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

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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 http://hdl.handle.net/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

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