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    Journals >Electronics Optics & Control >Volume 23 >Issue 5 >Page 50 > Article
    • Electronics Optics & Control
    • Vol. 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
    Author Affiliations
  • 1[in Chinese]
  • 2[in Chinese]
  • 3[in Chinese]
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    DOI: 10.3969/j.issn.1671-637x.2016.05.011 Cite this Article
    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 Copy Citation Text show less
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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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