Radio channel measurements and characterization inside aircrafts for in-cabin wireless networks

Moraitis, N; Constantinou, P

dc.contributor.author	Moraitis, N	en
dc.contributor.author	Constantinou, P	en
dc.date.accessioned	2014-03-01T02:45:45Z
dc.date.available	2014-03-01T02:45:45Z
dc.date.issued	2008	en
dc.identifier.issn	15502252	en
dc.identifier.uri	https://dspace.lib.ntua.gr/xmlui/handle/123456789/32372
dc.subject	Aircraft	en
dc.subject	In-cabin	en
dc.subject	Measurements	en
dc.subject	Wireless networks	en
dc.subject.other	Aircraft	en
dc.subject.other	Fading (radio)	en
dc.subject.other	Fading channels	en
dc.subject.other	Frequency bands	en
dc.subject.other	Image compression	en
dc.subject.other	Wireless networks	en
dc.subject.other	Airbus A340	en
dc.subject.other	Aircrafts	en
dc.subject.other	Coherence times	en
dc.subject.other	Different frequencies	en
dc.subject.other	Doppler spreads	en
dc.subject.other	Dynamic ranges	en
dc.subject.other	In-cabin	en
dc.subject.other	Path losses	en
dc.subject.other	Radio channel measurements	en
dc.subject.other	Reference levels	en
dc.subject.other	Cabins (aircraft)	en
dc.title	Radio channel measurements and characterization inside aircrafts for in-cabin wireless networks	en
heal.type	conferenceItem	en
heal.identifier.primary	10.1109/VETECF.2008.63	en
heal.identifier.secondary	http://dx.doi.org/10.1109/VETECF.2008.63	en
heal.identifier.secondary	4656895	en
heal.publicationDate	2008	en
heal.abstract	This paper presents a measurement campaign conducted inside a large Airbus A340-300 aircraft for the development of in-cabin wireless networks. The measurements were conducted in three different frequency bands in order to provide various services. It was found that the path loss factor along the aircraft corridors varies between 2.0 and 2.7 depending on frequency. The average K-factor in the aircraft aisles was found between 9.5 and 10.1 dB, for line-of-sight (LoS) conditions, and between 3.7 and 5.0 dB for non-line-of-sight (NLoS) cases. The average dynamic range of fading varies between 12 and 14 dB for LoS, and between 25 and 28 dB for NLoS situations respectively. The maximum Doppler spread was calculated between 15 and 17 Hz, whereas the coherence time was found between 25 and 29 ms for a reference level of -3 dB. ©2008 IEEE.	en
heal.journalName	IEEE Vehicular Technology Conference	en
dc.identifier.doi	10.1109/VETECF.2008.63	en