• 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