@inproceedings{oai:jaxa.repo.nii.ac.jp:00007769,
 author = {石橋, 史朗 and 大西, 隆史 and 辻本, 滋雄 and 黒須, 勝利 and 吉川, 真 and 加藤, 隆二 and 市川, 勉 and 山川, 宏 and 川口, 淳一郎 and Ishibashi, Shiro and Onishi, Takafumi and Tsujimoto, Shigeo and Kurosu, Katsutoshi and Yoshikawa, Makoto and Kato, Takaji and Ichikawa, Tsutomu and Yamakawa, Hiroshi and Kawaguchi, Junichiro},
 book = {平成14年度アストロダイナミクスシンポジウム:講演後刷り集, ISAS Proceedings of 12th Workshop on Astrodynamics and Flight Mechanics 2002: A Collection of Technical Papers},
 month = {Feb},
 note = {従来の深宇宙探査機の軌道決定では、地上局から衛星を見た視線方向の情報量をもつレンジ・レンジレート観測量を用いるため、これと垂直方向の軌道決定精度には限界がある。一方、VLBI観測データは視線垂直方向に感度をもつため、これら両者のデータを組み合わせて使用すれば、軌道決定精度の向上が期待できる。本論文では、宇宙科学研究所の深宇宙探査機に、VLBI観測データを併用した軌道決定を適用した場合のケーススタディを行い、軌道決定精度の向上効果について述べる。, In orbit determination of a deep-space satellite, traditional radiometric data, that is, range and range rate data are used in most cases. Since these data have sensitivity in line of site direction, orbit determination accuracy is good in this direction, but there is less accuracy in perpendicular directions. On the other hand, VLBI data have sensitivity perpendicular to the line of site direction, so the combination of traditional radiometric data and VLBI data are very effective to improve the orbit determination accuracy. In this paper, the orbit determination analysis is carried out by using VLBI observation data, and some typical results for ISAS deep-space satellites are shown., 資料番号: AA0045497007},
 pages = {39--44},
 publisher = {宇宙科学研究所, The Institute of Space and Astronautical Science (ISAS)},
 title = {Orbit determination analysis using VLBI observation data},
 year = {2003}
}