@inproceedings{oai:jaxa.repo.nii.ac.jp:00038816,
 author = {田中., 啓太 and 加藤, 貴昭 and 桑尾, 文博 and 上野, 真史 and 山元, 透 and 村上, 尚美 and 植田, 聡史 and Tanaka, Keita and Kato, Takaaki and Kuwao, Fumihiro and Ueno, Masafumi and Yamamoto, Toru and Murakami, Naomi and Ueda, Satoshi},
 book = {第59回宇宙科学技術連合講演会講演集, Proceedings of 59th Space Sciences and Technology Conference},
 month = {Oct},
 note = {第59回宇宙科学技術連合講演会（2015年10月7日-9日. かごしま県民交流センター), 鹿児島市, 鹿児島, The attention to the use of the EML2 and its halo orbits as a hub for deep space exploration has been growing. It is important to establish the way to make a spacecraft safely approach to and dock with the hub. This paper discusses rendezvous trajectories to the target on the EML2 halo. Two types of trajectories are evaluated in term of ΔV and the collision avoidance. The results show that the proposed rendezvous strategies enable the chaser to approach the target with small ΔV avoiding the risk of collision., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AC1600085000, レポート番号: JSASS-2015-4055},
 publisher = {日本航空宇宙学会(JSASS), The Japan Society for Aeronautical and Space Sciences (JSASS)},
 title = {EML2ハロ上のターゲットへのランデブ},
 year = {2015}
}