Reconfiguration and Optimization of Lunar Navigation Satellite Constellation Targeting South Hemisphere
Shuo YANG, Rui ZHONG, Franco BERNELLI ZAZZERA
Abstract. The Lunar Navigation Satellite System (LNSS) is a critical initiative in response to the current surge in international lunar exploration. Compared to Global Navigation Satellite Systems (GNSS), the development of LNSS involves significantly higher costs and longer deployment cycles. As a result, optimizing constellation design to maximize the use of limited resources has become a popular topic. This work adopts two constellation reconfiguration strategies and a multi-objective optimization approach to extend the target area from the lunar South Pole to the whole Southern Hemisphere. First, Hohmann-type phasing maneuvers are applied to in-orbit satellites, with optimization of both fuel consumption and maneuver time, resulting in a notable improvement in dual coverage performance over the South Hemisphere. Second, new satellites are introduced to restore high-quality service in the South Pole region. Simulation results of coverage and navigation performance at the lunar South Pole confirm the effectiveness of the final constellation scheme.
Keywords
Lunar Constellation, Constellation Reconfiguration, Multi-Objective Optimization
Published online 7/20/2026, 6 pages
Copyright © 2026 by the author(s)
Published under license by Materials Research Forum LLC., Millersville PA, USA
Citation: Shuo YANG, Rui ZHONG, Franco BERNELLI ZAZZERA, Reconfiguration and Optimization of Lunar Navigation Satellite Constellation Targeting South Hemisphere, Materials Research Proceedings, Vol. 69, pp 1140-1145, 2026
DOI: https://doi.org/10.21741/9781644904251-196
The article was published as article 196 of the book CEAS – AIDAA Conference 2025
Content from this work may be used under the terms of the Creative Commons Attribution 3.0 license. Any further distribution of this work must maintain attribution to the author(s) and the title of the work, journal citation and DOI.
References
[1] K. Bhasin, A. Hackenberg, R. Slywczak, P. Bose, M. Bergamo, J. Hayden, Lunar relay satellite network for space exploration: architecture, technologies and challenges, in: 24th AIAA International Communications Satellite Systems Conference, AIAA, San Diego, California, 2006, p. 5363. https://doi.org/10.2514/6.2006-5363
[2] C. Circi, D. Romagnoli, F. Fumenti, Halo orbit dynamics and properties for a lunar global positioning system design, Monthly Notices of the Royal Astronomical Society. 442 (2014) 3511-3527. https://doi.org/10.1093/mnras/stu1085
[3] G. Zanotti, M. Ceresoli, A. Pasquale, J. Prinetto, M. Lavagna, High performance lunar constellation for navigation services to moon orbiting users, Advances in Space Research. 73 (2024) 5665-5679. https://doi.org/10.1016/j.asr.2023.03.032
[4] M. Ferringer, D. Spencer, R. Clifton, T. Thompson, P. Reed, Pareto-hypervolumes for the reconfiguration of satellite constellations, in: AIAA/AAS Astrodynamics Specialist Conference and Exhibit, AIAA, Honolulu, Hawaii, 2008, p. 6611. https://doi.org/10.2514/6.2008-6611
[5] D. Arnas, R. Linares, Uniform satellite constellation reconfiguration, Journal of Guidance, Control, and Dynamics. 45 (2022), 1241-1254. https://doi.org/10.2514/1.G006514
[6] O.L. De Weck, U. Scialom, A. Siddiqi, Optimal reconfiguration of satellite constellations with the auction algorithm, Acta Astronautica. 62 (2008), 112-130. https://doi.org/10.1016/j.actaastro.2007.02.008
[7] A.N. Straub, D.E. Hastings, D.W. Miller, O.L. De Weck, Deployment strategies for reconfigurable satellite constellations, in: ASCEND 2020, AIAA, VirtualEvent, 2020, p. 4246. https://doi.org/10.2514/6.2020-4246
[8] S. Yang, R. Zhong, Optimization method for lunar navigation satellite constellation targeting south pole, in: L. Yan, H. Duan, Y. Deng (Eds.), Advances in Guidance, Navigation and Control, Springer Nature Singapore, 2025, pp. 495-504. https://doi.org/10.1007/978-981-96-2248-1\_48

