| 捷联惯导与导航卫星组合技术的发展趋势 |
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| 引用本文： | 彭允祥.捷联惯导与导航卫星组合技术的发展趋势[J].导弹与航天运载技术,1999(4):58-62. |
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| 作者姓名： | 彭允祥 |
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| 作者单位： | 北京控制仪器研究所,北京,100085 |
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| 摘 要： | 惯性技术逐渐从平台系统过渡到捷联系统，从机械转子陀螺向固态陀螺发展，以惯性技术为基础的组合导航系统得到了重视和发展，介绍了捷联系统和组合导航系统在发展过程存在的各种技术问题和解决这些技术难题的技术途径。
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| 关 键 词： | 捷联式惯性制导 组合导航技术 全球定位系统 |
| 修稿时间： | 1999-02-03 |
The Development Tendency of Combination Technology of Strapdown Inertial Guidance and Navigation Satellite |
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| Peng Yunxiang.The Development Tendency of Combination Technology of Strapdown Inertial Guidance and Navigation Satellite[J].Missiles and Space Vehicles,1999(4):58-62. |
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| Authors: | Peng Yunxiang |
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| Abstract: | Inertial technology is transformed from platform system into strapdown system gradually, and gyroscope is changed from mechanical rotor model into solid state one. Combined navigation system based on inertial technology is paid attention to and developed. The various technical problems encountered during the development of strapdown system and combined navigation system are introduced and the technical ways used to solve the problems are given. |
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| Keywords: | Strapdown inertial guidance +Combined navigation Global positioning system |
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