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Motion analysis of satellites after separation from M-V-7 rocket
https://jaxa.repo.nii.ac.jp/records/7508
https://jaxa.repo.nii.ac.jp/records/7508526c272f-94aa-4a5b-9dfb-dd4b7e35e88a
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 | Motion analysis of satellites after separation from M-V-7 rocket | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ひので | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | SOLAR-B | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 太陽観測衛星 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 運動解析 | |||||
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 | 軌道要素 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 距離 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 推力 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 衛星軌道 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | モンテカルロ法 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 計算機シミュレーション | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 衝突 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 弾道係数 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | HINODE | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | SOLAR-B | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Solar Physics Satellite | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | motion analysis | |||||
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 | orbital element | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | distance | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | thrust | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | satellite orbit | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Monte Carlo method | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | computerized simulation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | collision | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | ballistic coefficient | |||||
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 | M-V7号機衛星分離後の軌道上運動解析 | |||||
著者 |
山本, 高行
× 山本, 高行× Yamamoto, Takayuki |
|||||
著者所属 | ||||||
宇宙航空研究開発機構 | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency | ||||||
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. 37-41, 発行日 2007-03 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 今年度夏期に打ち上げが予定されているM-V7号機では、主衛星であるSOLAR-Bと共に2つの小型衛星がサブペイロードとして搭載される。単純に軌道面外方向へ分離が行われると、軌道半周期後に衝突することになる。本研究では各衛星の分離後、軌道上において各衛星およびロケット上段の軌道運動を解析し、ノミナルのシーケンスから衛星分離速度および分離方向に誤差が生じたり、各衛星の弾道係数の見積もり誤差あるいは大気抵抗の変動がある場合にも、衝突が生じないことを検証する。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | M-V-7 rocket, witch would be launched in this summer, bring main satellite 'SOLAR-B' and two small satellites as sub payload. If one of the small satellite separate from M-V-7 upper stage to normal direction as for velocity, the satellite would come into collision with M-V-7 upper stage after half period of orbit. In this paper, the on-orbit motion of each satellite and M-V-7 upper stage would by analyzed after separation. Under the consideration of several uncertainties like ballistic coefficient of each satellite and variation of air drag, the separation method witch doesn't happen to come into collision would be proposed. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0063481007 |