| 最小高度变化轨道 |
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| 引用本文： | 杨维廉.最小高度变化轨道[J].中国空间科学技术,1988(3). |
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| 作者姓名： | 杨维廉 |
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| 作者单位： | 空间飞行器总体设计部 |
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| 摘 要： | 一类地球观测卫星要求在特定的区域其高度变化最小,以便星上遥感器能始终处于最佳的距离范围内工作,这样就可以得到清晰的、比例尺基本不变的遥感图片。本文推导了这种最小高度变化轨道的条件,并给出了相应的参数。
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| 关 键 词： | 卫星轨道 高度控制 轨道控制 |
MINIMUM ALTITUDE VARIATION ORBIT |
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| Yang Weilian.MINIMUM ALTITUDE VARIATION ORBIT[J].Chinese Space Science and Technology,1988(3). |
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| Authors: | Yang Weilian |
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| Institution: | Institute of spacecraft systems engineerjng |
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| Abstract: | Some earth observation satellites require minimum altitude variation in certain areas in order to provide satellites with optimal range at which onboard remote sensing devices operate, so that images can be sharp and with near constant scale. In this paper conditions for such a kind of orbits, the minimum altitude variation orbits, are derived and related parameters are given. |
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| Keywords: | Satellite orbit Altitude control Orbit calculation |
| 本文献已被 CNKI 等数据库收录！ |
