An easy-to-produce HIS-based MIMO radio altimeter antenna design for aircraft

IF 1.3 4区 工程技术 Q3 ENGINEERING, AEROSPACE Aircraft Engineering and Aerospace Technology Pub Date : 2023-11-28 DOI:10.1108/aeat-02-2023-0034
Serap Kiriş, Muharrem Karaaslan
{"title":"An easy-to-produce HIS-based MIMO radio altimeter antenna design for aircraft","authors":"Serap Kiriş, Muharrem Karaaslan","doi":"10.1108/aeat-02-2023-0034","DOIUrl":null,"url":null,"abstract":"<h3>Purpose</h3>\n<p>The purpose of this study is to design a radio altimeter antenna whose production process is facilitated and can work with multiple-input multiple-output (MIMO) properties to provide space gain on the aircraft.</p><!--/ Abstract__block -->\n<h3>Design/methodology/approach</h3>\n<p>To create an easy-to-produce MIMO, a two-storied structure consisting of a reflector and a top antenna was designed. The dimensions of the reflector were prevented to get smaller to supply easy production. The unit cell nearly with the same dimensions of a lower frequency was protected through the original cell design. The co-planar structure with the use of a via connection was modified and a structure was achieved with no need to via for easy production, too. Finally, the antennas were placed side by side and the distance between them was optimized to achieve a MIMO operation.</p><!--/ Abstract__block -->\n<h3>Findings</h3>\n<p>As a result, an easy-to-produce, compact and successful radio altimeter antenna was obtained with high antenna parameters such as 10.14 dBi gain and 10.55 dBi directivity, and the conical pattern along with proper MIMO features, through original reflector surface and top antenna system.</p><!--/ Abstract__block -->\n<h3>Originality/value</h3>\n<p>Since radio altimeter antennas require high radiation properties, the microstrip antenna structure is generally used in literature. This paper contributes by presenting the radio altimeter application with antenna-reflective structure participation. The technical solutions were developed during the design, focusing on an easy manufacturing process for both the reflective surface and the upper antenna. Also, the combination of International Telecommunication Union’s recommended features that require high antenna properties was achieved, which is challenging to reach. In addition, by operating the antenna as a successful MIMO, two goals of easy production and space gain on aircraft have been attained at the same time.</p><!--/ Abstract__block -->","PeriodicalId":55540,"journal":{"name":"Aircraft Engineering and Aerospace Technology","volume":"59 2","pages":""},"PeriodicalIF":1.3000,"publicationDate":"2023-11-28","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Aircraft Engineering and Aerospace Technology","FirstCategoryId":"5","ListUrlMain":"https://doi.org/10.1108/aeat-02-2023-0034","RegionNum":4,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q3","JCRName":"ENGINEERING, AEROSPACE","Score":null,"Total":0}
引用次数: 0

Abstract

Purpose

The purpose of this study is to design a radio altimeter antenna whose production process is facilitated and can work with multiple-input multiple-output (MIMO) properties to provide space gain on the aircraft.

Design/methodology/approach

To create an easy-to-produce MIMO, a two-storied structure consisting of a reflector and a top antenna was designed. The dimensions of the reflector were prevented to get smaller to supply easy production. The unit cell nearly with the same dimensions of a lower frequency was protected through the original cell design. The co-planar structure with the use of a via connection was modified and a structure was achieved with no need to via for easy production, too. Finally, the antennas were placed side by side and the distance between them was optimized to achieve a MIMO operation.

Findings

As a result, an easy-to-produce, compact and successful radio altimeter antenna was obtained with high antenna parameters such as 10.14 dBi gain and 10.55 dBi directivity, and the conical pattern along with proper MIMO features, through original reflector surface and top antenna system.

Originality/value

Since radio altimeter antennas require high radiation properties, the microstrip antenna structure is generally used in literature. This paper contributes by presenting the radio altimeter application with antenna-reflective structure participation. The technical solutions were developed during the design, focusing on an easy manufacturing process for both the reflective surface and the upper antenna. Also, the combination of International Telecommunication Union’s recommended features that require high antenna properties was achieved, which is challenging to reach. In addition, by operating the antenna as a successful MIMO, two goals of easy production and space gain on aircraft have been attained at the same time.

查看原文
分享 分享
微信好友 朋友圈 QQ好友 复制链接
本刊更多论文
一种易于生产的基于his的MIMO无线电高度计天线设计
本研究的目的是设计一种无线电高度计天线,其生产过程方便,可以使用多输入多输出(MIMO)特性,为飞机提供空间增益。设计/方法/方法为了创建一个易于生产的MIMO,设计了一个由反射器和顶部天线组成的两层结构。为了便于生产,防止反射镜的尺寸变小。原电池设计保护了几乎具有相同尺寸的低频率单元电池。改进了使用过孔连接的共面结构,实现了不需要过孔的结构,也便于生产。最后,将天线并排放置,并优化天线之间的距离,实现MIMO操作。结果表明,通过原反射面和顶部天线系统,获得了易于制作、结构紧凑、具有10.14 dBi增益和10.55 dBi指向性的高天线参数,以及具有适当MIMO特性的锥形方向图。由于无线电测高仪天线对辐射性能要求较高,文献中一般采用微带天线结构。本文介绍了天线反射结构参与的无线电高度计的应用。技术解决方案是在设计过程中开发的,重点是反射表面和上部天线的简单制造过程。此外,还实现了国际电信联盟推荐的需要高天线性能的功能组合,这是具有挑战性的。此外,通过将天线作为一个成功的MIMO操作,同时达到了易于生产和在飞机上获得空间的两个目标。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 去求助
来源期刊
Aircraft Engineering and Aerospace Technology
Aircraft Engineering and Aerospace Technology 工程技术-工程:宇航
CiteScore
3.20
自引率
13.30%
发文量
168
审稿时长
8 months
期刊介绍: Aircraft Engineering and Aerospace Technology provides a broad coverage of the materials and techniques employed in the aircraft and aerospace industry. Its international perspectives allow readers to keep up to date with current thinking and developments in critical areas such as coping with increasingly overcrowded airways, the development of new materials, recent breakthroughs in navigation technology - and more.
期刊最新文献
Wind tunnel investigation of hemispherical forebody interaction on the drag coefficient of a D-shaped model Parameter tuning for active disturbance rejection control of fixed-wing UAV based on improved bald eagle search algorithm Integrating urban air mobility into smart cities: a proposal for relevant use cases in the next decades Heavy fuel preparation effects on the operation of a spark ignition unmanned aerial vehicle engine Flame stabilization and emission reduction: a comprehensive study on the influence of swirl velocity in hydrogen fuel-based burner design
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
现在去查看 取消
×
提示
确定
0
微信
客服QQ
Book学术公众号 扫码关注我们
反馈
×
意见反馈
请填写您的意见或建议
请填写您的手机或邮箱
已复制链接
已复制链接
快去分享给好友吧!
我知道了
×
扫码分享
扫码分享
Book学术官方微信
Book学术文献互助
Book学术文献互助群
群 号:604180095
Book学术
文献互助 智能选刊 最新文献 互助须知 联系我们:info@booksci.cn
Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。
Copyright © 2023 Book学术 All rights reserved.
ghs 京公网安备 11010802042870号 京ICP备2023020795号-1