共查询到17条相似文献，搜索用时 187 毫秒
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针对北斗卫星导航系统(BDS)在轨卫星原子钟的评估问题,从三个性能指标即准确度、漂移率和稳定性出发进行了评估,并利用同一时段的GPS/GLONASS星载原子钟性能评估结果做了比较。算例采用GPS 1751-1758共8周的数据,评估结果发现:BDS在轨卫星的准确度在10-11量级,漂移率在10-15量级,与GPS/GLONASS星载原子钟的水平相当,但钟的稳定性方面由于BDS存在着几颗天稳较大的钟,所以其天稳的平均值在10-13量级,比GPS和GLONASS卫星略差。 相似文献
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为研究满足HY-2B星载GPS定轨要求的EGM2008重力场模型合理阶次和HY-2B卫星简化动力学定轨精度,采用HY-2B卫星14天星载GPS观测数据及不同阶次EGM2008重力场,进行简化动力学轨道确定。结果表明：采用120阶及以上阶次的EGM2008重力场模型,能够获得厘米级高精度定轨结果。同时,检核结果显示：采用简化动力学法定轨时,载波相位残差结果稳定在6.2～6.8 mm之间,重叠轨道对比结果在轨道径向、切向、法向上均优于0.6 cm, SLR检核整体轨道精度优于4 cm。定轨结果满足测高卫星需求,可为后续我国海洋系列卫星精密轨道确定等相关科学研究提供借鉴。 相似文献
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从地球重力场测量要素出发,按照局部重力场模型、区域重力场模型、全球重力场模型求解的发展思路,分析了对地球重力场测量技术手段的要求。根据高-低卫星跟踪卫星的距离和距离变率开展定轨研究的概念,梳理了卫星跟踪卫星重力测量系统的发展。针对卫星跟踪卫星重力测量技术的内涵,分析了高-低卫星跟踪卫星测量模式（SST-hl）和高-低低卫星跟踪卫星测量模式（SST—hll）的地球重力场测量本质。 相似文献
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对3颗高度计卫星TOPEX/POSEIDON(TP),Jason-1(J1),Jason-2(J2)自1992—2011年683个重复周期,共18.6年的数据进行分析,得到全球海洋潮汐调和常数,并重点分析了采用不同样本大小的卫星高度计数据对潮汐信息提取的准度和精度所带来的影响。研究结果表明,参与分析的卫星高度计数据观测样本数的增加可以降低其反演潮汐各分潮振幅时的误差。观测时间为18.6年的高度计数据调和分析所得的主要半日分潮与实测比较,其振幅差相比于利用10年数据的计算结果减小约0.5cm;但是由于忽略了卫星更替过程所带来的观测时间差来进行调和分析,将会对计算分析过程中产生的迟角误差造成影响,主要全日分潮的迟角误差增加约2°,而半日潮迟角误差的改变则比较小。本文进一步用理想化实验解释了造成这种迟角计算误差变化的原因,比较了轨道交叉点上,由卫星在升轨和降轨2个轨道上各自的观测数据计算得到的调和常数,发现随着参与分析的高度计观测样本数的增加,调和分析计算潮汐调和常数时的内符精度也会显著提高。利用18.6年数据比利用10年数据进行调和分析时,主要半日潮调和常数的精度提高了约7%。 相似文献
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YOKE T. YOON STEVEN R. NEREM MICHAEL M. WATKINS BRUCE J. HAINES GERHARD L. KRUIZINGA 《Marine Geodesy》2013,36(3-4):773-787
We have used GPS carrier phase integer ambiguity resolution to investigate improvements in the orbit determination for the Jason-1 satellite altimeter mission. The technique has been implemented in the GIPSY orbit determination software developed by JPL. The radial accuracy of the Jason-1 orbits is already near 1 cm, and thus it is difficult to detect the improvements gained when the carrier phase ambiguities are resolved. Nevertheless, each of the metrics we use to evaluate the orbit accuracy (orbit overlaps, orbit comparisons, satellite laser ranging residuals, altimeter crossover residuals, orbit centering) show modest improvement when the ambiguities are resolved. We conservatively estimate the improvement in the radial orbit accuracy is at the 10–20% level. 相似文献
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海洋二号卫星厘米级定轨的实施建议 总被引：1，自引：0，他引：1
针对海洋二号（HY-2）卫星如何实现厘米级定轨问题,提出下列建议：海洋二号卫星不必采用DORIS定轨;给海洋二号卫星装备无电功耗需求的激光后向反射镜阵列,以便对它进行多个SRL测站观测的激光厘米级定轨;给海洋二号卫星装备具有双频载波相位测量能力的GPS信号接收机,实现高精度的星载GPS测量定轨. 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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《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