低推力を用いた編隊飛行制御の応用
| Autor: | Yoshikawa, Shoji |
|---|---|
| Jazyk: | japonština |
| Rok vydání: | 2008 |
| Předmět: |
satellite constellation
numerical analysis formation flying 数値解析 低高度地球周回軌道 low Earth orbit coordinate system 編隊飛行 衛星姿勢制御 低推力推進 low thrust propulsion 衛星配置 very long base interferometry 座標系 Physics::Space Physics Astrophysics::Earth and Planetary Astrophysics minimum impulse satellite attitude control 最小インパルス 超長基線干渉法 |
| Zdroj: | 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 = JAXA Special Publication: Collection of Papers Presented at the Meeting on the Study of Space Missions Propelled by Low-Thrust and Sustained Acceleration. :49-55 |
| ISSN: | 1349-113X |
| Popis: | 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). 資料番号: AA0063739008 レポート番号: JAXA-SP-07-020 |
| Databáze: | OpenAIRE |
| Externí odkaz: |
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