| 搭载小卫星轨道控制策略研究与实际应用 |
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| 引用本文： | 谭炜,杨开忠,赵丽.搭载小卫星轨道控制策略研究与实际应用[J].飞行器测控学报,2006,25(3):13-19. |
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| 作者姓名： | 谭炜 杨开忠 赵丽 |
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| 作者单位： | 西北工业大学航天学院 陕西西安.710072(谭炜)，西安卫星测控中心 陕西西安.710043(杨开忠，赵丽) |
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| 摘 要： | 随着小卫星应用领域的日益广阔和小卫星数量的不断增长,对小卫星轨道控制技术的要求也越来越高。本文以某搭载小卫星(下面简称搭载星)为例,对太阳同步轨道小卫星的轨道特性、轨道控制策略等问题进行了较深入的探讨,并对变轨策略实施的理论计算结果和实测定轨结果进行了对比分析。
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| 关 键 词： | 搭载卫星 小卫星 轨道控制 |
| 收稿时间： | 2005-12-21 |
| 修稿时间： | 2006-03-23 |
Research and Application on the Orbit Control Strategy for the Carried Small Satellite |
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| TAN Wei, YANG Kai-zhong, ZHAO Li.Research and Application on the Orbit Control Strategy for the Carried Small Satellite[J].Journal of Spacecraft TT&C Technology,2006,25(3):13-19. |
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| Authors: | TAN Wei YANG Kai-zhong ZHAO Li |
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| Abstract: | With the wide application of small satellite and its increasing quantity,the requirements for orbit control technology of the small satellite is becoming more strict.This paper takes one carried small satellite(hereafter referred to as carried satellite) as an example in order to discuss deeply the orbit characteristics and the control strategy about the sun synchronous small satellite.Furthermore,the analysis is made by comparing the theoretic calculation of the implemented orbit control strategy with the actual orbit determined result. |
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| Keywords: | Carried Satellite Small Satellite Orbit Control |
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