Autonomous and Earth-Independent Orbit Determination for a Lunar Navigation Satellite System

In recent years, the number of expected missions to the Moon has increased significantly. With limited terrestrial-based infrastructure to support this number of missions, as well as restricted visibility over intended mission areas, there is a need for space navigation system autonomy. Autonomous o...

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Bibliographic Details
Published in:Aerospace 2024-02, Vol.11 (2), p.153
Main Authors: Critchley-Marrows, Joshua J. R., Wu, Xiaofeng, Kawabata, Yosuke, Nakasuka, Shinichi
Format: Article
Language:English
Subjects:
Artificial satellites
Autonomous navigation
Autonomy
Communication
Communications equipment
Electronics in navigation
Formation flying
Global navigation satellite system
guidance
Infrastructure
Intersatellite communications
lunar
Lunar environments
Moon
navigation
Navigation satellites
Navigation systems
Onboard equipment
Orbit determination
Orbital mechanics
Orbits
PNT
Satellite communications
Satellite observation
Satellites
Sensors
Space missions
Space navigation
Visibility
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Summary:In recent years, the number of expected missions to the Moon has increased significantly. With limited terrestrial-based infrastructure to support this number of missions, as well as restricted visibility over intended mission areas, there is a need for space navigation system autonomy. Autonomous on-board navigation systems in the lunar environment have been the subject of study by a number of authors. Suggested systems include optical navigation, high-sensitivity Global Navigation Satellite System (GNSS) receivers, and navigation-linked formation flying. This paper studies the interoperable nature and fusion of proposed autonomous navigation systems that are independent of Earth infrastructure, given challenges in distance and visibility. This capability is critically important for safe and resilient mission architectures. The proposed elliptical frozen orbits of lunar navigation satellite systems will be of special interest, investigating the derivation of orbit determination by non-terrestrial sources utilizing celestial observations and inter-satellite links. Potential orbit determination performances around 100 m are demonstrated, highlighting the potential of the approach for future lunar navigation infrastructure.
ISSN:2226-4310
2226-4310
DOI:10.3390/aerospace11020153