• DocumentCode
    2223393
  • Title

    A Nonlinear Geometric Fault Detection and Isolation Approach for Almost-Lighter-Than-Air-Vehicles

  • Author

    Meskin, N. ; Jiang, T. ; Sobhani, E. ; Khorasani, K. ; Rabbath, C.A.

  • Author_Institution
    Dept. of Electr. & Comput. Eng., Concordia Univ., Montreal, QC
  • fYear
    2007
  • fDate
    1-3 Oct. 2007
  • Firstpage
    1073
  • Lastpage
    1078
  • Abstract
    In this paper, the problem of actuator fault detection and isolation (FDI) for almost-lighter-than-air-vehicles (ALTAVs) is investigated using a nonlinear geometric approach. Due to the particular dynamics of the ALTAV, six detection filters are designed for FDI of the four input channels of the ALTAV. Four of the detection filters are designed such that each input channel affects only one of the actuators and the other two detection filters are affected by the corresponding two input channels. Using an appropriate combination of detection filters, one may detect and isolate the faults in all the input channels associated with single as well as simultaneous multiple actuators faults. Numerous simulation results demonstrate and show the excellent performance of the designed nonlinear detection filters.
  • Keywords
    actuators; aircraft control; fault diagnosis; nonlinear control systems; almost-lighter-than-air-vehicles; fault isolation; multiple actuators faults; nonlinear geometric fault detection; six detection filters; Actuators; Control systems; Electrical fault detection; Fault detection; Fault diagnosis; Filters; Nonlinear control systems; Nonlinear systems; Research and development; Unmanned aerial vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Applications, 2007. CCA 2007. IEEE International Conference on
  • Conference_Location
    Singapore
  • Print_ISBN
    978-1-4244-0442-1
  • Electronic_ISBN
    978-1-4244-0443-8
  • Type

    conf

  • DOI
    10.1109/CCA.2007.4389376
  • Filename
    4389376