DocumentCode :
1992265
Title :
Parametric effects in not directed antennas, installed on the helicopter fuselage
Author :
Ivanov, V.A. ; Zadorozhniy, A.S.
Author_Institution :
Nat. Aviation Univ., Kiev, Ukraine
fYear :
2013
fDate :
16-20 Sept. 2013
Firstpage :
378
Lastpage :
380
Abstract :
The paper shows that the system "A Standard Omnidirectional Antenna - Metal Body of the Helicopter" becomes non-parametric system at rotation of main rotor. Under this condition the effective height of the antenna is the parametric factor. Distortions of the spectrum of radio signals on the input of the standard antenna are consequence of periodic changes of the effective antenna height. In the paper, the method of analysis of signal spectrum after parametrical distortions is developed, namely: quantitative estimation of attenuation of spectral components of useful signal and detection of combination frequencies of unwanted components-satellites. Spectral distortions of some types of modulated and manipulated signals on the output of parametrical antenna system are also considered.
Keywords :
aircraft antennas; distortion; omnidirectional antennas; parametric devices; rotors; signal detection; directed antennas; helicopter fuselage; nonparametric system; parametric effect; parametrical antenna system; parametrical distortion; radio signal spectrum distortion; rotor rotation; standard omnidirectional antenna; Antenna theory; Distortion; Equations; Frequency modulation; Helicopters; Metals; directivity diagram; effective length of the antenna; helicopter screw; parametric signal conversion; radio signal; spectrum; video impulses;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Antenna Theory and Techniques (ICATT), 2013 IX International Conference on
Conference_Location :
Odessa
Print_ISBN :
978-1-4799-2896-5
Type :
conf
DOI :
10.1109/ICATT.2013.6650784
Filename :
6650784
Link To Document :
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