北斗全球卫星导航系统试验卫星测距信号质量分析

许扬胤, 杨元喜, 何海波, 李金龙, 唐斌, 章林锋

许扬胤, 杨元喜, 何海波, 李金龙, 唐斌, 章林锋. 北斗全球卫星导航系统试验卫星测距信号质量分析[J]. 武汉大学学报 ( 信息科学版), 2018, 43(8): 1214-1221. DOI: 10.13203/j.whugis20160219
引用本文: 许扬胤, 杨元喜, 何海波, 李金龙, 唐斌, 章林锋. 北斗全球卫星导航系统试验卫星测距信号质量分析[J]. 武汉大学学报 ( 信息科学版), 2018, 43(8): 1214-1221. DOI: 10.13203/j.whugis20160219
XU Yangyin, YANG Yuanxi, HE Haibo, LI Jinlong, TANG Bin, ZHANG Linfeng. Quality Analysis of the Range Measurement Signals of Test Satellites in BeiDou Global System[J]. Geomatics and Information Science of Wuhan University, 2018, 43(8): 1214-1221. DOI: 10.13203/j.whugis20160219
Citation: XU Yangyin, YANG Yuanxi, HE Haibo, LI Jinlong, TANG Bin, ZHANG Linfeng. Quality Analysis of the Range Measurement Signals of Test Satellites in BeiDou Global System[J]. Geomatics and Information Science of Wuhan University, 2018, 43(8): 1214-1221. DOI: 10.13203/j.whugis20160219

北斗全球卫星导航系统试验卫星测距信号质量分析

基金项目: 

国家重点研发计划 2016YFB0501700

国家重点研发计划 2016YFB0501701

国家自然科学基金 41374019

国家自然科学基金 41474015

详细信息
    作者简介:

    许扬胤, 博士生, 主要从事GNSS多频实时精密定位理论与算法研究。xu_yangyin@163.com

  • 中图分类号: P228

Quality Analysis of the Range Measurement Signals of Test Satellites in BeiDou Global System

Funds: 

The National Key R&D Program 2016YFB0501700

The National Key R&D Program 2016YFB0501701

the National Natural Science Foundation of China 41374019

the National Natural Science Foundation of China 41474015

More Information
    Author Bio:

    XU Yangyin, PhD candidate, specializes in the theory and algorithm of GNSS real-time precise positioning. E-mail:xu_yangyin@163.com

  • 摘要: 目前,北斗全球卫星导航系统有5颗试验卫星发射试验信号。试验卫星数据质量分析是北斗全球系统信号体制验证的重要内容。基于单测站北斗试验卫星观测数据,采用伪距相位差组合和伪距多径组合方法,初步分析了试验卫星民用信号以及Bs频点信号伪距测量噪声和多径误差。结果表明,倾斜同步轨道卫星伪距测量精度优于中轨道卫星;在各导航信号中,B2a+b信号伪距测量精度最高,具有最优的抗多径性能;B1C信号伪距测量精度最低,抗多径性能最差;Bs信号伪距测量精度较差,但优于B1C信号,且其伪距多径存在一个与高度角相关的系统误差,在高度角最大时可达0.5 m。
    Abstract: Currently, there are five testing satellites of BeiDou Global Satellite Navigation System broadcasting new signals. Quality analysis of testing satellite observations is a significant content for the verification of the new signal system. Based on single station measurement of BeiDou testing satellites, the code minus phase combination (CC) and multipath combination (MP) are employed to analyze the code noise and multipath errors of civil signals and Bs signal of the test satellites. The result shows that the pseudorange measurement accuracy of inclined geosynchronous satellite orbit (IGSO) satellite is better than that of the medium earth orbit (MEO) satellite; B2a+b signal has the highest pseudorange measurement accuracy as well as the best anti-multipath performance, while the B1C signal performs the worst in both aspects; the pseudorange measurement accuracy of Bs signal is rela-tively poor, yet better than that of the B1C signal and a systematic error related to elevation exists in the code multipath series of Bs signal with its maximum value up to 0.5 meter.
  • 图  1   信噪比随高度角变化情况

    Figure  1.   Carrier-to-Noise Density as a Function of Elevation Angle

    图  2   伪距噪声RMS值随高度角变化情况

    Figure  2.   RMS of Code Noise as a Function of Elevation Angle

    图  3   I2-S和M1-S卫星全球系统信号MP时间序列

    Figure  3.   MP Time Series of New Signals of I2-S and M1-S Satellites

    图  4   二号一期和试验卫星IGSO卫星B1I和B3I信号MP时间序列对比图

    Figure  4.   MP Time Series of B1I and B3I Signals of Testing and Compass II IGSO Satellites

    图  5   二号一期和试验卫星MEO卫星B1I和B3I信号MP时间序列对比图

    Figure  5.   MP Time Series of B1I and B3I Signals of Testing and Compass II MEO Satellites

    图  6   Bs频点伪距多径误差随高度角变化情况

    Figure  6.   Code Multipath Error as a Function of Elevation Angle of Bs Signal

    图  7   伪距多径RMS值随高度角变化情况

    Figure  7.   RMS of Code Multipath and Noise as a Function of Elevation Angle

    图  8   试验卫星伪距多径RMS

    Figure  8.   RMS of Code Multipath of Testing Satellites

    图  9   B1I和B3I信号伪距多径RMS

    Figure  9.   RMS of Code Multipath of B1I and B3I Signals

    表  1   本文所分析试验卫星信号

    Table  1   Signals of Test Satellites Analyzed in This Contribution

    卫星 卫星类型 信号
    I1-S IGSO B1I、B3I
    I2-S IGSO B1I、B1C、B2a、B2b、B2a+b、B3I、Bs
    M1-S MEO B1I、B1C、B2a、B2b、B2a+b、B3I、Bs
    M2-S MEO B1I、B1C、B2a、B2b、B2a+b、B3I
    下载: 导出CSV

    表  2   各试验卫星伪距噪声RMS/ m

    Table  2   RMS of Code Noise of Test Satellites/ m

    卫星 B1 B2 B3 Bs
    B1I B1C B2a B2b B2a+b B3I B3C
    I1-S 0.10 0.06
    I2-S 0.10 0.18 0.11 0.06 0.03 0.05 0.12
    M1-S 0.23 0.28 0.20 0.19 0.07 0.20 0.26
    M2-S 0.23 0.29 0.22 0.19 0.07 0.21
    下载: 导出CSV
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  • 收稿日期:  2016-11-16
  • 发布日期:  2018-08-04

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