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Impact of GPS receiver antenna GRAPHIC residual variations on single-frequency orbit determination of LEO satellites

机译:GPS接收机天线GRAPHIC残差对LEO卫星单频轨道确定的影响

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Single-frequency (SF) precise orbit determination (POD) using space-borne Global Positioning System (GPS) measurements is a prerequisite for the success of many low-cost small/micro low Earth orbit (LEO) satellite missions. The first-order ionospheric effects are usually eliminated by group and phase ionospheric correction (GRAPHIC) combinations. GPS receiver antenna GRAPHIC residual variations (GRVs) are important systematic error sources in SF orbit determination. Azimuth and elevation dependent GRVs are estimated and obtained based on the GRAPHIC combination residuals in an in-flight calibration. One month of data from GRACE-A, GRACE-B, CHAMP and HY-2A satellites is used to assess the potential of receiver antenna GRVs in SF orbit determination. It is the first time to study the impact of receiver antenna GRVs on SF orbit determination for different LEO satellites, which exhibit different altitudes and data qualities. The impact of receiver antenna GRVs on SF orbit determination is significant. The use of in-flight determined receiver antenna GRVs leads to a better consistency between SF and dual-frequency POD solutions. The improvements are more obvious for GRACE-A and CHAMP satellites, whose receiver antenna GRV patterns demonstrate clear characteristics of systematic deviations. After correcting the receiver antenna GRVs, the root-mean-square of satellite laser ranging validation residuals are 3.11 cm, 2.31 cm, 2.86 cm and 5.29 cm for GRACE-A, GRACE-B, CHAMP and HY-2A satellites, respectively, which are reduced by 11.1%, 4.6%, 14.6% and 4.7%, respectively. At last, a set of a priori GDV corrections of GPS transmitter antennas are used in SF orbit determination and its effects on receiver antenna GRVs estimation and SF orbit determination are analyzed. Applying these corrections can slightly improve the SF orbit quality of GRACE-A satellite. (C) 2019 Published by Elsevier Ltd on behalf of COSPAR.
机译:使用星载全球定位系统(GPS)测量的单频(SF)精确轨道确定(POD)是许多低成本小/微低地球轨道(LEO)卫星任务成功的先决条件。通常通过组和相位电离层校正(GRAPHIC)组合消除一阶电离层效应。 GPS接收机天线GRAPHIC残差(GRV)是确定SF轨道的重要系统误差源。在飞行中校准时,将根据GRAPHIC组合残差估算和获得与方位角和仰角相关的GRV。来自GRACE-A,GRACE-B,CHAMP和HY-2A卫星的一个月数据用于评估接收机天线GRV在SF轨道确定中的潜力。这是第一次研究接收机天线GRV对不同LEO卫星的SF轨道确定的影响,这些卫星表现出不同的高度和数据质量。接收机天线GRV对SF轨道确定的影响很大。使用机载确定的接收器天线GRV可以在SF和双频POD解决方案之间实现更好的一致性。对于GRACE-A和CHAMP卫星,其改进更为明显,它们的接收器天线GRV模式显示出明显的系统偏差特征。校正接收器天线GRV之后,对于GRACE-A,GRACE-B,CHAMP和HY-2A卫星,卫星激光测距确认残差的均方根分别为3.11 cm,2.31 cm,2.86 cm和5.29 cm,分别为分别减少了11.1%,4.6%,14.6%和4.7%。最后,将一组GPS发射机天线的先验GDV校正用于SF轨道确定,并分析其对接收机天线GRVs估计和SF轨道确定的影响。应用这些校正可以略微改善GRACE-A卫星的SF轨道质量。 (C)2019由Elsevier Ltd代表COSPAR发布。

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