摘要
提出一种短弧段ETALON卫星的SLR数据处理策略,仅解算卫星轨道、测站距离偏差、地球自转参数,并利用2018-01~10数据进行验证。结果表明,ETALON-1/2卫星定轨残差RMS分别为1.11 cm、1.08 cm;与IERS-C04产品相比,短弧段数据解算的X_(p)、Y_(p)、LOD参数误差RMS分别为2.21 mas、2.26 mas、218.30μs/d;与ILRS事后最终轨道相比,ETALON-1卫星R、T、N方向轨道精度分别为1.6 cm、8.5 cm、6.8 cm,ETALON-2卫星R、T、N方向轨道精度分别为2.1 cm、8.9 cm、8.7 cm。
We propose a new strategy of SLR data short-arc analysis of ETALON satellites in this paper,which also solves satellite orbit parameters,earth rotation parameters and range bias parameters.The new strategy is verified using the data from January to October in 2018.The results show that:the root mean square of residuals for ETALON-1/2 satellites is 1.11cm and 1.08cm respectively;compared with IERS-C04 product,the precision of X_(p),Y_(p) and LOD parameters is 2.21 mas,2.26 mas and 218.30μs/d respectively;compared with the final orbit of ILRS,the orbit accuracy of ETALON-1 satellite in radial,track and normal direction is 1.6 cm,8.5 cm and 6.8 cm respectively,while that of ETALON-2 satellite is 2.1 cm,8.9 cm and 8.7 cm respectively.
作者
张小贞
卢晓春
孔垚
ZHANG Xiaozhen;LU Xiaochun;KONG Yao(National Time Service Center,CAS,Xi’an 710600,China;School of Astronomy and Space Science,University of Chinese Academy of Sciences,Beijing 100049,China;Key Laboratory of Precise Positioning and Timing Technology,CAS,Xi’an 710600,China;School of Electronics and Information,Xi’an Polytechnic University,Xi’an 710048,China)
出处
《大地测量与地球动力学》
CSCD
北大核心
2021年第10期1030-1034,共5页
Journal of Geodesy and Geodynamics
基金
转发式卫星导航试验系统项目(ZFS19001D)
陕西省自然科学基础研究计划(2021JQ-656)。