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Orbital Filter Aiding of a High Sensitivity GPS Receiver for Lunar Missions

Farine, Pierre-Andr�; Capuano, Vincenzo; Botteron, Cyril; Blunt, Paul

Authors

Pierre-Andr� Farine

Vincenzo Capuano

Cyril Botteron



Abstract

Recent studies have shown that weak global navigation satellite system (GNSS) signals could potentially be used to navigate from Earth to the Moon. This would increase autonomy, robustness, and flexibility of the navigation architectures for future lunar missions. However, the utilization of GNSS signals at very high altitudes close to the Moon can be significantly limited by the very low power levels seen at the receiver's antenna. This can result in a strongly reduced visibility of the GNSS satellites, which can worsen the already poor relative geometry of the GNSS receiver to the GNSS satellites. Furthermore, during most of a Moon transfer orbit (MTO), the very weak GNSS signals are also affected by Doppler shifts and Doppler rates larger than the ones generally experienced on Earth, due to the much higher relative dynamics between the receiver and the transmitters. As a consequence, commercial GNSS receivers for terrestrial use cannot successfully acquire and track such signals. More advanced architectures and specific implementations are thus required to use GNSS for lunar missions. In this paper, we propose the use of an adaptive orbital filter to aid the GNSS acquisition and tracking modules and to strongly increase the achievable navigation accuracy. The paper describes the orbital filter architecture and tests results carried out by processing realistic radio frequency (RF) signals generated by our Spirent GSS 8000 full constellation simulator for a highly elliptical MTO.

Citation

Farine, P.-A., Capuano, V., Botteron, C., & Blunt, P. (2017). Orbital Filter Aiding of a High Sensitivity GPS Receiver for Lunar Missions. Navigation, 64(3), 323-338. https://doi.org/10.1002/navi.185

Journal Article Type Article
Acceptance Date Mar 23, 2017
Online Publication Date Jun 5, 2017
Publication Date 2017-10
Deposit Date Sep 30, 2020
Journal Navigation
Electronic ISSN 2161-4296
Publisher Wiley
Peer Reviewed Peer Reviewed
Volume 64
Issue 3
Pages 323-338
DOI https://doi.org/10.1002/navi.185
Public URL https://nottingham-repository.worktribe.com/output/3780870
Publisher URL https://onlinelibrary.wiley.com/doi/10.1002/navi.185
Additional Information Capuano, V., Blunt, P., Botteron, C., & Farine, P.-A. (2017). Orbital Filter Aiding of a High Sensitivity GPS Receiver for Lunar Missions. Navigation, 64(3), 323–338. https://doi.org/10.1002/navi.185