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首页> 外文期刊>IEEE Transactions on Vehicular Technology >Air-Ground Channel Characterization for Unmanned Aircraft Systems—Part IV: Airframe Shadowing
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Air-Ground Channel Characterization for Unmanned Aircraft Systems—Part IV: Airframe Shadowing

机译:无人飞机系统的空地通道特征-第四部分:机身阴影

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摘要

Applications of unmanned aircraft systems (UAS) are expected to expand dramatically in the coming decades. In order to provide safe and reliable links for UAS, NASA Glenn Research Center sponsored a measurement campaign in 2013 to characterize air-ground (AG) channels. In the first three of our AG channel characterization series papers, path loss, small scale fading, stationarity distance, root mean square (RMS) delay spread, spatial correlations, and tapped delay line models were presented for a range of ground site environment. In this paper, we expand the results to a unique and little-studied characteristic of the AG channels-airframe shadowing-for a medium-sized aircraft. Airframe shadowing occurs when the line-of-sight signal is obstructed by the airplane itself in some specific maneuvers. Based on over 200 aircraft wing/engine shadowing events in both C-band (5060 MHz) and L-band (968 MHz) collected in the measurement campaign, shadowing depth, duration, multiple antenna diversity gain, and small scale fading results and their statistics are reported. Algorithms are proposed to simulate a random shadowing event based upon shadowing depth and duration cumulative density functions. Airframe shadowing characteristics are independent of the local ground site conditions and link distance. The shadowing loss is modeled as a function of aircraft roll angle, but shadowing loss and duration are essentially uncorrelated. The maximum shadowing loss measured was over 35 dB and the duration was up to 74 s. As expected, deployment of multiple aircraft antennas is shown helpful to mitigate this shadowing.
机译:预计在未来几十年中,无人机系统(UAS)的应用将大大扩展。为了为UAS提供安全可靠的链接,美国国家航空航天局格伦研究中心在2013年发起了一项测量活动,以表征空地(AG)通道。在我们的AG信道表征系列的前三篇论文中,针对一系列地面站点环境,介绍了路径损耗,小尺度衰落,平稳距离,均方根(RMS)延迟扩展,空间相关性和抽头延迟线模型。在本文中,我们将结果扩展到中型飞机的AG通道(机身阴影)的独特且研究较少的特征。当在某些特定的操作中飞机自身遮挡了视线信号时,就会出现机体阴影。根据测量活动中收集到的200多个C波段(5060 MHz)和L波段(968 MHz)的飞机机翼/发动机遮挡事件,遮挡深度,持续时间,多天线分集增益和小规模衰落结果及其统计数据已报告。提出了基于阴影深度和持续时间累积密度函数来模拟随机阴影事件的算法。机身遮蔽特性与当地地面状况和链路距离无关。遮蔽损失被建模为飞机侧倾角的函数,但是遮蔽损失和持续时间本质上是不相关的。测得的最大阴影损失超过35 dB,持续时间长达74 s。不出所料,部署多个飞机天线有助于减轻这种阴影。

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