用于卫星航空电子设备的模块化、可定制、适应友好型天线系统:开发、原型设计和验证

M. Saporetti, A. Giacomini, L. Foged, C. Occhiuzzi, L. Piazzon, P. Colantonio, G. Marrocco, G. Galagani, G. Scozza, M. Sabbadini
{"title":"用于卫星航空电子设备的模块化、可定制、适应友好型天线系统:开发、原型设计和验证","authors":"M. Saporetti, A. Giacomini, L. Foged, C. Occhiuzzi, L. Piazzon, P. Colantonio, G. Marrocco, G. Galagani, G. Scozza, M. Sabbadini","doi":"10.1109/METROAEROSPACE.2014.6865987","DOIUrl":null,"url":null,"abstract":"In the frame of ESA program AO/1-6737/11/NL/MH, an innovative X-band antenna system for satellite avionics has been studied, demonstrated and validated at Proof of Concept Model level. The innovative contribution of such an antenna system relies on modularity, customizability and accommodation friendliness. The antenna concept is based on a Plug and Play architecture, where the basic module is a 2.7 cm-cube with a mass of 53 gr, which can be clustered in array configuration. A catalogue of predefined and ready-to-use clusters could be developed with the possibility of adapting the antenna systems to various platform types by tuning just a few control parameters. Different levels of customization are, in fact, easily achievable reducing the qualification effort. The proposed antenna system has been prototyped and has been validated through two measurement campaigns, in standalone configuration and accommodated on a platform demonstrator having the shape of an ESA Proba V satellite. The whole antenna system has been also simulated with the commercial program ADF-EMS and a good agreement with measurements has been achieved, proving that the characteristics of such an antenna system can be very accurately predicted even in the most complex configurations. A comparison between the proposed solution and a more conventional space avionic radiator has been carried out: even though the EM performances are comparable, mass and encumbrance are instead extremely reduced in MCAS.","PeriodicalId":162403,"journal":{"name":"2014 IEEE Metrology for Aerospace (MetroAeroSpace)","volume":"411 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2014-05-29","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":"{\"title\":\"Modular, customisable, accomodation-friendly antenna system for satellite avionics: Development, prototyping and validation\",\"authors\":\"M. Saporetti, A. Giacomini, L. Foged, C. Occhiuzzi, L. Piazzon, P. Colantonio, G. Marrocco, G. Galagani, G. Scozza, M. Sabbadini\",\"doi\":\"10.1109/METROAEROSPACE.2014.6865987\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"In the frame of ESA program AO/1-6737/11/NL/MH, an innovative X-band antenna system for satellite avionics has been studied, demonstrated and validated at Proof of Concept Model level. The innovative contribution of such an antenna system relies on modularity, customizability and accommodation friendliness. The antenna concept is based on a Plug and Play architecture, where the basic module is a 2.7 cm-cube with a mass of 53 gr, which can be clustered in array configuration. A catalogue of predefined and ready-to-use clusters could be developed with the possibility of adapting the antenna systems to various platform types by tuning just a few control parameters. Different levels of customization are, in fact, easily achievable reducing the qualification effort. The proposed antenna system has been prototyped and has been validated through two measurement campaigns, in standalone configuration and accommodated on a platform demonstrator having the shape of an ESA Proba V satellite. The whole antenna system has been also simulated with the commercial program ADF-EMS and a good agreement with measurements has been achieved, proving that the characteristics of such an antenna system can be very accurately predicted even in the most complex configurations. A comparison between the proposed solution and a more conventional space avionic radiator has been carried out: even though the EM performances are comparable, mass and encumbrance are instead extremely reduced in MCAS.\",\"PeriodicalId\":162403,\"journal\":{\"name\":\"2014 IEEE Metrology for Aerospace (MetroAeroSpace)\",\"volume\":\"411 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2014-05-29\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"1\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2014 IEEE Metrology for Aerospace (MetroAeroSpace)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/METROAEROSPACE.2014.6865987\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2014 IEEE Metrology for Aerospace (MetroAeroSpace)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/METROAEROSPACE.2014.6865987","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 1

摘要

在欧空局AO/1-6737/11/NL/MH项目框架下,一种用于卫星航空电子设备的创新x波段天线系统在概念模型验证级别进行了研究、演示和验证。这种天线系统的创新贡献依赖于模块化,可定制性和住宿友好性。天线概念基于即插即用架构,其中基本模块是一个2.7厘米的立方体,质量为53克,可以集群成阵列配置。可以开发一个预定义的和随时可用的集群目录,通过调整几个控制参数使天线系统适应各种平台类型的可能性。实际上,不同级别的定制很容易实现,从而减少了认证工作。拟议的天线系统已经原型化,并通过两次测量活动进行了验证,在独立配置中,并容纳在具有欧空局Proba V卫星形状的平台演示器上。用商业程序ADF-EMS对整个天线系统进行了仿真,结果与实测结果吻合良好,证明即使在最复杂的配置下,也能非常准确地预测该天线系统的特性。提出的解决方案与更传统的空间航空电子散热器之间的比较已经进行了:即使电磁性能相当,质量和拖累在MCAS中反而大大减少。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Modular, customisable, accomodation-friendly antenna system for satellite avionics: Development, prototyping and validation
In the frame of ESA program AO/1-6737/11/NL/MH, an innovative X-band antenna system for satellite avionics has been studied, demonstrated and validated at Proof of Concept Model level. The innovative contribution of such an antenna system relies on modularity, customizability and accommodation friendliness. The antenna concept is based on a Plug and Play architecture, where the basic module is a 2.7 cm-cube with a mass of 53 gr, which can be clustered in array configuration. A catalogue of predefined and ready-to-use clusters could be developed with the possibility of adapting the antenna systems to various platform types by tuning just a few control parameters. Different levels of customization are, in fact, easily achievable reducing the qualification effort. The proposed antenna system has been prototyped and has been validated through two measurement campaigns, in standalone configuration and accommodated on a platform demonstrator having the shape of an ESA Proba V satellite. The whole antenna system has been also simulated with the commercial program ADF-EMS and a good agreement with measurements has been achieved, proving that the characteristics of such an antenna system can be very accurately predicted even in the most complex configurations. A comparison between the proposed solution and a more conventional space avionic radiator has been carried out: even though the EM performances are comparable, mass and encumbrance are instead extremely reduced in MCAS.
求助全文
通过发布文献求助,成功后即可免费获取论文全文。 去求助
来源期刊
自引率
0.00%
发文量
0
×
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
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
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 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:604180095
Book学术官方微信