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"publish_date": "2015-03-26", "publish_status": "0", "recid": "7505", "relation": {}, "relation_version_is_last": true, "title": ["Spacecraft formation flying in eccentric orbits"], "weko_shared_id": -1}
Spacecraft formation flying in eccentric orbits
https://jaxa.repo.nii.ac.jp/records/7505
https://jaxa.repo.nii.ac.jp/records/7505acc0e4ff-477b-4f5c-aa77-7247b6956ca3
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Spacecraft formation flying in eccentric orbits | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 編隊飛行 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 軌道計算 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 偏心軌道 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 対称性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 数学モデル | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 参照軌道 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 相対軌道 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 編隊軌道 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 円軌道 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 楕円軌道 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 偏心率 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 運動方程式 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙機軌道 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | formation flying | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | orbit calculation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | eccentric orbit | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | symmetry | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | mathematical model | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | reference trajectory | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | relative trajectory | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | formation trajectory | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | circular orbit | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | elliptical orbit | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | eccentricity | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | equation of motion | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | spacecraft trajectory | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
アクセス権 | ||||||
アクセス権 | metadata only access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_14cb | |||||
その他のタイトル | ||||||
その他のタイトル | 楕円軌道のフォーメーションフライトに関する考察 | |||||
著者 |
山田, 克彦
× 山田, 克彦× 吉河, 章二× 島, 岳也× Yamada, Katsuhiko× Yoshikawa, Shoji× Shima, Takeya |
|||||
著者所属 | ||||||
名古屋大学 | ||||||
著者所属 | ||||||
三菱電機 | ||||||
著者所属 | ||||||
三菱電機 | ||||||
著者所属(英) | ||||||
en | ||||||
Nagoya University | ||||||
著者所属(英) | ||||||
en | ||||||
Mitsubishi Electric Corporation | ||||||
著者所属(英) | ||||||
en | ||||||
Mitsubishi Electric Corporation | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構宇宙科学研究本部 | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS) | |||||
書誌情報 |
第16回アストロダイナミクスシンポジウム講演後刷り集 2006 en : Proceedings of 16th Workshop on JAXA Astrodynamics and Flight Mechanics p. 22-27, 発行日 2007-03 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 本稿では楕円軌道における宇宙機の編隊飛行制御について検討する。相対的なフォーメーション軌道において、楕円軌道と同じ対称性を仮定することによってフォーメーションの初期条件を導く。この初期条件から従宇宙機が主宇宙機の周りを少ない距離変動で周回するような軌道や、従宇宙機が局所水平面内で周回する軌道など、いくつかの特徴的な軌道を求めることができる。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Formation flight of spacecraft in eccentric orbits is considered in this paper. Symmetry of the eccentric orbits is assumed in a relative formation trajectory, and under this assumption, relations of initial conditions in formation flight are derived. Some characteristic trajectories are obtained from these relations, such as a trajectory where a deputy spacecraft rotates around a chief spacecraft with relatively small variation in the distance between the two spacecraft, or a trajectory where the deputy spacecraft moves on a local horizontal plane on which the chief spacecraft exists. Formation flight by plural spacecraft is possible by combining these relative trajectories. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0063481004 |