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广播星历下多系统卫星位置、速度计算及精度分析 总被引：1，自引：0，他引：1
目前GNSS空间部分主要由GPS、GLONASS、Galileo、BDS 4系统构成,在利用广播星历进行多星组合导航时,需要根据不同卫星星座广播星历精度信息实现多系统定位信息的组合。现有研究对GPS、GLONASS广播星历精度进行了充分分析,但对由Galileo、BDS广播星历计算卫星位置、速度及其精度的研究相对较少。本文利用精密星历对GNSS广播星历计算的卫星位置、速度精度进行了分析。结果表明,GPS广播星历解算的卫星位置误差小于2 m,GLONASS广播星历解算的卫星位置误差最大在4 m左右,Galileo广播星历解算的卫星位置误差最大在3 m左右,BDS广播星历解算的GEO卫星位置误差最大在40 m左右,IGSO卫星位置误差最大在9 m左右,MEO卫星位置误差最大在5 m左右。GPS、Galileo、BDS速度误差在1 mm/s内,GLONASS速度误差在2 mm/s内。 相似文献
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可见卫星数是评价导航系统定位性能的一个重要指标,也是系统可用性的基本要求。均方根差(亦称中误差)是观测精度的数据标准。本文通过实验分析了不同环境下的多系统组合的可见星数以及中误差,进而研究了多系统组合在不同环境中的可用性及定位精度。实验结果表明:在相同环境下,系统组合的可用性大幅提高,精度高于单GPS系统的精度,其中GPS/BDS/GLONASS三系统组合测量精度最高,GPS/BDS组合精度次之,GPS/GLONASS组合精度略低于GPS/BDS组合。 相似文献
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GLONASS卫星位置解算是GLONASS接收机定位解算的重要步骤,要求算法的精度高、运算量小、稳定性好。介绍了一种求解GLONASS导航卫星位置的新方法——基于Cowell预测校正积分的GLONASS卫星位置计算方法。采用实际数据对该算法和四阶龙格-库塔算法进行了对比验证。结果表明,该方法是一种高效的GLONASS卫星位置解算方法,其稳定度优于四阶龙格-库塔算法,且计算量小。 相似文献
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准天顶卫星系统目前利用QZS-2~QZS-43颗卫星播发L6E信号,为东亚和大洋洲地区用户提供实时的增强服务。该文分析了L6E信号结构及轨道和钟差的计算模型,研究了目前L6E信号的覆盖范围和可用性,评估了L6E改正数恢复的卫星轨道和钟差及其用于动态PPP的精度水平。结果表明:我国用户在使用15°截止高度角时L6E信号仍有100%的可用性;L6E改正数恢复的GPS和GLONASS卫星轨道的3D RMS平均值分别为5.3和13.9 cm,卫星钟差的STD平均值分别为0.14和0.22 ns,利用GPS卫星的轨道和钟差进行的动态PPP可以获得水平优于10 cm、高程优于15 cm的精度,在加入GLONASS卫星后,东方向和高程方向定位误差和收敛时间均有明显改善。 相似文献
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分析了GLONASS广播星历的用户算法,指出由于星历参数表示及用户算法的不完善对轨道拟合精度带来损失;分析了用户算法的误差源,并对其大小进行了计算.结果显示,在利用GLONASS广播星历采用数值积分时,由于模型的简化卫星位置计算的精度损失可达0.5 m. 相似文献
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GLONASS广播星历用户算法精度分析 总被引：2，自引：0，他引：2
分析了GLONASS广播星历的用户算法，指出由于星历参数表示及用户算法的不完善对轨道拟合精度带来损失；分析了用户算法的误差源，并对其大小进行了计算。结果显示，在利用GLONASS广播星历采用数值积分时，由于模型的简化卫星位置计算的精度损失可达0．5m。 相似文献
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相比于单一卫星导航系统,多卫星导航系统组合具有显著增加可用卫星数目、改善卫星空间几何结构等优点,因而多卫星导航系统组合应用成为近年来关注的热点。在复杂观测条件下,利用BDS/GPS/GLONASS组合进行载体姿态测量具有单系统无法比拟的优势。首先阐述了BDS/GPS/GLONASS组合超短基线解算的双差模型以及姿态测量基本原理;然后分析了BDS/GPS/GLONASS组合多频单历元姿态测量性能。通过实测静态数据设置不同高度截止角进行分析表明:相比于单系统及双系统组合的姿态测量,BDS/GPS/GLONASS组合能够有效地提高姿态测量的精度、稳定性和可用性。当运动载体处于高楼、峡谷等受遮挡严重的复杂环境时,BDS/GPS/GLONASS组合单历元姿态测量更具有应用价值。 相似文献
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GPS Solutions - A theoretical performance analysis of Kalman Filters for Global Navigation Satellite System GNSS-based space vehicle position estimation in varying Position Dilution of Precision... 相似文献
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A combination of GPS and GLONASS observations can offer improved reliability, availability and accuracy for precise point positioning (PPP). We present and analyze a combined GPS/GLONASS PPP model, including both functional and stochastic components. Numerical comparison and analysis are conducted with respect to PPP based on only GPS or GLONASS observations to demonstrate the benefits of the combined GPS/GLONASS PPP. The observation residuals are analyzed for more appropriate stochastic modeling for observations from different navigation systems. An analysis is also made using different precise orbit and clock products. The performance of the combined GPS/GLONASS PPP is assessed using both static and kinematic data. The results indicate that the convergence time can be significantly reduced with the addition of GLONASS data. The positioning accuracy, however, is not significantly improved by adding GLONASS data if there is a sufficient number of GPS satellites with good geometry. 相似文献
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By the beginning of 1996 the Russian Global Navigation Satellite System (GLONASS) constellation was completely deployed,
although several satellites have already been decommissioned since then. With 17 satellites in operation (status as of 21
December 1997, although two of them are unusable and one is a non-operative spare), GLONASS is now an alternative and a complement
to GPS. We present an evaluation of the current status of the GLONASS system, paying particular attention to its possible
geodetic applications. Data from several receivers were used for this evaluation, including data from GPS receivers in order
to allow for a comparison between GLONASS and GPS. We tested the quality of the geodetic observables, the consistency of the
broadcast orbits, the single-point positioning results, and we also looked at multipath errors and cycle slips in our GLONASS
data. In general the GLONASS performance has been found to be very satisfactory, even better than GPS in aspects such as single-receiver
positioning or in the quality of the second-frequency pseudo-ranges due to the degradation of the GPS measurement quality
under selective availability and anti-spoofing.
Received: 26 November 1996 / Accepted: 16 January 1998 相似文献
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基于DREAMNET的GPS/BDS/GLONASS多系统网络RTK定位性能分析 总被引：1，自引：1，他引：0
随着BDS系统完成亚太地区组网、GLONASS系统再次实现满星座部署以及GPS系统的现代化,多系统集成已逐步成为网络RTK技术的发展趋势。本文结合笔者所在课题组自主研发的网络RTK数据处理系统DREAMNET,对不同卫星系统组合模式下的定位精度进行比较分析。试验结果表明,GPS/BDS/GLONASS网络RTK和GPS/BDS网络RTK的定位精度最高,GPS、BDS单系统网络RTK次之。此外,随着高度角的增加,GPS单系统网络RTK的可用性显著降低,而GPS/BDS/GLONASS网络RTK在高度角为40°时依然可以在99.84%的时间里提供水平精度0.01 m、高程精度0.025 m的定位服务。最后,对15 d的定位结果进行统计,包括不依赖GPS系统的BDS和BDS/GLONASS在内的6种组合方式皆可达到水平0.01 m、高程0.025 m的定位精度,其中GPS/BDS/GLONASS网络RTK则可以得到水平0.006 m、高程0.015 m的定位精度,证明DREAMNET的定位精度和稳定性完全可以满足测绘作业的需要。 相似文献
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Benefiting from multi-constellation Global Navigation Satellite Systems (GNSS), more and more visible satellites can be used to improve user positioning performance. However, due to limited tracking receiver channels and power consumption, and other issues, it may be not possible, or desirable, to use all satellites in view for positioning. The optimal subset is generally selected from all possible satellite combinations to minimize either Geometric Dilution of Precision (GDOP) or weighted GDOP (WGDOP). However, this brute force approach is difficult to implement in real-time applications due to the time- and power-consuming calculation of the DOP values. As an alternative to a brute force satellite selection procedure, the authors propose an end-to-end deep learning network for satellite selection based on the PointNet and VoxelNet networks. The satellite selection is converted to a satellite segmentation problem, with specified input channel for each satellite and two class labels, one for selected satellites and the other for those not selected. The aim of the satellite segmentation is that a fixed number of satellites with the minimum GDOP/WGDOP value can be segmented from any feeding order of input satellites. To validate the proposed satellite segmentation network, training and test data from 220 IGS stations tracking GPS and GLONASS satellites were used. The segmentation performance using different architectures and representations of input channels, including receiver-to-satellite unit vector and elevation and azimuth, were compared. It was found that the input channel with elevation and azimuth can achieve better performance than using the receiver-to-satellite unit vector, and an architecture with stacked feature encoding (FE) layers has better satellite segmentation performance than one without stacked FE layers. In addition, the models with GDOP and WGDOP criteria for selecting 9 and 12 satellites were trained. It was demonstrated that the satellite segmentation network was about 90 times faster than using the brute force approach. Furthermore, all the trained models can effectively select the satellites making the most contribution to the desired GDOP/WGDOP value. Approximately 99% of the tests had GDOP and WGDOP value differences smaller than 0.03 and 0.2, respectively, between the predicted subset and the optimal subset. 相似文献
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SLR资料精密测定GLONASS卫星轨道 总被引：3，自引：0，他引：3
将SLR资料计算的轨道与CODE轨道进行了比较，并将比较结果转换到RTN坐标系中。通过比较分析发现，两种轨道差值在轨道径向、法向和沿轨方向的精度分别优于10cm、50cm和45cm；SLR和微波资料确定的GLONASS卫星轨道在径向存在系统误差，该系统误差随卫星轨道面的不同而不同。 相似文献
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A technique for obtaining clock measurements from individual GNSS satellites at short time intervals is presented. The methodology developed in this study allows for accurate satellite clock stability analysis without an ultra-stable clock at the ground receiver. Variations in the carrier phase caused by the satellite clock are isolated using a combination of common GNSS carrier-phase processing techniques. Furthermore, the white phase variations caused by the thermal noise of the collection and processing equipment are statistically modeled and removed, allowing for analysis of clock performance at subsecond intervals. Allan deviation analyses of signals collected from GPS and GLONASS satellites reveal distinct intervals of clock noise for timescales less than 100 s. The clock data collected from GPS Block IIA, IIR, IIR-M, and GLONASS satellites reveal similar stability performance at time periods greater than 20 s. The GLONASS clock stability in the 0.6–10 s range, however, is significantly worse than GPS. Applications that rely on ultra-stable clock behavior from the GLONASS satellites at these timescales may therefore require high-rate corrections to estimate and remove oscillator-based errors in the carrier phase. 相似文献
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The International GLONASS Experiment 1998 (IGEX-98) was the first international tracking campaign of the Russian counterpart
to the Global Positioning System (GPS), GLONASS. Started in October 1998, the campaign was originally scheduled to last for
three months. However, the launch of additional GLONASS satellites and a widespread enthusiasm among the participants led
to an indefinite continuation of the campaign on a “best effort” basis.
At the Delft University of Technology, the data of six IGEX-98 stations have been analyzed in detail with integrity monitoring
software, developed at the Department of Mathematical Geodesy and Positioning of the University. The software aims to detect
outliers and slips in code and phase observations in real time. In addition, the software also allows the validation of the
information contained in the broadcast navigation messages.
The results of the IGEX-98 data analyses will be presented in a three-part series. In the second part, GLONASS outlier and
slips statistics will be discussed, while in the third part the anomaly detection results of the GLONASS and GPS messages
will be shown. In this first part of the series, however, the most basic of all statistics will be considered: a simple day-to-day
count of the number of GLONASS and GPS observations. Although simple, this statistic yields a surprising amount of information
both on the availability of the GLONASS satellites and on the peculiarities of some of the receiver makes participating in
the IGEX-98 campaign. ? 2000 John Wiley & Sons, Inc. 相似文献