共查询到19条相似文献，搜索用时 128 毫秒
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针对2018年实现全星座试运行的日本区域性卫星导航系统QZSS的定位服务性能评估问题,首次利用MGEX实验网日本区域4个均可接收全部4颗QZSS卫星信号的测站数据对GPS/QZSS系统在日本境内的定位服务性能进行了分析。结果表明:联合QZSS的GPS系统在各种遮挡环境下的定位性能较独立GPS系统均有显著改善;这些改善在高截止高度角情况下更为明显。 相似文献
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针对日本准天顶卫星系统（QZSS）对北斗二号（BDS-2）和北斗三号（BDS-3）短基线相对定位性能的影响,本文基于国际GNSS服务（IGS）跟踪站组成的5 km和10km两条短基线,分析了QZSS、BDS-2、BDS-3不同组合短基线相对定位精度．经研究发现,QZSS能有效改善BDS-2和BDS-3卫星可见数与卫星空间几何构型,而BDS-2／BDS-3组合下的卫星可见数与卫星空间几何构型优于任一单系统．在定位精度方面,QZSS与数据缺失情况下BDS-3组合定位精度与BDS-2相当,同时QZSS能有效提升BDS-2和BDS-2／BDS-3相对定位精度,而BDS-3对BDS-2定位精度的提升要优于QZSS． 相似文献
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印度区域导航卫星系统（IRNSS）与日本准天顶系统（QZSS）是近年来宣布正式运行的两个区域卫星导航系统。本文首先评估了IRNSS和QZSS在各自主服务区域的L5信号单点定位性能。然后,为了探究导航星座结构差异对各区域系统联合GPS在城市峡谷环境下定位性能的影响程度,详细对比分析了卫星截止高度角为5°、15°、25°、35°、45°、55°时各区域系统在其主服务区内联合GPS定位的表现。结果表明：① IRNSS在其主服务区内可提供全天连续独立L5定位服务,水平方向定位精度小于2.50m,高程方向定位精度小于4.10m;② QZSS在其主服务区内只能提供全天部分时段的独立L5定位服务,水平方向定位精度小于4.80m,高程方向定位精度小于7.40m;③由于QZSS独特的星座结构,其在主服务区城市峡谷环境中联合GPS定位的性能要优于IRNSS在其相应主服务区联合GPS定位的表现,尤其是在天空视野有限的情况下。本文结果对决策者设计新的区域导航系统具有一定的参考价值。 相似文献
4.
《武汉大学学报(信息科学版)》2020,(4)
利用多星座实验(the multi-GNSS experiment,MGEX)监测网的观测数据分别从可见卫星数、精度衰减因子(dilution of precision,DOP)、多路径效应、信噪比、静态/动态精密单点定位(precise point positioning,PPP)几个方面对北斗卫星导航系统(BeiDou Navigation Satellite System,BDS)/准天顶卫星系统(Quasi-Zenith Satellite System,QZSS)及其组合系统在中国和日本及周边地区的定位性能进行评估与分析。分析结果表明:QZSS与BDS系统组合,卫星数增加,能提供较好的空间几何构型分布,从而保证了定位的精度、可靠性和可用性;由于QZSS卫星的星座结构与BDS卫星类似,其多路径效应的变化规律表现出与BDS卫星一致性的特点;BDS和QZSS卫星各频点信号的信噪比与高度角相关趋势几乎相同,相同高度角条件下,地球中轨道(medium earth orbit,MEO)卫星信噪比要比倾斜地球同步轨道(inclined geosynchronous orbit,IGSO)卫星高2～3 dBHz;静态PPP和动态PPP方面,在高度角较大时(40°),BDS+QZSS组合比BDS单系统在低高度角情形下改善更为明显。E、N和U方向静态PPP改善率可达20%以上,动态PPP改善率可达30%以上。QZSS系统卫星对日本、中国以及周边区域BDS定位具有一定的补充和增强作用,在信号易遮挡的复杂环境(如城市、建筑物密集区、山区、树林等)下,具有较好的应用价值。 相似文献
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在日本和中国中东部地区,就日本准天顶卫星系统(QZSS)对GPS导航精度增强、完好性增强以及可用性增强进行了仿真计算比较。结果表明,只有3颗卫星组成的QZSS在这些区域内对GPS提供了有效的性能增强,而且随着卫星截止角的增加,这种性能增强显得更为明显;QZSS在战时可有效降低由于部分GPS卫星失效而导致的性能恶化程度。分析结果对于我国在中部地区和东部热点地区有效利用GNSS导航资源具有指导作用。 相似文献
7.
QZSS系统在中国区域增强服务性能评估与分析 总被引：1，自引：0，他引：1
《武汉大学学报(信息科学版)》2016,(3)
日本准天顶卫星系统(QZSS)是区域性辅助与区域增强一体的导航系统,覆盖区域为日本及周边区域,包括我国部分区域,该系统采用IGSO卫星播发L1-SAIF与LEX两类增强信息,可以提供我国部分区域用户的高精度定位。本文从可用性、空间信号精度、用户动态精密单点定位几个方面对QZSS两类增强信号在中国区域的性能进行较为全面的评估,并采用QZS-1卫星实测数据进行实验,结果表明,以20°为截止高度角,中国大部分区域,尤其是东部沿海地区一天之内80%的时段可连续观测QZSS卫星;L1-SAIF差分增强信息可实现与目前WAAS相当的精度,URE约0.56m,满足1m左右的精密单点定位,平面精度优于1m;与L1-SAIF相比,LEX精度更高,轨道与钟差精度可达dm级,URE约0.4m,可实现亚m级定位,平面0.2m,高程0.5m。 相似文献
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通过STK软件对BDS、QZSS、IRNSS卫星星座结构仿真的基础上,选择BDS、BDS/QZSS、BDS/IRNSS、BDS/QZSS/IRNSS、QZSS/IRNSS等定位方式对中国大陆单观测站与整体范围最小可见卫星数、GDOP值、定位误差进行覆盖分析,确定了QZSS与IRNSS在我国的覆盖范围及对BDS定位性能增强作用的评估。结果表明,BDS/QZSS/IRNSS组合在我国的最小可见卫星数可达16~21颗,GDOP值在1.4~1.7之间,定位误差达5.5~7.5m,相比单BDS定位最小可见卫星数增加了6~8颗,GDOP值减小了0.3~0.5,定位精度提升了2.0~3.0m,对华南地区的定位性能有明显提升,而对东北等地区定位性能的提升较小。 相似文献
10.
为了对多个全球导航卫星系统（global navigation satellite system, GNSS）当前的广播星历精度进行一个全面的分析,对比了2014—2018年共5 a的GNSS广播星历与精密星历,并对全球定位系统（global positioning system, GPS）、格洛纳斯卫星导航系统（global navigation satellite system, GLONASS）、伽利略卫星导航系统（Galileo satellite navigation system, Galileo）、北斗卫星导航系统（BeiDou navigation satellite system, BDS）、准天顶卫星系统（quasi-zenith satellite system, QZSS）等5个系统的广播星历长期精度变化进行了分析。结果表明:5 a中GPS的广播星历轨道及钟差精度最稳定;GLONASS的广播星历轨道精度稳定性较好,但其钟差精度存在较大的离散度;Galileo得益于具备全面运行能力（full operational capability, FOC）卫星的大量发射及运行,其广播星历轨道、钟差精度大幅度变好,切向轨道、法向轨道与钟差精度已赶超GPS;BDS的广播星历轨道精度离散度较大,钟差精度出现不稳定现象;QZSS的广播星历轨道与钟差精度的稳定性与离散度相对最差。以2018年1 a的广播星历与精密星历为例分析了各个系统当前的广播星历精度,结果表明,当前GPS、GLONASS、Galileo、BDS、QZSS的考虑轨道误差与钟差误差贡献的空间信号测距误差（signal-in-space ranging error,SISRE）分别为0.806 m、2.704 m、0.320 m、1.457 m、1.645 m,表明Galileo广播星历整体精度最高,GPS次之,其次分别是BDS、QZSS和GLONASS。只考虑轨道误差贡献的SISRE分别为0.167 m、0.541 m、0.229 m、0.804 m、0.675 m,表明GPS广播星历轨道精度最高,其次分别是Galileo、GLONASS、QZSS和BDS。GPS卫星广播星历中新型号卫星的钟差精度总体要优于旧型号卫星。 相似文献
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The Indian Regional Navigation Satellite System (IRNSS), which is being developed for positioning services in and around India, is the latest addition to the global family of satellite-based navigation systems. As IRNSS only shares the L5-frequency with GPS, the European Galileo, and the Japanese Quasi-Zenith Satellite System (QZSS), it has at least at present a limited interoperability with the existing systems. Noting that the L5-frequency capability is under development even for GPS, this contribution assesses the interoperability of the IRNSS L5-signal with the GPS, Galileo, and QZSS L5/E5a-signals for positioning and navigation using real data collected in Perth, Australia. First, the noise characteristic of the IRNSS L5-signal and its comparison with that of the GPS, Galileo, and QZSS L1/E1- and L5/E5a-signals is presented. Then, the L5-observables of combined systems (formed from IRNSS, GPS, Galileo, and QZSS) are assessed for real-time kinematic positioning using the standard LAMBDA method and for instantaneous attitude determination using the constrained LAMBDA method. The results show that the IRNSS L5-signal has comparable noise characteristics as that of the other L5/E5a-signals. For single-frequency carrier phase-based positioning and navigation, the results show better ambiguity resolution performance of L5/E5a-only processing than that of L1/E1-only processing. 相似文献
12.
Results are presented for Michibiki, the first satellite of Japan’s Quasi-Zenith Satellite System. Measurements for the analysis
have been collected with five GNSS tracking stations in the service area of QZSS, which track five of the six signals transmitted
by the satellite. The analysis discusses the carrier-to-noise density ratio as measured by the receiver for the different
signals. Pseudorange noise and multipath are evaluated with dual-frequency and triple-frequency combinations. QZSS uses two
separate antennas for signal transmission, which allows the determination of the yaw orientation of the spacecraft. Yaw angle
estimation results for an attitude mode switch from yaw-steering to orbit-normal orientation are presented. Estimates of differential
code biases between QZSS and GPS observations are shown in the analysis of the orbit determination results for Michibiki.
The estimated orbits are compared with the broadcast ephemerides, and their accuracy is assessed with overlap comparisons. 相似文献
13.
卫星钟差数据插值是高精度定位数据处理中的重要环节,其插值结果直接影响定位精度,但常用的插值或拟合方法具有不同缺点. 本文尝试将广义延拓逼近法应用于准天顶卫星系统(QZSS)卫星钟差数据的处理中,介绍了Lagrange插值法、切比雪夫拟合法和广义延拓逼近法的原理,以及滑动式与非滑动式的区别;然后使用QZSS钟差数据探讨三种方法的参数(组)取值与插值结果精度的关系;最后比较三种方法在各自最优参数(组)取值情况下对QZSS卫星钟差的插值精度. 结果表明:选取合理的参数组合,广义延拓逼近法完全适用于QZSS卫星钟差的插值,且插值精度明显高于其他两种方法. 相似文献
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Dennis Odijk Nandakumaran Nadarajah Safoora Zaminpardaz Peter J. G. Teunissen 《GPS Solutions》2017,21(2):439-450
Knowledge of inter-system biases (ISBs) is essential to combine observations of multiple global and regional navigation satellite systems (GNSS/RNSS) in an optimal way. Earlier studies based on GPS, Galileo, BDS and QZSS have demonstrated that the performance of multi-GNSS real-time kinematic positioning is improved when the differential ISBs (DISBs) corresponding to signals of different constellations but transmitted at identical frequencies can be calibrated, such that only one common pivot satellite is sufficient for inter-system ambiguity resolution at that particular frequency. Recently, many new GNSS satellites have been launched. At the beginning of 2016, there were 12 Galileo IOV/FOC satellites and 12 GPS Block IIF satellites in orbit, while the Indian Regional Navigation Satellite System (IRNSS) had five satellites launched of which four are operational. More launches are scheduled for the coming years. As a continuation of the earlier studies, we analyze the magnitude and stability of the DISBs corresponding to these new satellites. For IRNSS this article presents for the first time DISBs with respect to the L5/E5a signals of GPS, Galileo and QZSS for a mixed-receiver baseline. It is furthermore demonstrated that single-frequency (L5/E5a) ambiguity resolution is tremendously improved when the multi-GNSS observations are all differenced with respect to a common pivot satellite, compared to classical differencing for which a pivot satellite is selected for each constellation. 相似文献
15.
The L1-SAIF (L1 Submeter-class Augmentation with Integrity Function) signal is one of the Quasi-Zenith Satellite System (QZSS)
navigation signals, which provides an augmentation function for mobile users in Japan. The tropospheric delay correction in
the L1-SAIF augmentation is discussed in detail. Because the topographical features in Japan are complicated, the correction
information is generated from GPS observation data collected at 200 GPS stations which are densely distributed over Japan.
A total of 210 Tropospheric Grid Points (TGPs) are arranged to fully cover Japan. The TGPs that provide the correction information
are selected adaptively to achieve the expected correction accuracy. This selection of TGPs is provided by the TGP mask message.
Mobile users acquire the zenith tropospheric delay (ZTD) value at neighboring TGPs from the correction messages, and can estimate
the local ZTD value accurately by using a suitable ZTD model. Only up to seven L1-SAIF messages are sufficient to provide
the full correction information. Accuracy evaluations have proven that it is possible to achieve a correction accuracy of
13.4 mm RMS. The strategy presented here has been implemented into the augmentation system using the L1-SAIF signal, and its
application guidance is presented in the QZSS interface specification. 相似文献
16.
与全球定位系统（global positioning system,GPS）不同,北斗区域卫星导航系统（BeiDou navigation satellite system,BDS）采用了5颗地球静止轨道卫星、5颗倾斜地球同步轨道卫星和4颗中圆轨道卫星的混合星座,星座分布不均匀。特殊星座决定了不同纬度地区用户的可见卫星数量和观测几何结构存在明显差异,用户的导航定位性能存在明显的纬度效应。分别从理论模型和实际观测两个方面对不同纬度地区用户的可见卫星数目、观测几何结构和导航定位性能进行较全面分析,使用了多家厂商的接收机,在不同纬度地区进行了GPS、BDS以及两系统融合定位试验。结果表明,BDS定位性能存在明显的纬度效应,即定位精度随纬度升高而降低;GPS导航定位性能没有明显的纬度效应;BDS/GPS数据融合可以减弱纬度效应,提高导航定位服务的精度和可靠性。 相似文献
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从全球国际地球参考框架（International Terrestrial Reference Frame，ITRF）的建立、维护与发展，卫星测高、卫星重力等的发展及应用，全球卫星导航系统（Global Navigation Satellite System，GNSS）、卫星激光测距（Satellite Laser Ranging，SLR）、甚长基线干涉测量（very Long Baseline Interferometry，VLBI）、卫星多普勒定轨定位（Doppler Orbitography by Radiopositioning Integrated on Satellite，DORIS）的融合应用，海洋测绘和室内定位的发展等几个方面综述了大地测量学及卫星导航定位技术的最新进展，并提出中国2000国家大地坐标系与自主卫星导航系统的主要应用及发展目标。 相似文献
18.
Haibo Ge Bofeng Li Song Jia Liangwei Nie Tianhao Wu Zhe Yang Jingzhe Shang Yanning Zheng Maorong Ge 《地球空间信息科学学报》2022,(1):1-13
With the completion of Chinese BeiDou Navigation Satellite System (BDS), the world has begun to enjoy the Positioning, Navigation, and Timing (PNT) services of ... 相似文献
19.
It has been noted that the satellite laser ranging (SLR) residuals of the Quasi-Zenith Satellite System (QZSS) Michibiki satellite orbits show very marked dependence on the elevation angle of the Sun above the orbital plane (i.e., the \(\beta \) angle). It is well recognized that the systematic error is caused by mismodeling of the solar radiation pressure (SRP). Although the error can be reduced by the updated ECOM SRP model, the orbit error is still very large when the satellite switches to orbit-normal (ON) orientation. In this study, an a priori SRP model was established for the QZSS Michibiki satellite to enhance the ECOM model. This model is expressed in ECOM’s D, Y, and B axes (DYB) using seven parameters for the yaw-steering (YS) mode, and additional three parameters are used to compensate the remaining modeling deficiencies, particularly the perturbations in the Y axis, based on a redefined DYB for the ON mode. With the proposed a priori model, QZSS Michibiki’s precise orbits over 21 months were determined. SLR validation indicated that the systematic \(\beta \)-angle-dependent error was reduced when the satellite was in the YS mode, and better than an 8-cm root mean square (RMS) was achieved. More importantly, the orbit quality was also improved significantly when the satellite was in the ON mode. Relative to ECOM and adjustable box-wing model, the proposed SRP model showed the best performance in the ON mode, and the RMS of the SLR residuals was better than 15 cm, which was a two times improvement over the ECOM without a priori model used, but was still two times worse than the YS mode. 相似文献