誘導制御機器の信頼性向上の研究:IRUの高信頼性化の研究

Material type: 文書・図像類

Author: 里, 誠ほか

Publisher: 宇宙航空研究開発機構

Publication date: 2004-10-29

Material Format: Digital

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Note (General)：: Japan Aerospace Exploration Agency (JAXA), formerly named as National Space Development Agency (NASDA), developed Tuned Dry Gyroscope (TDG), as suprem...

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Material Type: 文書・図像類
Title: 誘導制御機器の信頼性向上の研究:IRUの高信頼性化の研究
Author/Editor: 里, 誠
Sato, Makoto
Author Heading: 里, 誠
Sato, Makoto
Publication, Distribution, etc.: 宇宙航空研究開発機構
Publication Date: 2004-10-29
Publication Date (W3CDTF): 2004-10-29
Alternative Title: Study on improvement for guidance and control actuators/sensors: The development of high-reliable Inertial Reference Unit
Periodical title: 宇宙航空研究開発機構研究開発資料: 平成15年度総合技術研究本部宇宙領域研究成果報告書:衛星系 = JAXA Research and Development Memorandum: FY15 Annual Report of Research & Development on Space Technology in the Institute of Space Technology and Aeronautics: Satellite System
No. or year of volume/issue: JAXA-RM-04-010
Volume: JAXA-RM-04-010
Pages: 19-22
ISSN (Periodical Title): ISSN : 1349-1121
Text Language Code: jpn
Subject Heading: IRU
信頼性
ジャイロスコープ
衛星姿勢制御
エンジニアリングモデル
精度
電子装置
柔軟性
reliability
gyroscope
satellite attitude control
engineering model
accuracy
electronic device
flexibility
Target Audience: 一般
Note (General): 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, it was 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. Prepared was every document needed. In FY 2004, an engineering model is built and its function and performance are qualified. In FY 2005, this study will be completed.
資料番号: AA0048057004
レポート番号: JAXA-RM-04-010
Access Restrictions: 限定公開
Periodical Title (NCID): AA11983593
https://ci.nii.ac.jp/ncid/AA11983593
Data Provider (Database): 国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
https://irdb.nii.ac.jp
Original Data Provider (Database): 宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ