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
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