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気球切離しコマンド機能の二重化 : 航空保安用コマンドシステムの開発
https://jaxa.repo.nii.ac.jp/records/33146
https://jaxa.repo.nii.ac.jp/records/331468640a1bc-5001-4fd1-acd5-bc707afde6c3
名前 / ファイル | ライセンス | アクション |
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SA0167035.pdf (1.2 MB)
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Item type | 紀要論文 / Departmental Bulletin Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 気球切離しコマンド機能の二重化 : 航空保安用コマンドシステムの開発 | |||||
言語 | ||||||
言語 | jpn | |||||
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 | departmental bulletin paper | |||||
その他のタイトル(英) | ||||||
その他のタイトル | A New Command Reciever for Balloon Flight Temination | |||||
著者 |
矢島, 信之
× 矢島, 信之× 山上, 隆正× 太田, 茂雄× 本田, 秀之× 長尾, 和男× 川瀬, 克行× Yajima, Nobuyuki× Yamagami, Takamasa× Ohota, Shigeo× Honda, Hideyuki× Nagao, Kazuo× Kawase, Katsuyuki |
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著者所属 | ||||||
宇宙科学研究所 | ||||||
著者所属 | ||||||
宇宙科学研究所 | ||||||
著者所属 | ||||||
宇宙科学研究所 | ||||||
著者所属 | ||||||
宇宙科学研究所 | ||||||
著者所属 | ||||||
松下通信工業電波事業部 | ||||||
著者所属 | ||||||
松下通信工業電波事業部 | ||||||
出版者 | ||||||
出版者 | 宇宙科学研究所 | |||||
出版者(英) | ||||||
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 31, p. 3-21, 発行日 1993-03 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A tele-command radio receiver is to be equipped on a large scientific balloon in order to control on-board equipments such as a outlet valve of a ballast hopper, an air duct valve attached at a top of a balloon and also other scientific instruments. In those many functions, the command which terminate balloon flight plays the most important role for balloon flight controls. This command activates a separation mechanism which is inserted in suspension ropes. Then a balloon gondola descends to the ground (or sea) by a parachute. The reliability of this flight termination command had better to be impoved by full redundant system. This paper deals with a newly developed command receiver which has a single function to receive a flight termination command. This command receiver is attached near a balloon bottom and directly connected to the separation mechanism. To combine this receiver and an ordinal command receiver attached in the gondola, the flight termination command becomes dual system. At first the design concept of this new command receiver is explained in detail in relation to the total command system. Then the actual system construction and some results of its flight test are described. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0285-9920 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN00354485 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: SA0167035000 |