Electronics Optics & Control, Volume. 23, Issue 5, 50(2016)

A Method for Missile-Borne Inertial/Astronomical Attitude Integrated Navigation

ZHU Jian-bin1... TAN Shou-lin1, TAN Fei2 and LI Fang3 |Show fewer author(s)
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    ZHU Jian-bin, TAN Shou-lin, TAN Fei, LI Fang. A Method for Missile-Borne Inertial/Astronomical Attitude Integrated Navigation[J]. Electronics Optics & Control, 2016, 23(5): 50

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    Paper Information

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    Received: Apr. 27, 2015

    Accepted: --

    Published Online: Jun. 6, 2016

    The Author Email:

    DOI:10.3969/j.issn.1671-637x.2016.05.011

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