Electronics Optics & Control, Volume. 27, Issue 3, 104(2020)

Sliding Mode Control for Longitudinal State of Aircraft Based on Fast Double-Power Reaching Law with Unidirectional Auxiliary Surface

SHAO Peng... KANG Chuanhua, ZHAI Wenhua, ZHONG Zhao and WANG Lei |Show fewer author(s)
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    References(5)

    [2] [2] XU B, PAN Y P, WANG D W, et al.Discrete-time high speed vehicle control based on extreme learning machine[J].Neurocomputing, 2014, 128:232-241.

    [6] [6] KACHROO P.Existence of solutions to a class of nonlinear convergent chattering-free sliding mode control systems[J].IEEE Transactions on Automatic Control, 1999, 44(8):1620-1624.

    [7] [7] CHEN S Y, LIN F J.Robust nonsingular terminal sliding mode control for nonlinear magnetic bearing system[J].IEEE Transactions on Control Systems Technology, 2011, 19(3):636-643.

    [9] [9] WANG Y M, FENG Y, YU X H.Higher-order nonsingular terminal sliding mode control of uncertain multivariable systems[C]//The 33rd Annual Conference of the IEEE Industrial Electronics Society, 2007:710-714.

    [11] [11] FU J, WU Q X, CHEN W H, et al.Chattering-free condition for sliding mode control with unidirectional auxiliary surfaces[J].Transactions of the Institute of Measurement and Control, 2013, 35(5):593-605.

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    SHAO Peng, KANG Chuanhua, ZHAI Wenhua, ZHONG Zhao, WANG Lei. Sliding Mode Control for Longitudinal State of Aircraft Based on Fast Double-Power Reaching Law with Unidirectional Auxiliary Surface[J]. Electronics Optics & Control, 2020, 27(3): 104

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    Paper Information

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    Received: Mar. 29, 2019

    Accepted: --

    Published Online: Dec. 23, 2020

    The Author Email:

    DOI:10.3969/j.issn.1671-637x.2020.03.020

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