Antenna Design · HFSS · 3 GHz

Rectangular Patch Antenna

An inset-fed 3 GHz microstrip patch developed from closed-form synthesis through full-wave tuning, near-field inspection, and far-field characterization.

HFSS rectangular patch antenna with the 3 GHz realized-gain radiation pattern overlaid on the physical model

September 3, 2026

Design3.000 GHz inset-fed patchRogers RO4350B, 50 Ω microstrip excitation
Input match−41.66 dB S11\(Z_{in}=50.82-j0.15\ \Omega\), VSWR 1.0167
Bandwidth56 MHz1.87% fractional −10 dB impedance bandwidth
Radiation6.36 dBi realized gain85.38% total efficiency, broadside main beam

1. Design Objective

The objective of this project is to design and analyze a rectangular microstrip patch antenna operating at a center frequency of 3 GHz. The antenna is designed for a 50 Ω input impedance and uses an inset-fed microstrip transmission line to provide direct impedance matching between the feed line and the radiating patch.

The initial patch dimensions are determined analytically using the transmission-line model of a rectangular microstrip antenna. These dimensions are then implemented in Ansys HFSS, where the geometry is refined through full-wave electromagnetic simulation. Patch length is adjusted to place the resonant frequency accurately, while feed position is studied to obtain the desired 50 Ω input match.

The final design is evaluated in terms of reflection coefficient, input impedance, impedance bandwidth, realized gain, radiation efficiency, and far-field radiation pattern. Surface-current and electromagnetic-field distributions are also examined to verify the expected resonant behavior of the patch.

2. Antenna Theory and Initial Design

A rectangular microstrip patch antenna consists of a conductive radiating patch separated from a ground plane by a dielectric substrate. The patch behaves approximately as a half-wavelength resonator, with radiation occurring primarily due to the fringing electric fields at the two open edges of the patch.

For the fundamental \(TM_{10}\) mode, the electric-field distribution varies mainly along the patch length. The effective electrical length is therefore approximately one-half of the guided wavelength:

\[L_{\text{eff}} \approx \frac{\lambda_g}{2}\]

where

\[\lambda_g=\frac{\lambda_0}{\sqrt{\epsilon_{\text{eff}}}}\]

and

\[\lambda_0=\frac{c}{f_0}.\]

The antenna is designed for \(f_0=3\ \mathrm{GHz}\) using Rogers RO4350B with \(\epsilon_r=3.48\) and substrate thickness \(h=1.52\ \mathrm{mm}\).

2.1 Initial Patch Width

The initial patch width is estimated using

\[W=\frac{c}{2f_0}\sqrt{\frac{2}{\epsilon_r+1}}.\]

This expression is based on the half-wavelength behavior of the patch, modified to account for dielectric loading. The width is chosen to provide suitable radiation conductance and efficiency for the dominant mode.

Using \(c\approx3\times10^8\ \mathrm{m/s}\),

\[W=\frac{3\times10^8}{2(3\times10^9)}\sqrt{\frac{2}{3.48+1}},\]

which gives

\[\boxed{W\approx33.4\ \mathrm{mm}}.\]

2.2 Effective Dielectric Constant

The electromagnetic fields of a microstrip structure are not confined entirely within the dielectric substrate. Part of the field exists within the substrate, while part extends into the surrounding air. The propagating wave therefore experiences an effective dielectric constant satisfying

\[1<\epsilon_{\text{eff}}<\epsilon_r.\]

A commonly used approximation is

\[\epsilon_{\text{eff}}=\frac{\epsilon_r+1}{2}+\frac{\epsilon_r-1}{2}\left(1+\frac{12h}{W}\right)^{-1/2}.\]

This relation comes from quasi-TEM microstrip transmission-line models and approximates the effect of electromagnetic-field energy being distributed between the dielectric and air. Substituting the selected parameters gives

\[\boxed{\epsilon_{\text{eff}}\approx3.237}.\]

2.3 Fringing-Field Correction

The patch does not behave as an ideal cavity with perfectly confined fields. At the two open ends, the electric field extends beyond the physical conductor, making the patch appear electrically longer than its physical length.

The additional effective length at each end is approximated by

\[\frac{\Delta L}{h}=0.412\frac{(\epsilon_{\text{eff}}+0.3)\left(\frac{W}{h}+0.264\right)}{(\epsilon_{\text{eff}}-0.258)\left(\frac{W}{h}+0.8\right)}.\]

This is a semi-empirical microstrip approximation rather than a direct closed-form solution of Maxwell's equations. For the selected geometry,

\[\boxed{\Delta L\approx0.726\ \mathrm{mm}}.\]

2.4 Patch Length

Ignoring fringing fields, the resonant length would approximately correspond to one-half of the guided wavelength:

\[L_{\text{eff}}=\frac{c}{2f_0\sqrt{\epsilon_{\text{eff}}}}.\]

Using the calculated effective dielectric constant,

\[L_{\text{eff}}=\frac{3\times10^8}{2(3\times10^9)\sqrt{3.237}}\approx27.77\ \mathrm{mm}.\]

Because fringing fields extend the electrical length by approximately \(\Delta L\) at each end,

\[L=L_{\text{eff}}-2\Delta L,\]

and therefore

\[\boxed{L\approx26.32\ \mathrm{mm}}.\]
ParameterInitial Value
Target frequency, \(f_0\)3.00 GHz
Relative permittivity, \(\epsilon_r\)3.48
Substrate thickness, \(h\)1.52 mm
Effective dielectric constant, \(\epsilon_{\text{eff}}\)3.237
Patch width, \(W\)33.4 mm
Effective patch length, \(L_{\text{eff}}\)27.77 mm
Fringing extension, \(\Delta L\)0.726 mm
Physical patch length, \(L\)26.32 mm

These values provide an analytical starting point rather than final antenna dimensions. Full-wave simulation is used to determine the actual resonant frequency and refine the physical geometry.

3. HFSS Model and Initial Full-Wave Simulation

The analytically calculated patch dimensions were transferred to Ansys HFSS for full-wave electromagnetic simulation. The purpose of the initial model was to evaluate how closely the closed-form design equations predicted the behavior of the complete physical antenna before numerical optimization.

The antenna was modeled as an inset-fed rectangular copper patch fabricated on Rogers RO4350B. The initial analytical dimensions were retained without modification:

\[W_p=33.40\ \mathrm{mm},\qquad L_p=26.32\ \mathrm{mm}.\]

The substrate parameters were \(\epsilon_r=3.48\), \(\tan\delta=0.0037\), and \(h=1.52\ \mathrm{mm}\). A copper thickness of \(t_{\text{Cu}}=0.035\ \mathrm{mm}\) was used for both the patch/feed conductor and ground plane.

3.1 Inset-Fed Geometry

The patch was excited using a 50 Ω microstrip feed line extending from the edge of the substrate into a rectangular inset cut into the radiating patch. The initial feed width was \(W_f=3.48\ \mathrm{mm}\), corresponding approximately to a 50 Ω microstrip line on the selected substrate. An initial inset depth of \(L_{\text{inset}}=9.50\ \mathrm{mm}\) was used, with \(G_{\text{notch}}=0.50\ \mathrm{mm}\) clearance between each side of the feed line and the surrounding patch conductor.

Parameterized HFSS model of the inset-fed rectangular patch antenna
Figure 3.1. Parameterized HFSS model of the 3 GHz inset-fed rectangular patch antenna, showing the copper patch, microstrip feed, dielectric substrate, and ground plane.

3.2 Excitation and Boundary Conditions

The antenna was excited using a 50 Ω lumped port positioned at the outer end of the microstrip feed. The port sheet extended vertically between the feed conductor and ground plane, with the integration line directed from ground toward the signal conductor.

The antenna was surrounded by an air region terminated with a radiation boundary. The boundary spacing was selected as approximately one-quarter of the free-space wavelength at the design frequency:

\[d_{\text{rad}}\approx\frac{\lambda_0}{4}.\]

At 3 GHz, \(\lambda_0\approx100\ \mathrm{mm}\), giving \(d_{\text{rad}}\approx25\ \mathrm{mm}\).

3.3 Simulation Setup

The HFSS solution was configured using the Driven Modal solver with an adaptive solution frequency of \(f_{\text{adapt}}=3\ \mathrm{GHz}\). The adaptive convergence criterion was \(\Delta S_{\max}=0.02\), with a maximum of 15 adaptive passes and two converged passes required. The reflection coefficient was evaluated over 2–4 GHz, and an infinite-sphere far-field setup was included for later gain and radiation-pattern extraction.

3.4 Initial Simulation Result

The first simulation used the analytical dimensions and initial inset-feed geometry without full-wave tuning.

Initial HFSS S11 response of the analytically sized patch antenna
Figure 3.2. Initial HFSS reflection coefficient of the analytically designed patch antenna. The dominant resonance occurs at approximately 2.888 GHz with a minimum \(S_{11}\) of approximately −18.4 dB.

The initial resonance occurred at

\[\boxed{f_{r,\text{initial}}=2.888\ \mathrm{GHz}}\]

with

\[\boxed{S_{11,\min}=-18.4\ \mathrm{dB}}.\]

The resonance was therefore 112 MHz below the intended 3 GHz operating frequency, corresponding to an error of approximately 3.7%. The result indicated that the full-wave antenna was electrically longer than required, motivating a controlled patch-length sweep.

4. Resonant Frequency Optimization

For the dominant \(TM_{10}\) mode, resonant frequency is primarily controlled by the electrical length of the patch:

\[f_r\approx\frac{c}{2L_{\text{eff}}\sqrt{\epsilon_{\text{eff}}}},\qquad L_p\downarrow\Rightarrow f_r\uparrow.\]

Because the initial resonance occurred below 3 GHz, a parametric sweep of \(L_p\) was performed while substrate, feed width, inset depth, and all other dimensions were held constant.

4.1 Patch-Length Sweep

HFSS resonant-frequency sweep versus patch length
Figure 4.1. Simulated resonant frequency as a function of patch length. Reducing the patch length shifts the fundamental resonance upward in frequency, consistent with half-wavelength resonator behavior.

The sweep identified \(L_p=25.50\ \mathrm{mm}\) as the geometry that places the resonance at \(3.000\ \mathrm{GHz}\). Compared with the analytical starting value, the required adjustment was

\[\Delta L_p=26.32-25.50=0.82\ \mathrm{mm},\]

or approximately

\[\boxed{3.1\%}\]

of the analytical length.

4.2 Verification of the Optimized Patch Length

S11 response after optimizing patch length to 25.50 mm
Figure 4.2. Simulated reflection coefficient after optimizing the patch length to 25.50 mm. The antenna resonates at 3.000 GHz with a minimum \(S_{11}\) of approximately −41.66 dB.

The optimized geometry produced

\[\boxed{f_r=3.000\ \mathrm{GHz}},\qquad \boxed{S_{11,\min}=-41.66\ \mathrm{dB}}.\]

Changing patch length also improved the input match substantially. Although patch length primarily controls resonance, geometry and feed impedance are coupled; in this case the corrected resonant length also placed the existing inset feed very close to its optimum matching condition.

5. Feed Position and Impedance Matching

With \(L_p=25.50\ \mathrm{mm}\) fixed, the inset depth was swept from 7.5 mm to 11.5 mm in 0.5 mm increments. No further optimization was strictly required—the existing 9.5 mm inset already produced an excellent match—but the sweep was used as a sensitivity study to show how feed location controls the input impedance.

5.1 Effect of Inset Depth on Reflection Coefficient

HFSS S11 response for the inset-depth sweep
Figure 5.1. Simulated \(S_{11}\) response for inset depths from 7.5 mm to 11.5 mm with the optimized patch length held constant at 25.50 mm.
S11 at 3 GHz versus inset depth
Figure 5.2. Reflection coefficient at 3 GHz as a function of inset depth. The strongest match occurs at an inset depth of 9.5 mm.

The strongest matching condition occurs at

\[\boxed{L_{\text{inset}}=9.5\ \mathrm{mm}},\qquad \boxed{S_{11}(3\ \mathrm{GHz})=-41.66\ \mathrm{dB}}.\]

5.2 Input-Impedance Variation

For a 50 Ω source, the desired antenna impedance at the design frequency is \(Z_{\text{in}}\approx50+j0\ \Omega\).

Real and imaginary antenna input impedance at 3 GHz versus inset depth
Figure 5.3. Real and imaginary components of the antenna input impedance at 3 GHz as a function of inset depth.

Near \(L_{\text{inset}}=9.5\ \mathrm{mm}\), the real component approaches 50 Ω while the reactive component approaches zero. This directly explains the deep \(S_{11}\) minimum and demonstrates the inset feed as an impedance-matching mechanism.

5.3 Coupling Between Feed Position and Resonant Frequency

Resonant frequency versus inset depth
Figure 5.4. Simulated resonant frequency as a function of inset depth with patch length fixed at 25.50 mm.

Across the sweep, resonance shifts only from roughly 3.013 GHz to 2.963 GHz—about 50 MHz or 1.7% of the design frequency—while the matching response changes much more strongly. The result supports the practical interpretation that patch length primarily controls resonance and inset depth primarily controls matching, while also showing that the two effects are not perfectly independent.

6. Final Input Performance

Following the patch-length and inset-depth studies, the final geometry was evaluated in terms of reflection coefficient, impedance bandwidth, Smith-chart response, input impedance, and VSWR.

6.1 Reflection Coefficient and Impedance Bandwidth

Final S11 response and minus 10 dB bandwidth
Figure 6.1. Final reflection coefficient of the optimized antenna, showing the 3 GHz resonance and the lower and upper −10 dB impedance-bandwidth limits.

The −10 dB crossings are \(f_L=2.972\ \mathrm{GHz}\) and \(f_H=3.028\ \mathrm{GHz}\). Therefore,

\[BW=f_H-f_L=56\ \mathrm{MHz}\]

and

\[\boxed{FBW=\frac{56\ \mathrm{MHz}}{3\ \mathrm{GHz}}\times100\%\approx1.87\%}.\]

6.2 Smith-Chart Response

Smith chart of the final antenna design near 3 GHz
Figure 6.2. Smith-chart response of the final antenna design around the 3 GHz operating region. The 3 GHz point lies close to the center of the chart, indicating a near-50 Ω resistive input impedance.

At 3 GHz, the normalized impedance is approximately \(z_{\text{in}}=1.0164-j0.0030\). With 50 Ω normalization,

\[Z_{\text{in}}=50(1.0164-j0.0030)\approx50.82-j0.15\ \Omega.\]

6.3 Input Impedance

Real and imaginary input impedance versus frequency
Figure 6.3. Real and imaginary components of antenna input impedance versus frequency. At 3 GHz, the resistance is approximately 50.82 Ω while the reactance is close to zero.

At the design frequency, HFSS gives

\[\boxed{Z_{\text{in}}(3\ \mathrm{GHz})\approx50.82-j0.15\ \Omega}.\]

6.4 Voltage Standing Wave Ratio

VSWR versus frequency around the 3 GHz design point
Figure 6.4. Voltage standing wave ratio of the optimized antenna around the 3 GHz operating frequency. The minimum VSWR is approximately 1.017 at resonance.

At 3 GHz,

\[\boxed{\mathrm{VSWR}=1.0167}.\]
MetricFinal Result
Resonant frequency3.000 GHz
Minimum \(S_{11}\)−41.66 dB
Lower −10 dB frequency2.972 GHz
Upper −10 dB frequency3.028 GHz
−10 dB bandwidth56 MHz
Fractional bandwidth1.87%
Input impedance at 3 GHz\(50.82-j0.15\ \Omega\)
VSWR at 3 GHz1.0167

7. Surface Current and Field Distribution

The input-response results confirm that the antenna is resonant and well matched at 3 GHz, but S-parameters alone do not show how electromagnetic fields are distributed across the structure. Surface current and electric field were therefore examined at the design frequency to verify the expected patch behavior.

7.1 Surface Current Distribution

Surface current magnitude on the patch and feed at 3 GHz
Figure 7.1. Surface-current magnitude of the optimized antenna at 3 GHz. The field display is scaled logarithmically to reveal both localized current concentrations and lower-level current distribution across the patch; the simulated localized maximum is approximately 51.6 A/m.

Strong current is visible along the microstrip feed and around the inset transition, where power transfers into the radiating patch. The current then spreads over the patch and forms the distributed pattern associated with the resonant antenna mode. Localized edge currents dominate the absolute maximum, while the broader current distribution illustrates the standing-wave nature of the structure.

7.2 Electric Field Magnitude

Electric field magnitude on a longitudinal XZ cut plane at 3 GHz
Figure 7.2. Electric-field magnitude in the longitudinal XZ plane at 3 GHz. A logarithmic display scale reveals both strong localized fields near the antenna and weaker fields extending into the surrounding air.

Strong fields occur near the feed/inset discontinuity and the open regions of the resonant patch. A significant portion of the field extends into the air rather than remaining confined to the dielectric; this fringing-field behavior is the mechanism responsible for radiation from the microstrip patch.

7.3 Electric Field Direction

Electric field vectors on the longitudinal XZ cut plane at 3 GHz
Figure 7.3. Electric-field vector distribution in the longitudinal XZ plane at 3 GHz, showing field closure between patch and ground and fringing into the surrounding air near the open patch regions.

The vector representation shows the instantaneous field direction at the selected phase. Within the microstrip structure, the field couples between patch and ground; near open patch regions, the vectors bend outward into air. A 180° phase shift would reverse the displayed vector directions without changing the field-magnitude distribution or radiation behavior.

7.4 Verification of Resonant Patch Behavior

Taken together, the current and field results show current delivery through the inset-fed line, distributed resonant current across the patch, field coupling to the ground plane, and fringing fields extending into air. These characteristics are consistent with operation in the intended fundamental \(TM_{10}\)-type mode and confirm that the 3 GHz port resonance corresponds to the expected physical antenna behavior.

8. Far-Field Radiation Performance

After verifying the input match and near-field behavior, the far-field radiation characteristics were evaluated at 3 GHz. Realized gain was used as the primary radiation metric because it includes both antenna loss and input mismatch:

\[G_{\text{realized}}=(1-|\Gamma|^2)G,\qquad \Gamma=S_{11}.\]

Because \(S_{11}\approx-41.7\ \mathrm{dB}\) at 3 GHz, mismatch loss is negligible and realized gain is almost identical to conventional gain.

8.1 Three-Dimensional Radiation Pattern

Three-dimensional realized gain pattern overlaid on the final patch antenna
Figure 8.1. Three-dimensional realized-gain pattern overlaid on the optimized patch antenna at 3 GHz. A local coordinate system centered on the patch is used for visualization.
Standalone 3D total realized gain pattern at 3 GHz
Figure 8.2. Three-dimensional total realized-gain pattern of the optimized antenna at 3 GHz.

The dominant radiation is directed normal to the patch along approximately +Z, giving the expected broadside pattern. The maximum realized gain is

\[\boxed{G_{\text{realized,max}}=6.36\ \mathrm{dBi}}.\]

Back radiation is substantially lower because of the ground plane, though finite substrate and ground dimensions allow a smaller rear lobe.

8.2 E-Plane Radiation Pattern

E-plane total realized gain polar pattern at 3 GHz
Figure 8.3. E-plane total realized-gain pattern of the optimized patch antenna at 3 GHz.

The E-plane pattern exhibits a broad main lobe centered approximately at \(\theta=0^\circ\), corresponding to radiation normal to the patch surface. Forward/backward asymmetry is expected because the complete model includes the inset feed and finite substrate and ground plane.

8.3 H-Plane Radiation Pattern

H-plane total realized gain polar pattern at 3 GHz
Figure 8.4. H-plane total realized-gain pattern of the optimized patch antenna at 3 GHz.

The orthogonal H-plane cut also shows a broad main beam along +Z. The E- and H-plane shapes differ because the patch dimensions and field distributions differ along their two principal axes.

8.4 Directivity, Gain, and Realized Gain

Directivity and gain were extracted from the HFSS far-field solution associated with Infinite Sphere1 at 3 GHz. For directivity, a report used the total-directivity quantity DirTotal with the expression max(dB(DirTotal)). The maximum was evaluated over elevation angle \(\theta\) for each azimuth \(\phi\), and the global maximum was identified using an HFSS marker.

This produced

\[\boxed{D_{\max}=7.04\ \mathrm{dBi}}\]

with a more precise value of 7.0423 dBi.

The same method was used for conventional gain, replacing DirTotal with GainTotal and evaluating max(dB(GainTotal)). The peak gain was

\[\boxed{G_{\max}=6.36\ \mathrm{dBi}}\]

or 6.3564 dBi. The realized-gain maximum was extracted from dB(RealizedGainTotal) in the 3D pattern, giving 6.3559 dBi.

The difference between gain and realized gain is below 0.001 dB, so input mismatch contributes essentially no additional loss at 3 GHz. The approximately 0.68 dB difference between directivity and gain results primarily from conductor and dielectric losses.

8.5 Radiation and Total Efficiency

Radiation and total efficiency were extracted directly from HFSS Antenna Parameters at 3 GHz. RadiationEfficiency and TotalEfficiency are dimensionless ratios, so the report expressions 100*RadiationEfficiency and 100*TotalEfficiency were used to display percentage values.

HFSS reported

\[\boxed{\eta_{\text{rad}}=85.39\%},\qquad \boxed{\eta_{\text{total}}=85.38\%}.\]

As a consistency check, radiation efficiency can also be computed from gain and directivity:

\[\eta_{\text{rad}}=10^{(G-D)/10}=10^{(6.3564-7.0423)/10}\approx0.854,\]

which agrees closely with the HFSS value. Total efficiency includes mismatch loss:

\[\eta_{\text{total}}=\eta_{\text{rad}}(1-|\Gamma|^2).\]
MetricResult
Operating frequency3.000 GHz
Peak directivity7.04 dBi
Peak gain6.36 dBi
Peak realized gain6.36 dBi
Radiation efficiency85.39%
Total efficiency85.38%
Primary radiation directionBroadside, approximately +Z

9. Analytical and Full-Wave Design Comparison

The final stage compares the initial closed-form dimensions with the geometry obtained after full-wave tuning. The analytical design produced \(W_p=33.40\ \mathrm{mm}\) and \(L_p=26.32\ \mathrm{mm}\). The final HFSS patch length was \(25.50\ \mathrm{mm}\), a correction of

\[\Delta L_p=25.50-26.32=-0.82\ \mathrm{mm}\]

or approximately

\[\boxed{-3.12\%}.\]

The initial full-wave resonance was 2.888 GHz, 3.73% below target. After the 3.1% reduction in physical patch length, resonance shifted to 3.000 GHz, consistent with the approximate relationship \(f_r\propto1/L_{\text{eff}}\).

9.1 Initial and Final Reflection Response

Initial and final S11 reflection coefficient comparison
Figure 9.1. Initial and final reflection-coefficient responses. Reducing the patch length from 26.32 mm to 25.50 mm shifts the dominant resonance upward toward the 3 GHz design frequency while simultaneously improving the input match.

The final antenna reaches \(S_{11}(3\ \mathrm{GHz})\approx-41.66\ \mathrm{dB}\), compared with approximately −18.4 dB for the analytical starting geometry at its original resonance. The feed-position study subsequently confirmed that the original 9.5 mm inset was already close to the optimum matching location.

9.2 Analytical and Final Design Summary

ParameterAnalytical / Initial DesignFinal HFSS DesignChange
Patch width \(W_p\)33.40 mm33.40 mm0%
Patch length \(L_p\)26.32 mm25.50 mm−3.12%
Inset depth \(L_{\text{inset}}\)9.50 mm9.50 mm0%
Resonant frequency2.888 GHz3.000 GHz+112 MHz
Minimum \(S_{11}\)−18.4 dB−41.66 dBImproved
Input impedance at 3 GHz\(50.82-j0.15\ \Omega\)
−10 dB bandwidth56 MHz
Peak realized gain6.36 dBi
Total efficiency85.38%
Design workflow: analytical sizing → full-wave validation → parameter sensitivity → final tuning.

Rather than replacing the analytical model, HFSS refined it. Only a modest geometric correction was required to achieve the final 3 GHz antenna response.

10. Final Design Summary

The completed design combines the analytical synthesis, full-wave tuning, impedance-matching study, near-field inspection, and far-field characterization into one final geometry.

Final top view of the optimized inset-fed rectangular patch antenna
Figure 10.1. Final top-view geometry of the optimized inset-fed rectangular patch antenna.

10.1 Final Geometrical Parameters

ParameterFinal Value
Design frequency3.000 GHz
SubstrateRogers RO4350B
Relative permittivity, \(\epsilon_r\)3.48
Loss tangent, \(\tan\delta\)0.0037
Substrate thickness, \(h\)1.52 mm
Copper thickness, \(t_{\text{Cu}}\)0.035 mm
Patch width, \(W_p\)33.40 mm
Patch length, \(L_p\)25.50 mm
Feed width, \(W_f\)3.48 mm
Inset depth, \(L_{\text{inset}}\)9.50 mm
Inset side gap, \(G_{\text{notch}}\)0.50 mm

10.2 Final Input Performance

MetricFinal Result
Resonant frequency3.000 GHz
Minimum \(S_{11}\)−41.66 dB
Input impedance at 3 GHz\(50.82-j0.15\ \Omega\)
VSWR at 3 GHz1.0167
Lower −10 dB frequency2.972 GHz
Upper −10 dB frequency3.028 GHz
−10 dB bandwidth56 MHz
Fractional bandwidth1.87%

10.3 Final Radiation Performance

MetricFinal Result
Peak directivity7.04 dBi
Peak gain6.36 dBi
Peak realized gain6.36 dBi
Radiation efficiency85.39%
Total efficiency85.38%
Main radiation directionBroadside, approximately +Z

10.4 Overall Design Outcome

The final antenna meets the original 3 GHz inset-fed patch objective. The project demonstrates that analytical formulas provide a strong starting point, full-wave EM simulation is needed to refine physical resonant dimensions, patch length is the dominant resonance-tuning variable, inset depth is the dominant impedance-matching variable, near-field inspection verifies the expected current and fringing behavior, and far-field analysis confirms the expected broadside radiation pattern.

11. Conclusion and Future Work

This project developed a 3 GHz rectangular inset-fed microstrip patch antenna from analytical synthesis through full-wave electromagnetic validation in HFSS.

The analytical geometry initially resonated at 2.888 GHz, about 3.7% below the target. Reducing the patch length from 26.32 mm to 25.50 mm shifted the resonance to 3.000 GHz. The final 9.50 mm inset depth produced \(Z_{\text{in}}\approx50.82-j0.15\ \Omega\), \(S_{11}\approx-41.66\ \mathrm{dB}\), and VSWR ≈ 1.017. The final −10 dB impedance bandwidth was 56 MHz, corresponding to 1.87% fractional bandwidth.

Near-field analysis connected the port response to the antenna physics: surface current spread from the inset-fed line into the patch, and electric-field magnitude/vector plots showed the standing-wave and fringing-field behavior associated with radiation. The far-field response exhibited the expected broadside pattern, with 7.04 dBi peak directivity, 6.36 dBi peak realized gain, and 85.38% total efficiency.

Overall, the project demonstrates the complementary roles of analytical antenna theory and full-wave electromagnetic simulation. Closed-form equations provided an effective starting point, while HFSS captured finite geometry, feed discontinuity, material loss, and the full electromagnetic field distribution of the physical antenna.

Future Work

Fabrication and measurement of a physical prototype would provide the most useful next validation step. Measured \(S_{11}\), gain, and radiation patterns could be compared directly with HFSS predictions, including the effects of manufacturing tolerances, connector launches, substrate-property variation, and measurement fixtures.

A tolerance study could quantify the sensitivity of patch length, inset depth, feed width, and substrate thickness. Bandwidth-enhancement techniques—such as thicker or lower-permittivity substrates, stacked patches, slots, parasitic elements, or alternative feeds—could also be explored, together with cross-polarization and front-to-back-ratio characterization.

Finally, the same workflow could be extended to additional antenna types and topologies, including circular patches, slot antennas, monopoles, dipoles, PIFA structures, broadband printed antennas, and eventually antenna arrays. Comparing these designs would broaden the study of how antenna geometry controls impedance, polarization, bandwidth, gain, and radiation pattern while building on the HFSS modeling and post-processing workflow developed here.