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J. Electromagn. Eng. Sci > Volume 26(3); 2026 > Article
Hadee, Bilal, Bhattacharjee, and Cho: Ultra-Wideband Antipodal Vivaldi Antenna Design with Gain Enhancement by the Application of Multiple Bar Shaped Longitudinal Patches

Abstract

This paper presents a method of introducing novel bar shaped multiple patches to enhance the gain of the often-ignored North Atlantic Treaty Organization (NATO) radio frequencies E-band, that is from 2–3 GHz while maintaining high gain through the entire bandwidth of the antenna. The patches are introduced in the vicinity of the antenna flares. The length of the patches increases subsequently in the end fire direction to cater for different frequency fields. This approach improves the gain and directivity by field coupling, without getting a tradeoff with the absolute bandwidth of the antenna. This new antenna prototype has dimensions of 100 mm × 90 mm × 1.5 mm with measured gain from 3.8–7.8 dBi from 2–10 GHz and for NATO E-band the gain ranges from 3.8–5 dBi which is better than the previous designs with respective antenna size.

I. Introduction

With the advancement of commercial and consumer wireless communication devices, the electromagnetic spectrum at ultrahigh frequency keeps getting congested and restricted [1]. This draws attention to high frequency bands from 2 GHz to 10 GHz and at the same time demands ultra-wideband (UWB) characteristics. UWB technology applies to numerous areas like satellite communication, radars, bio detection, pulse communication as well as high pulsed sources [24]. As frequency increases the antenna size reduces but to incorporate low frequencies in the UWB antenna, simultaneously maintaining the modern compact size, the integration requires miniaturization of the design [4]. The Vivaldi antenna adapts to all these challenges. It is linearly polarized, has an ultra-wide bandwidth (BW) with a stable radiation pattern and gives incremental gain to a broader extent over the wide frequency range [4].
It behaves as a travelling wave antenna at higher frequencies while acts as a resonant antenna at lower frequencies [1, 3]. However, it comes at the expense of a complex fan shaped feeding structure. This structure is a transition from microstrip to a slot line which works as a feeding balun, this limits its BW especially the lower cutoff frequency and gives distorted gain, radiation pattern, and higher sidelobes as well grating lobes at higher frequencies [3, 4].
The Vivaldi antenna, first introduced by Gibson in 1979 as the Aerial Vivaldi, is commonly referred to as the tapered slot antenna (TSA) or coplanar Vivaldi antenna [5]. This coplanar end-fire radiator provides wide impedance bandwidth but suffers from limited gain and radiation pattern instability at higher operating frequencies. To overcome these limitations, Gazit proposed the antipodal Vivaldi antenna (AVA) in 1988 [6]. In this configuration, the exponential flares are printed on opposite sides of the substrate in a symmetric fashion, with one arm functioning as the radiator while the other provides the ground reference. Compared to the coplanar TSA, the AVA exhibits improved impedance matching over a wide frequency range, stable end-fire radiation, and higher gain with enhanced directivity [6].
Despite these advantages, further research has focused on extending the intrinsic performance of the AVA. Reported approaches include the use of anisotropic metamaterials and low-permittivity/loss-tangent substrates to improve realized gain, bandwidth, and return loss [7, 8]. Other studies have investigated modifications to the exponential taper, including leaf-shaped, binomial, and elliptical profiles, or the introduction of multiple tapered slots, thereby enabling multiband operation and gain enhancement [912].
Another notable direction has been the integration of parasitic patches which act as director structures beyond the radiating aperture of the Vivaldi antenna. These director-loaded designs, inspired by Yagi–Uda configurations, employ dipole-like or strip directors aligned in the end-fire direction to reinforce radiation and significantly enhance gain, often achieving 10–12 dBi. However, such external directors are highly sensitive to geometric spacing, leading to increased design complexity and fabrication tolerance issues [3, 13]. More importantly, the additional parasitic elements narrow the impedance bandwidth, elevate sidelobe levels, and enlarge the overall antenna profile, thereby compromising one of the fundamental advantages of the Vivaldi class: UWB performance with compact physical size [13].
In contrast to external directors, recent studies have demonstrated that parasitic conductive patches embedded within the aperture of the AVA can effectively enhance gain and directivity without substantially degrading bandwidth. These patches, typically fabricated from metals such as copper, couple electromagnetically to the tapered flares and extend the effective aperture through localized current induction. Various geometries, including circular, diamond, trapezoidal, elliptical, and staircase shapes, have been proposed [1319]. While each geometry exhibits distinct frequency-dependent responses, the overall mechanism is consistent: electromagnetic (EM) coupling between the patches and the main radiator increases directivity in the end-fire axis. A typical trade-off is that certain patch geometries, such as staircase structures, enhance gain substantially but reduce bandwidth and induce multiband behavior [18], its mitigation is discussed in Section V.
Building upon this body of research, the present work introduces a modified AVA with optimized director-like parasitic patches integrated inside the aperture, thereby combining the gain-enhancing properties of Yagi-inspired designs with the bandwidth-preserving characteristics of embedded patch loading. Unlike conventional director-loaded Vivaldi antennas that extend the aperture and restrict usable frequency range, the proposed architecture maintains wideband impedance matching while achieving high gain and directivity enhancement in the end-fire direction. This yields a compact, high-performance solution suitable for applications demanding ultra-wideband radiation stability and elevated gain, including ground-penetrating radar (GPR), microwave imaging, and ultra-wideband wireless communication systems.

II. Antenna Design and Geometry

Fig. 1 shows the radiator flare and the ground flare of the fabricated prototype of the AVA with bar patches. 0.3 mm thick copper is used as the conductor for the AVA flares as well as for the bar patches. The substrate is FR4 with relative permittivity (ɛr ) of 4.5, loss tangent (tanα) of 0.025 and thickness is 1.5 mm. The schematic of the AVA is shown in Fig. 2. This configuration of AVA is also called as “Exponentially tapered slot antenna” (ETSA) [11].
The outer flare height (Hfo ) should be at least λh4 and the inner flare length (Lfi ) should be at least λh3 where λh is the minimum frequency wavelength. Lfo is the length of outer flare and Hfi represent the inner flare height. The equation for the flare design given in [14] is
(1)
F=C1ekx+C2
where x is the horizontal component of the flare and the constants C1 and C2 are given as
(2)
C1=y2-y1ekx2-ekx1
(3)
C2=y2ekx2-y1ekx1ekx2-ekx1
Here y2, y1, x2, and x1 are the start and end points of the exponential profile and k is the expansion factor, the rate at which the taper profile grows. Whereas fi is the feedline length and fw is the feedline width. Fig. 3 shows the parameters for the bar patches. After numerous simulations and design iterations it was found that the length of the bar patches can be approximated by Eq. (4). The objective of these simulations was to find the optimum length of the bar patches and these simulations are discussed in detail in Section VI.
(4)
Lpx=L-(x-1)
Here L is the initial length of the first patch element and x ranges from 1–4. Lpx is the length of the bar patch, and the width of the patch is represented by Wpx which is constant. This antenna uses parallel plate transmission line but since its impedance is greater than 50 Ω, it is transitioned to a microstrip feed with 50 Ω impedance.

III. Radiation Mechanism

The AVA behaves as a travelling wave antenna at higher frequencies as mentioned in [3], so the radiation comes from coupling of electric field (E-field) between the two flares. When the patches are present in the vicinity of the two flares, this high frequency E-field couples to the patches and produces strong radiation in the end fire direction. The dimension of these patches relates directly to the frequency. The higher the frequency, the smaller the length of the patch. The bar patches and the antenna flares are conductors with the FR4 as a dielectric between them. This is also referred to as capacitive EM coupling.
Fig. 4(a) shows E-field distribution on the surface of AVA with units of volts per meter (V/m) at 8 GHz without bar patches. Weak EM coupling is observed along the antenna axis in the end fire direction almost equal to 300 V/m. The E-field in this case is relatively widely distributed and results in a wider half-power beamwidth (HPBW) and so eventually less directivity is obtained. Fig. 4(b) shows E-field distribution at 8 GHz with bar patches and here on the contrary, strong EM coupling is observed with the bar patches along the antenna axis in the range of 800 V/m. Here most of the bar patch length is being utilized and contributes to the EM coupling and so the E-field is focused and will result in a narrower HPBW, hence more directivity is obtained. Fig. 5 represents E-field comparison in the end fire direction. The results also prove a direct relation between the gain and E-field as the highest E-field value corresponds to high gain. This plot is obtained using far-field approximation at 1 cm over the entire BW. From this, it is proved that the bar patches significantly increase the E-field strength by EM coupling.
Fig. 6 visualizes where and how intensely current flows on the device’s surface at 8 GHz. This simulation result substantiates the E-field distribution results discussed earlier in Fig. 4. So, strong coupling leads to higher current distribution in the bar patches which leads to a higher gain. This proves the application of EM-coupling to enhance antenna radiation.

IV. Simulation Setup

The simulation was carried out in CST Microwave Studio. The time domain solver was used with the hexahedral mesh and 20 cells per wavelength near to model. The fraction of maximum cell near to model was 100 and the cells far from model were only 2. The boundary setup was open and added space perfectly matched layer (PML) with frequency from 2 GHz to 10 GHz. To produce high quality results, adaptive mesh refinement was used with a maximum of 4 passes and as a result the total mesh cell count was progressively over 80 million.

V. Multiband Problem

The multiband problem arises when the patches are too close to the inner flares. Refer to Fig. 2 when D is 24 mm and Fig. 7 when D becomes 1 mm. To resolve this multiband issue and make the antenna gain higher without compromising the BW, the position of the bar patches relative to the inner flare makes the most difference. The term multiband refers to an antenna that is capable of operating effectively on two or more distinct frequency bands. Each of these bands corresponds to different radio frequency ranges, allowing the antenna to transmit and receive signals at multiple frequencies rather than being limited to a single frequency range. In UWB application the multiband feature is considered undesirable as it reduces the absolute BW of the antenna. The same Multiband problem is present in [18] where the staircase patches are used to increase gain of the AVA.
Fig. 8 shows us that when the bar patches are in very close proximity to the inner flares, the multiband problem arises, and the absolute BW is reduced. This problem was reported in [18] when staircase patches were introduced to improve the radiation characteristics of the AVA. So, by increasing the value of D the multiband issue can be easily resolved, but this is not the only problem, because the gain of the AVA is also dependent on the parameter D. Fig. 9 represents how the gain in the end fire direction that is theta 0° and phi 0° is affected at higher frequencies by different values of D. By keeping all the parameters same as shown in Table 1 and manipulating only D the results in Fig. 6 are obtained. At D = 24 mm the gain curve shows the highest value at higher frequencies.

VI. Parametric Case Study

The bar patch lengths contribute differently to the gain of AVA at variant frequencies. To find the best case for fabrication of the design, a parametric study of different bar lengths was done with D = 24 mm. Table 2 gives the dimensions of the bar patches. These values are obtained from Eq. (4) by substituting the values of L. Each value of L derives the four different lengths of the bar patches. Fig. 10 shows the simulation results of the effect of different bar patch lengths on the gain of AVA in the end fire direction. From these curves, it is deduced that the curves align and show no difference at the starting and mid frequencies but after 8 GHz the gain plummets to a meager value of 4 dB for the two larger bar lengths, that is for L = 10 mm and 9 mm. The other two curves, for L = 8 mm and for L = 7 mm, give similar results with a difference of ±0.2 dB. Keeping manufacturing tolerances in mind L = 8 mm is the optimum option for the bar patch lengths.
Fig. 11 shows the effect of bar patch lengths on the reflection coefficient of AVA. For all the bar lengths the reflection coefficient remains below −10 dB from 2–10 GHz, and it can be deduced that it has no effect on the absolute BW of the AVA.

VII. Measurement and Observations

Fig. 12 shows the fabricated antenna under test (AUT), in over-the-air (OTA) antenna chamber. A 50-Ω PCB mount SMA connector is used to feed the antenna. The AUT is mounted on the turning arm in an azimuthal plane.
Fig. 13 illustrates a comparison between simulated and measured reflection coefficient. The reflection coefficient value is below −10 dB from 2 GHz to 10 GHz and beyond but since the antenna is designed and optimized for up to 10 GHz, the results up to only 10 GHz are presented. Both the curves of S11 are of AVA with bar patches. The results confirm that the −10 dB BW of the AVA was not compromised with the introduction of bar patches. The absolute BW of AVA is 8 GHz with the fractional bandwidth (FBW) of over 130%. Fig. 14 shows the realized gain vs frequency plot of simulation of both cases, with and without the bar patches as well as the measured gain of AVA with bar patches. It is evident from the measurement that the bar patches significantly increase the gain. The measured gain is from 3.8 dB to a maximum of 7.8 dB, having gain greater than 5 dB through frequency range of 3–10 GHz. The small deviation between the slopes of measured curve and simulated curve is possibly due to the alignment error between the AUT and the reference antenna in the OTA antenna chamber.
Table 3 shows the comparison between different antenna’s gain measurements in the North Atlantic Treaty Organization (NATO) E-band that is from 2–3 GHz and the 2–10 GHz BW of their respective frequency range. The antenna size is given in terms of the wavelength in the dielectric medium to account for the effect of the permittivity of substrate. The wavelength in the medium is calculated as
(5)
λm=cfɛr
where c is the speed of light in meter per second, f is the lowest frequency of the absolute bandwidth that is 2 GHz. From the results in Table. 3, it is evident that the proposed design with bar patches has the highest gain in the NATO E-band with the most compact size in terms of λm. This is an improvement to the best of author’s knowledge over the AVA designs present in the published literature as the other antenna designs considerably underperform in NATO E-band with the gain hardly close to 3 dB meanwhile the proposed AVA has E-band gain ranging from 3.8–5 dB. Some AVA designs have a max gain 2–3 dB higher than the proposed AVA, for instance [3] and [20] but their size in terms of wavelength is also greater, and the gain is directly related to the size of antenna [3].
Hence for a compact size, the proposed AVA has the highest gain in the NATO E-band and maintains a high gain in the range of 5–7.8 dB through the remaining BW. Using low permittivity substrates can further improve the characteristics of the AVA as it is directly related to the frequency losses [21]. Moreover, FR4’s optimum frequency range is from a few megahertz to 4 GHz and at higher frequencies the FR4 substrate incurs high losses [22]. Besides all this FR4 remains an adequate choice for research purposes with its ease of availability and cost effectiveness.
Fig. 15 shows the polar radiation patterns of E-plane at nine different frequencies of the measured AVA superimposed on the simulated AVA pattern. The measured pattern is represented with solid blue line while the simulated pattern is represented with dashed red color. The plot angles are represented here on a 360° scale with an angle theta ranging from 0° to 359°. The inner circles on the plot are on a scale of dB ranging from -30 dB to 10 dB. From these polar plots, it can be easily acknowledged that the measured patterns align perfectly with the simulated patterns and only slight deviations are observed at higher frequencies. These deviations are due to the fabrication tolerances, as higher frequencies become more prone to even the minimal manufacturing tolerance values.
Fig. 16 shows the total efficiency of the proposed AVA, and it ranges from 55% to a maximum of about 87%.

VIII. Conclusion

The novel bar-shaped multiple patches are introduced in the vicinity of the AVA flares without compromising on the UWB characteristics of the AVA. This approach significantly improves the gain at the most often ignored NATO radio frequencies E-band without doubling the antenna size and maintains a high gain greater than 5 dB through 85% of the BW. It also increases directivity and stabilizes the radiation pattern at high frequencies with main lobe or boresight shifting only a couple of degrees from the end-fire axis of the antenna.

Notes

This work was supported by the Institute of Information and Communications Technology Planning and Evaluation (Grant No. RS-2023-00227929, Research for Alzheimer’s Disease Therapy Utilizing the Electromagnetic Wave) funded by the Korea Government (MSIT).

Fig. 1
Fabricated AVA with bar patches.
jees-2026-3-r-365f1.jpg
Fig. 2
Schematic diagram of proposed AVA design.
jees-2026-3-r-365f2.jpg
Fig. 3
Schematic for bar patches.
jees-2026-3-r-365f3.jpg
Fig. 4
E-field Contour graph of AVA in CST at 8 GHz: (a) without bar patches and (b) with bar patches.
jees-2026-3-r-365f4.jpg
Fig. 5
Relation of bar patches with E-field strength.
jees-2026-3-r-365f5.jpg
Fig. 6
Surface current distribution at 8 GHz.
jees-2026-3-r-365f6.jpg
Fig. 7
Schematic for multiband problem.
jees-2026-3-r-365f7.jpg
Fig. 8
S11 simulation for multiband problem.
jees-2026-3-r-365f8.jpg
Fig. 9
Gain simulation by varying factor D.
jees-2026-3-r-365f9.jpg
Fig. 10
Relation of bar patch length with the gain.
jees-2026-3-r-365f10.jpg
Fig. 11
Bar patch length and reflection coefficient.
jees-2026-3-r-365f11.jpg
Fig. 12
Antenna under test in OTA chamber.
jees-2026-3-r-365f12.jpg
Fig. 13
S-parameter measurement plot of the AVA.
jees-2026-3-r-365f13.jpg
Fig. 14
Comparison of measured gain curves of AVA.
jees-2026-3-r-365f14.jpg
Fig. 15
E-plane plot of measured and simulated AVA. (a) 2 GHz, (b) 3 GHz, (c) 4 GHz, (d) 5 GHz, (e) 6 GHz, (f) 7 GHz, (g) 8 GHz, (h) 9 GHz, and (i) 10 GHz.
jees-2026-3-r-365f15.jpg
Fig. 16
Measured total efficiency of AVA.
jees-2026-3-r-365f16.jpg
Table 1
Dimensions of AVA (unit: mm)
Parameter Length Parameter Length
Ws 90 Lp1 8
Ls 100 Hfo 100
Lfi 62 fi 3.2
Lfo 40 fw 2.4
Hfi 35.2 Wpx 1.5
D 24
Table 2
Parametric dimensions of bar patch lengths (unit: mm)
L Lp1 Lp2 Lp3 Lp4
10 10 9 8 7
9 9 8 7 6
8 8 7 6 5
7 7 6 5 4
Table 3
Gain comparison of antenna designs in literature with starting 1 GHz BW
Study Efficiency (%) λm (mm) ɛr Gain (dB)

E-band 2–10 GHz
Nassar & Weller [3] Not given 87.4 2.9 1–3 0–10
Li et al. [11] Not given 101.1 2.2 0–1.8 0–7
Agahi et al. [15] Not given 86.6 3.0 1.5–2 0–5
Bang et al. [16] Not given 86.6 3.0 1–3 1–9
Zhang et al. [17] Not given 70.7 4.5 2–3 2–6
Karmakar et al. [20] 40–85 87.4 2.9 2–3 3–11
This work 55–87 70.7 4.5 3.8–5 3.8–7.8

References

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Biography

jees-2026-3-r-365f17.jpg
Abdul Hadee, https://orcid.org/0000-0002-1449-5337 received B.E. degree in Avionics engineering from Institute of Space Technology, Islamabad, Pakistan in 2020. He is currently pursuing an integrated M.S. & Ph.D. in Smart Air Mobility at Korea Aerospace University, Republic of Korea. He started his career as a trainee engineer at the Radar Lab of School of Interdisciplinary Engineering and Sciences, National University of Science & Technology, Islamabad, Pakistan. He also worked as an assistant executive engineer at a public sector organization in Pakistan. His research interests include antenna array design and radar signal processing.

Biography

jees-2026-3-r-365f18.jpg
Ahmad Bilal, https://orcid.org/0000-0003-4806-4428 received B.S. degree in electronic engineering from Ghulam Ishaq Khan Institute of Engineering Sciences and Technology, Topi, Pakistan, in 2015 and M.S. degree in electrical engineering from Lahore University of Management Sciences, Lahore, Pakistan, in 2017. He received a second M.S. degree in avionics engineering from Air University, Kamra, Pakistan in 2021. He is currently pursuing a Ph.D. in Smart Air Mobility at Korea Aerospace University, Republic of Korea. From 2018 to 2021, he was a design engineer at Pakistan Aeronautical Complex, Kamra, Pakistan. His research interests include FDA transceiver design and AI based radar signal processing.

Biography

jees-2026-3-r-365f19.jpg
Sohom Bhattacharjee, https://orcid.org/0000-0001-8705-1473 received B.Tech. degree in electrical engineering from Netaji Subhash Engineering College, MAKAUT, Kolkata, India in 2018. He is currently pursuing an integrated M.S. & Ph.D. in Smart Air Mobility at Korea Aerospace University, Republic of Korea. His research interests include antenna design, applications of electromagnetic waves in biomedical engineering and molecular dynamics.

Biography

jees-2026-3-r-365f20.jpg
Choon Sik Cho, https://orcid.org/0000-0003-0833-5254 received B.S. degree from the Department of Control and Instrumentation Engineering, Seoul National University, Korea in 1987 and Ph.D. in electrical & computer engineering from University of Colorado at Boulder, USA in 1998. He joined Korea Aerospace University in 2004 and is currently serving as a professor at the Department of Electrical & Electronic Engineering. From 1987 to 1993, he worked with LG Information & Communication and from 1999 to 2003 he worked with Pantech and Curitel, Korea. His research interests include RFIC design, bio-electromagnetics and radar systems.

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