• DocumentCode
    184091
  • Title

    A sensor fault detection for aircraft using a single Kalman filter and hidden Markov models

  • Author

    Rudin, Konrad ; Ducard, Guillaume J. J. ; Siegwart, Roland Y.

  • Author_Institution
    Autonomous Syst. Lab. (ASL), Zürich, Switzerland
  • fYear
    2014
  • fDate
    8-10 Oct. 2014
  • Firstpage
    991
  • Lastpage
    996
  • Abstract
    This paper presents a new scheme for sensor fault detection and isolation. It uses a single Kalman filter and a Gaussian hidden Markov model for each of the monitored sensors. This combination is able to simultaneously detect single and multiple sensor faults, still guaranteeing optimal system state estimation. This algorithm also can run on systems with limited computational power. The efficiency of the approach is evaluated through simulation of an aircraft to detect airspeed and GPS sensor faults. The results show fast fault detection and low false-alarm rate.
  • Keywords
    Gaussian processes; Global Positioning System; Kalman filters; aircraft; autonomous aerial vehicles; fault diagnosis; hidden Markov models; sensors; state estimation; GPS sensor faults; Gaussian hidden Markov model; airspeed sensor faults; computational power; false-alarm rate; optimal system state estimation; sensor fault detection; sensor fault isolation; single Kalman filter; Covariance matrices; Fault detection; Global Positioning System; Hidden Markov models; Quaternions; Technological innovation; Vectors;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Applications (CCA), 2014 IEEE Conference on
  • Conference_Location
    Juan Les Antibes
  • Type

    conf

  • DOI
    10.1109/CCA.2014.6981464
  • Filename
    6981464