Electronics Optics & Control, Volume. 22, Issue 12, 59(2015)

Variable Structure Guidance Law Based on Genetic Algorithm

XING Jin-he... WANG Xue-mei, XU Zhe and ZHENG Gang |Show fewer author(s)
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    References(7)

    [1] [1] QIAN X F,LIN R X,ZHAO Y N.Flight mechanics of guided missile[M].Beijing:Beijing Institute of Technology Press,2008.

    [2] [2] ZARCHAN P.Tactical and strategic missile guidance[M].5th ed.San Diego:American Institute of Aeronautics and Astronautics,2007.

    [3] [3] ZHOU D,MU C,LING Q,et al.Optimal sliding-mode guidance of a homing-missile[J].Chinese Journal of Aeronautics,1999,12(4):236-241.

    [4] [4] ZHOU D,MU C,XU W L.Adaptive sliding-mode guidance of a homing missile[J].Journal of Guidance,Control and Dynamics,1999,22(4):589-594.

    [5] [5] WANG Z,JIA X H,YAN J.Study on the ENDGAME sliding-mode guidance law of air-to-air missile[J].Aero Weaponry,2005(2):3-6.

    [6] [6] LI Y.Study on variable structure terminal guidance law and stability of space interception[D].Harbin:Harbin Institute of Technology,2011.

    [7] [7] YUAN L Y.Nonlinear guidance law for interception of maneuvering target[D].Harbin:Harbin Institute of Technology,2008.

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    XING Jin-he, WANG Xue-mei, XU Zhe, ZHENG Gang. Variable Structure Guidance Law Based on Genetic Algorithm[J]. Electronics Optics & Control, 2015, 22(12): 59

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    Paper Information

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    Received: Nov. 14, 2014

    Accepted: --

    Published Online: Dec. 18, 2015

    The Author Email:

    DOI:10.3969/j.issn.1671-637x.2015.12.012

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