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Improving the geometry of Kaguya extended mission data through refined orbit determination using laser altimetry.通过利用激光测高法进行精确轨道测定来改善“辉夜”号延长任务数据的几何精度。
Icarus. 2020 Jan 15;336. doi: 10.1016/j.icarus.2019.113454. Epub 2019 Sep 30.
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Orbit determination of the Lunar Reconnaissance Orbiter: Status after Seven Years.月球勘测轨道飞行器的轨道确定:七年后的状况
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Lunar global shape and polar topography derived from Kaguya-LALT laser altimetry.源自“辉夜号”激光高度计的月球全球形状和极地地形。
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本文引用的文献

1
Orbit determination of the Lunar Reconnaissance Orbiter: Status after Seven Years.月球勘测轨道飞行器的轨道确定:七年后的状况
Planet Space Sci. 2018 Nov 1;162:2-19. doi: 10.1016/j.pss.2017.10.004. Epub 2017 Oct 12.
2
Lunar impact basins revealed by Gravity Recovery and Interior Laboratory measurements.重力恢复与内部实验室测量揭示的月球撞击盆地
Sci Adv. 2015 Oct 30;1(9):e1500852. doi: 10.1126/sciadv.1500852. eCollection 2015 Oct.
3
GRGM900C: A degree 900 lunar gravity model from GRAIL primary and extended mission data.GRGM900C:一个基于圣杯号主要任务和扩展任务数据的900阶月球重力模型。
Geophys Res Lett. 2014 May 28;41(10):3382-3389. doi: 10.1002/2014GL060027. Epub 2014 May 29.
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Gravity field of the Moon from the Gravity Recovery and Interior Laboratory (GRAIL) mission.月球的重力场来自重力恢复和内部实验室(GRAIL)任务。
Science. 2013 Feb 8;339(6120):668-71. doi: 10.1126/science.1231507. Epub 2012 Dec 5.
5
Constraints on the volatile distribution within Shackleton crater at the lunar south pole.限制在月球南极的雪莱顿陨石坑内挥发性物质的分布。
Nature. 2012 Jun 20;486(7403):378-81. doi: 10.1038/nature11216.
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The LCROSS cratering experiment.LCROSS 撞击实验。
Science. 2010 Oct 22;330(6003):468-72. doi: 10.1126/science.1187454.
7
Global distribution of large lunar craters: implications for resurfacing and impactor populations.大型月球陨石坑的全球分布:对覆盖层和撞击器种群的影响。
Science. 2010 Sep 17;329(5998):1504-7. doi: 10.1126/science.1195050.
8
Farside gravity field of the moon from four-way Doppler measurements of SELENE (Kaguya).通过“月亮女神”(辉夜姬)号的四路多普勒测量得到的月球远侧重力场。
Science. 2009 Feb 13;323(5916):900-5. doi: 10.1126/science.1168029.
9
Lunar global shape and polar topography derived from Kaguya-LALT laser altimetry.源自“辉夜号”激光高度计的月球全球形状和极地地形。
Science. 2009 Feb 13;323(5916):897-900. doi: 10.1126/science.1164146.
10
The shape of 433 eros from the NEAR-shoemaker laser rangefinder.近地小行星会合-舒梅克号激光测距仪探测到的433号小行星的侵蚀形状。
Science. 2000 Sep 22;289(5487):2097-101. doi: 10.1126/science.289.5487.2097.

通过利用激光测高法进行精确轨道测定来改善“辉夜”号延长任务数据的几何精度。

Improving the geometry of Kaguya extended mission data through refined orbit determination using laser altimetry.

作者信息

Goossens Sander, Mazarico Erwan, Ishihara Yoshiaki, Archinal Brent, Gaddis Lisa

机构信息

CRESST, University of Maryland, Baltimore County, Baltimore, Maryland, USA.

NASA Goddard Space Flight Center, Greenbelt, Maryland, USA.

出版信息

Icarus. 2020 Jan 15;336. doi: 10.1016/j.icarus.2019.113454. Epub 2019 Sep 30.

DOI:10.1016/j.icarus.2019.113454
PMID:32454532
原文链接:https://pmc.ncbi.nlm.nih.gov/articles/PMC7243822/
Abstract

The Japan Aerospace Exploration Agency's (JAXA) Kaguya spacecraft carried a suite of instruments to map the Moon and its environment globally. During its extended mission, the average altitude was 50 km or lower, and Kaguya science products using these data hence have an increased spatial resolution. However, the geodetic position quality of these products is much worse than that of those acquired during the primary mission (at an altitude of 100 km) because of reduced radiometric tracking and frequent thrusting to maintain spacecraft attitude after the loss of momentum wheels. We have analyzed the Kaguya tracking data using gravity models based on the Gravity Recovery and Interior Laboratory (GRAIL) mission, and by making use of a new data type based on laser altimeter data collected by Kaguya: we adjust the spacecraft orbit such that the altimetry tracks fit a precise topographic basemap based on the Lunar Reconnaissance Orbiter's (LRO) Lunar Orbiter Laser Altimeter (LOLA) data. This results in geodetically accurate orbits tied to the precise LOLA/LRO frame. Whereas previously archived orbits show errors at the level of several a level of several tens of meters. When altimetry data are not available, the combination of GRAIL gravity and radio tracking results in an orbit precision of around several hundreds of meters for the low-altitude phase of the extended mission. Our greatly improved orbits result in better geolocation of the Kaguya extended mission data set.

摘要

日本宇宙航空研究开发机构(JAXA)的“辉夜”号航天器搭载了一套仪器,用于对月球及其环境进行全球测绘。在其延长任务期间,平均高度为50千米或更低,因此利用这些数据生成的“辉夜”号科学产品具有更高的空间分辨率。然而,由于辐射测量跟踪减少以及在动量轮失去作用后为维持航天器姿态而频繁进行推力操作,这些产品的大地测量位置质量比在主要任务期间(高度为100千米)获取的产品要差得多。我们利用基于重力恢复及内部实验室(GRAIL)任务的重力模型,对“辉夜”号的跟踪数据进行了分析,并利用了一种基于“辉夜”号收集的激光高度计数据的新数据类型:我们调整航天器轨道,使测高轨道与基于月球勘测轨道飞行器(LRO)的月球轨道激光高度计(LOLA)数据的精确地形底图相匹配。这产生了与精确的LOLA/LRO框架相关的大地测量精确轨道。而之前存档的轨道显示误差在几十米的水平。当没有测高数据时,GRAIL重力和无线电跟踪相结合,在延长任务的低空阶段可实现约几百米的轨道精度。我们大幅改进的轨道使得“辉夜”号延长任务数据集的地理定位更加精确。