# Design of Rhombus-Shaped Slot Patch Antenna for Wireless Communications

Authors: Manavalan Saravanan; Madihally Janardhana Srinivasa Rangachar
Journal: Journal of Computer Networks and Communications
 (2019)

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## Abstract

A single feed circularly polarized patch antenna is presented. The antenna consists of a rhombus-shaped slot incorporated in the radiating patch at its center. The antenna is designed to operate at 2.3 GHz band. The antenna achieves left-hand polarization or right-hand polarization based on the orientation of the slot in the radiating patch. The antenna parameters are synthesized using a high-frequency structure simulator and its characteristics are validated by the Agilent network analyzer (N9925A) and antenna test systems. The measured results obtained agree with simulated results and show that the antenna achieves −10 dB impedance bandwidth of 85 MHz (2.27 GHz–2.355 GHz) for left-hand polarization and 85 MHz (2.26 GHz–2.345 GHz) for right-hand polarization. The antenna gives a 3 dB axial ratio beamwidth of 95°(−35° ≤ AR ≤ 60°) for both left-hand polarization and right-hand polarization along with better 3 dB axial ratio bandwidth of 140° in the operating band. The antenna also achieves a good cross-polarization isolation of −17 dBic for both left-hand and right-hand polarization at its operating frequency. Hence, the antenna is best suited for modern wireless communication systems.


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## Body

## 1. Introduction

Compact circular polarized patch antennas play a vital role in satellite communications and airborne communication due to their low profile and lightweight. These antennas require low cross-polarization isolation in order to mitigate multipath interference and wider axial ratio beamwidth to provide a wide coverage area. However, 3 dB axial ratio beamwidth of the antenna suffers from a narrow beamwidth and cannot meet the required practical applications. A lot of researchers have been proposed to improve axial ratio beamwidth and to reduce cross-polarization isolation. One way of improving the beamwidth is to employ a 3D ground structure as in [1, 2]. These structures utilize a multilayer stacked structure which diffracts the electromagnetic waves from the ground plane, thereby altering the radiation pattern of the antenna. However, these structures increase the overall width of the antenna. In [3], the beamwidth of the antenna is improved by altering the spacing between the two crossed dipoles placed in a square-shaped contour. However, it results in a bidirectional radiation pattern and thus results in power loss in the undesired direction. Another way of improving the beamwidth is by exciting surface waves through substrates extended on the ground plane as given in [4]. This technique significantly produces backward radiations, thereby interfering with other circuit elements.A popular technique to improve the beamwidth is by introducing parasitic elements around the patch. However, the space required for these patch elements are higher and hence increases the overall length of the antenna [5]. A 3D circularly polarized patch is presented in [6]. The antenna uses a crossed slot in the radiating patch, and a triangular feed structure is made to improve the bandwidth of the antenna. Though the techniques discussed increase the axial ratio beamwidth of the antenna, the technique fails to suppress the cross-polarization isolation, especially at low elevation angles [7, 8]. One more technique to improve the beamwidth is by introducing lumped elements in the radiating patch. In [9], PIN diodes are placed along diagonals of the square patch, and the beamwidth is fully controlled by the shunt inductive load. The antenna uses the dual feed to excite two orthogonal modes. In [10, 11], a circularly polarized antenna with an improved axial ratio beamwidth is proved. However, it suffers from poor cross-polarization isolation. In [12], parasitic stubs are used to perturb the surface fields on the radiating patch to achieve circular polarization with an improved axial ratio beamwidth. Recently, a slot of appropriate shape is etched in the circular radiating patch is used to achieve circular polarization [13–15].In this paper, a rhombus-shaped slot patch antenna operating at 2.3 GHz band is presented. The antenna is fabricated on FR4 substrate, and its performance is measured using the Agilent network analyzer and antenna test systems. The measured results are compared with simulation results and show that the antenna is best suited for airborne wireless communication systems.


## 2. Geometry of Proposed Antenna

The geometry of the proposed antenna is illustrated in Figure1. The antenna is fabricated on fire retardant dielectric substrate (FR4) having a relative permittivity of εr = 4.4 and dielectric loss tangent of ζ = 0.02. In order to have low profile thickness, the substrate is chosen to have a thickness of 1.6 mm. A rhombus-shaped slot is etched in the radiating element in order to excite two orthogonal modes. This perturbs the surface current over the patch element, thereby generating circular polarization. The orientation of the slot determines the nature of polarization. The antenna is fed by 50 Ω SMA connector. A quarter wave transformer having an impedance of 50 Ω is used for impedance matching.Figure 1
Antenna geometry. (a) LHCP. (b) RHCP.
(a)
(b)


### 2.1. Surface Current Distribution

The surface current distribution over the radiating patch is simulated and is shown in Figure2. Figure 2(a) shows surface current distribution corresponding to left-hand circular polarization (LHCP). Here, surface current in the right half plane along X-axis perturbs near the corner of the slot in advance when compared to the left half plane. This adds a 90° phase delay in the surface current between both the half planes, which results in LHCP. Figure 2(b) shows surface current distribution corresponds to right-hand circularly polarization (RHCP). Here, surface current in the left half plane along X-axis perturbs near the corner of the slot in advance when compared to the right half plane. This adds a 90° phase delay in the surface current between both the half planes, which results in LHCP. Thus, based on the orientation of the slot, the antenna achieves either left-hand or right-hand polarization.Figure 2
Simulated surface current distribution. (a) LHCP. (b) RHCP.
(a)
(b)


## 2.1. Surface Current Distribution

The surface current distribution over the radiating patch is simulated and is shown in Figure2. Figure 2(a) shows surface current distribution corresponding to left-hand circular polarization (LHCP). Here, surface current in the right half plane along X-axis perturbs near the corner of the slot in advance when compared to the left half plane. This adds a 90° phase delay in the surface current between both the half planes, which results in LHCP. Figure 2(b) shows surface current distribution corresponds to right-hand circularly polarization (RHCP). Here, surface current in the left half plane along X-axis perturbs near the corner of the slot in advance when compared to the right half plane. This adds a 90° phase delay in the surface current between both the half planes, which results in LHCP. Thus, based on the orientation of the slot, the antenna achieves either left-hand or right-hand polarization.Figure 2
Simulated surface current distribution. (a) LHCP. (b) RHCP.
(a)
(b)


## 3. Antenna Design Considerations

A circular shape is considered as the basic antenna geometry shape for the proposed antenna model. Hence, the radius of the circular patch [16] is calculated from the following equation:(1)a=1.8412∗c2π∗fr∗εr,where a = radius of the patch (m), c = velocity of light in vacuum = 3 ∗ 108 m/s, fr = resonant frequency (GHz), and εr = relative permittivity  = 4.4 (no unit).The introduction of the slot in the radiating element increases the electrical length of the antenna and it shifts the operating frequency. Therefore, an offset length introduced in the radial length of the patch is needed and is given in the following equation:(2)R=a−0.0134∗λεr,where R = effective radius of the antenna.Since slot dimensions greatly affect the purity of polarization, the dimension of the slot has to be carefully chosen for the antenna to radiate circular polarization. The following equation gives optimal slot dimension of the proposed model:(3)L=R4.7,SlotX=2L,SlotY=32L.Table1 gives overall dimensions of the proposed antenna model operating at the 2.3 GHz band.Table 1
Antenna design specifications.
Parameters
Specifications
Operating frequency
2.3 GHz
R
17.39 mm
L
3.70 mm
Slot_X ∗ Slot_Y
5.23 mm ∗ 5.55 mm
Q_X ∗ Q_Y
12 mm ∗ 0.96 mm
Feed_X ∗ Feed_Y
8 mm ∗ 2.4 mm


## 4. Results and Discussions

To verify the feasibility of the presented circular polarized antenna, a prototype is fabricated on FR4 substrate having a thickness of 1.6 mm. A 50 Ω SMA connector is used to feed the model.In order to analyze the characteristics of the proposed antenna, the prototype is tested using the network analyzer N9924A as shown in Figure3, and its radiation characteristics are measured using the antenna test setup shown in Figure 4. A 50 Ω N-type adapter is used to couple the network analyzer with the model.Figure 3
Testing of antenna.Figure 4
Radiation pattern measurement setup.The impedance curve measured using a network analyzer is shown in Figure5 and is compared with simulation results. It is observed that the antenna resonates at 2.3 GHz band and achieves a −10 dB impedance bandwidth of 85 MHz (2.27 GHz–2.355 GHz) for left-hand polarization and 85 MHz (2.26 GHz–2.345 GHz) for right-hand polarization. In order to validate the radiation characteristics, the fabricated model is tested under the antenna test system. The measured radiation characteristics are compared with simulation results and are shown in Figure 6.Figure 5
Reflection coefficient (dB).Figure 6
Simulated and measured radiation pattern of (a) LHCP and (b) RHCP.
(a)
(b)A standard pyramidal horn antenna having a gain of 9 dB is used as a reference antenna. The distance between two antennas (R) is measured, and the gain is calculated using the Friis transmission equation given below:(4)PrPt=λ4πR2GtGr.Figure6(a) shows measured radiation characteristics corresponding to antenna geometry shown in Figures 1(a) and 6(b) and measured radiation characteristics corresponding to antenna geometry shown in Figure 1(b). The simulation results agree with measured results, and the antenna gives symmetrical radiation pattern around zenith. The antenna achieves a good cross-polarization isolation of −17 dBic for both LHCP and RHCP configurations at its operating frequency.Figure7 shows a variation of axial ratio against frequencies for both LHCP and RHCP configurations. It is observed from Figure 7 that the antenna gives minimum axial ratio at the 2.3 GHz operating frequency for both the configurations and achieves a measured wide 3 dB axial ratio bandwidth of 140 MHz in the operating band.Figure 7
Axial ratio vs. frequency.Figure8 shows measured E plane and H plane radiation characteristics of both LHCP and RHCP configurations. It is observed that the antenna achieves a good axial ratio (AR) over a wide beam angle ratio beamwidth of 95°(−35° ≤ AR ≤ 60°) for left-hand polarization and 95°(−35° ≤ AR ≤ 60°) for right-hand polarization. The measured gain is calculated using the gain comparison method. A standard pyramidal horn antenna having a gain of 9 dB is used as a reference antenna as shown in Figure 4. The distance between two antennas (R) is measured, and the gain is calculated using Friis transmission equation.Figure 8
Radiation pattern measured at the minimum axial ratio. (a) LHCP. (b) RHCP.
(a)
(b)The gain characteristics of the proposed antenna with respect to operating band are given in Figure9. It is observed that the antenna gives a nearly flat gain over the operating band. The measured gain for LHCP is 5.16 dBic and RHCP is 4.82 dBic at the boresight of the antenna. This small difference in gain results is due to fabrication loss and antenna alignment losses.Figure 9
Variation of frequency (GHz) with respect to gain (dB).Table2 gives performance comparison of proposed antenna with traditional antenna models. It is observed that the proposed model achieves better axial ratio bandwidth when compared to the traditional antenna model given in Table 2. Moreover, the cross-polarization isolation is better in the proposed antenna and is not studied in conventional antennas given in Table 2. In addition to this, the proposed antenna is simple and is modelled on the single layer instead of multilayer substrate as in Ref. [14], which makes it easy to integrate with other high-frequency circuits. Though the antenna has limitation of narrow 3 dB axial ratio bandwidth when compared to other traditional antennas, the 3 dB axial ratio beamwidth achieved by the proposed antenna is sufficient to cover one complete sector of a mobile cell network and also suitable for many wireless applications including MIMO application.Table 2
Performance comparison of the proposed model with the traditional antenna model.
Parameter
Ref. [12]
Ref. [13]
Ref. [14]
Ref. [15]
Proposed model
Reflection coefficient (dB)
−21 dB
−13 dB
−20 dB
−25 dB
−20.6 dB
Maximum gain (dB)
4.5 dB
5.3 dBic
6.8 dBic
6.1 dBic
5.16 dBic (LHCP)4.82 dBic (RHCP)
3 dB axial ratio bandwidth (dB)
55 MHz
40 MHz
100 MHz
40 MHz
140 MHz
3 dB axial ratio beamwidth (dB)
176°
140°
100°
180°
95°
Cross-polarization isolation (dB)
NA
NA
NA
NA
−17 dB


## 5. Conclusion

This paper introduces a novel circularly polarized patch antenna operating at 2.3 GHz. A rhombus-shaped slot is etched in radiating patch located at its center. The dimension of the slot is tuned to achieve minimum axial ratio at its operating frequency. The antenna radiates either left-hand or right-hand polarization based on the orientation of the slot. The measured radiation characteristics show that the proposed antenna attains 5.16 dBic for LHCP and 4.82 dBic for RHCP at the boresight of the antenna. The antenna achieves good cross-polarization isolation of −17 dBic and wider 3 dB axial ratio beamwidth of 95°(−35° ≤ AR ≤ 60°) for both left-hand polarization and right-hand polarization at operating frequency along with better 3 dB axial ratio bandwidth of 140° in the operating band which best suited for airborne communication.



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*Source: 5149529-2019-01-10.xml*