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磁気軸受アクチュエータを用いたアクティブ擾乱抑制実験
https://jaxa.repo.nii.ac.jp/records/38756
https://jaxa.repo.nii.ac.jp/records/3875675228f80-86e5-4a2b-8264-d09b77d0bf2a
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2016-08-15 | |||||
タイトル | ||||||
タイトル | 磁気軸受アクチュエータを用いたアクティブ擾乱抑制実験 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Active distrubance suppression | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Magnetic bearing actuator | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Precision pointing | |||||
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 | |||||
アクセス権 | ||||||
アクセス権 | metadata only access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_14cb | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Experiments on Active Disturbance Suppression using Magnetic Bearing Actuator | |||||
著者 |
茂渡, 修平
× 茂渡, 修平× 神澤, 拓也× 山中, 浩二× Shigeto, Shuhei× Kanzawa, Takuya× Yamanaka, Koji |
|||||
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 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
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 | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
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59回宇宙科学技術連合講演会講演集 en : Proceedings of 59th Space Sciences and Technology Conference 発行日 2015-10-07 |
|||||
関係URI | ||||||
識別子タイプ | URI | |||||
関連識別子 | https://www.jsass.jp/conference/sstc59.php | |||||
関連名称 | https://www.jsass.jp/conference/sstc59.php | |||||
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59回宇宙科学技術連合講演会(2015年10月7日-9日. かごしま県民交流センター), 鹿児島市, 鹿児島県 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In astronomy- and Earth-observation satellites, disturbances induced by internal mechanisms degrade the pointing stability. Though satellites suppress the disturbance using passive-typeisolators that consist of dampers and springs, its capability is limited. Instead of passive isolators, authors developed the active disturbance suppression using accelerator and magnetic bearing actuator. This paper describes the configuration of the active disturbance suppression and experimental results. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11800503 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AC1600012000 | |||||
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-2015-4557 |