Title :
Electromagnetic coupling and interference predictions using the frequency-domain physical optics method and the time-domain finite-element method [aircraft antenna applications]
Author :
Riley, Douglas J. ; Riley, Norma W. ; Clark, Wally T., III ; Del Aguila, Hector ; Kipp, Robert
Author_Institution :
Northrop Grumman Corp., Albuquerque, NM, USA
Abstract :
Two predictive techniques, the frequency-domain physical optics (PO) method, and the time-domain finite-element (TD FE) method, are presented with application to system-level electromagnetic coupling and interference issues. Full-wave solvers, such as finite-element and integral-equation methods, are very powerful but have practical upper frequency limits of application. The physical optics method, which has traditionally been used for far-field scattering and antenna pattern predictions, is shown in this paper to be useful for estimating on-platform antenna coupling. Although PO methods do not provide the fidelity and accuracy of full-wave methods, they can nevertheless often provide useful coupling estimates for the entire platform in a matter of seconds, whereas full-wave methods may take many hours (or days) of computation time and often solve only a subset of the overall platform. The utility of PO methods is demonstrated in this paper through validation of antenna coupling on a Boeing F15B.
Keywords :
aircraft antennas; electromagnetic coupling; electromagnetic interference; finite element analysis; physical optics; time-domain analysis; FETD; PO methods; aircraft antennas; electromagnetic coupling; electromagnetic interference; frequency-domain physical optics method; on-platform antenna coupling; time-domain finite-element method; Aircraft; Electromagnetic coupling; Electromagnetic interference; Electromagnetic scattering; Finite element methods; Frequency; Iron; Optical scattering; Physical optics; Time domain analysis;
Conference_Titel :
Antennas and Propagation Society International Symposium, 2004. IEEE
Print_ISBN :
0-7803-8302-8
DOI :
10.1109/APS.2004.1329813