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高精度画像処理アルゴリズムによる「いぶき」太陽電池パネル挙動計測
https://jaxa.repo.nii.ac.jp/records/22421
https://jaxa.repo.nii.ac.jp/records/2242130cd8f18-ce52-4ac9-b9fa-56b6d096c707
名前 / ファイル | ライセンス | アクション |
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PA1410057.pdf (1.5 MB)
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Item type | 学術雑誌論文 / Journal Article(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 高精度画像処理アルゴリズムによる「いぶき」太陽電池パネル挙動計測 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Image Processing; Measurement Method; Space Equipment; Solar Array Paddle; Flexible Structure | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_6501 | |||||
資源タイプ | journal article | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Measurement of the “IBUKI” Solar Array Panel's Behavior Using High Precision Image Processing | |||||
著者 |
鈴木, 悟史
× 鈴木, 悟史× 中村, 俊之× 吉井, 正広× 中島, 正勝× 中西, 洋喜× 本田, 瑛彦× 小田, 光茂× Suzuki, Satoshi× Nakamura, Toshiyuki× Yoshii, Masahiro× Nakajima, Masakatsu× Nakanishi, Hiroki× Honda, Akihiko× Oda, Mitsushige |
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著者所属 | ||||||
(株)エイ・イー・エス | ||||||
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 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
東京工業大学大学院 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Advanced Engineering Services Co.,Ltd. | ||||||
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) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency(JAXA) | ||||||
出版者 | ||||||
出版者 | 日本機械学会 | |||||
書誌情報 |
日本機械学會論文集 C編 巻 79, 号 807, p. 4233-4248, 発行日 2013-11 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Generally, many space satellites have large solar array panels for power generation and large antennas for observation and communication. The panels and antennas must be lightweight because of the payload weight limit of the launch vehicle. So, they are very flexible, with little damping ability. This results in vibrations cause serious problems. When the thermal environment around a flexible structure on orbit such as a solar array panel changes to cold or hot, the flexible structure produces its own deformation or vibration. These occur most often during rapid temperature changes called thermal snap or thermally-induced vibration, which has been known to cause attitude disturbance in Low Earth Orbit (LEO) satellites. Thermal snap vibration occurring on a flexible solar array panel is very slow. It is very difficult to measure thermal snap motion by sensors such as accelerometer. The behavior of a space structure affected by thermal snap has never been observed directly in space so far. This report presents the measurement results of “IBUKI” solar array panel's behavior using monitor camera. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0387-5024 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN00187463 | |||||
DOI | ||||||
関連タイプ | isVersionOf | |||||
識別子タイプ | DOI | |||||
関連識別子 | http://dx.doi.org/10.1299/kikaic.79.4233 | |||||
関連名称 | info:doi/10.1299/kikaic.79.4233 | |||||
権利 | ||||||
権利情報 | (C)2013 日本機械学会 | |||||
著者版フラグ | ||||||
出版タイプ | AM | |||||
出版タイプResource | http://purl.org/coar/version/c_ab4af688f83e57aa | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: PA1410057000 |