• DocumentCode
    428643
  • Title

    Fault diagnosis in satellites using H estimators

  • Author

    Grenaille, S. ; Henry, D. ; Zolghadri, A.

  • Author_Institution
    Laboratoire d´´Automatique, Bordeaux I Univ., Talence, France
  • Volume
    6
  • fYear
    2004
  • fDate
    10-13 Oct. 2004
  • Firstpage
    5195
  • Abstract
    A model-based approach for on-line fault diagnosis in satellite is presented in this paper. The satellite studied is named MICROSCOPE. MICROSCOPE is a micro satellite under development at CNES (Centre National d´Etudes Spatiales, France). Its attitude and linear acceleration are controlled by 12 thrusters. The class of faults to be diagnosed is the thruster´s faults occurring when a thruster blocks itself or closes itself during operating. The method used to tackle the problem is based on H fault estimations techniques. The solution involves linear matrix inequalities (LMI) optimization techniques. Simulation results illustrate the potential of the method.
  • Keywords
    H optimisation; artificial satellites; computerised monitoring; fault diagnosis; linear matrix inequalities; H fault estimations technique; MICROSCOPE micro satellite; fault sensitivity; linear matrix inequalities optimization technique; model-based approach; online fault diagnosis; thruster failure; Acceleration; Actuators; Attitude control; Fault detection; Fault diagnosis; Linear matrix inequalities; Microscopy; Monitoring; Robustness; Satellites;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Systems, Man and Cybernetics, 2004 IEEE International Conference on
  • ISSN
    1062-922X
  • Print_ISBN
    0-7803-8566-7
  • Type

    conf

  • DOI
    10.1109/ICSMC.2004.1401019
  • Filename
    1401019