Integrated Navigation and Communication Service for LEO Satellites Based on BDS-3 Global Short Message Communication

被引:4
|
作者
Guo, Shuren [1 ]
Li, Gang [1 ]
Zheng, Jiaju [2 ]
Ren, Qianyi [2 ]
Wu, Yifan [2 ]
Shen, Guanhao [2 ]
Yue, Hengyi [3 ]
机构
[1] Beijing Inst Tracking & Telecommun Technol, Beijing 100094, Peoples R China
[2] Innovat Acad Microsatellites CAS, Shanghai 201304, Peoples R China
[3] Chinese Acad Sci, Shanghai Astron Observ, Shanghai 200030, Peoples R China
关键词
BDS-3; global short message communication; LEO satellites; orbit determination; communication;
D O I
10.1109/ACCESS.2023.3236670
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
Massive global Low Earth Orbit (LEO) constellations have been developed rapidly with the characteristics of larger number and shorter orbital periods of LEO satellites in recent years. The increasing requirements of real-time orbit determination and emergency data transfer in full arc can hardly meet the traditional strategies based on regional ground stations. An integrated communication and navigation service architecture based on the third phase of the BeiDou system (BDS-3) Global Short Message Communication (GSMC) is proposed, which enables global coverage and random access. The GSMC downlink single-frequency signal is used for real-time orbit determination, and is further combined with B1C navigation signal for real-time dual-frequency high-precision orbit determination. Considering fast moving of LEO satellites and short burst of uplink messages, the uplink BDS-3 satellite selection strategy based on carrier-to-noise ratio, and uplink high-precision compensation of frequency shift are adopted to increase the communication success rate. The service architecture proposed can improve the precision of the autonomous orbit determination and enhance the capability of real-time command transmission of LEO satellites even without the traditional ground stations involved. Integrated communication and navigation service has been validated by simulation and on-board BDS-3 GSMC test data. The precision of single-frequency real-time orbit determination can reach 2.86m, and the precision of dual-frequency can reach 0.26m. The average time delay of communication is about 11.45s, and the success rate is about 99.8%. The method may provide alternative means of real-time high-precision orbit determination and emergency data transfer of LEO satellites.
引用
收藏
页码:6623 / 6631
页数:9
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