Item type |
紀要論文 / Departmental Bulletin Paper(1) |
公開日 |
2015-03-26 |
タイトル |
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タイトル |
「よじれリアクション」制御方式 |
言語 |
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言語 |
jpn |
資源タイプ |
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資源タイプ識別子 |
http://purl.org/coar/resource_type/c_6501 |
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資源タイプ |
departmental bulletin paper |
その他のタイトル(英) |
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その他のタイトル |
"Yojire-Reaction" Azimuth Control System for Balloon Gondola |
著者 |
矢島, 信之
太田, 茂雄
並木, 道義
渕山, 央樹
Yajima, Nobuyuki
Ohta, Sigeo
Namiki, Michiyosi
Fuchiyama, Ohmi
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著者所属 |
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宇宙科学研究所 |
著者所属 |
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宇宙科学研究所 |
著者所属 |
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宇宙科学研究所 |
著者所属 |
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東海大学工学部 |
出版者 |
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出版者 |
宇宙科学研究所 |
出版者(英) |
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出版者 |
Institute of Space and Astronautical Science |
書誌情報 |
宇宙科学研究所報告. 特集: 大気球研究報告
巻 30,
p. 13-30,
発行日 1992-02
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抄録(英) |
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内容記述タイプ |
Other |
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内容記述 |
A new type of attitude control system using a reaction wheel has been developed for an azimuth control of a balloon gondola. This control system has long rotation arms and dummy weights attached each end of them. These arms act as a fly-wheel with large moment of inertia and are driven by a geared DC motor. The fly-wheel and its driving mechanisms are attached to a top of gondola. Compared with a conventional reaction wheel control system which is instralled in a gondola, this control system is compact, light weight and easy to handle. This paper describes hardware characteristrics and also control performance of this new system. This control system was applied to azimuth control of the astronomical telescope for infrared observations. The balloon experiments carried out two times at the National Scientific Balloon Facility at Palestine, Texas in May and June 1991. During the balloon flight, this control system worked well and accomplished precision raster scanning of the central region of the Galaxy with high accuracy which have been verified by the preliminary ground test. Some results of the flight tests are also described in this paper. |
ISSN |
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収録物識別子タイプ |
ISSN |
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収録物識別子 |
0285-9920 |
書誌レコードID |
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収録物識別子タイプ |
NCID |
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収録物識別子 |
AN00354485 |
資料番号 |
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内容記述タイプ |
Other |
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内容記述 |
資料番号: SA0167024000 |