Intersatellite laser ranging instrument for the GRACE follow-on mission

Intersatellite laser ranging instrument for the GRACE follow-on mission
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DOI:
10.1007/s00190-012-0566-3
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发表时间:
2012-12-01
期刊:
影响因子:
4.4
通讯作者:
Folkner, W. M.
Folkner, W. M.
中科院分区:
地球科学1区
文献类型:
--
作者:
Sheard, B. S.;Heinzel, G.;Folkner, W. M.

文献摘要

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重力恢复和气候实验(GRACE)表明,低-低卫星间跟踪能够监测全球范围内地球重力场的时间变化,特别是由水圈内的质量传输引起的变化。由于长期持续监测地球引力场变化的重要性以及GRACE的寿命有限,目前计划于2017年发射后续任务。为了最大限度地减少风险和发射时间,后续任务将基本上是GRACE的重建,以微波测距作为测量星间距离变化的主要仪器。激光干涉测量法已被提议作为一种为未来类似 GRACE 任务提高测距精度的方法,因此预计将作为演示实验纳入目前正在开发的后续任务中。本文介绍了干涉式激光测距系统的顶层架构,旨在演示该技术也可以与 GRACE 后续任务的微波测距系统并行运行。
The Gravity Recovery and Climate Experiment (GRACE) has demonstrated that low-low satellite-to-satellite tracking enables monitoring the time variations of the Earth's gravity field on a global scale, in particular those caused by mass-transport within the hydrosphere. Due to the importance of long-term continued monitoring of the variations of the Earth's gravitational field and the limited lifetime of GRACE, a follow-on mission is currently planned to be launched in 2017. In order to minimise risk and the time to launch, the follow-on mission will be basically a rebuild of GRACE with microwave ranging as the primary instrument for measuring changes of the intersatellite distance. Laser interferometry has been proposed as a method to achieve improved ranging precision for future GRACE-like missions and is therefore foreseen to be included as demonstrator experiment in the follow-on mission now under development. This paper presents the top-level architecture of an interferometric laser ranging system designed to demonstrate the technology which can also operate in parallel with the microwave ranging system of the GRACE follow-on mission.