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. 2025 Jul 2;15:22723. doi: 10.1038/s41598-025-07208-x

Printed multiple input multiple output antennas powered by passive metamaterial and defected ground for diverse sixth generation applications

Shahanawaz Kamal 1,, Padmanava Sen 1
PMCID: PMC12214527  PMID: 40595168

Abstract

The evolution of 6th generation (6G) wireless technology has become imperative due to the exponential growth of wireless devices and applications. In a macro-cellular scenario, the 6 GHz electromagnetic spectrum is projected to be the framework for 6G commencement. However, the main obstacles that inhibit their potential at the physical layer are the fabrication intricacies entailed in comprehending high port isolation (Inline graphic) and other key performance indicator (KPI) of compact printed multiple-input-multiple-output (MIMO) antennas. Subsequently, to overcome these impediments, six novel meander line-based MIMO antennas (Inline graphic) have been introduced for diverse 6G use cases, including internet of things, extended reality, artificial intelligence, vehicle-to-everything, unmanned aerial vehicle, and device-to-device integrated sensing and communications. Furthermore, two unique passive metamaterial structures of square ring (Inline graphic) and shorting pins (Inline graphic) have been studied for attaining an electromagnetic bandgap (EBG). Their performance were investigated by means of numerical simulations and validated through measurements conducted within the anechoic chamber. Meticulous strategies for accomplishing impedance matching, circularly polarization (CP), and high Inline graphic values have been presented. Each of the proposed MIMO antennas employed dual radiators, a defected ground, and an EBG structure to exhibit Inline graphic of Inline graphic21 dB, quasi-isotropic CP, and other desirable KPI of MIMO antennas. Their assembly possessed a low-profile of 0.03 free-space wavelength (Inline graphic) and an area of 1.1Inline graphic Inline graphic 1.1Inline graphic, thus being preferable for cost-effective compact terminals. During the measurements, each prototype yielded one or more remarkable MIMO antenna KPI in the 6 GHz band. Particularly, Inline graphic enabled filtered bandwidth (BW) of 8.84% and modest gain (G) of 6.4 dBic, Inline graphic attained high G of 7.1 dBic and enhanced efficiency (Inline graphic) of 87%, Inline graphic yielded high Inline graphic of 94%, Inline graphic established notable radiation pattern with fair G of 5.8 dBic, Inline graphic provided filtered BW of 9.69% and prominent Inline graphic of 93%, and Inline graphic featured wide axial ratio (AR-BW) of 60.63%. Furthermore, all antenna measurements demonstrated good MIMO performance with envelope correlation coefficient and diversity gain of <0.2 and Inline graphic10 dB, respectively. The novelty of this work lies in the radiator and ground designs, as well as the accomplishment of numerous KPI that surpass state-of-the art MIMO antennas.

Subject terms: Electrical and electronic engineering, Metamaterials

Introduction

The installation of cables across diverse locations for wireline communication manifests practical challenges and high expenditures1. A wireless transceiver that uses a printed antenna to convert electric current into and from EM waves represents an inexpensive alternative to a wireline system2. Therefore, the wireless technology has become essential in most of the facets of modern civilization3,4. However, the existing 5th generation (5G) network cannot accommodate the swift expansion of wireless devices and applications5, necessitating the development of 6G wireless technology6. The upper 6 GHz EM spectrum is estimated to remain utilized by both licensed and license-exempt incumbents to further 5G evolution7, and ultimately serve as the foundation for 6G commencement in a macro-cellular scenario8. Furthermore, 6G systems will initially assess the adaptability of antenna beam control by visualizing the quasi-isotropic radiation pattern (RP) at 6 GHz spectrum for channel approximation of millimeter (mm) waves9,10.

Typically, the performance of a single-input-single-output (SISO) system is significantly impacted by link disruptions induced by misaligned transmitting and receiving antennas11. The deployment of a printed antenna array with directional beam scanning operation could lead to trustworthy communication, but it often calls for a substantial amount of space, making it inappropriate for compact devices.12. An additional viable approach involves the use of a linearly polarized (LP) quasi-isotropic MIMO antenna, which increases the transmission capacity while generating nearly null-free RP in all directions13. However, the 6 GHz EM signals are susceptible to environmental factors and would eventually lead to the failure of a wireless system in many real-life circumstances14. Integrating a MIMO antenna with quasi-isotropic CP RP constitutes a realistic alternative to prevent multiple paths fading from the ionosphere, thereby making it an important aspect of a 6G system15,16.

The work efficacy of a 6G system can be determined by evaluating the KPI expressions of antenna17 and MIMO18. However, specific KPI are of critical importance depending on 6G use cases, as indicated in Fig. 1. Descriptively, the low power wide area (LPWA) technology intended for operation in the licensed narrow-spectrum to enable low data rate IoT services like environment monitoring and vehicle parking necessitates a narrow impedance bandwidth (I-BW)/AR-BW antenna with good G performance19,20. Similarly, UAV use cases that are capable of traveling far distances, such as drones, need a limited I-BW/AR-BW21. However, to sustain a prolonged flight duration with reduced power consumption, Inline graphic of a 6G UAV antenna should be maximized22. On the contrary, antennas for XR use cases, including a head-mounted display, should render reasonably wide I-BW/AR-BW with good G and Inline graphic performance23. Particularly because a 6G XR antenna would share I-BW/AR-BW requirements with other consumer electronics, and their G and Inline graphic are often affected by the vicinity of other sub-system hardware and the human head24. Furthermore, in AI-based robot communication, compliance with security standards to preserve personnel from injury constitutes a significant difficulty that can be addressed with a high Inline graphic antenna25,26. Another related use case that requires a high G antenna is V2X communication, which gathers, analyzes, and exchanges data from many infrastructures27,28. Finally, for 6G D2D ISAC, a small, low-profile antenna with high Inline graphic and wide I-BW/AR-BW will be required because these use cases entail direct communication between several handheld devices without the involvement of a base station29,30.

Figure 1.

Figure 1

Antenna KPI based on 6G use cases (drawn by the author: Kamal, S.).

Generally, closely-placed MIMO antennas in a compact and low-profile arrangement are susceptible to trade-off in Inline graphic values31,32. In the past, Inline graphic values between antenna elements have been manipulated by deploying defected ground33, neutralization lines34, parasitic elements35, excitation of different modes36, MTM37, or a combination of one38 or many39, which weaken, resist, or lower the surface current flow. Then again, realization of high Inline graphic values in the entire operating spectrum still remains an open challenge. Similarly, the literature presents a number of antennas to accomplish quasi-isotropic CP RP that can be grouped into two primary categories: multi-antenna and perturbation techniques. The multi-antenna solution incorporates a particular feeding architecture to excite CP RP in antennas of identical or combination types, such as cavity40, dipole41, inverted-F42, and microstrip43. These multi-antenna arrangements are capable of enabling wide AR-BW, but at the expense of considerable volumes. On the contrary, the perturbation approach generates two orthogonal RP modes of CP by constructing parasitic frameworks44, etching slots45, or slicing edges46 in the primary radiating element of an antenna. However, these perturbation-based antennas are capable of producing narrow AR-BW. Furthermore, G deviation47 and low Inline graphic48 remains important challenges in most of the quasi-isotropic CP antennas, making their straightforward integration in portable devices difficult.

Based on the above motivation, the main objective of this work was focused on the design of lucrative printed antennas for diverse 6G uses cases entailing quasi-isotropic CP coverage in the 6 GHz EM spectrum. Sequentially, the following three tasks were attempted and solved successfully. The first part was focused on the design of quasi-isotropic LP SISO antennas operating in the 6 GHz EM spectrum with enhanced performance. The second phase concentrated on converting LP waves to CP RP by integrating apertures in the ground plane, without modifying the design of the proposed SISO radiating element. The final section of the study concentrated on using passive MTM to enable improved Inline graphic values in closely-placed MIMO antenna configurations of the proposed CP SISO antenna designs. All antennas were analyzed through simulation studies, while all MIMO antennas rendering quasi-isotropic CP RP were subjected to fabrication and measurements.

Methods

Antenna configuration and analysis technique

The configuration of the proposed printed circuit board (PCB)-based MIMO antenna elements at various phases of ANSYS high frequency structure simulator (HFSS) simulation are shown in Fig. 2 and their corresponding parameter values in Inline graphic at center frequency (Inline graphic) Inline graphic 6 GHz are listed in Table 1. Five unique designs of SISO radiator/top copper (Inline graphic) are demonstrated in Fig. 2a. Where, Inline graphic indicates circular radiator associated with 0.25Inline graphic-fed rectilinear microstrip; Inline graphic denotes circular radiator amalgamated amidst 0.25Inline graphic-fed meander line; Inline graphic symbolizes meandered radiator enclosed by microstrip bracket coupled to 0.25Inline graphic-fed rectilinear trace; Inline graphic manifests meandered radiator within microstrip frame attached to 0.25Inline graphic-fed meander line; Inline graphic exemplifies crescent-axed meandered radiator juxtaposed to 0.25Inline graphic-fed meander line.

Figure 2.

Figure 2

Proposed antenna parts. Layout: gray, Inline graphic; light gray, Inline graphic; black, Inline graphic; Inline graphic, port. (a) SISO Inline graphic; (b) SISO Inline graphic; (c) Inline graphic; (d) Inline graphic; (e) Brillouin zone; (f) MTM boundary setup; (g) MTM array; (h) Inline graphic; (i) Fabricated prototypes.

Table 1.

Parameter values of the proposed antenna elements in Inline graphic at Inline graphic Inline graphic 6 GHz.

Tag Value Description Tag Value Description
Inline graphic 0.03 Substrate height Inline graphic 0.08 Gap between two shorting pins
Inline graphic 0.50 Single element substrate length Inline graphic 0.02 Transition slot length
Inline graphic 0.50 Single element substrate width Inline graphic 0.06 Transition slot width
Inline graphic 0.10 Microstrip feed length Inline graphic 0.09 Gap between Inline graphic and substrate edge
Inline graphic 0.06 Microstrip feed width Inline graphic 0.25 Gap between Inline graphic and substrate edge
Inline graphic 0.25 Wavelength transformer length Inline graphic 0.18 Gap between two transition slots
Inline graphic 0.04 Wavelength transformer width Inline graphic 0.21 Rectangular slot length
Inline graphic 0.08 Middle section link length Inline graphic 0.16 Rectangular slot width
Inline graphic 0.14 Meander line length Inline graphic 0.03 Gap between upper transition slot and Inline graphic
Inline graphic 0.02 Meander line width Inline graphic 0.18 Gap between upper Inline graphic and substrate edge
Inline graphic 0.01 Meander line twist length Inline graphic 0.46 Crescent-axed microstrip diameter
Inline graphic 0.04 Variation in meander line twist length Inline graphic 0.02 Gap between Inline graphic and Inline graphic
Inline graphic 0.04 Final meandered section length Inline graphic 0.10 Partial ground length
Inline graphic 0.01 Final meandered section width Inline graphic 0.5 Partial ground width
Inline graphic 0.01 Adjacent link length Inline graphic 0.10 Right-bottom cage slot length
Inline graphic 0.46 Outer microstrip diameter Inline graphic 0.09 Right-middle cage slot length
Inline graphic 0.33 Inner microstrip diameter Inline graphic 0.04 Right-top cage slot length
Inline graphic 0.06 Radiating parasitic element width Inline graphic 0.13 Left-bottom cage slot length
Inline graphic 0.52 Gap between Inline graphic and substrate edge Inline graphic 0.09 Left-middle cage slot length
Inline graphic 0.02 Opening in parasitic element Inline graphic 0.01 Left-top cage slot length
Inline graphic 0.02 Gap between two parasitic slot elements Inline graphic 0.01 Cage slot width
Inline graphic 0.02 Shorting pin diameter

Similarly, five different layouts of SISO ground/bottom copper (Inline graphic) are depicted in Fig. 2b. Where, Inline graphic illustrates full ground; Inline graphic signifies partial ground; Inline graphic expresses defected 0.25Inline graphic transition points, cage slotted central segment and radiator; Inline graphic represents cage slotted radiator, defected middle section and 0.25Inline graphic transition regions; Inline graphic exhibits defected 0.25Inline graphic transitions, intermediate passage and radiator.

Furthermore, two distinct passive MTM-based EBG cell of square ring (Inline graphic) and shorting pin (Inline graphic)/via copper (Inline graphic) are displayed in Fig. 2c, d, respectively. The microstrip elements and spacing between them may be specified by inductance (L) and capacitance (C), respectively, as illustrated in Fig. 2c. The Brillouin49,50 domain was applied to anticipate the characteristics of EBG framework. Where, the Inline graphic position denotes the focal point of the Brillouin zone, while the M and X locations correspond to the midpoints of an edge and a face, respectively, as depicted in Fig. 2e. The master-slave boundary setup in ANSYS HFSS eigenmode simulation setting was used to study a MTM cell, as shown in Fig. 2f. The optimum arrangement involves unit MTM cell arranged in an array, as shown in Fig. 2g.

The finalized layout of a MIMO antenna comprises of twin radiating elements, a defected ground, and a MTM-based EBG cell array. Six antenna configurations have been regarded as optimum, including Inline graphic (Inline graphic; Inline graphic), Inline graphic (Inline graphic; Inline graphic), Inline graphic (Inline graphic; Inline graphic), Inline graphic (Inline graphic; Inline graphic), Inline graphic (Inline graphic; Inline graphic), and Inline graphic (Inline graphic; Inline graphic). The top and bottom perspectives of one of the proposed antenna (Inline graphic) as well as the equivalent circuit model of a meandering portion are depicted in Fig. 2h. Two alike radiating elements were positioned adjacent to each other in close proximity on the top surface of PCB, whereas a defected ground was incorporated onto the bottom side of PCB. The two radiating elements were fed from the identical edge of PCB and separated by an array of unit Inline graphic cell.

Figure 2i displays photographs of the six fabricated MIMO antenna prototypes, with bottom configurations shown as their respective insets. All MIMO antennas were manufactured on the flame retardant (FR-4) substrate (Inline graphic Inline graphic 4.4, Inline graphic Inline graphic Inline graphic 0.02) using the photo-lithography method and fed with the SubMiniature Version A (SMA) BU-1420701851 connector. Their performance was measured with Diamond Engineering Antenna Measurement Studio and a standard horn antenna in the anechoic chamber at Barkhausen Institut, Germany. Descriptively, the values of reflection coefficient (Inline graphic) and Inline graphic were obtained whilst connecting the two ports of a MIMO antenna to Keysight N5224B PNA microwave network analyzer. However, when RP, G and other MIMO antenna parameters were being measured, one of the two ports was equipped with the 50Inline graphic termination resistance. Furthermore, the far-field parameters were evaluated in the direction of maximum radiation, which was near the broadside direction. The MIMO antenna under test was configured in the Inline graphic Inline graphic Inline graphic and Inline graphic Inline graphic Inline graphic directions, and RP were recorded for each of the two different alignments. The axial ratio (AR) values were equated by the G difference between the Inline graphic Inline graphic Inline graphic and Inline graphic Inline graphic Inline graphic orientations. The computation of directivity from the measured RP in the Inline graphic Inline graphic Inline graphic and Inline graphic Inline graphic Inline graphic planes formed the basis for Inline graphic evaluation. Finally, the ECC, DG, total active reflection coefficient (TARC), and channel capacity loss (CCL) values were estimated using Equations16,51,52 1, 2, 3, and 49, respectively. Where, Inline graphic and Inline graphic represents the ith and jth elements of RP, respectively.

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This research addresses all physical factors that could possibly influence the proposed antennas’ impedance and radiation characteristics. Given the substantial amount of radiator, ground, and metamaterial combinations that have been explored, each result shows the considered design on the right/left hand side bottom. Furthermore, the figure caption specifies the serial number of the top copper (Inline graphic), bottom copper (Inline graphic), and metamaterial (MTM) configurations under consideration as their superscript, allowing readers to easily determine which antenna data are presented.

Design formulation for impedance matching

The preliminary layout of the proposed SISO antenna was based on the hypothesis53 of a circular-patterned radiating element with radius (Inline graphic/2) estimated using Equations17 10 and 11. Particularly because circular antennas have multiple advantages over other shapes, including design flexibility, wide I-BW, and enhanced quasi-isotropic G performance30. These benefits, however, depend on the formulation of the impedance matching network17. A straightforward technique to match a real load impedance to a variable source impedance constitutes the utilization of a 0.25Inline graphic line, which can be expanded to multi-section configurations54. Therefore, the 0.25Inline graphic line was selected as the feed mechanism of the proposed antennas. Nevertheless, direct connection of a circular radiator to a 0.25Inline graphic line yields narrow I-BW5557. Thus, the initial objective was to attain an appropriate impedance matching with enhanced I-BW in the 6 GHz EM spectrum. Subsequently, Inline graphic and AR response of a SISO antenna comprising of a circular radiator associated with 0.25Inline graphic-fed rectilinear microstrip was studied, as depicted in Fig. 3a. A Inline graphic of −6 dB with AR of >3 dB was ascertained at 7.1 GHz and 8.1 GHz. The second resonance was produced by the middle segment of rectilinear line, whose width was kept narrower than the 0.25Inline graphic feed line to manipulate the impedance values. Figure 3b reveals that G of Inline graphic3 dBi and Inline graphic of Inline graphic75Inline graphic were perceived at 7.1 GHz, while Fig. 3c demonstrates that quasi-isotropic co-polar (co) and cross-polar (Inline graphic) RP became apparent at 7.1 GHz.

Figure 3.

Figure 3

Proposed LP SISO antenna. Layout: Inline graphic; Inline graphic. Simulated results: (a) AR, Inline graphic; (b) Inline graphic, G; (c) RP at 7.1 GHz.

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Given that fulfillment of Inline graphic Inline graphic −10 dB counts for a number of use cases, further investigation of the aforementioned antenna design remained important. One of the many crucial components affecting the antenna impedance includes the dimension of the radiating element. Typically, the antenna resonance shifts to lower frequencies when the dimensions of the radiator is lengthened or shortened. However, this methodology results in an enlarged footprint when employed for switching to lower frequencies. Therefore, the conductor was folded in the form of a meander line to increase the microstrip length, shift the antenna resonance to the desired frequencies, and ensure better utilization of the available area. Particularly, a 0.25Inline graphic-fed meander line was introduced as a connection to the circular radiator. Their dimensions were estimated from the characteristic impedance (Inline graphic) of a transmission line with effective dielectric constant (Inline graphic) Equations58 12 and 13. An appropriate impedance matching of −10 dB with AR of >3 dB was established at 6.8 GHz and 8.3 GHz, as demonstrated in Fig. 4a. Furthermore, at 6.8 GHz, G of >3.5 dBi and Inline graphic of >75Inline graphic were achieved as shown in Fig. 4b, with quasi-isotropic RP as depicted in Fig. 4c.

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The preceding simulation phases proved that integrating the middle segment contributes to generating additional resonance. Hence, the next part of the study was focused on incorporating another section to obtain supplementary resonances. Specifically, a SISO antenna consisting of a meandered radiator and a microstrip bracket connected to a 0.25Inline graphic-fed rectilinear trace was studied. The length of a meander line and the gap between two meander lines were computed using Equations59 14 and 15 with permeability (Inline graphic) permittivity (Inline graphic) of the vacuum. The modified antenna design produced multiple resonances with AR of >3 dB, as shown in Fig. 5a. These operating frequencies included 4.3 GHz, 6.7 GHz, 7 GHz, 7.6 GHz, and 8.6 GHz. Furthermore, G of >2 dBi and Inline graphic of Inline graphic45Inline graphic were attained at 8.6 GHz, as revealed in Fig. 5b. However, the responses of G and Inline graphic appeared to be subpar at other frequencies, with values ranging from Inline graphic3 to Inline graphic1 dBi and from Inline graphic10Inline graphic to Inline graphic40Inline graphic, respectively. Yet, reasonable quasi-isotropic RP was established at 7 GHz, as demonstrated in Fig. 5c.

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Figure 4.

Figure 4

Proposed LP SISO antenna. Layout: Inline graphic; Inline graphic. Simulated results: (a) AR, Inline graphic; (b) Inline graphic, G; (c) RP at 6.8 GHz.

Figure 5.

Figure 5

Proposed LP SISO antenna. Layout: Inline graphic; Inline graphic. Simulated results: (a) AR, Inline graphic; (b) Inline graphic, G; (c) RP at 7 GHz.

To advance the last investigation, the influence of substituting the middle portion of the rectilinear line with a meander line was considered. The antenna exhibited AR of >3 dB and −10 dB Inline graphic resonances almost similar to the previous design, namely at 4.3 GHz, 6.8 GHz, 7.1 GHz, 7.7 GHz, and 8.6 GHz, as portrayed in Fig. 6a. However, relatively higher G of Inline graphic3 dBi and Inline graphic of Inline graphic60Inline graphic were achieved at 8.6 GHz, as illustrated in Fig. 6b. At other frequencies, the responses of Inline graphic and G also appeared to be substantially better, with values ranging from Inline graphic20Inline graphic to Inline graphic70Inline graphic and Inline graphic1 dBi to Inline graphic3 dBi, respectively. Furthermore, Fig. 6c reveals that an adequate quasi-isotropic RP was accomplished at 7.1 GHz.

Figure 6.

Figure 6

Proposed LP SISO antenna. Layout: Inline graphic; Inline graphic. Simulated results: (a) AR, Inline graphic; (b) Inline graphic, G; (c) RP at 7.1 GHz.

The radiator design was further examined to enable improved antenna performance based on the advantages of meandered microstrip found in the simulation studies outlined above. Descriptively, a meander line characterized by an irregular trend of four different parts was taken into consideration. The first segment entailed bending the microstrip in the opposite orientation to shift the trajectory of the electric current. In the subsequent section, a narrow trace was implemented in conjunction to an obese track. The third region integrated the slimmest microstrip of a circular meander structure. Finally, the circuit terminated at a crescent-shaped line. With AR of >3 dB, the antenna yielded Inline graphic Inline graphic −10 dB at 4.17 GHz, 4.58 GHz, 5.78 GHz, 6.08 GHz, 6.89 GHz, 7.83 GHz, and 8.39 GHz, as indicated in Fig. 7a. Their G values spanned between Inline graphic2 dBi and Inline graphic2 dBi, while their Inline graphic values ranged from Inline graphic14 to Inline graphic45Inline graphic, as illustrated in Fig. 7b. Particularly, at 6.08 GHz, quasi-isotropic RP was achieved with −2 dBi G and 15Inline graphic Inline graphic, as shown in Fig. 7c. In contrast to the other designs mentioned above, G and/or Inline graphic results seem to be less noteworthy, yet this antenna configuration was important in the realization of wideband CP EM waves that is described in the remainder of this paper.

Figure 7.

Figure 7

Proposed LP SISO antenna. Layout: Inline graphic; Inline graphic. Simulated results: (a) AR, Inline graphic; (b) Inline graphic, G; (c) RP at 6.08 GHz.

The current distributions of all the proposed LP SISO antenna radiators have been presented in Fig. 8 to elucidate their working mechanisms. The ground plane currents that traversed to the radiating elements resisted the phase shift of field components. Hence, the antenna radiators exhibited LP behavior with >3 dB AR values. Besides, the fundamental surface currents, highlighted in red, were primarily concentrated on the feed line in the Inline graphic configuration. The integration of meandering feed line to the circular radiator contributed to a proper distribution of the surface currents throughout the entire Inline graphic configuration. Similarly, the successive evolution of distinct designs (Inline graphic) resulted in equally distributed fundamental currents throughout the radiators, enabling wide I-BW. These results eventually justify the importance of the proposed feed method.

Figure 8.

Figure 8

Simulated current distributions of the proposed LP SISO antenna radiators: Inline graphic at 7.1 GHz, Inline graphic at 6.8 GHz, Inline graphic at 7 GHz, Inline graphic at 7.1 GHz, and Inline graphic at 6.08 GHz.

Blueprint for generating circular polarization

Typically, a CP antenna comprises of time-varying current paths on the radiator and prerequisites I-BW and CP BW that corresponds to −10 dB Inline graphic and 3 dB AR, respectively60. In order to regulate the resonant properties of the proposed LP antennas, adjust the current directions on the radiators to generate CP waves, and retain the compact profile and dimensions, the ground plane designs were meticulously studied. Initially, the partial ground plane design (Inline graphic) was investigated in conjunction to Inline graphic radiator. The antenna operated from 5.7 GHz to 6.1 GHz with AR-BW of Inline graphic0.4 GHz, as shown in Fig. 9a. In the entire operating band, their G and Inline graphic values remained >2 dBic and Inline graphic70Inline graphic, respectively, as demonstrated in Fig. 9b. Furthermore, quasi-isotropic CP RP was ascertained at 6 GHz, as illustrated in Fig. 9c.

Figure 9.

Figure 9

Proposed CP Inline graphic antenna. Layout: Inline graphic; Inline graphic. Simulated results: (a) AR, Inline graphic; (b) Inline graphic, G; (c) RP at 6 GHz.

Since, the realization of CP waves was largely attributed to the introduction of apertures in the ground plane, further research was conducted to realize the additional antenna KPI necessary for various use cases. Particularly, slots were inserted near impedance transition points and radiating elements to form caged apertures in the ground plane. In contrast to the aforementioned CP antenna arrangement, the setup composed of Inline graphic and Inline graphic, enabled wide total BW (at Inline graphic) of 0.25 GHz (at 4.75 GHz), 0.02 GHz (at 5.35 GHz), 0.23 GHz (at 6.08 GHz), and 0.46 GHz (at 8.41 GHz) with AR Inline graphic3 dB, as displayed in Fig. 10a. Furthermore, their G and Inline graphic values ranged between −1.5 dBic to 3.3 dBic and 25Inline graphic to 65Inline graphic, respectively, as shown in Fig. 10b. At 6 GHz, quasi-isotropic CP RP was accomplished, as portrayed in Fig. 10c.

Figure 10.

Figure 10

Proposed CP Inline graphic antenna. Layout: Inline graphic; Inline graphic. Simulated results: (a) AR, Inline graphic; (b) Inline graphic, G; (c) RP at 6 GHz.

The caged slot layout of the ground plane in the previous design increased the −10 dB I-BW, but their 3 dB CP BW did not fully match it. In order to identify the main cause of the 3 dB AR-BW limitation, the ground plane arrangement next to the meandered feed was changed to a relatively larger aperture in the subsequent study. The Inline graphic and AR curves for the new ground plane design (Inline graphic) on the previously considered radiator design (Inline graphic) are demonstrated in Fig. 11a. Multiple resonances including 4.55–4.78 GHz, 5.44–5.59 GHz, 6.12–6.31 GHz, and 7.64–8.64 GHz were accomplished. Furthermore, an appropriate AR of <3 dB was established in all operating bands, which led to the conclusion that this improvement may have been due to the reduction in ground plane currents’ interference with the radiating elements. Additionally, as shown in Fig. 11b, peak G and Inline graphic of Inline graphic3.5 dBic and >60Inline graphic were acquired, respectively, and a quasi-omnidirectional CP RP was achieved at 6.2 GHz, as shown in Fig. 11c.

Figure 11.

Figure 11

Proposed CP Inline graphic antenna. Layout: Inline graphic; Inline graphic. Simulated results: (a) AR, Inline graphic; (b) Inline graphic, G; (c) RP at 6.2 GHz.

Given the previous study demonstrated that increasing the ground plane aperture area close to the feed line improves the AR values, the subsequent study concentrated on assessing the effect of expanding the ground plane slot region beneath the main radiating elements on the antenna KPI. Particularly, the combination of Inline graphic and Inline graphic arrangement was explored, which showed notable improvement in the 3 dB AR values for both the −10 dB Inline graphic resonances between 6.56–6.78 GHz and 8.23–8.55 GHz, as illustrated in Fig. 12a. Similarly, Fig. 12b displays a significant improvement in G of Inline graphic4.5Inline graphic dBic and Inline graphic of Inline graphic80Inline graphic, while Fig. 12c indicates reasonable quasi-omnidirectional CP RP at 6.6 GHz.

Figure 12.

Figure 12

Proposed CP Inline graphic antenna. Layout: Inline graphic; Inline graphic. Simulated results: (a) AR, Inline graphic; (b) Inline graphic, G; (c) RP at 6.6 GHz.

Subsequently, the Inline graphic ground plane configuration was explored when integrated with the Inline graphic radiator design. As shown in Fig. 13a, the antenna exhibited appropriate impedance matching at 5.65 GHz, 6.46 GHz, and 7.28 GHz with Inline graphic0.2 GHz I-BW for each resonant frequencies. Additionally, with exceptions at a few frequencies, the AR values stayed <3 dB across a significant number of operating ranges. Besides, as Fig. 13b illustrates, good G of Inline graphic4 dBic and Inline graphic of Inline graphic70Inline graphic were obtained. The CP RP curves confirm a notable improvement in Fig. 13c.

Figure 13.

Figure 13

Proposed CP Inline graphic antenna. Layout: Inline graphic; Inline graphic. Simulated results: (a) AR, Inline graphic; (b) Inline graphic, G; (c) RP at 6 GHz.

Figure 14 presents the current distributions on the ground planes and radiating elements of all the proposed CP SISO antennas to gain insight into their operating mechanisms. The principal currents were formed in the south-west direction at Inline graphic and the north-east direction at Inline graphic in the highlighted segments of Inline graphic (Inline graphic; Inline graphic), Inline graphic (Inline graphic; Inline graphic), and Inline graphic (Inline graphic; Inline graphic) radiators. Similarly, the fundamental currents in the highlighted portions of the Inline graphic (Inline graphic; Inline graphic) and Inline graphic (Inline graphic; Inline graphic) radiators were formed at Inline graphic and Inline graphic in the north-east and south-west directions, respectively. Furthermore, other radiating elements exhibited identical responses to the primary current directions at different phase angles. Therefore, a phase shift between the two fundamental field components of Inline graphic was accomplished. The CP characteristics were rendered as the true nature of the top copper sections became apparent by altered impedance levels at multiple radiator segments and reduced coupling from the ground plane.

Figure 14.

Figure 14

Simulated current distributions of the proposed CP SISO antennas at 6 GHz.

Note that, out of the multiple practicable combinations of proposed radiating elements (Inline graphic) and ground planes (Inline graphic), only the most pertinent ones have been described, taking into account the current project requirements. However, the presented results offer ample data to estimate the effects of remaining combinations.

Road map for isolation enhancement

The ultimate goal of this work was to conclude MIMO-based antenna designs. Hence, the study of closely-placed 2-port arrangement of Inline graphic CP antenna was initially considered for the subsequent optimization phases. In particular, their surface current distribution was examined, and Fig. 15a shows that a significant amount of current traveled from port Inline graphic to port Inline graphic. Therefore, a square ring (Inline graphic) shaped transmission line was studied for enabling EBG properties. Their initial dimensions were predicted from Equations61 16, 17, 18, 19, and 20. The dispersion diagram of unit Inline graphic cell with two modes (Inline graphic and Inline graphic) activated is displayed in Fig. 15b. An EBG BW of Inline graphic1 GHz was yielded. Subsequently, an array of unit Inline graphic cell was positioned between the two Inline graphic radiating elements with Inline graphic ground plane. Their current distribution was then assessed, and the results showed a significant decrease in the mutual coupling between port Inline graphic and port Inline graphic, as portrayed in Fig. 15c.

Figure 15.

Figure 15

Proposed CP MIMO antennas. Layout: Inline graphic; Inline graphic. Simulated surface current distributions of antennas at 6 GHz: (a) without MTM; with (c) Inline graphic and (e) Inline graphic. Dispersion diagrams of (b) Inline graphic and (d) Inline graphic. Simulated Inline graphic and Inline graphic of antennas: (f) without MTM; with (g) Inline graphic and (h) Inline graphic.

Realizing a wide isolation BW constitutes one of the major objectives of this work. Although Inline graphic enabled an adequate EBG BW, another MTM design was explored to enhance it further. The research presented in the preceding sections indicate that the ground plane currents significantly affect the antenna’s overall behavior. Additionally, it has been demonstrated that periodic surfaces composed of regions with shorting pins exhibit notable EBG in their dispersion diagrams, which prevent surface waves from propagation62. Hence, a setup based on shorting pins (Inline graphic) was considered was investigation. An equivalent parallel resonant LC circuit may be employed to describe architectures characterized by shorting pins63. Consequently, their initial dimensions were estimated using Eq.61 16, taking into account that C and L correspond to the patch dimension and the shorting pin length, respectively. Figure 15d illustrates the dispersion diagram of Inline graphic with Inline graphic and Inline graphic excited, which enabled an EBG BW of Inline graphic2 GHz. The two Inline graphic radiators were then separated by an array of unit Inline graphic cells with Inline graphic ground plane. When their current distribution was analyzed, relatively better reduction in the mutual coupling between ports Inline graphic and Inline graphic was noticed, as shown in Fig. 15e. Note that the current distributions of the remaining CP antennas were assessed using both Inline graphic and Inline graphic cells, which showed comparable results to those stated in Fig. 15. Furthermore, exploring this work’s prerequisites, only the most relevant MIMO and MTM combinations have been explained out of the numerous feasible possibilities.

graphic file with name d33e3642.gif 16
graphic file with name d33e3648.gif 17
graphic file with name d33e3654.gif 18
graphic file with name d33e3660.gif 19
graphic file with name d33e3769.gif 20

The Inline graphic and Inline graphic curves for the three scenarios–without any MTM, with Inline graphic, and with Inline graphic–have been examined in order to gain a better understanding of the isolation mechanism. In the 6 GHz band, the MIMO antenna without MTM enabled I-BW Inline graphic 0.3 GHz and Inline graphic Inline graphic −36 dB, as portrayed in Fig. 15f. The introduction of Inline graphic realized Inline graphic Inline graphic −45 dB, without altering the I-BW, as depicted in Fig. 15g. Furthermore, the addition of Inline graphic contributed to improvements in both I-BW and Inline graphic values to Inline graphic 0.4 GHz and Inline graphic −39 dB, respectively, as apparent in Fig. 15h.

Measurement results

The simulated and measured results of Inline graphic are portrayed in Fig. 16. The measured Inline graphic curve indicates that a filtered −10 dB I-BW from 5.5–6.1 GHz was established, as shown in Fig. 16a. The measured results presented in Fig. 16b affirm that Inline graphic of Inline graphic40 dB was yielded, representing high isolation between ports Inline graphic and Inline graphic. The measured 3 dB AR-BW and −10 dB I-BW corresponds to each other with relative BW of 8.84%, as displayed in Fig. 16c. A reasonable peak G of 6.4 dBic was noticed during measurements with average G of Inline graphic4 dBic across the operational BW, as apparent in Fig. 16d. The measured RP of port Inline graphic in Inline graphic Inline graphic Inline graphic and Inline graphic Inline graphic Inline graphic planes at 6 GHz are depicted in Fig. 16e, f, respectively. In both planes, stable quasi-omnidirectional RPs were confirmed. Inline graphic’s suitability under CP standards was guaranteed by Inline graphic20 dB difference between co-polar, right hand (RHCP) and Inline graphic-polar, left hand (LHCP) fields. Figure 16g exemplifies that the measured total power radiated within the operation BW ranged from 50 to 65%. The performance of Inline graphic was further supported by the measurements of ECC and DG. Figure 16h demonstrates that ECC of <0.2 was measured, indicating that there was nearly no correlation between the two antennas. Furthermore, the measured DG of Inline graphic is plotted in Fig. 16i. In MIMO antennas, DG constitutes an important measure that relies on a number of factors, for instance elevation angle, frequency, and spatial separation, among others. With DG of Inline graphic10 dB over the operating BW, Inline graphic demonstrates the device’s outstanding reliability. The general decline in I-BW was caused by the restricted bandwidth of square ring Inline graphic and the reduced strength of primary currents on the main radiating segments due to the partial ground plane. The aforementioned along with notable G values may be regarded as important contributions of Inline graphic because these antenna KPI are essential for IoT use cases.

Figure 16.

Figure 16

Proposed CP Inline graphic antenna. Layout: Inline graphic; Inline graphic; Inline graphic. Simulated and measured results: (a) Inline graphic; (b) Inline graphic; (c) AR; (d) G; (e) Inline graphic Inline graphic Inline graphic and (f) Inline graphic Inline graphic Inline graphic RP at 6 GHz; (g) Inline graphic; (h) ECC; (i) DG.

Figure 17 shows the simulated and measured results of Inline graphic. Referring to the measured Inline graphic trajectory, as illustrated in Fig. 17a, −10 dB I-BW of 33.01% was established. A peak Inline graphic of −56 dB was obtained, indicating low mutual coupling between ports Inline graphic and Inline graphic, according to the measured results shown in Fig. 17b. The measured values of AR that remained <3 dB are provided in Fig. 17c. The measurements revealed a high peak G of 7.1 dBic, as indicated in Fig. 17d. The measured RP of port Inline graphic in Inline graphic Inline graphic Inline graphic and Inline graphic Inline graphic Inline graphic planes at 6 GHz are manifested in Fig. 17e, f, respectively. The appropriateness of Inline graphic under CP regulations was proven by steady quasi-omnidirectional RPs in both planes, exhibiting a Inline graphic20 dB difference between RHCP and LHCP RPs. There was a slight overlap between RHCP and LHCP RPs near Inline graphic and Inline graphic because only one shorting pin could be soldered to the partial ground plane, and the substrate’s remaining holes were left unfilled, resulting in reflection and diffraction. The maximum measured Inline graphic was 87%, as shown in Fig. 17g. The measured ECC and DG performance are displayed in Fig. 17h, i, respectively. The remarkable reliability of Inline graphic was demonstrated by the recording of ECC of <0.2 and DG of Inline graphic10 dB over the operating BW. Although Inline graphic had similar radiating elements to Inline graphic, their I-BW, G, and Inline graphic performances were greatly improved. This was due to the shorting pin Inline graphic configuration, which featured wide EBG characteristics. Furthermore, because of the partial ground arrangement, only one shorting pin could be integrated, resulting in ground plane currents flowing towards the main radiator. Ultimately, the overall signal strength of the radiating components was improved. Thus, Inline graphic remains an excellent choice for XR use cases that need high G and enhanced Inline graphic performance of antennas.

Figure 17.

Figure 17

Proposed CP Inline graphic antenna. Layout: Inline graphic; Inline graphic; Inline graphic. Simulated and measured results: (a) Inline graphic; (b) Inline graphic; (c) AR; (d) G; (e) Inline graphic Inline graphic Inline graphic and (f) Inline graphic Inline graphic Inline graphic RP at 6 GHz; (g) Inline graphic; (h) ECC; (i) DG.

The simulated and measured results of Inline graphic are provided in Fig. 18. The measured Inline graphic versus frequency curves displayed in Fig. 18a proves that an appropriate −10 dB impedance matching at 6 GHz with I-BW of 31.64% was realized. Figure 18b shows the measured Inline graphic results, which confirms that a peak Inline graphic of −48 dB was established, signifying reasonable isolation between port Inline graphic and port Inline graphic. The variations in AR against frequency are shown in Fig. 18c. Within the operating spectrum, the measured AR was Inline graphic3 dB. Furthermore, a peak measured G of 4.7 dBic was yielded, as indicated in Fig. 18d. The quasi-omnidirectional operation of Inline graphic at 6 GHz has been substantiated by a comparison of simulated and measured RP of port Inline graphic in Inline graphic Inline graphic Inline graphic and Inline graphic Inline graphic Inline graphic planes, as shown in Fig. 18e, f, respectively. The direction of maximum radiation was tilted from the broadside direction to Inline graphic Inline graphicorientation in Inline graphic Inline graphic Inline graphic plane by the caged slot layouts on the ground plane close to both radiating segments. Furthermore, in Inline graphic Inline graphic Inline graphic plane, a minor overlap of LHCP and RHCP fields was noticed near Inline graphic and Inline graphic angles. Similar effects were observed in Inline graphic Inline graphic Inline graphic plane, with subtle distortion in RP at a few angles. These impacts have been associated to the coupling of the ground currents towards the radiators. However, at remaining angles, the difference between LHCP and RHCP values were well within the range of Inline graphic20 dB, indicating noteworthy CP functionality. This ultimately confirms the feasibility of tolerable radiation performance. The measured Inline graphic, ECC, and DG performance are demonstrated in Fig. 18g–i, respectively. Excellent Inline graphic of 94%, ECC of <0.2, and DG of Inline graphic10 dB over the operating BW was corroborated. These established antenna KPI, with a main contribution in substantial Inline graphic, reveal that Inline graphic meets the requirements of AI-based robot use cases, which often require high Inline graphic antennas.

Figure 18.

Figure 18

Proposed CP Inline graphic antenna. Layout: Inline graphic; Inline graphic; Inline graphic. Simulated and measured results: (a) Inline graphic; (b) Inline graphic; (c) AR; (d) G; (e) Inline graphic Inline graphic Inline graphic and (f) Inline graphic Inline graphic Inline graphic RP at 6 GHz; (g) Inline graphic; (h) ECC; (i) DG.

Figure 19 demonstrates the simulated and measured results of Inline graphic. A −10 dB I-BW of 29.01% was established in the 6 GHz band, as shown by the measured Inline graphic curves in Fig. 19a. Low mutual coupling between ports Inline graphic and Inline graphic with a peak Inline graphic of −45 dB was accomplished, evidenced by the measured results in Fig. 19b. The measured values of AR stayed <3 dB, as shown in Fig. 19c. A fairly significant peak G of 5.8 dBic became apparent in the measurements, which is illustrated in Fig. 19d. The measured RP of port Inline graphic in Inline graphic Inline graphic Inline graphic and Inline graphic Inline graphic Inline graphic planes at 6 GHz are conveyed in Fig. 19e, f, respectively. Stable quasi-omnidirectional RPs across the two fundamental planes with Inline graphic20 dB difference between RHCP and LHCP fields demonstrated the suitability of Inline graphic according to CP norms. The highest measured Inline graphic was 76%, as Fig. 19g exemplifies. The measured ECC and DG performance are revelead in Fig. 19h, i, respectively. The measurement of ECC of <0.2 and DG of Inline graphic10 dB across the operational BW verified the outstanding reliability of Inline graphic. High G antennas are required for V2X use cases, and Inline graphic makes for a suitable candidate. Particularly because reasonably high G with notable CP RP performance was rendered with Inline graphic. While Inline graphic offers a relatively higher G, their CP RP does not constitute a great option for V2X use cases, where a variety of environmental conditions affect the antenna’s performance and attaining minimal overlap between RHCP and LHCP fields remain crucial.

Figure 19.

Figure 19

Proposed CP Inline graphic antenna. Layout: Inline graphic; Inline graphic; Inline graphic. Simulated and measured results: (a) Inline graphic; (b) Inline graphic; (c) AR; (d) G; (e) Inline graphic Inline graphic Inline graphic and (f) Inline graphic Inline graphic Inline graphic RP at 6 GHz; (g) Inline graphic; (h) ECC; (i) DG.

The simulated and measured results of Inline graphic are shown in Fig. 20. The measured −10 dB I-BW in the 6 GHz band was 9.69%, as portrayed in Fig. 20a. In the operating spectrum, the measured Inline graphic between ports Inline graphic and Inline graphic extended from −25 dB to −40 dB, as illustrated in Fig. 20b. The measured 3 dB AR-BW agreed with −10 dB I-BW, as displayed in Fig. 20c. In the functional BW, stable G of 4.7−5.8 dBic was measured, as revealed in Fig. 20d. The measured RP of port Inline graphic in Inline graphic Inline graphic Inline graphic and Inline graphic Inline graphic Inline graphic planes at 6 GHz exhibited steady quasi-omnidirectional RPs with Inline graphic20 dB difference between RHCP and LHCP patterns, as demonstrated in Fig. 20e, f, respectively. The measured Inline graphic ranged from 88 to 93%, as evidenced in Fig. 20g. The measured ECC was <0.2 and DG was Inline graphic10 dB, as presented in Fig. 20h, i, respectively. Overall, Inline graphic established an adequate MIMO antenna KPI, with high Inline graphic and narrow I-BW/AR-BW being their key characteristics, which are essential for UAV use cases.

Figure 20.

Figure 20

Proposed CP Inline graphic antenna. Layout: Inline graphic; Inline graphic; Inline graphic. Simulated and measured results: (a) Inline graphic; (b) Inline graphic; (c) AR; (d) G; (e) Inline graphic Inline graphic Inline graphic and (f) Inline graphic Inline graphic Inline graphic RP at 6 GHz; (g) Inline graphic; (h) ECC; (i) DG.

The simulated and measured results of Inline graphic are displayed in Fig. 21. Measurements proved −10 dB I-BW from 4.42–8.24 GHz, covering the entire 6 GHz band, as shown in Fig. 21a. Notable peak and average Inline graphic values of, respectively, −40 dB and Inline graphic20 dB were measured between ports Inline graphic and Inline graphic, as evidenced in Fig. 21b. In the operating BW, AR of <3 dB and G of Inline graphic4 dBic were measured, as shown in Fig. 21c, d, respectively. Typically, AR-BW involves intricate design elements that degrades CP antenna performance. By exploiting apertures on the ground plane at strategic locations along with the Inline graphic-based EBG structure, the current distribution on Inline graphic radiating elements were modified. Particularly, the meandered and crescent axed segments governed the stronger currents, and the disparity between the distribution of two orthogonal currents yielded a wide AR-BW of 60.63%, which represents a significant contribution of Inline graphic. The measured RP of port Inline graphic in Inline graphic Inline graphic Inline graphic and Inline graphic Inline graphic Inline graphic planes at 6 GHz are presented in Fig. 21e, f, respectively. Quasi-omnidirectional RP with Inline graphic20 dB difference between RHCP and LHCP fields were measured in both planes. The measurement of reasonable Inline graphic of Inline graphic65Inline graphic, ECC of <0.2, and DG of Inline graphic10 dB in the operating BW are portrayed in Fig. 21g–i, respectively. Based on these results, Inline graphic represents a fairly competitive design that may be applied to D2D ISAC use cases.

Figure 21.

Figure 21

Proposed CP Inline graphic antenna. Layout: Inline graphic; Inline graphic; Inline graphic. Simulated and measured results: (a) Inline graphic; (b) Inline graphic; (c) AR; (d) G; (e) Inline graphic Inline graphic Inline graphic and (f) Inline graphic Inline graphic Inline graphic RP at 6 GHz; (g) Inline graphic; (h) ECC; (i) DG.

In order to further validate the MIMO performance of the proposed antennas, TARC and CCL responses have been illustrated in Fig. 22. All of the proposed antennas yielded reasonable TARC and CCL performance with Inline graphic0 and Inline graphic0.4 bps/Hz values in their operating bands, respectively. Besides, it is crucial to explain the reason behind the measured data being distorted, with certain curves not matching the simulated plots. The deterioration of the results was caused by a number of factors, including misalignment, undesirable radiations from the feed cable, SMA connector tolerances, 50Inline graphic termination resistance, hand soldering of shorting pins, and changes in the physical parameters throughout the fabrication process. Finally, the authors would like to highlight that an insignificant portion of Inline graphic antenna was presented at a high-impact scientific conference in Leuven, Belgium, in 202464.

Figure 22.

Figure 22

Simulated TARC and CCL results of the proposed CP MIMO antennas: (a) Inline graphic; (b) Inline graphic; (c) Inline graphic; (d) Inline graphic; (e) Inline graphic; (f) Inline graphic.

Benchmarking

A summary of the proposed antenna elements has been presented for the ease of understanding the design methodology in Fig. 23. Furthermore, the proposed CP MIMO antennas (Inline graphic) have been compared with state-of-the-art CP MIMO antennas in Table 2, and discussed below to highlight their novelty. The cited works substantially boost the overall antenna and MIMO performance, but they have a number of limitations that have been addressed in this work. The novelty and importance of the proposed research has been addressed in the ensuing points.

Figure 23.

Figure 23

A summary of the proposed antenna elements.

Table 2.

Performance summary of the (a) proposed and (b) state-of-the-art quasi-isotropic antennas.

Inline graphic Inline graphic Inline graphic Inline graphic Inline graphic Inline graphic Inline graphic
(a)
Layout graphic file with name 41598_2025_7208_Figa_HTML.gif graphic file with name 41598_2025_7208_Figb_HTML.gif graphic file with name 41598_2025_7208_Figc_HTML.gif graphic file with name 41598_2025_7208_Figd_HTML.gif graphic file with name 41598_2025_7208_Fige_HTML.gif graphic file with name 41598_2025_7208_Figf_HTML.gif
Size [Inline graphic] 1.1Inline graphic1.1 1.1Inline graphic1.1 1.1Inline graphic1.1 1.1Inline graphic1.1 1.1Inline graphic1.1 1.1Inline graphic1.1
Profile [Inline graphic] 0.03 0.03 0.03 0.03 0.03 0.03
Layers 2 2 2 2 2 2
Inline graphic [GHz] 6.0 6.0 6.0 6.0 6.0 6.0
I-BW [%] 8.84 33.01 31.64 29.01 9.69 60.63
AR-BW [%] 8.84 33.01 31.64 29.01 9.69 60.63
Inline graphic [dB] 40−58 31−56 24−48 21−45 25−40 21−40
G [dBic] 3.6−6.4 3.9−7.1 1.2−4.7 2.8−5.8 4.7−5.8 1.9−4.2
Inline graphic [%] 50−65 55−87 56−94 45−76 88−93 60−68
Inline graphic 202572 202473 2024 74 2023 75 2022 76 2020 77
(b)
Layout graphic file with name 41598_2025_7208_Figg_HTML.gif graphic file with name 41598_2025_7208_Figh_HTML.gif graphic file with name 41598_2025_7208_Figi_HTML.gif graphic file with name 41598_2025_7208_Figj_HTML.gif graphic file with name 41598_2025_7208_Figk_HTML.gif graphic file with name 41598_2025_7208_Figl_HTML.gif
Size [Inline graphic] 0.1Inline graphic0.2 0.2Inline graphic0.2 0.6Inline graphic0.5 0.1Inline graphic0.1 1.9Inline graphic1.9 2.0Inline graphic2.0
Profile [Inline graphic] 0.03 0.0005 0.03 0.02 0.11 0.04
Layers 2 2 2 2 >2 >2
Inline graphic [GHz] 8.9 2.5 5.6 3.5 5.8 6.2
I-BW [%] 125.8 18.9 12.5 146 8.5 6.4
AR-BW [%] 10.8 47 0.04 6.4
Inline graphic [dB] 21−25 23−31 40−67 38−52
G [dBi] Inline graphic2.2 Inline graphic2.2 3.9−4.9 7.6−10.5 6.0−8.0
Inline graphic [%] Inline graphic85 Inline graphic95 94−95 79−95
  1. Antenna layout. The polarization of antennas, LP and CP, is anticipated to play a vital role in enabling current and future applications, including but not limited to ISAC. The radiator and ground configurations presented in two patents65,66 are based on the meander lines and/or defected ground. However, both these patents described their arrangements for generating LP waves only, whereas the proposed antenna designs are suitable for realizing both LP as well as CP waves. Furthermore, the integration of varied dimensions of the meander lines (obese and thin tracks) represents a uniqueness of the proposed layouts. Particularly because the arrangement modifies the antenna’s impedance values and contributes to enabling wide AR-BW with compact size. On the other hand, the cited patents utilized meander lines with similar outlines. Besides, defected ground has been utilized to reduce the front-to-back ratio of the antenna featuring directional radiation pattern in one patent66. However, there are two significant differences between the proposed geometries and the relevant patent. First, the proposed patterns of the ground plane produces radiations that eventually lead to the formation of quasi-omnidirectional RP with notable antenna KPI, which are required for densely populated applications. Second, the proposed designs of the ground plane as well as the radiators are entirely novel in terms of configurations. Scholarly papers over the years have been explored to further explain the novelty of the proposed antenna designs. Numerous antennas with meander lines adhering to a particular impedance and/or defected ground have been researched6771. However, the benefits and drawbacks of transforming the meander line impedance have never been fully established. Therefore, based on existing patents and scholarly papers, the present research offers the first precise comprehension into the impact of altering meander line impedance on overall antenna performance.

  2. Antenna performance pros. All of the proposed antennas feature a low-profile with two planar layers, signifying feasibility for mass production with minimal fabrication complexities. Four papers7275 rendered the same, but at the cost of I-BW and/or AR-BW performance. The other two articles76,77 exhibited reasonably good G and Inline graphic values, however at the expense of complex design besides from having relatively poor I-BW and AR-BW results. Overall, the proposed antennas delivers significant Inline graphic-BW, unlike previous efforts that only exhibited notable Inline graphic for limited BW. Another important achievement of this research (Inline graphic) is the realization of AR-BW of 60.63%, which to the best of the authors’ knowledge, is the widest AR-BW ever accomplished. Finally, note that this work has been presented based on the specific requirements of the project and practical scenarios, and the proposed antennas are interchangeable for diverse use cases.

  3. Antenna performance cons. Typically, the antenna design stages include the process of striking the ideal balance between competing attributes to realize the optimum performance for a particular application. Correspondingly, the proposed antennas have design and performance trade-offs that are addressed as follows. Firstly, the entire array of unit EBG design does not follow the same pattern in Inline graphic antenna layout, eventually resulting in an imbalanced electric field around the primary radiating elements and increased cross polarization magnitudes. Secondarily, the radiation from the asymmetrical defected ground design altered the cross polarization magnitudes of the primary radiators in the Inline graphic antenna arrangement. Finally, the G deviation has been noted in a few of the proposed MIMO antennas, which may be attributed to the substantially different designs of the radiating parts, including the ground plane that operates as a radiator and the top copper elements. However, all of these drawbacks are justified because the higher cross polarization magnitudes exist for extremely limited angles, and the ratio of G divergence was Inline graphic3 dBic, making all of the proposed antennas viable for real-world applications.

Conclusion

This paper introduced six novel and lucrative printed MIMO antennas featuring quasi-isotropic CP for six different 6G uses cases–IoT, XR, AI, V2X, UAV, and D2D ISAC–in the 6 GHz band. Systematic mechanisms for concluding impedance matching, realizing CP, and reducing Inline graphic values have been described. The measurement results points strongly to the benefits of every proposed MIMO antennas. Their main highlights include notable Inline graphic-BW, wide AR-BW, and simple construction. The overall study indicates potentially scalable approaches for mm waves.

Acknowledgements

This work was developed within the “Perceptive communication networks with integrated sensors for 6th generation mobile communications (KOMSENS-6G)” project, supported by the Federal Ministry of Education and Research (BMBF), Germany under the funding code 16KISK122. The responsibility for the content of this publication lies with the authors.

Author contributions

Conceptualization, SK; Data curation, SK and PS; Formal analysis, SK; Funding acquisition, PS; Visualization, SK; Writing—original draft, SK; Writing—review and editing, SK and PS; Software and Resources, SK and PS; Supervision, PS.

Data availability

The data supporting the reported results in this study are not available due to confidentiality restrictions. However, the data generated during and/or analyzed during the current study are available from the corresponding author on reasonable request. Contact person: shahanawaz.kamal@barkhauseninstitut.org or shahanawazkamal@gmail.com.

Declarations

Competing interests

The authors declare no competing interests.

Footnotes

Publisher's note

Springer Nature remains neutral with regard to jurisdictional claims in published maps and institutional affiliations.

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Associated Data

This section collects any data citations, data availability statements, or supplementary materials included in this article.

Data Availability Statement

The data supporting the reported results in this study are not available due to confidentiality restrictions. However, the data generated during and/or analyzed during the current study are available from the corresponding author on reasonable request. Contact person: shahanawaz.kamal@barkhauseninstitut.org or shahanawazkamal@gmail.com.


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