Design and simulation of a closed-loop deployable structure

被引：0
|
作者：
Zheng, Fei [1 ]
Chen, Mei [1 ]
Hao, Bei [1 ]
机构：
[1] Xidian Univ, Sch Electromech Engn, Xian 710071, Peoples R China
来源：
ISSCAA 2006: 1ST INTERNATIONAL SYMPOSIUM ON SYSTEMS AND CONTROL IN AEROSPACE AND ASTRONAUTICS, VOLS 1AND 2 | 2006年
关键词：
D O I：
暂无
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
A closed-loop deployable structure has potential applications for ultra-lightweight solar arrays, solar sails, and radar structures. We firstly proposed a reasonable structure of this kind of structure in order to build up a feasible deployable paraboloid antenna with a diameter of 3 in for a good packaging ratio. Then dynamic simulations of the deploying processes with two typical working conditions are presented, which reveals that our design is feasible. Next the detailed structures of our design are given out. The stowed diameter of the structure is 0.09 m and the mass of it is 0.6 Kg. With a packaging ratio to be 0.03 and an ultra-lightweight mass, such a structure has a great potential to be used in a huge deployable mesh antenna.
引用
收藏
页码：1295 / +
页数：2
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