| “和平保卫者”导弹惯性制导器件和系统设计的进展 |
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| 引用本文： | 孙梅,王永平.“和平保卫者”导弹惯性制导器件和系统设计的进展[J].航天控制,1993(2). |
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| 作者姓名： | 孙梅 王永平 |
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| 作者单位： | 北京航天自动控制研究所，北京航天自动控制研究所 |
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| 摘 要： | 本文综述了“和平保卫者”导弹惯性制导系统的设计、导弹精度和一些设计成果的经验。并且分析在实际设计时,如何考虑这些影响,以满足系统的性能等要求。
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| 关 键 词： | MGM-118导弹 惯性制导系统 惯性测量装置 |
Evolution of The Peacekeeper Inertial Guidance Components and System Designs |
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| Sun Mei Wang Yongping Beijing Aerospace Automatic Control Institute.Evolution of The Peacekeeper Inertial Guidance Components and System Designs[J].Aerospace Control,1993(2). |
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| Authors: | Sun Mei Wang Yongping Beijing Aerospace Automatic Control Institute |
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| Institution: | Sun Mei Wang Yongping Beijing Aerospace Automatic Control Institute |
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| Abstract: | This paper describes the Peacekeeper missile's inertia! guidancee system design, missile accuracy and provides just a taste of the design efforts. Examples are given of how these impacts are addressed in the actual design to meet performance, hardness and other system requirements. |
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| Keywords: | MGM-118 missile Inertial guidance system Inertial measurement unit |
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