@inproceedings{oai:jaxa.repo.nii.ac.jp:00005590,
 author = {吉河, 章二 and Yoshikawa, Shoji},
 book = {宇宙航空研究開発機構特別資料: 低推力・連続加速を用いた宇宙ミッションに関する研究会論文集, JAXA Special Publication: Collection of Papers Presented at the Meeting on the Study of Space Missions Propelled by Low-Thrust and Sustained Acceleration},
 month = {Feb},
 note = {Future scientific missions such as virtual telescope and interferometer require precise formation flying where relative positions of spacecraft are controlled very precisely. A feature of the low thrust that the minimum impulse is small is very attractive for such applications. This paper takes an along-track formation control in low earth orbit as an example and numerically investigates how the size of minimum impulse affects control accuracy under the two representative natural disturbances (J2 term and air drag)., 資料番号: AA0063739008, レポート番号: JAXA-SP-07-020},
 pages = {49--55},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {低推力を用いた編隊飛行制御の応用},
 volume = {JAXA-SP-07-020},
 year = {2008}
}