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Dynamic range enhancement of a novel phase-locked coherent optical phase demodulator

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Abstract

We report on a novel cancellation technique, for reducing the nonlinearity associated with the tracking phase-modulator in recently proposed phase-locked coherent demodulator for phase modulated analog optical links. The proposed cancellation technique is input RF signal power and frequency independent leading to a significant increase in dynamic range of the coherent demodulator. Furthermore, this technique demonstrates that large values of the signal-to-intermodulation ratio of the demodulated signal can be obtained even though the tracking phase modulator is fairly nonlinear, and thereby relaxing the linearity requirements for the tracking phase modulator. A new model is developed and the calculated results are in good agreement with measurements.

©2007 Optical Society of America

1. Introduction

The use of optical links for the transmission of RF signals is a subject of considerable interest for future commercial and military systems [1, 2]. Intensity modulated analog optical links have been limited in performance by the nonlinear response of optical modulators [1]. The underlying reason for this is that the response of optical intensity modulators is ‘hard-limited’ by zero and full transmission. In contrast, optical phase modulation has no fundamental limit to modulation depth besides that given by the available modulation range in optical phase modulators. The challenge to implement a linear phase-modulated optical link lies in the receiver structure. A traditional coherent receiver has a sinusoidal response limiting the overall dynamic range of the optical link [3]. We have recently proposed, theoretically investigated and experimentally demonstrated a novel coherent optical phase-locked demodulator with feedback [4, 5, 6, 7] resulting in 15 dB of SFDR improvement compared to the traditional approach. The concept of this novel receiver is illustrated in Fig. 1. The output from the phase demodulator (a balanced optical mixer) is amplified and filtered by electronics, and then feed back to a local tracking phase modulator. Within the loop bandwidth, the effect of the feedback is to reduce the difference in phase between the local optical wave and the incoming wave. Therefore, the effective swing across the phase demodulator is reduced, resulting in an improved SFDR. This reduction could also be obtained by reducing the modulation depth at the transmitter but the signal-to-noise ratio (SNR) is reduced as a consequence. In contrast, in the proposed receiver, both the signal and the noise swings are reduced by the same factor (loop gain), retaining the SNR while improving the SFDR as shown in [4, 6]. However, to achieve a high bandwidth phase-locked receiver, compact semiconductor phase modulators have to be used to keep loop delay sufficiently low. These modulators can have fairly nonlinear response significantly limiting the dynamic range of the receiver [9]. Furthermore, the modulator distortion usually dominates over photodiode distortion and compensating for the modulators nonlinearities is therefore of significant importance [1]. In this paper, the impact of system nonlinearity, associated with tracking phase modulator, on the demodulated signal are determined in terms of the signal-to-intermodulation ratio. Furthermore, we propose a method to cancel out nonlinearities associated with the tracking phase modulator and inherently nonlinear response of the balanced detector.

2. Novelty of the work

A review of different linearization (cancellation) techniques can be found in reference [8]. So far, linearization techniques have been applied to intensity modulated analog optical links and mostly concentrated on the transmitter side. In many cases, the linearizer circuit was design to cancel either quadratic or cubic nonlinearity and cancellation of nonlinearities occurred in relatively narrow band (input RF signal power and frequency) [8]. We show that we can simultaneously cancel nonlinearities associated with the balanced receiver and tracking LO phase modulator by purely adjusting the loop gain and tailoring the nonlinearities of the tracking LO phase modulator. No extra circuitry is needed in order to obtain the cancellation. The proposed cancellation technique in this paper is frequency and power independent and has not been reported previously. Furthermore, the overall receiver concept is novel for linear optical phase demodulation, and as such, the first paper providing detailed analysis and deeper understanding of the receiver must therefore be not only novel but also very useful.

3. Model set-up

The set-up of the phase-locked optical demodulator, on which we base our model, is shown in Fig. 1.

 figure: Fig. 1.

Fig. 1. General outline of phase-modulated optical link and phase-locked optical demodulator at the receiver unit.

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The received RF signal, Vin(t) is used to directly modulate an optical phase modulator at the remote antenna unit. The corresponding optical signal Ein(t), see Fig. 1, is then written in complex notation as 1:

Ein(t)=Pinej(ω0t+ϕin(t))

where ω 0 is the optical frequency and Pin is the power of the optical field. Taking into consideration the nonlinearities associated with the (input) phase-modulator located at the remote antenna unit the phase of the optical signal, φin(t), is expressed as:

ϕin(t)=πVin(t)Vπ,in(1+a2a1Vπ,inVin(t)+a3a1Vπ,in2Vin2(t))

where V π,in is the voltage of the input phase-modulator, in order to obtain π phase shift and a 1,a 2 and a 3 represent the terms of the polynomial expansion of the input modulator nonlinear phase response. In order to characterize dynamic range of the demodulator, the input RF signal Vin(t) is assumed to consist of relatively closely spaced tones [10]:

Vin(t)=V1sin[ω1t]+V2sin[ω2t]

where V 1 and V 2 are the amplitudes of the input RF signals and ω 1 and ω 2 are the input RF signal frequencies. The optical signal Ein(t) is then transported to the receiver unit where its phase, is compared to the phase of the local optical signal ELO(t), using the balanced detector pair with load resistance RL. A single optical source is used for both the remote antenna and the receiver unit. The optical LO signal, ELO(t), is thereby expressed as:

ELO(t)=PLO(t)ej(ω0t+ϕLO(t))

where ϕLO(t) is reference phase (signal) and is function of the feedback loop parameters, see Fig. 1 and PLO is the power of the optical field2. Following Fig. 1 after the 3-dB coupler, we have in one arm:

E1(t)=12Pinej(ω0t+ϕin(t)π2)+12PLO(t)ej(ω0t+ϕLO(t)π)

The output of the second arm is:

E2(t)=12Pinej(ω0t+ϕin(t)π)+12PLO(t)ej(ω0t+ϕLO(t)π2)

where in equations (5) and (6) an ideal coupler has been assumed, i.e. equal splitting ratios. Taking into account the non-linearities associated with the photodetectors, the photocurrents generated in each branch of the balanced receiver, I 1(t) and I 2(t), containing the phase difference between ϕin(t) and ϕLO(t) are then expressed as:

I1(t)=RpdE1(t)2(1+b2E1(t)2b1+b3E1(t)3b1)
=Rpdn=13bnb1(12Pin+12PLO(t)PinPLO(t)sin[ϕin(t)ϕLO(t)])n
I2(t)=RpdE2(t)2(1+b2E2(t)2b1+b3E2(t)3b1)
=Rpdn=13bnb1(12Pin+12PLO(t)+PinPLO(t)sin[ϕin(t)ϕLO(t)])n

where Rpd is the responsivity of the photodetectors and is assumed equal for both photodetectors. bn represent the terms of polynomial expansion of the non-linear response of the photodiodes and n is an integer. In practise, it is only necessary to consider n=1..3. The output signal from the balanced photodetector pair with load resistance RL contains the phase difference between ϕin(t) and ϕLO(t) is expressed as:

Vpd(t)=RL(I2(t)I1(t))

The signal Vpd(t) is then used to control the feedback loop. (After the loop has acquired lock, the phase difference ϕin(t)-ϕLO(t) will approach zero.) The signal Vpd(t) is then passed through the loop filter (low pass) and amplified:

dVoutdt=A[Vpd(t)Vout(t)τLF]

where τLF=1/2πfLF is inversely proportional to the bandwidth of the loop filter and A is the gain of the loop filter. Vout(t) is the output of the loop filter and the desired demodulated RF signal. Vout(t) is then applied to the tracking LO phase modulator. The phase vs. voltage characteristic of the LO phase modulator is nonlinear. In practice, for the semiconductor phase modulators the quadratic and cubic nonlinearity terms will dominate over the higher order terms, and the phase-voltage relation can thereby be expressed as:

ϕLO(t)=πVout(t)Vπ,LO(1+c2c1Vπ,LOVout(t)+c3c1Vπ,LO2Vout2(t))

where c 1,c 2 and c 3 represent the terms of the polynomial expansion of the LO phase modulator response. In addition to nonlinearity associated with phase vs. voltage characteristic of the LO phase-modulator, any residual amplitude modulation, as would be expected in practice, may affect the performance of the demodulator in an adverse way. The normalized E-field amplitude of the (optical) LO signal can therefore be expressed as:

PLO(t)P0=ALO(t)A0=1+D1Vout(t)+D2Vout2(t)+D3Vout3(t)

where A 0 if the E-field amplitude of the LO signal in the absence of amplitude modulation. In order to determine the overall dynamical response of the loop, the total phase error is defined as:

ϕe(t)=ϕin(t)ϕLO(t)

Taking the derivative of equation (13), (11) and (2), we obtain the differential equation describing the total phase error in the loop expressed in its general form as:

edt=πVπ,in(ω1V1cos[ω1t]+ω2V2cos[ω2t])
(1+2a2a1Vπ,in(V1sin[ω1t]+V2sin[ω2t])+3a3a1Vπ,in2(V1sin[ω1t]+V2sin[ω2t])2)
AπτLFVπ,LO(1+2c2c1Vπ,LOVout(t)+3c3c1Vπ,LO2Vout2(t))(Vpd(t)Vout(t))

It should be noted that Eq. (14) includes the effects of cascaded sources of nonlinearities associated with the input phase modulator, sinusoidal response of the balanced receiver, photodetectors and tracking LO phase modulator, giving a good insight into demodulators dynamics. We are therefore going to base our model on Eq. (14) and (10). By solving Eq. (10) together with Eq. (14), the desired demodulated signal, Vout(t), is obtained characterizing the overall nonlinear response of the loop. Eq. (14) and (10) are first order non-linear differential equations and their solutions can be obtained numerically.

When the input RF signal consists of relatively closely spaced frequencies, the nonlinear response of the loop components will result in intermodulation distortion of the demodulated signal. 3rd order intermodulation products are especially important because they may set the Spurious Free Dynamic Range (SFDR) of the system [10]. The demodulated signal, Vout(t) is then characterized by the Signal-to-Intermodulation Ratio (SIR) which is the ratio between the power of the demodulated signal (ω 1 or ω 2) and 3rd order mixing product (2ω 1-ω 2,2ω 2-ω 1). Loop gain is defined as: K=(πPinP0ARpdRL)Vπ,LOτLF .

4. Linearity analysis based on perturbation theory

The time domain numerical model, based on nonlinear differential Eq. (14) and (10) is of rather complex nature and there are many parameters involved. The model is therefore detailed and in good agreement with experimental results, as it will be shown in section 5. However, due to the complex behavior of the nonlinear systems, it may be cumbersome to interpret its results. In this section, we therefore derive simple approximate analytical expressions which are qualitatively in good agreement with time domain numerical model. The analytical expressions are going to be used to interpret results obtained by the detailed time domain numerical model. For simplicity, the loop filter and nonlinearities associated with the photodetectors are not considered. Furthermore, Vπ is assumed equal for the input and tracking LO phase modulator.

Let Vref(t) denote the signal incident at the tracking LO phase modulator when the loop is open:

Vref(t)=2RpdPinPLORLAsin[πVπ,LOVin(t)πVπ,LO(Vout(t)+c′2Vout2(t)+c′3Vout3(t))+ϕ0]
2RpdPinPLORLAsin[ϕ0]+G1[Vin(t)Vout(t)c′2Vout2(t)c′3Vout3(t)]
G2[Vin(t)Vout(t)c′2Vout2(t)c′3Vout3(t)]2
G3[Vin(t)Vout(t)c′2Vout2(t)c′3Vout3(t)]3

where c2=c 2/(c 1 V π,LO), c3=c 3/(c 1 V 2 π,LO) and ϕ 0 is a constant. G1=(2RpdPinPLORLAπ3cos[ϕ0])6Vπ,LO3 , G2=(2RpdPinPLORLAπ2sin[ϕ0])2Vπ,LO2 and G3=(2RpdPinPLORLAπ3cos[ϕ0])6Vπ,LO3 . However, since the DC term is out of the signal band and it is filtered away when the loop is locked, we chose not to consider the DC term. Since the response of the optical phase demodulator will be nonlinear due to the inherently nonlinear response of the balanced receiver (tracking signal Vref(t) is a nonlinear function), the output signal of the demodulator, Vout(t), after locking the loop can be approximated as [10]:

Vout(t)=A1Vin(t)+A2Vin2(t)+A3Vin3(t)

where A 1, A 2 and A 3 are constants. We assume that 3rd mixing product A 3 V 3 in(t) will have larger impact on the SFDR than the second order mixing product A 2 V 2 in(t) and we chose therefore not to consider the second order mixing product. Furthermore, the input signal Vin(t) consists of closely spaced tones: Vin(t)=V 1sin[ω 1 t]+V 1sin[ω 2 t]. In order to find A 1 and A 3, we lock the loop Vref(t)=Vout(t) and insert Eq. (16) in (15). Using the method of harmonic balance the coefficients A 1 and A 3 are found. The demodulated signal, Vout(t) is then expressed as:

Vout(t)=G11+G1Vin(t)(c′3G14+G32G2c′2G12)(1+G1)4Vin3(t)

It is observed from Eq. (17), that for a specific c2 by adjusting the loop parameters, the 3rd order mixing product of the demodulated signal can be (theoretically) brought to zero, i.e. A 3=0. In other words the feedback circuit in combination with second order nonlinearity associated with tracking LO phase modulator response, results into cancellation of 3rd order mixing product of the demodulated signal.

In addition to nonlinearities of the LO phase-modulator, any residual amplitude modulation would be present as explained in section 3. We therefore need to investigate the impact of the residual amplitude modulation on the SIR. Inserting Eq. (12) and (16) in (15), and locking the loop Vref(t)=Vout(t), the output signal can be expressed as:

Vout(t)=G11+G1Vin(t)(2G2c′2G12+D1G14c′2+G3+c′3G14D2G13D1G1G2(1+G1)4)Vin3(t)

The result presented in Eq. (18) is encouraging since the nonlinearities associated with the tracking LO phase modulator can be cancelled out. Either loop gain can be used in order to obtain cancellation of the nonlinearities, or for a specific loop gain the tracking LO can be tailored such that the nonlinearities cancel out.

5. Experimental results

The simulation results shown in this section and next sections are obtained by the detailed time domain numerical model based on Eq. (14) and (10). The experimental set-up, similar to Fig. 1, was constructed in order to verify the model [4]. The experimental bandwidth is limited by the time delay imposed by the discrete components of the receiver. An integrated version of the receiver is necessary to scale to GHz operation.

 figure: Fig. 2.

Fig. 2. (a) One tone measurement. Output of the balanced photodetector, Vpd(t), as a function of loop gain. (b) Two tone measurement. SIR as a function of input signal modulation depth, Min.

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In Fig. 2 (a), a one-tone measurement is shown together with simulation results. Due to the experimental bandwidth limitation the input RF signal frequency is only f 1=150 kHz and the loop filter bandwidth is 1.1 MHz. The amplitude of the signal after balanced photodetection, Vpd(t), is plotted as a function of the loop gain, K. Experimental and simulation results show that as the loop gain is increased, the amplitude of Vpd(t) is reduced, i.e. the linearity of the demodulator is improved. Good agreement between the experimental and simulation results is obtained for one tone measurement. In Fig. 2 (b), results of the two tone measurement are shown together with the simulation results. The SIR is plotted as a function of the modulation depth, Min=(π/V π,in)V 1, of the input RF signal. V 1 is the amplitude of the input RF signal and is assumed equal for both tones. The input RF signal frequencies are: f 1=150 kHz and f 2=170 kHz. As expected, the SIR decreases as Min is increased. Once again good agreement between the model and experimental results is observed.

6. Effects of loop gain and LO phase-modulator nonlinearities

We set a goal of 90 dB of the SIR for the modulation depth of π/2. As mentioned in the introduction the modulator distortion, especially of the tracking LO phase modulator in the considered case, will usually dominate over the photodiode distortion. We therefore assume that the tracking LO phase modulator is much more nonlinear than the photodiodes, i.e. c 2/b 2>>1 and c 3/b 3>>1. Furthermore, electronics nonlinearities can be suppressed by the feedback loop and only need to be lower than the nonlinearities of the tracking LO phase modulator response. In contrast, the tracking LO phase modulator nonlinearities are not suppressed and must therefore be carefully considered. However, a linear input phase modulator is considered.

In Fig. 3 (a), Signal-to-Intermodulation Ratio (SIR) is computed as a function of the loop gain when the ratio between loop filter bandwidth and the RF input signal frequency, (fLF/f 1), is varied. Input RF signal Vin(t) includes two closely spaced frequencies: ω 1/2π=f 1 and ω 2/2π=f 2, as shown in Eq. (3). Linear tracking LO phase-modulator is assumed in Fig. 3 (a). The intermodulation is the magnitude of the mixing terms (2f 1-f 2,2f 2-f 1).

 figure: Fig. 3.

Fig. 3. RF input signal modulation depth Min=π/2. (a) SIR of the demodulated signal as a function of normalized loop gain for selected values of the ratio fLF/f 1. (b) SIR of the demodulated signal as a function of the ratio c 1/c 3 of the LO phase-modulator. Quadratic term c 2=0.

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Figure 3 (a) illustrates that as the loop gain K is increased, the performance of the phase-locked demodulator improves in terms of SIR, i.e. the SIR of the demodulated signal increases. As the ratio, (fLF/f 1), is significantly increased, the SIR converges. Furthermore, the slope of the SIR line is approximately 3. As observed in Fig. 3 (a) relatively large values of the SIR can be obtained provided large loop gain and linear tracking LO phase-modulator. Using Eq. (17) and setting c 2,c 3=0, the expression for the SIR can be obtained:

SIR=20log[8(1+G1)3Min2]

Even though Eq. (19) is derived for the loop without the loop filter, it is in good correspondence with Fig. 3 (a). Eq. (19) and Fig. 3 (a) show that the SIR increases with loop gain with a slope of 3.

One of the key challenges in creating a linear demodulator is the linearity of the tracking LO phase-modulator. The phase-change vs. voltage characteristic of the LO phase-modulator is nonlinear and thereby reducing the SIR of the demodulated signal. First, we are going to investigate the impact of cubic nonlinearity on the SIR. In Fig. 3 (b), SIR is computed as the ratio between the linear term (c 1) and cubic term (c 3) of the LO phase-modulator response for selected values of the loop gain. In general, the SIR decreases as the ratio c 1/c 3 decreases. The values of c 1/c 3 for which SIR starts to decrease are loop gain dependent since the nonlinearities of the LO phase-modulator become more enhanced as the loop gain is increased. This is also in accordance with Eq. (17), i.e. as the loop gain is increased 3rd order mixing product increases as well. For the loop gain of K=10∙107 rad/s, the ratio c 1/c 3 needs to be > 200, to maintain the SIR of 90 dB. Very recently, the the ratio between cubic term and linear term c 1/c 3 of the semiconductor phase modulator has been measured to be 26 [9]. Obviously, a lot of improvement is needed in order to obtain the c 1/c 3=200.

Next, we investigate how the quadratic term c 2 of the nonlinear response of the phase modulator can be used to cancel out 3rd order mixing product of the demodulated signal.

 figure: Fig. 4.

Fig. 4. SIR of the demodulated signal as a function of c 1/c 3. The ratio c 1/c 2 takes values: 80,60,40,20. (b) SIR of the demodulated signal as a function of loop gain, K. c 1/c 2=40 and c 1/c 3=20+Δoffset.

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In Fig. 4 (a), SIR of the demodulated signal is computed as a function of the ratio c 1/c 3 for the selected values of c 1/c 2 ratio. For the reference a SIR is also plotted for the case when c 2=0. The selected values of the ratio c 1/c 2 are experimentally obtainable for electrical circuits [10]. To the author’s best knowledge the measurement of the quadratic term for the semiconductor phase-modulators has not been performed yet, however, some initial measurements are under constructions by the authors group. We have therefore varied the ratio c 1/c 2 in order to cover low and high values. Fig. 4 (a) shows that as the ratio c 1/c 2 is decreased the SIR becomes severely limited by the second order nonlinearity. Furthermore, for low values of the third order nonlinearity of the LO phase modulator, the SIR becomes completely dominated by the second order nonlinearity, i.e. independent of the c 1/c 3 ratio. This is in accordance with Eq. (17), i.e. if c 3 is low 3rd order mixing product of the demodulated signal is dominated by c 2. However, the results in Fig. 4 (a) also show that for non-zero values of c 2, there exist a combination of c 2 and c 3 for which the 3rd order mixing product is minimized, i.e. peaking (resonance) of the SIR. This implies that the combined effects of the nonlinearities associated with the balanced receiver and the nonlinear LO phase-modulator response plus the gain contribution from the feedback loop, result in cancellation of 3rd order mixing product. This is also observed from Eq. (17) as stated earlier. Furthermore, the resonance peak moves towards lower higher of c 3 as c 2 is increased. So, by having second order nonlinearity associated with tracking LO phase modulator, we can tolerate more cubic nonlinearity, c 3. Having the ratio c 1/c 3 of only 20 and c 1/c 2=40, the SIR of 90 dB can still be obtained.

Suppose that we want to tailor the phase-modulator such that SIR peaking is obtained. In practise, we may not be able to match exactly the required values of c 1/c 3 and c 1/c 2 in order to obtain SIR peaking, so we need to investigate what happens if we are slightly off. In Fig. 4 (b), the SIR is computed as a function of loop gain when the ratio c 1/c 3 is varied from the exact value of c 1/c 3 for which the SIR peaking is obtained, i.e. c 1/c 3=20+Δoffset. The ratio c 1/c 2=40 is held constant. Fig. 4 (b) shows that the SIR peaking is dependent on the loop gain and it occurs in a relatively wide band of the loop gain. It is also noticed that as the ratio c 1/c 3 is varied, the resonant peak of the SIR moves as well. So, by adjusting the loop gain resonant peaking of the SIR can be re-obtained. Another, thing which should be addressed is frequency dependence of c 3 if the demodulator is operated over wide frequency range. Frequency dependence will cause the c 1/c 3 to vary, and Fig. 4 (b) can be used to observe the effect of varying c 1/c 3. If the ratio c 1/c 3 varies with frequency for a specific loop gain, we will move away from the resonant peaking of the SIR. One solution could be to re-adjust the loop gain or to design wide band tracking LO phase modulator. Furthermore, the demodulator could be designed to operate in narrow frequency band.

7. Effects of residual amplitude modulation

In this section, the impact of residual amplitude modulation on the SIR is considered. Nonlinear phase response associated with the tracking LO phase modulator is set to zero, i.e. c 2=c 3=0. From Eq. (18) it can be observed that D 1 and D 2 will have impact on the 3rd order mixing product of the demodulated signal. However, as seen in Eq. (18) D 3 has no impact on the 3rd order mixing product of the demodulated signal. In practice, coefficients D 1, D 2 and D 3 can be related to the absorption coefficient of the tracking LO phase modulator.

 figure: Fig. 5.

Fig. 5. (a) SIR of the demodulated signal as a function of Dx for x=1,2,3. (c2, c3)=0. (b) SIR of the demodulated signal as a function of c 1/c 3 for selected values of the quadratic term, D 2, of the residual amplitude modulation. c 1/c 2=40 and D 1=0.03 1/V.

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In Fig. 5 (a), the SIR of the demodulated signal is computed as a function of Dx where x=1,2 and 3. We assume that terms Dx where x > 3 are negligible, as it would be expected in practice. Fig. 5 shows that as D 1 (Dx=0,x=2,3) is increased beyond 5∙10-3 1/V, the SIR starts to decrease. When D 2 is varied (Dx=0,x=1,3) resonant behavior of the SIR, similar to Fig. 4(b), is observed, i.e. there exist a value of D 2 for which the 3rd order mixing product is minimized. Furthermore, we observe, Fig. 5 (a), that the effect of D 1 is more deteriorating than that of D 2. For the case when D 3 is varied (Dx=0,x=1,2), the SIR is not affected and this is in accordance with Eq. (18). Usually, for the semiconductor phase modulator, the quadratic term of the amplitude modulation is more difficult to minimize than the linear term. We therefore need to concentrate on the quadratic term of amplitude modulation.

8. Combined effects of nonlinearities and their cancellation

In this section, the combined effect of nonlinearities (nonlinear phase response and residual amplitude modulation) associated with tracking LO phase modulator are considered. We pay more attention on the quadratic term, D 2, of the residual amplitude modulation since it is more difficult to reduce (in practice) for semiconductor phase modulators, compared to the linear term, D 1.

In Fig. 5 (b), SIR is computed as a function of the the ratio c 1/c 3 when D 2 is varied from 10-3 1/V to 10-1 1/V. The ratio c 1/c 2 is set to 40 and D 1=0.03 1/V. It is observed from Fig. 5 (b) that for low values of cubic nonlinearity (c 3) of the phase modulator response, the SIR is fully limited by the quadratic term of residual amplitude modulation, D 2. However, Fig. 5(b) also shows that there exists a combination of c 3, c 2, D 1 and D 2 for which the 3rd order mixing product is minimized, i.e. peaking (resonance) of the SIR. The resonant peak moves towards lower values of c 1/c 3 ratio as D 2 is increased. Fig. 5 (b) is in accordance with Eq. (18) which states that 3rd order mixing product can be reduced by proper combination of the loop gain and tracking LO phase modulator nonlinearities. The cascaded sources of nonlinearities associated with balanced detector, phase and amplitude modulation of the tracking LO phase modulator cancel each other. Fig. 5 (b) illustrates that even though the ratio c 1/c 3 is low for the measured semiconductor phase modulator (c 1/c 3=26[9]), high values of the SIR are still obtainable.

Next, we are going to investigate how the resonant peaking of the SIR scales with input RF signal voltage and frequency. We must be sure that the cancellation of the nonlinearities does not only occur at single power level or single frequency. Nonlinearities associated with the tracking LO phase modulator are chosen such that resonant peaking of the SIR is obtained, see Fig. 5 (b). In Fig. 6 (a), we plot the amplitude of the fundamental of the demodulated signal (f 1) and amplitude of the 3rd order intermodulation product (2f 1-f 2) as a function of input signal voltage, Vin. The amplitude of the fundamental and 3rd order intermodulation product (IM3 curve) of the demodulated signal increases with the input signal voltage, as expected. It should be observed that there are no dips in the IM3 curve as the input signal voltage is varied. This means that the cancellation of the nonlienarities associated with the balanced receiver and phase modulator occurs over broad range of input RF signal powers. In Fig. 6 (b), the SIR is computed as a function of input RF signal frequency as the input signal modulation depth, Min takes values from π to π/7. Fig. 6 (b) shows that the SIR remains constant as the input RF signal frequency is increased. As the input RF signal modulation depth decreases, the SIR increases as expected.

9. Conclusion

A novel cancellation technique, which is RF signal power and frequency independent, for the recently demonstrated phase-locked coherent optical phase demodulator is proposed and numerically investigated. It has been shown that the interplay between the loop gain of the feedback circuit and nonlinearities of the tracking LO phase modulator may result in cancellation of the third order intermodulation product of the demodulated signal. The cancellation of the third order intermodulation product can be achieved by carefully tailoring the nonlinearities of the tracking LO phase modulator, or for the specific set of nonlinearities loop gain can be adjusted such that cancellation is obtained. The proposed technique significantly reduces linearity requirements for the tracking LO phase modulator and large values of the signal-to-intermodulation ratio can thereby be obtained even though the tracking LO phase modulator is fairly nonlinear.

 figure: Fig. 6.

Fig. 6. c 1/c 3=10, c 1/c 2=40, D 1=0.03 1/V and D 2=0.05 1/V. (a) Amplitude of the fundamental and 3rd order mixing product (IM3 curve) of the demodulated signal as a function of input signal voltage, Vin. (b) SIR of the demodulated signal as a function of input signal frequency for selected values of modulation depth Min

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Acknowledgments

This material is based upon work supported by the DARPA PHOR-FRONT program under United States Air Force contract number FA8750-05-C-0265. The authors thank Larry Lembo, Steve Pappert, Larry Coldren, Mat Sysak, Mark Rodwell and Roy Smith for useful conversations and input.

Footnotes

The scalar notation is used for both Ein(t) and ELO(t) by assuming that the two fields are identically polarized.
Due to the residual amplitude modulation of the tracking LO phase modulator PLO will be time dependent. This is explained in more details later in the text

References and links

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7. D. Zibar, L. A. Johansson, H. F. Chou, A. Ramaswamy, and J. E. Bowers, “Time Domain Analysis of a Novel Phase-Locked Coherent Optical Demodulator,” in Optical Amplifiers and Their Applications/Coherent Optical Technologies and Applications, Technical Digest (CD) (Optical Society of America, 2006), paper JWB11.

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Figures (6)

Fig. 1.
Fig. 1. General outline of phase-modulated optical link and phase-locked optical demodulator at the receiver unit.
Fig. 2.
Fig. 2. (a) One tone measurement. Output of the balanced photodetector, Vpd (t), as a function of loop gain. (b) Two tone measurement. SIR as a function of input signal modulation depth, Min .
Fig. 3.
Fig. 3. RF input signal modulation depth Min =π/2. (a) SIR of the demodulated signal as a function of normalized loop gain for selected values of the ratio fLF /f 1. (b) SIR of the demodulated signal as a function of the ratio c 1/c 3 of the LO phase-modulator. Quadratic term c 2=0.
Fig. 4.
Fig. 4. SIR of the demodulated signal as a function of c 1/c 3. The ratio c 1/c 2 takes values: 80,60,40,20. (b) SIR of the demodulated signal as a function of loop gain, K. c 1/c 2=40 and c 1/c 3=20+Δ offset .
Fig. 5.
Fig. 5. (a) SIR of the demodulated signal as a function of Dx for x=1,2,3. (c2, c3)=0. (b) SIR of the demodulated signal as a function of c 1/c 3 for selected values of the quadratic term, D 2, of the residual amplitude modulation. c 1/c 2=40 and D 1=0.03 1/V.
Fig. 6.
Fig. 6. c 1/c 3=10, c 1/c 2=40, D 1=0.03 1/V and D 2=0.05 1/V. (a) Amplitude of the fundamental and 3rd order mixing product (IM3 curve) of the demodulated signal as a function of input signal voltage, Vin . (b) SIR of the demodulated signal as a function of input signal frequency for selected values of modulation depth Min

Equations (26)

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E in ( t ) = P in e j ( ω 0 t + ϕ in ( t ) )
ϕ in ( t ) = π V in ( t ) V π , in ( 1 + a 2 a 1 V π , in V in ( t ) + a 3 a 1 V π , in 2 V in 2 ( t ) )
V in ( t ) = V 1 sin [ ω 1 t ] + V 2 sin [ ω 2 t ]
E LO ( t ) = P LO ( t ) e j ( ω 0 t + ϕ LO ( t ) )
E 1 ( t ) = 1 2 P in e j ( ω 0 t + ϕ in ( t ) π 2 ) + 1 2 P LO ( t ) e j ( ω 0 t + ϕ LO ( t ) π )
E 2 ( t ) = 1 2 P in e j ( ω 0 t + ϕ in ( t ) π ) + 1 2 P LO ( t ) e j ( ω 0 t + ϕ LO ( t ) π 2 )
I 1 ( t ) = R pd E 1 ( t ) 2 ( 1 + b 2 E 1 ( t ) 2 b 1 + b 3 E 1 ( t ) 3 b 1 )
= R pd n = 1 3 b n b 1 ( 1 2 P in + 1 2 P LO ( t ) P in P LO ( t ) sin [ ϕ in ( t ) ϕ LO ( t ) ] ) n
I 2 ( t ) = R pd E 2 ( t ) 2 ( 1 + b 2 E 2 ( t ) 2 b 1 + b 3 E 2 ( t ) 3 b 1 )
= R pd n = 1 3 b n b 1 ( 1 2 P in + 1 2 P LO ( t ) + P in P LO ( t ) sin [ ϕ in ( t ) ϕ LO ( t ) ] ) n
V pd ( t ) = R L ( I 2 ( t ) I 1 ( t ) )
dV out dt = A [ V pd ( t ) V out ( t ) τ LF ]
ϕ LO ( t ) = πV out ( t ) V π , LO ( 1 + c 2 c 1 V π , LO V out ( t ) + c 3 c 1 V π , LO 2 V out 2 ( t ) )
P LO ( t ) P 0 = A LO ( t ) A 0 = 1 + D 1 V out ( t ) + D 2 V out 2 ( t ) + D 3 V out 3 ( t )
ϕ e ( t ) = ϕ in ( t ) ϕ LO ( t )
e dt = π V π , in ( ω 1 V 1 cos [ ω 1 t ] + ω 2 V 2 cos [ ω 2 t ] )
( 1 + 2 a 2 a 1 V π , in ( V 1 sin [ ω 1 t ] + V 2 sin [ ω 2 t ] ) + 3 a 3 a 1 V π , in 2 ( V 1 sin [ ω 1 t ] + V 2 sin [ ω 2 t ] ) 2 )
A π τ LF V π , LO ( 1 + 2 c 2 c 1 V π , LO V out ( t ) + 3 c 3 c 1 V π , LO 2 V out 2 ( t ) ) ( V pd ( t ) V out ( t ) )
V ref ( t ) = 2 R pd P in P LO R L A sin [ π V π , LO V in ( t ) π V π , LO ( V out ( t ) + c′ 2 V out 2 ( t ) + c′ 3 V out 3 ( t ) ) + ϕ 0 ]
2 R pd P in P LO R L A sin [ ϕ 0 ] + G 1 [ V in ( t ) V out ( t ) c′ 2 V out 2 ( t ) c′ 3 V out 3 ( t ) ]
G 2 [ V in ( t ) V out ( t ) c′ 2 V out 2 ( t ) c′ 3 V out 3 ( t ) ] 2
G 3 [ V in ( t ) V out ( t ) c′ 2 V out 2 ( t ) c′ 3 V out 3 ( t ) ] 3
V out ( t ) = A 1 V in ( t ) + A 2 V in 2 ( t ) + A 3 V in 3 ( t )
V out ( t ) = G 1 1 + G 1 V in ( t ) ( c′ 3 G 1 4 + G 3 2 G 2 c′ 2 G 1 2 ) ( 1 + G 1 ) 4 V in 3 ( t )
V out ( t ) = G 1 1 + G 1 V in ( t ) ( 2 G 2 c′ 2 G 1 2 + D 1 G 1 4 c′ 2 + G 3 + c′ 3 G 1 4 D 2 G 1 3 D 1 G 1 G 2 ( 1 + G 1 ) 4 ) V in 3 ( t )
SIR = 20 log [ 8 ( 1 + G 1 ) 3 M in 2 ]
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