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Title
Japanese:可変形状姿勢制御実証衛星ひばりのFM開発と運用計画 
English: 
Author
Japanese: 渡邉奎, 小林 寛之, 川口 直毅, 佐藤 宗一, 根路銘 省伍, 天木 祐希, 佐川 文隆, 笹川 悠太, 高橋 健一郎, 宮本 清菜, 中条 俊大, 谷津 陽一, 松永 三郎.  
English: Kei Watanabe, 小林 寛之, 川口 直毅, 佐藤 宗一, 根路銘 省伍, 天木 祐希, 佐川 文隆, 笹川 悠太, 高橋 健一郎, 宮本 清菜, 中条 俊大, Yoichi Yatsu, 松永 三郎.  
Language Japanese 
Journal/Book name
Japanese:スペース・エンジニアリング・コンファレンス講演論文集 
English: 
Volume, Number, Page Vol. 2021.30    No. 0    pp. A11
Published date  
Publisher
Japanese:一般社団法人 日本機械学会 
English: 
Conference name
Japanese: 
English: 
Conference site
Japanese: 
English: 
Abstract <p>We have developed a 50kg class microsatellite "HIBARI". The mission of this satellite is to demonstrate a novel attitude control method for microsatellites which is called “Variable Shape Attitude Control (VSAC).” VSAC is a method using anti-torque by driving variable shape structures. HIBARI has four drivable solar array paddles, and demonstrates rapid attitude control using the reaction force that moves them. HIBARI was adopted as the demonstration theme of the Japan Aerospace Exploration Agency (JAXA) Innovative Satellite Technology Demonstration-2, and will be launched by Epsilon Rocket. This paper describes the HIBARI project outline, system design, Flight Model development and on-orbit demonstration plan.</p>

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