Art

J-GLOBAL ID：201002232522475905   Reference number：10A0019961

Development of a Small-spin-axis Controller and Its Application to a Solar Sail Subpayload Satellite

小型スピン軸制御器の開発とソーラーセイルサブペイロード衛星へのその応用

Author (6)： SAIKI Takanao (The Inst. of Space and Astronautical Sci. / Japan Aerospace Exploration Agency) ,  NAKAYA Koji (The Inst. of Space and Astronautical Sci. / Japan Aerospace Exploration Agency) ,  YAMAMOTO Takayuki (The Inst. of Space and Astronautical Sci. / Japan Aerospace Exploration Agency) ,  TSUDA Yuichi (The Inst. of Space and Astronautical Sci. / Japan Aerospace Exploration Agency) ,  MORI Osamu (The Inst. of Space and Astronautical Sci. / Japan Aerospace Exploration Agency) ,  KAWAGUCHI Jun'ichiro (The Inst. of Space and Astronautical Sci. / Japan Aerospace Exploration Agency)
Material： Transactions of the Japan Society for Aeronautical and Space Sciences, Space Technology Japan (Web)  (Trans Jpn Soc Aeronaut Space Sci Space Technol Jpn (Web))
Volume： 7  Page： 25-32 (J-STAGE)  Publication year： 2009 
JST Material Number： U0121A  ISSN： 1347-3840  Document type： Article
Article type： 原著論文  Country of issue： Japan (JPN)  Language： ENGLISH (EN)

Thesaurus term： nutation ,  *propulsion system ,  *attitude control ,  spin ,  demonstration experiment ,  *control law ,  *solar sail ,  *spinning satellite
Semi thesaurus term： *スピン安定衛星 ,  spin (air vehicle)

JST classification (1)： Flight control systems  (QK05020Z)

Reference (5)：

• 1) Kawaguchi, J., Morita, Y., Nakajima, T., Ishii, N., Hashimoto, T., Yamakawa, H., Hirokawa, E., Yasuda, S. and Balloon Group: Flight Test of the Rhumb Line Control System via Balloon, Proceedings of the 3rd Workshop on Astrodynamics and Flight Mechanics, 1993, pp.156-161.
• 2) Kawaguchi, J.: On the Simplified Recursive Formula of Rhumb Line Maneuvers with its Application to Identification of Directional Dispersion, Proceedings of the 3rd Workshop on Astrodynamics and Flight Mechanics, 1993, pp.194-199.
• 3) Yamamoto, T., Mori, O., Shida, M. and Kawaguchi, J.: Development of Gas-Liquid Equilibrium Thruster for Small Satellite, International Symposium on Space Technology and Science, ISTS 2006-k-32, 2006.
• 4) Tsuda, Y., Mori, O., Nishimura. Y. and Kawaguchi,J.: Deployment Experiment of Thin Flexible Membrane Using Sounding Rocket for Future Solar Sail Mission, International Symposium on Space Technology and Science, ISTS 2004-c-11, 2004.
• 5) Nishimura, Y., Tsuda, Y., Mori, O. and Kawaguchi, J.: The Deployment Experiment of Solar Sail with Sounding Rocket, 55th International Astronautical Congress, IAC-04-A.5.10, 2004.

Terms in the title (5)： スピン軸 ,  制御器 ,  開発 ,  衛星 ,  応用