张宇, 段建锋, 孔静, 曹建峰, 韩意, 李翠兰, 宋辰, 陈明. 嫦娥五号双目标联合定轨技术研究[J]. 武汉大学学报 ( 信息科学版). DOI: 10.13203/j.whugis20210591
引用本文: 张宇, 段建锋, 孔静, 曹建峰, 韩意, 李翠兰, 宋辰, 陈明. 嫦娥五号双目标联合定轨技术研究[J]. 武汉大学学报 ( 信息科学版). DOI: 10.13203/j.whugis20210591
ZHANG Yu, DUAN Jianfeng, KONG Jing, CAO Jianfeng, HAN Yi, LI Cuilan, SONG Chen, CHEN Ming. Research on CE-5' Dual-target Joint Orbit Determination Technology[J]. Geomatics and Information Science of Wuhan University. DOI: 10.13203/j.whugis20210591
Citation: ZHANG Yu, DUAN Jianfeng, KONG Jing, CAO Jianfeng, HAN Yi, LI Cuilan, SONG Chen, CHEN Ming. Research on CE-5' Dual-target Joint Orbit Determination Technology[J]. Geomatics and Information Science of Wuhan University. DOI: 10.13203/j.whugis20210591

嫦娥五号双目标联合定轨技术研究

Research on CE-5' Dual-target Joint Orbit Determination Technology

  • Abstract: Based on CE-5' dual-target joint measurement, we established the same beam measurement and inter-satellite measurement model, and designed a statistical orbit determination algorithm combined with orbiter and ascender. We used the reference orbit to analyze delay and delay rate accuracy of the same beam measurement, and the range and range data accuracy of microwave radar/laser radar. The accuracy of the same beam measurement is equivalent to that of VLBI measurement, and the range accuracy of microwave radar/laser radar is at meter level. By establishing the relative motion relationship between the two targets, the relative orbit accuracy can be significantly improved in orbit determination.

     

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