| CZ-2F高可靠内冗余三轴惯性稳定平台系统 |
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| 引用本文： | 陈东生,闵跃军,门吉卓.CZ-2F高可靠内冗余三轴惯性稳定平台系统[J].导弹与航天运载技术,2004(1):38-44. |
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| 作者姓名： | 陈东生 闵跃军 门吉卓 |
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| 作者单位： | 中国航天时代电子公司设计中心,北京,100854;中国航天时代电子公司设计中心,北京,100854;中国航天时代电子公司设计中心,北京,100854 |
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| 摘 要： | 介绍了三轴惯性平台系统(8K40-2F)的功能、组成和结构,简要说明了平台系统的工作原理,并着重阐述了为满足载人航天高可靠性的要求所采取的技术改进设计方案及措施.
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| 关 键 词： | 惯性平台系统 可靠性 冗余 |
| 文章编号： | 1004-7182(2004)01-0038-07 |
| 修稿时间： | 2004年12月5日 |
Highly Reliable Triaxial Redundant Inertial Stabilized Platform System of LM-2F Launch Vehicle |
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| Chen Dongsheng,Min Yaojun,Men Jizhuo.Highly Reliable Triaxial Redundant Inertial Stabilized Platform System of LM-2F Launch Vehicle[J].Missiles and Space Vehicles,2004(1):38-44. |
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| Authors: | Chen Dongsheng Min Yaojun Men Jizhuo |
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| Abstract: | The function, composition and structure of triaxial inertial platform system are introduced in this paper. The operating principle of the platform system is briefly described, and the technical concepts and measures which are adopted to meet the requirements of high reliability of manned space flight are emphatically expounded. |
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| Keywords: | Inertial platform system Reliability Redundancy |
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