@inproceedings{oai:jaxa.repo.nii.ac.jp:00007314,
 author = {山田, 克彦 and 木村, 将哉 and Yamada, Katsuhiko and Kimura, Masaya},
 book = {アストロダイナミクスシンポジウム講演後刷り集, Proceedings of 19th workshop on JAXA Astrodynamics and Flight Mechanics},
 month = {Mar},
 note = {アストロダイナミクスシンポジウム (2009年7月30-31日. 宇宙航空研究開発機構宇宙科学研究本部)), Workshop on JAXA Astrodynamics and Flight Mechanics, 2009 (July 30-31, 2009. Institute of Space and Astronautical Science (ISAS), Japan Aerospace Exploration Agency (JAXA)), Sagamihara, Kanagawa Japan, 2機の宇宙機によるフォーメーションフライトの相対位置を高精度に制御する問題について考察する．天体観測への応用を念頭に，ケプラー軌道上で部分的な相対位置制御を行うこととし，さらに相対位置は慣性座標系において指定するものとする．このとき制御時間と燃料消費量を最小とする最適離心率の関係を調べる．, The problem of precise relative position keeping is studied in the formation flight of two spacecraft. Taking into account the applications to astronomic observation, the relative position of spacecraft is controlled to be precisely preserved on the part of the Keplerian orbits; moreover, it is preserved in the inertial coordinates. Then, the fuel-optimal eccentricities are studied for each length of control time., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0064734009},
 publisher = {宇宙航空研究開発機構宇宙科学研究本部, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)},
 title = {Relative Position Keeping of Spacecraft Formation Flying in the Inertial Coordinates},
 volume = {2009},
 year = {2010}
}