低成本GNSS接收机观测值噪声水平评估

Assessment of observation noise levels of low-cost GNSS receivers

  • 摘要: 针对现有研究中对国产低成本多频接收机观测噪声分析不足的问题,引入零基线双差残差恢复单差残差的处理方法,详细分析了基于UM960模组的低成本接收机不同观测信号随高度角变化特性,并对其伪距、载波相位噪声水平进行评估. 结果表明:北斗卫星导航系统(BeiDou Navigation Satellite System, BDS)卫星噪声水平整体上优于GPS,在伪距观测值中体现更为明显. 具体来看,BDS各频点伪距观测值噪声处于厘米级,其中B2a频点噪声最小,为1.49 cm;B2I、B1C、B3I、B1I频点噪声依次增大,最大值为2.87 cm. 对于BDS载波观测值,B1I频点噪声水平为0.24 mm,B2I、B1C频点与其相当,B2a和B3I频点略高,分别为0.37 mm和0.62 mm,总体控制在亚毫米级. 此外,不同轨道类型卫星的观测噪声亦有显著区别,中地球轨道(medium Earth orbit, MEO)卫星和倾斜地球同步轨道(inclined geosynchronous orbit,IGSO)卫星在各频点下的观测噪声水平较为接近,而地球静止轨道(geostationary Earth orbit,GEO)卫星观测值噪声普遍高于前两者. 对于GPS,各频点间伪距观测噪声差异较大,其中L2噪声为9.40 cm,约为L5的6倍;载波观测噪声相对接近,在L1、L2、L5中依次为0.31 mm、0.75 mm、0.35 mm. 该类接收机观测性能和传统测量型接收机基本一致,可满足各类导航定位的应用需求.

     

    Abstract: To address the limited analysis of observation noise in domestically developed low-cost multi-frequency GNSS receivers, this study introduces a zero-baseline double-differencing approach to recover single-differenced residuals. The elevation-dependent behavior of signals from a UM960-based receiver is examined, and the pseudorange and carrier phase noise characteristics are evaluated. Results indicate that the BeiDou Navigation Satellite System (BDS) exhibits lower overall satellite observation noise than the GPS, with the difference being more pronounced in pseudorange measurements. Specifically, BDS pseudorange noise remains at the centimeter level across all frequencies, with B2a the lowest at 1.49 cm, rising through B2I, B1C, and B3I, and reaching a maximum on B1I at 2.87 cm. Carrier phase noise remains within the sub-millimeter range, with B1I at 0.24 mm, B2I and B1C at similar levels, and B2a and B3I slightly higher at 0.37 mm and 0.62 mm, respectively. Noise levels also vary by orbit type, with medium Earth orbit (MEO) and inclined geosynchronous orbit (IGSO) satellites performing similarly and GEO satellites exhibiting higher noise. For GPS, pseudorange noise differs significantly across frequencies, with L2 reaching 9.40 cm, approximately six times that of L5, while carrier phase noise remains relatively stable at 0.31 mm, 0.75 mm, and 0.35 mm for L1, L2, and L5, respectively. The results demonstrate that the receiver achieves observation performance comparable to geodetic-grade equipment, meeting the requirements of typical navigation and positioning applications.

     

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