@inproceedings{oai:jaxa.repo.nii.ac.jp:00007268,
 author = {山田, 和彦 and 山田, 哲哉 and 松岡, 正敏 and Yamada, Kazuhiko and Yamada, Tetsuya and Matsuoka, Masatoshi},
 book = {アストロダイナミクスシンポジウム講演後刷り集, The 20th Workshop on JAXA Astrodynamics and Flight Mechanics},
 month = {Mar},
 note = {第20回アストロダイナミクスシンポジウム (2010年7月26-27日. 宇宙航空研究開発機構宇宙科学研究所), 相模原市, 神奈川県, The 20th Workshop on JAXA Astrodynamics and Flight Mechanics 2010 (July 26-27, 2010. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan, 摘要: 2010年6月13日に小惑星探査機「はやぶさ」の再突入カプセルが地球に帰還し、カプセル本体、及び、ヒートシールドの回収は成功裏に完了した。本稿では，その帰還回収運用においてのEDL (Entry, Descent and Landing) 解析の役割と成果について報告する。EDL 解析による再突入軌道と着地点の予測は，軌道計画段階において着地点目標の策定に必須であり、また、回収運用の現場において、軌道決定と連携し、迅速かつ正確な着地点予測を行うことにより、スムーズな回収作業に貢献した。, "HAYABUSA" sample return capsule returned to the Earth with success in 13th June, 2010. The instrument module which has the asteroid "ITOKAWA" sample and two heat shields were completely recovered as scheduled at Woomera Prohibit Area in Australia. The prediction of the reentry trajectory and the landing point by EDL (Entry, Descent and Landing) analysis contributed to smooth recovery operation. When planning a trajectory correction maneuver, the target landing point was determined based on EDL analysis. In the on-site recovery operation, EDL analysis delivered the accurate information about the reentry trajectory and the landing position by cooperating with the orbital determination. In this paper, the contribution and the achievement of EDL analysis in "HAYABUSA" reentry and recovery operation are reported., 資料番号: AA0065115021},
 pages = {115--118},
 publisher = {宇宙航空研究開発機構宇宙科学研究所 (JAXA)(ISAS), Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)},
 title = {EDL analysis for "HAYABUSA" reentry and recovery operation},
 volume = {20},
 year = {2011}
}