| 运载火箭制导系统冗余设计技术研究 |
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| 引用本文： | 胡云中.运载火箭制导系统冗余设计技术研究[J].航天控制,1998,16(2):10-15. |
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| 作者姓名： | 胡云中 |
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| 作者单位： | 北京航天自动控制研究所,100854 |
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| 摘 要： | 针对提高运载火箭飞行控制系统可靠性问题，从制导系统角度给出了两种系统级冗余方案，对其冗余配置、可靠性、冗余管理、故障检测和隔离、系统同步问题进行了讨论。
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| 关 键 词： | 运载火箭 控制系统 冗余技术 故障检测 |
| 修稿时间： | 1998年4月8日 |
Research for Redundant Technology of Launch Vehicle Guidance System |
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| Hu Yunzhong.Research for Redundant Technology of Launch Vehicle Guidance System[J].Aerospace Control,1998,16(2):10-15. |
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| Authors: | Hu Yunzhong |
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| Abstract: | To improve the reliability of flight control system of launch vehicle, two systemic redundant scheme are proposed in this paper at the view of guidance system. Moreover, research is delved in aspect of reliability, failure detection, redundant configuration and management as well as synchronous problem of the redundant system. |
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| Keywords: | Launch vehicle Control system Redundant technology Failure detection |
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