Overview of Differential VLBI Observations of Lunar Orbiters in SELENE (Kaguya) for Precise Orbit Determination and Lunar Gravity Field Study

被引:9
|
作者
Hanada, Hideo [1 ]
Iwata, Takahiro [2 ]
Liu, Qinghui [3 ]
Kikuchi, Fuyuhiko [1 ]
Matsumoto, Koji [1 ]
Goossens, Sander [1 ]
Harada, Yuji [1 ]
Asari, Kazuyoshi [1 ]
Ishikawa, Toshiaki [1 ]
Ishihara, Yoshiaki [1 ]
Noda, Hirotomo [1 ]
Tsuruta, Seiitsu [1 ]
Petrova, Natalia [4 ]
Kawano, Nobuyuki [3 ,5 ]
Sasaki, Sho [1 ]
Sato, Kaori [1 ]
Namiki, Noriyuki [6 ]
Kono, Yusuke [7 ]
Iwadate, Kenzaburo [8 ]
Kameya, Osamu [8 ]
Shibata, Katsunori M. [7 ]
Tamura, Yoshiaki [8 ]
Kamata, Shunichi [9 ]
Yahagi, Yukihiro [10 ]
Masui, Wataru [11 ]
Tanaka, Koji [2 ]
Maejima, Hironori [12 ]
Hong, Xiaoyu [3 ]
Ping, Jinsong [3 ]
Shi, Xian [3 ]
Huang, Qian [3 ]
Aili, Yusufu [13 ]
Ellingsen, Simon [14 ]
Schlueter, Wolfgang [15 ]
机构
[1] Natl Astron Observ Japan, RISE Project, Oshu, Iwate 0230861, Japan
[2] Japan Aerosp Explorat Agcy, Inst Space & Astronaut Sci, Sagamihara, Kanagawa 2298510, Japan
[3] Chinese Acad Sci, Shanghai Astron Observ, Shanghai 200030, Peoples R China
[4] Kazan VI Lenin State Univ, Kazan 420008, Russia
[5] Oushu Space & Astron Museum, Oshu, Iwate 0230861, Japan
[6] Chiba Inst Technol, Chiba 2750016, Japan
[7] Natl Astron Observ Japan, Mizusawa VLBI Observ, Tokyo 1818588, Japan
[8] Natl Astron Observ Japan, Mizusawa VLBI Observ, Oshu, Iwate 0230861, Japan
[9] Univ Tokyo, Chiba 2778561, Japan
[10] NEC Engn Ltd, Tokyo 1838502, Japan
[11] NEC Corp Ltd, Tokyo 1838501, Japan
[12] Japan Aerosp Explorat Agcy, Inst Space & Astronaut Sci, Tsukuba, Ibaraki 3058505, Japan
[13] Chinese Acad Sci, Urumqi Astron Observ, Urumqi 830011, Xingjiang, Peoples R China
[14] Univ Tasmania, Hobart, Tas 7001, Australia
[15] Fundamentalstn Wettzell, D-93444 Kotzting, Germany
基金
日本学术振兴会;
关键词
Lunar explorer; VLBI; Gravity field; Orbit determination; PHASE CHARACTERISTICS; CRUSTAL THICKNESS; TRACKING DATA; PROSPECTOR; CONSTRAINTS; MISSION; MODELS; MOON;
D O I
10.1007/s11214-010-9656-9
中图分类号
P1 [天文学];
学科分类号
0704 ;
摘要
The Japanese lunar explorer SELENE (Kaguya), which was launched on September 14th, 2007, was the target of VLBI observations over the period November 2007 to June 2009. These observations were made in order to improve the lunar gravity field model, in particular the lower degree coefficients and the model near the limb. Differential VLBI Radio sources, called VRAD instruments, were on-board the subsatellites, Rstar (Okina) and Vstar (Ouna), and the radio signals were observed by the Japanese VERA (VLBI Exploration of Radio Astrometry) network, and an international VLBI network. Multi-frequency and same-beam VLBI techniques were utilized and were essential aspects of the successful observing program. Multi-frequency VLBI was employed in order to improve the accuracy of the orbit determination obtained from the phase delay from the narrow-band satellite signals, while the same-beam VLBI method was used to resolve the cycle ambiguity which is inherent in the multi-frequency VLBI method. The observations were made at three S-band frequencies (2212, 2218 and 2287 MHz), and one X-band frequency (8456 MHz). We have succeeded in correlating the recorded signals from Okina/Ouna, and we obtained phase delays with an accuracy of several pico-seconds at S-band.
引用
收藏
页码:123 / 144
页数:22
相关论文
共 21 条
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