The Gravity Probe B (GP-B) satellite has recently completed its science mission. The payload is equipped with two redundant TANS Vector III GPS receivers, used to reconcile vehicle time with Coordinated Universal Time (UTC) and to provide coarse satellite position data. GPS position accuracy easily outperforms mission requirements of 100 m RMS per axis for onboard solutions. The GP-B precision orbit is determined in ground processing of 30-hour and 18-hour GPS data segments using MicroCosm software. Overlaps of consecutive 18-hour ephemeris segments are found to have maximum position errors whose RMS is 2.5 meters, and maximum velocity errors whose RMS is 2.2 mm/sec. Satellite Laser Ranging (SLR) measurements provide independent verification of the GPS-derived GP-B orbit. This paper begins with a brief background of the GP-B mission including a description of the GPS equipment and orbit determination operations. GP-B ephemeris errors estimated using ephemeris overlap comparisons and SLR residual computations are detailed. We conclude with a brief description of in-progress investigations that are anticipated to improve results.
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机译:重力探测B(GP-B)卫星最近完成了其科学使命。有效载荷配备了两个冗余烘焙仪III GPS接收器,用于协调车辆时间与协调的通用时间(UTC),并提供粗略卫星位置数据。 GPS位置精度容易优于每轴100米RMS的任务要求,用于车载解决方案。使用MicrocoSM软件在30小时和18小时GPS数据段的地面处理中确定GP-B精密轨道。连续18小时的星历遗物段的重叠具有最大位置误差,其RMS为2.5米,最大速度误差为2.2 mm / sec。卫星激光测距(SLR)测量提供了对GPS衍生的GP-B轨道的独立验证。本文始于GP-B任务的简要背景,包括GPS设备和轨道确定操作的描述。使用星麦宫重叠比较和SLR残差计算估计的GP-B闭文误差。我们结束了预期改善结果的进展调查的简要说明。
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