1. A preliminary result for centralized autonomous orbit determination of gnss constellation and lunar satellite based on inter-satellite link measurements.
- Author
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Luo, Peng, Song, Ye-Zhi, Yang, Jianhua, Hu, Xiaogong, Tang, Chengpan, Li, Kai, and Wu, Qingfeng
- Abstract
The Inter-Satellite Link (ISL) technology plays a vital role in BeiDou Navigation Satellite System (BDS), and it's a developmental trend of the future GNSS. However, ISL is insensitive to both the Earth's rotation and the constellation's overall rotation, which has resulted in persistent overall constellation drift issues for autonomous navigation. Due to technical limitations, the current method for autonomous navigation requires adding ground anchor stations in order to connect the satellite constellation to Earth's surface, thereby minimizing the drift of constellation. Nevertheless, this approach is not a fully autonomous navigation as we expected. This paper proposes an autonomous navigation scheme based on ISL utilizing a lunar satellite as a spatial anchor point and leveraging lunar gravity to establish an inertial space direction reference for the satellite constellation. The feasibility and effectiveness of this scheme are validated through theoretical analysis and simulation experiments. After 120 days of precise orbit determination simulation, the accuracy of result is improved from 408.56 m to 7.78 m, which shows a 98% improvement for all GNSS orbit by adding a lunar satellite into ISL net. This improvement is primarily observed in terms of tangent and normal directions, which experience enhancements of 89.6% and 98.6%, respectively. Specifically, we achieve an improvement of approximately 89% in the accuracy of the inclination angle, around 99% in the right ascension of ascending node, and about 89% in the sum of the argument of perigee and mean anomaly. [ABSTRACT FROM AUTHOR]
- Published
- 2024
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