Precise orbit determination for low Earth orbit satellites using GNSS:Observations,models,and methods  

作　　者：Xinyuan Mao Wenbing Wang Yang Gao 

机构地区：[1]Technology and Engineering Center for Space Utilization,Chinese Academy of Sciences,Beijing,100094,China [2]University of Chinese Academy of Sciences,Beijing,101408,China

出　　处：《Astrodynamics》2024年第3期349-374,共26页航天动力学（英文）

基　　金：supported by the Strategic Priority Research Program of the Chinese Academy of Sciences(Grant Nos.XDA30010000 and XDA30010300).

摘　　要：Spaceborne global navigation satellite system(GNSS)has significantly revolutionized the development of autonomous orbit determination techniques for low Earth orbit satellites for decades.Using a state-of-the-art combination of GNSS observations and satellite dynamics,the absolute orbit determination for a single satellite reached a precision of 1 cm.Relative orbit determination(i.e.,precise baseline determination)for the dual satellites reached a precision of 1 mm.This paper reviews the recent advancements in GNSS products,observation processing,satellite gravitational and non-gravitational force modeling,and precise orbit determination methods.These key aspects have increased the precision of the orbit determination to fulfill the requirements of various scientific objectives.Finally,recommendations are made to further investigate multi-GNSS combinations,satellite high-fidelity geometric models,geometric offset calibration,and comprehensive orbit determination strategies for satellite constellations.

关 键 词：low Earth orbit(LEO) precise orbit determination(POD) precise baseline determination(PBD) global navigation satellite system(GNSS) multi-GNSS satellite constellation 

分 类 号：P22[天文地球—大地测量学与测量工程]