Axisymmetric Gregorian Reflector System for a Space-Deployed Inflatable Antenna: Simulations and Measurements

A. Fenn, Jesse H. Mills, F. Robey, P. Dufilié, M. Hecht
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引用次数: 3

Abstract

An axisymmetric array-fed confocal parabolic Gregorian reflector antenna system for potential space deployment is explored. The simulated antenna at Ku-band utilizes a planar array located near the vertex of the primary reflector. Numerical electromagnetic simulations based on the multilevel fast multipole method (MLFMM) were used to analyze and optimize the antenna parameters for fixed on-axis peak directivity performance at Ku-band. Simulations of the radiation pattern performance of the dual reflector system with a 2.4m diameter primary reflector and 0.25m diameter subreflector operating at Ku band are presented. Compact range measurements of a prototype inflatable reflector system with an X-band horn-lens feed are compared with simulations.
空间部署充气天线轴对称格里高利反射系统:仿真与测量
研究了一种用于潜在空间部署的轴对称阵列馈电共聚焦抛物面格里高利反射面天线系统。ku波段模拟天线采用了位于主反射器顶点附近的平面阵列。采用基于多电平快速多极子方法(MLFMM)的电磁数值模拟,对ku波段固定轴上峰值指向性性能的天线参数进行了分析和优化。对2.4m主反射镜和0.25m副反射镜在Ku波段工作的双反射系统的辐射方向图性能进行了仿真。对x波段喇叭透镜馈源充气反射系统原型进行了距离测量,并与仿真结果进行了比较。
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