• DocumentCode
    809824
  • Title

    Fault tolerant control system design with explicit consideration of performance degradation

  • Author

    Zhang, Youmin ; Jiang, Jin

  • Author_Institution
    Dept. of Electr. & Comput. Eng., Univ. of Western Ontario, London, Ont., Canada
  • Volume
    39
  • Issue
    3
  • fYear
    2003
  • fDate
    7/1/2003 12:00:00 AM
  • Firstpage
    838
  • Lastpage
    848
  • Abstract
    A new approach is proposed for active fault tolerant control systems (FTCS), which allows one to explicitly incorporate allowable system performance degradation in the event of partial actuator fault in the design process. The method is based on model-following and command input management techniques. The degradation in dynamic performance is accounted for through a degraded reference model. A novel method for,selecting such a model is also presented. The degradation in steady-state performance is dealt with using a command input adjustment technique. When a fault is detected by the fault detection and diagnosis (FDD) scheme, the reconfigurable controller is designed automatically using an eigenstructure assignment algorithm in an explicit model-following framework so that the dynamics of the closed-loop system follow that of the degraded reference model. In the mean time, the command input is also adjusted automatically to prevent the actuators from saturation. The proposed method has been evaluated using the lateral dynamics of an F-8 aircraft against actuator faults subject to constraints on the magnitude of actuator inputs. Very encouraging results have been obtained.
  • Keywords
    actuators; aircraft control; closed loop systems; eigenvalues and eigenfunctions; fault tolerance; military aircraft; F-8 aircraft; actuator faults; closed-loop system; command input adjustment technique; command input management techniques; degraded reference model; eigenstructure assignment algorithm; explicit model-following framework; fault detection; fault tolerant control system design; lateral dynamics; model-following techniques; partial actuator fault; performance degradation; reconfigurable controller; steady-state performance; Actuators; Automatic control; Control systems; Degradation; Fault detection; Fault diagnosis; Fault tolerant systems; Process design; 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/TAES.2003.1238740
  • Filename
    1238740