WEKO3
アイテム
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ストラップダウン方式用広角度積分ジャイロの研究
https://jaxa.repo.nii.ac.jp/records/44596
https://jaxa.repo.nii.ac.jp/records/445966654a828-10f6-460d-b22a-aa518216c52b
名前 / ファイル | ライセンス | アクション |
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naltr00349.pdf (2.2 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 | ストラップダウン方式用広角度積分ジャイロの研究 | |||||
言語 | ||||||
言語 | jpn | |||||
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 on a Wide Angle Miniature Integrating Gyro for Strapdown System | |||||
著者 |
大月, 正男
× 大月, 正男× 新宮, 博公× 鈴木, 孝雄× 円居, 繁治× 田畑, 浄治× OTSUKI, Masao× SHINGU, Hirokimi× SUZUKI, Takao× ENKYO, Shigeharu× TABATA, Joji |
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著者所属 | ||||||
航空宇宙技術研究所計測部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所計測部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所計測部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所計測部 | ||||||
著者所属 | ||||||
宇宙開発事業団 | ||||||
著者所属 | ||||||
元・航空宇宙技術研究所計測部 | ||||||
著者所属(英) | ||||||
en | ||||||
Instrumentation and Control Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Instrumentation and Control Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Instrumentation and Control Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Instrumentation and Control Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
National Space Development Agency of Japan(NASDA) | ||||||
著者所属(英) | ||||||
en | ||||||
Former Instrumentation and Control Division, National Aerospace Laboratory(NAL) | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory(NAL) | |||||
書誌情報 |
航空宇宙技術研究所報告 en : Technical Report of National Aerospace Laboratory TR-349 巻 349, p. 20, 発行日 1975-11 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | This paper describes the historical procedure and the result of study on the development of the gyro with higher performance and precision, which is called WAMIG(wide angle miniature integrating gyro). NAL began development of the gyro for strapdown inertial guidance in 1964. In the first stage of development, the MIG(miniature integrating gyro), which was a prototype gyro, was studied in order to clarify difficulties in developing the WAMIG. Secondly, an orifice damper was developed for obtaining the wider angle and a balance pan was applied to the slight adjustment of the unbalanced mass. Finally, the development of the WAMIG was made possible through the design of a permanent-magnet and moving-coil type torque generator. The recently developed gyros have the following performance features: service life of more than 1000 hr., random drift 0.02 deg/hr., elastic restraint coefficient 0.05 deg/hr/mRad, anisoelastic coefficient 0.1 deg/hr/g2 and day to day stabilities 0.2 deg/hr(acceleration-insensitive drift), and 0.2 deg/hr/g(acceleration-sensitive drift). | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0389-4010 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: NALTR0349000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL TR-349 |