DocumentCode :
3457552
Title :
The observation and simulation of the airplane flutter on low band television broadcasting signal
Author :
Wonggeeratigun, A. ; Sangonchat, P. ; Noppanakeepong, S. ; Leelaruji, N. ; Moriya, Y.
Author_Institution :
Fac. of Eng. & Res. Center for Commun. & Inf. Technol., King Mongkut´´s Inst. of Technol., Bangkok, Thailand
fYear :
2003
fDate :
25-26 Aug. 2003
Firstpage :
118
Lastpage :
122
Abstract :
The paper studies the effect of quasi-periodic or airplane flutter phenomenon on television broadcasting. Airplane flutter is a very important problem. It causes the receiving antenna to receive both direct signal by the Tx (transmitter antenna) and reflected signal scattered by the airplane with phase delay. The sum of two signals results in fading, sometime collapse and distortion of picture on TV screen. We performed measurement and modeling of this phenomenon on TV signal when the airplane flew across and the range Tx and Rx (receiver antenna). The 60.75 MHz frequency (aural frequency of CH3) is used under tests. A single scatter multipath model is introduced. It is used to duplicate some of the measured data and show the dependence of power variation on the airplane fluttering. The fluctuation of the airplane flutter phenomenon was calculated to be around 2-4 dB.
Keywords :
VHF antennas; receiving antennas; television broadcasting; television interference; transmitting antennas; 60.75 MHz; airplane flutter phenomenon; low band television broadcasting signal; phase delay; quasiperiodic phenomenon; receiver antenna; signal scattering; single scatter multipath model; television broadcasting; transmitter antenna; Airplanes; Antenna measurements; Delay; Frequency; Receiving antennas; Reflector antennas; Scattering; TV broadcasting; Transmitters; Transmitting antennas;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Research and Development, 2003. SCORED 2003. Proceedings. Student Conference on
Print_ISBN :
0-7803-8173-4
Type :
conf
DOI :
10.1109/SCORED.2003.1459677
Filename :
1459677
Link To Document :
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