Optimization of a novel, bidirectional, double-ring, deployable mesh antenna with a super-large aperture

被引:3
作者
Liu, Zhaoyang [1 ]
Ding, Yunlong [1 ]
Quan, Chaoyang [1 ]
Fan, Guozhuang [1 ]
Song, Jun [1 ]
Yang, Dongwu [1 ]
机构
[1] Xidian Univ, Sch Mechanoelect Engn, Xian 710071, Peoples R China
基金
中国国家自然科学基金;
关键词
Super -large -aperture deployable antenna; Double -ring truss; Structural design; Form -finding analysis; Modal analysis; DEPLOYMENT DYNAMICS; TENSION TRUSS; SPACE ANTENNA; DESIGN; REFLECTORS; MECHANISM;
D O I
10.1016/j.actaastro.2023.10.031
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The development of large antennas deployable in space is particularly important. A mesh antenna would be ideal because of its high surface accuracy and storage ratio. Here, we develop a novel, double-ring, deployable mesh antenna, then perform mass evaluation and modal analyses. The antenna exhibited better stiffness and a greater storage ratio, compared with typical mesh antennas. However, the mass was excessive. To overcome this problem, we designed a lightweight 5-m truss antenna, then measured its stiffness and strength. We optimized the computer-aided design of a mesh antenna with a super-large aperture, and we performed form-finding analysis of the cable-net. The new antenna included bidirectional deployment and exhibited a greater storage ratio and stiffness, compared with the conventional AstroMesh antenna. The first-order natural frequency was twofold greater than that of the AstroMesh antenna. Our work will aid fabrication of antennas with super-large apertures.
引用
收藏
页码:202 / 215
页数:14
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