Initial Intension Analysis of Astromesh Structure of the Astromesh Deployable Antenna

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Abstract:

The reflector of the astromesh deployable antenna is formed with metallic net fixed on the nodes of its astromesh. The astromesh determines shape of the reflector, so analysis of the astromesh is necessary. With force density method and paraboloid equation, balance equations of the astromesh were set up at first. Length and tension of the cords, coordinates of the nodes and outer forces on the nodes were included in the equations. After the coefficient matrix was transformed, a group of orthogonal normalization basis in its null space was obtained. Solving method of the balance equations was analyzed. After optimized with the genetic algorithm, initial tensions of all cords were obtained finally. The analysis method can make design of the astromesh more rational and reliable.

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99-102

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July 2011

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© 2011 Trans Tech Publications Ltd. All Rights Reserved

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[1] Niu Zhiyong, Wang Sanmin and Wang Lei: Mechanical Science and Technology for Aerospace Engineering Vol. 3 (2009), p.331

Google Scholar

[2] Li Tuanjie, Zhang Yan and Li Tao: Acta Aeronautica Et Astronautica Sinica Vol. 3 (2009), p.444

Google Scholar

[3] Zhao Mengliang , Wu Kaicheng and Guan Fuling: Journal of Zhejiang University Vol. 39 (2005), p.1669

Google Scholar

[4] Yang Yulong and Guan Fuling: Chinese Journal of Space Science Vol. 5 (2009), p.529

Google Scholar

[5] LUO Ani, DENG Zongquan, LIU Rongqiang and LIU Heping: Journal of Harbin Engineering University Vol. 3 (2011), p.355

Google Scholar