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SUPPORTING THE COPERNICUS POD SERVICE

机译:支持哥白尼POD服务

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The Copernicus POD (Precise Orbit Determination) Service is part of the Copernicus PDGS (Payload Data Ground Segment) of the Sentinel missions. A GMV-led consortium is operating the Copernicus POD Service being in charge of generating precise orbital products and auxiliary data files for their use as part of the processing chains of the respective Sentinel PDGS. As part of the consortium PosiTim is responsible for implementing and testing software and model updates thoroughly before integrating them in the operational chain of the Copernicus POD Service.rnThe NAPEOS (Navigation Package for Earth Observation Satellites) software is used for the generation of the orbit products within the Copernicus POD Service.rnThe test procedures and results obtained for a recent software and model update to IERS 2010 Conventions are presented. It has been tested as well that the arc length of 72 hours for the non-time critical (NTC) orbit solutions might be shorten to 48 hours without losing accuracy. Orbit comparisons to external solutions help to validate the different orbit solutions.rnGPS antenna phase centre variations (PCVs) are one of the largest systematic error sources in POD. Since the satellite body may cause signal multipath a ground calibration of the GPS antenna without taking into account the satellite body might not be sufficient to quantify the PCVs. The PCVs are therefore obtained by an in-flight calibration.rnA first map for the PCVs determined from a limited amount of data at the beginning of the mission has shown significant multipath signals in parts of the antenna for code and carrier phase measurements. Since the satellite has moving parts it has been checked carefully if these multipath regions are moving as well or if they are antenna-fixed.rnNormally the correction maps are only applied for the carrier phase measurements. Since significant multipath has been spotted for the code measurements as well investigations are performed to study the impact of additionally applying code correction maps in the POD process.
机译:哥白尼POD(精确轨道确定)服务是前哨任务的哥白尼PDGS(有效载荷数据地面部分)的一部分。由GMV领导的财团正在运营哥白尼POD服务,该服务负责生成精确的轨道产品和辅助数据文件,以将其用作各个Sentinel PDGS的处理链。作为财团的一部分,PosiTim负责彻底实施和测试软件及模型更新,然后再将其集成到Copernicus POD服务的运营链中。rnNAPEOS(地球观测卫星导航软件包)软件用于生成轨道产品在Copernicus POD服务中提供。rn介绍了针对IERS 2010公约的最新软件和模型更新所获得的测试程序和结果。还已经测试过,非时间关键(NTC)轨道解决方案的72小时弧长可以缩短到48小时而不会损失准确性。与外部解决方案的轨道比较有助于验证不同的轨道解决方案。GPS天线相位中心变化量(PCV)是POD中最大的系统误差源之一。由于卫星主体可能导致信号多径,因此在不考虑卫星主体的情况下对GPS天线进行地面校准可能不足以量化PCV。因此,PCV是通过飞行中的校准获得的。在任务开始时从数量有限的数据确定的PCV的第一张图显示,在天线的某些部分中存在明显的多径信号,用于代码和载波相位测量。由于卫星具有运动部件,因此已经仔细检查了这些多径区域是否也在运动或它们是否是天线固定的。通常,校正图仅用于载波相位测量。由于已经发现重要的多径用于代码测量,因此也进行了研究以研究在POD过程中额外应用代码校正图的影响。

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  • 来源
  • 会议地点 Venice(IT)
  • 作者单位

    PosiTim UG, In den Löser 15, 64342 Seeheim-Jugenheim, Germany, Email:heike.peter@positim.com;

    PosiTim UG, In den Löser 15, 64342 Seeheim-Jugenheim, Germany;

    PosiTim UG, In den Löser 15, 64342 Seeheim-Jugenheim, Germany;

    GMV AD., Isaac Newton 11, 28760 Tres Cantos, Spain, Email:jfernandez@gmv.com;

    GMV AD., Isaac Newton 11, 28760 Tres Cantos, Spain;

    ESA/ESRIN, Via Galileo Galilei, I-00044 Frascati, Italy, Email:pierre.femenias@esa.int;

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