@inproceedings{oai:jaxa.repo.nii.ac.jp:00038826,
 author = {工藤, 翔平 and 柳澤, 正久 and 河本, 聡美 and 壹岐, 賢太郎 and Kudo, Shohei and Yanagisawa, Masahisa and Kawamoto, Satomi and Iki, Kentaro},
 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, As a countermeasure for suppressing space debris growth, the Japan Aerospace Exploration Agency (JAXA) is investigating an active space debris removal system that employs highly efficient electrodynamics tether (EDT) technology as its orbital transfer system. In numerical simulation to evaluate the tether’s dynamics, tether has been modeled as point masses connected by linear springs and viscous dampers. However the actual tether shows non-linear behavior. In this paper, non-linear springs model are developed based on the results of dynamic tensile test of the tether. Then numerical simulations are conducted to investigate the effects of non-linearity, especially for the cases when the tether deployment is stopped suddenly, 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AC1600095000, レポート番号: JSASS-2015-4674},
 publisher = {日本航空宇宙学会(JSASS), The Japan Society for Aeronautical and Space Sciences (JSASS)},
 title = {導電性テザーの非線形バネとしての性質の影響評価},
 year = {2015}
}