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IRUの高信頼性化の研究:プロジェクトの支援
https://jaxa.repo.nii.ac.jp/records/6307
https://jaxa.repo.nii.ac.jp/records/630754e70cc1-18f3-46ae-9808-f885d7374dab
名前 / ファイル | ライセンス | アクション |
---|---|---|
49054051.pdf (624.7 kB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | IRUの高信頼性化の研究:プロジェクトの支援 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | チューンドドライジャイロ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 衛星姿勢制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 部品信頼性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 慣性基準装置 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ダイナミックレンジ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | VFコンバータ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 高精度 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙機電子機器 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 性能試験 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | tuned dry gyro | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | satellite attitude control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | component reliability | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | inertial reference unit | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | dynamic range | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | VF converter | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | high accuracy | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | spacecraft electronic equipment | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | performance test | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル(英) | ||||||
その他のタイトル | The development of high-reliable Inertial Reference Unit: Project support | |||||
著者 |
里, 誠
× 里, 誠× 川井, 洋志× Sato, Makoto× Kawai, Hiroshi |
|||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構 | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航空研究開発機構特別資料: 平成16年度総合技術研究本部宇宙領域宇宙科学研究本部合同研究成果報告書:人工衛星系基盤技術 en : JAXA Special Publication: FY2004 Report of Joint Research Achievements of the Space Division of Institute of Aerospace Technology and Institute of Space and Astronautical Science: Basic Technologies of Satellite Systems 巻 JAXA-SP-05-008, p. 253-256, 発行日 2006-01-20 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Japan Aerospace Exploration Agency (JAXA), formerly named as National Space Development Agency (NASDA), developed Tuned Dry Gyroscope (TDG), as supreme precision rate sensor for satellite attitude control. JAXA also developed Inertial Reference Unit (IRU) using TDG. This IRU is used on almost every JAXA satellite. It has passed about fifteen years since the development. It is difficult to purchase some kind of electronics parts nowadays. Meanwhile, satellite system requires higher accuracy, more operation flexibility and so on. So, we decided to redesign IRU. Aiming is high-reliability and high-accuracy. The study has started in FY 2001. In FY 2003 IRU redesign was completed and we prepared every document needed. In FY 2004, we built an Engineering Model and qualify its function and performance. In FY 2005, we will complete this study. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-113X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11984031 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0049054051 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-SP-05-008 |