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低推力を用いた編隊飛行制御の応用
https://jaxa.repo.nii.ac.jp/records/5590
https://jaxa.repo.nii.ac.jp/records/559018c156a9-a58b-4234-a7af-e3e8371dcb5a
名前 / ファイル | ライセンス | アクション |
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63739008.pdf (1.3 MB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 低推力を用いた編隊飛行制御の応用 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 低推力推進 | |||||
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 | 衛星配置 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 最小インパルス | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 低高度地球周回軌道 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 超長基線干渉法 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 衛星姿勢制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 数値解析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 座標系 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | low thrust propulsion | |||||
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 | satellite constellation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | minimum impulse | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | low Earth orbit | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | very long base interferometry | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | satellite attitude control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | numerical analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | coordinate system | |||||
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 | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Application of formation flying control with low thrust satellites | |||||
著者 |
吉河, 章二
× 吉河, 章二× Yoshikawa, Shoji |
|||||
著者所属 | ||||||
三菱電機 先端技術総合研究所 | ||||||
著者所属(英) | ||||||
en | ||||||
Mitsubishi Electric Corporation Advanced Technology R & D Center | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構 | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航空研究開発機構特別資料: 低推力・連続加速を用いた宇宙ミッションに関する研究会論文集 en : JAXA Special Publication: Collection of Papers Presented at the Meeting on the Study of Space Missions Propelled by Low-Thrust and Sustained Acceleration 巻 JAXA-SP-07-020, p. 49-55, 発行日 2008-02-29 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Future scientific missions such as virtual telescope and interferometer require precise formation flying where relative positions of spacecraft are controlled very precisely. A feature of the low thrust that the minimum impulse is small is very attractive for such applications. This paper takes an along-track formation control in low earth orbit as an example and numerically investigates how the size of minimum impulse affects control accuracy under the two representative natural disturbances (J2 term and air drag). | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-113X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11984031 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0063739008 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-SP-07-020 |