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中性大気密度計測用加速度計に関する6自由度制御の研究
https://jaxa.repo.nii.ac.jp/records/3792
https://jaxa.repo.nii.ac.jp/records/3792d4a01393-e6a7-4cf7-91dd-e491e51f5c6f
名前 / ファイル | ライセンス | アクション |
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AA1530019007.pdf (426.4 kB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-05-08 | |||||
タイトル | ||||||
タイトル | 中性大気密度計測用加速度計に関する6自由度制御の研究 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Space | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Neutral atmospheric density | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Accelerometer | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Six-DOF control | |||||
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 | Study on the six-DOF control for a neutral atmospheric density measurement accelerometer | |||||
著者 |
大里, 優一郎
× 大里, 優一郎× 新谷, 昌人× 東尾, 奈々× 渡邉, 力夫× Osato, Yuichiro× Araya, Akito× Higashio, Nana× Watanabe, Rikio |
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著者所属 | ||||||
東京都市大学 | ||||||
著者所属 | ||||||
東京大学 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
東京都市大学 | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo City University | ||||||
著者所属(英) | ||||||
en | ||||||
The University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo City University | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構(JAXA) | |||||
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: 第11回宇宙環境シンポジウム講演論文集 en : JAXA Special Publication: Proceedings of the 11th Spacecraft Environment Symposium 巻 JAXA-SP-14-012, p. 61-64, 発行日 2015-03-20 |
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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11回宇宙環境シンポジウム (2014年12月10日-11日. 大阪府立大学 I-siteなんば), 大阪 | |||||
会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 11th Spacecraft Environment Symposium (December 10-11, 2014, I-site Namba, Osaka Prefecture University), Osaka, Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A low-orbit spacecraft receives large air drag because neutral atmosphere gets denser in lower earth orbit. A thermosphere model NRL-MSIS00 was establishes based on measurement data of neutral atmospheric density and it is currently used for spacecraft drag estimation. However, the model is unable to be applied to the super low Earth orbit because measurement of neutral atmospheric density at this altitude is difficult due to high density of air. In order to obtain neutral atmospheric density, an accelerometer is used to detect deceleration of spacecraft due to air drag. In the case of super low altitude air density estimation, highly sensitive and wide-range accelerometers that can detect 10(exp -8) - 10(exp -2) m/s2 is required. Thus a new type of accelerometers which consists of contactless optical displacement sensors and magnetic actuators that has enough controlling force is proposed. This research investigates of elemental technology of the new type accelerometer. An experimental model of the new type of accelerometer demonstrated detection of two-DOF acceleration. A six-DOF accelerometer extended from the two-DOF will be constructed. | |||||
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 | |||||
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: AA1530019007 | |||||
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-14-012 |