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A hybrid UTD-MM analysis of the radiation from a composite slot-blade cavity-backed antenna on realistic aircraft configurations

机译:混合UTD-MM分析现实飞机配置中复合式缝隙式叶片背腔天线的辐射

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摘要

A hybrid method which combines the uniform geometrical theory of diffraction (UTD) with a numerical moment method (MM) technique is presented for the analysis of the radiation from a composite slot-blade cavity-backed antenna located on realistic aircraft configurations. The excitation of the antenna is due to a delta gap generator in a thin-wire probe feed that is placed inside a rectangular cavity. The MM procedure is used to solve coupled integral equations that are formulated for the unknown equivalent electric current distribution on the blade and the unknown equivalent magnetic current distribution over the slot, when this slot-blade antenna configuration resides on an infinite ground plane. The UTD is next used to efficiently and accurately calculate the radiation from these equivalent current distributions for the slot-blade antenna combination when the latter are now located on realistic aircraft geometries instead of a flat ground plane. Calculated radiation patterns of the composite slot-blade cavity-backed antennas placed on a Boeing 737 commercial airplane and an F-16 fighter aircraft are presented to illustrate the utility of this hybrid approach.
机译:提出了一种混合方法,该方法结合了统一的衍射几何理论(UTD)和数值矩量法(MM)技术,用于分析位于实际飞机配置上的复合缝隙叶片背腔天线的辐射。天线的激励归因于位于矩形空腔内的细线探针馈源中的增量间隙发生器。 MM过程用于求解耦合积分方程,当该缝隙叶片天线配置位于无限接地平面时,该方程式针对叶片上的未知等效电流分布和狭缝上的未知等效磁电流分布制定。接下来,当缝隙刀片天线组合位于实际的飞机几何形状而不是平坦的地面上时,接下来将使用UTD来根据这些等效电流分布为缝隙刀片天线组合有效且准确地计算辐射。介绍了放置在波音737商用飞机和F-16战斗机上的复合缝隙叶片背腔天线的计算辐射方向图,以说明这种混合方法的实用性。

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