| 运载火箭姿态控制系统冗余方案分析研究 |
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| 引用本文： | 孙培磊.运载火箭姿态控制系统冗余方案分析研究[J].导弹与航天运载技术,2001(6):9-14. |
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| 作者姓名： | 孙培磊 |
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| 作者单位： | 上海航天自动控制设备设计研究所, |
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| 摘 要： | 针对提高运载火箭姿态控制系统可靠性问题，从姿态角速度信号获取及伺服系统回路设计两方面提出了故障吸收冗余方案模式，对其冗余配置、工作原理、可靠性问题进行了讨论，并对方案可行性进行了设计分析。
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| 关 键 词： | 运载火箭 姿态控制系统 速率陀螺 伺服机构 冗余技术 |
Analysis and Research on the Redundance Concept of the Attitude Control System of Launch Vehicle |
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| Sun Peilei.Analysis and Research on the Redundance Concept of the Attitude Control System of Launch Vehicle[J].Missiles and Space Vehicles,2001(6):9-14. |
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| Authors: | Sun Peilei |
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| Abstract: | To raise the reliability of attitude control system of launch vehicle, the failure elimination redundance concept mode is given for attitude angular rate measurement and servo system loop design. The redundant layout,operating priniciple and reliability of the concept are discussed. The concept feasibility is analysied. |
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| Keywords: | Lanuch vehicle Attitude control Rate gyro Servomechanism |
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