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1.
Pascal Willis Claude Boucher Hervé Fagard Zuheir Altamimi 《Comptes Rendus Geoscience》2005,337(7):653-662
IGN is in charge of the installation and maintenance of the DORIS orbit determination network. More recently, in collaboration with JPL, precise geodetic computations were performed. The goal of this paper is to recall the various historic contributions of IGN to the DORIS system in their international context and then to describe a new estimation technique developed for a multi-satellite mode, making full profit of a better modeling for satellites and ground clocks as well as tropospheric correction parameters. Derived geodetic results demonstrate a precision in the order of 1 cm for station positions. To cite this article: P. Willis et al., C. R. Geoscience 337 (2005). 相似文献
2.
现代大地测量的进展主要是空间大地测量的进展 ,而空间大地测量的进展以 GPS的进展最为突出。因此 ,本刊曾在 2 0 0 0年 4期和 2 0 0 1年 1期连载了 GPS的最新进展。现陆续介绍现代空间大地测量最新进展的全貌 ,包括 :1.空间大地测量最新进展的概况 ;2 .甚长基线干涉测量 (VL BI)的最新进展 ;3.激光测月 (L L R)和激光测卫 (SL R)的最新进展 ;4.卫星雷达测高的最新进展 ;5 .合成孔径雷达干涉测量 (INSAR)的最新进展 ;6 .由卫星集成的多普勒和无线电定位系统 (DORIS)的最新进展等 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
5.
CHRISTIAN JAYLES PATRICK VINCENT FABIEN ROZO FABIEN BALANDREAUD 《Marine Geodesy》2013,36(3-4):753-771
DIODE (Doris Immediate On-board orbit DEtermination) is a series of real-time orbit determination software, which process one-way up-link Doppler measurements performed by a DORIS receiver on a satellite. The DIODE software are embedded within the DORIS receivers, and they provide orbit and time determination to the user as well as technical parameters to adjust the tracking loop within the instrument. After a first successful flight on-board SPOT4, the second generation of the family operates on-board Jason-1, with more efficient and more accurate algorithms. Similar versions have been embarked onboard SPOT5 and ENVISAT. The accuracy is between 10 and 30 centimeters RMS for the radial component, and about 50 centimeters RMS in 3D. With several Failure Detection and Incident Recovery (FDIR) enhancements implemented in the software, DIODE/Jason-1 has experienced only one anomaly in July 2004; its availability is 99.7%, after two years and a half in-orbit. This article describes the DORIS/DIODE element of the Jason-1 system. It summarizes the main results obtained from the various verification activities that concerned all parts of this navigation and time-tagging Jason-1 subsystem. 相似文献
6.
Systematic biases in DORIS-derived geocenter time series related to solar radiation pressure mis-modeling 总被引：2，自引：1，他引：1
M. L. Gobinddass P. Willis O. de Viron A. Sibthorpe N. P. Zelensky J. C. Ries R. Ferland Y. Bar-Sever M. Diament 《Journal of Geodesy》2009,83(9):849-858
As any satellite geodesy technique, DORIS can monitor geocenter variations associated to mass changes within the Earth–Atmosphere–Continental
hydrosphere–Oceans system. However, especially for the Z-component, corresponding to a translation of the Earth along its rotation axis, the estimated geocenter is usually affected
by large systematic errors of unknown cause. By reprocessing old DORIS data, and by analyzing single satellite solutions in
the frequency domain, we show that some of these errors are satellite-dependent and related to the current DORIS orbit determination
strategy. In particular, a better handling of solar pressure radiation effects on SPOT-2 and TOPEX satellites is proposed
which removes a large part of such artifacts. By empirically multiplying the current solar pressure model with a single coefficient
(1.03 for TOPEX/Poseidon after 1993.57, and 0.96 before; and 1.08 for SPOT-2) estimated over a long time period, we can improve
the measurement noise of the Z-geocenter component from 47.5 to 30.4 mm for the RMS and from 35 to 6 mm for the amplitude of the annual signal. However,
the estimated SRP coefficient for SPOT-2 presents greater temporal variability, indicating that a new, dedicated solar radiation
pressure model is still needed for precise geodetic applications. In addition, for the TOPEX satellite, a clear discontinuity
of unknown cause is also detected on July 27, 1993. 相似文献
7.
针对GPS、SLR和DORIS三种不同手段的各自定轨精度问题,本文基于不同的轨道评估方法进行了深入分析。以JASON-2卫星为例,分析了姿态模型误差及其对定轨精度的影响,分别讨论了GPS、SLR和DORIS的定轨策略和定轨精度,并基于轨道评估结果进行了轨道叠加。基于实测数据进行了试验,试验结果表明,JASON-2卫星姿态模型误差对DORIS、GPS和SLR轨道影响分别为0.040、0.036和0.033m;DORIS定轨结果优于GPS和SLR,SLR定轨精度最差;基于SLR验证和轨道重叠结果加权,对GPS、SLR和DORIS轨道进行轨道叠加,其精度一致,通过与JPL轨道比较,其径向精度为2cm。 相似文献
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DORIS applications for solid earth and atmospheric sciences 总被引：2，自引：0，他引：2
Pascal Willis Laurent Soudarin Christian Jayles Lucie Rolland 《Comptes Rendus Geoscience》2007,339(16):949-959
9.
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
10.