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宇宙用高精度MEMS ジャイロ開発の中間報告
https://jaxa.repo.nii.ac.jp/records/38616
https://jaxa.repo.nii.ac.jp/records/386164638b762-e2a7-4c4d-b10b-d82cce604161
名前 / ファイル | ライセンス | アクション |
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AC1400032.pdf (1.2 MB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 宇宙用高精度MEMS ジャイロ開発の中間報告 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | MEMS; Gyro; IMU; digital compensation; bias instability | |||||
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 | |||||
その他のタイトル(英) | ||||||
その他のタイトル | An Interim Report on the Development of High-Accuracy MEMS Gyros for Space Applications | |||||
著者 |
笹田, 武志
× 笹田, 武志× 嶋根, 愛理× 西田, 宏× 森口, 孝文× 内納, 亮平× 孫崎, 太× Sasada, Takeshi× Shimane, Eri× Nishida, Hiroshi× Moriguchi, Takafumi× Uchino, Ryouhei× Magosaki, Futoshi |
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著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
住友精密工業株式会社 | ||||||
著者所属 | ||||||
住友精密工業株式会社 | ||||||
著者所属 | ||||||
住友精密工業株式会社 | ||||||
著者所属 | ||||||
住友精密工業株式会社 | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Sumitomo Precision Products Co. Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Sumitomo Precision Products Co. Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Sumitomo Precision Products Co. Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Sumitomo Precision Products Co. Ltd. | ||||||
出版者 | ||||||
出版者 | 日本航空宇宙学会(JSASS) | |||||
出版者(英) | ||||||
出版者 | The Japan Society for Aeronautical and Space Sciences(JSASS) | |||||
書誌情報 |
第57回宇宙科学技術連合講演会講演集 en : Proceedings of 57th Space Sciences and Technology Conference 発行日 2013-10 |
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会議概要(会議名, 開催地, 会期, 主催者等) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 第57回宇宙科学技術連合講演会(2013年10月9日-11日. 米子コンベンションセンター(BiG SHiP)), 米子市, 鳥取県 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The development of high-accuracy Micro Electro Mecanical Systems (MEMS) gyroscopes for space applications havebeen started under the framework of the JAXA Aerospace Open Laboratory program in 2012. Taking advantage ofMEMS capabilities such as small, lightweight, low power consumption, and low cost, to modify the existing gyroproducts for navigation-grade. Two approaches; (1) advanced digital compensation for temperature variation, and (2)improvements of characteristics for MEMS sensor head, are adopted to accomplish the ten times better than theperformance of existing gyros (0.1 or less degrees per hours of bias instability). This paper reports a research outline,interim results, and revealed technical issues for high-accuracy. | |||||
権利 | ||||||
権利情報 | (C)2013 一般社団法人 日本航空宇宙学会 | |||||
著者版フラグ | ||||||
出版タイプ | VoR | |||||
出版タイプResource | http://purl.org/coar/version/c_970fb48d4fbd8a85 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AC1400032000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JSASS-2013-4365 |