| 采用捷联惯性导航系统的战术导弹初始对准误差分离方法研究 |
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| 引用本文： | 吴向东.采用捷联惯性导航系统的战术导弹初始对准误差分离方法研究[J].现代防御技术,2000,28(3):31-36. |
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| 作者姓名： | 吴向东 |
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| 作者单位： | 中国航天机电集团二院二部,北京,100854 |
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| 摘 要： | 捷联惯性导航系统的初始对准误差是战术地空导弹精度分配中的主要误差源之一 ,研究在外场条件下初始对准误差的快速分离方法对于提高导弹制导精度具有积极意义。
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| 关 键 词： | 战术地空导弹 捷联惯性导航系统 初始对准 误差 |
| 修稿时间： | 1999-12-25 |
Separation Technique of Strapdown Inertial Navigation System(SINS) Initial Alignment Error for Tactical Surface to Air Missile |
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| WU Xiang-dong.Separation Technique of Strapdown Inertial Navigation System(SINS) Initial Alignment Error for Tactical Surface to Air Missile[J].Modern Defence Technology,2000,28(3):31-36. |
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| Authors: | WU Xiang-dong |
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| Abstract: | SINS initial alignment error is one of the important error sources for tactical surface to air missile precision allocation.It is necessary and advantageous to research quickly separate technique of SINS initial alignment error in outfield for improving missile guidance precision. |
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| Keywords: | Tactical surface to air missile Strapdown inertial navigation system Initial alignment Error |
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