@inproceedings{oai:jaxa.repo.nii.ac.jp:00038762,
 author = {加藤, 貴昭 and 田中, 啓太 and 大塚, 聡子 and 桑尾, 文博 and 山元, 透 and 村上, 尚美 and 中島, 悠 and Kato, Takaaki and Tanaka, Keita and Otsuka, Akiko and Kuwao, Fumihiro and Yamamoto, Toru and Murakami, Naomi and Nakajima, Yu},
 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, 鹿児島県, This paper shows the simulation results of the debris’ motion connected with the ADR satellite by towing wire. The satellite is equipped with the propulsion system to control its own attitude and orbit and it can be also used to control the debris’ motion. We model the wire as a multi-mass system and construct the thruster-control laws to make the debris’ attitude lower and get rid of it from the orbit. The results show that adding constant acceleration can make the debris’ attitude lower without divergence., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AC1600018000, レポート番号: JSASS-2015-4598},
 publisher = {日本航空宇宙学会(JSASS), The Japan Society for Aeronautical and Space Sciences (JSASS)},
 title = {牽引索を用いたデブリ除去衛星の軌道姿勢シミュレーション},
 year = {2015}
}