• DocumentCode
    2761864
  • Title

    Path loss from a personal electronic device inside an aircraft cabin to an exterior fuselage-mounted antenna

  • Author

    Hurst, K.W. ; Ellingson, S.W.

  • Author_Institution
    Bradley Dept. of Electr. & Comput. Eng., Virginia Polytech. Inst. & State Univ., Blacksburg, VA
  • fYear
    2008
  • fDate
    5-11 July 2008
  • Firstpage
    1
  • Lastpage
    4
  • Abstract
    In this paper we consider the problem of how to determine path loss from a personal electronic device (PED) radiating in the cabin of a large passenger aircraft to the terminals of a ldquovictimrdquo antenna mounted on the fuselage. The ability to perform such calculations quickly and accurately is important in the analysis of electromagnetic compatibility (EMC) between PEDs and aircraft navigation and communications systems. Solutions for this problem using full-wave integral equation methods or ray tracing methods is awkward due to the large dimensions of the fuselage relative to the wavelengths of interest (as small as 6 mm) and the fact that the cabin consists of a complex collection of objects including people and seats. Prior investigations have mostly bypassed this problem by focussing on the path loss measured from the point at which power leaves the fuselage to the victim antenna. However, lossy materials within the cabin play an important role in determining the overall path loss. Therefore, it is desirable that any new analysis technique yield reasonable estimates in the presence of interior features, but at the same time should not require detailed information about the specific geometries or constitutive parameters of the media. Section 2 of this paper presents our solution to this problem, which involves a combination of techniques including microwave cavity theory for the interior part of the problem and the uniform geometrical theory of diffraction (UTD) for the exterior part of the problem. In Section 3, we demonstrate the effectiveness of the technique by comparison to measurements of various aircraft at the L1 (1575.42 MHz) frequency of the U.S. Global Positioning System (GPS).
  • Keywords
    UHF antennas; aircraft antennas; aircraft communication; geometrical theory of diffraction; integral equations; ray tracing; GPS; U.S. Global Positioning System; aircraft cabin; aircraft navigation; communications systems; electromagnetic compatibility analysis; exterior fuselage-mounted antenna; frequency 1575.42 MHz; full-wave integral equation methods; microwave cavity theory; path loss; personal electronic device; ray tracing methods; uniform geometrical theory of diffraction; victim antenna; Aerospace electronics; Aircraft navigation; Antenna measurements; Communication systems; Electromagnetic analysis; Electromagnetic compatibility; Global Positioning System; Integral equations; Performance analysis; Ray tracing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Antennas and Propagation Society International Symposium, 2008. AP-S 2008. IEEE
  • Conference_Location
    San Diego, CA
  • Print_ISBN
    978-1-4244-2041-4
  • Electronic_ISBN
    978-1-4244-2042-1
  • Type

    conf

  • DOI
    10.1109/APS.2008.4619021
  • Filename
    4619021