• DocumentCode
    2752064
  • Title

    A novel design for robust fault diagnostic observer

  • Author

    Xiong, Yi ; Saif, Mehrdad

  • Author_Institution
    Sch. of Eng. Sci., Simon Fraser Univ., Burnaby, BC, Canada
  • Volume
    1
  • fYear
    1998
  • fDate
    1998
  • Firstpage
    592
  • Abstract
    A new approach for the design of robust fault diagnostic observers is proposed in this article. The design is carried out through transformation of the system into its special coordinate basis (SCB) form, and with the aid of loop transfer recovery (LTR) like techniques. Furthermore, simple necessary and sufficient conditions for existence of perfect disturbance decoupled residual are presented. The proposed design approach offers computational simplicity and unifies approaches using eigenstructure assignment and unknown input observer design. Finally, an example dealing with sensor and actuator failure diagnosis of a vertical takeoff and landing- (VTOL) aircraft is given to illustrate the proposed approach
  • Keywords
    computational complexity; eigenstructure assignment; fault diagnosis; observers; LTR; SCB form; VTOL aircraft; actuator failure diagnosis; computational simplicity; eigenstructure assignment; loop transfer recovery; necessary and sufficient conditions; perfect disturbance decoupled residual; robust fault diagnostic observer; sensor failure diagnosis; special coordinate basis form; unknown input observer design; Air safety; Aircraft; Fault detection; Fault diagnosis; Observers; Redundancy; Robustness; Sensor systems; State estimation; Uncertainty;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Decision and Control, 1998. Proceedings of the 37th IEEE Conference on
  • Conference_Location
    Tampa, FL
  • ISSN
    0191-2216
  • Print_ISBN
    0-7803-4394-8
  • Type

    conf

  • DOI
    10.1109/CDC.1998.760743
  • Filename
    760743