WEKO3
アイテム
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Tokyo Tech's CubeSat CUTE-1: Operation reports and analyses of pico-satellite dynamics
https://jaxa.repo.nii.ac.jp/records/7707
https://jaxa.repo.nii.ac.jp/records/7707de76e086-d3b3-4b7e-8e5f-581409110be1
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 | Tokyo Tech's CubeSat CUTE-1: Operation reports and analyses of pico-satellite dynamics | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | CubeSat Cute-1 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 姿勢制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 衛星通信 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 学生 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 温度センサー | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 角速度 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ピコ衛星 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 飛行試験 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | CubeSat Cute-1 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | attitude control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | satellite communication | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | student | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | temperature sensor | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | angular velocity | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | pico-satellite | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flight test | |||||
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 | 東京工業大学CubeSat CUTE-1:打ち上げ成果とダイナミクスについて | |||||
著者 |
宇井, 恭一
× 宇井, 恭一× 此上, 一也× 澤田, 弘崇× 中谷, 幸司× 宮下, 直己× 居相, 政史× 占部, 智之× 柏, 宗孝× 山口, 伸斉× 立川, 智章× Ui, Kyoichi× Konoue, Kazuya× Sawada, Hirotaka× Nakaya, Koji× Miyashita, Naoki× Iai, Masafumi× Urabe, Tomoyuki× Kashiwa, Munetaka× Yamaguchi, Nobumasa× Tatsukawa, Tomoaki |
|||||
著者所属 | ||||||
東京工業大学 大学院理工学研究科 | ||||||
著者所属 | ||||||
東京工業大学 大学院理工学研究科 | ||||||
著者所属 | ||||||
東京工業大学 大学院理工学研究科 | ||||||
著者所属 | ||||||
東京工業大学 大学院理工学研究科 | ||||||
著者所属 | ||||||
東京工業大学 大学院理工学研究科 | ||||||
著者所属 | ||||||
東京工業大学 大学院理工学研究科 | ||||||
著者所属 | ||||||
東京工業大学 大学院理工学研究科 | ||||||
著者所属 | ||||||
東京工業大学 大学院理工学研究科 | ||||||
著者所属 | ||||||
東京工業大学 大学院理工学研究科 | ||||||
著者所属 | ||||||
東京工業大学 大学院理工学研究科 | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Institute of Technology Graduate School of Science and Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Institute of Technology Graduate School of Science and Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Institute of Technology Graduate School of Science and Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Institute of Technology Graduate School of Science and Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Institute of Technology Graduate School of Science and Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Institute of Technology Graduate School of Science and Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Institute of Technology Graduate School of Science and Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Institute of Technology Graduate School of Science and Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Institute of Technology Graduate School of Science and Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Institute of Technology Graduate School of Science and Engineering | ||||||
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15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 13th Workshop on Astrodynamics and Flight Mechanics 2003: A Collection of Technical Papers p. 29-34, 発行日 2004-02 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 東工大松永研究室では、CUTE-1と呼ぶ1kg、10cm立法の超小型衛星の設計と製作を学生主導により進めてきた。そして、2003年6月31日ロシアのプレセツク宇宙基地より成功裏に打ち上げられ、現在も正常に動作している。CUTE-1は、超小型衛星用バスシステムの開発を目的として、通信、姿勢・温度計測およびアンテナ・太陽電池パドルの展開の3つのミッションを行う。本稿では、まずCUTE-1のシステム概要と打ち上げから軌道投入までの流れについて説明する。次にCUTE-1の運用報告として、CUTE-1の軌道上の角速度や温度について述べ、そしてCUTE-1のテレメトリデータを用いた超小型衛星のダイナミクス解析について解説する。特にCUTE-1搭載のジャイロデータよリ計測した角速度を用いたアンテナと太陽電池パドルの展開の影響に対する評価や、太陽セルの発生電流から推測する太陽方向ベクトルに対する運動との比較結果について述べる。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | At Laboratory for Space Systems, Tokyo Institute of Technology, students had designed and fabricated a pico-satellite (1 kg, 10 cm cube), named CUTE-1. CUTE-1 was successfully launched at the Plesetsk Cosmodrome, Russia aboard ROCKOT on Jun 30, 2003, and is properly working. CUTE-1 has three missions. First one is communication, second one is attitude and temperature sensing, and third one is deployment of antennas and solar paddle. The objectives of these missions are to establish bus component design for pico-satellites like the CubeSat. At first, this paper mentions the system overview of CUTE-1 and the procedure from launch to injection into the orbit. Second, results of temperature and angular velocity measurement are described as the operation reports. Third, analyses of nano satellite dynamics is explained using CUTE-1's telemetry data. Especially, the effect of deployment of antenna and solar paddle is examined using the angular velocity calculated gyro data on CUTE-1. Furthermore, the angular velocity during steady rotation is compared with the motion of a vector toward Sun, which is estimated using current data of each solar cell array. | |||||
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: AA0046652006 |