Electronics Optics & Control, Volume. 25, Issue 8, 74(2018)

Neural Network Controller Design for Missil Compound Control System

SONG Xiaona, LIU Kai, and SONG Shuai
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    References(3)

    [4] [4] SHTESSEL Y B, SHKOLNIKOV I A, LEVANT A.Gui-dance and control of missile interceptor using second-order sliding modes[J].IEEE Transactions on Aerospace & Elec-tronic Systems, 2009, 45(1):110-124.

    [5] [5] CHOI J Y, CHWA D.Adaptive control based on a parametric affine model for tail-controlled missiles[J].IEEE Transactions on Aerospace & Electronic Systems, 2006, 42(2):659-669.

    [10] [10] YEH F K.Adaptive-sliding-mode guidance law design for missiles with thrust vector control and divert control system[J].IET Control Theory & Applicationsc2012, 6(4):552-559.

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    [1] TIAN Beibei, ZHAO Feng. Robust Optimal Sliding Mode Control of Missile Autopilot Based on Adaptive Dynamic Programming[J]. Electronics Optics & Control, 2021, 28(11): 54

    [2] WANG Liangliang, LIU Wenxue, XUE Fangfang, FENG Wei, CAO Lin. A Method of Automatic Activation for Planned Flight Segment[J]. Electronics Optics & Control, 2021, 28(7): 108

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    SONG Xiaona, LIU Kai, SONG Shuai. Neural Network Controller Design for Missil Compound Control System[J]. Electronics Optics & Control, 2018, 25(8): 74

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    Paper Information

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    Received: Aug. 7, 2017

    Accepted: --

    Published Online: Jan. 19, 2021

    The Author Email:

    DOI:10.3969/j.issn.1671-637x.2018.08.015

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