WEKO3
アイテム
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Flight test of rocket sun aspect sensor and attitude determination system on the ground by M-V-8 launch
https://jaxa.repo.nii.ac.jp/records/7520
https://jaxa.repo.nii.ac.jp/records/7520c3f02bb0-9e52-4924-9bc0-28fa6042abc9
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 | Flight test of rocket sun aspect sensor and attitude determination system on the ground by M-V-8 launch | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 太陽センサ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 地磁気 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ロケット-太陽アスペクトセンサ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | RSAS | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | M-V-8飛翔試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 姿勢決定 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 打上げ機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 計測装置 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 遠隔計測 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 姿勢角 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 角度分解能 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 上昇角 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | フォトダイオード | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 月探査 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | solar sensor | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | geomagnetism | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | rocket sun aspect sensor | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | RSAS | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | M-V-8 flight test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | attitude determination | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | launch vehicle | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | measuring instrument | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | telemetry | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | attitude angle | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | angular resolution | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | elevation angle | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | photodiode | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | lunar exploration | |||||
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-V-8号機飛翔試験におけるロケット太陽センサおよび地上局システムの動作確認 | |||||
著者 |
成田, 伸一郎
× 成田, 伸一郎× 太刀川, 純孝× 森田, 泰弘× 広川, 英治× Narita, Shinichiro× Tachikawa, Sumitaka× Morita, Yasuhiro× Hirokawa, Eiji |
|||||
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 | ||||||
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 |
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. 107-110, 発行日 2007-03 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | スピン型飛翔体の姿勢決定において、太陽角を高精度かつ広視野で検出することが要求される。一方で、高信頼性を確保するためミッション要求に合わせて簡易なシステム構成とすることが要求される。今回視野120度、精度0.5度のセンサと共に、動作確認を行う姿勢決定地上システムを開発し、M-V-8号機飛翔試験を通して動作確認を行った。その結果を報告する。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In the case of spinning spacecraft attitude determination, detection of sun angle in high resolution and wide field of view is needed. We have developed the Rocket Sun Aspect Sensor (RSAS) with a field of view of 128 degree and resolution of 0.5 degree. Furthermore, in order attitude determination of the spacecraft, two reference vectors and angles between the reference objects and spacecraft are needed, for example, sun and geomagnetic angle. Therefore, we developed the attitude determination system on the ground and software to receive rocket telemetry data, and calculate sun and geomagnetic angle. In this flight test, we verified the motion of RSAS and this attitude determination system by M-V-8 launch. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0063481019 |