基于RINEX4.0广播ERP参数的BDS星历误差实时补偿方法

Real-time compensation method for BDS ephemeris errors based on RINEX 4.0 broadcast earth rotation parameters

  • 摘要: 地球自转参数(earth rotation parameters,ERP)不仅对于地球参考框架的维持至关重要,而且对于卫星的精密轨道确定也具有重要意义. 2021年12月,国际GNSS服务组织(International GNSS Service,IGS)发布了接收机独立交换(Receiver Independent Exchange,RINEX)4.00协议,首次在广播星历中包含了ERP参数. 本文利用RINEX4.00格式的广播ERP,对星历误差进行补偿,提取2022—2023年的广播星历文件中的ERP数据记录,评估了GPS和北斗三号全球卫星导航系统(BeiDou-3 Navigation Satellite System,BDS-3)广播ERP的精度. 针对重复和异常ERP提出了一种行之有效的数据编辑方法,并且采用IERS C04产品作为参考基准评估GPS和BDS-3广播ERP的精度:GPS广播ERP极移参数 x_p y_p与日长变化参数\Delta _\textUT1相对于C04差值的均方根(root mean square,RMS)分别为2.309 mas、1.433 mas~0.303 ms,而BDS-3的广播ERP相对于C04差值的RMS分别为2.769 mas、1.748 mas和0.372 ms,后者与前者相比3个参数的差值RMS增大19.9%、22.0%、22.8%,精度较低. 在此基础上,本文研究了广播ERP误差与轨道旋转参数的相关性,并且设计了一种利用GPS广播ERP的BDS-3星历误差实时补偿方案. 实验表明,该方案能够达到最终解C04产品补偿效果的40%~60%.

     

    Abstract: Earth rotation parameters (ERP) are crucial for maintaining the Earth reference frame and have significant importance for precise satellite orbit determination. In December 2021, the International GNSS Service (IGS) released the Receiver Independent Exchange (RINEX) version 4.00 protocol, which for the first time included ERP in the broadcast ephemeris. This study utilizes the broadcast ERP from the RINEX 4.00 format to compensate for ephemeris errors. We extract ERP data records from broadcast ephemeris files from 2022 to 2023 to assess the accuracy of GPS and BDS-3 broadcast ERP. An effective data editing method is proposed to address duplicate and anomalous ERP, and the accuracy of GPS and BDS-3 broadcast ERP is evaluated using the IERS C04 product as a reference. The root mean square (RMS) of differences between the GPS broadcast ERP parameters and the C04 product were 2.309 mas for the polar motion parameters and 0.303 ms for the length of day parameter, while the RMS of differences for the BDS-3 broadcast ERP are 2.769 mas, 1.748 mas, and 0.372 ms, respectively. Compared to GPS, the RMS differences for the three BDS-3 parameters increase by 19.9%, 22.0%, and 22.8%, indicating lower accuracy. Based on this, the correlation between broadcast ERP errors and orbital rotation parameters is studied, and a real-time compensation scheme for BDS-3 ephemeris errors using GPS broadcast ERP is designed. Experiments show that this scheme can achieve 40%~60% of the compensation effect of the final IERS C04 product.

     

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