EventsEuropean Navigation Conference 2025
Published
This submission belongs to the session 6. Future Trends in Navigation of the event European Navigation Conference 2025
Published date
03 Oct, 2025
Academic Editor
author-avatarTomasz Hadas
Citation
Yoann AUDET, Michele Ceresoli, Floor Thomas Melman, Dimitrios V. Psychas, Richard Swinden, Cosimo Stallo, Javier Venturat-Traveset, Assessment of lunar users’ PVT performances tightly coupling Moonlight signal with IMU, in Proceedings of European Navigation Conference 2025, Wrocław, 21 May–23 May 2025, MDPI: Basel, Switzerland
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Assessment of lunar users’ PVT performances tightly coupling Moonlight signal with IMU

Floor Thomas Melman 3
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Cosimo Stallo 3
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1. ESA, The Netherlands
2. Department of Aerospace Science and Technology, Politecnico di Milano, Via La Masa 34, 20156 Milan, Italy, Italy
3. European Space Agency, The Netherlands
Abstract

Abstract:
The increasing interest in the Moon, highlighted by the rapidly growing number of planned lunar missions for the next decade, presents a significant challenge for ensuring reliable communications and navigation. Space agencies worldwide are developing communication and navigation constellations to provide services that enable missions to achieve their objectives. To support its exploration vision, the European space agencies have proposed the Moonlight program to develop a constellation for navigation and communication. This initiative is part of a global effort to create interoperable systems under the LunaNet framework [1].
In this contribution, the performances of the 4 satellites Moonlight constellation will be updated compared to previous works [2], [3], by presenting results assuming the user is equipped with an IMU. This study will first present a high-fidelity modelling of the IMU sensor and of its errors (such as noise and bias terms, scale factors, non-orthogonality and quantization) as well as its integration within the navigation filter. The analyses will then focus on two scenarios, one involving a moving surface rover and the second one on a lunar landing trajectory. Sensitivity analyses to assess the impact of the IMU grade on the user positioning performances will also be performed. Finally, a test case scenario involving IMU measurements faults will be analysed to assess the reliability enhancements that the additional Moonlight measurements can provide to the navigation filter and whether their usage can successfully prevent catastrophic failures such as those of the Mars Schiaparelli probe.
Bibliography:
[1] NASA; ESA; JAXA, “Draft 5 LunaNet Interoperability Specifications,” 2025.
[2] Y. Audet, F. T. Melman, D. V Psychas, R. D. Swinden, and J. Ventura-Traveset, “Positioning of a Lunar Lander using a dedicated Lunar Communication and Navigation System assuming realistic ODTS performances,” 2023. doi: 10.3390/0.
[3] Y. Audet et al., “Positioning of a lunar surface rover on the south pole using LCNS and DEMs,” Advances in Space Research, vol. 74, no. 6, pp. 2532–2550, Sep. 2024, doi: 10.1016/j.asr.2024.06.022.

Keywords
Moonlight
LunarPNT
IMU
Lander
Experimentation of an integrated Vision-aided Inertial Navigation System with Orthophoto matching on a fixed-wing UAV
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