Aircraft Coupling Model Evaluations at SHF/EHF

G. Genello, A. Pesta
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引用次数: 1

Abstract

Severe overcrowding of t h e RF spect rum, e s p e c i a l l y a t UHF, has been one pr imary m o t iv a t o r to extend m i l i t a r y communications i n t o t h e SHF and f i n a l l y th e EHF band. The p o t e n t i a l i n t e r f e r e n c e of p l a c ­ ing new SHF/EHF te r m i n a l s on-board e x i s t i n g and new a i r c r a f t p la t f o r m s i s unknown and must be ass es se d . Several EMC-related computer a n a l y s i s programs a re a v a i l a b l e t o p r e d i c t th e coupl ing be­ tween a i r c r a f t an tennas . However, th e models con­ t a i n e d i n t h e s e codes may no t be adequa te f o r p re ­ d i c t i o n a n a l y s i s a t t h e s e h igher f r e q u e n c i e s . Coupling measurements have been performed on a KC135 s t y l e a i r c r a f t and a F-16 t a c t i c a l f i g h t e r to e v a l u a t e t h e v a l i d i t y of th e computer models. A comparison a n a l y s i s of p r e d i c te d and ac tua l coup­ l i n g d a t a i s p re se n te d .
超高频/超高频下飞机耦合模型评估
超高频(UHF)射频频谱的严重拥挤问题,一直是将移动通信扩展到甚高频(SHF)和超高频(EHF)频段的主要原因。新的 SHF/EHF 车载电子 x i s t i n g 和新的 a i r c r a f t p la t f o r m s 的 p o t e r f e r i a l i n c e尚不清楚,必须加以确定。一些与电磁兼容性相关的计算机程序可用于检测天线之间的耦合。然而,这些代码中的模型可能无法满足更高功率的耦合要求。在 KC135 s t y l e a i r c r a f t 和 F-16 t a c t i c a l f i g h t e r 上进行了耦合测量,以评估计算机模型的性能。在此基础上,比较了计算机模型与实际数据的差异。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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