@inproceedings{oai:jaxa.repo.nii.ac.jp:00038715,
 author = {春木, 美鈴 and 松本, 秀一 and 近藤, 義典 and 尾川, 順子 and 竹内, 央 and 藤田, 和央 and Haruki, Misuzu and Matsumoto, Shuichi and Kondoh, Yoshinori and Ogawa, Naoko and Takeuchi, Hiroshi and Fujita, Kazuhisa},
 book = {第58回宇宙科学技術連合講演会講演集, Proceedings of 58th Space Sciences and Technology Conference},
 month = {Nov},
 note = {第58回宇宙科学技術連合講演会（2014年11月12日-14日. 長崎ブリックホール), 長崎市, 長崎県, The Mars EDL Demonstrator WG is planning the Mars Surface Exploration Demonstrator mission to realize entry, descent, landing and exploration on a planet with the Mars in early 2020’s. Guided Reentry Flight in Martian atmosphere is needed in order to Mars pin-point landing. The paper reports characteristics of Aerodynamics guidance in Martian atmosphere and shows guidance error analysis for the mission., 資料番号: AC1500075000, レポート番号: JSASS-2014-4159},
 publisher = {日本航空宇宙学会(JSASS), The Japan Society for Aeronautical and Space Sciences (JSASS)},
 title = {火星大気中の空力誘導の特徴及び誘導誤差解析},
 year = {2014}
}