共查询到19条相似文献，搜索用时 93 毫秒
1.
为了评价GPS与VLBI这两种空间技术测定的地心坐标的真正实现精度,选择使用它们的并置站坐标数据,在进行了历元改正和偏心改正后,计算了这两种技术实现的参考架的转换参数,并分析了它们坐标不符值的中误差,得出GPS与VLBI这两种技术实现的参考架的外符合精度在1cm之内,表明了GPS与VLBI这两种技术测定的地心坐标精度已经达到毫米量级。 相似文献
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随着我国GPS一级网的成功建立及GPS二级网工作的顺利展开,建立我国高精度地心坐标系统的条件已日臻成熟。目前为了满足某些工程测量的需要,利用现有的全国高精度GPS一级网及天文大地网资料,求得了WGS—84坐标系与BJZ54坐标系(整体平差转换值)的转换参数,该转换参数的出现,已引起有关专家及应用部门的关注。 相似文献
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国际地球参考框架(ITRF)是目前理论背景最完善、构建方法最全面、实现精度最高的全球地心基准,也是世界各国在建立区域地心基准时的重要参考。给出了国际地球自转与参考系统服务组织(IERS)最新发布的ITRF2020的理论定义,重点讨论了各专业技术组织提供的数据资源和计算模型,以及IERS在数据整合时的处理策略,并对基于震后形变(PSD)模型的位置计算进行了讨论,给出了相对于ITRF2014的改进和转换参数。ITRF2020首次区分了地球的质量中心和形状中心,并考虑了PSD模型的季节性信号,提高了坐标框架精度,为地球科学研究和应用提供了统一基准,对精化和维持我国地心参考框架具有重要参考意义。 相似文献
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介绍ITRF2014的定义、测站分布、输入数据、分析策略以及与ITRF2008的转换参数,并分析ITRF2014相对于ITRF2008的改进。ITRF2014是国际地球参考框架ITRF的最近一次更新,它是基于四种空间大地测量技术(VLBI、SLR、GNSS和DORIS)重新处理解实现的。相较于ITRF2008,ITRF2014不仅在观测数据和测站数量上有所增加,还改善了对非线性运动的处理,包括对周期性信号的估计以及对震后形变(post-seismic deformation,PSD)的改正,并提供了PSD模型和地球质心运动模型两个新产品。ITRF2014为地球科学等相关领域的研究与应用提供了统一的空间基准,也为其他坐标框架的维持与精化提供了参考。 相似文献
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GPS水准拟合与精度分析 总被引：3，自引：2，他引：1
本文首先分析了目前GPS水准拟合方法中存在的问题,详细的阐述了WGS-84大地高与我国所采用的正常高之间的关系,提出了先进行平面内的坐标转换,再分别采用各种数学模型进行GPS水准拟合的方法。通过对大连地区实测GPS资料的试验表明:利用本文所讨论的方法求出的GPS水准可以达到1.41cm的精度,能够满足大比例快速测图的要求。 相似文献
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坐标系统的统一是1个地区地理信息资源共享和标准统一的基础,目前,很多地区采用多个测量坐标系统,为实现测量坐标系统的统一,需要对不同坐标系的地理信息成果进行坐标转换。本文结合青岛市实际,对青岛市已有地理信息由原来采用的"青岛市城市坐标系"向国家统一的"1980西安坐标系"之间的转换精度和可靠性进行了探讨,通过具体数据的分析计算得出,2套坐标系之间转换切实可行,完全满足精度要求。 相似文献
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起算点精度对GPS基线解算质量的影响 总被引：1，自引：0，他引：1
基线处理时要求知道一个点的坐标,其精度对GPS基线的解算结果有影响。采用实测数据研究起算点精度对GPS基线解算质量的影响,得出了其影响规律,同时给出了提高起算点精度的方法。 相似文献
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为实现远岸潮汐精确监测,基于GPS PPK技术开展了远距离高精度GPS验潮方法研究。研究给出了GPS潮位测量方法,其次联合GPS定位信息和IMU姿态信息,通过坐标转换原理得到瞬时水面的精确高程。在此基础上,研究利用基于FFT的低通滤波技术提取潮位信息。最后在烟台港进行了实际工程试验。试验结果表明,当GPS PPK验潮距离达98km时,潮位误差可控在!15cm以内,验潮精度仍可优于10cm。 相似文献
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PIERRE EXERTIER JOËLLE NICOLAS PHILIPPE BERIO DAVID COULOT PASCAL BONNEFOND OLIVIER LAURAIN 《Marine Geodesy》2013,36(1-2):333-340
The French Transportable Laser Ranging System (FTLRS), a highly transportable Satellite Laser Ranging (SLR) instrument, was set up in Corsica (from January to September 2002) for participating to the JASON-1 altimeter verification phase. In addition to the tracking of oceanographic satellite missions and in order to perform an accurate positioning, the FTLRS also acquired laser ranging data on geodetic satellites, STARLETTE and STELLA essentially. The paper describes the analysis strategy mainly based on the use of a short-arc orbit technique to compute accurate 1 cm local orbits, and then the geocentric positioning (2–3 mm relative to GPS). Finally, we established the JASON-1 absolute calibration value, based on 9 SLR short-arcs (between cycles 1 and 26), at 108.2 ± 8.7 mm; the 10-day repeatability is of 26.1 mm showing that a great accuracy has been reached. 相似文献
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Pierre Exertier Joë lle Nicolas Philippe Berio David Coulot Pascal Bonnefond Olivier Laurain 《Marine Geodesy》2004,27(1):333-340
The French Transportable Laser Ranging System (FTLRS), a highly transportable Satellite Laser Ranging (SLR) instrument, was set up in Corsica (from January to September 2002) for participating to the JASON-1 altimeter verification phase. In addition to the tracking of oceanographic satellite missions and in order to perform an accurate positioning, the FTLRS also acquired laser ranging data on geodetic satellites, STARLETTE and STELLA essentially.
The paper describes the analysis strategy mainly based on the use of a short-arc orbit technique to compute accurate 1 cm local orbits, and then the geocentric positioning (2-3 mm relative to GPS). Finally, we established the JASON-1 absolute calibration value, based on 9 SLR short-arcs (between cycles 1 and 26), at 108.2 ± 8.7 mm; the 10-day repeatability is of 26.1 mm showing that a great accuracy has been reached. 相似文献
The paper describes the analysis strategy mainly based on the use of a short-arc orbit technique to compute accurate 1 cm local orbits, and then the geocentric positioning (2-3 mm relative to GPS). Finally, we established the JASON-1 absolute calibration value, based on 9 SLR short-arcs (between cycles 1 and 26), at 108.2 ± 8.7 mm; the 10-day repeatability is of 26.1 mm showing that a great accuracy has been reached. 相似文献
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《Marine Geodesy》2013,36(3-4):399-421
The Jason-1 radar altimeter satellite, launched on December 7, 2001 is the follow on to the highly successful TOPEX/Poseidon (T/P) mission and will continue the time series of centimeter level ocean topography measurements. Orbit error is a major component in the overall error budget of all altimeter satellite missions. Jason-1 is no exception and has set a 1-cm radial orbit accuracy goal, which represents a factor of two improvement over what is currently being achieved for T/P. The challenge to precision orbit determination (POD) is both achieving the 1-cm radial orbit accuracy and evaluating the performance of the 1-cm orbit. There is reason to hope such an improvement is possible. The early years of T/P showed that GPS tracking data collected by an on-board receiver holds great promise for precise orbit determination. In the years following the T/P launch there have been several enhancements to GPS, improving its POD capability. In addition, Jason-1 carries aboard an enhanced GPS receiver and significantly improved SLR and DORIS tracking systems along with the altimeter itself. In this article we demonstrate the 1-cm radial orbit accuracy goal has been achieved using GPS data alone in a reduced dynamic solution. It is also shown that adding SLR data to the GPS-based solutions improves the orbits even further. In order to assess the performance of these orbits it is necessary to process all of the available tracking data (GPS, SLR, DORIS, and altimeter crossover differences) as either dependent or independent of the orbit solutions. It was also necessary to compute orbit solutions using various combinations of the four available tracking data in order to independently assess the orbit performance. Towards this end, we have greatly improved orbits determined solely from SLR+DORIS data by applying the reduced dynamic solution strategy. In addition, we have computed reduced dynamic orbits based on SLR, DORIS, and crossover data that are a significant improvement over the SLR- and DORIS-based dynamic solutions. These solutions provide the best performing orbits for independent validation of the GPS-based reduced dynamic orbits. The application of the 1-cm orbit will significantly improve the resolution of the altimeter measurement, making possible further strides in radar altimeter remote sensing. 相似文献
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The 1-Centimeter Orbit: Jason-1 Precision Orbit Determination Using GPS, SLR, DORIS, and Altimeter Data 总被引：1，自引：0，他引：1
S. B. Luthcke N. P. Zelensky D. D. Rowlands F. G. Lemoine T. A. Williams 《Marine Geodesy》2003,26(3):399-421
The Jason-1 radar altimeter satellite, launched on December 7, 2001 is the follow on to the highly successful TOPEX/Poseidon (T/P) mission and will continue the time series of centimeter level ocean topography measurements. Orbit error is a major component in the overall error budget of all altimeter satellite missions. Jason-1 is no exception and has set a 1-cm radial orbit accuracy goal, which represents a factor of two improvement over what is currently being achieved for T/P. The challenge to precision orbit determination (POD) is both achieving the 1-cm radial orbit accuracy and evaluating the performance of the 1-cm orbit. There is reason to hope such an improvement is possible. The early years of T/P showed that GPS tracking data collected by an on-board receiver holds great promise for precise orbit determination. In the years following the T/P launch there have been several enhancements to GPS, improving its POD capability. In addition, Jason-1 carries aboard an enhanced GPS receiver and significantly improved SLR and DORIS tracking systems along with the altimeter itself. In this article we demonstrate the 1-cm radial orbit accuracy goal has been achieved using GPS data alone in a reduced dynamic solution. It is also shown that adding SLR data to the GPS-based solutions improves the orbits even further. In order to assess the performance of these orbits it is necessary to process all of the available tracking data (GPS, SLR, DORIS, and altimeter crossover differences) as either dependent or independent of the orbit solutions. It was also necessary to compute orbit solutions using various combinations of the four available tracking data in order to independently assess the orbit performance. Towards this end, we have greatly improved orbits determined solely from SLR+DORIS data by applying the reduced dynamic solution strategy. In addition, we have computed reduced dynamic orbits based on SLR, DORIS, and crossover data that are a significant improvement over the SLR- and DORIS-based dynamic solutions. These solutions provide the best performing orbits for independent validation of the GPS-based reduced dynamic orbits. The application of the 1-cm orbit will significantly improve the resolution of the altimeter measurement, making possible further strides in radar altimeter remote sensing. 相似文献
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With the implementation of the Jason-1 satellite altimeter mission, the goal of reaching the 1-cm level in orbit accuracy was set. To support the Precision Orbit Determination (POD) requirements, the Jason-1 spacecraft carries receivers for DORIS (Doppler Orbitography and Radiopositioning Integrated by Satellite) and GPS (Global Positioning System), as well as a retroreflector for SLR (Satellite Laser Ranging). The overall orbit accuracy for Jason will depend on the quality and the relative weighting of the available tracking data. In this study, the relative importance of the SLR, DORIS, and GPS tracking data is assessed along with the most effective parameterization for accounting for the unmodeled accelerations through the application of empirical accelerations. The optimal relative weighting for each type of tracking data was examined. It is demonstrated that GPS tracking alone is capable of supporting a radial orbit accuracy for Jason-1 at the 1-cm level, and that including SLR tracking provides additional benefits. It is also shown that the GRACE (Gravity Recovery and Climate Experiment) gravity model GGM01S provides a significant improvement in the orbit accuracy and reduction in the level of geographically correlated orbit errors. 相似文献
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With the implementation of the Jason-1 satellite altimeter mission, the goal of reaching the 1-cm level in orbit accuracy was set. To support the Precision Orbit Determination (POD) requirements, the Jason-1 spacecraft carries receivers for DORIS (Doppler Orbitography and Radiopositioning Integrated by Satellite) and GPS (Global Positioning System), as well as a retroreflector for SLR (Satellite Laser Ranging). The overall orbit accuracy for Jason will depend on the quality and the relative weighting of the available tracking data. In this study, the relative importance of the SLR, DORIS, and GPS tracking data is assessed along with the most effective parameterization for accounting for the unmodeled accelerations through the application of empirical accelerations. The optimal relative weighting for each type of tracking data was examined. It is demonstrated that GPS tracking alone is capable of supporting a radial orbit accuracy for Jason-1 at the 1-cm level, and that including SLR tracking provides additional benefits. It is also shown that the GRACE (Gravity Recovery and Climate Experiment) gravity model GGM01S provides a significant improvement in the orbit accuracy and reduction in the level of geographically correlated orbit errors. 相似文献
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GPS测量直接获得点位的精确三维坐标,通过空间直角坐标系、大地坐标系、站心地平直角坐标系、站心极坐标系等一系列转换,再加入大气折光差改正和垂线偏差改正,就可以快速获得设备标校所需的精确基准。与采用常规测量方法、分别计算设备标校基准相比,不仅大大减少了工作量,还提高了计算结果的精度。 相似文献
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Comparing to single BeiDou Navigation Satellite System (BDS) Precise Point Positioning (PPP), a method which can more quicklydetermine the ambiguity parameters of BDS through applying the contribution of GPS observations is proposed and analyzed in this article. The numerical examples and analysis show that the ionosphere-free ambiguities of BDS satellites can be determined and converged more quickly because of the contribution of GPS observations. The average improvement of the convergent speed of positioning is 18.5% and its positioning accuracy in N, E, and U components are improved by 29.4, 30.3, and 34.4%, respectively, with the contribution of the a priori coordinates obtained from GPS observations. This method is useful for single BDS system positioning when there is a priori information provided by GPS or other sensors which be replaced by and can be applied at the beginning of the computation. 相似文献