Design of an Orbital Infrastructure to Guarantee Continuous Communication to the Lunar South Pole Region

The lunar south pole has gained significant attention due to its unique scientific value and potential for supporting future human exploration. Its potential water ice reservoirs and favourable conditions for long-term habitation make it a strategic target for upcoming space missions. This has led t...

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Published in:Aerospace
Main Authors: Nicolò Trabacchin, Giacomo Colombatti
Format: Text
Language:English
Published: Multidisciplinary Digital Publishing Institute 2025
Subjects:
Online Access:https://doi.org/10.3390/aerospace12040289
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author Nicolò Trabacchin
Giacomo Colombatti
author_facet Nicolò Trabacchin
Giacomo Colombatti
author_sort Nicolò Trabacchin
collection MDPI Open Access Publishing
container_issue 4
container_start_page 289
container_title Aerospace
container_volume 12
description The lunar south pole has gained significant attention due to its unique scientific value and potential for supporting future human exploration. Its potential water ice reservoirs and favourable conditions for long-term habitation make it a strategic target for upcoming space missions. This has led to a continuous increase in missions towards the Moon thanks mainly to the boost provided by NASA’s Artemis programme. This study focuses on designing a satellite constellation to provide communication coverage for the lunar south pole. Among the various cislunar orbits analysed, the halo orbit families near Earth–Moon Lagrangian points L1 and L2 emerged as the most suitable ones for ensuring continuous communication while minimising the number of satellites required. These orbits, first described by Farquhar in 1966, allow spacecraft to maintain constant communication with Earth due to their unique geometric properties. The candidate orbits were initially implemented in MATLAB using the Circular Restricted Three-Body Problem (CR3BP) to analyse their main features such as stability, periodicity, and coverage time percentage. In order to develop a more detailed and realistic scenario, the obtained initial conditions were refined using a full ephemeris model, incorporating a ground station located near the Connecting Ridge Extension to evaluate communication performance depending on the minimum elevation angle of the antenna. Different multi-body constellations were propagated; however, the constellation consisting of three satellites around L2 and a single satellite around L1 turned out to be the one that best matches the coverage requirements.
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spelling ftmdpi:oai:mdpi.com:/2226-4310/12/4/289/ 2025-04-27T14:36:00+00:00 Design of an Orbital Infrastructure to Guarantee Continuous Communication to the Lunar South Pole Region Nicolò Trabacchin Giacomo Colombatti 2025-03-30 application/pdf https://doi.org/10.3390/aerospace12040289 eng eng Multidisciplinary Digital Publishing Institute Astronautics & Space Science https://dx.doi.org/10.3390/aerospace12040289 https://creativecommons.org/licenses/by/4.0/ Aerospace Volume 12 Issue 4 Pages: 289 lunar south pole constellation design CR3BP high-fidelity model Text 2025 ftmdpi https://doi.org/10.3390/aerospace12040289 2025-03-31T14:26:03Z The lunar south pole has gained significant attention due to its unique scientific value and potential for supporting future human exploration. Its potential water ice reservoirs and favourable conditions for long-term habitation make it a strategic target for upcoming space missions. This has led to a continuous increase in missions towards the Moon thanks mainly to the boost provided by NASA’s Artemis programme. This study focuses on designing a satellite constellation to provide communication coverage for the lunar south pole. Among the various cislunar orbits analysed, the halo orbit families near Earth–Moon Lagrangian points L1 and L2 emerged as the most suitable ones for ensuring continuous communication while minimising the number of satellites required. These orbits, first described by Farquhar in 1966, allow spacecraft to maintain constant communication with Earth due to their unique geometric properties. The candidate orbits were initially implemented in MATLAB using the Circular Restricted Three-Body Problem (CR3BP) to analyse their main features such as stability, periodicity, and coverage time percentage. In order to develop a more detailed and realistic scenario, the obtained initial conditions were refined using a full ephemeris model, incorporating a ground station located near the Connecting Ridge Extension to evaluate communication performance depending on the minimum elevation angle of the antenna. Different multi-body constellations were propagated; however, the constellation consisting of three satellites around L2 and a single satellite around L1 turned out to be the one that best matches the coverage requirements. Text South pole MDPI Open Access Publishing South Pole Aerospace 12 4 289
spellingShingle lunar south pole
constellation design
CR3BP
high-fidelity model
Nicolò Trabacchin
Giacomo Colombatti
Design of an Orbital Infrastructure to Guarantee Continuous Communication to the Lunar South Pole Region
title Design of an Orbital Infrastructure to Guarantee Continuous Communication to the Lunar South Pole Region
title_full Design of an Orbital Infrastructure to Guarantee Continuous Communication to the Lunar South Pole Region
title_fullStr Design of an Orbital Infrastructure to Guarantee Continuous Communication to the Lunar South Pole Region
title_full_unstemmed Design of an Orbital Infrastructure to Guarantee Continuous Communication to the Lunar South Pole Region
title_short Design of an Orbital Infrastructure to Guarantee Continuous Communication to the Lunar South Pole Region
title_sort design of an orbital infrastructure to guarantee continuous communication to the lunar south pole region
topic lunar south pole
constellation design
CR3BP
high-fidelity model
topic_facet lunar south pole
constellation design
CR3BP
high-fidelity model
url https://doi.org/10.3390/aerospace12040289