• Electronics Optics & Control
  • Vol. 23, Issue 10, 104 (2016)
LI Yong and CAO Dong
Author Affiliations
  • [in Chinese]
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    DOI: 10.3969/j.issn.1671-637x.2016.10.022 Cite this Article
    LI Yong, CAO Dong. Analytical Model Based Fault Diagnosis for Actuator of Flight Control System[J]. Electronics Optics & Control, 2016, 23(10): 104 Copy Citation Text show less
    References

    [4] GUO Y Y, JIANG B, ZHANG Y M, et al.Novel robust fault diagnosis method for flight control systems[J].Journal of Systems Engineering and Electronics, 2008, 19(5):1017-1023.

    [6] MERRILL W C.Sensor failure detection for jet engines using analytical redundancy[J].Journal of Guidance, Control and Dynamics, 1985, 8(6):673-682.

    [7] GOPISETTY S W M.Failure detection and identification:application to aircraft control[D].Princeton:Princeton University, 2000.

    [8] LI X R, WANG L.Fault detection using sequential proba-bility ratio test[C]//IEEE, 1999.doi:10.1109/PESW.1999.747296.

    [9] XIA G H.Failure detection, isolation and compensation[D].Los Angeles:University of California, 1982.

    [10] TUULA R.Nonlinear filtering techniques for failure detection in dynamic systems[D].Boca Raton:Florida Atlantic University, 1989.

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    LI Yong, CAO Dong. Analytical Model Based Fault Diagnosis for Actuator of Flight Control System[J]. Electronics Optics & Control, 2016, 23(10): 104
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