| 捷联惯导系统初始对准技术的研究 |
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| 引用本文： | 于国宏.捷联惯导系统初始对准技术的研究[J].上海航天,1995(3):11-13. |
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| 作者姓名： | 于国宏 |
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| 作者单位： | 上海航天局第八○三研究所 |
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| 摘 要： | 以舰空导弹捷联惯导为背景，研究了捷联系系统在舰船支基座情况下的初始对准问题。介绍了目前国内外正在使用与正在研究的各种初始对准方法。比较了它们的性质与使用局限性。这些方法可以作为确定初始对准方案的参考。
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| 关 键 词： | 惯性导航 舰载导弹 初始对准 导弹 制导 |
STUDY ON INITIAL ALIGNING TECHNIQUE FOR STRAPDOWN INERTIAL NAVIGATION SYSTEM |
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| Yu Guohong.STUDY ON INITIAL ALIGNING TECHNIQUE FOR STRAPDOWN INERTIAL NAVIGATION SYSTEM[J].Aerospace Shanghai,1995(3):11-13. |
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| Authors: | Yu Guohong |
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| Institution: | The No. 803 Institute of Shanghai Bureau of Astronautics |
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| Abstract: | The initial alignment of strapdown system in case of moving bases in ships is studied on the background of strapdown inertial navigation for ship to air missiles. Different initial aligning methods being used and studied at home and abroad are introduced; the comparison on their properties and limitations can be regarded as a reference for determining an initial aligning program. |
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| Keywords: | Strapdown inertial navigation Shipborne missile Initial aligning method |
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