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Optimal design of a microring cavity optical modulator for efficient RF-to-optical conversion

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Abstract

The efficiency of optical sideband generation with a microring resonator modulator as a function of modulator parameters is studied taking into account the photon dynamics inside the resonator. The best achievable modulation efficiency is determined for any choice of the resonator intrinsic quality factor, and analytic solutions for the optimum modulator parameters, namely the coupling coefficient and the detuning between the frequencies of the input laser light and the microring resonance, are provided. This analysis is carried out both for a narrowband RF signal, in which case the modulator is optimized for the center frequency of this signal, and for wideband signals, when high conversion efficiency over a wide range of RF frequencies is desired. The obtained results are expected to be useful coherent optical links, direct detection RF receivers, and optical wavelength converters

© 2018 Optical Society of America under the terms of the OSA Open Access Publishing Agreement

1. Introduction

An electrooptic modulator is a key component of RF photonic links, where it is used to transfer an input RF signal into the optical domain for further processing using photonic means [1]. Integrated technology is attractive for implementing RF photonic circuits because of scalability to large circuit complexity, reduced packaging costs, improved reliability, reduced size and weight, and potentially higher energy efficiency and performance [2]. A proven solution for RF photonic links is to use Mach-Zehnder modulators, which have wide electrical and optical bandwidth and are relatively simple to control. A possible alternative to Mach-Zehnder modulators are microring resonator modulators [3, 4], which are significantly smaller in size and can provide higher modulation efficiency. The higher efficiency is achieved because light traveling around the resonator experiences the phase shift induced by the applied RF signal not once, but multiple times, in proportion to the photon lifetime in the resonator relative to the round trip travel time, where a long photon lifetime corresponds to high quality factor Q. However, the photon lifetime limits the speed with which the resonator responds to the applied RF field, with shorter lifetimes required for higher RF frequencies. However, shorter lifetimes brings the modulation efficiency down, so that there is a trade-off between the modulator bandwidth and efficiency. This work examines the maximum efficiency which can be achieved in a single-ring modulator with a given intrinsic quality factor as a function of RF frequency, and the modulator parameters need to be selected to achieve this maximum efficiency.

The RF response of a microring modulator considering the photon dynamics inside the resonator has been studied in multiple publications [5–12]. Analytic formulas for the frequency response has been derived in small-signal approximation [7–10, 12], and optimum conditions for the laser detuning from the microring resonance [7–9, 12] and the resonator coupling coefficient [8] have been obtained.

Similar to previous publications [7–10, 12], this work studies the small-signal modulator response considering the photon dynamics inside the resonator. However, this work optimizes the modulator for different applications, and the definition of modulation efficiency adopted in this work is different as well. Prior publications examined the modulation of the optical intensity at the output of the modulator, which is determined by the beating between the optical carrier and the sidebands produced by the modulator. On the other hand, this work considers the modulator as an RF mixer which upconverts the RF signal into one of the optical sidebands, and seeks to maximize the optical sideband amplitude independently from the carrier. Such a regime is of interest in coherent detection schemes, where the carrier is supplied by the local oscillator, as well as in RF receivers where the optical sidebands are detected without the carrier [13–15]. More details can be found in Sec. 2.1.

The expressions for efficiency of conversion into the optical sideband are derived in small-signal approximation and their physical significance is analyzed in Section 2. Optimization of modulator parameters – the detuning between the laser and the microring resonance frequency and the ring-to-bus coupling coefficient – is performed in Section 3 for narrowband, and in Section 4 for wideband RF signals. In both cases, analytic solutions for the optimum parameters and the obtained efficiency are given and analyzed.

2. Calculation of conversion efficiency

2.1. Problem Formulation

The single-ring resonant modulator studied in this work is illustrated in Fig. 1(a). The input laser light at frequency ωl passes through a waveguide with a microring resonator modulator coupled to it. The resonant frequency of the resonator in absence of applied RF signal is ωo. The transmission of the modulator depends on how close the laser frequency ωl is to the resonance frequency ωo, with the transmission minimum at ωl = ωo. The RF signal applied to the modulator changes the resonant frequency, modulating the transmission of laser light.

 figure: Fig. 1

Fig. 1 (a) The microring resonator modulator studied in this work. (b) The spectra of the optical input sin, applied RF signal vRF, and the output optical signal sout with multiple sidebands generated by the modulator. The modulator is considered as a mixer which upconverts the input RF signal at frequency Ω into the optical signal ωl + Ω, which is the first sideband of the output signal sout.

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In this work, the modulator is considered as a mixer which upconverts the RF signal at frequency Ω to an optical signal at frequency ωl + Ω. In general, when the modulator is driven by the RF frequency Ω, the output light has frequency components ωl ± nΩ, where n = 0 corresponds to the optical carrier and n = ±1, ±2, … to the sideband frequencies, see Fig. 1(b). Usually, the two sidebands with n = ±1 have much larger magnitudes than the ones with |n| > 1. Out of these two sidebands, we pick the one with n = +1, and study conversion from RF frequency Ω to optical frequency ωl + Ω, with a specific interest to maximize the efficiency of that single sideband’s generation. The conversion efficiency G is defined here as the fraction of the input optical power which is converted into that of the sideband at ωl + Ω,

G=|Sout(ωl+Ω)|2|Sin(ωl)|2,
where Sin(ω) and Sout(ω) are the amplitudes of the input and output optical waves at frequency ω.

As mentioned in the introduction, this work analyzes the modulator operation in the regime which is different from the regime used in for regular data interconnects and conventional RF photonic links [5–12]. In particular, in RF photonics, the links are analyzed in terms of link gain which is defined as the RF power at frequency Ω at the output of the link relative to input RF power at the same frequency. The output RF signal at Ω is created at the photodetector due to the beating between the optical carrier at ωl and the sidebands at ωl ± Ω (the term Sout(Ω)Sout(ωl + Ω)), so that the link gain depends not only on the magnitude of the sideband but also on the magnitude of the carrier. This means that maximizing magnitude of the sidebands alone, as it is done in this work, does not necessarily lead to the maximum gain in a conventional RF link. However, maximizing the sidebands is what needs to be done for example, for coherent detection, when the optical carrier is supplied by the local oscillator at the receiver so that the resulting RF power is maximized when the optical sidebands are maximized. The sideband needs to be maximized independently from the carrier also in the direct detection RF receivers [13–15]. Alternatively, one can envisage an integrated circuit where the optical carrier is controlled independently from the sidebands by analogy with the techniques used for conventional RF photonic links to improve the link noise performance and avoid photodetector saturation, such as low biasing of Mach-Zehnder modulators [16, 17] and carrier filtering [18, 19]. The carrier filtering technique in particular is well suited for implementation using integrated optics technology. The regime of operation studied in this work is also relevant for wavelength converters [20].

2.2. Small signal analysis

The optical sideband conversion efficiency G can be found analytically in small-signal approximation using the coupled mode theory in time (CMT) [21, 22]. According to CMT, the energy amplitude inside the ring resonator a evolves in time according to

dadt=(jωo+jδωm2cos(Ωt)rore)aj2resin,
where ωo is the nominal (unmodulated) resonant frequency of the microring, δωm cos (Ωt)/2 is the resonance frequency shift due to modulation by RF voltage v(t) = vRF cos(Ωt)/2 applied to the microring, δωm is the peak-to-peak amplitude of the resonant frequency shift related to the peak-to-peak RF voltage amplitude vRF through δωm=ωovRFvRF, with ωovRF being the optical resonant frequency shift (rad/s) per volt of applied voltage, and sin being the incident wave amplitude.

The coefficients ro and re are the decay rates of the energy amplitude a due to the optical losses inside the ring and the ring-to-waveguide external coupling, respectively. These decay rates are related to the loss-limited photon lifetime τp (or associated field decay time τo and the ring-to-waveguide power coupling coefficient κ2 as [22] ro = 1/τo = 1/2τp and re=κ22(2πRvg)1 where R is the microring radius, and vg is the group velocity. The loss quality factor is Qo=ωo/2ro=ωo/Δω3dB(o), the external quality factor is Qe = ωo/2re, and the total quality factor Qtotal = ωo/[2(re +ro)] = ωoω3dB, where Δω3dB(o) is the intrinsic linewidth and Δω3dB is the full linewidth of the resonance.

The wave amplitude at the output of the modulator is

sout=sinj2rea.
For steady-state input sin=Aejωlt, the solution of the first-order differential equation system (2), (3) is
soutsin=12rem=Jm(δωm2Ω)ejmΩt×n=(1)nJn(δωm2Ω)ejnΩtjδω+re+ro+jnΩ,
in agreement with [8]. In this equation,
δω=ωlωo
is the optical frequency detuning of the laser from the microring resonance and Jn(z) is the n-th-order Bessel function of the first kind. Bessel functions can be approximated by J0(z) ≃ 1, J1(z) ≃ z/2, and Jn(z)1n!(z2)n for n ⩾ 2, if the argument z is small, i.e. δωm ⩽ 2Ω. Selecting the terms of Eq. (4) that oscillate at Ω and neglecting the terms of the second and higher orders in δωm/2Ω, we obtain
Sout(ωl+Ω)sin(ωl)=2reJ0(δωm2Ω)J1(δωm2Ω)ejΩt(1jδω+re+ro+jΩ1jδω+re+ro)δωmre2ΩejΩt(1jδω+re+ro+jΩ1jδω+re+ro),
where the Bessel functions above have been replaced with their approximate values, J0(δωm2Ω)J1(δωm2Ω)δωm4Ω. The expression for the optical sideband amplitude (5) is consistent with the derivations in [7–9]. The small z requirement suggests that this expression is only valid when the RF carrier frequency is much larger than the driven resonance swing, δωm ⩽ 2Ω. However, it can be shown that the obtained formula for the conversion efficiency is in fact valid in the small-signal regime for any Ω, when the created sidebands are small relative to the optical carrier, so that carrier depletion due to modulation can be neglected. The conversion efficiency G is then found as the magnitude squared of Eq. (5),
G=(δωmre/2)2[δω2+(re+ro)2][(δω+Ω)2+(re+ro)2].
It can also be expressed in normalized form using parameters normalized by loss rate ro,
G=(δωmre/2)2[δω2+(re+1)2][(δω+Ω)2+(re+1)2],
where the normalized parameters are δωm=δωm/ro, re=re/ro, δω′ = δω/ro, and Ω′ = Ω/ro.

2.3. Analysis of the expression for conversion efficiency

The conversion efficiency G given by Eq. (6) can be expressed as

G=[δωmre/2(re+ro)2]2Λ(δω)Λ(δω+Ω),
where
Λ(δω)(re+ro)2δω2+(re+ro)2
is the Lorentzian function describing the resonant lineshape that promotes efficient conversion on resonance (here the frequency is detuned by δω from the the resonance). The important conclusion from Eq. (8) is that the conversion efficiency is proportional to the resonant enhancement of both the input carrier frequency via Λ(δω) and to that of the generated sideband frequency via Λ(δω + Ω). Efficient conversion occurs when both frequencies are resonant in the cavity. This is illustrated in Fig. 2(a), where the laser carrier frequency ωl and the sideband frequency ωs are indicated by the two arrows; the conversion efficiency is proportional to the product of the Lorentzian function values at these two frequencies. Figure 2(b) plots an example of the dependence of the conversion efficiency on RF frequency Ω for a negative detuning δω = ωlωo. At zero Ω, the red arrow in Fig. 2(a) coincides with the blue one; as Ω increases, the red arrow shifts to the right, tracing the Lorentzian function. The efficiency increases until it reaches its peak at ωs = ωl + Ω = ωo (when the red arrow is at the center of the Lorentzian), and then goes down at higher frequencies Ω, which is consistent with the optical peaking phenomenon observed in [5–7, 9, 12]. The resulting G(Ω) is plotted in Fig. 2(b).

 figure: Fig. 2

Fig. 2 (a) The Lorentzian profile Λ(ω) as defined by Eq. (9), describing resonant enhancement in the microring resonator; the red and the blue arrows indicate the input laser carrier at frequency ωl and the generated sideband at frequency ωl + Ω, respectively. In this example, laser detuning δω = ωlωo is assumed to be negative. (b) The conversion efficiency G as a function of applied RF frequency Ω.

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The following sections study optimization of the modulator design for maximum conversion efficiency. According to Eq. (6), the conversion efficiency G depends on the coupling rate re, intrinsic loss ro, laser detuning δω, resonant frequency swing under drive δωm, and the RF frequency Ω. The dependence on δωm and ro is simple: δωm should be increased and ro decreased for maximum conversion efficiency. Optimization with respect to the detuning δω and the coupling rate re is less straightforward and is carried out in the following sections.

3. Optimum design for a given RF driving frequency

Equation (6) can now be used to study how the modulator parameters and frequency detuning δω can be selected to maximize the efficiency. This section finds the parameters which maximize the conversion efficiency at a given RF frequency Ωo, which is of interest for narrowband RF signals centered around Ωo. The next section (Sec. 4) deals with wideband RF signals.

3.1. Optimum detuning δω for a given modulator design

First, we consider a modulator with a fixed design (i.e. fixed ring-to-bus coupling rate, re), and find which frequency detuning δω = ωlωo maximizes the conversion efficiency at a given RF frequency Ωo. The frequency detuning can be controlled by adjusting the laser frequency ωl or tuning the resonant frequency of the modulator ωo.

The optimum δω can be found by equating the first derivative of the conversion efficiency given by Eq. (6) to zero while making sure the second derivative is negative. This leads to the following solutions:

δω=Ωo2,G=(δωmre/2)2[(re+ro)2+(Ωo2)2]2ifΩoΔω3dB,
δω1,2=Ωo2±(Ωo2)2(re+ro)2,G=(δωmre/2)2(re+ro)2Ωo2ifΩo>Δω3dB,
where Δω3dB is defined to be the 3dB bandwidth of the microring resonance (in rad/s) [see also Q definitions in Sec. (2.2)],
Δω3dB2(re+ro).

The optimum detuning δω is plotted in Fig. 3(a) as a function of RF frequency Ωo, with the resulting frequency configurations illustrated in Fig. 3(b) at several representative points of this plot. If the RF frequency Ωo is smaller than the 3dB linewidth of the resonance, Δω3dB, the optimum solution is to set the laser at δω = −Ωo/2. In this case the sideband is generated symmetrically at the opposite side of the resonance peak, at δωs = +Ωo/2, see point A in Fig. 3(b). If Ωo exceeds the linewidth Δω3dB, there are two optimum solutions for δω, see points B and C in Fig. 3(a). These two solutions are symmetric with respect to the resonance frequency in the sense that δω1 = −δωs2 and δω2 = −δωs1, where δωs1 = δω1 + Ωo and δωs2 = δω2 + Ωo are the sideband frequencies corresponding to the two values of the laser detuning, see Fig. 3(b). In the limiting case when Ωo ≫ Δω3dB, the first of these solutions corresponds to the laser being at the resonance frequency ωo, see point D in Fig. 3, and the second solution corresponds to the sideband generated at the resonance frequency ωo, see point E in Fig. 3.

 figure: Fig. 3

Fig. 3 (a) The optimum frequency detuning δω as given by Eqs. (10), (11) which maximizes the conversion efficiency at frequency Ωo shown along the x-axis. (b) Location of the laser frequency ωl and the sideband frequency ωl + Ωo relative to the Lorentzian resonance of the microring centered at ωo for several representative points from plot (a).

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3.2. Optimization of modulator design

The previous section determined the frequency detuning values which maximize the conversion efficiency for a modulator with fixed coupling coefficient re. This section goes a step further and finds the ring-to-bus coupling re which allows one to achieve the highest conversion efficiency, Gmax, possible at RF frequency Ωo, for given loss rate ro (i.e. intrinsic quality factor Qo) and modulation amplitude δωm (i.e. the drive signal voltage and the electrooptic resonant frequency shift per volt).

The conversion efficiency G from Eq. (6) is plotted in Fig. 4 as a function of frequency detuning δω and coupling coefficient re. Figure 4(a) corresponds to the case when ΩoΔω3dB(o), where

Δω3dB(o)2ro
is the intrinsic linewidth of the resonator (in rad/s), i.e. the 3dB linewidth in absence of coupling to the bus waveguide. In this case Ωo < Δω3dB = 2(re + ro) for any re, and the optimum detuning is always −Ωo/2 as given by Eq. (10). Gmax can be found by maximizing G from Eq. (10) with respect to re.

 figure: Fig. 4

Fig. 4 The conversion efficiency G as a function of coupling rate re (normalized by loss rate ro) and frequency detuning δω (normalized by RF frequency Ωo) as given by Eq. (6). Plot (a) represents the case when ΩoΔω3dB(o) (with this particular plot created for Ωo=Δω3dB(o)/2), and (b) represents the case when Ωo>Δω3dB(o) (with this particular plot created for Ωo=2Δω3dB(o)). Without loss of generality, δωm/Δω3dB(o)=1 is assumed.

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Figure 4(b) corresponds to Ωo>Δω3dB(o). In this case, Ωo > Δω3dB for small values of re, and there are two optimum detuning values as given by Eq. (11). In this region the conversion efficiency plot of Fig. 4(b) has two ridges. As the coupling coefficient re increases, the linewidth Δω3dB increases as well and at some point becomes larger than Ωo. In this case, the optimum detuning is −Ωo/2 as given by Eq. (10), and the conversion efficiency plot has only one ridge. Note that this agrees with Fig. 3(a), where there are two δω curves for frequencies above the linewidth Δω3dB, and one δω curve for frequencies below the linewidth. The single-ridge region of Fig. 4(b) rises above the double-ridge region, which means that the maximum efficiency Gmax is achieved for re high enough to fit Ωo within the linewidth, i.e. Ωo < Δω3dB.

According to the analysis above, for both cases shown in Fig. 4 the maximum conversion efficiency is achieved when Ωo < Δω3dB. The optimum ring-to-bus coupling reopt can be found rigorously by setting the derivative of G from Eq. (10) over re to zero. This leads to the solution

reopt=ro2+(Ωo/2)2,δω=Ωo/2.

Equation (13) suggests that as the frequency Ωo increases, the coupling coefficient re needs to be increased as well to make sure the modulator is capable of operating at higher speeds. Another interpretation is that at slow RF frequencies, Ωoro, re = ro to be sure to get the sideband out of the cavity before it is lost due to ro. For high Ωoro, re ≈ Ωo/2 to ensure the resonance is wide enough to span both the laser and the sideband. The corresponding maximum conversion efficiency Gmax is found by substituting reopt into Eq. (10),

Gmax=[δωmreopt/2(reopt+ro)2+(Ωo/2)2]2=[δωmreopt/2(Δω3dB/2)2+(Ωo/2)2]2.

The maximum efficiency Gmax is plotted in Fig. 5(a) as a function of the RF frequency normalized by the intrinsic linewidth Δω3dB(o) [solid red curve]. At each point of this plot, the modulator design is optimized as described above. Without loss of generality, the modulation amplitude is chosen to be such that δωm/Δω3dB(o)=1. The efficiencies for other values of δωm can be found by multiplying the values shown in Fig. 5(a) by (δωm/Δω3dB(o))2 [as follows from Eq. (6)].

 figure: Fig. 5

Fig. 5 (a) Solid red curve: the maximum conversion efficiency Gmaxo) achievable in the modulator optimized for frequency Ωo, with Ωo/Δω3dB(o) plotted along the x-axis. Dashed curves: conversion efficiency profiles G(Ω) for modulators optimized for 3 different frequencies Ωo, with the respective values of Ωo indicated by circles and Ω/Δω3dB(o) plotted along the x-axis. The resonant frequency swing δωm equal to the intrinsic linewidth Δω3dB(o) is assumed. (b) The maximum conversion efficiency Gmax vs. non-normalized frequency Ωo for 4 values of Δω3dB(o), with modulation frequency swing δωm/2π = 1 GHz.

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Once the modulator parameters needed for maximum efficiency at the RF frequency Ω = Ωo are determined from Eq. (13), the efficiency at all other frequencies Ω can be found from Eq. (6) or (7). The G(Ω) plots for several values of Ωo are shown in Fig. 5(a) [dashed curves]. It is interesting to note that the response G(Ω) of a modulator optimized at frequency Ωo peaks at Ω = Ωo/2, rather than Ωo which is the solid circle that lies on the negative slope of G(Ω). For example, for the modulator optimized for Ωo/Δω3dB(o)=4, the Ω/Δω3dB(o)=4 point is on the negative slope of its response curve [the green dashed curve in Fig. 5(a)]. The modulator whose response peaks at Ω/Δω3dB(o)=4 is the modulator optimized at Ωo/Δω3dB(o)=8 [the orange dashed curve]. However, the peak of the orange curve is below the Ω/Δω3dB(o)=4 point of the green curve, justifying our optimum solution.

While Fig. 5(a) plots the efficiency versus frequency normalized by intrinsic linewidth Δω3dB(o), Fig. 5(b) plots the maximum efficiency Gmax as a function of absolute frequency Ωo for several values of Δω3dB(o), for modulation frequency swing δωm/2π = 1 GHz. At high RF frequencies ΩoΔω3dB(o), the maximum efficiency becomes independent of Δω3dB(o),

Gmax(Ωo)=(δωm2Ωo)2.

At low frequencies ΩoΔω3dB(o), the maximum efficiency is determined by the frequency shift δωm relative to loss ro (and intrinsic linewidth Δω3dB(o)=2ro),

Gmax(Ωo0)=116(δωmΔω3dB(o))2.

3.3. Obtained RF bandwidth

The modulator design optimization so far has been performed for best performance at a single RF frequency Ωo. This section examines how well a modulator optimized at Ωo performs if the RF signal has non-zero spectral bandwidth around Ωo. Figure 6(a) illustrates the frequency response G(Ω) of the modulator optimized for frequency Ωo. The efficiency goes up below Ωo and goes down above Ωo; from Eq. (6), the frequency at which the response drops by 3dB relative to Go) is

Ω3dB=δω+2δω2+(re+ro)2.

 figure: Fig. 6

Fig. 6 (a) An example of frequency response G(Ω) of the modulator optimized for maximum efficiency at Ωo. 3dB bandwidth BW is defined as the bandwidth around Ωo within which the response goes down by no more than 3dB with respect to the response at the center frequency Go). (b) The bandwidth BW normalized by center frequency Ωo in the modulator optimized for Ωo as a function of Ωo, as given by Eq. (15).

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From Eq. (13), δω = −Ωo/2 and Ω3dB becomes

Ω3dB=Ωo2+Ωo2+2(re+ro)22.

Therefore, if the RF signal has bandwidth BW centered around Ωo, see Fig. 6(a),

BW=2(Ω3dBΩo)=2Ωo2+2(re+ro)22Ωo,
the conversion efficiency within the bandwidth of such a signal is guaranteed not to drop by more than 3dB relative to the efficiency at the center frequency Ωo.

The bandwidth BW normalized by Ωo is plotted in Fig. 6(b) as a function of Ωo/Δω3dB(o), with the modulator optimized at each point according to Eq. (13). The relative bandwidth decreases with Ωo and in the high frequency limit becomes

BW(Ωo)=(31)Ωo0.73Ωo.

This means that the optimization strategy presented in this section works well for band-limited RF signals with relatively high RF bandwidths relative to their RF center frequency. Modulator optimization for wideband RF signals with frequencies going down to DC is carried out in the following section.

4. Optimization for a wideband RF signal

The results of the previous sections can conveniently be used for signals with bandlimited spectra centered around some center frequency. However, many applications require even baseband operation of the modulator, when the RF spectrum has components that can go down to zero frequency. This section optimizes the modulator design for performance with such RF signals. Similar to the analysis above, the optimization is performed in two steps: optimization of frequency detuning δω for fixed modulator design (i.e. fixed re), and optimization of both δω and re.

4.1. Formulation of the optimization problem

A representative profile of the conversion efficiency G(Ω) given by Eq. (6) is shown in Fig. 7 with logarithmic scale used for the x-axis. The response profile can be described by the following parameters:

  • GDC, the conversion efficiency at low RF frequencies, which can be found from Eq. (6):
    GDC=(δωmre/2)2[δω2+(re+ro)2]2;
  • 3 dB bandwidth Ω3dB, the frequency at which the efficiency goes down by 3dB relative to GDC, which is given by Eq. (14);
  • ripple α, which indicates by how much the peak of the response Gmax is higher than the low-frequency response GDC,
    α=Gmax/GDC.

 figure: Fig. 7

Fig. 7 A representative frequency response G(Ω) of a resonant modulator, indicating the response metrics used in modulator design optimization for baseband RF signals. The x-axis is the frequency Ω in logarithmic scale. Plots of G(Ω) with x axis in linear scale can be found in Fig. 2(b) and Fig. 6(a).

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The ripple can be found from Eq. (6),

α=δω2+(re+ro)2(re+ro)2.

The modulator optimization problem in the broadband case can be formulated as follows: for given loss ro, find such values of frequency detuning δω and coupling rate re that

  1. the conversion efficiency GDC is as high as possible, while
  2. Ω3dBΩ3dBmin, i.e. the modulator has the 3dB bandwidth of at least the specified minimum bandwidth Ω3dBmin, and
  3. ααmax, i.e. the ripple does not exceed the specified maximum ripple αmax.

4.2. Optimum detuning δω for a given modulator design

First, the optimization is performed for a modulator with fixed coupling rate re. The optimization problem formulated above can be solved analytically using the conversion efficiency given by Eq. (6); the obtained solutions are given in the Appendix. The results are analyzed below.

Figure 8 plots the conversion efficiency GDC as a function of the normalized coupling rate re/ro and minimum bandwidth Ω3dBmin/Δω3dB(o) for δωm/Δω3dB(o)=1. At each point, the detuning δω is selected in such a way that the ripple α [which is directly related to δω through Eq. (17)] has the minimum possible value which ensures that Ω3dBΩ3dBmin; according to Eq. (16), such ripple also maximizes the efficiency GDC and therefore corresponds to the solution of the modulator optimization problem. The obtained ripple values are shown with the white contour lines in Fig. 8 for few values of the ripple. This plot can be used in the following way: if the required maximum ripple αmax for the modulator with given re and the required Ω3dBmin is higher than the ripple α shown in the plot, the value of α from the plot [and δω related to it through Eq. (17)] should be used for the modulator design. If the required αmax is lower than shown in the plot, such an optimization problem has no solutions.

 figure: Fig. 8

Fig. 8 Conversion efficiency GDC (in dB) as a function of the required minimum 3 dB bandwidth Ω3dBmin and coupling rate re normalized by loss rate ro. The white lines are the contour lines of the obtained ripple values for the obtained ripple value α = 0, 1, 3, and 6 dB. Red circles indicate the designs with the best efficiency for several fixed values of Ω3dBmin, assuming the ripple α is not constrained. The efficiencies are calculated for δωm/Δω3dB(o)=1. The formulas used to create this plot can be found in the Appendix.

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Note that the points below the 0 dB ripple line all have 0 dB ripple and correspond to δω = 0 with Ω3dB = re + ro = Δω3dB/2. When the required minimum bandwidth Ω3dBmin exceeds Δω3dB/2, the value of δω has to be decreased below 0 to increase Ω3dB, which leads to higher ripple α and lower efficiency GDC.

4.3. Optimization of modulator design

Figure 9 shows the conversion efficiency GDC for the case when the coupling rate re is optimized in addition to δω. This plot can be understood by going back to Fig. 8 which has re as its x-axis. Let’s assume first that there no restrictions on the ripple, so that the optimum value of re is the one which maximizes GDC for the required Ω3dBmin, regardless of the ripple. Such points for several values of Ω3dBmin are shown in Fig. 8 with red circles. Looking at the location of the red circles with respect to the ripple contour lines in Fig. 8, one can conclude that for each required bandwidth Ω3dBmin there exists an optimum ripple value, i.e. the ripple value which corresponds to the maximum GDC. These optimum ripple values are plotted in Fig. 9 as the “optimum ripple” line; note that the red points of Fig. 8 lie on this line. Now, let us consider the case when the maximum ripple αmax is constrained. If the required αmax value is above the optimum line, the optimum modulator design is the one with the optimum ripple; this is the reason why the efficiency contour lines in Fig. 9 are vertical above the optimum line. If the required ripple αmax is below the optimum line, one needs to go back to Fig. 8 and select a larger value of re which corresponds to this αmax; the design with such re will have smaller efficiency GDC.

 figure: Fig. 9

Fig. 9 The conversion efficiency GDC (in dB) for modulators optimized to have the 3 dB bandwidth of at least the Ω3dBmin value shown along the x axis, and the ripple of at most αmax shown along the y axis. Both detuning δω and coupling rate re are optimized at each point; the analytic solutions are given in the Appendix. The white line labeled the “optimum ripple” indicates the optimum ripple α which maximizes the efficiency for given Ω3dB/δω3dB(o). Without loss of generality δωm/δω3dB(o)=1 is assumed.

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The conversion efficiency of optimized modulators is shown in Fig. 10 in a different way. The efficiency is plotted versus the minimum required bandwidth Ω3dBmin which is not normalized by Δω3dB(o) for several values of the ripple αmax and the intrinsic linewidth Δω3dB(o), for modulation frequency swing δωm/2π = 1 GHz. One can see that for low bandwidths, the efficiency of the optimized modulator is limited mostly by the loss while for high bandwidths, the efficiency is almost independent of the loss, which is consistent with the behavior of the modulators optimized for narrowband operation (see Fig. 5). For high bandwidths, a modest efficiency improvement (up to about 3dB) can be achieved by allowing some ripple in the response.

 figure: Fig. 10

Fig. 10 The conversion efficiency GDC for modulators optimized for given minimum 3 dB bandwidth Ω3dBmin for several values of the required maximum ripple αmax. Three sets of curves are for different loss rates ro. Modulation frequency swing δωm/2π = 1 GHz.

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5. Summary and conclusions

This work solves the modulator design problem for a single-mode resonant modulator and provides analytic solutions for modulator parameters needed to maximize the conversion efficiency for narrowband and wideband RF signals driving a microring modulator as an RF mixer which upconverts the RF signal into the optical domain. It finds the maximum conversion efficiency possible using a single-ring modulator design, establishing a baseline that other, more complex modulator designs such as [15, 20, 23] can be benchmarked against.

As expected, there is a trade-off between the modulation speed and efficiency, with the efficiency going down at higher frequencies. The fact that the modulation efficiency goes down at higher frequencies shows the fundamental limitation of the selected modulator architecture, and suggests that different architectures might need to be considered when high efficiency at high frequencies is required. Note that the efficiency reduction happens even in the idealized case considered in this work when the modulation frequency swing δωm is not a function of frequency. In reality, δωm can go down with frequency as well because of the RC constant of the modulator, which further reduces the efficiency.

It should be noted that the results presented in this work are obtained in small-signal approximation, when the resonant frequency modulation δωm is small enough so that the conversion of optical power from the carrier to the sideband does not deplete the carrier. It remains to be studied how the presented results are to be adjusted when the small-signal approximation no longer applies.

While this work establishes the fundamental limits of modulation efficiency which are possible to achieve with a single-ring modulator, the performance in any real-life scenario will be affected by fabrication tolerances. For instance, the frequency detuning δω will be affected by temperature fluctuations on the chip, requiring utilization of resonant frequency stabilization techniques [24]. The coupling between the microring and the bus waveguide in a fabricated device will deviate from the design target provided in this work, which can be mitigated by using a tunable Mach-Zehnder interferometer-based couplers.

This work optimizes the modulator operation for applications in coherent optical links and direct detection RF receivers, and the conversion efficiency used in this work is defined as the fraction of input optical power which is converted into the optical sideband, see Eq. (1). As explained in Sec. 2.1, this definition is different from the link gain usually used to describe RF links, which differentiates this work from prior art [7–10, 12]. The efficiency definition used here is useful for RF links where the magnitude of the carrier is controlled independently from the sidebands, such as in coherent links where the carrier is supplied by the local oscillator, direct detection links [13–15], or optical wavelength converters [20].

Appendix

This appendix provides the analytic solution for modulator parameters optimized for wideband operation, solving the optimization problem formulated in Sec. 4. This is done first for the case when the detuning δω is optimized and re is fixed, and then for the case when both δω and re are optimized.

For convenience, the solutions below are formulated in terms of ripple α rather than detuning δω. The detuning δω can always be found from the ripple using Eq. (17)

δω=(re+ro)α1,
where the “−” sign for δω was selected because because the root of Eq. (17) with the negative sign always leads to a response with larger bandwidth (Eq. (14)) and the same GDC (Eq. (16)) as the root with the positive sign.

The formulas below also include the variable x defined as

xΩ3dBminΔω3dB/2=Ω3dBmin(re+ro)

Optimization of detuning δω for a given modulator design

The solution for the wideband modulator optimization problem for fixed re is the following.

If x ⩽ 1,

α=1,GDC=(δωmre/2)2(re+ro)4.

If 1<xαmax1+2αmax1,

α=3x22x2x21,GDC=(δωmre/2)2[α(re+ro)2]2.

If x>αmax1+2αmax1, the optimization problem has no solutions.

Optimization of modulator design

The solution for the wideband modulator optimization problem when both δω and re can be varied is the following.

If Ω3dBminΔω3dB(o)=2ro

α=1,re=ro,GDC=116(δωm2ro)2.

If Ω3dBmin>Δω3dB(o)=2ro, there are two potential solutions out of which the one with the larger re should be chosen. The first one is

re=6Ω3dBmin2(3ro24ro2+Ω3dBmin2)16roΩ3dBmin2+8ro38ro2+18Ω3dBmin2,

α=3x22x2x21, with x given by Eq. (18):

The second option is

re=Ω3dBminαmax1+2αmax1,α=αmax.

The option with larger re should be selected. The efficiency can be found from

GDC=(δωmre/2)2[α(re+ro)2]2.

Funding

This work was supported by Ball Aerospace and Technologies Corp. and by National Science Foundation grant 1701596. We thank Todd Pett, Michael D. Lieber, and Hayk Gevorgyan for their input and discussions.

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Figures (10)

Fig. 1
Fig. 1 (a) The microring resonator modulator studied in this work. (b) The spectra of the optical input sin, applied RF signal vRF, and the output optical signal sout with multiple sidebands generated by the modulator. The modulator is considered as a mixer which upconverts the input RF signal at frequency Ω into the optical signal ωl + Ω, which is the first sideband of the output signal sout.
Fig. 2
Fig. 2 (a) The Lorentzian profile Λ(ω) as defined by Eq. (9), describing resonant enhancement in the microring resonator; the red and the blue arrows indicate the input laser carrier at frequency ωl and the generated sideband at frequency ωl + Ω, respectively. In this example, laser detuning δω = ωlωo is assumed to be negative. (b) The conversion efficiency G as a function of applied RF frequency Ω.
Fig. 3
Fig. 3 (a) The optimum frequency detuning δω as given by Eqs. (10), (11) which maximizes the conversion efficiency at frequency Ωo shown along the x-axis. (b) Location of the laser frequency ωl and the sideband frequency ωl + Ωo relative to the Lorentzian resonance of the microring centered at ωo for several representative points from plot (a).
Fig. 4
Fig. 4 The conversion efficiency G as a function of coupling rate re (normalized by loss rate ro) and frequency detuning δω (normalized by RF frequency Ωo) as given by Eq. (6). Plot (a) represents the case when Ω o Δ ω 3 d B ( o ) (with this particular plot created for Ω o = Δ ω 3 d B ( o ) / 2 ), and (b) represents the case when Ω o > Δ ω 3 d B ( o ) (with this particular plot created for Ω o = 2 Δ ω 3 d B ( o ) ). Without loss of generality, δ ω m / Δ ω 3 d B ( o ) = 1 is assumed.
Fig. 5
Fig. 5 (a) Solid red curve: the maximum conversion efficiency Gmaxo) achievable in the modulator optimized for frequency Ωo, with Ω o / Δ ω 3 d B ( o ) plotted along the x-axis. Dashed curves: conversion efficiency profiles G(Ω) for modulators optimized for 3 different frequencies Ωo, with the respective values of Ωo indicated by circles and Ω / Δ ω 3 d B ( o ) plotted along the x-axis. The resonant frequency swing δωm equal to the intrinsic linewidth Δ ω 3 d B ( o ) is assumed. (b) The maximum conversion efficiency Gmax vs. non-normalized frequency Ωo for 4 values of Δ ω 3 d B ( o ), with modulation frequency swing δωm/2π = 1 GHz.
Fig. 6
Fig. 6 (a) An example of frequency response G(Ω) of the modulator optimized for maximum efficiency at Ωo. 3dB bandwidth BW is defined as the bandwidth around Ωo within which the response goes down by no more than 3dB with respect to the response at the center frequency Go). (b) The bandwidth BW normalized by center frequency Ωo in the modulator optimized for Ωo as a function of Ωo, as given by Eq. (15).
Fig. 7
Fig. 7 A representative frequency response G(Ω) of a resonant modulator, indicating the response metrics used in modulator design optimization for baseband RF signals. The x-axis is the frequency Ω in logarithmic scale. Plots of G(Ω) with x axis in linear scale can be found in Fig. 2(b) and Fig. 6(a).
Fig. 8
Fig. 8 Conversion efficiency GDC (in dB) as a function of the required minimum 3 dB bandwidth Ω 3 d B m i n and coupling rate re normalized by loss rate ro. The white lines are the contour lines of the obtained ripple values for the obtained ripple value α = 0, 1, 3, and 6 dB. Red circles indicate the designs with the best efficiency for several fixed values of Ω 3 d B m i n, assuming the ripple α is not constrained. The efficiencies are calculated for δ ω m / Δ ω 3 d B ( o ) = 1. The formulas used to create this plot can be found in the Appendix.
Fig. 9
Fig. 9 The conversion efficiency GDC (in dB) for modulators optimized to have the 3 dB bandwidth of at least the Ω 3 d B m i n value shown along the x axis, and the ripple of at most αmax shown along the y axis. Both detuning δω and coupling rate re are optimized at each point; the analytic solutions are given in the Appendix. The white line labeled the “optimum ripple” indicates the optimum ripple α which maximizes the efficiency for given Ω 3 d B / δ ω 3 d B ( o ). Without loss of generality δ ω m / δ ω 3 d B ( o ) = 1 is assumed.
Fig. 10
Fig. 10 The conversion efficiency GDC for modulators optimized for given minimum 3 dB bandwidth Ω 3 d B m i n for several values of the required maximum ripple αmax. Three sets of curves are for different loss rates ro. Modulation frequency swing δωm/2π = 1 GHz.

Equations (33)

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G = | S o u t ( ω l + Ω ) | 2 | S i n ( ω l ) | 2 ,
d a d t = ( j ω o + j δ ω m 2 cos ( Ω t ) r o r e ) a j 2 r e s i n ,
s o u t = s i n j 2 r e a .
s o u t s i n = 1 2 r e m = J m ( δ ω m 2 Ω ) e j m Ω t × n = ( 1 ) n J n ( δ ω m 2 Ω ) e j n Ω t j δ ω + r e + r o + j n Ω ,
δ ω = ω l ω o
S o u t ( ω l + Ω ) s i n ( ω l ) = 2 r e J 0 ( δ ω m 2 Ω ) J 1 ( δ ω m 2 Ω ) e j Ω t ( 1 j δ ω + r e + r o + j Ω 1 j δ ω + r e + r o ) δ ω m r e 2 Ω e j Ω t ( 1 j δ ω + r e + r o + j Ω 1 j δ ω + r e + r o ) ,
G = ( δ ω m r e / 2 ) 2 [ δ ω 2 + ( r e + r o ) 2 ] [ ( δ ω + Ω ) 2 + ( r e + r o ) 2 ] .
G = ( δ ω m r e / 2 ) 2 [ δ ω 2 + ( r e + 1 ) 2 ] [ ( δ ω + Ω ) 2 + ( r e + 1 ) 2 ] ,
G = [ δ ω m r e / 2 ( r e + r o ) 2 ] 2 Λ ( δ ω ) Λ ( δ ω + Ω ) ,
Λ ( δ ω ) ( r e + r o ) 2 δ ω 2 + ( r e + r o ) 2
δ ω = Ω o 2 , G = ( δ ω m r e / 2 ) 2 [ ( r e + r o ) 2 + ( Ω o 2 ) 2 ] 2 if Ω o Δ ω 3 d B ,
δ ω 1 , 2 = Ω o 2 ± ( Ω o 2 ) 2 ( r e + r o ) 2 , G = ( δ ω m r e / 2 ) 2 ( r e + r o ) 2 Ω o 2 if Ω o > Δ ω 3 d B ,
Δ ω 3 d B 2 ( r e + r o ) .
Δ ω 3 d B ( o ) 2 r o
r e o p t = r o 2 + ( Ω o / 2 ) 2 , δ ω = Ω o / 2 .
G m a x = [ δ ω m r e o p t / 2 ( r e o p t + r o ) 2 + ( Ω o / 2 ) 2 ] 2 = [ δ ω m r e o p t / 2 ( Δ ω 3 d B / 2 ) 2 + ( Ω o / 2 ) 2 ] 2 .
G m a x ( Ω o ) = ( δ ω m 2 Ω o ) 2 .
G m a x ( Ω o 0 ) = 1 16 ( δ ω m Δ ω 3 d B ( o ) ) 2 .
Ω 3 d B = δ ω + 2 δ ω 2 + ( r e + r o ) 2 .
Ω 3 d B = Ω o 2 + Ω o 2 + 2 ( r e + r o ) 2 2 .
B W = 2 ( Ω 3 d B Ω o ) = 2 Ω o 2 + 2 ( r e + r o ) 2 2 Ω o ,
B W ( Ω o ) = ( 3 1 ) Ω o 0.73 Ω o .
G D C = ( δ ω m r e / 2 ) 2 [ δ ω 2 + ( r e + r o ) 2 ] 2 ;
α = G m a x / G D C .
α = δ ω 2 + ( r e + r o ) 2 ( r e + r o ) 2 .
δ ω = ( r e + r o ) α 1 ,
x Ω 3 d B m i n Δ ω 3 d B / 2 = Ω 3 d B m i n ( r e + r o )
α = 1 , G D C = ( δ ω m r e / 2 ) 2 ( r e + r o ) 4 .
α = 3 x 2 2 x 2 x 2 1 , G D C = ( δ ω m r e / 2 ) 2 [ α ( r e + r o ) 2 ] 2 .
α = 1 , r e = r o , G D C = 1 16 ( δ ω m 2 r o ) 2 .
r e = 6 Ω 3 d B m i n 2 ( 3 r o 2 4 r o 2 + Ω 3 d B m i n 2 ) 16 r o Ω 3 d B m i n 2 + 8 r o 3 8 r o 2 + 18 Ω 3 d B m i n 2 ,
r e = Ω 3 d B m i n α m a x 1 + 2 α m a x 1 , α = α m a x .
G D C = ( δ ω m r e / 2 ) 2 [ α ( r e + r o ) 2 ] 2 .
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