• DocumentCode
    1558912
  • Title

    Integrated active fault-tolerant control using IMM approach

  • Author

    Zhang, Youmin ; Jiang, Jin

  • Author_Institution
    Dept. of Electr. & Comput. Eng., Univ. of Western Ontario, London, Ont., Canada
  • Volume
    37
  • Issue
    4
  • fYear
    2001
  • fDate
    10/1/2001 12:00:00 AM
  • Firstpage
    1221
  • Lastpage
    1235
  • Abstract
    An integrated fault detection, diagnosis, and reconfigurable control scheme based on interacting multiple model (IMM) approach is proposed. Fault detection and diagnosis (FDD) is carried out using an IMM estimator. An eigenstructure assignment (EA) technique is used for reconfigurable feedback control law design. To achieve steady-state tracking, reconfigurable feedforward controllers are also synthesized using input weighting approach. The developed scheme can deal with not only actuator and sensor faults, but also failures in, system components. To achieve fast and reliable fault detection, diagnosis, and controller reconfiguration, new fault diagnosis and controller reconfiguration mechanisms have been developed by a suitable combination of the information provided by the mode probabilities from the IMM algorithm and an index related to the closed-loop system performance. The proposed approach is evaluated using an aircraft example, and excellent results have been obtained
  • Keywords
    adaptive control; aircraft control; closed loop systems; control system synthesis; eigenstructure assignment; fault diagnosis; fault tolerance; feedforward; hidden Markov models; linear quadratic control; probability; robust control; state estimation; state feedback; Kalman filter; LQR-based control design; actuator faults; aircraft fault detection; closed-loop system performance; closed-loop system stability; eigenstructure assignment; fast reliable fault detection; fault detection and diagnosis; finite-state Markov chain; input weighting approach; integrated active fault-tolerant control; interacting multiple model approach; mode probabilities; reconfigurable feedback control law design; reconfigurable feedforward controllers; robustness; sensor faults; state estimation; steady-state tracking; Actuators; Control system synthesis; Control systems; Fault detection; Fault diagnosis; Fault tolerance; Feedback control; Sensor systems; Steady-state; System performance;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/7.976961
  • Filename
    976961