Electronics Optics & Control, Volume. 23, Issue 5, 50(2016)
A Method for Missile-Borne Inertial/Astronomical Attitude Integrated Navigation
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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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Received: Apr. 27, 2015
Accepted: --
Published Online: Jun. 6, 2016
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