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Same-beam VLBI observations of SELENE for improving lunar gravity field model

Authors :
Noriyuki Namiki
Xiaoyu Hong
Yusufu Aili
Simon Ellingsen
Nobuyuki Kawano
Katsunori M. Shibata
Gerhard Kronschnabl
Takahiro Iwata
Qian Huang
Jinsong Ping
Wenjun Yang
Qing-Yuan Fan
W. Hankey
Tao An
Qinghui Liu
Bo Xia
Y. Harada
Yoshihiko Tamura
Osamu Kameya
Seiitsu Tsuruta
Kenzaburo Iwadate
Hideo Hanada
Kazuyoshi Asari
B Reid
F. Kikuchi
Hirotomo Noda
H Zhang
Yoshiaki Ishihara
Takaaki Jike
Jamie McCallum
Koji Matsumoto
Sho Sasaki
Wolfgang Schlüter
K. Sato
Xian Shi
T Ishikawa
Sander Goossens
Shunichi Kamata
Source :
Radio Science. 45
Publication Year :
2010
Publisher :
American Geophysical Union (AGU), 2010.

Abstract

The Japanese lunar mission, Selenological and Engineering Explorer (Kaguya), which was successfully launched on 14 September 2007, consists of a main satellite and two small satellites, Rstar and Vstar. Same-beam very long baseline interferometry (VLBI) observations of Rstar and Vstar were performed for 15.4 months from November 2007 to February 2009 using eight VLBI stations. In 2008, S band same-beam VLBI observations totaling 476 h on 179 days were undertaken. The differential phase delays were successfully estimated for most ( about 85%) of the same-beam VLBI observation periods. The high success rate was mainly due to the continuous data series measuring the differential correlation phase between Rstar and Vstar. The intrinsic measurement error in the differential phase delay was less than 1 mm RMS for small separation angles and increased to approximately 2.5 mm RMS for the largest separation angles ( up to 0.56 deg). The long-term atmospheric and ionospheric delays along the line of sight were reduced to a low level ( several tens of milimeters) using the same-beam VLBI observations, and further improved through application of GPS techniques. Combining the eight-station ( four Japanese telescopes of VLBI Exploration of Radio Astrometry and four international telescopes) S band same-beam VLBI data with Doppler and range data, the accuracy of the orbit determination was improved from a level of several tens of meters when only using Doppler and range data to a level of 10 m. As a preliminary test of the technique, the coefficient sigma degree variance of the lunar gravity field was compared with and without 4 months of VLBI data included. A significant reduction below around 10 deg ( especially for the second degree) was observed when the VLBI data were included. These observations confirm that the VLBI data contribute to improvements in the accuracy of the orbit determination and through this to the lunar gravity field model.

Details

ISSN :
00486604
Volume :
45
Database :
OpenAIRE
Journal :
Radio Science
Accession number :
edsair.doi...........4a7e01729cf813cda70b22a756bebdc8
Full Text :
https://doi.org/10.1029/2009rs004203