共查询到19条相似文献，搜索用时 109 毫秒
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电离层延迟误差是单频GPS实时/事后定位误差的一个重要来源,目前尚无有效的方法来削弱其影响。针对这一状况,该文首先介绍了单频GPS改正电离层延迟误差的常用方法,通过分析说明了电离层格网数据能够有效改善单频GPS实时/事后定位误差。给出了电离层格网数据的建立、预报方法,并详细介绍了刺入点地心经纬度VTEC值的计算方法、四点格网法内插刺入点天顶方向的总电子含量以及单层模型投影函数。结合算例,分析比较了不同类型电离层改正数据与卫星星历数据对单频GPS实时/事后定位精度的影响。实验结果表明,利用电离层格网预报数据能够显著改善单频GPS的实时/事后导航定位精度,对提高单频GPS定位精度具有一定实用价值。 相似文献
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本文对组合GNSS系统进行静态相对定位测量与RTK测量试验,研究结果表明:在静态相对定位测量中,BDS的数据利用率、多路径效应误差优于GPS与GLONASS,BDS的定位精度优于GLONASS略低于GPS;组合系统中GPS/BDS与GPS/BDS/GLONASS的定位精度较优,引入GLONASS对定位精度改善的作用不明显。在RTK测量中,当观测条件理想时,GPS/BDS较GPS可见卫星数目多,PDOP值低,中误差小。当观测条件较差时,GPS/BDS较GPS可见卫星数目多,PDOP平均值低,中误差小,限差内固定解获得时间减少76.1%;GPS/BDS/GLONASS较GPS/BDS在中误差、水平精度和垂直精度上更优,限差内固定解获得时间更稳定可靠。 相似文献
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GPS现代化后电离层折射误差高阶项的三频改正方法 总被引：13，自引：1，他引：13
研究了电离层对GPS观测信号的主要影响及电离层折射误差模型,总结了电离层双频改正模型。针对GPS现代化中增加的第三频率,系统推导了三个频率的电离层改正模型及相位观测值无电离层组合(LC组合)模型。该模型将电离层折射误差模型改正至二阶项,可进一步提高GPS定位精度,同时,为GPS定位中其他误差的改正及分离、周跳的探测等提供了有力的技术手段。 相似文献
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针对单频精密单点定位(PPP)两种常用的定位模型:非组合模型和附加电离层约束模型,同时综合考虑电离层约束模型三种不同约束策略(常数约束,时空约束,逐步松弛),对比分析了其使用GPS单系统及GPS+BDS双系统观测值的定位收敛时间,定位精度及其优缺点. 实验结果表明:使用GPS单系统,附加不同电离层约束对单频PPP收敛时间缩短效果显著,其中逐步松弛约束平均收敛时间最短,其平均收敛时间为32.36 min,四种定位模型收敛后的定位精度基本相当. 加入北斗卫星导航系统(BDS)后,四种定位模型的收敛时间均有不同程度的缩短,其中时空约束模型缩短最为显著,收敛时间缩短为单系统的59.22%. 在定位精度方面,加入BDS观测值后水平方向定位精度可提升0.5～1.3 cm,垂直方向定位精度略有下降. 相似文献
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电离层对GPS的影响 总被引：1，自引：0，他引：1
电离层效应是GPS导航定位的主要误差。本文论述电离层的特征及电离层的下列影响：电离层码群延、电离层载波相位超前、电离层多普勒频移、电离层折射与高度角的关系、振幅闪烁、磁暴对GPS的影响、电离层对差分GPS的影响和GPS接收机的电离层改正。 相似文献
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GPS/BDS中长距离RTK定位因为电离层和对流层残余误差的影响,其性能相对于常规RTK有所降低。将GPS/BDS卫星双差电离层误差和对流层误差作为参数,采用卡尔曼滤波进行实时估计。为了验证算法的有效性,利用武汉地区103 km静态基线24 h双频观测数据,分析了GPS和BDS单系统以及二者组合双系统中长距离RTK定位性能。实验结果表明,精确估计的双差电离层残余误差达到米级、对流层误差达到分米级;经过改正后,GPS/BDS单系统的定位精度在1 cm左右,组合双系统则实现了中长距离基线毫米级的高精度定位。 相似文献
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针对常规模式下。单系统实时精密单点定位精度受接收机环境和可视卫星数量影响严重等问题,研究了GPS/BDS双系统实时精密单点定位,采用非差无电离层组合载波和伪距观测值,详细推论了Kalman滤波参数估计方法的基本原理,并利用其进行参数估计,最后通过IGS站和实测数据进行了实时PPP实验,实验表明:GPS/BDS双系统定位模式较GPS单系统有明显改善,在E、N、U方向收敛后RMS值分别达到0.125 m、0.117 m、0.289 m,较单系统在各方向分别改善了11.9%、18.1%、22.5%。证明了GPS/BDS实时PPP能够达到分米级到厘米级定位精度。 相似文献
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精密单点定位(PPP)-实时动态(RTK)技术借助区域大气改正数可实现快速精密定位,被认为是未来自动驾驶的首选技术.然而，PPP-RTK在电离层闪烁环境下难以维持稳定可靠的定位，闪烁已成为PPP-RTK面临的重大挑战之一.本文阐述了PPP-RTK模型和电离层闪烁特性，并基于香港卫星定位参考站网(SatRef)的实验数据从观测质量、周跳探测、大气产品和终端定位性能四个层面评估了电离层闪烁对PPP-RTK的影响.结果表明：闪烁会降低观测质量，增大周跳误判的概率；GPS、Galileo、BDS三系统改正数精度分别降低了64.7%、64.0%、247.5%，改正数总数减少了4.5个；PPP-RTK定位误差较平静期增大了11.8倍，固定率下降了55.76%;GPS、Galileo、BDS三系统融合解算可大幅改善定位性能，较单GPS解算定位精度提升了93.06%，固定率提升了51.88%，但仍无法达到平静期的效果. 相似文献
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Xiaopeng Li 《Journal of Geodesy》2011,85(9):597-605
Combining data from a Strapdown Inertial Navigation System and a Differential Global Positioning System (SINS/DGPS) has shown
great promise in estimating gravity on moving platforms. Previous studies on a ground-vehicle system obtained 1–3 mGal precision
with 2 km spatial resolution. High-accuracy Inertial Measurement Units (IMU) and cm-level positioning solutions are very important
in obtaining mGal-level gravity disturbance estimates. However, these ideal configurations are not always available or achievable.
Because the noise level in the SINS/DGPS gravimetric system generally decreases with an increase of speed and altitude of
the platform, the stringent constraints on the IMU and GPS may be relieved in the airborne scenario. This paper presents an
investigation of one navigation-grade and one tactical-grade IMU for the possibility of low-cost INS/GPS airborne gravimetry.
We use the data collected during the Gravity-Lidar Study of 2006 (GLS06), which contains aerogravity, GPS, and INS along the
northern coastline of the Gulf of Mexico. The gravity disturbance estimates from the navigation-grade IMU show 0.5–3.2 mGal
precision compared with the onboard gravimeter’s measurements and better than 3 mGal precision compared with the upward continued
surface control data. Due to relatively large (240 s) smoothing window, the results have about 34 km along-track resolution.
But the gravity estimates from the tactical-grade IMU have much poorer precisions. Nonetheless, useful contributions from
the tactical-grade IMU could be extracted for longer wavelengths. 相似文献
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Xiuxiao Yuan Jianhong Fu Hongxing Sun Charles Toth 《ISPRS Journal of Photogrammetry and Remote Sensing》2009,64(6):541-550
In traditional GPS-supported aerotriangulation, differential GPS (DGPS) positioning technology is used to determine the 3-dimensional coordinates of the perspective centers at exposure time with an accuracy of centimeter to decimeter level. This method can significantly reduce the number of ground control points (GCPs). However, the establishment of GPS reference stations for DGPS positioning is not only labor-intensive and costly, but also increases the implementation difficulty of aerial photography. This paper proposes aerial triangulation supported with GPS precise point positioning (PPP) as a way to avoid the use of the GPS reference stations and simplify the work of aerial photography.Firstly, we present the algorithm for GPS PPP in aerial triangulation applications. Secondly, the error law of the coordinate of perspective centers determined using GPS PPP is analyzed. Thirdly, based on GPS PPP and aerial triangulation software self-developed by the authors, four sets of actual aerial images taken from surveying and mapping projects, different in both terrain and photographic scale, are given as experimental models. The four sets of actual data were taken over a flat region at a scale of 1:2500, a mountainous region at a scale of 1:3000, a high mountainous region at a scale of 1:32000 and an upland region at a scale of 1:60000 respectively. In these experiments, the GPS PPP results were compared with results obtained through DGPS positioning and traditional bundle block adjustment. In this way, the empirical positioning accuracy of GPS PPP in aerial triangulation can be estimated. Finally, the results of bundle block adjustment with airborne GPS controls from GPS PPP are analyzed in detail.The empirical results show that GPS PPP applied in aerial triangulation has a systematic error of half-meter level and a stochastic error within a few decimeters. However, if a suitable adjustment solution is adopted, the systematic error can be eliminated in GPS-supported bundle block adjustment. When four full GCPs are emplaced in the corners of the adjustment block, then the systematic error is compensated using a set of independent unknown parameters for each strip, the final result of the bundle block adjustment with airborne GPS controls from PPP is the same as that of bundle block adjustment with airborne GPS controls from DGPS. Although the accuracy of the former is a little lower than that of traditional bundle block adjustment with dense GCPs, it can still satisfy the accuracy requirement of photogrammetric point determination for topographic mapping at many scales. 相似文献
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A combined algorithm of improving INS error modeling and sensor measurements for accurate INS/GPS navigation 总被引：1，自引：1，他引：1
Although the integrated system of a differential global positioning system (DGPS) and an inertial navigation system (INS)
had been widely used in many geodetic navigation applications, it has sometimes a major limitation. This limitation is associated
with the frequent occurrence of DGPS outages caused by GPS signal blockages in certain situations (urban areas, high trees,
tunnels, etc.). In the standard mechanization of INS/DGPS navigation, the DGPS is used for positioning while the INS is used
for attitude determination. In case of GPS signal blockages, positioning is provided using the INS instead of the GPS until
satellite signals are obtained again with sufficient accuracy. Since the INS has a very short-time accuracy, the accuracy
of the provided INS navigation parameters during these periods decreases with time. However, the obtained accuracy in these
cases is totally dependent on the INS error model and on the quality of the INS sensor data. Therefore, enhanced navigation
parameters could be obtained during DGPS outages if better inertial error models are implemented and better quality inertial
measurements are used. In this paper, it will be shown that better INS error models are obtained using autoregressive processes
for modeling inertial sensor errors instead of Gauss–Markov processes that are implemented in most of the current inertial
systems and, on the other hand, that the quality of inertial data is improved using wavelet multi-resolution techniques. The
above two methods are discussed and then a combined algorithm of both techniques is applied. The performance of each method
as well as of the combined algorithm is analyzed using land-vehicle INS/DGPS data with induced DGPS outage periods. In addition
to the considerable navigation accuracy improvement obtained from each single method, the results showed that the combined
algorithm is better than both methods by more than 30%. 相似文献
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随着差分GPS技术的发展,其应用于工程测量也越来越及,但随着基线长度的增加,常规差分GPS定位精度亦随之降低。为此,本文研究了基于虚拟参考站(Virtual Reference Station,VRS)的差分GPS定位算法,它能有效克服常规差分GPS存在的缺陷,使移动测量用户可在较大空间范围内获得均匀、高精度和可靠的定位结果。 相似文献