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Optimal illusion and invisibility of multilayered anisotropic cylinders and spheres

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Abstract

In this paper, full-wave electromagnetic scattering theory is employed to investigate illusion and invisibility of inhomogeneous anisotropic cylinders and spheres. With the use of a shell designed according to Mie series theory for multiple piecewise anisotropic layers, radar cross section (RCS) of the coated inhomogeneous anisotropic object can be dramatically reduced or disguised as another object in the long-wavelength limit. With the suitable adjustment of the anisotropy parameters of the shell, optimal illusion and invisibility characteristics of the coated inhomogeneous anisotropic object can be achieved. Details of theoretical analysis and numerical examples are presented to validate the proposed methodology.

© 2016 Optical Society of America

1. Introduction

The subject of electromagnetic invisibility cloak has attracted great attention from both physics and engineering societies. The method of transformation optics (TO) independently developed by Pendry [1] and Leonhardt [2] is arguably the most popular for design of various invisibility cloaks. In the TO method, electromagnetic wave is controlled to go around the object, and then come back to the original trajectory. With theoretical verification [3, 4] and experimental realization [5–8], invisibility cloaks have experienced a tremendous development in the past few years, such as complementary cloak [9–11], carpet cloak [12] and anti-cloak [13, 14]. However, currently available technologies to convert the transformation-based cloaks into practical applications are still facing numerous bottlenecks. Particular challenges are laid on extreme electromagnetic parameters and narrow operating band. In an attempt to relieve the limitations of physical realization on the cloaks, many other means for manipulation of electromagnetic wave have been developed including conformal transformation [15, 16], surface wave cloak [17–19], and coding metamaterial [20], etc.

Alternatively, scattering cancellation method [21] has been proposed to achieve electromagnetic transparency using a shell with appropriately designed permittivity and permeability. Due to the ease of implementation, various invisibility [22–28], illusion [29], inhomogeneous [30], and bifunctional [31] cloaks based on the scattering cancellation method have been developed. On the other hand, with rapid advances in material technology, anisotropic materials allow for greater design flexibility and novel application in microwave engineering. Electromagnetic analysis of the anisotropic materials has been a subject of great interest [32, 33], and the scattering cancellation-based cloaks for anisotropic objects have been developed [34, 35]. However, to our best knowledge, no reports have been given to analyze invisibility and illusion effects of inhomogeneous anisotropic cylindrical and spherical objects. Moreover, how to design a cloak with the optimal invisibility and illusion performances according to the scattering cancellation method has not yet been studied.

The principal purpose of this paper is to achieve both the optimal invisibility and illusion for inhomogeneous anisotropic cylindrical and spherical objects with electrically small size. The inhomogeneous anisotropic objects are modeled as many thin layers of piecewise homogeneous layers. Following Mie series theory, Bessel and Hankel functions of the fractional orders are employed to expand the electromagnetic fields in each homogeneous anisotropic layer, and the corresponding scattering coefficients are determined according to the boundary conditions. With the resultant scattering coefficients, explicit expressions for geometric and electromagnetic parameters of the coating are derived to realize invisibility and illusion of the inhomogeneous anisotropic objects. By appropriately adjusting anisotropy parameters of the coating, the optimal illusion and invisibility effects can be achieved. Some cylindrical and spherical examples from the perspective of near and far fields are given to validate the proposed methodology.

2. Theoretical analysis

2.1 Illusion and Invisibility of inhomogeneous anisotropic cylinders and spheres

Consider an inhomogeneous object composed of n piecewise anisotropic layers illuminated by a plane wave. The time harmonic dependence of ejωtis assumed. Without loss of generality, TM polarized plane wave is considered in this paper. TE polarized case can be obtained by interchanging the role of permittivity and permeability according to duality relationship. Wrapping the inhomogeneous object with a slab of homogeneous material whose radius, permittivity and permeability tensors are rn+1, ε¯¯n+1, andμ¯¯n+1, respectively, to achieve invisibility and illusion performances.

2.2.1 Illusion and Invisibility of inhomogeneous anisotropic cylinder

At first, we analyze scattering behavior of a two-layer inhomogeneous cylinder (n = 2) concretely. In ith layer whose radius is ri, permittivity and permeability tensors in cylindrical coordinate are expressed as

ε¯¯i=[εirεiθε0],μ¯¯i=[μ0μ0μiz].
A homogeneous material slab covers the inhomogeneous cylinder to achieve the illusion and invisibility. According to wave transformation relationship, a TM-polarized plane wave can be written in terms of a linear superposition of cylindrical waves [36]
Hzinc=m=jmJm(k0r)ejmθ,
in which Jm is mth-order Bessel function of the first kind. The total fields in each layer of the coated cylinder can be expressed in terms of non-integer Bessel and Hankel functions according to Mie series expansion method as follows:
{Hz=m=jmAmJ1m(k1r)ejmθr<r1Hz=m=jm[BmJ2m(k2r)+CmY2m(k2r)]ejmθr1<r<r2Hz=m=jm[FmJ3m(k3r)+GmY3m(k3r)]ejmθr2<r<r3Hz=m=jm[Jm(k0r)+DmHm(1)(k0r)]ejmθr>r3,
where Jim, Yim, and Hm(1) represent imth-order Bessel functions of the first and second kinds, mth-order Hankel function of the first kind, respectively, and Am, Bm, Cm, Fm, Gm, and Dm are corresponding expansion coefficients. Here ki=ωμizεiθ and im=mARi (i=0,1,2,3), in which ARi=εiθ/εir denotes the electric anisotropy ratio. For an arbitrarily anisotropic material with εirεiθ, im is a non-integer, while im becomes an integer for an isotropic material. Hence the resultant scattering field can be written as

Hzsca=m=jmDmHm(1)(k0r)ejmθ.

Applying continuous conditions of tangential components of the total fields at each interface, the scattering coefficient Dm can be derived as

Dm=J1m(k1r1)J2m(k2r1)Y2m(k2r1)000k1ωε1θJ1m(k2r1)k2ωε2θJ2m(k2r1)k2ωε2θY2m(k2r1)0000J2m(k2r2)N2m(k2r2)J3m(k3r2)Y3m(k3r2)00k2ωε2θJ3m(k2r2)k2ωε2θN3m(k2r2)k3ωε3θJ3m(k3r2)k3ωε3θY3m(k3r2)0000J3m(k3r3)Y3m(k3r3)Jm(k0r3)000k3ωε3θJm(k3r3)k3ωε3θNm(k3r3)k0ωε0Jm(k0r3)J1m(k1r1)J2m(k2r1)Y2m(k2r1)000k1ωε1θJ1m(k2r1)k2ωε2θJ2m(k2r1)k2ωε2θY2m(k2r1)0000J2m(k2r2)Y2m(k2r2)J3m(k3r2)Y3m(k3r2)00k2ωε2θJm(k2r2)k2ωε2θY2m(k2r2)k3ωε3θJ3m(k3r2)k3ωε3θY3m(k3r2)0000J3m(k3r3)N3m(k3r3)Hm(1)(k0r3)000k3ωε3θJ3m(k3r3)k3ωε3θY3m(k3r3)k0ωε0Hm(1)(k0r3),
in which the prime denotes the derivative with respect to the argument. With the scattering coefficient Dm, radar scattering section (RCS) σ and scattering cross section (SCS) Csca can be calculated, respectively, as

σ=limr[2πr|Hzsca|2|Hzinc|2],Csca=4k0m=|Dm|2.

In order to determine the effect of the number of the scattering coefficients Dm on the scattering section, we consider a nonmagnetic homogeneous anisotropic cylinder with a radius of a. Figure 1 illustrates variation of the SCS with the argumentk0a for different number of the scattering coefficients Dm. For comparison, the SCS of a homogeneous isotropic cylinder is also plotted in Fig. 1. It can be seen that when k0a is small, the SCS solved by the scattering coefficients with m = 1 is coincident with that calculated by the scattering coefficients with m = 5. Hence the SCS is dominated by m = 0 and m = 1 terms of the scattering coefficients in the long wavelength limit.

 figure: Fig. 1

Fig. 1 SCS of a cylinder versus the argument k0r.

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To achieve the illusion, the scattering coefficients of the coated anisotropic cylinder are set as same as that of an isotropic cylinder with a radius of re, permittivity of εe, and permeability of μe. According to standard Mie series expansion method, scattering coefficient Sm of the isotropic illusion cylinder can be got as

Sm=Jm(kere)Jm(k0re)keωεeJm(kere)k0ωε0Jm(k0re)Jm(kere)Hm(1)(k0re)keωεeJm(kere)k0ωε0Hm(1)(k0re).
Thus, the illusion condition can be obtained as D0=S0 and D1=S1. Considering the approximationsJ0(x)1,J0(x)x/2, H0(1)=1+j2ln(x/2)/π, and H0(1)=x/2+j2/(πx) in the long wavelength limit, we can derive the illusion conditions as
(r3r1)2=(μ2zμ1z)+(μ3zμ2z)(r2r1)2+(μeμ0)(rer1)2μ3zμ0,
(r3r2)2t3=ε3θt3εe(2)ε3θ+t3εe(2)r32(ε3θ+ε0t3)(εe+ε0)re2(ε3θε0t3)(εeε0)r32(ε3θε0t3)(εe+ε0)re2(ε3θ+ε0t3)(εeε0),
where
εe(2)=ε2θ+εe(1)t2ε2θεe(1)t2(r1r2)2t2ε2θ+εe(1)t2ε2θεe(1)t2+(r1r2)2t2ε2θt2,εe(1)={ε1θt1thecoreisdielectric0thecoreisconductor,
ti=ARi(i=1,2,3).
Note that εe(l)(l=1,2) in Eq. (10) represents the equivalent permittivity of the region from the lth layer to the innermost layer.

We extend the above procedure to an inhomogeneous anisotropic cylinder composed of n piecewise homogeneous layers, the corresponding illusion conditions can be got as follows:

(rn+1r1)2=(μ2zμ1z)+(μ3zμ2z)(r2r1)2+(μ4zμ3z)(r3r1)2++(μ(n+1)zμnz)(rn1r1)2+(μeμ0)(rer1)2μ(n+1)zμ0,
(rn+1rn)2tn+1=ε(n+1)θtn+1εe(n)ε(n+1)θ+tn+1εe(n)rn+12(ε(n+1)θ+ε0tn+1)(εe+ε0)re2(ε(n+1)θε0tn+1)(εeε0)rn+12(ε(n+1)θε0tn+1)(εe+ε0)re2(ε(n+1)θ+ε0tn+1)(εeε0),
in which
εe(n)=εnθ+εe(n-1)tnεnθεe(n-1)tn(rn1rn)2tnεnθ+εe(n-1)tnεnθεe(n-1)tn+(rn1rn)2tnεnθtn,εe(1)={ε1θt1thecoreisdielectric0thecoreisconductor.
It is worthwhile pointing out that invisibility conditions can be easily derived according to the illusion conditions only by replacing εe, μe, and re in Eqs. (12) and (13) by ε0, μ0, and rn+1.

2.2.2 Illusion and Invisibility of inhomogeneous sphere

Similarly, we starts with illusion and invisibility of a two-layer inhomogeneous anisotropic sphere coated by a layer of anisotropic dielectric. The nonmagnetic constitutive relation of each layer in spherical coordinate can be expressed as

ε¯¯i=[εirεiθεiθ].

With the wave transformation relationship, the incident wave with x-polarization can be written in terms of a linear superposition of spherical waves as [36]

Eθinc=E0cosφk0rn=1jn(2n+1)J^n(k0r)Pn(cosθ),
where F^l(x)=πx/2Fl(x) and Pn(cosθ) is nth-order Legendre polynomial. The total fields in each layer can be expressed by spherical wave functions as follows:
{Eθ=E0cosφωm=1jm2m+1m(m+1)AmJ^1m(k1r)Pm1(cosθ)r<r1Eθ=E0cosφωm=1jm2m+1m(m+1)[BmJ^2m(k2r)+CmY^2m(k2r)]Pm1(cosθ)r1<r<r2Eθ=E0cosφωm=1jm2m+1m(m+1)[FmJ^3m(k3r)+GmY^3m(k3r)]Pm1(cosθ)r2<r<r3Eθ=E0cosφωm=1jm2m+1m(m+1)[J^m(k0r)+DmH^m(1)(k0r)]Pm1(cosθ)r>r3,
in which Pn1(cosθ)=dPn(cosθ)/dθ, ki=ωμ0εiθ, and im=2m(m+1)ARi+0.250.5(i=1,2,3). Therefore, the corresponding scattering field is obtained as

Eθ=E0cosφωm=1jm2m+1m(m+1)DmH^m(1)(k0r)Pm1(cosθ)

The scattering coefficients Dm of the coated anisotropic sphere are determined by matching the boundary conditions which require continuity of the tangential components of the total fields on the interface, e.g.,

Dm=J^1m(k1r1)J^2m(k2r1)Y^2m(k2r1)000k1ωε1θJ^1m(k1r1)k2ωε2θJ^2m(k2r1)k2ωε2θY^2m(k2r1)0000J^2m(k2r2)Y^2m(k2r2)J^3m(k3r2)Y^3m(k3r2)00k2ωε2θJ^2m(k2r2)k2ωε2θY^2m(k2r2)k3ωε3θJ^3m(k3r2)k3ωε3θY^3m(k3r2)0000J^3m(k3r3)Y^3m(k3r3)J^m(k0r3)000k3ωε3θJ^3m(k3r3)k3ωε3θY^3m(k3r3)k0ωε0J^m(k0r3)J^1m(k1r1)J^2m(k2r1)Y^2m(k2r1)000k1ωε1θJ^1m(k1r1)k2ωε2θJ^2m(k2r1)k2ωε2θY^2m(k2r1)0000J^2m(k2r2)Y^2m(k2r2)J^3m(k3r2)Y^3m(k3r2)00k2ωε2θJ^2m(k2r2)k2ωε2θY^2m(k2r2)k3ωε3θJ^3m(k3r2)k3ωε3θY^3m(k3r2)0000J^3m(k3r3)Y^3m(k3r3)H^m(1)(k0r3)000k3ωε3θJ^3m(k3r3)k3ωε3θY^3m(k3r3)k0ωε0H^m(1)(k0r3).
Therefore, the RCS and SCS are expressed in terms of the scattering coefficients Dm respectively as

σ=limr[4πr2|Esc|2|Einc|2],Csca=2πk02m=1(2m+1)|Dm|2.

Figure 2 shows the SCS for the homogeneous anisotropic and isotropic spheres with the radius of a. It can be seen that for small argument k0a, i.e., in the quasistatic limit, only one term Dm dominates the SCS.

 figure: Fig. 2

Fig. 2 SCS of a sphere versus the argument k0a.

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To make the coated anisotropic sphere behave like an isotropic sphere with a radius of re, permittivity of εe, and permeability of μe, Dm must be equal to the corresponding scattering coefficients of the isotropic sphere given by

Sm=J^m(kere)J^m(k0re)keωεeJ^m(kere)k0ωε0J^m(k0re)J^m(kere)H^m(1)(k0re)keωεeJ^m(kere)k0ωε0H^m(1)(k0re).
Therefore, the illusion conditions for the two-layer anisotropic sphere can be obtained by setting D1=S1. Further, with a generalized procedure, the illusion conditions for a n-layer anisotropic sphere can be get as
(rn+1rn)2tn+1+1=ε(n+1)θ12(1+tn+1)εe(n)ε(n+1)θ+12tn+1εe(n)rn+13(2ε0+εe)(ε(n+1)θ+12tn+1ε0)+re3(ε0εe)(ε(n+1)θtn+1ε0)rn+13(2ε0+εe)[ε(n+1)θ12(1+tn+1)ε0]+re3(ε0εe)[ε(n+1)θ+(1+tn+1)ε0],
in which
εe(n)=2(rnrn1)2tn+12εnθ12(1+tn)εe(n1)εnθ+12tnεe(n1)(1+tn)(rnrn1)2tn+1+tnεnθ12(1+tn)εe(n1)εnθ+12tnεe(n1)εnθ,εe(1)={2ε1θ1+t1thecoreisdielectric0thecoreisconductor,
ti=2ARi+0.250.5(i=1,2n+1).
The invisibility conditions of inhomogeneous anisotropic sphere can be obtained by substituting the equations εe=ε0 and rn+1=re into Eq. (22).

2.2 Optimization of illusion and invisibility effects

According to the above discussion, we can know that when a coating with the parameters determined by Eqs. (12), (13) and (22) is used, the invisibility and illusion phenomena of the inhomogeneous anisotropic cylindrical and spherical objects appear. Given the radius of the coating, its different anisotropic parameters generate different invisibility and illusion effects. Specifically, electromagnetic parameters of the coating in Eqs. (12), (13) and (22) depend on the electric anisotropy ratio ARi. Hence, we can find the optimal invisibility and illusion of the inhomogeneous anisotropic object by suitably adjusting ARi of the coating. In order to measure the optimal invisibility and illusion effects, we define the following evaluation functions:

σ1=14π0π02π|σc(θ,φ)σi(θ,φ)|sinθdφdθforillusion,
σ2=14π0π02π|σc(θ,φ)|sinθdφdθforinvisibility,
where σc(θ,φ) and σi(θ,φ) represent the RCS of the coated cylinder (sphere) and the corresponding illusion object, respectively. It is worthwhile noticing that if the scattering fields from the cylinder (sphere) are of the symmetry, two plane cuts through the symmetric axis, called the principal plane (E-plane or H-plane) are sufficient to represent the scattering fields. In this scenario, the evaluation functions around all the solid angle can be reduced to that in two principle planes. In the following numerical examples, the evaluation functions in two principle planes are used. According to Eq. (25), we can know that the best illusion effect can be obtained, when σ1 reaches the minimum value. Likewise, the best invisibility effect occurs with the minimum σ2. Therefore, ARi is searched for to minimize σ1 and σ2 for the optimal illusion and invisibility. In addition, note that the formulations for the invisibility and illusion of inhomogeneous cylinder and sphere, e.g., Eqs. (12), (13) and (22), are derived under the condition of the quasi-static approximation. Hence the electrical sizes of the cylindrical and spherical objects should be small. With the increase of the electrical sizes of the objects, more scattering coefficients are required to derive the invisibility and illusion condition.

3. Numerical simulations

To validate the above theoretical design, some numerical examples are given in this section. A finite element solver COMSOL MULTIPHYSICS is used to simulate illusion and invisibility of inhomogeneous anisotropic cylinders and spheres. A TM incident wave is considered in the simulation and the scattering boundary conditions are utilized to terminate the simulation region.

As the first example, consider a conducting sphere coated by a continuously inhomogeneous anisotropic nonmagnetic material. The relative permittivity tensor of the material is εr=2.734×105r33.139×104r2+742.5r+15 and εθ=εφ=1.519×105r31.924×104r2+442.5r+14, as shown in Fig. 3(a). In order to model the inhomogeneous material, the material slab is divided into three layers of piecewise homogeneous anisotropic layers. Figure 3(b) shows the electromagnetic and geometric parameters of each layer. To realize the illusion of the inhomogeneous sphere, an anisotropic coating is designed so that the resultant RCS of the coated sphere is similar to that of an anisotropic sphere with re=4λ0/15 and εe=3.874ε0. According to Eq. (22), the parameters of the coating are determined as r4=3.5λ0/15, ε4r=14.6139ε0/1.2, and ε4θ=ε4φ=14.6139ε0. Figures 4(a) and 4(b) show magnetic field distributions for the coated and illusion spheres at 900MHz in XOY plane, respectively. Two similar magnetic field distributions can be observed. Further, comparison of bistatic RCS between the coated and illusion spheres is given in Fig. 4(c). A very small difference of the RCS between them can be observed, which validates the proposed methodology.

 figure: Fig. 3

Fig. 3 A continuously inhomogeneous sphere. (a) constitutive parameters. (b) approximation model with piecewise homogeneous layers.

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 figure: Fig. 4

Fig. 4 Illusion for a continuously inhomogeneous sphere. (a) magnetic field distribution of the coated sphere in the XOY plane at 900MHz. (b) magnetic field distribution of the illusion sphere in the XOY plane at 900MHz. (c) bistatic RCSs of the coated and illusion spheres in XOY plane.

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In the second example, we consider an inhomogeneous anisotropic sphere composed of three nonmagnetic homogeneous layers. The parameters of the inhomogeneous sphere are as follows: ε1r=40ε0/3, ε1θ=ε1φ=5ε0, ε2r=2ε0/0.28, ε2θ=ε2φ=2ε0, ε3r=6ε0/0.28, ε3θ=ε3φ=6ε0, r1=λ0/29, r2=2λ0/29, and r3=3λ0/29. In order to make the inhomogeneous sphere behave like a nonmagnetic isotropic sphere with εe=4.13ε0 and re=4.5λ0/29, parameters of the coating are determined according to Eq. (22) as follows: ε4r=9ε0/0.055, ε4θ=ε4φ=9ε0, and r4=4λ0/29. According to designer’s intention, the outermost radius of the coated sphere can be arbitrarily chosen. In this example, the outermost radius of the coated sphere is 4λ0/29, which is different from that of the illusion sphere 4.5λ0/29. As shown in Figs. 5 (a) and 5(b), magnetic field distribution for the coated sphere is similar to that for the illusion sphere. Figures 5(c) and 5(d) show comparison of bistatic RCS between the coated and illusion spheres in XOY and XOZ planes, respectively. With the designed coating, a small difference of the RCS between them can be observed.

 figure: Fig. 5

Fig. 5 Illusion for a two-layer inhomogeneous sphere. (a) magnetic field distribution of the coated sphere in the XOY plane at 500MHz. (b) magnetic field distribution of the illusion sphere in the XOY plane at 500MHz. (c) bistatic RCS of the coated and illusion spheres in XOY plane. (d) bistatic RCSs of the coated and illusion spheres in XOZ plane

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To demonstrate how to obtain the best illusion effect, consider a homogeneous sphere with a radius of r1=2λ0/18. Its permittivity tensor in spherical coordinate is ε1r=24ε0/0.48 and ε1θ=ε1φ=24ε0. A coating with a radius of r2=4λ0/18 is designed such that the coated sphere has the most similar image to an isotropic sphere with re=5λ0/18 and εe=3.3ε0. Figure 6(a) illustrates the dependence of σ1 on anisotropic ratio AR of the coating. From the Fig. 6(a) we can see that AR = 1 leads to the minimal σ1. Substituting AR = 1 into Eq. (22), the parameters of the coating can be determined as ε2r=16.225ε0, and ε2θ=ε2φ=16.225ε0. Figure 6(b) shows bistatic RCS in XOY plane for different AR of the coating. It can be seen that RCS for AR = 1 approximately coincides with that of the illusion sphere. Figure 7 shows comparison of magnetic field distribution between the coated sphere with the optimal AR and the illusion sphere. Very good illusion effect can be obtained.

 figure: Fig. 6

Fig. 6 Optimal illusion effect of a homogeneous sphere. (a) evaluation function versus AR. (b) bistatic RCSs for different AR.

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 figure: Fig. 7

Fig. 7 Illusion for a homogeneous anisotropic sphere. (a) magnetic field distribution of the coated sphere with the optimal AR in the XOY plane at 400MHz. (b) magnetic field distribution of the illusion sphere in the XOY plane at 400MHz.

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In the following, the above method is used to design an invisibility cloak of a two-layer inhomogeneous sphere with a PEC core. The parameters of the inhomogeneous sphere are ε2r=35ε0/1.68, ε2θ=ε2φ=35ε0, r1=λ0/14, and r2=1.5λ0/14. In order to dramatically reduce RCS of the inhomogeneous sphere, a shell is introduced to cover the sphere. According to Eq. (22), parameters of the shell can be determined as ε3r=0.34ε0, ε3θ=ε3φ=0.24ε0, and r3=2λ0/14. Figures 8(a) and 8(b) depict magnetic field distributions for the uncoated and coated spheres at 600MHz, respectively. A good invisibility of the coated sphere can be observed. Further, Figs. 9(a) and 9(b) show comparison of bistatic RCS between the uncoated and coated spheres in XOY and XOZ planes, respectively. In XOY plane, RCS reduction of 19dB at θ=0o and 23dB at θ=180o can be obtained, and in XOZ plane, RCS reduction larger than 19dB can be achieved. For comparison, the TE polarization case is given in Figs. 9(c) and 9(d). It can be seen from Figs. 9(c) and 9(d) that RCS reduction of 9dB at θ=180o in XOY plane and 4dB at θ=0o in XOZ plane can be obtained, respectively. According to Fig. 9, we can know that the invisibility performance for TE polarization is worse than that for TM polarization.

 figure: Fig. 8

Fig. 8 Invisibility for a two-layer inhomogeneous sphere. (a) magnetic field distribution of the uncoated sphere in the XOY plane at 600MHz. (b) magnetic field distribution of the coated sphere in the XOY plane at 600MHz.

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 figure: Fig. 9

Fig. 9 Comparison of bistatic RCS between the coated and uncoated spheres. (a) RCS in XOY plane for TM polarization. (b) RCS in XOZ plane for TM polarization. (c) RCS in XOY plane for TE polarization. (d) RCS in XOZ plane for TE polarization.

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In order to further decrease RCS of the inhomogeneous sphere, electric anisotropy ratio AR of the coating is optimized. Figures 10(a) and 10(b) show variation of evaluation function σ2 with AR of the coating and bistatic RCS for different AR of the coating, respectively. It can be seen that the smallest RCS can be obtained when AR is equal to 3.01, which corresponds to the minimal σ2. Compared with the previous design with AR = 0.71, RCS with the optimized AR decreases 20dB at θ=0o and 54dB at θ=180o. Note that when AR of the coating increases to a certain extent, RCS of the coated sphere obviously increases. This is because with the increase of AR, electric size of the coated sphere increases accordingly such that the quasistatic limit condition cannot be satisfied.

 figure: Fig. 10

Fig. 10 Optimal invisibility effect of an inhomogeneous sphere. (a) evaluation function versus AR. (b) bistatic RCSs for different AR.

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Next, consider a two-layer inhomogeneous cylinder whose permittivity and permeability tensors are ε1r=6.25ε0, ε1θ=4ε0, ε2r=0.777ε0, ε2θ=0.304ε0, μ1z=3μ0, and μ2z=μ0/3. The radius of each layer is r1=λ0/138 and r2=2λ0/138. Scattering effect of the inhomogeneous cylinder is manipulated by using a coating such that the resultant electromagnetic response is similar to that of an isotropic cylinder with a radius of re=4.5λ0/138, permittivity of εe=6.28ε0, and permeability of μe=4μ0. According to Eqs. (12) and (13), parameters of the coating are obtained as ε3r=56.25ε0, ε3θ=36ε0, μ3z=4.0625μ0, and r3=4λ0/138. Figures 11(a) and 11(b) show magnetic field distributions for the coated and illusion cylinders, respectively. Scattering field depicted in Fig. 11(a) is in good agreement with that shown in Fig. 11(b). Further, in order to obtain the optimal illusion effect, Fig. 12(a) demonstrates variation of evaluation function σ1 with AR of the coating, when the radius of the coating is fixed. It can be seen that when AR = 0.64, σ1 reaches the minimum value. Figure 12(b) shows bistatic RCSs for different AR. The RCS for AR = 0.64 coincides with that of the illusion cylinder, thus leading to a best illusion effect.

 figure: Fig. 11

Fig. 11 Illusion for a two-layer inhomogeneous cylinder. (a) magnetic field distribution at 300MHz for the coated cylinder. (b) magnetic field distribution at 300MHz for the illusion cylinder.

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 figure: Fig. 12

Fig. 12 Optimal illusion effect of an inhomogeneous cylinder. (a) evaluation function versus AR. (b) bistatic RCSs for different AR.

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In the following, a four-layer inhomogeneous cylinder is considered. In the cylinder, the innermost layer is a conductor, and electromagnetic parameters of the remaining layers are ε2r=40.5ε0, ε2θ=18ε0, ε3r=8ε0/0.36, ε3θ=8ε0, ε4r=5ε0/0.64, and ε4θ=5ε0. Dimensions of the four-layer cylinder are r1=λ0/30, r2=1.5λ0/30, r3=2λ0/30, and r4=3λ0/30. To greatly reduce RCS of the cylinder, a coating whose parameters are ε5r=0.33ε0, ε5θ=0.08ε0, and r5=4λ0/30 is designed. Figures 13(a) and 13(b) illustrate magnetic field distributions for the uncoated and coated cylinders, respectively. Figure 13(c) shows bistatic RCSs of the uncoated and coated cylinders, and a significant reduction of 18dB at θ=0o and 12.5dB at θ=180o is observed. As shown in Fig. 13, the cylindrical object is well hidden by the use of the coating from the perspective of near and far fields. We further search for the optimal invisibility performance by adjusting the coating’s anisotropy ratio. Figure 14(a) shows variation of the evaluation function σ2 with AR of the coating. We can see that the coating with AR = 7 results in the minimum σ2. The bistatic RCSs for different AR of the coating are compared in Fig. 14(b). The best invisibility effect with RCS reduction of 19dB at θ=0o and 41dB at θ=180o occurs when AR = 7. It is worthwhile pointing out that when AR of the coating becomes large enough, the resultant RCS increases due to the invalid long-wavelength limit. Further, the invisibility of the loss object is studied. Firstly, assume εθ of each layer lossy with lossless εr. Specifically, εθ of each layer is as follows: ε2θ=(18-3j)ε0, ε3θ=(82j)ε0, and ε4θ=(53j)ε0. Figure 15 shows the magnetic field distribution and the bistatic RCS of the lossy cylinder with the above designed lossless coating. It can be seen that the cylindrical object is well hidden. In the following, consider lossy εr of each layer with lossless εθ. The corresponding εr of each layer is as follows: ε2r=(40.50.5j)ε0, ε3r=(8/0.360.5j)ε0, and ε4r=(5/0.640.2j)ε0. As shown in Fig. 16, good invisibility of the loss cylinder can be realized with the use of the designed lossless coating. It is worthwhile pointing out that the electromagnetic parameters of the coating in Eqs. (12), (13) and (22) are determined with the assumption of inhomogeneous anisotropic lossless object. When the loss of the target is small, good invisibility and illusion are still achieved with the designed coating.

 figure: Fig. 13

Fig. 13 Invisibility for a four-layer inhomogeneous cylinder. (a) magnetic field distribution at 800MHz for the uncoated target. (b) magnetic field distribution at 800MHz for the coated target. (c) bistatic RCSs of the uncoated and coated cylinders.

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 figure: Fig. 14

Fig. 14 Optimal invisibility effect of an inhomogeneous cylinder. (a) evaluation function versus AR. (b) bistatic RCSs for different AR.

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 figure: Fig. 15

Fig. 15 An inhomogeneous cylinder with lossy εθ. (a) magnetic field distribution at 800MHz for the uncoated target. (b) magnetic field distribution at 800MHz for the coated target. (c) bistatic RCSs of the uncoated and coated cylinders.

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 figure: Fig. 16

Fig. 16 An inhomogeneous cylinder with lossy εr. (a) magnetic field distribution at 800MHz for the uncoated target. (b) magnetic field distribution at 800MHz for the coated target. (c) bistatic RCSs of the uncoated and coated cylinders.

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Finally, we consider a practical engineering implementation for illusion of a conducting cylinder with a radius of λ0/10 by using composite optical material, as shown in Fig. 17(a). In order to manipulate the scattering field of the PEC cylinder similar to a dielectric cylinder with a radius of λ0/5 and permittivity of εe=3.473ε0, a coating with a radius of λ0/5 and permittivity tensor of ε2r=2.878ε0 and ε2θ=6.769ε0 is used, according to Eqs. (12) and (13). A set of plasmonic spherical nanoparticles with a random distribution embedded in a dielectric host can be equivalent to a slab material with anisotropic dielectric [37, 38] in THz frequency band. According to the Maxwell Garnett effective medium theory, the permittivity tensor can be obtained as [37, 38]

εr=εh(1+f)εm+(1f)εh(1+f)εh+(1f)εm,εθ=fεm+(1f)εh,
where f is the filling factor of nanoparticles in the dielectric host, εh is permittivity of the dielectric host, and εm is permittivity of the spherical nanoparticle, which follows Drude model according to
εm=εωp2ω2jωγ,
in which ε is high frequency dielectric constant, ωp is plasma frequency, and γ is damping term. In order to realize the electromagnetic parameters of the coating, the dielectric host is chosen as Poly Tetra Fluor Ethylene with the relative permittivity of 1.7689 [39]. The nanoparticles are made of silver with ε=5, ωp=13666rad/s, and γ=2733rad/s [40], and the filling factor of particles f is 0.5. Figure 17(b) shows RCS comparison between the conducting and the coated cylinders at 3THz, with a good agreement with each other. In addition, comparison of magnetic field distribution between them is given in Figs. 17(c) and 17(d). Two very similar magnetic distributions can be observed.

 figure: Fig. 17

Fig. 17 Illusion of a conducting cylinder. (a) schematic figure of the structure. (b) bistatic RCS of the uncoated and coated cylinders. (c) magnetic field distribution at 3THz for the coated cylinder. (d) magnetic field distribution at 3THz for the illusion cylinder.

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4. Conclusion

This paper focuses on the design of illusion and invisibility cloaks for arbitrarily inhomogeneous anisotropic cylindrical and spherical objects based on Mie scattering theory. With the proposed formulations, parameters of the coating can be analytically solved to achieve illusion and invisibility of the object in the long-wavelength limit. Much efforts have been put on the analyses of the effects of the coating’s electric anisotropy ratio on the RCS. By optimizing the electric anisotropy ratio of the coating, the optimal illusion and invisibility can be achieved. A fairly good agreement between the simulation and the theory validates the proposed method.

Funding

The Program for the New Scientific and Technological Star of Shaanxi Province (No.2013KJXX-66, No. BD11015020008); Technology Innovation Research Project of the CETC; Fundamental Research Funds for the Central Universities (No. SPSZ031410).

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Figures (17)

Fig. 1
Fig. 1 SCS of a cylinder versus the argument k 0 r .
Fig. 2
Fig. 2 SCS of a sphere versus the argument k 0 a .
Fig. 3
Fig. 3 A continuously inhomogeneous sphere. (a) constitutive parameters. (b) approximation model with piecewise homogeneous layers.
Fig. 4
Fig. 4 Illusion for a continuously inhomogeneous sphere. (a) magnetic field distribution of the coated sphere in the XOY plane at 900MHz. (b) magnetic field distribution of the illusion sphere in the XOY plane at 900MHz. (c) bistatic RCSs of the coated and illusion spheres in XOY plane.
Fig. 5
Fig. 5 Illusion for a two-layer inhomogeneous sphere. (a) magnetic field distribution of the coated sphere in the XOY plane at 500MHz. (b) magnetic field distribution of the illusion sphere in the XOY plane at 500MHz. (c) bistatic RCS of the coated and illusion spheres in XOY plane. (d) bistatic RCSs of the coated and illusion spheres in XOZ plane
Fig. 6
Fig. 6 Optimal illusion effect of a homogeneous sphere. (a) evaluation function versus AR. (b) bistatic RCSs for different AR.
Fig. 7
Fig. 7 Illusion for a homogeneous anisotropic sphere. (a) magnetic field distribution of the coated sphere with the optimal AR in the XOY plane at 400MHz. (b) magnetic field distribution of the illusion sphere in the XOY plane at 400MHz.
Fig. 8
Fig. 8 Invisibility for a two-layer inhomogeneous sphere. (a) magnetic field distribution of the uncoated sphere in the XOY plane at 600MHz. (b) magnetic field distribution of the coated sphere in the XOY plane at 600MHz.
Fig. 9
Fig. 9 Comparison of bistatic RCS between the coated and uncoated spheres. (a) RCS in XOY plane for TM polarization. (b) RCS in XOZ plane for TM polarization. (c) RCS in XOY plane for TE polarization. (d) RCS in XOZ plane for TE polarization.
Fig. 10
Fig. 10 Optimal invisibility effect of an inhomogeneous sphere. (a) evaluation function versus AR. (b) bistatic RCSs for different AR.
Fig. 11
Fig. 11 Illusion for a two-layer inhomogeneous cylinder. (a) magnetic field distribution at 300MHz for the coated cylinder. (b) magnetic field distribution at 300MHz for the illusion cylinder.
Fig. 12
Fig. 12 Optimal illusion effect of an inhomogeneous cylinder. (a) evaluation function versus AR. (b) bistatic RCSs for different AR.
Fig. 13
Fig. 13 Invisibility for a four-layer inhomogeneous cylinder. (a) magnetic field distribution at 800MHz for the uncoated target. (b) magnetic field distribution at 800MHz for the coated target. (c) bistatic RCSs of the uncoated and coated cylinders.
Fig. 14
Fig. 14 Optimal invisibility effect of an inhomogeneous cylinder. (a) evaluation function versus AR. (b) bistatic RCSs for different AR.
Fig. 15
Fig. 15 An inhomogeneous cylinder with lossy εθ. (a) magnetic field distribution at 800MHz for the uncoated target. (b) magnetic field distribution at 800MHz for the coated target. (c) bistatic RCSs of the uncoated and coated cylinders.
Fig. 16
Fig. 16 An inhomogeneous cylinder with lossy εr. (a) magnetic field distribution at 800MHz for the uncoated target. (b) magnetic field distribution at 800MHz for the coated target. (c) bistatic RCSs of the uncoated and coated cylinders.
Fig. 17
Fig. 17 Illusion of a conducting cylinder. (a) schematic figure of the structure. (b) bistatic RCS of the uncoated and coated cylinders. (c) magnetic field distribution at 3THz for the coated cylinder. (d) magnetic field distribution at 3THz for the illusion cylinder.

Equations (28)

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ε ¯ ¯ i = [ ε i r ε i θ ε 0 ] , μ ¯ ¯ i = [ μ 0 μ 0 μ i z ] .
H z i n c = m = j m J m ( k 0 r ) e j m θ ,
{ H z = m = j m A m J 1 m ( k 1 r ) e j m θ r < r 1 H z = m = j m [ B m J 2 m ( k 2 r ) + C m Y 2 m ( k 2 r ) ] e j m θ r 1 < r < r 2 H z = m = j m [ F m J 3 m ( k 3 r ) + G m Y 3 m ( k 3 r ) ] e j m θ r 2 < r < r 3 H z = m = j m [ J m ( k 0 r ) + D m H m ( 1 ) ( k 0 r ) ] e j m θ r > r 3 ,
H z s c a = m = j m D m H m ( 1 ) ( k 0 r ) e j m θ .
D m = J 1 m ( k 1 r 1 ) J 2 m ( k 2 r 1 ) Y 2 m ( k 2 r 1 ) 0 0 0 k 1 ω ε 1 θ J 1 m ( k 2 r 1 ) k 2 ω ε 2 θ J 2 m ( k 2 r 1 ) k 2 ω ε 2 θ Y 2 m ( k 2 r 1 ) 0 0 0 0 J 2 m ( k 2 r 2 ) N 2 m ( k 2 r 2 ) J 3 m ( k 3 r 2 ) Y 3 m ( k 3 r 2 ) 0 0 k 2 ω ε 2 θ J 3 m ( k 2 r 2 ) k 2 ω ε 2 θ N 3 m ( k 2 r 2 ) k 3 ω ε 3 θ J 3 m ( k 3 r 2 ) k 3 ω ε 3 θ Y 3 m ( k 3 r 2 ) 0 0 0 0 J 3 m ( k 3 r 3 ) Y 3 m ( k 3 r 3 ) J m ( k 0 r 3 ) 0 0 0 k 3 ω ε 3 θ J m ( k 3 r 3 ) k 3 ω ε 3 θ N m ( k 3 r 3 ) k 0 ω ε 0 J m ( k 0 r 3 ) J 1 m ( k 1 r 1 ) J 2 m ( k 2 r 1 ) Y 2 m ( k 2 r 1 ) 0 0 0 k 1 ω ε 1 θ J 1 m ( k 2 r 1 ) k 2 ω ε 2 θ J 2 m ( k 2 r 1 ) k 2 ω ε 2 θ Y 2 m ( k 2 r 1 ) 0 0 0 0 J 2 m ( k 2 r 2 ) Y 2 m ( k 2 r 2 ) J 3 m ( k 3 r 2 ) Y 3 m ( k 3 r 2 ) 0 0 k 2 ω ε 2 θ J m ( k 2 r 2 ) k 2 ω ε 2 θ Y 2 m ( k 2 r 2 ) k 3 ω ε 3 θ J 3 m ( k 3 r 2 ) k 3 ω ε 3 θ Y 3 m ( k 3 r 2 ) 0 0 0 0 J 3 m ( k 3 r 3 ) N 3 m ( k 3 r 3 ) H m ( 1 ) ( k 0 r 3 ) 0 0 0 k 3 ω ε 3 θ J 3 m ( k 3 r 3 ) k 3 ω ε 3 θ Y 3 m ( k 3 r 3 ) k 0 ω ε 0 H m ( 1 ) ( k 0 r 3 ) ,
σ = lim r [ 2 π r | H z s c a | 2 | H z i n c | 2 ] , C s c a = 4 k 0 m = | D m | 2 .
S m = J m ( k e r e ) J m ( k 0 r e ) k e ω ε e J m ( k e r e ) k 0 ω ε 0 J m ( k 0 r e ) J m ( k e r e ) H m ( 1 ) ( k 0 r e ) k e ω ε e J m ( k e r e ) k 0 ω ε 0 H m ( 1 ) ( k 0 r e ) .
( r 3 r 1 ) 2 = ( μ 2 z μ 1 z ) + ( μ 3 z μ 2 z ) ( r 2 r 1 ) 2 + ( μ e μ 0 ) ( r e r 1 ) 2 μ 3 z μ 0 ,
( r 3 r 2 ) 2 t 3 = ε 3 θ t 3 ε e ( 2 ) ε 3 θ + t 3 ε e ( 2 ) r 3 2 ( ε 3 θ + ε 0 t 3 ) ( ε e + ε 0 ) r e 2 ( ε 3 θ ε 0 t 3 ) ( ε e ε 0 ) r 3 2 ( ε 3 θ ε 0 t 3 ) ( ε e + ε 0 ) r e 2 ( ε 3 θ + ε 0 t 3 ) ( ε e ε 0 ) ,
ε e ( 2 ) = ε 2 θ + ε e ( 1 ) t 2 ε 2 θ ε e ( 1 ) t 2 ( r 1 r 2 ) 2 t 2 ε 2 θ + ε e ( 1 ) t 2 ε 2 θ ε e ( 1 ) t 2 + ( r 1 r 2 ) 2 t 2 ε 2 θ t 2 , ε e ( 1 ) = { ε 1 θ t 1 t h e c o r e i s d i e l e c t r i c 0 t h e c o r e i s c o n d u c t o r ,
t i = A R i ( i = 1 , 2 , 3 ) .
( r n + 1 r 1 ) 2 = ( μ 2 z μ 1 z ) + ( μ 3 z μ 2 z ) ( r 2 r 1 ) 2 + ( μ 4 z μ 3 z ) ( r 3 r 1 ) 2 + + ( μ ( n + 1 ) z μ n z ) ( r n 1 r 1 ) 2 + ( μ e μ 0 ) ( r e r 1 ) 2 μ ( n + 1 ) z μ 0 ,
( r n + 1 r n ) 2 t n + 1 = ε ( n + 1 ) θ t n + 1 ε e ( n ) ε ( n + 1 ) θ + t n + 1 ε e ( n ) r n + 1 2 ( ε ( n + 1 ) θ + ε 0 t n + 1 ) ( ε e + ε 0 ) r e 2 ( ε ( n + 1 ) θ ε 0 t n + 1 ) ( ε e ε 0 ) r n + 1 2 ( ε ( n + 1 ) θ ε 0 t n + 1 ) ( ε e + ε 0 ) r e 2 ( ε ( n + 1 ) θ + ε 0 t n + 1 ) ( ε e ε 0 ) ,
ε e ( n ) = ε n θ + ε e ( n - 1 ) t n ε n θ ε e ( n - 1 ) t n ( r n 1 r n ) 2 t n ε n θ + ε e ( n - 1 ) t n ε n θ ε e ( n - 1 ) t n + ( r n 1 r n ) 2 t n ε n θ t n , ε e ( 1 ) = { ε 1 θ t 1 t h e c o r e i s d i e l e c t r i c 0 t h e c o r e i s c o n d u c t o r .
ε ¯ ¯ i = [ ε i r ε i θ ε i θ ] .
E θ i n c = E 0 cos φ k 0 r n = 1 j n ( 2 n + 1 ) J ^ n ( k 0 r ) P n ( cos θ ) ,
{ E θ = E 0 cos φ ω m = 1 j m 2 m + 1 m ( m + 1 ) A m J ^ 1 m ( k 1 r ) P m 1 ( cos θ ) r < r 1 E θ = E 0 cos φ ω m = 1 j m 2 m + 1 m ( m + 1 ) [ B m J ^ 2 m ( k 2 r ) + C m Y ^ 2 m ( k 2 r ) ] P m 1 ( cos θ ) r 1 < r < r 2 E θ = E 0 cos φ ω m = 1 j m 2 m + 1 m ( m + 1 ) [ F m J ^ 3 m ( k 3 r ) + G m Y ^ 3 m ( k 3 r ) ] P m 1 ( cos θ ) r 2 < r < r 3 E θ = E 0 cos φ ω m = 1 j m 2 m + 1 m ( m + 1 ) [ J ^ m ( k 0 r ) + D m H ^ m ( 1 ) ( k 0 r ) ] P m 1 ( cos θ ) r > r 3 ,
E θ = E 0 cos φ ω m = 1 j m 2 m + 1 m ( m + 1 ) D m H ^ m ( 1 ) ( k 0 r ) P m 1 ( cos θ )
D m = J ^ 1 m ( k 1 r 1 ) J ^ 2 m ( k 2 r 1 ) Y ^ 2 m ( k 2 r 1 ) 0 0 0 k 1 ω ε 1 θ J ^ 1 m ( k 1 r 1 ) k 2 ω ε 2 θ J ^ 2 m ( k 2 r 1 ) k 2 ω ε 2 θ Y ^ 2 m ( k 2 r 1 ) 0 0 0 0 J ^ 2 m ( k 2 r 2 ) Y ^ 2 m ( k 2 r 2 ) J ^ 3 m ( k 3 r 2 ) Y ^ 3 m ( k 3 r 2 ) 0 0 k 2 ω ε 2 θ J ^ 2 m ( k 2 r 2 ) k 2 ω ε 2 θ Y ^ 2 m ( k 2 r 2 ) k 3 ω ε 3 θ J ^ 3 m ( k 3 r 2 ) k 3 ω ε 3 θ Y ^ 3 m ( k 3 r 2 ) 0 0 0 0 J ^ 3 m ( k 3 r 3 ) Y ^ 3 m ( k 3 r 3 ) J ^ m ( k 0 r 3 ) 0 0 0 k 3 ω ε 3 θ J ^ 3 m ( k 3 r 3 ) k 3 ω ε 3 θ Y ^ 3 m ( k 3 r 3 ) k 0 ω ε 0 J ^ m ( k 0 r 3 ) J ^ 1 m ( k 1 r 1 ) J ^ 2 m ( k 2 r 1 ) Y ^ 2 m ( k 2 r 1 ) 0 0 0 k 1 ω ε 1 θ J ^ 1 m ( k 1 r 1 ) k 2 ω ε 2 θ J ^ 2 m ( k 2 r 1 ) k 2 ω ε 2 θ Y ^ 2 m ( k 2 r 1 ) 0 0 0 0 J ^ 2 m ( k 2 r 2 ) Y ^ 2 m ( k 2 r 2 ) J ^ 3 m ( k 3 r 2 ) Y ^ 3 m ( k 3 r 2 ) 0 0 k 2 ω ε 2 θ J ^ 2 m ( k 2 r 2 ) k 2 ω ε 2 θ Y ^ 2 m ( k 2 r 2 ) k 3 ω ε 3 θ J ^ 3 m ( k 3 r 2 ) k 3 ω ε 3 θ Y ^ 3 m ( k 3 r 2 ) 0 0 0 0 J ^ 3 m ( k 3 r 3 ) Y ^ 3 m ( k 3 r 3 ) H ^ m ( 1 ) ( k 0 r 3 ) 0 0 0 k 3 ω ε 3 θ J ^ 3 m ( k 3 r 3 ) k 3 ω ε 3 θ Y ^ 3 m ( k 3 r 3 ) k 0 ω ε 0 H ^ m ( 1 ) ( k 0 r 3 ) .
σ = lim r [ 4 π r 2 | E s c | 2 | E i n c | 2 ] , C s c a = 2 π k 0 2 m = 1 ( 2 m + 1 ) | D m | 2 .
S m = J ^ m ( k e r e ) J ^ m ( k 0 r e ) k e ω ε e J ^ m ( k e r e ) k 0 ω ε 0 J ^ m ( k 0 r e ) J ^ m ( k e r e ) H ^ m ( 1 ) ( k 0 r e ) k e ω ε e J ^ m ( k e r e ) k 0 ω ε 0 H ^ m ( 1 ) ( k 0 r e ) .
( r n + 1 r n ) 2 t n + 1 + 1 = ε ( n + 1 ) θ 1 2 ( 1 + t n + 1 ) ε e ( n ) ε ( n + 1 ) θ + 1 2 t n + 1 ε e ( n ) r n + 1 3 ( 2 ε 0 + ε e ) ( ε ( n + 1 ) θ + 1 2 t n + 1 ε 0 ) + r e 3 ( ε 0 ε e ) ( ε ( n + 1 ) θ t n + 1 ε 0 ) r n + 1 3 ( 2 ε 0 + ε e ) [ ε ( n + 1 ) θ 1 2 ( 1 + t n + 1 ) ε 0 ] + r e 3 ( ε 0 ε e ) [ ε ( n + 1 ) θ + ( 1 + t n + 1 ) ε 0 ] ,
ε e ( n ) = 2 ( r n r n 1 ) 2 t n + 1 2 ε n θ 1 2 ( 1 + t n ) ε e ( n 1 ) ε n θ + 1 2 t n ε e ( n 1 ) ( 1 + t n ) ( r n r n 1 ) 2 t n + 1 + t n ε n θ 1 2 ( 1 + t n ) ε e ( n 1 ) ε n θ + 1 2 t n ε e ( n 1 ) ε n θ , ε e ( 1 ) = { 2 ε 1 θ 1 + t 1 t h e c o r e i s d i e l e c t r i c 0 t h e c o r e i s c o n d u c t o r ,
t i = 2 A R i + 0.25 0.5 ( i = 1 , 2 n + 1 ) .
σ 1 = 1 4 π 0 π 0 2 π | σ c ( θ , φ ) σ i ( θ , φ ) | sin θ d φ d θ for illusion ,
σ 2 = 1 4 π 0 π 0 2 π | σ c ( θ , φ ) | sin θ d φ d θ for invisibility ,
ε r = ε h ( 1 + f ) ε m + ( 1 f ) ε h ( 1 + f ) ε h + ( 1 f ) ε m , ε θ = f ε m + ( 1 f ) ε h ,
ε m = ε ω p 2 ω 2 j ω γ ,
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