WEKO3
アイテム
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Orbit design & delta-V operation of asteroid sample return spacecraft HAYABUSA
https://jaxa.repo.nii.ac.jp/records/7700
https://jaxa.repo.nii.ac.jp/records/7700f0c45439-bf82-44e2-8d7f-4eeacb02e9d1
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 | Orbit design & delta-V operation of asteroid sample return spacecraft HAYABUSA | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | はやぶさ宇宙機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 小惑星いとかわ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | サンプルリターンミッション | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | イオンエンジン | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙ランデブー | |||||
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 | 地球スウィングバイ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 軌道設計 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | HAYABUSA spacecraft | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Asteroid ITOKAWA | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | sample return mission | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | ion engine | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | space rendezvous | |||||
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 | Earth swingby | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | orbit design | |||||
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 | 小惑星探査機はやぶさの軌道計画とΔV運用 | |||||
著者 |
大島, 武
× 大島, 武× 萩野, 慎二× 木村, 雅文× 松岡, 正敏× 小湊, 隆× Oshima, Takeshi× Hagino, Shinji× Kimura, Masafumi× Matsuoka, Masatoshi× Kominato, Takashi |
|||||
著者所属 | ||||||
NEC東芝スペースシステム | ||||||
著者所属 | ||||||
NEC東芝スペースシステム | ||||||
著者所属 | ||||||
NEC航空宇宙システム | ||||||
著者所属 | ||||||
NEC航空宇宙システム | ||||||
著者所属 | ||||||
NEC航空宇宙システム | ||||||
著者所属(英) | ||||||
en | ||||||
NEC TOSHIBA Space Systems Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
NEC TOSHIBA Space Systems Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
NEC Aerospace Systems Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
NEC Aerospace Systems Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
NEC Aerospace Systems Ltd. | ||||||
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 |
平成16年度アストロダイナミクスシンポジウム:講演後刷り集 en : ISAS proceedings of 14th Workshop on Astrodynamics and Flight Mechanics 2004: A Collection of Technical Papers p. 387-392, 発行日 2005-03 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 小惑星探査機はやぶさは、2003年5月9日に打上げられ、イオンエンジンによる低推力ΔVにより継続的な軌道変更を行った後、2004年5月19日の地球Swing Byによって、小惑星ITOKAWAに向かう軌道へと移った。Swing By後も、2005年8月末のITOKAWAランデブーに向け、引き続き、軌道計画→イオンエンジン運用→軌道決定→軌道計画のサイクルを回していく。本論文では、1)イオンエンジンによる低推力飛行の軌道計画手法、2)軌道計画から運用手順作成までの手法、3)はやぶさΔV運用/軌道実績、4)低推力飛行における軌道運用のポイント、について報告する。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The Asteroid Sample Return Spacecraft HAYABUSA was launched in May 9th, 2003. After the launch, it continuously changed its orbit by Ion Engine and swung by earth in May 19th, 2004. Now it heads in the direction of ITOKAWA (Asteroid 25143). HAYABUSA will rendezvous with ITOKAWA at the end of August 2005. The operation team designs the orbit, operates Ion Engine, determines the orbit with the ranging data and then designs the next orbit. This cycle will be performed continuously until the earth return. This paper describes 1) the orbit design method for low thrust delta-V performed by Ion Engine, 2) the method to create the operation sequence from the delta-V plan, 3) the results of HAYABUSA delta-V operation and the realized orbit, and 4) the important issues for the orbit design with low thrust continuous delta-V. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0918-8053 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0047897067 |