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[an error occurred while processing this directive]Design of a Missile-borne Circularly Polarized Microstrip Antenna
Received date: 2009-10-26
Online published: 2025-05-28
常树茂 . 弹载圆极化微带天线设计[J]. 弹箭与制导学报, 2010 , 30(4) : 187 -189 . DOI: 10.15892/j.cnki.djzdxb.2010.04.060
The design of a missile-borne circularly polarized circular microstrip antenna was proposed. Theoretical analysis and simulation results with HFSS show that the antenna can achieve a maximal gain of 4. 7dBi and polarization axial ratio of 1. 1~3.3dB in the direction of ±60° scanning space. The results of the simulated and the antenna size were presented.
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