Electronics Optics & Control, Volume. 21, Issue 9, 95(2014)

MidGuidance Instruction Calculation of Medium Range Air to Air Intercept Missile

KANG Zhiqiang... KOU Yingxin, LI Zhanwu and CHEN Lei |Show fewer author(s)
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    References(6)

    [1] [1] HOU Z QYANG JFAN G L.Design of optimal midcourse guidance law for antiradar missile[J].Computer Simulation201128(7):71-74.

    [2] [2] ZHAO Z WZHANG AXIA Q Jet al. Simulated computation of targetacquisition probability of intermediatelongrange airtoair missile[J].Fire Control & Command Control201136(10):160-164.

    [3] [3] ZHOU Z G.Aviation integrated fire control principle[M].Beijing:National Defense Industry Press2008.

    [4] [4] QIAN H MCHEN LMAN G Jet al.Adaptive tracking algorithm of maneuvering targets based on current statistical model[J].Systems Engineering and Electronics201133(10):2154-2158.

    [6] [6] ZHOU H RJING Z LWANG P D.Maneuvering target tracking[M].Beijing:National Nefense Industry Press1991.

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    KANG Zhiqiang, KOU Yingxin, LI Zhanwu, CHEN Lei. MidGuidance Instruction Calculation of Medium Range Air to Air Intercept Missile[J]. Electronics Optics & Control, 2014, 21(9): 95

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    Paper Information

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    Received: Oct. 21, 2013

    Accepted: --

    Published Online: Sep. 15, 2014

    The Author Email:

    DOI:10.3969/j.issn.1671-637x.2014.09.021

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