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Investigation and design of a very compact circularly polarized microstrip antenna for use on microsatellites.

机译:用于微型卫星的非常紧凑的圆极化微带天线的研究和设计。

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摘要

Microsatellites are becoming increasingly viable as a platform for research and communication. Their small size and weight demand innovative and compact electrical and antenna systems There has been significant research into the miniaturization of microstrip patch antennas. The main techniques for miniaturization include the incorporation of various shorting or loading schemes, including the very popular quarter-wave patch arrangement, and the use of high dielectric constant materials. The quarter-wave concept was extended by proposing the idea of folding both the patch and the ground plane into layers to create a folded shorted patch (S-P) further reducing the antenna element size. This thesis presents the investigation and design of a circularly polarized folded S-P antenna using multilayer printed circuit board (PCB) technology for use in microsatellite communication.;This thesis describes the theoretical, simulation, and experimental based investigation of the performance of a folded S-P structure. Transmission line models for a linearly polarized antenna element were developed and extended for use with dielectric substrate materials. Using the theoretical models as a starting point, simulations were carried out on various single element configurations to qualitatively understand their effects on antenna performance. These configurations included probe, aperture, and capacitive plate terminated probe feed systems, different dielectric materials, and the usage of electrical vias to form electrical walls. Findings of the single element investigation were then applied in the design and optimization of a four-element antenna array where the elements and their corresponding feed signals were sequentially rotated and phased to generate circular polarization.;Both a linearly polarized single element prototype and a four-element circularly polarized prototype were fabricated. The four-element array prototype was designed to work at 400MHz. It had a length, width, and height of 150mm x 150mm x 40mm which is equivalent to 0.2lambdao x 0.2lambda o x 0.053lambdao. Experimental performance of the prototypes in terms of the return loss (S11) and radiation patterns was measured and analyzed. The results supported the simulation findings. The measured impedance bandwidth for the array prototype was greater than 20MHz and the simulation predicted a boresight realized gain of 2.3dBic. The results and subsequent analysis show that implementation of a circularly polarized folded S-P antenna using multilayer PCB techniques has good potential for CP antenna systems on microsatellites where size is critical.;Keywords: Antenna, design, compact, circular polarization, folded, microsatellite.
机译:作为研究和交流的平台,微卫星正变得越来越可行。它们的体积小,重量轻,需要创新,紧凑的电气和天线系统。微带贴片天线的小型化已得到大量研究。小型化的主要技术包括采用各种短路或负载方案,包括非常流行的四分之一波长贴片布置,以及使用高介电常数材料。通过提出将贴片和接地层都折叠成多层以产生折叠的短路贴片(S-P)的想法,扩展了四分之一波的概念,从而进一步减小了天线元件的尺寸。本文提出了一种用于微卫星通信的圆极化折叠式SP天线的研究和设计,该天线采用多层印刷电路板(PCB)技术。本文描述了基于理论,仿真和实验的折叠式SP结构性能研究。 。开发并扩展了用于线性极化天线元件的传输线模型,以用于介电基板材料。以理论模型为起点,对各种单元素配置进行了仿真,以定性地了解它们对天线性能的影响。这些配置包括探针,孔和电容板端接的探针馈送系统,不同的介电材料以及使用电过孔来形成电壁。然后将单元素研究的结果应用到四元素天线阵列的设计和优化中,其中元素及其相应的馈电信号依次旋转和定相以产生圆极化;线性极化的单元素原型和四个制作了圆偏振原件。四元素阵列原型设计为在400MHz下工作。它的长度,宽度和高度为150mm x 150mm x 40mm,相当于0.2lambdao x 0.2lambda o x 0.053lambdao。测量并分析了原型在回波损耗(S11)和辐射方向图方面的实验性能。结果支持了仿真结果。阵列原型的测量阻抗带宽大于20MHz,仿真预测视轴实现的增益为2.3dBic。结果和随后的分析表明,使用多层PCB技术实现圆极化折叠式S-P天线对于尺寸至关重要的微卫星CP天线系统具有良好的潜力。关键词:天线,设计,紧凑,圆极化,折叠,微卫星

著录项

  • 作者

    Murdoch, Andrew P.;

  • 作者单位

    Royal Military College of Canada (Canada).;

  • 授予单位 Royal Military College of Canada (Canada).;
  • 学科 Engineering Electronics and Electrical.
  • 学位 M.A.Sc.
  • 年度 2012
  • 页码 224 p.
  • 总页数 224
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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