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**Two-Dimensional Topology Optimization of a Horn Antenna** ()

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*Open Journal of Optimization*,

**9**, 39-46. doi: 10.4236/ojop.2020.93004.

1. Introduction

Antennas are devices acting as a transition between the free space and the power source [1] [2]. They play an important role in wireless communication, where these devices transmit and receive signals from afar. In their long history, many types of antennas have been developed and constructed over nearly a century [3] - [8]. Among them, horn antennas are built to achieve high gain in frequencies above very high frequency.

Topology optimization is a method that optimizes material layout within a given design space, under a set of constraints. In order to generate the optimal topologies, microstructures, composites of material and void, are employed to form the domain. Therefore, the topology optimization problem in fact turns into a material distribution problem, whose calculation requires considerably less computing costs. Typical algorithm employed is either gradient-based methods such as the optimality criteria algorithm and the method of moving asymptotes (MMA) or non-gradient-based algorithms such as particle swarm or genetic algorithms. Topology optimization has a wide range of applications in aerospace, mechanical, bio-chemical and civil engineering [9] [10].

In this work, we adopt topology optimization method for designing a two-dimensional horn antenna.

Optimization results show that a highly directive antenna with non-intuitive materials distribution can be obtained with this powerful method, opening new ways for future antenna design.

2. Background and Model Definition

In electromagnetics, Maxwell’s equations govern. Together with proper boundary conditions, the radiation pattern of antennas can be solved.

The simulation implemented in this paper seeks to find an optimal material distribution for a two-dimensional horn antenna in order to reach a high gain. Leaving the geometry unchanged, the material configuration can be another angle for antenna design and whose optimization might improve the antenna’s performances, particularly its gain as being discussed in this paper.

In this model, every point in the domain of the horn is assigned a *η* variable, whose value is to be changed by the optimization. *η* determines the permittivity, or equivalently what material is used, at one point according to the *ε _{ramp}* function.

*η*ranges from 0 to 1; when

*η*decreases from 0.5, the value of

*ε*reduces rapidly to 1, suggesting a usage of air; when

_{ramp}*η*increases from 0.5, the value of

*ε*rises sharply to 3.5, implying a usage of polyimide (PI).

_{ramp}*ε*as a function of

_{ramp}*η*is shown in Equation (1). When the

*η*value at one point equals to 0.5, it is saying that a composite of 50% air and 50% polyimide is used. However, in practice this sort of composite may be difficult to comprehend or implement. A definite usage of material is preferred. To ensure that most points are assigned a

*η*value away from ambiguity, a lower bound of the average of all points’ Weight function’s value is applied to the domain in the optimization. Weight function yields a large value when

*η*at that specific point is very different from 0.5, whereas when

*η*is close to 0.5, it contributes negligibly to the congregation. The graphs of the

*ε*and Weight functions are shown in Figure 1 and Figure 2, respectively. The reason why only permittivity changed is that both permeability and conductivity of air and polyimide are nearly equal. All parameters used in this work are listed in Table 1.

_{ramp}${\epsilon}_{\text{ramp}}={\epsilon}_{\text{air}}+\frac{{\epsilon}_{\text{polymide}}-{\epsilon}_{\text{air}}}{1+\left[1+{e}^{-3p1\left(\eta -0.5\right)}\right]}$ (1)

$\text{Weight}=1+\frac{1}{1+{e}^{-7p\left(\eta -0.68\right)}}-\frac{1}{1+{e}^{-7p\left(\eta -0.32\right)}}$ (2)

Figure 1. The graph of function *ε*_{ramp}.

Figure 2. The graph of function weight.

Table 1. Parameters used in this study.

$\text{Objective}=\frac{2\text{\pi}{r}_{\text{integration}}{{\displaystyle \int}}_{A}^{B}{E}_{\text{normalized}}\left(\theta \right)\text{d}\theta}{{L}_{\text{integration}}{{\displaystyle \oint}}^{\text{}}{E}_{\text{normalized}}\left(\theta \right)\text{d}\theta}$ (3)

$\text{Reflection}={\left(S11\right)}^{2}$ (4)

The layout of the antenna and its corresponding simulation region is shown in Figure 3. A perfectly matched layer with circular shape surrounds the entire simulation region to eliminate any reflection that could occur at the outer boundary.

The optimization objective expressed in Equation (3) is defined as the ratio of the radiation intensity in the far field at one particular direction to the average radiation intensity of an isotropic antenna: the linear integration of the normalized far field strength over the arc AB over the linear integration of the normalized far field strength over the entire circle, on which the arc AB lies, namely the total power. In the optimization, the Reflection is given an upper bound of 0.45, because excessive reflection from the hardware not only influences the power output, but can also damage the antenna and the transmitting line in practice. A uniform lumped port is used on arc CD to feed the antenna. Perfect electric conductor is applied to CE, DF, EG and FH, as shown in Figure 3. Finally, outside the antenna is defined as the far field, with the outermost layer being the perfectly matched layer to absorb radiation. Figure 4 depicts the mesh of the model. The Optimization module is set to find the maximum of the variable Objective, using the Method of Moving Asymptotes.

3. Results and Discussions

The final electric field norm and *η* distribution given by the topology optimization are shown in Figure 5. Particularly, on the right side, dark color denotes a low *η* value, indicating at that point, the permittivity is the permittivity of air. On the contrary, light color suggests a high *η* value, giving the point the permittivity of PI. In the horn, bands of air and PI appear alternately. Notably, dark points scatter in bands of air. The optimized results are quite non-intuitive, indicating the power of topology optimization.

Figures 6 to 8 show three variables as a function of iteration number during

Figure 3. Schematic of the antenna and outer simulation area under study.

Figure 4. Meshing for finite element method simulation. The antenna region is intentionally fine meshed to give better resolution.

Figure 5. Electromagnetic field distribution (left) and *η *value (right) after topology optimization.

Figure 6. Reflection vs. iteration number.

Figure 7. Weight/Area vs. iteration number.

optimization. As the optimization iterated, reflection drops and approaches 0.45, Weight/Area increases and approaches 0.94, and Objective approaches 105. Even though the reflection was still high in the end, the polar graph demonstrates that the power was indeed concentrated on the desired direction, as shown in Figure 9.

Figure 8. Objective vs. iteration number.

Figure 9. Far field projection of the antenna after topology optimization.

4. Conclusion

The topology optimization shows that a distribution of strips of air and polyimide occurring alternatingly provides a high gain for the horn antenna in this study. The materials distribution is non-intuitive, opening new ways for antenna performance optimization. This method could be developed to more complicated scenarios, such as phase arrays. Further researches can be conducted to find more combination of materials which may yield even better results.

Conflicts of Interest

The author declares no conflicts of interest regarding the publication of this paper.

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