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HAYABUSA orbit determination under low thrust
https://jaxa.repo.nii.ac.jp/records/7694
https://jaxa.repo.nii.ac.jp/records/7694ba3efe85-fcf7-484f-946f-19e7775feeb2
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 | HAYABUSA orbit determination under low thrust | |||||
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 | 低推力推進 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 軌道決定 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 破片 | |||||
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 | 予測精度 | |||||
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 | ||||||
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 | low thrust propulsion | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | orbit determination | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | fragment | |||||
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 | prediction accuracy | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Earth swingby | |||||
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 | 電気推進推力下におけるはやぶさ軌道決定 | |||||
著者 |
大西, 隆史
× 大西, 隆史× 石橋, 史朗× 吉川, 真× 加藤, 隆二× 市川, 勉× 山川, 宏× 川口, 淳一郎× Onishi, Takafumi× Ishibashi, Shiro× Yoshikawa, Makoto× Kato, Takaji× Ichikawa, Tsutomu× Yamakawa, Hiroshi× Kawaguchi, Junichiro |
|||||
著者所属 | ||||||
富士通 | ||||||
著者所属 | ||||||
富士通 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 | ||||||
著者所属(英) | ||||||
en | ||||||
Fujitsu Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Fujitsu Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science | ||||||
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. 352-356, 発行日 2005-03 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 「はやぶさ」は2003年5月9目に内之浦からM-V5号機によって打ち上げられた、世界初の小惑星サンプルリターンミッションを有する探査機である。「はやぶさ」は電気推進を主たる推進機関としており、打上げから地球帰還までのほとんど全期間に渡って、電気推進による常時加速を行ないながら惑星間空間を航行する。追跡誘導の観点からは、電気推進推力のモデル誤差が軌道決定および軌道予報の精度に大きな影響を与えるため、これを如何にモデル化するかということと、必要に応じて推力推定を行なうことが、重要な課題となる。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Hayabusa is a spacecraft to explore the asteroid (25143) Itokawa, and it is going to get an asteroid's fragments for the first time in the world. Hayabusa carries an Ion Engines System (IES) as main propulsion in cruising. From the viewpoint of orbit determination, an error in acceleration modeling of low thrust has a great influence both on orbit determination and prediction accuracy. This paper describes an evaluation for orbit propagation under low thrust operation, as well as a method which is adopted in the routine navigation for Hayabusa. | |||||
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: AA0047897061 |