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Influence of the finite duration on a fly-by
https://jaxa.repo.nii.ac.jp/records/7450
https://jaxa.repo.nii.ac.jp/records/7450e094f42d-1c3a-4fd7-b6c7-d5137f53641b
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 | Influence of the finite duration on a fly-by | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 3体問題 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 2体問題 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 軌道解析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | エネルギー交換 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 軌道力学 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 数学的解析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | フライバイ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | マヌーバ | |||||
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 | 軌道 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 円錐曲線貼り合わせ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 影響球 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | SOI | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | three body problem | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | two body problem | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | trajectory analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | energy exchange | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | orbital mechanics | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | mathematical analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flyby | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | maneuver | |||||
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 | trajectory | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | patched conic | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | sphere of influence | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | SOI | |||||
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 | |||||
著者 |
Janssens, Frank
× Janssens, Frank |
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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17回アストロダイナミクスシンポジウム講演後刷り集 2007 en : Proceedings of 17th Workshop on JAXA Astrodynamics and Flight Mechanics p. 69-83, 発行日 2008-03 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Patched conics is the standard tool for designing fly-by or gravity assist maneuvers performed by a spacecraft about a planet. In this procedure, the trajectory of the spacecraft about the planet is taken as a perfect hyperbola once the spacecraft is in the sphere of influence of the planet. All other perturbations are neglected. As a consequence the outgoing V infinity is identical to the incoming V infinity. In reality, the spacecraft spends a finite time in the sphere of influence of the planet. A typical time is a week. The small perturbations caused by the Sun will affect the ideal hyperbolic trajectory. When the fly-by planet is the Earth, the Moon and J2 cause also small changes in the hyperbola. The small changes in V infinity are the subject of this paper. The perturbation of the Sun can be modeled as a restricted three body problem or analyzed with the standard averaging technique applied to an hyperbolic orbit. We compare our results to the real data of the fly-by past the Earth on March 4, 2005 by the Rosetta spacecraft on his way to the comet Churymov-Gerasimenko (2014). | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0063718013 |