| 空基激光陀螺捷联惯导系统导航精度的分析与研究 |
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| 引用本文： | 岳明桥,李高鹏.空基激光陀螺捷联惯导系统导航精度的分析与研究[J].战术导弹技术,2005(4):40-43. |
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| 作者姓名： | 岳明桥 李高鹏 |
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| 作者单位： | 92941部队,辽宁葫芦岛125001 |
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| 摘 要： | 从现代导弹的实际情况出发, 通过对空基激光陀螺捷联惯导系统导航工作原理的分析, 总结了空基激光陀螺捷联惯导系统导航误差产生的原因, 归纳了激光陀螺和加速度计的误差模型和补偿.
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| 关 键 词： | 捷联惯导 惯性导航 激光陀螺 加速度计 |
| 文章编号： | 1009-1300(2005)04-0040-03 |
| 修稿时间： | 2004年11月24 |
Analysis and Study on Navigation Accuracy of Laser Gyro SINS System of Vacuous Basis |
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| Yue Mingqiao,Li Gaopeng.Analysis and Study on Navigation Accuracy of Laser Gyro SINS System of Vacuous Basis[J].Tactical Missile Technology,2005(4):40-43. |
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| Authors: | Yue Mingqiao Li Gaopeng |
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| Abstract: | Going from the practical situation of modern missile,the operation theory of laser gyro SINS system of vacuous basis is analyzed.The generated reasons of navigation error of laser gyro SINS system of vacuous basis are summarized.The error model and compensation of laser gyro and acceleration are generalized. |
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| Keywords: | SINS inertial navigation laser gyro acceleration |
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