共查询到19条相似文献，搜索用时 406 毫秒
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针对PPP-B2b服务钟差产品包含相比于其他实时钟差产品更大的钟差常数偏差，可能会影响精密单点定位收敛时间的问题，该文利用非差法解算接收机信号失真偏差时钟差常数偏差和SDB相互耦合的关系，对钟差常数偏差进行分离，并分析了PPP-B2b服务钟差中常数偏差的特性及其对定位的影响。发现此项偏差随卫星弧段不同变化，不同弧段之间的差异能达到3.5 ns,进一步在伪距观测量中改正此项偏差可分别使BDS和GPS精密单点定位收敛时间减少55.4%和53.5%。上述实验结果表明，PPP-B2b服务中钟差常数偏差在不同弧段间存在较大差异，并且显著影响定位收敛速度。 相似文献
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《武汉大学学报(信息科学版)》2016,(5)
研究并实现了基于非差观测量的北斗卫星实时钟差估计算法,利用全球53个多模全球导航卫星系统(global navigation satellite system,GNSS)实验跟踪网(multi-GNSS experiment,MGEX)站的北斗与全球定位系统(global positioning system,GPS)观测数据进行实时钟差估计,分析了实时钟差产品的精度与定位性能。多天统计结果表明,本文生成的GPS实时钟差与事后钟差符合较好,精度优于0.07ns,略低于事后钟差产品,验证了基于非差观测量的实时钟差估计软件的处理精度。本文解算的北斗实时钟差的精度为0.1~0.15ns,略低于GPS卫星。基于实时钟差进行模拟动态精密单点定位(precise point positioning,PPP)实验,北斗与GPS在水平方向的定位精度为0.041m和0.058m,高程方向的精度为0.069m和0.037m,定位结果分别与事后钟差解算的结果符合较好,表明实时钟差与事后钟差差异不大。 相似文献
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实时GNSS精密单点定位(PPP)技术必须使用实时的高精度卫星精密轨道和钟差。本文研究了精密卫星钟差融合解算模型及策略,并利用滤波算法实现了北斗/GPS实时精密卫星钟差融合估计算法。仿真实时试验结果显示:获得的北斗/GPS实时钟差与GFZ事后多GNSS精密钟差(GBM)的标准差在0.15 ns左右;使用该钟差进行GPS动态PPP试验,收敛后水平精度优于5 cm,高程精度优于10 cm;使用仿真实时钟差进行的北斗动态PPP与使用GFZ事后多GNSS精密钟差开展的试验相比精度相当,可实现分米级定位。 相似文献
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多星座数据融合处理时,由于接收机钟差和信号传播延迟的影响,导致信号发射时刻的卫星位置不能精确求定。在定位解算里,可以通过星间差分消除与光速有关的接收机钟差影响,然而与卫星径向速度有关的接收机钟差项却得不到消除。该文详细分析了多星座接收机不同钟差值的产生原因,推导了卫星径向速度对站星距的影响,提出了一种针对多星座的单基准站接收机钟差估计方法,通过统一修正各星座卫星位置,有效消除了与卫星速度有关的接收机钟差项的误差,并且适用于存在1ms时钟跳跃的接收机,实现多星座融合的高精度定位。 相似文献
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实时钟差产品是高精度广域差分位置服务（亚米级、分米级、厘米级）的基础产品,通过研究BDS/GPS融合的ISB,研究了各类型接收机BDS GEO/IGSO/MEO ISB差异,提出了在BDS/GPS联合的实时钟差估计中引入3个ISB参数的函数模型,在此基础上基于非差法实现了BDS/GPS联合的实时钟差估计。采用MGEX和湖南CORS实时观测数据进行了实时钟差解算,利用iGMAS产品综合中心提供的事后精密钟差产品作为基准,对比分析了新方法与原有方法的实时钟差产品的精度差异。结果表明,该方法与原方法估计的GPS钟差精度相当,对BDS实时钟差精度改进显著,尤其对BDS IGSO/MEO卫星,改进幅度在20%以上,验证了算法的有效性。 相似文献
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《测绘地理信息》2020,(3)
基于GNSS(global navigation satellite system)非差观测量,利用双线程钟差加密的方法,本文实现了导航卫星实时钟差的逐秒更新。通过选取全球均匀分布的76个参考站对四系统钟差进行联合估计,并从实时轨道精度,解算效率,钟差精度和精密单点定位(precision point positioning,PPP)定位结果对该系统进行分析和评估。结果表明,GPS预报轨道径向精度为2.3 cm,GLONASS和Galileo预报轨道径向精度为3 cm和3.5 cm,北斗GEO、IGSO、MEO卫星预报轨道径向精度分别为31 cm,17 cm和5.3 cm;钟差统计结果表明,GPS实时钟差精度优于0.2 ns,GLONASS钟差精度优于0.4 ns,Galileo钟差精度优于0.3 ns,受轨道影响,北斗GEO实时钟差精度为0.6～1.0 ns,IGSO钟差精度为0.4～0.7 ns,MEO钟差精度为0.3～0.4 ns;PPP定位结果表明,解算钟差定位精度与事后钟差定位结果相当,平面精度在3 cm以下,高程精度在5 cm以下。 相似文献
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Kinematic positions of Low Earth Orbiters based on GPS tracking are frequently used as pseudo-observations for single satellite gravity field determination. Unfortunately, the accuracy of the satellite trajectory is partly limited because the receiver synchronization error has to be estimated along with the kinematic coordinates at every observation epoch. We review the requirements for GPS receiver clock modeling in Precise Point Positioning (PPP) and analyze its impact on kinematic orbit determination for the two satellites of the Gravity Recovery and Climate Experiment (GRACE) mission using both simulated and real data. We demonstrate that a piecewise linear parameterization can be used to model the ultra-stable oscillators that drive the GPS receivers on board of the GRACE satellites. Using such a continuous clock model allows position estimation even if the number of usable GPS satellites drops to three and improves the robustness of the solution with respect to outliers. Furthermore, simulations indicate a potential accuracy improvement of the satellite trajectory of at least 40 % in the radial direction and up to 7 % in the along-track and cross-track directions when a 60-s piecewise linear clock model is estimated instead of epoch-wise independent receiver clock offsets. For PPP with real GRACE data, the accuracy evaluation is hampered by the lack of a reference orbit of significantly higher accuracy. However, comparisons with a smooth reduced-dynamic orbit indicate a significant reduction of the high-frequency noise in the radial component of the kinematic orbit. 相似文献
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基于VRS的GPS测量误差分析 总被引：1，自引：0，他引：1
系统误差包括卫星轨道误差、卫星钟差、接收机钟差及大气折射误差等。是GPS测量的主要误差源。但系统误差通常可以采用适当的方法来减弱或消除,如建立误差改正模型对观测值进行改正,或选择良好的观测条件,采用适当地观测方法,进行线性差分等.本文介绍了基于VRS的GPS测量要解决的一个主要问题即在系统运行中产生的各种误差进行改正,使之减小或者消除。并就影响VRS精度的各种误差予以分析 相似文献
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Patrick J. Fell 《Journal of Geodesy》1980,54(4):564-574
Geodetic positioning accuracies obtained from range, integrated Doppler and double differenced interferometric phase observations
from a constellation of twenty-four Global Positioning System satellites are presented. It is demonstrated that GPS range
and Doppler observations will provide sufficient accuracy for the estimation of geodetic coordinates. However the instability
of the receiver atomic oscillator will limit the usefulness of these observations in providing rapid first-order baseline
determination. Interferometric phase measurements twice differenced to eliminate clock error appear as an alternate procedure
for providing such accuracies. 相似文献
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An algorithm for very accurate absolute positioning through Global Positioning System (GPS) satellite clock estimation has
been developed. Using International GPS Service (IGS) precise orbits and measurements, GPS clock errors were estimated at
30-s intervals. Compared to values determined by the Jet Propulsion Laboratory, the agreement was at the level of about 0.1 ns
(3 cm). The clock error estimates were then applied to an absolute positioning algorithm in both static and kinematic modes.
For the static case, an IGS station was selected and the coordinates were estimated every 30 s. The estimated absolute position
coordinates and the known values had a mean difference of up to 18 cm with standard deviation less than 2 cm. For the kinematic
case, data obtained every second from a GPS buoy were tested and the result from the absolute positioning was compared to
a differential GPS (DGPS) solution. The mean differences between the coordinates estimated by the two methods are less than
40 cm and the standard deviations are less than 25 cm. It was verified that this poorer standard deviation on 1-s position
results is due to the clock error interpolation from 30-s estimates with Selective Availability (SA). After SA was turned
off, higher-rate clock error estimates (such as 1 s) could be obtained by a simple interpolation with negligible corruption.
Therefore, the proposed absolute positioning technique can be used to within a few centimeters' precision at any rate by estimating
30-s satellite clock errors and interpolating them.
Received: 16 May 2000 / Accepted: 23 October 2000 相似文献
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Due to the limited frequency stability and poor accuracy of typical quartz oscillators built-in GNSS receivers, an additional receiver clock error has to be estimated in addition to the coordinates. This leads to several drawbacks especially in kinematic applications: At least four satellites in view are needed for navigation, high correlations between the clock estimates and the up-coordinates. This situation can be improved distinctly when connecting atomic clocks to GNSS receivers and modeling their behavior in a physically meaningful way (receiver clock modeling). Recent developments in miniaturizing atomic clocks result in so-called chip-scale atomic clocks and open up the possibility of using stable atomic clocks in GNSS navigation. We present two different methods of receiver clock modeling, namely in an extended Kalman filter and a sequential least-squares adjustment for code-based GNSS navigation using three different miniaturized atomic clocks. Using the data of several kinematic test drives, the benefits of clock modeling for GPS navigation solutions are assessed: decrease in the noise of the up-coordinates by up to 69 % to 20 cm level, decrease in minimal detectable biases by 16 %, and elimination of spikes and subsequently decrease in large position errors (35 %). Hence, a more robust position is obtained. Additionally, artificial partial satellite outages are generated to demonstrate position solutions with only three satellites in view. 相似文献
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Real-time clock jump compensation for precise point positioning 总被引：1，自引：1，他引：0
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Since the Selective Availability was turned off, the velocity and acceleration can be determined accurately with a single GPS receiver using raw Doppler measurements. The carrier-phase-derived Doppler measurements are normally used to determine velocity and acceleration when there is no direct output of the raw Doppler observations in GPS receivers. Due to GPS receiver clock drifts, however, a GPS receiver clock jump occurs when the GPS receiver clock resets itself (typically with 1 ms increment/decrement) to synchronize with the GPS time. The clock jump affects the corresponding relationship between measurements and their time tags, which results in non-equidistant measurement sampling in time or incorrect time tags. This in turn affects velocity and acceleration determined for a GPS receiver by the conventional method which needs equidistant carrier phases to construct the derived Doppler measurements. To overcome this problem, an improved method that takes into account, GPS receiver clock jumps are devised to generate non-equidistant-derived Doppler observations based on non-equidistant carrier phases. Test results for static and kinematic receivers, which are obtained by using the conventional method without reconstructing the equidistant continuous carrier phases, show that receiver velocity and acceleration suffered significantly from clock jumps. An airborne kinematic experiment shows that the greatest impact on velocity and acceleration reaches up to 0.2 m/s, 0.1 m/s2 for the horizontal component and 0.5 m/s, 0.25 m/s2 for the vertical component. Therefore, it can be demonstrated that velocity and acceleration measurements by using a standalone GPS receiver can be immune to the influence of GPS receiver clock jumps with the proposed method. 相似文献
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Analyses and Solutions of Errors on GPS／GLONASS Positioning 总被引：1，自引：0，他引：1
ZHANGYongjun WANGZemin 《地球空间信息科学学报》2002,5(2):6-12
This paper focuses mainly on the major errors and their reduction approaches pertaining to combined GPS/GLONASS positioning.To determine thd difference in the time reference systems,different receiver clock offsets are introduced with respect to GPS and GLONASS system time.A more desirable method for introducing a independent unknown parameter of fifth receiver,which can be canceled out when forming difference measurements,is discussed.The error of orbit integration and the error of transformation parameters are addressed in detail.Results of numerical integration are give.To deal with the influence of ionospheric delay,a method for forming dual-frequency ionospheric free carrier phase measurements is detailed. 相似文献