@inproceedings{oai:jaxa.repo.nii.ac.jp:00005899,
 author = {岩田, 隆浩 and 並木, 則行 and 花田, 英夫 and RSAT/VRADグループ and Iwata, Takahiro and Namiki, Noriyuki and Hanada, Hideo and RSAT/VRAD Group},
 book = {宇宙航空研究開発機構特別資料: 先進的軌道計測・決定技術に関する研究会論文集, JAXA Special Publication: Proceedings of Advanced Orbit Measurement and Orbit Calculation Technologies},
 month = {Mar},
 note = {SELENEによる測月観測のためのリレー衛星中継器(RSAT; Relay Satellite Transponders)は、リレー衛星(Rstar)に搭載されるRSAT-1と主衛星に搭載されるRSAT-2から構成され、主衛星の月の裏側の軌道をRstar経由の4wayドプラ計測により観測する。RSATによる月裏側の重力場分布の観測と、相対VLBI用電波源(VRAD)による重力場低次項の精測により、月重力場モデルの改善を図る。, Global mapping of the lunar gravity field will be conducted by using two small sub-satellites of SELENE (SELenological and Engineering Explorer): the Relay Satellite (Rstar) and the VLBI (Very Large Baseline Interferometry) Radio Satellite (Vstar). Four-way Doppler measurements toward the SELENE Main Orbiter above the lunar far side will be carried out by the Relay Satellite Transponders (RSAT) on Rstar and the Main Orbiter. Phase-delay differential VLBI observations will be performed for multi-frequency carrier waves emitted from the Differential VLBI Radio Sources (VRAD) on Rstar and Vstar. We have executed proto-flight tests and confirmed that instruments and the ground system of RSAT and VRAD have enough performances to improve the accuracy of the lunar gravity field., 資料番号: AA0063223013, レポート番号: JAXA-SP-06-015},
 pages = {85--90},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {SELENEの3機の月周回衛星を用いた軌道決定による月重力場観測システム},
 volume = {JAXA-SP-06-015},
 year = {2007}
}