# Minimized Low-Profile Wideband Antennas Using High Impedance Surface

Authors: Yizhu Shen
Journal: International Journal of Antennas and Propagation
 (2017)

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## Abstract

This paper proposes minimized low-profile wideband antenna by employing high impedance surface (HIS), for wireless application scenarios at radio frequency, microwave, and even terahertz. To validate this concept with low cost and easy measurement, two prototypes at radio frequency are fabricated and tested. Firstly, antenna with dielectric-substrate reflector is proposed and analyzed and 4 × 6 HIS array is employed to minimize the antenna size to0.57λL×0.86λL×0.078λL, while maintaining antenna performances such as bandwidth, gain, and directive radiation. Secondly, a substrate-less HIS is proposed to improve the antenna bandwidth from 36% to 52% and also reduces the antenna weight by 72%.


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## Body

## 1. Introduction

Antenna with low-profile and high directive gain has been widely researched, and the demand in practical applications is increasing [1, 2]. Generally, there are two methods to realize it. One way is to add electromagnetic absorber in the backside cavity of antenna [3, 4]. However, this will reduce the efficiency of the antenna, and there is a tradeoff among the cavity thickness, bandwidth, and the antenna gain. The other common approach is employing the metallic ground as a reflector [5, 6]. Nevertheless, because the reflection of metallic ground is out-of-phase, a separation gap about quarter-wavelength between the antenna and the reflector is required, to generate the constructive interference between the incident and reflected waves. This quarter-wavelength gap results in two problems, that is, narrow bandwidth and bulky size. To alleviate these problems, electromagnetic bandgap (EBG) structure, which is also known as metamaterial, photonic bandgap (PBG), or hard/soft surfaces, is proposed by changing the surface characteristics on the ground [7–10].Among these EBG structures, high impedance surface (HIS) has demonstrated many advantages in low-profile antenna designs. It was invented by Sievenpiper et al. in [1], to emulate a perfect magnetic conductor (PMC). Compared to conventional perfect electric conductor (PEC), PMC generates an in-phase reflection phase response, which enables locating the antenna closer to the reflector ground. It is worth mentioning that HIS only achieves the pure in-phase response at the resonant frequency, while its phase response decreases from 180° to −180° with increased frequencies. Therefore, the pseudo-PMC effect of HIS is defined as bandgap range of 0° ± 90°.Using HIS as a reflector, a lot of low-profile antennas have been reported [11–16]. A planar folded dipole on via-less dog bone-shaped HIS array is presented in [11], achieving a measured impedance bandwidth of 6% and a boresight gain of 6.4 dBi. A planar antenna with extremely low profile (λ0/74) is proposed in [12], but it is narrowband (<1%) resonant only at a single frequency. By inserting via only at reflector edges, while the center part is via-less, a hybrid HIS is proposed in [13], which significantly alleviates antenna beam distortion and reduces side lobe level. Low-profile bowtie antennas are published in [14–16] with wide bandwidth and small physical thickness. However, the electrical thickness is still large.This paper presents HIS based antennas with minimized electrical size and low profile as well as wide bandwidth and directive radiation patterns. Firstly, a dielectric-substrate HIS is employed as the ground reflector of a bow tie antenna, and the effect of the reflector size to the antenna performance is investigated. In this way, a minimized ground reflector is realized. Secondly, to improve the bandwidth, an air-gap HIS is designed without bulky dielectric substrate.This paper is organized as follows. Section2 introduces the operating principle of low-profile bow tie antenna on top of a dielectric-substrate HIS array. The minimization of HIS ground size and its effect to the antenna performance are analyzed. In the following, Section 3 presents a compact antenna design based on substrate-less HIS. Section 4 describes the measurement verifications of these two designs and also compares the proposed methods with other state-of-the-art designs. Finally, Section 5 concludes this paper.


## 2. Antenna with Dielectric-Substrate HIS

### 2.1. Dielectric-Substrate HIS

HIS is a class of periodic structure, of which the cell size is much smaller than one wavelength. Many forms of periodic structures were studied in detail for its surface wave guiding abilities between 1950s and 1960s.As shown in Figure1(a), the HIS structure invented by Sievenpiper et al. [1] is in the form of grounded top-hat, that is, a common flat metallic ground at the bottom and periodical metallic patches on the top. They are connected to each other with vertical metal via. The operating principle of HIS can be explained using an equivalent parallel LC filter: the capacitance is introduced by the gap between two adjacent patches, and the inductance is generated in the loop which goes through vias between the two patches. Therefore, their analytical formula can be derived and listed as follows [1]:(1)C=wε0εr1+εr2πcosh-1ag,L=μ0h,where a, g, w, and h are width/thickness marked in Figure 1(a), ε0 and μ0 are the free-space permittivity and permeability, respectively, and εr1 and εr2 are the relative dielectric constant of materials surrounded at two sides of HIS top patches. The resonant frequency, surface input impedance, and bandwidth can be derived from this parallel LC filter as follows [1]:(2)fc=12πLC,(3)Zs=jωL//1jωC=jωL1-ω2LC,(4)B.W.=Δωω0=L/Cη.Figure 1
The proposed HIS structure: (a) HIS cross-sectional view, (b) the unit cell, (c) proposed 6 × 6 HIS array, and (d) reflection phase response.
(a)
(b)
(c)
(d)Based on this, the HIS unit cell proposed in this paper is shown in Figure1(b). It is based on air and Teflon substrate (εr1=1 and εr2=2.1). Brass square patches with a thickness of h1=0.5 mm and aluminum with a thickness h2=6 mm are located on the top and bottom layers, respectively. M10 metallic screws with diameter r=10 mm are used as shorting vias.Figure1(d) shows the HIS reflection phase response, derived from the full-wave analysis of the unit cell with periodic boundary conditions. By fixing h1, h2 and r, the other three key parameters (w, g, and h) are studied. As summarized in Table 1, when the HIS patch width w increases, the bandgap becomes narrower and the resonant frequency shifts to lower frequency. On the contrary, when the patch gap g increases, the bandgap becomes wider and the resonant frequency shifts to higher frequency. Additionally, thicker substrate h results in larger bandwidth, whereas the resonant frequency shifts to lower band. Therefore, after a tradeoff consideration, the HIS parameters are chosen as the second row in Table 1: w=70 mm, g=10 mm, and h=30 mm, to achieve an antenna with minimized size as well as large bandwidth.Table 1
Parameter study of HIS unit cell.
HIS(unit: mm)
Bandgap(0±90°)
Bandwidth
Resonant frequency
w = 70, g = 10, h = 30
(0.56–0.83) GHz
39%
0.68 GHz
w = 60, g=10, h=30
(0.59–0.92) GHz
44%
0.74 GHz
w = 80, g=10, h=30
(0.52–0.75) GHz
36%
0.625 GHz
w
=
70, g = 6, h=30
(0.50–0.72) GHz
36%
0.6 GHz
w
=
70, g = 13, h=30
(0.58–0.88) GHz
41%
0.715 GHz
w
=
70, g=10, h = 20
(0.71–0.97) GHz
31%
0.83 GHz
w
=
70, g=10, h = 40
(0.45–0.71) GHz
45%
0.57 GHzMeanwhile, employing (1)-(2), the theoretical equivalent circuit model of the HIS is calculated asC = 1.75 pF,L = 37.7 nH, andfc = 0.62 GHz, which is slightly lower than wave-full simulated 0.68 GHz. It is mainly because some parameters such ash1,h2, andrare considered as ideal in the theoretical analysis. Finally, employing the unit cell, a 6 × 6 HIS array is formed in Figure 1(c), with overall size of 480 × 480 × 36.5 mm3.


### 2.2. Wideband Bowtie Antenna

A bow tie antenna in free space is designed to cover the wide bandgap of the above-mentioned HIS. As shown in Figure2(a), the two bow tie arms are etched on top of a FR-4 substrate, with dielectric constant of 4.4 and thickness of 1.6 mm. The length and width of the bow tie antenna are 221.5 mm and 130 mm, respectively. There is no ground at the bottom side of FR-4.Figure 2
The bow tie antenna: (a) bow tie arms, (b) balun, (c)S11 curves, and (d) input impedance.
(a)
(b)
(c)
(d)To feed the differential bow tie antenna, a balun is designed as shown in Figure2(b). This balun is etched on double sides of a FR-4 substrate. It transfers from 50 Ω microstrip (line width of 3 mm) to stripline (line width of 2 mm). The balun has a total length of 54 mm and vertically feeds the two bowtie arms.As shown in Figure2(c), the 10 dB return-loss bandwidth of this bow tie antenna in free space is 0.42–0.79 GHz, with the input impedance shown in Figure 2(d).In the following, the 6 × 6 HIS array in Section2.1 is employed as the ground reflector of this bow tie antenna, as shown in Figure 3(a). The cross-sectional view in Figure 3(b) shows that there is no metal ground in the bow tie antenna in Figure 2(a); it thus can be directly located on top of the M10 screw head with height of 5.5 mm. In addition, a hole is excavated in the center part of both Teflon substrate and ground, to insert the balun to vertically feed the bowtie antenna.Figure 3
Low-profile bow tie antenna: (a) 3D view and (b) cross-sectional view.
(a)
(b)S
11 curves of this bow tie antenna with 6 × 6 HIS array are shown in Figure 2(c), and the HIS unit cell bandgap derived in Figure 1 is also given in Figure 2(c). Compared to bow tie in free space, the proposed antenna with HIS reflector covers 0.52–0.795 GHz or 42% referred to the center frequency of 0.658 GHz. The impact of HIS is highlighted by the HIS bandgap. The working bandwidth shifts slightly to the lower frequency due to the mutual coupling between bow tie and reflector, and the bandgap strongly affects the matching bandwidth of antenna. The proposed antenna features a physical size of 480 × 480 × 43.6 mm3, that is, a very small electrical size of 0.83λL×0.83λL×0.076λL (wherefL = 0.52 GHz).In addition, the simulated radiation patterns ofE-plane (z-x) and H-plane (z-y) at four selected frequency points are given in Figures 4(a) and 4(b). Directive radiation patterns are observed with maximum radiation about 7.6 dBi in the +z direction (θ = 0°), and the surface wave is highly suppressed in the x-y plane (when θ = ±90°).Figure 4
The radiation patterns of the bow tie antenna on 6 × 6 HIS array: (a)E-plane (z-x) and (b) H-plane (z-y).
(a)
(b)


### 2.3. HIS Reflector Minimization

Figure5 plots the surface current distribution on this 6 × 6 HIS array. It is observed that the current is mainly concentrated in the center area of the reflector, instead of spreading to the edges, showing that the surface wave propagation is highly suppressed by HIS. Additionally, there is little current distribution at the two utmost edges in the ±y direction, meaning that the characteristics and effect of HIS are not obvious at these areas. Therefore, these two edges can be removed, and the minimization to a 4 × 6 array becomes feasible. However, further reduction to 4 × 5 or 4 × 4 array is not practicable, since the current is strong at two utmost edges in the ±x direction especially in Figures 5(b) and 5(c). The above analysis indicates that the HIS reflector of this proposed antenna can be minimized to 4 × 6 array.Figure 5
The simulated surface current distribution on 6 × 6 HIS array: (a) 0.55 GHz, (b) 0.60 GHz, (c) 0.65 GHz, and (d) 0.70 GHz.
(a)
(b)
(c)
(d)To validate the above prediction, HIS effect on antenna performance is investigated. The only varying parameter is the cell number of HIS reflector, that is, 6 × 6, 5 × 6, 4 × 6, 4 × 5, and 4 × 4 arrays as listed in Figures6 and 7. The following phenomena are observed.Figure 6
The effect of HIS array size to the antenna: (a) impedance matching and (b) gain.
(a)
(b)Figure 7
Effect of HIS array size to the radiation patterns onE(z-x) and H(z-y) planes at four frequency points: 0.55 GHz, 0.60 GHz, 0.65 GHz, and 0.70 GHz.
(a)
0.55 GHz (E-plane)
(b)
0.60 GHz (E-plane)
(c)
0.65 GHz (E-plane)
(d)
0.70 GHz (E-plane)
(e)
0.55 GHz (H-plane)
(f)
0.60 GHz (H-plane)
(g)
0.65 GHz (H-plane)
(h)
0.70 GHz (H-plane)(
1
) When the reflector size is reduced from 6 × 6 to 5 × 6 and further to 4 × 6, the impedance bandwidth becomes wider as shown in Figure 6(a), and the highest operating frequency shifts from 0.795 GHz to 0.84 GHz. In Figure 6(b), antenna gain within 0.52–0.75 GHz slightly decreases due to the smaller reflector ground. Nevertheless, this reduction results in higher gain above 0.75 GHz due to the improved impedance matching. Additionally, both of the E- and H-plane radiation patterns in Figure 7 remain the same in the directive radiation and increase slightly in the back radiation (when θ = 180°) with reduced reflector.(
2
) When the reflector is further reduced to 4 × 5 or 4 × 4, it deteriorates the antenna impedance matching as shown in Figure 6(a), because the number of HIS arrays is too small to support the multiple resonances generated by the bow tie antenna as shown in Figure 5. It incurs a sharp drop in antenna gain above 0.65 GHz; additionally, this reduction will seriously affect the radiation patterns as illustrated in Figure 7. The HIS surface wave suppression ability becomes worse, as radiation becomes stronger at θ = ±90° in the E-plane; the backside radiation also increases in both E- and H-planes. Even worse, at higher operating frequency, the radiation pattern appears to have split up as in Figures 7(d) and 7(h), the maximum radiation is no longer in the +z direction (when θ = 0°) but changed to two peaks radiation at θ = ±40° for 4 × 5 and θ = ±60° for 4 × 4 array, respectively. This phenomenon is well explained in [17]. Meanwhile, as indicated in Figure 7, the impact of reflector size to the antenna cross-polarization radiation is not obvious, which is at least more than 20 dB for most of the above cases.In summary, the above analysis agrees well with the prediction from current distribution; that is, the HIS can be minimized to 4 × 6 array (or0.55λL×0.83λL×0.076λL referred tofL = 0.52 GHz), without affecting the antenna performances such as bandwidth, gain, and directive radiation.


## 2.1. Dielectric-Substrate HIS

HIS is a class of periodic structure, of which the cell size is much smaller than one wavelength. Many forms of periodic structures were studied in detail for its surface wave guiding abilities between 1950s and 1960s.As shown in Figure1(a), the HIS structure invented by Sievenpiper et al. [1] is in the form of grounded top-hat, that is, a common flat metallic ground at the bottom and periodical metallic patches on the top. They are connected to each other with vertical metal via. The operating principle of HIS can be explained using an equivalent parallel LC filter: the capacitance is introduced by the gap between two adjacent patches, and the inductance is generated in the loop which goes through vias between the two patches. Therefore, their analytical formula can be derived and listed as follows [1]:(1)C=wε0εr1+εr2πcosh-1ag,L=μ0h,where a, g, w, and h are width/thickness marked in Figure 1(a), ε0 and μ0 are the free-space permittivity and permeability, respectively, and εr1 and εr2 are the relative dielectric constant of materials surrounded at two sides of HIS top patches. The resonant frequency, surface input impedance, and bandwidth can be derived from this parallel LC filter as follows [1]:(2)fc=12πLC,(3)Zs=jωL//1jωC=jωL1-ω2LC,(4)B.W.=Δωω0=L/Cη.Figure 1
The proposed HIS structure: (a) HIS cross-sectional view, (b) the unit cell, (c) proposed 6 × 6 HIS array, and (d) reflection phase response.
(a)
(b)
(c)
(d)Based on this, the HIS unit cell proposed in this paper is shown in Figure1(b). It is based on air and Teflon substrate (εr1=1 and εr2=2.1). Brass square patches with a thickness of h1=0.5 mm and aluminum with a thickness h2=6 mm are located on the top and bottom layers, respectively. M10 metallic screws with diameter r=10 mm are used as shorting vias.Figure1(d) shows the HIS reflection phase response, derived from the full-wave analysis of the unit cell with periodic boundary conditions. By fixing h1, h2 and r, the other three key parameters (w, g, and h) are studied. As summarized in Table 1, when the HIS patch width w increases, the bandgap becomes narrower and the resonant frequency shifts to lower frequency. On the contrary, when the patch gap g increases, the bandgap becomes wider and the resonant frequency shifts to higher frequency. Additionally, thicker substrate h results in larger bandwidth, whereas the resonant frequency shifts to lower band. Therefore, after a tradeoff consideration, the HIS parameters are chosen as the second row in Table 1: w=70 mm, g=10 mm, and h=30 mm, to achieve an antenna with minimized size as well as large bandwidth.Table 1
Parameter study of HIS unit cell.
HIS(unit: mm)
Bandgap(0±90°)
Bandwidth
Resonant frequency
w = 70, g = 10, h = 30
(0.56–0.83) GHz
39%
0.68 GHz
w = 60, g=10, h=30
(0.59–0.92) GHz
44%
0.74 GHz
w = 80, g=10, h=30
(0.52–0.75) GHz
36%
0.625 GHz
w
=
70, g = 6, h=30
(0.50–0.72) GHz
36%
0.6 GHz
w
=
70, g = 13, h=30
(0.58–0.88) GHz
41%
0.715 GHz
w
=
70, g=10, h = 20
(0.71–0.97) GHz
31%
0.83 GHz
w
=
70, g=10, h = 40
(0.45–0.71) GHz
45%
0.57 GHzMeanwhile, employing (1)-(2), the theoretical equivalent circuit model of the HIS is calculated asC = 1.75 pF,L = 37.7 nH, andfc = 0.62 GHz, which is slightly lower than wave-full simulated 0.68 GHz. It is mainly because some parameters such ash1,h2, andrare considered as ideal in the theoretical analysis. Finally, employing the unit cell, a 6 × 6 HIS array is formed in Figure 1(c), with overall size of 480 × 480 × 36.5 mm3.


## 2.2. Wideband Bowtie Antenna

A bow tie antenna in free space is designed to cover the wide bandgap of the above-mentioned HIS. As shown in Figure2(a), the two bow tie arms are etched on top of a FR-4 substrate, with dielectric constant of 4.4 and thickness of 1.6 mm. The length and width of the bow tie antenna are 221.5 mm and 130 mm, respectively. There is no ground at the bottom side of FR-4.Figure 2
The bow tie antenna: (a) bow tie arms, (b) balun, (c)S11 curves, and (d) input impedance.
(a)
(b)
(c)
(d)To feed the differential bow tie antenna, a balun is designed as shown in Figure2(b). This balun is etched on double sides of a FR-4 substrate. It transfers from 50 Ω microstrip (line width of 3 mm) to stripline (line width of 2 mm). The balun has a total length of 54 mm and vertically feeds the two bowtie arms.As shown in Figure2(c), the 10 dB return-loss bandwidth of this bow tie antenna in free space is 0.42–0.79 GHz, with the input impedance shown in Figure 2(d).In the following, the 6 × 6 HIS array in Section2.1 is employed as the ground reflector of this bow tie antenna, as shown in Figure 3(a). The cross-sectional view in Figure 3(b) shows that there is no metal ground in the bow tie antenna in Figure 2(a); it thus can be directly located on top of the M10 screw head with height of 5.5 mm. In addition, a hole is excavated in the center part of both Teflon substrate and ground, to insert the balun to vertically feed the bowtie antenna.Figure 3
Low-profile bow tie antenna: (a) 3D view and (b) cross-sectional view.
(a)
(b)S
11 curves of this bow tie antenna with 6 × 6 HIS array are shown in Figure 2(c), and the HIS unit cell bandgap derived in Figure 1 is also given in Figure 2(c). Compared to bow tie in free space, the proposed antenna with HIS reflector covers 0.52–0.795 GHz or 42% referred to the center frequency of 0.658 GHz. The impact of HIS is highlighted by the HIS bandgap. The working bandwidth shifts slightly to the lower frequency due to the mutual coupling between bow tie and reflector, and the bandgap strongly affects the matching bandwidth of antenna. The proposed antenna features a physical size of 480 × 480 × 43.6 mm3, that is, a very small electrical size of 0.83λL×0.83λL×0.076λL (wherefL = 0.52 GHz).In addition, the simulated radiation patterns ofE-plane (z-x) and H-plane (z-y) at four selected frequency points are given in Figures 4(a) and 4(b). Directive radiation patterns are observed with maximum radiation about 7.6 dBi in the +z direction (θ = 0°), and the surface wave is highly suppressed in the x-y plane (when θ = ±90°).Figure 4
The radiation patterns of the bow tie antenna on 6 × 6 HIS array: (a)E-plane (z-x) and (b) H-plane (z-y).
(a)
(b)


## 2.3. HIS Reflector Minimization

Figure5 plots the surface current distribution on this 6 × 6 HIS array. It is observed that the current is mainly concentrated in the center area of the reflector, instead of spreading to the edges, showing that the surface wave propagation is highly suppressed by HIS. Additionally, there is little current distribution at the two utmost edges in the ±y direction, meaning that the characteristics and effect of HIS are not obvious at these areas. Therefore, these two edges can be removed, and the minimization to a 4 × 6 array becomes feasible. However, further reduction to 4 × 5 or 4 × 4 array is not practicable, since the current is strong at two utmost edges in the ±x direction especially in Figures 5(b) and 5(c). The above analysis indicates that the HIS reflector of this proposed antenna can be minimized to 4 × 6 array.Figure 5
The simulated surface current distribution on 6 × 6 HIS array: (a) 0.55 GHz, (b) 0.60 GHz, (c) 0.65 GHz, and (d) 0.70 GHz.
(a)
(b)
(c)
(d)To validate the above prediction, HIS effect on antenna performance is investigated. The only varying parameter is the cell number of HIS reflector, that is, 6 × 6, 5 × 6, 4 × 6, 4 × 5, and 4 × 4 arrays as listed in Figures6 and 7. The following phenomena are observed.Figure 6
The effect of HIS array size to the antenna: (a) impedance matching and (b) gain.
(a)
(b)Figure 7
Effect of HIS array size to the radiation patterns onE(z-x) and H(z-y) planes at four frequency points: 0.55 GHz, 0.60 GHz, 0.65 GHz, and 0.70 GHz.
(a)
0.55 GHz (E-plane)
(b)
0.60 GHz (E-plane)
(c)
0.65 GHz (E-plane)
(d)
0.70 GHz (E-plane)
(e)
0.55 GHz (H-plane)
(f)
0.60 GHz (H-plane)
(g)
0.65 GHz (H-plane)
(h)
0.70 GHz (H-plane)(
1
) When the reflector size is reduced from 6 × 6 to 5 × 6 and further to 4 × 6, the impedance bandwidth becomes wider as shown in Figure 6(a), and the highest operating frequency shifts from 0.795 GHz to 0.84 GHz. In Figure 6(b), antenna gain within 0.52–0.75 GHz slightly decreases due to the smaller reflector ground. Nevertheless, this reduction results in higher gain above 0.75 GHz due to the improved impedance matching. Additionally, both of the E- and H-plane radiation patterns in Figure 7 remain the same in the directive radiation and increase slightly in the back radiation (when θ = 180°) with reduced reflector.(
2
) When the reflector is further reduced to 4 × 5 or 4 × 4, it deteriorates the antenna impedance matching as shown in Figure 6(a), because the number of HIS arrays is too small to support the multiple resonances generated by the bow tie antenna as shown in Figure 5. It incurs a sharp drop in antenna gain above 0.65 GHz; additionally, this reduction will seriously affect the radiation patterns as illustrated in Figure 7. The HIS surface wave suppression ability becomes worse, as radiation becomes stronger at θ = ±90° in the E-plane; the backside radiation also increases in both E- and H-planes. Even worse, at higher operating frequency, the radiation pattern appears to have split up as in Figures 7(d) and 7(h), the maximum radiation is no longer in the +z direction (when θ = 0°) but changed to two peaks radiation at θ = ±40° for 4 × 5 and θ = ±60° for 4 × 4 array, respectively. This phenomenon is well explained in [17]. Meanwhile, as indicated in Figure 7, the impact of reflector size to the antenna cross-polarization radiation is not obvious, which is at least more than 20 dB for most of the above cases.In summary, the above analysis agrees well with the prediction from current distribution; that is, the HIS can be minimized to 4 × 6 array (or0.55λL×0.83λL×0.076λL referred tofL = 0.52 GHz), without affecting the antenna performances such as bandwidth, gain, and directive radiation.


## 3. Wideband Substrate-Less HIS

The above Section2 shows antenna with minimized size, whereas the bandwidth can be further improved. From (1) and (4), the HIS bandwidth can be improved either by increasingL or decreasingC; however, to maintain the low-profile characteristics, air-gap HIS (εr1 =εr2 = 1) is investigated in this section.As shown in Figure8(a), the unit cell is formed by air gap without any dielectric substrate like Teflon; that is, it is substrate-less. As compared in Figure 8(b), when the HIS substrate is changed from Teflon to air while keeping all other parameters, the resonant frequency shifts to higher frequency, and the bandgap becomes wider. Therefore, the following steps are carried on to update the HIS unit cell structure. Firstly, the HIS shorting via is changed from M10 screw tor = 7 mm, while keeping the same height (h = 30 mm), as well as maintaining the frequency response. Secondly, to shift down the resonant frequency, following the trend summarized in Table 1, the HIS patch width is increased tow = 80 mm, and the gap between two adjacent patches reduces to g=5 mm, respectively. The reflection response of substrate-less HIS is then almost equal to the substrate one as shown in Figure 8(b).Figure 8
The low-profile bow tie antenna on substrate-less HIS: (a) substrate-less HIS unit cell, (b) reflection phase response, (c) 3D view, and (d) cross-sectional view.
(a)
(b)
(c)
(d)This 4 × 6 air-gap HIS array is employed as the reflector, with 3D view in Figure8(c). In cross-sectional view in Figure 8(d), the antenna is located on top of spacer head with heighth3 = 2.2 mm. Other parameters keep the same as in Section 2, that is, top HIS brass patches withh1 = 0.5 mm and aluminum ground withh2 = 6 mm. Finally, the overall size of this antenna is 340 × 510 × 40.3 mm3. Simulated results are compared with measurement curves in Section 4.


## 4. Measurement Results and Discussions

Based on the above analysis, both of the antennas on substrate and substrate-less HIS are fabricated and shown in Figure9. In Figure 9(a), the 6 × 6 HIS array is assembled by two parts: the center part of 4 × 6 array and two 1 × 6 rows added at two edges. Therefore, both of the two antennas with 6 × 6 and 4 × 6 HIS reflectors can be measured. In Figure 9(b), nylon spacers are added in assembly at four corners of each brass patches to ensure the flatness.Figure 9
The fabricated prototype of low-profile bow tie antennas: (a) with dielectric-substrate HIS and (b) with substrate-less HIS.
(a)
(b)


### 4.1. Bowtie Antenna with Dielectric-Substrate HIS

Figure10 shows the simulated and measured results of the bow tie antennas with 6 × 6 and 4 × 6 HIS arrays. For the case of 6 × 6 array, the simulated 10 dB return-loss bandwidth is 0.52–0.79 GHz or a fractional bandwidth of 41%, whereas the measured one is slightly narrower, about 33% of 0.55–0.77 GHz. On the other hand, the antenna with a minimized 4 × 6 array has wider impedance bandwidth, up to 47% of 0.52–0.84 GHz in simulation and 36% of 0.54–0.78 GHz in measurement. The measured center frequency of both antennas is at 0.66 GHz. Correspondingly, based on measured results, the overall electrical sizes are 0.88λL×0.88λL×0.079λL (wherefL = 0.55 GHz, 480 × 480 × 43.1 mm3) for the 6 × 6 array and 0.57λL×0.86λL×0.078λL (wherefL = 0.54 GHz, 320 × 480 × 43.1 mm3) for the 4 × 6 array, respectively.Figure 10
The simulated and measured results of the antenna in Figure9(a): (a) return loss and (b) antenna gain.
(a)
(b)The antenna gain is plotted in Figure10(b), the antenna gain of the 6 × 6 array is higher than that of the 4 × 6 array, because of the larger reflector size. The maximum antenna gain is 5.6 dBi for the 6 × 6 array and 5.1 dBi for the 4 × 6 array.Because of the setup limitation in our anechoic chamber, only the front side (θ = 0° ± 90°) can be measured. Figures 11 and 12 present the normalized radiation patterns in both E-(z-x) and H-(z-y) planes. Good agreement is achieved between simulated and measured copolarization results. Generally, the measured cross-polarization value is slightly higher than the simulated ones, but also with at least 22 dB for both of the 6 × 6 and 4 × 6 array. Additionally, in Figure 12, although the reflector is minimized to 4 × 6, it does not affect the radiation patterns, that is, directive patterns with maximum radiation at θ = 0°. This measurement verifies the analysis as discussed in Section 2.3.Figure 11
The simulated and measured normalized radiation patterns of the antenna in Figure9(a) with 6 × 6 HIS array: (a) 0.55 GHz, (b) 0.60 GHz, (c) 0.65 GHz, and (d) 0.70 GHz.
(a)
(b)
(c)
(d)Figure 12
The simulated and measured normalized radiation patterns of the antenna in Figure9(a) with 4 × 6 HIS array: (a) 0.55 GHz, (b) 0.60 GHz, (c) 0.65 GHz, and (d) 0.70 GHz.
(a)
(b)
(c)
(d)


### 4.2. Bow Tie Antenna with Substrate-Less HIS

For the substrate-less antenna prototype in Figure9(b), as shown in Figure 13(a), the simulated S11 is 0.5–0.9 GHz, or 57% to the center frequency of 0.7 GHz, while the measured one is 0.5–0.85 GHz, about 52% to the center frequency at 0.675 GHz. Compared to antennas in Section 4.1, it is with wider bandwidth.Figure 13
The simulated and measured results of the antenna in Figure9(b): (a) return loss and (b) antenna gain.
(a)
(b)The antenna gain is shown in Figure13(b). The measured gain is slightly lower than the simulated one, and it varies from 3.7 dBi to 6 dBi covering the entire operation band. Figure 14 shows the normalized radiation patterns at four frequencies, that is, 0.55 GHz, 0.65 GHz, 0.75 GHz, and 0.85 GHz. The directive copolarization radiation is observed in both of the simulated and measured results, and the maximum radiation is atθ= 0°. It also achieves more than 20 dB cross-polarization, with measured E-plane results agreeing well with simulation while H-plane result is higher than simulation. The performances of the proposed and other reported bow tie antennas on HIS are summarized and compared in Table 2.Table 2
Performance summary and comparison of HIS antennas.
Substrate
Ground size
Thickness
Max gain
Bandwidth
This work
Antenna on 4 × 6 substrate-less HIS
Air-gap
0.57
λ
L
×
0.85
λ
L
0.067
λ
L
6.0 dBi
(0.5–0.85) GHz 52%
Antenna on 4 × 6 dielectric-substrate HIS
Teflon
0.57
λ
L
×
0.86
λ
L
0.078
λ
L
5.1 dBi
(0.54–0.78) GHz 36%
[13]
RT/duroid 5880
0.86
λ
L
×
0.86
λ
L
0.067
λ
L
8.7 dBi
(4.3–5) GHz 15%
[14]
RT/duroid 5880
1.25
λ
L
×
1.25
λ
L
0.06
λ
L
6.0 dBi
(1.06–1.5) GHz 34%
[15]
FR4
1.24
λ
L
×
1.24
λ
L
0.05
λ
L
9.4 dBi
(3.2–5) GHz 44%
[16]
RT/duroid 5880
0.67
λ
L
×
0.84
λ
L
0.102
λ
L
6.9 dBi
(2–3.2) GHz 46%Figure 14
The simulated and measured normalized radiation patterns of the antenna in Figure9(b): (a) 0.55 GHz, (b) 0.65 GHz, (c) 0.75 GHz, and (d) 0.85 GHz.
(a)
(b)
(c)
(d)


## 4.1. Bowtie Antenna with Dielectric-Substrate HIS

Figure10 shows the simulated and measured results of the bow tie antennas with 6 × 6 and 4 × 6 HIS arrays. For the case of 6 × 6 array, the simulated 10 dB return-loss bandwidth is 0.52–0.79 GHz or a fractional bandwidth of 41%, whereas the measured one is slightly narrower, about 33% of 0.55–0.77 GHz. On the other hand, the antenna with a minimized 4 × 6 array has wider impedance bandwidth, up to 47% of 0.52–0.84 GHz in simulation and 36% of 0.54–0.78 GHz in measurement. The measured center frequency of both antennas is at 0.66 GHz. Correspondingly, based on measured results, the overall electrical sizes are 0.88λL×0.88λL×0.079λL (wherefL = 0.55 GHz, 480 × 480 × 43.1 mm3) for the 6 × 6 array and 0.57λL×0.86λL×0.078λL (wherefL = 0.54 GHz, 320 × 480 × 43.1 mm3) for the 4 × 6 array, respectively.Figure 10
The simulated and measured results of the antenna in Figure9(a): (a) return loss and (b) antenna gain.
(a)
(b)The antenna gain is plotted in Figure10(b), the antenna gain of the 6 × 6 array is higher than that of the 4 × 6 array, because of the larger reflector size. The maximum antenna gain is 5.6 dBi for the 6 × 6 array and 5.1 dBi for the 4 × 6 array.Because of the setup limitation in our anechoic chamber, only the front side (θ = 0° ± 90°) can be measured. Figures 11 and 12 present the normalized radiation patterns in both E-(z-x) and H-(z-y) planes. Good agreement is achieved between simulated and measured copolarization results. Generally, the measured cross-polarization value is slightly higher than the simulated ones, but also with at least 22 dB for both of the 6 × 6 and 4 × 6 array. Additionally, in Figure 12, although the reflector is minimized to 4 × 6, it does not affect the radiation patterns, that is, directive patterns with maximum radiation at θ = 0°. This measurement verifies the analysis as discussed in Section 2.3.Figure 11
The simulated and measured normalized radiation patterns of the antenna in Figure9(a) with 6 × 6 HIS array: (a) 0.55 GHz, (b) 0.60 GHz, (c) 0.65 GHz, and (d) 0.70 GHz.
(a)
(b)
(c)
(d)Figure 12
The simulated and measured normalized radiation patterns of the antenna in Figure9(a) with 4 × 6 HIS array: (a) 0.55 GHz, (b) 0.60 GHz, (c) 0.65 GHz, and (d) 0.70 GHz.
(a)
(b)
(c)
(d)


## 4.2. Bow Tie Antenna with Substrate-Less HIS

For the substrate-less antenna prototype in Figure9(b), as shown in Figure 13(a), the simulated S11 is 0.5–0.9 GHz, or 57% to the center frequency of 0.7 GHz, while the measured one is 0.5–0.85 GHz, about 52% to the center frequency at 0.675 GHz. Compared to antennas in Section 4.1, it is with wider bandwidth.Figure 13
The simulated and measured results of the antenna in Figure9(b): (a) return loss and (b) antenna gain.
(a)
(b)The antenna gain is shown in Figure13(b). The measured gain is slightly lower than the simulated one, and it varies from 3.7 dBi to 6 dBi covering the entire operation band. Figure 14 shows the normalized radiation patterns at four frequencies, that is, 0.55 GHz, 0.65 GHz, 0.75 GHz, and 0.85 GHz. The directive copolarization radiation is observed in both of the simulated and measured results, and the maximum radiation is atθ= 0°. It also achieves more than 20 dB cross-polarization, with measured E-plane results agreeing well with simulation while H-plane result is higher than simulation. The performances of the proposed and other reported bow tie antennas on HIS are summarized and compared in Table 2.Table 2
Performance summary and comparison of HIS antennas.
Substrate
Ground size
Thickness
Max gain
Bandwidth
This work
Antenna on 4 × 6 substrate-less HIS
Air-gap
0.57
λ
L
×
0.85
λ
L
0.067
λ
L
6.0 dBi
(0.5–0.85) GHz 52%
Antenna on 4 × 6 dielectric-substrate HIS
Teflon
0.57
λ
L
×
0.86
λ
L
0.078
λ
L
5.1 dBi
(0.54–0.78) GHz 36%
[13]
RT/duroid 5880
0.86
λ
L
×
0.86
λ
L
0.067
λ
L
8.7 dBi
(4.3–5) GHz 15%
[14]
RT/duroid 5880
1.25
λ
L
×
1.25
λ
L
0.06
λ
L
6.0 dBi
(1.06–1.5) GHz 34%
[15]
FR4
1.24
λ
L
×
1.24
λ
L
0.05
λ
L
9.4 dBi
(3.2–5) GHz 44%
[16]
RT/duroid 5880
0.67
λ
L
×
0.84
λ
L
0.102
λ
L
6.9 dBi
(2–3.2) GHz 46%Figure 14
The simulated and measured normalized radiation patterns of the antenna in Figure9(b): (a) 0.55 GHz, (b) 0.65 GHz, (c) 0.75 GHz, and (d) 0.85 GHz.
(a)
(b)
(c)
(d)


## 5. Conclusion

This paper presents minimized low-profile antenna by using HIS ground reflector. A substrate-less HIS is proposed to achieve wide bandwidth up to 52%. Meanwhile, the effect and limitation of ground reflector are analyzed, and minimized reflector size is obtained without affecting antenna performance.



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*Source: 2563927-2017-09-19.xml*