Interference Path Loss Measurements of Beechcraft B300 Aircraft at 4 GHz Wireless Avionics Intra-Communication Band

S. Futatsumori, Nxorihiko Miyazaki, T. Hikage, T. Sekiguchi, M. Yamamoto, T. Nojima
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引用次数: 2

Abstract

Wireless Avionics Intra-Communication (WAIC) devices operate between 4,200 MHz and 4,400 MHz. This is the same frequency band as aircraft radio altimeters. In this paper, to investigate the coexistence conditions, the radio altimeter interference path loss (IPL) due to an assumed WAIC device is investigated. Firstly, an overview of the Beechcraft B300, a medium sized turboprop aircraft, is given. Then, the radio altimeter IPL measurement set-up is discussed. The measurement set-up and procedures are based on the RTCA DO-307A procedure. Finally, the IPL values are calculated using the measurement results. The minimum IPL value with the transmitting antenna inside of the cabin is 72.8 dB. This is not significantly small compared with that of the Airbus A321 (74.4 dB). In addition, the median IPL value with the transmitting antenna inside of the cabin is 90.9 dB.
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比奇B300飞机在4ghz无线航电内通信频段的干扰路径损耗测量
无线航空电子内部通信(WAIC)设备在4,200 MHz和4,400 MHz之间工作。这与飞机无线电高度表的频率相同。为了研究这种共存条件,本文研究了假设的WAIC器件对无线电高度计干扰路径损耗的影响。首先,对中型涡桨飞机比奇B300进行了概述。然后,讨论了射电高度计IPL测量装置。测量设置和程序基于RTCA DO-307A程序。最后,根据测量结果计算出IPL值。发射天线在舱内时,最小IPL值为72.8 dB。这与空客A321 (74.4 dB)相比并不算小。此外,在舱内安装发射天线时,IPL中值为90.9 dB。
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