Development of an out-of-Focus Irradiator Based on a Phased Antenna Array for a Space Communications' Parabolic Reflector Antenna

IF 0.2 Q4 INSTRUMENTS & INSTRUMENTATION Devices and Methods of Measurements Pub Date : 2019-09-09 DOI:10.21122/2220-9506-2019-10-3-233-242
D. V. Douksha, S. Liashkevich, V. Saetchnikov
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Abstract

Mirror antenna systems are widely used in satellite and space communication systems and radio astronomy. Development of these areas requires new efficient antenna systems' design. Possible technical solution for creating an effective mirror antenna is a “hybrid” scheme, when an adaptive phased antenna array is used as an irradiator. This paper is devoted to the development of an out-of-focus irradiator based on a phased antenna array for a space communications' parabolic reflector antenna. The aim of the work is to develop an optimal design of the irradiator with the choice of the structural element of the antenna array and experimental studies of the selected structural element.The wavefront recovery method was used as a tool for selecting the irradiator configuration. The idea of this method use is to reproduce the electromagnetic field of an incident plane wave with an irradiator in order to uniformly illuminate the aperture of the antenna mirror.In order to select the structural element of the irradiator several antennas were considered: a patch antenna, a flat spiral antenna, a conical spiral antenna. The requirements for the phased antenna array element were defined. The irradiator based on the above mentioned was simulated and the irradiator geometry was optimized according to the maximum gain criterion.The maximum gain was achieved for the irradiator based on conical spiral antennas and amounted to 30.8 dB, which for the considered mirror aperture of 2.4 m is close to traditional focal schemes. The results obtained make it possible to create an adaptive antenna system able to compensate for the deviations of the mirror's shape from the theoretical profile, as well as phase distortions in the atmosphere by changing the lattice weights coefficients.
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空间通信抛物面反射天线相控阵离焦辐照体的研制
镜面天线系统广泛应用于卫星和空间通信系统以及射电天文学。这些领域的发展需要新的高效天线系统的设计。创建有效镜像天线的可能技术解决方案是一种“混合”方案,即使用自适应相控阵天线作为辐照器。研究了一种用于空间通信抛物面反射面天线的基于相控阵的失焦辐照体的研制。本文的目的是通过对天线阵结构元件的选择和所选结构元件的实验研究,对辐照器进行优化设计。采用波前恢复法作为选择辐照体结构的工具。这种方法的思想是用辐照器再现入射平面波的电磁场,以便均匀地照亮天线反射镜的孔径。为了选择辐照体的结构单元,考虑了贴片天线、平面螺旋天线和锥形螺旋天线。确定了相控阵单元的要求。对基于上述原理的辐照器进行了仿真,并根据最大增益准则对辐照器的几何形状进行了优化。基于锥形螺旋天线的辐射器增益最大,达到30.8 dB,考虑到2.4 m的反射镜孔径,这与传统的聚焦方案接近。获得的结果使得创建一个自适应天线系统成为可能,该系统能够通过改变晶格权重系数来补偿镜面形状与理论轮廓的偏差,以及大气中的相位畸变。
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来源期刊
Devices and Methods of Measurements
Devices and Methods of Measurements INSTRUMENTS & INSTRUMENTATION-
自引率
25.00%
发文量
18
审稿时长
8 weeks
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