• DocumentCode
    1117931
  • Title

    Active fault tolerant control with actuation reconfiguration

  • Author

    Guangjun Liu ; Dejun Wang

  • Author_Institution
    Dept. of Aerosp. Eng., Ryerson Univ., Toronto, Ont., Canada
  • Volume
    40
  • Issue
    3
  • fYear
    2004
  • fDate
    7/1/2004 12:00:00 AM
  • Firstpage
    1110
  • Lastpage
    1117
  • Abstract
    This paper presents an integrated approach to fault detection, isolation, and fault tolerant control (FTC). In the proposed approach a constrained Kalman filter based fault detection and isolation (FDI) method (Larson et al., 2002) is modified to reduce its computation load and then applied to detect and isolate a faulty actuator or sensor. Explicit algorithms are derived to estimate the effectiveness factor of a detected faulty actuator or sensor. Furthermore, a design concept of actuation reconfiguration is proposed and implemented in the derived control scheme to restrain the workload of a faulty actuator while recovering the prefault system performance. Simulation results on an aircraft dynamic model have demonstrated the effectiveness of the proposed method.
  • Keywords
    Kalman filters; actuators; aircraft; control theory; fault location; fault tolerance; sensors; Kalman filter; active control; actuation reconfiguration; aircraft dynamic model; computation load reduction; effectiveness factor estimation; explicit algorithms; fault detection; fault isolation; fault tolerant control; faulty actuator; faulty sensor; prefault system performance; workload restraining; Actuators; Aircraft; Control systems; Fault detection; Fault tolerance; Noise measurement; Redundancy; Sensor systems; System performance; Time measurement;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/TAES.2004.1337485
  • Filename
    1337485