机载x波段维瓦尔第天线阵列的设计与开发

I. Mehmood, A. Qureshi, Muhammad Muaz, Channa Babar Ali
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引用次数: 0

摘要

本文介绍了一种用于机载有源相控阵雷达的x波段维瓦尔第天线阵列的设计分析。首先,进行了参数化研究,找出了维瓦尔第天线阵列的设计特性与其性能之间的关系。然后,在进行8×8天线阵列设计之前,设计了通向1×8均匀线性阵列的单个Vivaldi天线以获得最佳性能。此外,还对所设计的天线阵列进行了调谐和优化,以达到预期的效果。为了满足机载雷达系统的尺寸限制,在进给段采用了从带状线到槽线的过渡。设计的天线阵列工作在x波段,中心频率为10ghz。它包含64个元素的阵列(8×8),实现22 dB增益。在2 GHz带宽范围内(8.55 ~ 10.75 GHz),回波损耗(S11)小于−10 dB。发射峰值功率为640 W,方位角和仰角覆盖±60°,波束宽度为13°。两个元件之间的隔离度为20 dB,旁瓣电平(SLL)为−30 dBc。设计了单单元维瓦尔第天线和均匀线性1×8单元维瓦尔第阵列天线,形成了8×8单元天线阵。所有样机的回波损耗参数和辐射方向图与仿真结果吻合较好。利用厚度为1.57 mm的Rogers 5880衬底进行了制备。在ANSYS HFSS电磁仿真平台上进行了设计和仿真分析,并通过ADS生成了Gerber文件进行制作。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Design and Development of a Vivaldi Antenna Array for Airborne X-Band Applications
In this paper, design analysis of an X-band Vivaldi antenna array for airborne active phased array radar application has been presented. Initially, a parametric study has been conducted to find out the relationship between design characteristics of a Vivaldi antenna array and its performance. Thereafter, a single Vivaldi antenna leading to 1×8 uniform linear array was designed to achieve optimal performance before proceeding to 8×8 antenna array design. Moreover, the tuning and optimization of designed antenna array have also been performed to achieve the desired results. The transition from stripline to slotline in the feeding section was adopted to adhere to the size restrictions of airborne radar system. The designed antenna array operates in X-Band with a center frequency of 10 GHz. It comprises an array of 64-elements (8×8) and achieves a 22 dB gain. The return loss (S11) is better than −10 dB in 2 GHz bandwidth (8.55 – 10.75 GHz). With a transmitted peak power of 640 W, the Azimuth and Elevation coverage is ±60° and beamwidth is 13°. The isolation between two elements is 20 dB and Side Lobe Levels (SLL) are −30 dBc. The designed single-element Vivaldi antenna and uniform linear 1×8 elements Vivaldi array antenna have been fabricated to develop 8×8 elements antenna array. The return loss parameter and radiation patterns of all prototypes have been found in good agreement with simulation results. Rogers 5880 substrate with 1.57 mm thickness has been utilized for fabrication. The design and simulations analysis have been performed in ANSYS HFSS EM simulation platform and Gerber files have been generated through ADS for fabrication.
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