2019
DOI: 10.1029/2019gl085252
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Topographic Evolution of Von Kármán Crater Revealed by the Lunar Rover Yutu‐2

Abstract: Chang'e‐4 (CE‐4) achieved the first farside landing in Von Kármán crater. In the landing site, linear features have been identified previously from SLDEM and considered to be ejecta from the neighboring Finsen crater. The 5 cm grid spacing digital elevation model of the landing site, generated from the rover's panoramic images, provides more details of the rugged terrain. We further interpret the superimposition of NE‐SW ejecta from Finsen crater on the underlying SE‐NW dome‐like surface relief from Alder crat… Show more

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Cited by 40 publications
(41 citation statements)
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“…The mapping and localization products have also been frequently used to support various scientific investigations before and during the missions, e.g. to support data acquisition and analysis by other science instruments, such as the Visible and Near-Infrared Imaging Spectrometer (VNIS) and the Lunar Penetrating Radar (LPR) for investigations of mineralogical compositions and subsurface structures, respectively (Xiao et al 2015;Di et al 2016;Gou et al 2019;Di et al 2019b). Figure 2 shows the technical framework of the geospatial technologies developed and applied in CE-3 and CE-4 missions.…”
Section: Data and Technical Frameworkmentioning
confidence: 99%
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“…The mapping and localization products have also been frequently used to support various scientific investigations before and during the missions, e.g. to support data acquisition and analysis by other science instruments, such as the Visible and Near-Infrared Imaging Spectrometer (VNIS) and the Lunar Penetrating Radar (LPR) for investigations of mineralogical compositions and subsurface structures, respectively (Xiao et al 2015;Di et al 2016;Gou et al 2019;Di et al 2019b). Figure 2 shows the technical framework of the geospatial technologies developed and applied in CE-3 and CE-4 missions.…”
Section: Data and Technical Frameworkmentioning
confidence: 99%
“…The DEM and DOM have been used in topographic characterization (e.g. slop and crater distributions) of CE-3 and CE-4 landing sites (Wu, Hu, and Guo 2014;Di et al 2019b;Di, Liu, and Liu 2019c;Zhao, Li, and Wu 2019). CE-2 orbiter acquired 1.5-m resolution images at the pre-selected CE-3 landing site (40°N~50°N, 18°W 35°W).…”
Section: Landing Site Mapping Using Orbital Imagesmentioning
confidence: 99%
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