| 航天器入轨误差分析 |
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| 引用本文： | 佘明生.航天器入轨误差分析[J].中国空间科学技术,1987(4). |
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| 作者姓名： | 佘明生 |
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| 作者单位： | 空间飞行器总体设计部 |
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| 摘 要： | 由于发射时熄火点产生的误差,需要有一种误差分析以便确定运载火箭的制导精度。本文介绍了飞行路径上的小误差对航天器轨道的影响,接着讨论了确定制导精度的方法并给出了圆轨道的简化公式。
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| 关 键 词： | 航天器制导 轨道计算 误差分析 |
THE GUIDANCE ERRORS OF THE FLIGHT PATH ON THE VEHICLE ORBIT |
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| She Ming sheng.THE GUIDANCE ERRORS OF THE FLIGHT PATH ON THE VEHICLE ORBIT[J].Chinese Space Science and Technology,1987(4). |
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| Authors: | She Ming sheng |
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| Institution: | Beiling Institute of Spacecraft System Engineerng |
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| Abstract: | An error analysis is neccessary to determine the guidance accuracy due to errors at burnout accurring at launch. This paper presents the affect of small errors of the flight path on the vehicle orbit, subsquently, also discusses the method to determine the guidance accuracy and gives the simplified formula for the circular orbit. |
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| Keywords: | Spacecraft guidance Orbit calculation Error analysis |
| 本文献已被 CNKI 等数据库收录！ |
