| 单航天器无需机动对星座多星交会轨道全解 |
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| 引用本文： | 王威,付晓锋,郗晓宁.单航天器无需机动对星座多星交会轨道全解[J].宇航学报,2007,28(3):663-666. |
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| 作者姓名： | 王威 付晓锋 郗晓宁 |
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| 作者单位： | 1. 国防科学技术大学机电工程与自动化学院,长沙,410073
2. 国防科学技术大学航天与材料工程学院,长沙,410073 |
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| 基金项目： | 武器装备预研基金;武器装备预研基金 |
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| 摘 要： | 文献1,2]已研究了单航天器无需变轨对Walker星座多星交会的轨道设计,在此基础上,依据交会点必是轨道交点的轨道特性,提出了轨道全解的解析法,可给出该轨道所能够交会卫星的最大数目,研究结果可为单航天器无需大机动变轨对星座多星接近的轨道应用提供理论参考。
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| 关 键 词： | Walker星座 交会 接近 轨道设计 |
| 文章编号： | 1000-1328(2007)03-0663-04 |
| 修稿时间： | 2006年1月9日 |
Intact Resolution of Single Spacecraft Intersecting Multiple Satellites of a Constellation without Orbit Maneuver |
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| WANG Wei,FU Xiao-feng,XI Xiao-ning.Intact Resolution of Single Spacecraft Intersecting Multiple Satellites of a Constellation without Orbit Maneuver[J].Journal of Astronautics,2007,28(3):663-666. |
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| Authors: | WANG Wei FU Xiao-feng XI Xiao-ning |
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| Abstract: | Orbital design about single spacecraft intersecting multiple satellites of Walker Constellation without orbital maneuver had been discussed in Refs.According to the orbital feature that the intersecting point must be the orbit cross point,analytic method was presented to get the whole result of intersecting orbits in this paper,which is based on the orbital design.The method is able to provide the maximum number of the satellites which can be intersected.All of this can provide academic reference to orbital application of single spacecraft approaching multiple satellites of constellation. |
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| Keywords: | Walker constellation Intersection Approach Orbital design |
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