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Diffractively coupled Fabry-Perot resonator with power-recycling

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Abstract

We demonstrate the optical coupling of two cavities without light transmission through a substrate. As the all-reflective coupling component, we use a dielectric low-efficiency 3-port diffraction grating. In contrast to a conventional transmissive coupling component, such an all-reflective coupler avoids all thermal effects that are associated with light absorption in the substrate. An all-reflective scheme for cavity coupling is of interest in the field of gravitational wave detection. In such detectors light that is resonantly enhanced inside the so-called power-recycling cavity is coupled to (kilometre-scale) Fabry-Perot resonators representing the arms of a Michelson interferometer. We realized such an all-reflective coupling in a table-top experiment. Our findings are in qualitative agreement with the theoretical model incorporating the characteristics of the 3-port grating used, and therefore encourage the application of all-reflective cavity couplers in future gravitational wave detectors.

©2011 Optical Society of America

1. Introduction

Over the past several years an international network of laser-interferometric gravitational wave (GW) detectors has been built [13]. The detectors have reached sensitivities at or close to their design sensitivities; however, the first detection of a gravitational wave has not yet been achieved. Sensitivity upgrades of existing detectors are in progress [46] while new detectors such as the Japanese LCGT are being built [7], a southern hemisphere detector AIGO has been proposed [8] and investigations towards the third generation like the European Einstein Telescope are being carried out [9].

Present and also planned GW detectors are based on Michelson interferometers, which incorporate coupled optical cavities to improve their shot noise limited sensitivity. Fabry-Perot arm resonators coupled to a so-called power-recycling resonator provide very high light power build-ups inside the interferometer without decreasing the bandwidth too much. Figure 1 shows such an interferometer layout [1014]. For future detectors with further increased light power build-ups the optical absorption of the transmissive optics might become a sensitivity limiting problem. Light absorption in the substrates causes thermal effects like thermal lensing and photo-thermo-refractive noise [1517], and will therefore lead to an upper limit for the circulating power. This concerns the balanced beamsplitter and the coupling mirrors to the interferometer arm resonators (see Fig. 1). To reduce the absorption in substrates all-reflective technologies have been proposed and realized [1821]. The proposals rely on replacing the transmissive components with micro-structured dielectric reflection gratings that avoid any light transmission through the substrate. As another profiting aspect, all-reflective technologies allow the use of alternative materials with favourable mechanical and thermal properties [23] but possibly higher optical absorption. In [24] the all-reflective replacement of the balanced beamsplitter of a Michelson-type interferometer with an appropriate diffraction grating [25] was demonstrated experimentally. All-reflective cavity couplers proposed can be divided into 2-port-couplers operated in first-order Littrow arrangement, as realized in [19, 20], and 3-port-couplers operated in second-order Littrow arrangement, as realized in [21]. In [22] a diffractively coupled cavity in a suspended environment has been demonstrated. Generally, the 3-port grating introduces an additional port that potentially acts as an additional loss channel; however, it relies on only low diffraction efficiencies and correspondingly shallow grating structures, which suggests that cavities with well-defined Gaussian TEM00 modes and very high finesse values are feasible.

 figure: Fig. 1

Fig. 1 Michelson-type interferometer with power-recycling cavity and arm resonators. The transmissive beamsplitter (BS) and the coupling mirrors to the arm cavities (CMn) are exposed to high thermal load (red blur). Each arm cavity (coupling mirror CMn and end mirror EMn) together with the power-recycling mirror (PRM) forms a system of two coupled cavities.

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Here, we experimentally demonstrate the all-reflective coupling of a Fabry-Perot resonator with a power-recycling resonator. The coupling component is a custom made dielectric low-efficiency 3-port diffraction grating. Based on the theoretical analysis in [26] and the experimentally determined diffraction efficiencies and losses of the grating, we simulate the light powers at all three output ports of the coupled cavity system in dependence of the cavity detunings. The experimental observations show qualitative agreement with our theoretical model.

In the following we first start with a brief theoretical description of the coupled cavity system and also discuss our interferometer topology and requirements for the mode matching of the elliptical beam profiles involved.

2. 3-port grating coupled cavities

In contrast to a conventional coupling mirror, the 3-port grating couples an incoming beam into three instead of two output ports. Figure 2(a) shows a 3-port grating mounted in second-order Littrow configuration. The amplitude diffraction efficiencies of each diffraction order are denoted ηn and the amplitude reflectivity under normal incidence ρ 0, respectively. The arm cavity is then established perpendicular to the grating surface with a small first order diffraction efficiency as the coupling efficiency to the cavity [see Fig. 2(b)].

 figure: Fig. 2

Fig. 2 (a) 3-port grating in second-order Littrow mount. The amplitude diffraction efficiencies are denoted ηn and reflectivity under normal incidence ρ 0, respectively. (b) By inserting a mirror (EM) perpendicular to the grating a 3-port-grating cavity is generated, with the diffraction efficiency η 1 as the coupling efficiency. The light fields are labeled as follows: The backwards reflected field towards the laser source C1, the intra-cavity field C2, the forward reflected field at the additional grating port C3 and the transmitted field T. (c) Inserting the power-recycling mirror PRM in the entrance, a power-recycled 3-port grating coupled cavity is formed. The light fields are denoted C1PR, C2PR, C3PR and TPR.

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The back- and forward-reflected ports are denoted C1 and C3. In [27] the phase relations for a binary structured grating without asymmetry (blaze) were derived for the lossless case. For a Fabry-Perot cavity with a 3-port grating as the coupling component as shown in Fig. 2(b) the amplitude reflection coefficients for the back-reflected field c 1, the forward-reflected field c 3 as well as the amplitudes for the intra-cavity field c 2 and the transmitted field t are described as

c1=η2exp(iϕ2)+η12ρ2exp[i2(ϕ1+Φ2)]d2,
c2=η1exp(iϕ1)d2,
c3=η0+η12ρ2exp[i2(ϕ1+Φ2)]d2,
t=iτ2exp(iΦ2)c2,
where the amplitude reflectance and transmittance of the cavity end mirror as the second component are given by ρ 2 and τ 2, respectively. The resonance factor is given by d 2 = [1 − ρ 0 ρ 2 exp (i2Φ2)]−1, and the length L 2 of the grating cavity is expressed by the detuning parameter Φ2 = ωL 2/c, where ω is the angular frequency and c the speed of light. One possible set for the phase shifts of each diffraction order are
ϕ0=0,
ϕ1=1/2arccos((η122η02)/2ρ0η0),
ϕ2=arccos(η12/(2η2η0)).
Since the phase shifts depend on the diffraction efficiencies one can derive a minimal/maximal diffraction efficiency for the zeroth and second diffraction order η 0/2 = (1 ± ρ 0)/2. As a consequence the symmetric 3-port diffraction grating can be designed and manufactured with diffraction efficiencies only within these boundaries. However, independently from the grating’s specific diffraction efficiencies the implementation of an additional power-recycling mirror with the amplitude coefficients ρ 1 and τ 1 between the laser source and the grating forms two coupled resonators [see Fig. 2(c)]. In the following we will denote the first cavity, formed by the PR mirror and the grating, as the power-recycling cavity (PR cavity), with its parameters Φ1, L 1 and d 1, and the second cavity, formed by the grating and the end mirror, as the arm cavity, with its parameters Φ2, L 2 and d 2 given above. For such a system the amplitude reflection coefficients for the back-reflected field c 1PR, the forward-reflected field c 3PR, the intra-cavity field of the arm cavity c 2PR and the transmitted field t PR are
c1PR=[ρ1c1exp(i2Φ1)]d1,
c2PR=iτ1exp[i(Φ1+Φ2)]c2d1,
c3PR=iτ1exp(iΦ1)c3d1,
tPR=τ1τ2exp[i(Φ1+Φ2)]c2d1,
where cn are the amplitude reflection coefficients of the two-component cavity given above. The resonance factor of the PR cavity is given by d 1 = [1 – ρ 1 c 1 exp (i2Φ1)]−1, and the length L 1 of the PR cavity is expressed by the detuning parameter Φ1 = ω L 1/c. A more detailed deduction and the theoretical investigation of the system can be found in [26].

In current gravitational wave detectors the arm cavities are standing-wave cavities with an amplitude reflectivity of the end mirror of ρ221. Such a cavity always reflects the light back into the PR resonator, independently from the detuning of the cavity. This is in contrast to a 3-port-grating coupled cavity with the additional port C3. Hence, the light fields, that are back-reflected from the grating cavity and thus recoupled to the PR cavity, firstly depend on the grating-specific diffraction efficiencies and, secondly, on the tuning of the grating cavity. Note that the light amplitude reflected from the grating cavity c 1 [as given in Eq. (1)], can be seen as the compound component reflectivity ρ c2) of the grating and the end mirror [26]. In consequence the overall power build-up inside both cavities finally depends on the detuning of the PR cavity Φ1 and the detuning of the arm cavity Φ2. The additional third port C3PR is a loss channel showing a characteristic behavior which we present and discuss in the following experiment.

3. Geometrical considerations

Diffraction at a grating into an order > 0 changes the geometrical parameters of a gaussian beam if the angle of incidence and the diffraction angle are different. This leads to restrictions to the geometrical setup of a power-recycled 3-port-grating cavity for a stable resonator.

The arm cavity is a half-symmetric resonator consisting of a spherical end mirror (m) and a flat grating (g). The two components form a stable resonator if the stability criterion is fulfilled:

0gggm1
with
gg=1L2Rc,g=1andgm=1L2Rc,m,
where Rc, m denotes the radius of curvature of the end mirror and L 2 the length of the arm cavity as the second cavity of the system. Note, that the factor g g of the flat grating is unity, due to R c,g = ∞, whereas for the g-factor of the mirror g m, the unequality L 2 < R c,m has to be fulfilled to meet the stability criterion. In a half-symmetric resonator the beam waist of the round eigenmode of the cavity is positioned at the flat component [28] with a waist size
w02=L2λπgm1gm.

If a monochromatic TEM00 gaussian beam with round beam profile is incident on a grating in second-order Littrow configuration, the beam that is diffracted into the first diffraction order at an emergent angle of 0° will be elliptical. The angle of incidence (θ in) does not match the emergent angle (θ out) which results in a distortion of the gaussian beam profile in one dimension. The relation between the waist size of input and output beam in the affected dimension is given by:

wout=cos(θout)cos(θin)win.
Therefore the ratio between the x- and y-direction waist sizes is completely determined by the second-order Littrow angle (here 47.2°). In order to match the mode of the incoming beam to the round eigenmode of the arm cavity, the incident beam needs to have a degree of ellipticity that exactly compensates the beam deformation that is applied to the beam when diffracted into the first order. As a consequence the radii of curvature of the PR mirror need to be different in x- and y- direction, because the eigenmode of the power-recycling cavity is elliptical. For a given eigenmode of the arm cavity and length of the recycling cavity L 1, the desired radii of curvature of the recycling mirror are given by:
Rc,y=L1+π2w0,y4λ2L1,
Rc,x=L1+π2w0,x4λ2L1=L1+π2w0,y4λ2L1(cosθin)4.

The geometrical configuration of our experiment is shown in Fig. 3.

 figure: Fig. 3

Fig. 3 Geometrical configuration of the experiment. The second-order Littrow angle θ in determines the ratio of the waist size at the grating in horizontal and vertical direction w 0,x and w 0,y. The length of the arm L 2 and the radius of curvature of the end mirror R c defines the absolute waist size at the grating. Together with the length of the power-recycling cavity L 1 these parameters determine the radii of curvature of the PR mirror R c,x and R c,y.

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4. Experimental setup

The experimental setup is shown in Fig. 4. Light from a Nd:YAG laser was spatially filtered by a ring-mode-cleaner [29]. An electro-optical modulator (EOM) generated a 15 MHz phase modulation for a Pound-Drever-Hall (PDH) lock [30] of the cavity lengths. We designed and fabricated [31] a binary dielectric reflection 3-port grating with close to minimal second-order diffraction efficiency. We chose a grating period of 1450 nm, which provided a second-order Littrow angle of θ in = 47.2° and a first oder diffraction angle of θ out = 0° at the laser wavelength of 1064 nm. For each dimension two cylindrical lenses were employed to generate the elliptical beam profile that is needed in order to mode-match the incoming beam to the eigenmode of the recycling cavity. The table-top experiment was carried out under air, and the cavity and mirror parameters, including the custom made PR mirror having different radii of curvature in horizontal and vertical direction, were chosen as described in the previous section and shown in Fig. 3. A dieletric multilayer system was applied to the PR mirror providing a reflectivity of ρ12=0.96. The high-reflectivity end mirror had a transmissivity of τ22=7ppm. The PR mirror as well as the end mirror were mounted onto a piezo-electrical transducer (PZT) to linearly sweep the cavity lengths.

 figure: Fig. 4

Fig. 4 Experimental setup of a 3-port-grating cavity with power-recycling. Two cylindrical lenses for each dimension ln are needed to provide mode-matching to the eigenmode of the cavity. The spherical lens l0 compensates the distortion due to the PRM substrate. Photodiodes at the ports (PDC n) and in transmission of the grating PDGT allow monitoring. The beamsplitter BS in the entrance allows access to the back-reflected field C1PR.

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Initially the grating was characterized via a finesse measurement using the setup discussed in [20]. The diffraction efficiencies of the grating for s-polarized light were found to be η02=0.927±0.045, η12=0.0591±0.003 and η22=0.0001±50ppm and the reflectivity of the grating for normal incidence was ρ02=0.879±0.003. The total optical loss of the grating due to scattering, absorption and residual transmission was determined to A = 0.0027 ± 0.0061. The grating transmission was independently measured and was found to be τ02=123ppm. We used the light transmitted through the grating to monitor the power inside the arm cavity.

When the PR mirror was misaligned with respect to the actual optical axis of the recycling cavity (e.g. tilted), the mirror acted as an attenuator in front of the arm cavity. In this configuration the arm cavity properties could be determined without being influenced by the recycling cavity. The finesse of the arm cavity was found to be arm = 49.3 deduced from the measured line-width of FWHMarm = 3.73MHz. In a second step we re-aligned the PR mirror and locked the arm cavity length on resonance using the standard PDH method. We then scanned the length of the power-recycling cavity and also determined the finesse of the recycling cavity. Note that in this configuration the stabilized arm cavity acted as compound cavity end mirror with reflectivity ρ c2 = 0) [26]. The measured linewidths of the recycling cavity of FWHMPR = 5.79MHz yielded a finesse of PR = 52.3.

5. Power-recycling and cavity detunings

In this section we present measurements of the light power inside the arm cavity and at the two output ports of the coupled cavity system versus the detunings of the arm cavity and the PR cavity, respectively. We compare our results with a model that is based on Eqs. (1)(11) and measured diffraction efficiencies, mirror reflectivities and losses of the optical components. Note that our theoretical description of the 3-port-grating assumes zero optical loss [27]. In order to account for grating loss our model used a transmission of the arm cavity end mirror that was slightly higher than the actually measured one. Nevertheless, quantitative differences between our model and our experiment are still expected due to the imperfect matching of input and cavity modes, respectively.

Generally, the state of the coupled optical system depends on the detuning of both cavities Φ1 and Φ2. We therefore present the results of our model as three-dimensional plots showing light powers versus detunings [26]. However, in our measurement the detunings were not stabilized to certain points of the phase space but swept by applying sinusoidal voltages to piezo-electric transducers behind the cavity mirrors. One of the cavity detunings was varied slowly with a frequency below 1 Hz, whereas the other was varied fast with a frequency of about 1 kHz. From this procedure we derived two-dimensional plots showing light power versus the one detuning that was varied slowly. However, for any value of the slowly varied detuning, the voltage from the respective photo diode was sampled with a sufficiently high sampling rate (over 500000 data points per acquisition) to be able to pick its extreme values that occurred due to the fast varied detuning. The measured two-dimensional plots therefore correspond to a projection of our three-dimensional plot onto one of the detuning axes thereby collecting all maxima and minima along the other axis. The theoretical pictures for comparison with the experimental data corresponds to ‘side-views’ onto the plain in the three-dimensional plot along one or the other detuning axis. Note, that we have chosen the side-view-methodology as a compact description of the experiment without introducing challenging requirements to the control loop’s precision and stability. The alternative would have been to subsequently lock the experiment to all possible combinations of cavity detunings and map out the parameter space in Figs. 5(a) and 6(a).

 figure: Fig. 5

Fig. 5 Intra-cavity power build-up in the arm cavity as a function of the detunings Φ1 and Φ2 of the PR cavity and the arm cavity, respectively. Plot (a) shows the 2-dimensional simulation. Plots (b) and (c) are projections onto one of the axes, respectively. They well reproduce the experimental data as given in plots (d) and (e). The latter two show the intra-cavity powers transmitted through the grating as detected by photo diode PDGT. For both plots one of the cavity lengths was varied slowly whereas the other was varied fast.

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 figure: Fig. 6

Fig. 6 Output power at the additional grating port C3PR as a function of the detunings Φ1 and Φ2 of the power-recycling cavity and the arm cavity, respectively. Plot (a) shows the 2-dimensional simulation. Plots (b) and (c) are projections onto one of the axes, respectively. They well reproduce the experimental data as given in plots (d) and (e). The latter two show the output powers as detected by photo diode PDC3. For both plots one of the cavity lengths was varied slowly whereas the other was varied fast. The different peak heights in Fig. (d) were due to non-linearities in the PZTs used to vary the cavity lengths.

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Figure 5 presents the simulated values of the intra-cavity power versus detunings and the light power as detected by photo diode PDGT when varying the detunings in the way described before. The resonance pattern of Fig. 5(a) is periodic in Φ1 modπ and in Φ2 modπ. Power enhancement is present around a maximum at Φ1 = 90° and Φ2 = 0°. These phases are a consequence of the grating phase relations as introduced earlier, and account for 3-port gratings with a (close to) minimal value for the second order diffraction efficiency η22 [26]. Simulated and experimental data in Fig. 5(b), 5(c), and 5(d), 5(e), respectively, show a very good qualitative agreement. The existence of isolated, equidistant resonances in Fig. 5 is a special property of the optical cavity system as investigated here, and is in contrast to a conventional three-mirror cavity (confer Refs. [26, 32]). It is in fact a direct consequence of the additional port C3. In order to gain a high power build-up in the arm cavity, output at this port has to be avoided. This happens only if the detunings of the subsystem cavities have particular values (modulo π) providing destructive interference between the field from the power-recycling mirror and the field leaking out the arm cavity.

A stable operation of our cavity system at arbitrary points in phase space was not realized, however, it was realized at the point of maximum power build-up in the arm cavity. The error signal for the PDH length stabilization of the power-recycling cavity was generated from the output of photo-diode PDC1. The light power on photo-diode PDGT and the known transmissivity of the grating then allowed to determine the light power inside the arm cavity. Our simulations predicted an additional power build-up due to power-recycling by a factor of 24; however, the measured value was only 16 times higher than the independently measured power build-up inside the arm cavity without power-recycling. This deviation mainly originated from imperfect matching of the light’s input mode and the cavity modes, and experimental instabilities. The cavity system was realized as a table-top experiment under air, which caused jitter of the input beam as well as length fluctuations and which were not fully compensated by our control loops. Therefore, on an average a larger amount of light was reflected at the PR mirror. By contrast the simulation assumed perfect mode-matching.

Figure 6 presents the characterization of the additional port C3 of our cavity system. It shows simulated and measured light power leaving the coupled system at port C3. Again simulated and measured data show a high degree of agreement. In Fig. 6(a) it can be seen that for the detunings that provide the highest power build-up in the arm cavity a minimum light power is coupled out via port C3. Due to our measurement procedure this minimum is visible only in the projection onto detuning Φ1. However, stabilizing both cavities to the phase space point of maximum power inside the arm cavity, as described above, clearly provided a minimum light power at port C3. The doublet structure of the resonance in Fig. 6 is due to the power-recycling effect. When both cavities are far detuned from resonance most of the light is back-reflected towards the laser source. If the arm cavity is on resonance considerable power build-ups occur for a relatively wide range of detunings of the power-recycling cavity. But only for the optimum detuning of the power-recycling cavity (Φ1 = 90°) destructive interference occurs in port C3 giving rise to the sharp dip as shown in Fig. 6(d).

6. Conclusion

We have demonstrated the diffractive coupling of two optical resonators. In full agreement with our theoretical work in [26] we have experimentally shown that a dielectric 3-port grating can replace the transmissive coupling mirror located between a power-recycling cavity and a Fabry-Perot arm cavity as used in gravitational wave detectors. In combination with an all-reflective balanced beam splitter as demonstrated recently [24], a power-recycled Michelson interferometer is feasible without having to transmit high powers through internal optical components, as shown in Fig. 1. Although a 3-port grating as a coupling component of two resonators opens an additional port, which is the third grating port C3, a significant power-recycling factor was achieved. Almost no power was lost into the additional port due to destructive interference if the detunings of the two resonators were chosen properly. Since a 3-port grating introduces elliptical beam profiles the mode-matching of the coupled cavities was challenging; however, it could be efficiently realized utilizing a PR mirror with two different radii of curvature in horizontal and vertical dimension. A 3-port grating combines three, instead of the two light fields at each port. We have carried out a simulation based on measured parameters of the optical components and found good qualitative agreement between simulated and measured data.

Acknowledgments

This work has been supported by Deutsche Forschungsgemeinschaft within the Sonderforschungsbereich TR7 and the Excellence Cluster QUEST, the IMPRS on Gravitational Wave Astronomy and the ET design study supported by the European Commission under FP7 (Grant Agreement 211743).

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Figures (6)

Fig. 1
Fig. 1 Michelson-type interferometer with power-recycling cavity and arm resonators. The transmissive beamsplitter (BS) and the coupling mirrors to the arm cavities (CMn) are exposed to high thermal load (red blur). Each arm cavity (coupling mirror CMn and end mirror EMn) together with the power-recycling mirror (PRM) forms a system of two coupled cavities.
Fig. 2
Fig. 2 (a) 3-port grating in second-order Littrow mount. The amplitude diffraction efficiencies are denoted ηn and reflectivity under normal incidence ρ 0, respectively. (b) By inserting a mirror (EM) perpendicular to the grating a 3-port-grating cavity is generated, with the diffraction efficiency η 1 as the coupling efficiency. The light fields are labeled as follows: The backwards reflected field towards the laser source C1, the intra-cavity field C2, the forward reflected field at the additional grating port C3 and the transmitted field T. (c) Inserting the power-recycling mirror PRM in the entrance, a power-recycled 3-port grating coupled cavity is formed. The light fields are denoted C1PR, C2PR, C3PR and TPR.
Fig. 3
Fig. 3 Geometrical configuration of the experiment. The second-order Littrow angle θ in determines the ratio of the waist size at the grating in horizontal and vertical direction w 0,x and w 0,y. The length of the arm L 2 and the radius of curvature of the end mirror R c defines the absolute waist size at the grating. Together with the length of the power-recycling cavity L 1 these parameters determine the radii of curvature of the PR mirror R c,x and R c,y.
Fig. 4
Fig. 4 Experimental setup of a 3-port-grating cavity with power-recycling. Two cylindrical lenses for each dimension l n are needed to provide mode-matching to the eigenmode of the cavity. The spherical lens l0 compensates the distortion due to the PRM substrate. Photodiodes at the ports (PDC n ) and in transmission of the grating PDGT allow monitoring. The beamsplitter BS in the entrance allows access to the back-reflected field C1PR.
Fig. 5
Fig. 5 Intra-cavity power build-up in the arm cavity as a function of the detunings Φ1 and Φ2 of the PR cavity and the arm cavity, respectively. Plot (a) shows the 2-dimensional simulation. Plots (b) and (c) are projections onto one of the axes, respectively. They well reproduce the experimental data as given in plots (d) and (e). The latter two show the intra-cavity powers transmitted through the grating as detected by photo diode PDGT. For both plots one of the cavity lengths was varied slowly whereas the other was varied fast.
Fig. 6
Fig. 6 Output power at the additional grating port C3PR as a function of the detunings Φ1 and Φ2 of the power-recycling cavity and the arm cavity, respectively. Plot (a) shows the 2-dimensional simulation. Plots (b) and (c) are projections onto one of the axes, respectively. They well reproduce the experimental data as given in plots (d) and (e). The latter two show the output powers as detected by photo diode PDC3. For both plots one of the cavity lengths was varied slowly whereas the other was varied fast. The different peak heights in Fig. (d) were due to non-linearities in the PZTs used to vary the cavity lengths.

Equations (17)

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c 1 = η 2 exp ( i ϕ 2 ) + η 1 2 ρ 2 exp [ i 2 ( ϕ 1 + Φ 2 ) ] d 2 ,
c 2 = η 1 exp ( i ϕ 1 ) d 2 ,
c 3 = η 0 + η 1 2 ρ 2 exp [ i 2 ( ϕ 1 + Φ 2 ) ] d 2 ,
t = i τ 2 exp ( i Φ 2 ) c 2 ,
ϕ 0 = 0 ,
ϕ 1 = 1 / 2 arccos ( ( η 1 2 2 η 0 2 ) / 2 ρ 0 η 0 ) ,
ϕ 2 = arccos ( η 1 2 / ( 2 η 2 η 0 ) ) .
c 1 PR = [ ρ 1 c 1 exp ( i 2 Φ 1 ) ] d 1 ,
c 2 PR = i τ 1 exp [ i ( Φ 1 + Φ 2 ) ] c 2 d 1 ,
c 3 PR = i τ 1 exp ( i Φ 1 ) c 3 d 1 ,
t PR = τ 1 τ 2 exp [ i ( Φ 1 + Φ 2 ) ] c 2 d 1 ,
0 g g g m 1
g g = 1 L 2 R c , g = 1 and g m = 1 L 2 R c , m ,
w 0 2 = L 2 λ π g m 1 g m .
w out = cos ( θ out ) cos ( θ in ) w in .
R c , y = L 1 + π 2 w 0 , y 4 λ 2 L 1 ,
R c , x = L 1 + π 2 w 0 , x 4 λ 2 L 1 = L 1 + π 2 w 0 , y 4 λ 2 L 1 ( cos θ in ) 4 .
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