DocumentCode
1560187
Title
A reciprocity approach for calculating the far-field radiation patterns of a center-fed helical microstrip antenna mounted on a dielectric-coated circular cylinder
Author
Martin, Rodney A. ; Werner, Douglas H.
Author_Institution
Dept. of Electr. Eng., Pennsylvania State Univ., University Park, PA, USA
Volume
49
Issue
12
fYear
2001
fDate
12/1/2001 12:00:00 AM
Firstpage
1754
Lastpage
1762
Abstract
This paper presents an efficient approach based on reciprocity for calculating the far-field radiation pattern of a center-fed helical microstrip antenna mounted on a circular cylinder. The reciprocity theorem is used to find a completely analytical solution to the problem assuming that the helical microstrip is sufficiently thin with a sinusoidal current distribution. Two degenerate cases of the helical microstrip antenna, i.e., an axially and an azimuthally fed half-wave cylindrical-rectangular patch, are examined and compared to known results in order to provide validation for the general analytical solution. Further comparisons are made between the analytical results and the results obtained using a numerically rigorous method of moments (MoM) computer code
Keywords
antenna feeds; antenna radiation patterns; conformal antennas; current distribution; helical antennas; integral equations; microstrip antennas; MoM computer code; analytical solution; axially fed half-wave patch; azimuthally fed half-wave patch; center-fed helical microstrip antenna; conformal antennas; cylindrical-rectangular patch; dielectric-coated circular cylinder; far-field radiation pattern; far-field radiation patterns; helical microstrip; integral equations; method of moments; reciprocity theorem; Antenna radiation patterns; Current distribution; Dielectrics; Engine cylinders; Equations; Geometry; Helical antennas; Microstrip antennas; Moment methods; Pattern analysis;
fLanguage
English
Journal_Title
Antennas and Propagation, IEEE Transactions on
Publisher
ieee
ISSN
0018-926X
Type
jour
DOI
10.1109/8.982456
Filename
982456
Link To Document