Aircraft structures can be modeled by using a composite prolate spheroid for a fuselage and multiple finite plates and bent plates for wings and stabilizers. It is observed that the structure closest to a source location has the dominant effect on the radiation pattern. The analysis for radiated fields is based on the Geometrical Theory of Diffraction (GTD) which is a high frequency solution.
Computer simulation technique for the determination of the best location of airborne antennas
Rechnersimulationsverfahren zur Bestimmung des zweckmaessigsten Aufstellungsortes von Flugzeugantennen
1984
4 Seiten, 21 Bilder, 3 Quellen
Aufsatz (Konferenz)
Englisch
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