| 多惯性仪表冗余系统方案设计及其关键技术 |
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| 引用本文： | 夏克寒,牟建华,夏治寒.多惯性仪表冗余系统方案设计及其关键技术[J].导弹与航天运载技术,2007(6):21-24. |
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| 作者姓名： | 夏克寒 牟建华 夏治寒 |
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| 作者单位： | 1. 第二炮兵装备研究院,北京,100085
2. 中国人民解放军96604部队,北京,100085 |
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| 摘 要： | 首先介绍了多惯性仪表冗余系统的功能和优缺点,指出它是提高弹道导弹制导系统可靠性和精度的重要途径.然后讨论了实现多惯性仪表冗余系统所需解决的几项关键技术,包括冗余系统的配置方案、优化冗余方法、惯性仪表选取和数据融合方法等,并给出了相应的建议和对策,最后以仿真实例表明该方案是可行的.
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| 关 键 词： | 冗余技术 惯性仪表 精度 可靠性 |
| 文章编号： | 1004-7182（2007）06-0021-04 |
| 收稿时间： | 2007-02-08 |
| 修稿时间： | 2007年2月8日 |
Design of Redundant System with Multiple Inertial Measurement Units and Its Key Technologies |
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| Xia Kehan,Mu Jianhua,Xia Zhihan.Design of Redundant System with Multiple Inertial Measurement Units and Its Key Technologies[J].Missiles and Space Vehicles,2007(6):21-24. |
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| Authors: | Xia Kehan Mu Jianhua Xia Zhihan |
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| Abstract: | The merits,demerits and functions of redundant systems with inertial measurement units are introduced.The redundant technique is an important approach for increasing the accuracy and reliability of guidance systems.The key technologies of redundant system with inertial measurement units are discussed,including the optimal design method,optimal scheme and choosing of inertial instruments,etc.Finally,advice and countermeasures are given and validated by the simulation examples. |
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| Keywords: | Redundant technology Inertial instrument Precision Reliability |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
