@inproceedings{oai:jaxa.repo.nii.ac.jp:00007263,
 author = {大山, 聖 and 川勝, 康弘 and 萩原, 和子 and Oyama, Akira and Kawakatsu, Yasuhiro and Hagiwara, Kazuko},
 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, SOLAR-C Plan A SEPオプションの軌道設計問題に対して，多目的設計探査を行った．その結果，終端質量最大化，終端速度最大化，最小動径半径の最大化の間のトレードオフ関係などの軌道設計上有益な知見が得られた．また，軌道・機体同時設計の可能性が示された．, Multiobjective design exploration (MODE) framework is applied to the trajectory design problem for SOLAR-C Plan A SEP option. Present approach revealed some important design knowledge such as tradeoff information among maximization of final mass, maximization of final velocity, and maximization of minimum distance from the Sun. Present study also shows possibility of simultaneous design of trajectory and spacecraft., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0065115016},
 pages = {87--92},
 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 = {Application of Multiobjective Design Exploration to SOLAR-C Orbit Design},
 volume = {20},
 year = {2011}
}