Coverage Analysis of Lunar Communication/Navigation Constellations Based on Halo Orbits and Distant Retrograde Orbits
Coverage Analysis of Lunar Communication/Navigation Constellations Based on Halo Orbits and Distant Retrograde Orbits
复制标题
基于晕轨道和远逆行轨道的月球通信/导航星座覆盖分析
DOI:
10.1017/s0373463320000065
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发表时间:
2020-07-01
影响因子:
2.4
通讯作者:
Hou, Xi-Yun
中科院分区:
文献类型:
--
作者:
Gao, Zhao-Yang;Hou, Xi-Yun
With more and more missions around the Moon, a communication/navigation constellation around the Moon is necessary. Halo orbits, due to their unique geometry, are extensively studied by researchers for this purpose. A dedicated survey is carried out in this work to analyse the coverage ability of halo orbits. It is found that a two-satellite constellation is enough for continuous one-fold coverage of the north or the south polar regions but never both. A three-satellite constellation is enough for continuous one-fold coverage of both north and south polar regions. A four-satellite constellation can cover nearly 100% of the whole lunar surface. In addition, the coverage ability of another special orbit - distant retrograde orbit (DRO) - is analysed for the first time in this study. It is found that three satellites on DROs can cover 99 center dot 8% of the lunar surface, with coverage gaps at polar caps. A four-satellite constellation moving on spatial DROs can cover nearly the whole lunar surface. By combining halo orbits and DROs, we design a five-satellite constellation composed of three halo orbit satellites and two DRO satellites. This constellation can provide 100% continuous one-fold coverage of the whole lunar surface.