Electronics Optics & Control, Volume. 26, Issue 3, 16(2019)

Active Fault Tolerant Control of Aircraft Based on Integral Sliding Mode Control

LI Li-rong and LIU Chun-sheng
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  • [in Chinese]
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    References(2)

    [4] [4] SIDIM J.Spacecraft dynamics and control:a practical engineering approach[M].Cambridge:Cambridge University Press, 1997.

    [8] [8] XU J X, PAN Y J, LEE T H.Analysis and design of integral sliding mode control based on Lyapunov′s direct method[C]//American Control Conference, Denver, 2003:192-196.

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    LI Li-rong, LIU Chun-sheng. Active Fault Tolerant Control of Aircraft Based on Integral Sliding Mode Control[J]. Electronics Optics & Control, 2019, 26(3): 16

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    Paper Information

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    Received: Jan. 10, 2018

    Accepted: --

    Published Online: Mar. 25, 2019

    The Author Email:

    DOI:10.3969/j.issn.1671-637x.2019.03.004

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