Trajectory design of destiny mission

Mai Bando; Masaki Nakamiya; Yasuhiro Kawakatsu; Chikako Hirose; Takayuki Yamamoto

Trajectory design of destiny mission

Mai Bando, Masaki Nakamiya, Yasuhiro Kawakatsu, Chikako Hirose, Takayuki Yamamoto

研究成果: 書籍/レポートタイプへの寄稿 › 会議への寄与

抄録

The trajectory design of the interplanetary mission "Demonstration and Experiment of Space Technology for INterplanetary voYage, DESTINY" is discussed. The trajectory optimization of low-thrust spacecraft pose a difficult design challenge. Moreover, DESTINY mission requires many constraints for the orbital design. In advance of optimizing the whole transfer mission, we investigated the basic theory to design which can take into account such constraints.

本文言語	英語
ホスト出版物のタイトル	Space for Our Future - Advances in the Astronautical Sciences
ホスト出版物のサブタイトル	Proceedings of the 13th International Conference of Pacific-Basin Societies, ISCOPS 2012
ページ	321-322
ページ数	2
巻	146
出版ステータス	出版済み - 4月 24 2013
外部発表	はい
イベント	13th International Space Conference of Pacific-Basin Societies, ISCOPS 2012 - Kyoto, 日本継続期間: 5月 15 2012 → 5月 18 2012

その他

その他	13th International Space Conference of Pacific-Basin Societies, ISCOPS 2012
国/地域	日本
City	Kyoto
Period	5/15/12 → 5/18/12

!!!All Science Journal Classification (ASJC) codes

航空宇宙工学
宇宙惑星科学

他のファイルとリンク

引用スタイル

Bando, M, Nakamiya, M, Kawakatsu, Y, Hirose, C & Yamamoto, T 2013, Trajectory design of destiny mission. in Space for Our Future - Advances in the Astronautical Sciences: Proceedings of the 13th International Conference of Pacific-Basin Societies, ISCOPS 2012. vol. 146, pp. 321-322, 13th International Space Conference of Pacific-Basin Societies, ISCOPS 2012, Kyoto, 日本, 5/15/12.

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author = "Mai Bando and Masaki Nakamiya and Yasuhiro Kawakatsu and Chikako Hirose and Takayuki Yamamoto",

year = "2013",

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N2 - The trajectory design of the interplanetary mission "Demonstration and Experiment of Space Technology for INterplanetary voYage, DESTINY" is discussed. The trajectory optimization of low-thrust spacecraft pose a difficult design challenge. Moreover, DESTINY mission requires many constraints for the orbital design. In advance of optimizing the whole transfer mission, we investigated the basic theory to design which can take into account such constraints.

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ER -

Trajectory design of destiny mission

抄録

その他

!!!All Science Journal Classification (ASJC) codes

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