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- W164562618 abstract "Lunar relay satellite (LRS) constellation is required for the exploration of the back and polar regions of the moon. In order to provide high coverage rate, generally we choose high circular or elliptical orbits for the relay satellites. From discussion we can know that the elliptical orbit constellation consists of the minimum number of satellites needed to provide continuous coverage of the moon’s south pole regions. To save fuel needed for orbit maintenance and extend the lives of satellites, a stable elliptical frozen orbit is required. Here the lunar high frozen orbit relay constellation, which not only meets the demand for work, but also has high stability, has been found and designed through establishing the satellite’s force model and the perturbation function in lunar environment, and through designing the strategies of deployment and maintenance of the constellation." @default.
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- W164562618 date "2012-01-01" @default.
- W164562618 modified "2023-10-16" @default.
- W164562618 title "Lunar High Frozen Orbit Relay Satellite Constellation and Its Deployment and Maintenance" @default.
- W164562618 cites W2128410770 @default.
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- W164562618 doi "https://doi.org/10.1007/978-3-642-29187-6_25" @default.
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