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Circularly polarized ACPW Fed CRLH-TL based ZOR antenna with band notch characteristics

Published online by Cambridge University Press:  26 November 2019

Kalyanbrata Ghosh
Affiliation:
Department of Electronics Engineering, Indian Institute of Technology (Indian School of Mines), Dhanbad, Jharkhand, India
Sushrut Das*
Affiliation:
Department of Electronics Engineering, Indian Institute of Technology (Indian School of Mines), Dhanbad, Jharkhand, India
*
Author for correspondence: Sushrut Das, E-mail: sushrut@iitism.ac.in
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Abstract

In this paper, two asymmetric co-planar waveguide (ACPW) fed circularly polarized (CP) zeroth-order resonance (ZOR) antennas (Antenna I and II) are presented using a composite right and left-handed transmission line (CRLH-TL) approach. By adding a stub on the left side of the ACPW ground and adjusting its length, circularly polarization property has been achieved in Antenna I. The simulated 3 dB axial ratio bandwidth (ARBW) of Antenna I is 1750 MHz (3.50–5.25 GHz). Next, the left side ground plane of Antenna I is further defected by etching a quarter wavelength slit to introduce a notch band (Antenna II). Antenna II has an extended 10 dB return loss bandwidth of 2200 MHz (3.28–5.48 GHz) with a band notch from 4.18–4.65 GHz that isolates the WiMAX and 5.2 GHz WLAN bands. ARBWs of 1080 and 870 MHz are achieved in the first and second band of Antenna II. The overlapping 3 dB ARBW and 10 dB return loss bandwidths of Antenna II in these two bands are 770 and 830 MHz, respectively.

Information

Type
Research Papers
Copyright
Copyright © Cambridge University Press and the European Microwave Association 2019
Figure 0

Fig. 1. Geometry of the proposed Antenna-I. L = 20, l1 = 18.15, l2 = 11.65, l3 = 10.15, l4 = 4.05, l5 = 6, l6 = 1.6, l7 = 5.45, W = 26, w1 = 10.5, w2 = 7, w3 = 1, w4 = 3, w5 = 2.6, w6 = 2, w7 = 11, k1 = 6.5, k2 = 3.5, g1 = 0.9, g2 = 0.5, g3 = 0.3, t1 = 0.2, s1 = 2.2, s2 = 2, s3 = 4.4, s4 = 1.8, s5 = 1, and s6 = 1.2 (unit: millimeters).

Figure 1

Fig. 2. Equivalent CRLH-TL.

Figure 2

Fig. 3. Comparison of simulated |S11| (dB) responses of the Antenna-I with different values of s1.

Figure 3

Fig. 4. (a) Vector field and (b) surface current density distribution on the antenna at 4.65 GHz.

Figure 4

Fig. 5. Dispersion diagram shows the ZOR property of the proposed antenna.

Figure 5

Fig. 6. |S11| (dB) responses of the Antenna-I with the variation of k1.

Figure 6

Fig. 7. AR response of the Antenna-I with the variation of k1.

Figure 7

Fig. 8. |S11| (dB) responses of the Antenna-I with the variation of k2.

Figure 8

Fig. 9. AR response of the Antenna-I with the variation of k2.

Figure 9

Fig. 10. Vectored surface current distribution on the antenna with an unloaded ground stub at 4.65 GHz at ωt = 0°, 90°, 180°, and 270°.

Figure 10

Fig. 11. Vectored surface current distribution on the antenna with a ground stub at 4.65 GHz at ωt = 0°, 90°, 180°, and 270°.

Figure 11

Fig. 12. Ex/Ey ratio of the radiated field of the antenna with and without the ground stub (a) amplitude ratio and (b) phase difference.

Figure 12

Fig. 13. Photograph of the fabricated prototype I.

Figure 13

Fig. 14. Simulated and measured |S11| of the Antenna-I.

Figure 14

Fig. 15. Simulated and measured AR of the Antenna-I.

Figure 15

Fig. 16. Simulated and measured peak realized gain and simulated radiation efficiency of the proposed Antenna-I.

Figure 16

Fig. 17. Simulated and measured normalized RHCP and LHCP patterns (a) xz-plane and (b) yz-plane at 4.65 GHz.

Figure 17

Fig. 18. Structure of the proposed Antenna II: L = 20, l1 = 18.15, l2 = 11.65, l3 = 10.15, l4 = 4.05, l5 = 6, l6 = 1.6, l7 = 5.45, l8 = 7.6, W = 26, w1 = 10.5, w2 = 7, w3 = 1, w4 = 3, w5 = 2.6, w6 = 2, w7 = 11, g1 = 0.9, g2 = 0.5, g3 = 0.3, g4 = 0.5, t1 = 0.2, s1 = 2.2, s2 = 2, s3 = 4.4, s4 = 1.8, s5 = 1, and s6 = 1.2 (unit: millimeters).

Figure 18

Fig. 19. Photograph of the fabricated prototype II.

Figure 19

Fig. 20. Simulated and measured input reflection coefficient of Antenna II.

Figure 20

Fig. 21. Surface current (magnitude) distribution at 4.45 GHz.

Figure 21

Fig. 22. Input reflection coefficient of Antenna-II with the variation of l8.

Figure 22

Fig. 23. Simulated and measured axial ratio of Antenna-II.

Figure 23

Fig. 24. Simulated and measured peak realized gain and simulated radiation efficiency of the proposed Antenna-II.

Figure 24

Fig. 25. Simulated and measured normalized RHCP and LHCP patterns of the Antenna-II in xz- and yz-planes at (a) 3.7 GHz and (b) 5.1 GHz.

Figure 25

Table 1. Comparison of Antenna-I and Antenna-II with some previously reported CP antennas