Deployment dynamics of a simplified spinning IKAROS solar sail via absolute coordinate based method

Author:

Zhao Jiang,Tian Qiang,Hu Hai-Yan

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Computational Mechanics

Reference40 articles.

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2. Melnikov, V. M., Koshelev, V. A.: Large Space Structures Formed by Centrifugal Forces. (1st edn.) Earth Space Institute Book Series, Gordon and Breach, Amsterdam 4, 21–61 (1998)

3. Nakasuka, S., Aoki, T., Ikeda, I., et al.: “Furoshiki Satallite”-a large membrane structure as a novel space system. Acta Astronautica 48, 461–468 (2001)

4. Ruggiero, E.J., Inman, D.J.: Gossamer spacecraft: recent trends in design, analysis, experimentation, and control. Journal of Spacecraft and Rockets 43, 10–24 (2006)

5. Mori, O., Sawada, H., Hanaoka, F., et al.: Development of deployment system for small size solar sail mission. Transaction of JSASS, Space Technology Japan 7, Pd 87–Pd 94 (2009)

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