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High-accuracy same-beam VLBI observations using Shanghai and Urumqi telescopes

Science China(Physics,Mechanics & Astronomy) 2009年第10期52卷 1858-1866页

作者： kikuchi fuyuhiko KAMATA Shun'ichi MATSUMOTO Koji HANADA Hideo National Astronomical Observatory of Japan Tokyo University

The same-beam VLBI observations of Rstar and Vstar,which were two small satellites of Japanese lunar mission,SELENE,were successfully performed by using Shanghai and Urumqi 25-m telescopes. When the separation angle between Rstar and Vstar was less than 0.1 deg,the differential phase delay of the X-band signals between Rstar and Vstar on Shanghai-Urumqi baseline was obtained with a very small error of 0.15 mm rms,which was reduced by 1-2 order compared with the former VLBI results. When the separation angle was less than 0.56 deg,the differential phase delay of the S-band signals was also obtained with a very small error of several mm rms. The orbit determination for Rstar and Vstar was performed,and the accuracy was improved to a level of several meters by using VLBI and Doppler data. The high-accuracy same-beam differential VLBI technique is very useful in orbit determination for a spacecraft,and will be used in orbit determination for Mars missions of China Yinghuo-1 and Russia Phobos-grunt.

关键词： same-beam differential VLBI phase delay precise orbit determination

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Applications of same-beam VLBI in the orbit determination of multi-spacecrafts in a lunar sample-return mission

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Science China(Physics,Mechanics & Astronomy) 2010年第6期53卷 1153-1161页

作者： GOOSSENS Sander kikuchi fuyuhiko MATSUMOTO Koji HANADA Hideo National Astronomical Observatory of Japan

Same-beam VLBI means that two spacecrafts with small separation angles that transmit multi-frequency signals specially designed are observed simultaneously through the main beam of receiving antennas. In same-beam VLBI,the differential phase delay between the two spacecrafts and the two receiving antennas can be obtained within a small error of several picoseconds. As a successful application,the short-arc orbit determination of several hours for Rstar and Vstar,which are two small sub-spacecrafts of SELENE,has been much improved by using the same-beam VLBI data together with the Doppler and range data. The long-arc orbit determination of several days has also been accomplished within an error of about 10 m with the same-beam VLBI data incorporated. These results show the value of the same-beam VLBI for the orbit determination of multi-spacecrafts. This paper introduces the same-beam VLBI and Doppler observations of SELENE and the orbit determination results. In addition,this paper introduces how to use the same-beam VLBI for a lunar sample-return mission,which usually consists of an orbiter,a lander and a return unit. The paper also offers the design for the onboard radio sources in the lunar sample-return mission,and introduces applications of S-band multi-frequency same-beam VLBI in lunar gravity exploration and applications during all stages in the position/orbit determinations such as orbiting,landing,sampling,ascending,and docking.

关键词： same-beam VLBI differential phase delay sample-return orbit determination lunar gravity field

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用于未来月球探测的ILOM技术现状

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深空探测学报 2014年第3期1卷 200-204页

作者： Hideo HANADA Seiitsu TSURUTA Kazuyoshi ASARI Hiroshi ARAKI Hirotomo NODA Shingo KASHIMA Ken-ichi FUNAZAKI fuyuhiko kikuchi Koji MATSUMOTO Yusuke KONO Hiroo KUNIMORI Sho SASAKI 平劲松日本国立天文台RISE研究室综合研究大学院大学天文学部岩手大学工学院国立天文台水泽VLBI观测站国立信息通信技术研究院无线网络研究所大阪大学地球与空间科学部中科院国家天文台

使用面包板模型和仿真方法,在实验室内研究月球指向就位测量望远镜(ILOM)的基本特征,如望远镜星像中心点位置精度、温度效应、倾斜以及地面震动的影响。使用这个技术预期在月球表面观测月球自转时可以达到1ms的精度。将在地面上开展测... 详细信息

使用面包板模型和仿真方法,在实验室内研究月球指向就位测量望远镜(ILOM)的基本特征,如望远镜星像中心点位置精度、温度效应、倾斜以及地面震动的影响。使用这个技术预期在月球表面观测月球自转时可以达到1ms的精度。将在地面上开展测试验证观测以全面评价达到优于0.1″观测精度目标所需条件和特征。

关键词：月球 ILOM 望远镜照相天顶筒水银槽

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