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Transverse magnetooptic effect in multilayers applied to mapping of microwave currents

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Abstract

A sensor capable of mapping microwave (mw) currents in semiconductor circuits can be realized by exploiting magneto-optic effects (MO) at transverse magnetization (M) in ultrathin ferromagnetic or ferrimagnetic films. In the sensor, Mwould be induced in the magnetic film by the fringing fields of mw currents flowing in the semiconductor circuit along the plane of incidence. In this work, an evaluation of MO sensor performance was made for nanostructures consisting of ultrathin Fe layers sandwiched between AlN dielectric layers. The multilayer thin film stacks were grown on Si wafer substrates. The performance of the sensor systems is characterized in terms of magnetization-induced changes in the MO multilayer reflection coefficients, expressed analytically. Sensor configurations which optimize the operation at the laser wavelength of 410 nm, and which are still easy to fabricate, are proposed. Modeling predicts the strongest MO enhancement in a sensor incorporating two Fe nanolayers, each of a different thickness, formed by the layer sequence AlN/Fe/AlN/Fe/AlN/Au/Si. The use of ferrimagnetic hexagonal ferrite films with the in-plane c-axis as an alternative sensor material is also discussed.

© 2017 Optical Society of America

1. Introduction

It has been proposed to employ magneto-optical (MO) effects in ferro- or ferri-magnetic films for mapping microwave (mw) current distribution in integrated circuits (chip inspection). The mw currents generate fringing magnetic fields, which in turn cause the magnetization (M) in an adjacent magnetic film to precess [1–6]. The precessional angle, θ, is proportional to the mw current, Imw. It is advantageous that detection is contact-free and practically non-invasive. The precession-induced magnetization component, M, generates MO effects. The focus is on those MO effects which are odd in M. The MO polar Kerr effect detects the M component perpendicular to the film plane, while the MO effects at transverse or longitudinal magnetization detect the in-plane components. The configuration with polar M detects mw currents in the interface plane. It gives the strongest MO signal and the sensing can be performed with a polarized focused laser beam at arbitrary angles of incidence, φ(0). Usually, φ(0)≈0 are preferred for a good lateral resolution. The configurations with longitudinal or transverse M require φ(0)>0. The MO sensor employs in-plane static magnetic flux density field, Bappl, biasing the film close to the ferromagnetic resonance (FMR) at a desired mw frequency, f. The design must enable operation at moderate Bappl. Other sensor requirements include low mw power absorption with a strong MO response, and sufficient lateral resolution. The sensor should also be resistant against ambient effects and deposited on a thin substrate to reduce the distance between the sensor element and the semiconductor chip surface.

In present-day semiconductor circuits, the bandwidth may exceed 100 GHz. The requirement to keep Bappl reasonably low limits the material choices for the MO probe to either cubic Fe, for its high saturation magnetization, μ0Ms, or to Ba hexagonal ferrite, BaFe12O19 (BaM), with in-plane c-axis and a strong effective anisotropy field, BA. In an Fe film, the required Bappl can be evaluated from [7] fFe=γ2π[Bappl(Bappl+μ0Ms)]1/2,where γ2π×28GHz/Tesla and μ0Ms = 2.158 Tesla.

The estimate for BaM films with μ0Ms = 0.4 Tesla and BA≈1.7 Tesla using the formula [8,9], fBaM=γ2π[(Bappl+BA)(Bappl+BA+μ0Ms)]1/2,shows that for a given f the required Bappl is even lower in BaM (Fig. 1).

 figure: Fig. 1

Fig. 1 Ferromagnetic resonance frequency, f, as a function of the applied magnetic flux density, Bappl, in thin films of iron (Fe) and hexagonal ferrite (BaM).

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The present work deals with MO sensors using transverse MO effect (TMOE) designed for mapping Imw distribution in semiconductor circuits. Compared to the polar and longitudinal configurations, the operation at transverse M enables the easiest optical access, and may be done using a simpler optical element sequence which does not necessarily require a polarizer-analyzer pair. This potentially extends the working spectral range to the extreme ultraviolet regions where the lack of adequate polarizers presents difficulties [10]. The sensor operates in reflection mode, with direct laser irradiation of its surface. The sensor configuration along with the chosen Cartesian coordinate system is shown in Fig. 2. TMOE is proportional to M perpendicular to the plane of incidence and detects selectively Imw flowing in the adjustable plane of incidence. An efficient MO sensor performance requires multilayer structures with optimized layer thicknesses. The problem is illustrated on systems with Fe nanolayers as active MO elements and sandwiched between AlN dielectrics. The role of the AlN layers is to protect the Fe nanolayer(s) against ambient, and to maximize the MO response by tuning their thickness [6]. The approach can be applied to other systems including those incorporating hexagonal ferrite nanolayers.

 figure: Fig. 2

Fig. 2 Interpretation of geometry for transverse magnetization magnetooptic probe. The microwave current, Imw, the applied magnetic flux density field, Bappl, and the magnetization, M, are parallel to the y-axis. Mand Bmw denote the microwave magnetization and field components parallel to the x-axis and normal to the plane yz of light incidence.

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The performance is evaluated in terms of two characteristics: One is a complex perturbation, Δrpp, to the p-amplitude reflection coefficient, rpp; this effect is induced by the transverse magnetization, M,proportional to the microwave magnetic flux density, Bmw, |Δrpp||rpp|. There is a proportionality, |Δrpp|MImw.rpp|, characterizes the TMOE figure of merit. In the experiment, the complex Δrpp enters the ellipsometric ratio [11]. Secondly, the experimentally observable difference in the irradiation reflectance, Rpp, at ±M, i.e., ΔRpp=[Rpp(+M)Rpp(M)]/2, represents another useful sensor characteristic, which is also proportional to MImw. The parameters |Δrpp| and ΔRpp give the amplitude and power of the MOsignal delivered to the photodetector, the quantities important from the point of view of signal to noise ratio. TMOE is often evaluated in terms of the observable ratio ΔRpp/Rpp [12–16], though this parameter does not provide useful information without the knowledge of either ΔRpp or Rpp individually [17,18]. The TMOE sensor performance will be optimized for an incident plane wave polarized in the plane of incidence (p-polarized) at a convenient laser wavelength, λ = 410 nm. Here, |Δrpp| at an unprotected Fe surface peaks in the region of the principal angle of incidence, φP(0)≈72 deg, i.e., at an angle of incidence, φ(0)≈75 deg, |Δrpp|≈3.23 × 10‒3, ΔRpp peaks at φ(0)≈58 deg, ΔRpp≈1.125 × 10‒3. At the same λ, the maximum of ΔRpp/Rpp is situated at φ(0)≈68 deg and has the value ΔRpp/Rpp≈5.31 × 10‒3 [19–22]. A trade-off between lateral resolution of the polarized focused laser beam and MO signal amplitude requires smaller angles of incidence, φ(0).The TMOE sensor performance will therefore be optimized at a still acceptable φ(0) = 45 deg.

In multilayers, Δrpp can be determined using a transfer matrix approach. Here, it is sufficient to consider a multilayer structure consisting of five layers, indexed 1-5, surrounded by an isotropic ambient (0) and a substrate (6). By restricting Δrpp to terms linear in magnetization, a common approximation, Δrpp can be expressed analytically with a satisfactory precision. Then, the TMOE represents an independent component in the MO vector magnetometry affecting the diagonal elements of the Jones reflection matrix, rpp, while the polar and longitudinal components manifest themselves in the off-diagonal Jones reflection matrix elements [23–33].

In Section 2, the transfer matrix approach based on previous studies is briefly summarized [34–39], while Section 3 lists the analytical expressions for Δrpp and ΔRpp components. Section 4 provides practical sensor layer sequences with Fe and AlN on a Si substrate, leading to maxima in either |Δrpp| or ΔRpp. The discussion of results is given in the last section, Section 5. The conclusions are given in Section 6. Finally, the Appendix lists isotropic reflection and transmission coefficients required in the computing of Δrpp.

2. Transfer matrix approach

The specification of electromagnetic plane waves in multilayers at transverse magnetization employs the coordinate system with the z-axis normal to the interfaces where the plane of incidence is normal to the x-axis and to the magnetization, M=Mx. At the optical angular frequency, ω, a uniformly magnetized medium (m) with the magnetization vector parallel to the x-axis is characterized by a relative permittivity tensor

ε(m)(ω)=(εxx(m)(ω)000εyy(m)(ω)εyz(m)(ω)0εzy(m)(ω)εzz(m)(ω)).
With the restrictions to the terms of zero and first order in magnetization in the media of at least cubic symmetry, εxx(m)=εyy(m)=εzz(m)=ε0(m). Here the off-diagonal element εyz(m)(Mx)=εzy(m)(Mx)=jε1(m)(Mx)=jε1(m)(Mx). It is reasonable to assume (ε1(m)<<ε0(m)) and ε1(m)(Mx)Mx. The magnetic permeability, μ, is assumed equal to its vacuum value, μ0, a valid approximation for laser light at λ = 410 nm, even though μ changes significantly in the GHz frequency range, where Imw induces the precessional motion of M in the sensor.

The Helmholtz equation for the electric field vector E(m)=E0(m)exp[j(ωτγ(m)r)] of the plane waves propagating in the plane perpendicular to the x-axis with the propagation vector, γ(m)=(ω/c)(Nyy^+Nz(m)z^), becomes

(ε0(m)Ny2Nz(m)2)Ex(m)x^+(ε0(m)jε1(m)+NyNz(m)2Nz(m)2)Ey(m)y^+(ε0(m)+jε1(m)Ny2+NyNz(m)2)Ez(m)z^=0.
The propagation vector component, (ω/c)Nyy^, is an invariant. Here r, τ, and c denote the position vector, time and light velocity in a vacuum, x^,y^, and z^ are the unit vectors. Equation (2) provides four eigen-values of Nz(m), i.e., Nz1(m)=Nz0(m)=(ε0(m)Ny2)1/2=N(m)α(m),N(m)=ε0(m)1/2, Nz2(m)=Nz0(m) for the waves with the eigen-polarizations parallel to x^, e1,2(m)=x^, i.e., perpendicular to the plane of incidence (TE or s-polarized waves) and
Nz3(m)=Nz0(m)(1ε1(m)22ε0(m)Nz0(m)2)Nz0(m),Nz4(m)=Nz0(m)(1ε1(m)22ε0(m)Nz0(m)2)Nz0(m),
for the waves with the eigen-polarization e3,4(m)Nz0(m)2y^(NyNz3,4(m)jε1(m))z^, in the plane perpendicular to the x-axis, i.e., parallel to the plane of incidence (TM or p-polarized waves).

The multilayer problem can be dealt with rigorously using the 4 × 4 matrix formalism [34]. The case of Nz1,2(m) and e1,2(m) reduce to that of isotropic multilayers. It is therefore sufficient to consider the cases of e3,4(m) and Nz3,4(m) affected by the magnetization via ε1(m), and to reduce the formalism to that of 2 × 2 submatrices. The reduced dynamical matrix becomes

D(m_)=(Nz0(m)ε0(m)1/2Nz0(m)ε0(m)1/2ε0(m)1/2+jε1(m)NyNz0(m)1ε0(m)1/2ε0(m)1/2+jε1(m)NyNz0(m)1ε0(m)1/2)(C3(m)00C4(m)),
where C3(m) and C3(m)normalize the eigen-polarizations e3,4(m) to unity. The underlined superscript (m) indicates the medium with transverse magnetization. In the layer m, the dynamical matrix, D(m_), transforms the amplitudes of forward, E03(m_), and backward, E04(m_), propagating eigen-mode amplitudes at the front layer interface plane, z=z(m_1), into the tangential field amplitudes, E0y(m_) and H0x(m_), at the same plane, z=z(m_1),
(E0y(m_)(z(m_1))H0x(m_)(z(m_1)))=D(m_)(E03(m_)(z(m_1))E04(m_)(z(m_1))).
For a layer, the characteristic matrix relates the in-plane wave field components on the front layer boundary, z(m-1), to those on the back layer boundary, z(m),
(E0y(m_)(z(m_1))H0x(m_)(z(m_1)))=S(m_)(E0y(m_)(z(m_))H0x(m_)(z(m_))).
The characteristic matrix becomes
S(m_)=D(m_)P(m)D(m_)1=(cosβ(m)jNz0(m)ε0(m)sinβ(m)jε0(m)Nz0sinβ(m)cosβ(m))+q(m)sinβ(m)(1001),
where the TMOE parameter [20,21] is given by
q(m)(Mx)=ε1(m)(Mx)Nyε0(m)Nz0(m)=q(m)(Mx).
The product contains the propagation matrix
P(m_)=P(m)=(ejβ(m)00ejβ(m)),
where
β(m_)=β(m)=ωcNz0(m)d(m).
Here d(m) denotes the layer thickness. With the restriction to the terms of zero and first order in ε1(m), the transverse magnetization affects D(m_) while P(m_)=P(m) and β(m_)=β(m) take the values of isotropic layers.

Magneto-optic effects in multilayers consisting of N layers at transverse magnetization sandwiched between isotropic half-space (0) and the half space (N + 1) follow from 2 × 2 matrix product represented by

M=(M33M34M43M44)=D(0)1m_=1NS(m_)D(N+1_).
The reduced M matrix relates the electric fields of the incident (Ep(0)), reflected (Ep(0)),and transmitted (Ep(N+1)) p-polarized waves
(Ep(0)Ep(0))=(M33M34M43M44)(Ep(N+1)Ep(N+1)),
with eitherEp(N+1)=0 or Ep(0)=0. In some reflection problems, it is useful to account for the transverse magnetization in the half space (N + 1) represented by D(N+1_) (the case of the magnetic substrate at M). The form of D(N+1_) is given in Eq. (4). The inverse dynamical matrix of the entrance isotropic medium (0)
D(0)1=(2N(0)α(0))1(N(0)α(0)N(0)α(0))
with α(0)=cosφ(0), φ(0) denotes the angle of incidence. Then Ny=N(0)sinφ(0). The dynamical matrix of the isotropic exit medium (N + 1) is given by
D(N+1)=(α(N+1)α(N+1)N(N+1)N(N+1)),
where the cosine of the refraction angle is given by α(N+1)=Nz0(N+1)ε0(N+1)1/2. The reflection coefficient for the p-polarized wave incident from the medium (0) on a stack of layers 1 to N and the substrate N + 1 at M is given by rpp(01_N,N+1_),

rpp(01_N,N+1_)=Ep(0)Ep(0)=[M(01_N,N+1_)]43[M(01_N,N+1_)]331.

3. Analytical expressions

The formulae for a general multilayer at transverse magnetization,M,will be now applied to a five magnetic layer system on a magnetic substrate. The reflection coefficient follows from M(0123456_) represented by

M(0123456_)=D(0)1S(1_)S(2_)S(3_)S(4_)S(5_)D(6_).
Thanks to the restriction to terms linear in MxM, the total reflection coefficient, rpp(0123456_),of the structure can be expressed as a sum of components from individual layers
rpp(0123456_)=rpp(0123456)+Δrpp(01_23456)+Δrpp(012_3456)+...+Δrpp(0123456_),
where rpp(0123456) is the reflection coefficient of the corresponding isotropic system (M=0). The TMOE components are defined as
Δrpp(01_23456)=12[rpp(01_23456)(Mx)rpp(01_23456)(Mx)],Δrpp(012_3456)=12[rpp(012_3456)(Mx)rpp(012_3456)(Mx)],Δrpp(0123456_)=12[rpp(0123456_)(Mx)rpp(0123456_)(Mx)],
where
Δrpp(01_23456)=j2q(1)(1ej2β(1))(1rpp(123456)2e2jβ(1))tpp(01)tpp(10)(1rpp(10)rpp(123456)e2jβ(1))2,Δrpp(012_3456)=j2q(2)(1ej2β(2))(1rpp(23456)2e2jβ(2))tpp(012)tpp(210)(1rpp(210)rpp(23456)e2jβ(2))2,Δrpp(0123_456)=j2q(3)(1ej2β(3))(1rpp(3456)2e2jβ(3))tpp(0123)tpp(3210)(1rpp(3210)rpp(3456)e2jβ(3))2,
Δrpp(01234_56)=j2q(4)(1ej2β(4))(1rpp(456)2e2jβ(4))tpp(01234)tpp(43210)(1rpp(43210)rpp(456)e2jβ(4))2,Δrpp(012345_6)=j2q(5)(1ej2β(5))(1rpp(56)2e2jβ(5))tpp(012345)tpp(543210)(1rpp(543210)rpp(56)e2jβ(5))2,Δrpp(0123456_)=j12q(6)tpp(0123456)tpp(6543210).
They are given as a product of a corresponding TMOE parameter q(i), i = 1,…6, a factor j(1ej2β(i))/2, and the expressions constructed from reflection and transmission coefficients in isotropic multilayers (Appendix). The reflectance difference, ΔRpp, is defined as
ΔRpp(0123456_)=12[Rpp(+M)Rpp(M)]=12[rpp(0123456_)rpp(0123456_)*]+12[rpp(0123456_)rpp(0123456_)*]
The sum is approximated by
Rpp(0123456_)=12[rpp(0123456_)rpp(0123456_)*]++12[rpp(0123456_)rpp(0123456_)*]Rpp(0123456)
where Rpp(0123456)is the isotropic reflectance (M=0). It enters the expression for the ratio ΔRpp/Rpp. The total ΔRpp(0123456_) can be approximated as a sum of components originating from the layers 1-5 and the substrate (6)

ΔRpp(0123456_)12rpp(0123456)(Δrpp(01_23456)*+Δrpp(012_3456)*+...+Δrpp(0123456_)*)+12rpp(0123456)*(Δrpp(01_23456)+Δrpp(012_3456)+...+Δrpp(0123456_)).

4. Optimized sensor response

In this section, realistic configurations of TMOE sensors working in reflection mode will be evaluated at λ = 410 nm of the laser source and at φ(0) = 45 deg. The model applied to find an optimized sensor response will be demonstrated on multilayer systems with Fe and AlN layers on Si or Au/Si. The material optical and MO parameters for Fe are collected in Table 1 [19–22]. They include εxx(Fe) and εyz(Fe) defined in Eq. (1), the penetration depth, d(Fe)penetr, and q(Fe) defined in Eq. (6). For AlN, the real index of refraction is taken as N(AlN) = 1.9264 [6]. The thickness, d(λ/2) = 114.404 nm, corresponds to β(AlN) = π, Eq. (8). For Au, the relative permittivity assumes the value of ε(Au) = ‒1.70216‒5.71736j with ε(Au)1/2 = 1.46-1.958j, and the penetration depth, d(Au)penetr = 16.6633 nm [40]. The complex index of refraction is of Si, N(Si) = 5.289‒0.292j for the optically thick silicon wafer employed as a substrate [41]. The high resistivity Si is transparent for mw radiation up to terahertz frequencies [42].

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Table 1. Optical and magneto-optical parameters of Fe

The performance of sensor multilayers is evaluated in terms of their MO characteristics, |Δrpp| and ΔRpp. The maxima of |Δrpp| and ΔRpp are found by varying the thickness of layers forming the sensor. For the optimal sensor multilayers, it is interesting to record a set of additional parameters. These include the total reflectivity, Rpp, total absorbed power, App, the distribution of power dissipated in the absorbing layers, App(i) (i = 1,2,…,5), and the distribution among the Fe layers of Δrpp(i_)(including their phase relations) and ΔRpp(i_), where ΔRpp(i_)=12[(Δrpp(i_))*(rpp(0123456))+(Δrpp(i_))(rpp(0123456))*]. The conditions for maximal ΔRpp/Rpp are included.

4.1. Single Fe layer

The analysis starts with simpler structures. The thickness dependence of |Δrpp| and ΔRpp in an uncovered Fe film on Si substrate are not monotonous, but show slightly displaced flat maxima (Fig. 3). Table 2 gives the Fe thickness, dFe, required for the maximal |Δrpp|, ΔRpp, and ΔRpp/Rpp. The reflectance of the Fe film on Si as a function of dFe displays a pronounced maximum at dFe = 16 nm and a flat minimum at dFe = 61 nm.

 figure: Fig. 3

Fig. 3 Effect of the thickness, d(Fe), of the Fe layer on a Si substrate on the reflectance, Rpp, and the magneto-optic parameters, |∆rpp|, ∆Rpp, ∆Rpp/Rpp (See Table 2).

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A modest |Δrpp| and ΔRpp enhancement is achieved with a dielectric film on an optically thick Fe (Table 3).

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Table 3. Thick Fe film, dFe = 104 nm, with AlN cover, dAlN denotes the thickness of AlN cover

Both of |Δrpp| and ΔRpp are improved for optimized Fe and AlN thicknesses. The results are listed in Table 4. The optimized parameters are printed in bold.

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Table 4. AlN(d1)Fe(d2)Si structure

An attempt was made to further improve both |Δrpp| and ΔRpp by an AlN layer between Fe and Si. The results for the AlN(d1)Fe(d2)AlN(d3)Si structure are collected in Table 5. The optimization was achieved for the Fe thickness, d2 = 32 nm (Table 5). However, nosignificant improvement was achieved with respect to the simpler AlN(d1)Fe(d2)Si. Also, the replacement of the AlN layer with an Au reflector on Si was not very efficient (Table 6). The structure may be nevertheless of some interest as it avoids a more complicated Fe deposition on AlN. The value of App(Fe) shows that most power is absorbed in Fe and only a small part in Au layer.

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Table 5. AlN(d1)Fe(d2)AlN(d3)Si structure.

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Table 6. AlN(d1)Fe(d2)Au(d3)Si structure, d3 = 2 nm

Table 7 illustrates the addition of both lower AlN and Au reflector. Compared to the AlN(d1)Fe(d2)Si structure of Table 4, there is some improvement in ΔRpp, only. At the maximal ΔRpp/Rpp, the structure becomes anti-reflecting (Rpp≈0) with a low |Δrpp| and negligible ΔRpp.

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Table 7. AlN(d1)Fe(d2) AlN(d3)Au(d4)Si structure, d4 = 2 nm

In the optimized structures with a single ultrathin Fe, |Δrpp| and ΔRpp were enhanced with respect to an uncovered thick Fe film by the factors of 1.46 and 1.16, respectively.

4.2 Fe multilayers

Further increases in |Δrpp| and ΔRpp can be achieved by using structures with two or more ultrathin Fe layers. The effect is illustrated on Fe(d1)AlN(d2)Fe(d3)AlN(d4)Fe(d5)Si. Table 8 demonstrates the increase of the optimized |Δrpp| with number of Fe layers. In the optimized 3Fe system, the three Fe layers separated by AlN are of different thicknesses, the first Fe layer absorbs most power, App(1), and has the strongest MO components, i.e., |∆rpp(1)|>|∆rpp(3)|>|∆rpp(5)|, and |∆Rpp(1)|>|∆Rpp(3)|>|∆Rpp(5)|. The small difference between |∆rpp(1)| + |∆rpp(3)| + |∆rpp(5)|≈2.33 × 10‒3 and |∆rpp| = |∆rpp(1) + ∆rpp(3) + ∆rpp(5)|≈2.30 × 10‒3 indicates that the three components are almost in phase.

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Table 8. Fe(d1)AlN(d2)Fe(d3)AlN(d4)Fe(d5) structure on Si

4.3. Fe bilayers

In what follows, however, the analysis is confined to structures with Fe bilayers, as they give reasonable |Δrpp| and ΔRpp while remaining relatively easy to fabricate. The results of optimization for AlN(d1)Fe(d2)AlN(d3)Fe(d4)AlN(d5) structure on Si are collected in Table 9. The structure can be made anti-reflecting (Rpp = 4.09 × 10−5), but with |Δrpp| and ΔRpp too small for the practical sensor use. The replacement of the AlN layer on Si with an Au reflector on Si simplifies the deposition without any significant changes inperformance (Table 10). In the optimized structures with two Fe layers, |Δrpp| and ΔRpp were enhanced with respect to an uncovered thick Fe film (Table 2) by the factors of 1.78 (Table 10) and 1.55 (Table 9), respectively. The rates of decrease of |Δrpp| and ΔRpp when d1 through d5 deviate from their values found for |Δrpp|max and (ΔRpp)max follow from Eqs. (50) and (53). All characteristics are the functions of thicknesses of AlN layers, dAlN, with the period d(λ/2). In the following figures, the effect of dAlN is illustrated on the structure of Table 10 optimized for |∆rpp|max with varying d3, the thickness of the AlN spacer separating the Fe layers, i.e. on AlN(45 nm)Fe(17 nm) AlN(d3)Fe(31 nm)Au(2 nm) on Si. Figure 4 shows |∆rpp| = |∆rpp(2)| + |∆rpp(4)| and its components, |∆rpp(2)| and |∆rpp(4)|, originating from the second and fourth layers, Fe(17 nm) and Fe(31 nm), respectively. The complex ∆rpp(2) and ∆rpp(4) are exactly in phase at d3 = 93 nm (Fig. 5). The effect of d(3) on ∆Rpp and its components is shown in Fig. 6. Figures 7 and 8 display ΔRpp(d(3))/Rpp(d(3))and the optical parameters, i.e., the fractions of reflected power, Rpp(d(3)), transmitted power, Tpp(d(3)), and absorbed power, App(d(3)) and its distribution among the absorbing layers, App(2)(d(3)) and App(4)(d(3)). Inspection of Figs. 4, and 6-8 shows that the maxima of|∆rpp(d(3))| and ΔRpp(d(3)) are situated close to the maxima of Rpp(d(3)) and Tpp(d(3)) and close to the minimal App(d(3)). The maximal ΔRpp(d(3))/Rpp(d(3)) in the AlN(45 nm)Fe(17 nm)AlN(d(3))Fe(31 nm) Au(2 nm) multilayer (Fig. 7) shifts towards the minimum of Rpp(d(3)). The trends are almost the same in the structure optimized for (∆Rpp)max, i.e., in the AlN(26 nm)Fe(18 nm)AlN(d(3))Fe(29 nm)Au(2 nm) multilayer on Si, as illustrated in Fig. 9 for ΔRpp(d(3)). The ΔRpp/Rpp maxima are situated close to the Rpp minima and App maxima. As expected, the optimized |Δrpp|, ΔRpp, and ΔRpp/Rpp require low Tpp.

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Table 9. AlN(d1)Fe(d2)AlN(d3)Fe(d4)AlN(d5) structure on Si

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Table 10. AlN(d1)Fe(d2)AlN(d3)Fe(d4)Au(d5)Si structure, d5 = 2 nm

 figure: Fig. 4

Fig. 4 Absolute values of the magnetoooptic amplitude reflection coefficient, |∆rpp| = |∆rpp(2) + ∆rpp(4)|, and its components, |∆rpp(2)| and |∆rpp(4)| as functions of the thickness, d(3), of the AlN(d(3)) layer in the AlN(45 nm)Fe(17 nm)AlN(d(3))Fe(31 nm) Au(2 nm) multilayer on a Si substrate. See Table 10.

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 figure: Fig. 5

Fig. 5 Effect of the thickness, d(3), of the AlN(d(3)) layer, on |∆rpp(2)| + |∆rpp(4)|, |∆rpp(2) + ∆rpp(4)|, and their difference in the AlN(45 nm)Fe(17 nm)AlN(d(3))Fe(31 nm)Au(2 nm) multilayer on a Si substrate. See Table 10.

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 figure: Fig. 6

Fig. 6 Transverse magneto-optic reflectance difference, ∆Rpp = ∆Rpp(2) + ∆Rpp(4), and its components as functions of the thickness, d(3), of the AlN(d(3)) layer in the AlN(45 nm) Fe(17 nm) AlN(d(3)) Fe(31 nm) Au(2 nm) multilayer on a Si substrate. See Table 10.

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 figure: Fig. 7

Fig. 7 Transverse magneto-optic reflectance difference ratio, ∆Rpp/Rpp, reflectance, Rpp, and the power transmitted into the Si substrate, Tpp, in the AlN(45 nm) Fe(17 nm) AlN(d(3)) Fe(31 nm) Au(2 nm) multilayer. See Table 10.

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 figure: Fig. 8

Fig. 8 Power, App, absorbed in the AlN(45 nm) Fe(17 nm) AlN(d(3)) Fe(31 nm) Au(2 nm) multilayer on Si substrate and its distribution among the absorbing layers, Fe(d(2)), App(2), and Fe(d(4)), App(4), as functions of the thickness, d(3), of the AlN(d(3)). The power absorbed in the Au reflector, Au(d(5)) was below 0.0023 in the whole d(3) range. See Table 10.

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 figure: Fig. 9

Fig. 9 Transverse magneto-optic reflectance difference, ∆Rpp = ∆Rpp(2) + ∆Rpp(4), and its components as functions of the thickness, d(3), of the AlN(d(3)) layer in the AlN(26 nm) Fe(18 nm) AlN(d(3)) Fe(29 nm) Au(2 nm) multilayer on a Si substrate. See Table 10.

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5. Discussion

Tables 4-10 provide data required in the design of TMOE sensors with MO active Fe nanolayers operating at the wavelength of 410 nm at an angle of incidence of 45 deg. Both |∆rpp| and ∆Rpp increase in multilayers with two or more Fe nanolayers. The microwave energy losses in the sensor are expected to remain low as the total Fe thickness falls in a ten nm range. For practical reasons, the choice is restricted to structures with only one or two Fe layers, as the fabrication of structures with higher number of layers of defined thickness and low interface roughness requires more effortand cost. The simplest and cheapest solutions are represented by the structures deposited on a Si substrate with a single AlN protected Fe nanolayer, i.e., the AlN(40 nm)Fe(33 nm) bilayer optimized for |∆rpp|max≈2.77 × 10‒3 and the AlN(14 nm)Fe(31 nm) bilayer optimized for (∆Rpp)max≈1.19 × 10‒3 (Table 4). Cost effective solutions with an improved performance will employ structures on Si with the two Fe nanolayers of Table 10, i.e., the AlN(45 nm)Fe(17 nm)AlN(93 nm) Fe(31 nm)Au(2 nm) multilayer optimized for |∆rpp|max≈3.37 × 10‒3 (Fig. 4)and the AlN(26 nm)Fe(18 nm)AlN(92 nm)Fe(29 nm)Au(2 nm) multilayer optimized for (∆Rpp)max≈1.63 × 10‒3 in Fig. 9 (Table 9).

The choice of the short visible λ = 410 nm (E = 3.024 eV) of the laser source enables reasonable lateral resolution. Unfortunately, at E = 3.024 eV the function |q(E)| for Fe computed from the literature data [19–22] is close to its minimum (situated at E≈3.4 eV). In BaM, the situation is even less favorable, as shown in Fig. 10. The BaM spectrum of |q| was computed from the data by Atkinson et al. [43]. The shift of the operating wavelength to λ = 380 nm (E = 3.25 eV) would considerably improve the sensor performance. In addition to lower Bappl requirements, BaM is distinguished by a low FMR linewidth [8]. This, in principle, would enable a mw frequency selective operation. An order in magnitude lower FMR linewidth in BaM compared to Fe [9,44,45] may produce a more efficient coupling between Imw andM,and compensate for lower |q| in BaM. A practical realization of the MO sensor employing BaM with in-plane c-axis and high BA depends on the progress in technology. In the multilayer design of optimized structures, it is advantageous that BaM is compatible with oxide dielectrics and needs no protection against ambient.

 figure: Fig. 10

Fig. 10 Absolute value of the transverse magneto-optic parameter, q, for iron (Fe) and hexagonal ferrite (BaF) as a function of photon energy in eV at an angle of incidence of 45 deg.

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The analytical formulae for ∆rpp and ∆Rpp employed here in the design of TMOE sensor multilayers can be applied in other situations. These include MO magnetometry of exchange coupled layers (adjacent or coupled across a spacer), systems with coupling of pairs of magnetic layers across dielectric (AlN) or metallic (Au, Ag, Cu, Pt, Pd) spacers [31,46]. Here the system response can be compared with the model and separated into the TMOE contributions from individual layers. From them, the magnetic state of each layer can be deduced. In modeling non-uniform layers, the TMOE response can be approximated by that produced by a stack of uniform layers, which is much easier to compute. The approach may also be extended to multilayers with sandwiching layers made of plasmonic and double negative media [47–49]. The five layer system employed here can serve as a useful limiting case in the computer analysis of systems with higher number of magnetic layers.

6. Conclusions

Analytical expressions for the optical response in multilayers at transverse magnetization with up to five magnetic layers are applied to the evaluation of magnetooptic characteristics of sensors with several Fe nanolayers applied to mapping the microwave current distribution in integrated circuits with diffraction limited lateral resolution at a laser wavelength of 410 nm. The optimized sensor characteristics are expressed in terms of magnetooptic contributions to the reflected electric field amplitude, Δrpp and the reflected power ΔRpp, the parameter proportional to the energy delivered to the photodetector.

Appendix Reflection and transmission coefficients in isotropic multilayers

The reflection and transmission p-coefficients for isotropic multilayers can be obtained using transfer matrix formalism with M=0 or q(i)=0 (i=1,…6) [50–53]. Alternatively, they can be expressed analytically using the following parameters

A01=1,B01=rpp(01),C01=rpp(01),D01=1,
A02=1+rpp(01)rpp(12)e2jβ(1),B02=rpp(01)e2jβ(1)+rpp(12),C02=rpp(01)+rpp(12)e2jβ(1),D02=rpp(01)rpp(12)+e2jβ(1).
Then
A03=[(1+rpp(01)rpp(12)e2jβ(1))+(rpp(01)e2jβ(1)+rpp(12))rpp(23)e2jβ(2)]=A02+B03rpp(23)e2jβ(2),B03=[(1+rpp(01)rpp(12)e2jβ(1))rpp(23)+(rpp(01)e2jβ(1)+rpp(12))e2jβ(2)]=A02rpp(23)+B03e2jβ(2),
C03=[(rpp(01)+rpp(12)e2jβ(1))+(rpp(01)rpp(12)+e2jβ(1))rpp(23)e2jβ(2)]=C02+D02rpp(23)e2jβ(2),D03=[(rpp(01)+rpp(12)e2jβ(1))rpp(23)+(rpp(01)rpp(12)+e2jβ(1))e2jβ(2)]=C02rpp(23)+D02e2jβ(2),
and
A04=A03+B03rpp(34)e2jβ(3),B04=A03rpp(34)+B03e2jβ(3),C04=C03+D03rpp(34)e2jβ(3),D04=D03e2jβ(3)+C03rpp(34),
A05=A04+B04rpp(45)e2jβ(4),B05=A04rpp(45)+B04e2jβ(4),C05=C04+D04rpp(45)e2jβ(4),D05=D04e2jβ(4)+C04rpp(45),A06=A05+B05rpp(56)e2jβ(5),B06=A05rpp(56)+B05e2jβ(5),C06=C05+D05rpp(56)e2jβ(5),D06=D05e2jβ(5)+C05rpp(56),
and so on. The Fresnel reflection coefficients are defined as, (α(i)=cosφ(i))
rpp(i1,i)=rpp(i,i1)=N(i1)α(i)N(i)α(i1)N(i1)α(i)+N(i)α(i1),i=1,...,6.
The reflection coefficient for the wave incident from the medium (0)
rpp(0,1,...n,n+1)=C0,n+1A0,n+11,
and for the wave incident from the medium (n + 1)
rpp(n+1,n,...,1,0)=B0,n+1A0,n+11.
The transmission coefficient for the wave incident from the medium (0)
tpp(0,1,...n,n+1)=tpp(01)ejβ(1)tpp(12)ejβ(2)...tpp(n1,n)ejβ(n1)tpp(n,n+1)A0,n+11,
and for the wave incident from the medium (n + 1)
tpp(n+1,n,...,1,0)=tpp(10)ejβ(1)tpp(21)ejβ(2)...tpp(n,n1)ejβ(n1)tpp(n+1,n)A0,n+11,
where the Fresnel transmission coefficients are given by
tpp(i1,i)=2N(i1)α(i1)N(i1)α(i)+N(i)α(i1),i=1,...,6,andtpp(i,i1)=2N(i)α(i)N(i1)α(i)+N(i)α(i1),i=1,...,6.
The reflection and transmission s-coefficients for isotropic multilayers are obtained by replacing the Fresnel reflection and transmission p-coefficients by the corresponding s-coefficients
rss(i1,i)=rss(i,i1)=N(i1)α(i1)N(i)α(i)N(i1)α(i1)+N(i)α(i),i=1,...,6,
tss(i1,i)=2N(i1)α(i1)N(i1)α(i1)+N(i)α(i),i=1,...,6,
and

tss(i,i1)=2N(i)α(i)N(i1)α(i1)+N(i)α(i),i=1,...,6.

Funding

The work at Charles University was supported by Czech Science Foundation (15-21547S).

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Figures (10)

Fig. 1
Fig. 1 Ferromagnetic resonance frequency, f, as a function of the applied magnetic flux density, Bappl, in thin films of iron (Fe) and hexagonal ferrite (BaM).
Fig. 2
Fig. 2 Interpretation of geometry for transverse magnetization magnetooptic probe. The microwave current, Imw, the applied magnetic flux density field, Bappl, and the magnetization, M, are parallel to the y-axis. M and Bmw denote the microwave magnetization and field components parallel to the x-axis and normal to the plane yz of light incidence.
Fig. 3
Fig. 3 Effect of the thickness, d(Fe), of the Fe layer on a Si substrate on the reflectance, Rpp, and the magneto-optic parameters, |∆rpp|, ∆Rpp, ∆Rpp/Rpp (See Table 2).
Fig. 4
Fig. 4 Absolute values of the magnetoooptic amplitude reflection coefficient, |∆rpp| = |∆rpp(2) + ∆rpp(4)|, and its components, |∆rpp(2)| and |∆rpp(4)| as functions of the thickness, d(3), of the AlN(d(3)) layer in the AlN(45 nm)Fe(17 nm)AlN(d(3))Fe(31 nm) Au(2 nm) multilayer on a Si substrate. See Table 10.
Fig. 5
Fig. 5 Effect of the thickness, d(3), of the AlN(d(3)) layer, on |∆rpp(2)| + |∆rpp(4)|, |∆rpp(2) + ∆rpp(4)|, and their difference in the AlN(45 nm)Fe(17 nm)AlN(d(3))Fe(31 nm)Au(2 nm) multilayer on a Si substrate. See Table 10.
Fig. 6
Fig. 6 Transverse magneto-optic reflectance difference, ∆Rpp = ∆Rpp(2) + ∆Rpp(4), and its components as functions of the thickness, d(3), of the AlN(d(3)) layer in the AlN(45 nm) Fe(17 nm) AlN(d(3)) Fe(31 nm) Au(2 nm) multilayer on a Si substrate. See Table 10.
Fig. 7
Fig. 7 Transverse magneto-optic reflectance difference ratio, ∆Rpp/Rpp, reflectance, Rpp, and the power transmitted into the Si substrate, Tpp, in the AlN(45 nm) Fe(17 nm) AlN(d(3)) Fe(31 nm) Au(2 nm) multilayer. See Table 10.
Fig. 8
Fig. 8 Power, App, absorbed in the AlN(45 nm) Fe(17 nm) AlN(d(3)) Fe(31 nm) Au(2 nm) multilayer on Si substrate and its distribution among the absorbing layers, Fe(d(2)), App(2), and Fe(d(4)), App(4), as functions of the thickness, d(3), of the AlN(d(3)). The power absorbed in the Au reflector, Au(d(5)) was below 0.0023 in the whole d(3) range. See Table 10.
Fig. 9
Fig. 9 Transverse magneto-optic reflectance difference, ∆Rpp = ∆Rpp(2) + ∆Rpp(4), and its components as functions of the thickness, d(3), of the AlN(d(3)) layer in the AlN(26 nm) Fe(18 nm) AlN(d(3)) Fe(29 nm) Au(2 nm) multilayer on a Si substrate. See Table 10.
Fig. 10
Fig. 10 Absolute value of the transverse magneto-optic parameter, q, for iron (Fe) and hexagonal ferrite (BaF) as a function of photon energy in eV at an angle of incidence of 45 deg.

Tables (10)

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Table 1 Optical and magneto-optical parameters of Fe

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Table 3 Thick Fe film, dFe = 104 nm, with AlN cover, dAlN denotes the thickness of AlN cover

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Table 4 AlN(d1)Fe(d2)Si structure

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Table 5 AlN(d1)Fe(d2)AlN(d3)Si structure.

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Table 6 AlN(d1)Fe(d2)Au(d3)Si structure, d3 = 2 nm

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Table 7 AlN(d1)Fe(d2) AlN(d3)Au(d4)Si structure, d4 = 2 nm

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Table 8 Fe(d1)AlN(d2)Fe(d3)AlN(d4)Fe(d5) structure on Si

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Table 9 AlN(d1)Fe(d2)AlN(d3)Fe(d4)AlN(d5) structure on Si

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Table 10 AlN(d1)Fe(d2)AlN(d3)Fe(d4)Au(d5)Si structure, d5 = 2 nm

Equations (38)

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ε (m) ( ω )=( ε xx (m) ( ω ) 0 0 0 ε yy (m) ( ω ) ε yz (m) ( ω ) 0 ε zy (m) ( ω ) ε zz (m) ( ω ) ).
( ε 0 ( m ) N y 2 N z ( m )2 ) E x ( m ) x ^ +( ε 0 ( m ) j ε 1 ( m ) + N y N z ( m )2 N z ( m )2 ) E y ( m ) y ^ +( ε 0 ( m ) +j ε 1 ( m ) N y 2 + N y N z ( m )2 ) E z ( m ) z ^ =0.
N z3 (m) = N z0 (m) ( 1 ε 1 (m)2 2 ε 0 (m) N z0 (m)2 ) N z0 (m) , N z4 (m) = N z0 (m) ( 1 ε 1 (m)2 2 ε 0 (m) N z0 (m)2 ) N z0 (m) ,
D ( m _ ) =( N z0 (m) ε 0 (m)1/2 N z0 (m) ε 0 (m)1/2 ε 0 (m)1/2 +j ε 1 (m) N y N z0 (m)1 ε 0 (m)1/2 ε 0 (m)1/2 +j ε 1 (m) N y N z0 (m)1 ε 0 (m)1/2 )( C 3 (m) 0 0 C 4 (m) ),
( E 0y ( m _ ) ( z ( m _ 1 ) ) H 0x ( m _ ) ( z ( m _ 1 ) ) )= D ( m _ ) ( E 03 ( m _ ) ( z ( m _ 1 ) ) E 04 ( m _ ) ( z ( m _ 1 ) ) ).
( E 0y ( m _ ) ( z ( m _ 1 ) ) H 0x ( m _ ) ( z ( m _ 1 ) ) )= S ( m _ ) ( E 0y ( m _ ) ( z ( m _ ) ) H 0x ( m _ ) ( z ( m _ ) ) ).
S ( m _ ) = D ( m _ ) P (m) D ( m _ )1 =( cos β (m) j N z0 (m) ε 0 (m) sin β (m) j ε 0 (m) N z0 sin β (m) cos β (m) )+ q ( m ) sin β (m) ( 1 0 0 1 ),
q (m) ( M x )= ε 1 (m) ( M x ) N y ε 0 (m) N z0 (m) = q (m) ( M x ).
P ( m _ ) = P (m) =( e j β ( m ) 0 0 e j β ( m ) ),
β ( m _ ) = β ( m ) = ω c N z0 ( m ) d ( m ) .
M=( M 33 M 34 M 43 M 44 )= D (0)1 m _ =1 N S ( m _ ) D ( N+1 _ ) .
( E p ( 0 ) E p ( 0 ) )=( M 33 M 34 M 43 M 44 )( E p ( N+1 ) E p ( N+1 ) ),
D (0)1 = ( 2 N (0) α (0) ) 1 ( N (0) α (0) N (0) α (0) )
D (N+1) =( α ( N+1 ) α ( N+1 ) N ( N+1 ) N ( N+1 ) ),
r p p ( 0 1 _ N , N + 1 _ ) = E p ( 0 ) E p ( 0 ) = [ M ( 0 1 _ N , N + 1 _ ) ] 43 [ M ( 0 1 _ N , N + 1 _ ) ] 33 1 .
M ( 0 123456 _ ) = D (0)1 S ( 1 _ ) S ( 2 _ ) S ( 3 _ ) S ( 4 _ ) S ( 5 _ ) D ( 6 _ ) .
r pp ( 0 123456 _ ) = r pp ( 0123456 ) +Δ r pp ( 0 1 _ 23456 ) +Δ r pp ( 01 2 _ 3456 ) +...+Δ r pp ( 012345 6 _ ) ,
Δ r pp ( 0 1 _ 23456 ) = 1 2 [ r pp ( 0 1 _ 23456 ) ( M x ) r pp ( 0 1 _ 23456 ) ( M x ) ], Δ r pp ( 01 2 _ 3456 ) = 1 2 [ r pp ( 01 2 _ 3456 ) ( M x ) r pp ( 01 2 _ 3456 ) ( M x ) ], Δ r pp ( 012345 6 _ ) = 1 2 [ r pp ( 012345 6 _ ) ( M x ) r pp ( 012345 6 _ ) ( M x ) ],
Δ r pp ( 0 1 _ 23456 ) = j 2 q (1) ( 1 e j2 β (1) )( 1 r pp (123456)2 e 2j β (1) ) t pp (01) t pp (10) ( 1 r pp (10) r pp (123456) e 2j β (1) ) 2 , Δ r pp ( 01 2 _ 3456 ) = j 2 q (2) ( 1 e j2 β (2) )( 1 r pp (23456)2 e 2j β (2) ) t pp (012) t pp (210) ( 1 r pp (210) r pp (23456) e 2j β (2) ) 2 , Δ r pp ( 012 3 _ 456 ) = j 2 q (3) ( 1 e j2 β (3) )( 1 r pp (3456)2 e 2j β (3) ) t pp (0123) t pp (3210) ( 1 r pp (3210) r pp (3456) e 2j β (3) ) 2 ,
Δ r pp ( 0123 4 _ 56 ) = j 2 q (4) ( 1 e j2 β (4) )( 1 r pp (456)2 e 2j β (4) ) t pp (01234) t pp (43210) ( 1 r pp (43210) r pp (456) e 2j β (4) ) 2 , Δ r pp ( 01234 5 _ 6 ) = j 2 q (5) ( 1 e j2 β (5) )( 1 r pp ( 56 )2 e 2j β (5) ) t pp (012345) t pp (543210) ( 1 r pp ( 543210 ) r pp (56) e 2j β (5) ) 2 , Δ r pp ( 012345 6 _ ) =j 1 2 q (6) t pp (0123456) t pp (6543210) .
Δ R pp ( 0 123456 _ ) = 1 2 [ R pp ( + M ) R pp ( M ) ]= 1 2 [ r pp ( 0 123456 _ ) r pp ( 0 123456 _ )* ] + 1 2 [ r pp ( 0 123456 _ ) r pp ( 0 123456 _ )* ]
R pp ( 0 123456 _ ) = 1 2 [ r pp ( 0 123456 _ ) r pp ( 0 123456 _ )* ] + + 1 2 [ r pp ( 0 123456 _ ) r pp ( 0 123456 _ )* ] R pp ( 0123456 )
Δ R p p ( 0 123456 _ ) 1 2 r p p ( 0123456 ) ( Δ r p p ( 0 1 _ 23456 ) * + Δ r p p ( 01 2 _ 3456 ) * + ... + Δ r p p ( 012345 6 _ ) * ) + 1 2 r p p ( 0123456 ) * ( Δ r p p ( 0 1 _ 23456 ) + Δ r p p ( 01 2 _ 3456 ) + ... + Δ r p p ( 012345 6 _ ) ) .
A 01 =1, B 01 = r pp (01) , C 01 = r pp (01) , D 01 =1,
A 02 =1+ r pp (01) r pp (12) e 2j β (1) , B 02 = r pp (01) e 2j β (1) + r pp (12) , C 02 = r pp (01) + r pp (12) e 2j β (1) , D 02 = r pp (01) r pp (12) + e 2j β (1) .
A 03 =[ ( 1+ r pp (01) r pp (12) e 2j β (1) )+( r pp (01) e 2j β (1) + r pp (12) ) r pp (23) e 2j β (2) ]= A 02 + B 03 r pp (23) e 2j β (2) , B 03 =[ ( 1+ r pp (01) r pp (12) e 2j β (1) ) r pp (23) +( r pp (01) e 2j β (1) + r pp (12) ) e 2j β (2) ]= A 02 r pp (23) + B 03 e 2j β (2) ,
C 03 =[ ( r pp (01) + r pp (12) e 2j β (1) )+( r pp (01) r pp (12) + e 2j β (1) ) r pp (23) e 2j β (2) ]= C 02 + D 02 r pp (23) e 2j β (2) , D 03 =[ ( r pp (01) + r pp (12) e 2j β (1) ) r pp (23) +( r pp (01) r pp (12) + e 2j β (1) ) e 2j β (2) ]= C 02 r pp (23) + D 02 e 2j β (2) ,
A 04 = A 03 + B 03 r pp (34) e 2j β (3) , B 04 = A 03 r pp (34) + B 03 e 2j β (3) , C 04 = C 03 + D 03 r pp (34) e 2j β (3) , D 04 = D 03 e 2j β (3) + C 03 r pp (34) ,
A 05 = A 04 + B 04 r pp (45) e 2j β (4) , B 05 = A 04 r pp (45) + B 04 e 2j β (4) , C 05 = C 04 + D 04 r pp (45) e 2j β (4) , D 05 = D 04 e 2j β (4) + C 04 r pp (45) , A 06 = A 05 + B 05 r pp (56) e 2j β (5) , B 06 = A 05 r pp (56) + B 05 e 2j β (5) , C 06 = C 05 + D 05 r pp (56) e 2j β (5) , D 06 = D 05 e 2j β (5) + C 05 r pp (56) ,
r pp (i1,i) = r pp (i,i1) = N ( i1 ) α ( i ) N ( i ) α ( i1 ) N ( i1 ) α ( i ) + N ( i ) α ( i1 ) , i=1,...,6.
r pp ( 0,1,...n,n+1 ) = C 0,n+1 A 0,n+1 1 ,
r pp ( n+1,n,...,1,0 ) = B 0,n+1 A 0,n+1 1 .
t pp ( 0,1,...n,n+1 ) = t pp (01) e j β (1) t pp (12) e j β (2) ... t pp (n1,n) e j β (n1) t pp (n,n+1) A 0,n+1 1 ,
t pp ( n+1,n,...,1,0 ) = t pp (10) e j β (1) t pp (21) e j β (2) ... t pp (n,n1) e j β (n1) t pp (n+1,n) A 0,n+1 1 ,
t pp (i1,i) = 2 N ( i1 ) α ( i1 ) N ( i1 ) α ( i ) + N ( i ) α ( i1 ) , i=1,...,6, and t pp (i,i1) = 2 N ( i ) α ( i ) N ( i1 ) α ( i ) + N ( i ) α ( i1 ) , i=1,...,6.
r ss (i1,i) = r ss (i,i1) = N ( i1 ) α ( i1 ) N ( i ) α ( i ) N ( i1 ) α ( i1 ) + N ( i ) α ( i ) , i=1,...,6,
t ss (i1,i) = 2 N ( i1 ) α ( i1 ) N ( i1 ) α ( i1 ) + N ( i ) α ( i ) , i=1,...,6,
t s s ( i , i 1 ) = 2 N ( i ) α ( i ) N ( i 1 ) α ( i 1 ) + N ( i ) α ( i ) , i = 1 , ... , 6.
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