High Precision Spacecraft Landing on the Moon Through Lunar Satellite Navigation Systems and Local Ultra-Wideband Positioning Network

NASA and ESA have recently initiated Lunar Navigation Satellite System (LNSS) development programs to support upcoming lunar exploration missions. Unlike terrestrial Global Navigation Satellite Systems (GNSS), LNSS positioning accuracy is expected to be limited to several tens of meters due to constraints in monitoring and control infrastructure. This study explores a hybrid positioning approach that combines LNSS and an Ultra-Wideband (UWB) network to enhance precision landing for spacecraft on the Moon. We considered recently proposed LNSS constellations and operational concepts, along with a UWB network optimized for lunar surface operations using an in-house genetic algorithm. The UWB network layout was designed based on RF signal propagation characteristics and landing-phase accuracy requirements. To mitigate the positional uncertainty of rover antennas, which can reach several tens of meters with LNSS alone, we implemented a cooperative positioning (CP) technique that integrates LNSS and UWB-based inter-rover ranging, along with a post-process filtering method to further refine the estimated positions. This approach reduced rover antenna positioning errors to 5 meters or less (RMS). Simulation results confirm that the optimized UWB network, when integrated with LNSS and an altimeter, significantly improves spacecraft positioning accuracy, maintaining consistent performance regardless of LNSS constellation geometry and ensuring sufficient horizontal positioning accuracy up to 150 m altitude along the landing trajectory.

Authors

Publication Details

Journal
Proceedings of the Institute of Navigation ... International Technical Meeting/Proceedings of the ... International Technical Meeting of The Institute of Navigation
Published
2025-02-13
DOI
https://doi.org/10.33012/2025.19986
Citations
1
Primary Topic
Spacecraft Design and Technology
Type
article
Field-Weighted Citation Impact
4.99
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article

High Precision Spacecraft Landing on the Moon Through Lunar Satellite Navigation Systems and Local Ultra-Wideband Positioning Network

Euiho Kim, Dong-Ho Jung
1 citations
Proceedings of the Institute of Navigation ... International Technical Meeting/Proceedings of the ... International Technical Meeting of The Institute of Navigation
Spacecraft Design and Technology
4.99
article

High Precision Spacecraft Landing on the Moon Through Lunar Satellite Navigation Systems and Local Ultra-Wideband Positioning Network

Euiho Kim, Dong-Ho Jung
article en
1 citations

Abstract

NASA and ESA have recently initiated Lunar Navigation Satellite System (LNSS) development programs to support upcoming lunar exploration missions. Unlike terrestrial Global Navigation Satellite Systems (GNSS), LNSS positioning accuracy is expected to be limited to several tens of meters due to constraints in monitoring and control infrastructure. This study explores a hybrid positioning approach that combines LNSS and an Ultra-Wideband (UWB) network to enhance precision landing for spacecraft on the Moon. We considered recently proposed LNSS constellations and operational concepts, along with a UWB network optimized for lunar surface operations using an in-house genetic algorithm. The UWB network layout was designed based on RF signal propagation characteristics and landing-phase accuracy requirements. To mitigate the positional uncertainty of rover antennas, which can reach several tens of meters with LNSS alone, we implemented a cooperative positioning (CP) technique that integrates LNSS and UWB-based inter-rover ranging, along with a post-process filtering method to further refine the estimated positions. This approach reduced rover antenna positioning errors to 5 meters or less (RMS). Simulation results confirm that the optimized UWB network, when integrated with LNSS and an altimeter, significantly improves spacecraft positioning accuracy, maintaining consistent performance regardless of LNSS constellation geometry and ensuring sufficient horizontal positioning accuracy up to 150 m altitude along the landing trajectory.

Proceedings of the Institute of Navigation ... International Technical Meeting/Proceedings of the ... International Technical Meeting of The Institute of Navigation
Openalex Percentile: Top 7%
Spacecraft Design and Technology
4.99
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High Precision Spacecraft Landing on the Moon Through Lunar Satellite Navigation Systems and Local Ultra-Wideband Positioning Network — Euiho Kim, Dong-Ho Jung · Proceedings of the Institute of Navigation ... International Technical Meeting/Proceedings of the ... International Technical Meeting of The Institute of Navigation (2025) | TGRS Research Map | TGRS