Deployable and Reconfigurable Miura-Ori Reflectarray for Mission-Flexible Satellite Applications

C. A. Velez, Abdul-Sattar Kaddour, Collin Ynchausti, L. Howell, S. Magleby, S. Georgakopoulos
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引用次数: 2

Abstract

A novel foldable and reconfigurable reflectarray antenna (RA), operating at 8.425GHz for deep space communications based on an extended Miura-Ori origami pattern is presented. The aperture leverages the properties of subdivision and a folding feature to create a packable and reconfigurable antenna capable of changing its beam from a single pencil beam to a multi-beam aperture with beamsteering ability. A mechanical and theoretical EM analysis is carried out supported by a numerical algorithm using array theory. The results show that the proposed reflectarray can achieve a high packing efficiency of 92%. This RA provides a pencil beam in the broadside at (θ = 0°, ϕ = 0) in its flat configuration and multi-beam (dual, triple and quad-beams) depending on its folding angle. For CubeSat applications, the key advantages of this RA are its decreased stowage volume, reconfigurable EM performance, beamsteering capabilities, low fabrication cost, and reduced complexity.
用于任务柔性卫星应用的可部署和可重构的Miura-Ori反射器
提出了一种基于扩展Miura-Ori折纸模式的可折叠可重构深空通信反射天线(RA),工作频率为8.425GHz。该孔径利用细分特性和折叠特性来创建可包装和可重新配置的天线,能够将其波束从单个铅笔波束转变为具有波束导向能力的多波束孔径。在阵列理论的数值算法支持下,进行了力学和理论的电磁分析。结果表明,所提出的反射光封装效率高达92%。该RA在其平面配置中提供宽侧(θ = 0°,ϕ = 0)的铅笔光束,并根据其折叠角度提供多光束(双,三和四光束)。对于CubeSat应用来说,这种RA的主要优点是体积小、EM性能可重构、波束导向能力强、制造成本低、复杂性低。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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