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首页> 外文期刊>Microwave and optical technology letters >MEASUREMENT AND MODELING OF MULTIUSER MULTIANTENNA SYSTEM IN AIRCRAFT IN THE PRESENCE OF ELECTROMAGNETIC NOISE AND INTERFERENCE
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MEASUREMENT AND MODELING OF MULTIUSER MULTIANTENNA SYSTEM IN AIRCRAFT IN THE PRESENCE OF ELECTROMAGNETIC NOISE AND INTERFERENCE

机译:电磁噪声和干扰作用下飞机多用户多天线系统的测量与建模

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This article evaluates the accuracy with which the performance of a multiuser multiantenna system can be predicted with and without considering cochannel interference and noise (Gaussian, astable, and Cauchy) using a site-specific three-dimensional (3D) ray tracing algorithm as well as with statistical models with Gaussian and Nakagami-m channel models in small to medium sized aircraft. These models expand on previous statistical channel models such as the hyper-Rayleigh model by including the simultaneous effects of cochannel and adjacent channel interference, antenna matching, efficiency, directivity and polarization as well as (for the 3D model) site-specific multipath effects. Measurements and comparisons are made in a metallic-bodied Beech Baron BE 58P and a composite structure Rockwell T-39 Sabreliner. It was found that the 3D ray tracing model provides a mean capacity within 1% of those measured in the two aircraft in the presence of interference and noise. This was closely followed by the Nakagami-m distribution (m = 1.4), which was within 1-3% of measured capacity in the presence of interference and within 6% for a combination of interference and noise and the Gaussian model which was within 6% of measured capacity in the presence of interference and within 11% for a combination of interference and noise. The Cauchy noise degraded the capacity more than the other types of noise in the aircraft, providing a lower bound for capacity in an aircraft system.
机译:本文使用特定于站点的三维(3D)射线跟踪算法评估了在不考虑同信道干扰和噪声(高斯,非稳态和柯西)的情况下预测多用户多天线系统性能的准确性,以及在中小型飞机上使用高斯和Nakagami-m通道模型的统计模型。这些模型通过包含同信道和相邻信道干扰,天线匹配,效率,方向性和极化以及(针对3D模型)特定于站点的多径效应的同时影响,扩展了诸如Hyper-Rayleigh模型之类的先前统计信道模型。在金属车身的Beech Baron BE 58P和复合结构的Rockwell T-39 Sabreliner中进行测量和比较。已经发现,在存在干扰和噪声的情况下,3D射线追踪模型提供的平均容量不到两架飞机所测得的平均容量的1%。 Nakagami-m分布(m = 1.4)紧随其后,在存在干扰的情况下,该值在测量容量的1-3%之内,而在干扰和噪声的组合以及高斯模型的情况下,该值在6%以内(在6以内)在存在干扰的情况下,测量容量的百分比;对于干扰和噪声,则为11%以内。柯西噪声比飞机上其他类型的噪声更严重地降低了容量,从而为飞机系统的容量提供了下限。

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