IGS超快速产品(近)实时应用

T.A. Springer, U. Hugentobler
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引用次数: 70

摘要

自2000年3月5日第1052周以来,IGS正在生产一种新的组合轨道,称为IGS超快速产品,IGU。综合IGS超快速产品每天在UTC时间3:00和15:00提供两次,在包含的数据间隔结束后延迟3小时,并基于多达七个不同的IGS分析中心的解决方案。产生超快速产品的主要原因是对近实时大气监测(例如天气预报)的及时性和准确性的要求。每个超高速轨道文件覆盖48小时。轨道的前24小时是基于实际的GPS观测(实际轨道),后24小时是外推(预测轨道)。与IGS预测轨道(IGP)一样,超快速轨道可用于实时使用。然而,超高速轨道的质量应该明显更好,因为预测的平均年龄从36小时(IGP)减少到9小时(IGU)。在华盛顿特区的USNO举行的2000 IGS分析中心研讨会上,决定IGU产品的质量足以取代IGP产品。这一变化于11月5日生效,同时也是全球定位系统第1087周的开始。我们将证明IGS超快速轨道的精度在加权均方根意义上达到30 cm水平,这明显优于IGS预测轨道的70 cm精度。我们还将证明,利用这种轨道质量,有可能得出对流层天顶路径延迟估计,其精度为7毫米,相当于大约1毫米的可降水量。只有当“坏的”卫星预测被(自动)检测和处理时,才能达到这种精度。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
IGS ultra rapid products for (near-) real-time applications

Since GPS week 1052, 5 March 2000, the IGS is producing a new combined orbit called the IGS Ultra rapid product, IGU. The combined IGS Ultra rapid products are being made available twice every day, at 3:00 and 15:00 UTC, with a delay of 3 hours after the end of the included data interval, and are based on solutions from up to seven different IGS Analysis Centers. The main reason for the generation of the Ultra rapid products are the requirements, in both timeliness and accuracy, for near-real-time atmospheric monitoring, e.g., weather predictions. Each ultra rapid orbit file covers 48 hours. The first 24 hours of the orbit are based on actual GPS observations (real orbit), the second 24 hours are extrapolated (predicted orbit). Like the IGS Predicted (IGP) orbits, the Ultra rapid orbits are available for real-time usage. However, the quality of the Ultra rapid orbits should be significantly better because the average age of the predictions is reduced from 36 hours (IGP) to 9 hours (IGU). At the 2000 IGS Analysis Center workshop, held at the USNO in Washington, D.C., it was decided that the IGU products were of sufficient quality to replace the IGP products. This change took effect on November 5 with the start of GPS week 1087.

We will demonstrate that the accuracy of the IGS Ultra rapid orbits is at the 30 cm level, in a weighted RMS sense, which is significantly better than the 70 cm accuracy of the IGS Predicted orbits. We will also demonstrate that with this orbit quality it is possible to derive tropospheric zenith path delay estimates with a precision of 7 mm, which corresponds to approximately 1 mm precipitable water vapor. This level of precision is only achieved when “bad” satellite predictions are (automatically) detected and handled.

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