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Design and Deployment Experiment Research on Support Mechanism for Hexagonal Prism Modular Deployable Antenna

机译：六角形棱镜模块化可展位天线支撑机制的设计与部署试验研究

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摘要

In order to meet the requirements of the development trend of large aperture space deployable antenna, based on the characteristics of cellular structure, a configuration scheme of support mechanism for hexagonal prism modular deployable antenna is proposed. The topological law of the module is studied, and the configuration design is carried out. Then the multi module kinematic model is established, and the numerical simulation analysis is carried out. The experiment results show that the deployable antenna support mechanism can be successfully deployed in many deployment tests, and there is no jamming fault, which indicates that the mechanism configuration principle and design structure scheme are feasible. The research results provide a reference for other types of deployable antenna mechanism.
机译：为了满足大型光圈空间可展开天线的发展趋势的要求，基于蜂窝结构的特点，提出了一种六边形棱镜模块化可展开天线的支撑机构的配置方案。 研究了模块的拓扑规律，并进行了配置设计。 然后建立了多模块运动模型，并执行数值模拟分析。 实验结果表明，可以在许多部署测试中成功部署可展开的天线支撑机制，并且没有干扰故障，这表明机构配置原理和设计结构方案是可行的。 研究结果为其他类型的可展开天线机构提供了参考。

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