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高精度ファイバージャイロIRUの研究:高性能姿勢制御技術の研究
https://jaxa.repo.nii.ac.jp/records/6303
https://jaxa.repo.nii.ac.jp/records/6303ca73416f-a9d4-48c2-b32f-6445ea07bd61
名前 / ファイル | ライセンス | アクション |
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49054047.pdf (2.3 MB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 高精度ファイバージャイロIRUの研究:高性能姿勢制御技術の研究 | |||||
言語 | ||||||
言語 | jpn | |||||
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 | 慣性モーメント | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 光学ジャイロ | |||||
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 | FOG-IRU | |||||
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 | スタートラッカ | |||||
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 | moment of inertia | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | optical gyroscope | |||||
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 | FOG-IRU | |||||
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 | star tracker | |||||
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 | Study of high performance Fiber Optic Gyro Inertial Reference Unit: Study of high performance satellite attitude control system | |||||
著者 |
巳谷, 真司
× 巳谷, 真司× 鈴木, 秀人× 川井, 洋志× Mitani, Shinji× Suzuki, Hideto× Kawai, Hiroshi |
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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 | ||||||
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 | ||||||
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. 231-236, 発行日 2006-01-20 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Aiming for the application to the future spacecraft attitude control system, we are studying the high performance Fiber Optic Gyro Inertial Reference Unit (FOG-IRU). To fulfill the requirements of low noise, stable bias and stable scale factor, we adopt the high power Fiber Light Source, a long fiber coil (several kilo-meters) and the digital serrodyne closed loop configuration. This paper outlines the result of our FOG-IRU development during FY16 such as evaluation of the FOG Pre-EM model, evaluation of the temperature characteristics of the Pre-EM model, evaluation for the optical error factor, designs and re-fabrication for the performance improvement, and evaluation of the Pre-EM re-fabrication model. | |||||
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: AA0049054047 | |||||
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 |