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Characteristics of BeiDou Navigation Satellite System Multipath and Its Mitigation Method Based on Kalman Filter and Rauch-Tung-Striebel Smoother

机译:基于卡尔曼滤波和Rauch-Tung-Striebel平滑器的北斗导航卫星系统多径特性及其缓解方法

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摘要

Global Navigation Satellite System (GNSS) carrier phase measurement for short baseline meets the requirements of deformation monitoring of large structures. However, the carrier phase multipath effect is the main error source with double difference (DD) processing. There are lots of methods to deal with the multipath errors of Global Position System (GPS) carrier phase data. The BeiDou navigation satellite System (BDS) multipath mitigation is still a research hotspot because the unique constellation design of BDS makes it different to mitigate multipath effects compared to GPS. Multipath error periodically repeats for its strong correlation to geometry of satellites, reflective surface and antenna which is also repetitive. We analyzed the characteristics of orbital periods of BDS satellites which are consistent with multipath repeat periods of corresponding satellites. The results show that the orbital periods and multipath periods for BDS geostationary earth orbit (GEO) and inclined geosynchronous orbit (IGSO) satellites are about one day but the periods of MEO satellites are about seven days. The Kalman filter (KF) and Rauch-Tung-Striebel Smoother (RTSS) was introduced to extract the multipath models from single difference (SD) residuals with traditional sidereal filter (SF). Wavelet filter and Empirical mode decomposition (EMD) were also used to mitigate multipath effects. The experimental results show that the three filters methods all have obvious effect on improvement of baseline accuracy and the performance of KT-RTSS method is slightly better than that of wavelet filter and EMD filter. The baseline vector accuracy on east, north and up (E, N, U) components with KF-RTSS method were improved by 62.8%, 63.6%, 62.5% on day of year 280 and 57.3%, 53.4%, 55.9% on day of year 281, respectively.
机译:用于短基线的全球导航卫星系统(GNSS)载波相位测量可满足大型结构变形监测的要求。但是,载波相位多径效应是采用双差(DD)处理的主要误差源。有很多方法可以处理全球定位系统(GPS)载波相位数据的多径误差。北斗导航卫星系统(BDS)多径缓解仍然是研究的热点,因为BDS的独特星座设计使其与GPS相比在缓解多径效应方面有所不同。由于多径误差与卫星,反射面和天线的几何形状具有很强的相关性,因此会定期重复出现,这也是重复性的。我们分析了BDS卫星的轨道周期特征,该特征与相应卫星的多径重复周期一致。结果表明,BDS对地静止地球轨道(GEO)和倾斜地球同步轨道(IGSO)卫星的轨道周期和多径周期约为1天,而MEO卫星的周期约为7天。引入了Kalman滤波器(KF)和Rauch-Tung-Striebel平滑器(RTSS),以使用传统恒星滤波器(SF)从单差(SD)残差中提取多路径模型。小波滤波器和经验模式分解(EMD)也用于减轻多径效应。实验结果表明,三种滤波方法对提高基线精度都有明显的效果,KT-RTSS方法的性能略好于小波滤波和EMD滤波。在280年的一天中,使用KF-RTSS方法在东,北和上(E,N,U)分量上的基线向量精度分别提高了62.8%,63.6%,62.5%和280天的57.3%,53.4%,55.9%分别是281年

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