Electronics Optics & Control, Volume. 28, Issue 3, 46(2021)

Sliding Mode Guidance Law of Means Clustering Neural Network with Falling Angle Constraint

ZHANG Jiawen1... SHI Jinguang1, LIU Jiajia2 and XU Donghui2 |Show fewer author(s)
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    References(5)

    [9] [9] SONG J M, ZHANG T Q.Passive homing missiles variable structure proportional navigation with terminal angular constraint[J].Chinese Journal of Aeronautics, 2001, 14(2): 83-87.

    [10] [10] QIN T, CHEN W C, XING X L.A method for precision missile guidance with impact attitude angle constraint [J].Journal of Astronautics, 2012, 33(5): 570-576.

    [13] [13] KUMAR S R, RAO S, GHOSE D.Nonsingular terminal sliding mode guidance with impact angle constraints[J].Journal of Guidance, Control and Dynamics, 2014, 22(5): 1114-1130.

    [14] [14] ZHAO Y, SHENG Y Z, LIU X D.Sliding mode control based guidance law with impact angle constraint[J].Chinese Journal of Aeronautics, 2014, 27(1): 145-152.

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    ZHANG Jiawen, SHI Jinguang, LIU Jiajia, XU Donghui. Sliding Mode Guidance Law of Means Clustering Neural Network with Falling Angle Constraint[J]. Electronics Optics & Control, 2021, 28(3): 46

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    Paper Information

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    Received: Feb. 19, 2020

    Accepted: --

    Published Online: Aug. 22, 2021

    The Author Email:

    DOI:10.3969/j.issn.1671-637x.2021.03.009

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