    8-10 Oct. 2014
  • Firstpage
    451
  • Lastpage
    456
  • Abstract
    Helicopter flight control law design including rotor state feedback is considered and an approach based on structured H∞ control, capable of guaranteeing stability and performance robustness, is proposed. The framework also encompasses fault tolerance with respect to failures of the rotor state sensors. Simulation results comparing the proposed approach to results from the literature are presented and discussed.
  • Keywords
    H∞ control; aircraft control; control system synthesis; fault tolerant control; helicopters; robust control; rotors (mechanical); state feedback; fault tolerance; helicopter flight control law design; robustness; rotor state feedback; rotor state sensors; structured H∞ control; Bandwidth; Frequency control; Noise; Robustness; Rotors; Sensitivity; Uncertainty;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Applications (CCA), 2014 IEEE Conference on
  • Conference_Location
    Juan Les Antibes
  • Type

    conf

  • DOI
    10.1109/CCA.2014.6981387
  • Filename
    6981387
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=183942