Aircraft harness measurement campaign and investigations on introducing one pair Ethernet
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In this paper, the results of a measurement campaign on the data harness of an A321 aircraft will be presented. The S-parameters of the cabin harnesses of an existing system are illustrated, and these parameters will be used to model a cabin architecture based on the existing harnesses. This A321 aircraft, where the measurements were performed, is a 20-year-old aircraft; hence possible cable aging will be discussed. The currently used aeronautical-certified cables show a great potential on introducing new technologies to the aircraft cabin, driven from the automotive industry (like 100BASE-T1 or 1000BASE-T1), thus increasing the available bandwidth by a factor of up to 500 times compared with the existing systems, without increasing the most important factor for aircrafts, weight.
[1] Fabien Geyer,et al. Comparison of IEEE AVB and AFDX , 2012, 2012 IEEE/AIAA 31st Digital Avionics Systems Conference (DASC).
[2] Emanuel Heidinger. Performance Bounds in Switched Ethernet Onboard Networks , 2013 .
[3] Kerstin Siebert. Entwicklung von Mehrleitermodellen für Signalintegritäts- und EMV-Analysen von Kfz-Bussystemen , 2013 .