US 7,266,306 B1Grant
Method for optical carrier suppression and quadrature control
Issue Date:2007-09-04
•8 Claims
•7 Drawing Sheets
Abstract
A suppressed carrier optical communications signal is generated by driving (biasing) an optical modulator capable of complex modulation of an optical carrier signal to a bias point near a zero-crossing point of the modulator's E-field response. A complex input signal is then used to drive excursions of the E-field response to impress the input signal onto the optical carrier. The resulting lightwave emerging from the complex modulator exhibits an optical spectrum characterized by a pair of sidebands and a strongly suppressed carrier. Bias control of the complex modulator is implemented on the basis of the optical power detected at the output of the complex modulator. This enables the optical modulator to be treated as a “black box”, in that calculation of the bias signals does not relay on knowledge of the precise performance characteristics of the modulator.
Metadata
Assignee
- Nortel Networks Limited
Inventors
- James Harley
- Kim Roberts
Application Information
Application Number:US 10/677,276
Filing Date:2003-10-03
Priority Date:2003-10-03
Art Unit:2613
Classifications
IPC:
H04B10/04
Patent Drawings (7 sheets)
Description
CROSS-REFERENCE TO RELATED APPLICATIONS
[0001] This is the first application filed for the present invention.
BACKGROUND OF THE INVENTION
Microfiche Appendix
[0002] Not Applicable.
Technical Field
[0003] The present invention relates to optical signal transmitters for optical communications systems, and in particular to optical transmission carrier suppression in optical communications systems.
[0004] In the optical communications space, various techniques are used to synthesize an optical communications signal for transmission. A popular technique utilizes a laser 2 coupled to an external optical modulator 4, as shown in FIG. 1 a. The laser 2 generates a narrow-band continuous wave (CW) optical carrier signal 6 having a desired wavelength. The optical modulator 4 operates to modulate the amplitude and/or phase the carrier signal 6 to generate the optical communications signal 8 using a drive signal 10 that encodes data to be transmitted. Typically, an optical coupler 12 at the output of the optical modulator 4 taps the communications signal 8, and supplies the tapped signal 14 to a conventional photodetector 16. The detection signal 18 output by the photodetector 16 provides a feed-back signal that is used by control circuits (not shown) to monitor and optimize performance of both the laser 2 and modulator 4.
[0005] In the arrangement illustrated in FIG. 1 a, the optical modulator 4 is provided by a Mach-Zehnder (MZ) modulator. Other types of modulators may be used, depending on the desired type of modulation. For example, an electro-absorptive modulator (EAM) or a variable optical attenuator may be used for amplitude modulation; whereas phase shifters are well known for implementing phase modulation. In the case of a Mach-Zehnder modulator, the drive signal 10 and a DC bias 20 are used to control a differential phase delay experienced by light traversing the two branches 22a, b of the modulator, via the well known electro-optical effect. The optical power of the recombined lightwave (communications signal 8) emerging from the MZ modulator varies sinusoidally with the phase angle between the beams traversing to two branches 22, and thus can be controlled by the drive and bias signals 10 and 20. As such, the MZ modulator displays a sinusoidal response to the applied input voltage as shown in FIG. 2 .
[0006] In operation, the DC bias signal 20 is used to drive the modulator to a bias point 24 corresponding to an inflection point of the response curve (which normally corresponds to a phase difference of 90 degrees between the beams transiting the two branches of the MZ modulator). The drive signal 10, which carries the data being transmitted, can then drive excursions of the phase difference between 0 and 180 degrees, corresponding to maximum and minimum transmittance, respectively. This operation is typically employed in communications networks to implement On—Off—Keying (OOK) transmission protocols.
[0007] In theory, a phase difference of 180 degrees causes perfect destructive interference between the two light beams, resulting in total extinction of the communications signal 8 at the output of the modulator. However, in practice, manufacturing defects and other impairments mean that total extinction is rarely achieved. At least some light “leaks” through the modulator 4, and appears in the communications signal 8 as optical power at the carrier signal wavelength. In the modulator response curve (see FIG. 2 a) this “leakage” 26 manifests itself as a non-zero optical power at the minimum transmittance point 28.
[0008] FIG. 1 b illustrates a variant of the MZ modulator of FIG. 1 a, in which both branches of the MZ modulator can be independently driven using respective drive signals 10a and 10b. Differently driving both branches 22 of the MZ modulator (i.e., one drive signal 10a is the inverse of the other drive signal 10b) provides the same amplitude modulation functionality as that described above with reference to FIG. 1 a, but at lower voltage levels. Chirp in the recombined lightwave (communications signal 8) emerging from the MZ modulator can be controlled by applying a scaling factor to one (or both) of the differential drive signals 10a, 10b.
[0009] FIG. 1 c shows a complex optical modulator 30 composed of three nested MZ modulators. Thus, the CW carrier signal 6 from the laser 2 is divided into two branches 22a and 22b of an “outer” MZ modulator. Each branch 22a,b of the of outer MZ modulator includes a respective “branch” MZ modulator 4a,b of the type described above with reference to either of FIGS. 1 a and 1b. Such devices are commercially available, and provide a convenient hardware means of implementing independent phase and amplitude modulation of the CW carrier 6. Some commercially available devices include an integral optical tap 12 and photodetector 16 to facilitate monitoring of device operation. The nested MZ modulator architecture of FIG. 1 c enables use of complex modulation schemes, such as Quadrature Phase shift Keying (QPSK).
[0010] In all of these cases, the (or each) modulator 4, 30 is driven to a bias point 24 corresponding to an inflection point of its response curve (see FIG. 2 ), so that the drive signal(s) 10 can induce appropriate amplitude and/or phase excursions to encode data onto the carrier signal 6. A limitation of this approach is that the optical power of the communications signal 8 is distributed between a residual carrier signal 6a and a pair of side-bands 32a,b, as shown in FIG. 3 . The energy of the residual carrier signal 6a (hereinafter simply “carrier 6a”) is the result of contributions from both the bias point 24 (since it represents a “DC-offset” of the sinusoidal response curve) and leakage 26 at the minimum transmittance point. The side-bands 32 contain the frequency-content of the drive signal(s) 10, and thus represent the encoded data being conveyed by the communications signal 8. Because the carrier 6a does not contain encoded data, it is effectively redundant for communications purposes. However, the optical energy of the carrier 6a reduces the energy within the side-bands 32, and increases optical impairments within the communications system. Both of these factors reduce signal reach.
[0011] Accordingly, methods and apparatus for synthesizing an optical communications signal in which the carrier is suppressed, would be highly desirable.
SUMMARY OF THE INVENTION
[0012] Accordingly, an object of the present invention is to provide methods and apparatus for synthesizing a suppressed carrier optical communications signal.
[0013] Thus, and aspect of the present invention provides a method for synthesizing suppressed carrier optical communications signals. According to the invention, an optical modulator capable of complex modulation of an optical carrier signal is driven (biased) to a bias point near a zero-crossing point of the modulator's E-field response. A complex input signal is then used to drive excursions of the E-field response to impress the input signal onto the optical carrier. The resulting lightwave emerging from the complex modulator exhibits an optical spectrum characterised by a pair of sidebands and a strongly suppressed carrier. Bias control of the complex modulator is implemented on the basis of the optical power detected at the output of the complex modulator. This enables the optical modulator to be treated as a “black box”, in that calculation of the bias signals does not relay on knowledge of the precise performance characteristics of the modulator.
BRIEF DESCRIPTION OF THE DRAWINGS
[0014] Further features and advantages of the present invention will become apparent from the following detailed description, taken in combination with the appended drawings, in which:
[0015] FIGS. 1 a-1c schematically illustrate communications signal synthesizers known in the prior art;
[0016] FIG. 2 illustrates typical response of the synthesizers of FIGS. 1 a-1c;
[0017] FIG. 3 shows a typical spectrum of the optical communications signal generated by the synthesizers of FIGS. 1 a-1c;
[0018] FIGS. 4 a and 4b schematically illustrate principal elements an operation of a system for synthesizing suppressed carrier optical communications signals, in accordance with respective embodiments of the present invention;
[0019] FIG. 5 illustrates typical response of the system of FIGS. 4 a and 4b;
[0020] FIG. 6 shows a typical spectrum of the optical communications signal generated by the system of FIGS. 4 a and 4b;
[0021] FIG. 7 schematically illustrates principal elements and operation of a complex driver circuit usable in the embodiment of FIG 4a; and
[0022] FIG. 8 schematically illustrates principal elements an operation of a system for synthesizing suppressed carrier optical communications signals, in accordance with a third embodiment of the present invention.
[0023] It will be noted that throughout the appended drawings, like features are identified by like reference numerals.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT
[0024] The present invention provides methods and systems for synthesizing suppressed carrier optical communications signals. Embodiments of the invention are described below, by way of example only, with reference to FIGS. 4-8 .
[0025] In broad terms, the present invention provides a synthesizer system 33 comprising a complex optical modulator 30 and a controller 36, as shown in FIG. 4 a. In operation, the controller 36 drives the complex modulator 30 to a bias point near a zero-crossing point of the modulator's E-field response. A complex input signal 34 is then used to drive excursions of the E-field response about the bias point. Embodiments of the invention may also include a complex driver 58 for generating the complex input signal 34 based on a binary input signal x(t) (which may, for example, be a serial bit stream), as will be described below with reference to FIGS. 7 and 8 .
[0026] As shown in FIG. 4 a, the complex optical modulator may conveniently be provided by a conventional “nested” Mach-Zehnder modulator architecture of the type described above with reference to FIG. 1 c.
[0027] As described above, the optical tap 12 and detector 16 may be provided by a conventional optical coupler (e.g. a 20 dB coupler) and a photodetector 16. With this arrangement, a small portion of the communications signal ET(t) 8 emerging from the complex optical modulator 30 is tapped and supplied to the photodetector 16, the output of which is an electrical detector signal 18 (typically a current) proportional to the optical power [ET(t)]2. The detector signal 18 is supplied to the controller 36, and used to determine the level of bias signals b1-b3 for controlling the bias point of the complex optical modulator 30, as will be described in greater detail below.
[0028] The format of the complex input signal 34 will normally be selected to take best advantage of the architecture of complex modulator 30. In the embodiment of FIG. 4 , a nested MZ modulator architecture is used. With this architecture, the communications signal 8 is generated by summation of the modulated light emerging from each of the branch modulators 4a,4b. This architecture is particularly suited to being driven by a complex input signal 34 in the form of a pair of Cartesian coordinate signal components 10, such as, for example, In-Phase and Quadrature signal components VI(t) 10a and VQ(t) 10b. The signal components VI(t) 10a and VQ(t) 10b each include a unique low frequency (on the order of a few hundred Hertz) dither signal, d1 and d2 respectively. In the embodiment of FIG. 4 a, the dithers d1 and d2 are inserted into the signal components VI(t) 10a and VQ (t) 10b by complex driver 58. This embodiment is described in greater detail below with reference to FIG. 7 . FIG. 4 b illustrates an alternative arrangement, in which the dithers d1 and d2 are inserted into the signal components VI (t) 10a and VQ (t) 10b downstream of the complex driver 58. In either case, each of the signal components may be provided as a single signal (e.g. referenced to ground) or by a differential signal pair, as desired, and are used to drive respective branch MZ modulators 4a,4b of the complex optical modulator 30. With this arrangement, the signal components VI(t) 10a and VQ (t) 10b will be impressed onto the light traversing each respective branch 22a,22b of the complex modulator 30 to generate branch optical signals EI(t) and EQ (t). The branch optical signals are recombined at the output of the complex modulator 30 to generate the communications signal 8 in which the E-field ET(t) may be described by an equation of the form:
ET(t)=EI(t)+jEQ(t)ej74 q (Eq. 1)
where: θq is the phase difference (angle) between EI (t) and EQ (t). With this formation, the optical power [ET(t)]2 detected by the photodetector 16 will be given by:
|ET(t)|2=EI(t)2+EQ(t)2−2EI(t)EQ(t)sin(θq) (Eq. 2)
ET(t)=EI(t)+jEQ(t)ej74 q (Eq. 1)
where: θq is the phase difference (angle) between EI (t) and EQ (t). With this formation, the optical power [ET(t)]2 detected by the photodetector 16 will be given by:
|ET(t)|2=EI(t)2+EQ(t)2−2EI(t)EQ(t)sin(θq) (Eq. 2)
[0029] As mentioned above, the complex optical modulator 30 is driven (biased) by the controller 36 to a bias point near a zero crossing point of the E-field response of the complex optical modulator 30. In the embodiment of FIG. 4 , three bias signals b1-b3 are used for this purpose. Bias signals b1 and b2 control respective bias points of the branch MZ modulators 4a,4b. The third bias signal, b3, controls the phase difference (θq) between ET(t) and EQ(t), and thus the bias point of the “outer” MZ modulator. In the embodiment of FIG. 4 , the bias signals b1-b3 are supplied to respective bias signal input pins of the complex optical modulator 30.
[0030] With the dithers d1 and d2 included in branch signals EI(t) and EQ(t), respectively, the optical power [ET(t)]2 detected by the photodetector 16 will be given by:
|ET(t)|2=|dI(t)2+2EI(t)dI(t)+EI(t)2]+[dQ(t)2+2EQ(t)dQ(t)+EQ(t)2|−2sin (θq)[dI(t)dQ(t)+EQ(t(dI(t)+EI(t)dQ(t)+EQ(t)EI(t)] (Eq. 3)
|ET(t)|2=|dI(t)2+2EI(t)dI(t)+EI(t)2]+[dQ(t)2+2EQ(t)dQ(t)+EQ(t)2|−2sin (θq)[dI(t)dQ(t)+EQ(t(dI(t)+EI(t)dQ(t)+EQ(t)EI(t)] (Eq. 3)
[0031] As will be appreciated, EI(t) and EQ(t) are dominated by high-frequency components related to the line rate (e.g. 10 Gb/sec) of the optical communications system. For the purposes of the present invention, however, we are interested in low frequency dither components of the optical power [ET(t)2, corresponding to the bias signals b1-b3. Under these conditions, Equation 3 above can be simplified by replacing EI(t) and EQ(t) by their respective mean values mI and mQ to yield:
|ET(t)|2=dI(t)2+2mIdI(t)+m2I]+[dQ(t)2+2mQdQ(t)+m2Q]−2sin(θq)[dI(t)dQ(t)+mQdI(t)+mIdQ(t)+mQmI] (Eq. 4)
where: dI(t) and dI(t)2 are the first and second harmonics, respectively, of dither d1; and dQ(t) and dQ(t)2 are the first and second harmonics, respectively, of dither d2; and dI(t)dQ(t) is the beat frequency of dithers d1 and d2 are unique, and known, it is a simple matter to detect the first harmonics dI(t) and dQ(t), and the beat frequency component dI(t) dQ(t) in the optical power [ET(t)]2 detected by the photodetector 16. Thus, the controller 36 includes a respective correlator filter 38a,38b, 38c for detecting a level of each of di(t), dQ(t) and dI(t)dQ(t). The output of each correlator filter is then supplied to a processor 40 which uses this information to adjust respective values of each of the bias signals b1-b3.
|ET(t)|2=dI(t)2+2mIdI(t)+m2I]+[dQ(t)2+2mQdQ(t)+m2Q]−2sin(θq)[dI(t)dQ(t)+mQdI(t)+mIdQ(t)+mQmI] (Eq. 4)
where: dI(t) and dI(t)2 are the first and second harmonics, respectively, of dither d1; and dQ(t) and dQ(t)2 are the first and second harmonics, respectively, of dither d2; and dI(t)dQ(t) is the beat frequency of dithers d1 and d2 are unique, and known, it is a simple matter to detect the first harmonics dI(t) and dQ(t), and the beat frequency component dI(t) dQ(t) in the optical power [ET(t)]2 detected by the photodetector 16. Thus, the controller 36 includes a respective correlator filter 38a,38b, 38c for detecting a level of each of di(t), dQ(t) and dI(t)dQ(t). The output of each correlator filter is then supplied to a processor 40 which uses this information to adjust respective values of each of the bias signals b1-b3.
[0032] Carrier suppression occurs when the mean values mI and mQ are zero. As can be seen from Equation 4, when the mean values mI and mQ are zero, then the first harmonics dI(t) and dQ(t) will not be present in the detector signal 18. In general, the method of the invention is to step bias signal d3 to ensure quadrature, and then step bias signals b1 and b2 such that the detected harmonics dI(t) and dQ(t) are minimized. This is equivalent to minimizing the optical E field means mI mQ, which implies maximizing carrier suppression. As may be appreciated, this control approach uses features explicitly in the optical E field, rather than features explicitly in the electro-optic transfer function. This means the control is more robust to physical device variations.
[0033] More particularly, in order to maintain quadrature, the phase difference θq between ET(t) and EQ(t) must be zero, in which case Sin(θq)=0 and 2Sin(θq)dI(t)dQ(t) will be a minimum (ideally zero), independent of the detected levels of dI(t)2 and dQ(t)2. Since the phase difference θq can be directly controlled by the bias signal b3, the processor 40 operates to adjust the value of bias signal b3 to minimize the detected level of the beat frequency component dI(t)dQ(t), and thereby ensure quadrature. Preferably, the values of bias signals b1 and b2 will be held constant during adjustment of bias signal b3.
[0034] The first harmonic signals dI(t) and dQ(t) are independently controllable by the bias signals b1 and b2, respectively. Accordingly, the processor can operate to adjust bias signal b1 to minimize the detected level of dI(t); and adjust bias signal b2 to minimize the detected level of dQ(t).
[0035] As mentioned previously, FIG. 4 illustrates an embodiment in which the drive signals VI(t) and VQ(t) forming the complex input signal 34 include dithers d1 and d2. FIG. 7 shows a block diagram illustrating a complex driver circuit which provides a practical implementation of this approach.
[0036] In the embodiment of FIG. 7 , a digital input signal x(t), which may be in the form of a serial bit stream, is supplied to a digital filter 46, which implements a mapping function to generate corresponding In-phase and quadrature values I(n) and Q(n) of the complex input signal 34. If desired, the digital filter 46 may also implement a compensation function to electrically pre-compensate impairments of the optical communications system. This functionality is described in detail in application's co-pending U.S. patent applications Ser. Nos. 10/262,944 filed Oct. 3, 2002; 10/307,466 filed Dec. 2, 2002; 10/405,236 filed Apr. 3, 2003, and International Patent Application No. PCT/CA03/01044 filed Jul. 11, 2003. Various known digital filter types may be used to implement the digital filter 46, such as, for example, a Random Access Memory Look-up Table (RAM LUT). Alternatively, the digital filter 46 may be implemented using Finite Impulse Response (FIR) filters, Infinite Impulse Response (IIR) filters, and Fast Fourier Transform (FFT filters). In either case, the digital filter 46 generates the In-phase and quadrature signal component values I(n) and Q(n) 35 at a sample rate which is about double the bit-rate of the input signal x(t). A non-linear compensator 48 (which may also be implemented as a RAM LUT) is used to adjust the value of each successive sample I(n) and Q(n), by digitally adding successive dither values d1(n) of dither signal d1, and dither values d2(n) of dither signal d2, respectively. The non-linear compensator 48 may also be used to compensate non-linear performance of the complex modulator 30, as described in applicant's co-pending U.S. patent applications Ser. No. 10/262,944, filed Oct. 3, 2002; and 10/457,528 filed Jun 10, 2003 entitled “High Speed Digital-to Analog Converter”; and International Patent Application No. PCT/CA03/01044 filed Jul. 11, 2003. The non-linear compensator 48 may be implemented as a separate device cascaded with the digital filter 46, as shown in FIG. 7 , or may be “embedded” within the digital filter 46 by applying the dither signals d1 and d2 (and any other mapping function implemented by the non-linear compensator 48) to the digital filter 46.
[0037] Respective high-speed Digital-to-Analog Converters (DACs) 50a,50b can then be used to convert the sample values into corresponding analog signals. A high-speed DAC suitable for this purpose is known from applicant's co-pending U.S. patent application Ser. No. 10/457,528 filed Jun. 10, 2003. If desired, the analog signals can be conditioned, for example by means of respective filters 52a,52b and low noise amplifiers (LNA) 54a,54b, in a conventional manner, to remove out-of-band noise and to scale the signal amplitude to the dynamic range of the complex modulator 30.
[0038] As may be appreciated, the effects of the independent DACs 50a,50b, the filters 52a,52b and the LNAs 54a,54b for each signal component may cause differential propagation delays between the non-linear compensator 48 and the optical modulator 30. Such differential delay can be compensated by means of digital filters 56a,56b located in at least one of the signal paths. Each digital filter 56a,56b can be controlled in a known manner to impose a selected delay, which is calculated to compensate for the differential propagation delays experienced by each of the signal components.
[0039] As describe above, the bias signals b1-b3 are calculated from the optical power [ET(t)]2 detected by the photodetector 16. The optical power [ET(t)]2 at the output of the complex modulator 30 inherently also includes any effects due to the design and performance characteristics of the of the complex modulator 30. Consequently, the method of the invention automatically selects means values for the bias signals b1-b3 which account for these effects, by driving the modulator 30 to a bias point 42 which ensures quadrature and minimizes leakage. An advantage of this method is that it enables the optical modulator 30 to be treated as a “black box”, in that a generic algorithm can be developed for calculation of the bias signals b1-b3, without specific knowledge of the precise performance characteristics of the complex modulator 30.
[0040] In the embodiments of FIGS. 4-7 , the complex optical modulator 30 is provided using a set of three nested Mach-Zehnder modulators, which is capable of performing complex modulation of the carrier signal 6 when driven by a pair of Cartesian coordinate (e.g. in-phase and Quadrature) signal components. Equations 2-5 above were derived in light of this architecture. However, it will be appreciated that equivalent functionality can be implemented using any optical modulator capable of performing complex modulation of an optical carrier signal 6.
[0041] Referring now to FIG. 8 , there is shown an embodiment of a system 80 in accordance with the invention which generates a carrier suppressed polarization-interleaved communications signal 8′. In this case, a pair of parallel synthesizers 33a and 33b are provided, each of which comprises a respective complex driver 58 and complex modulator 30, which operate as described above with respect to FIGS. 4-7 to generate a respective carrier-suppressed optical signals 8a, 8b. A respective input signal xA(t) and xB(t) is supplied to each synthesizer 33. These input signals may be independent data streams or may be derived from a single data stream. A common narrow band laser 2 may be used for both synthesizers 33a,b, as shown in FIG. 8, although separate lasers may also be used if desired. In either case, both synthesizers 33a,b operate at the same CW signal wavelength.
[0042] The polarization interleaved communications signal 8′ is generated by combining the carrier-suppressed optical signals 8a, 8busing a polarization combiner 60. Respective polarization rotators 62a, 62b ensure orthogonal polarization states of the carrier-suppressed optical signals 8a, 8b. This ensures that the two carrier-suppressed optical signals 8a, 8b are fully orthogonal, and thus can be combined into the polarization-interleaved communications signal 8′ without interference. As may be appreciated, because the optical signals 8a, 8b generated by the synthesizers 33a, 33b are carrier suppressed, the polarization-interleaved communications signal 8′ will also be carrier suppressed.
[0043] If desired, each synthesizer 33a, 33b may be provided with a respective, independent controller 36 operating as described above with reference to FIGS. 4-6 . However, this solution also requires respective taps 12 and photo-detectors 16 for each synthesizer 33, which increases costs, signal noise, and sources of error. Accordingly, a single controller 82 is preferably used to control the bias point of both synthesizers 33a and 33b. This is a signal coupler 12 taps the polarization-interleaved communications signal 8′. The resulting tap signal 14 is supplied to a photo-detector 18, which generates a corresponding detection signal 18. Because the photodetector is substantially polarization insensitive, the optical power [ET(t)]2 detected by the photodetector 16 will be given by:
|ET(t)|2=|ETA(t)|+|ETB(t)|2 (Eq. 6)
Where [ETA(t)]2 and [ETB(t)]2 follow equation 2 above. Because ETA(t) and ETB(t) are orthogonal, each signal will be substantially free of interference components from the other signal. Accordingly, each signal will contain respective first harmonics dI(t) and dQ(t) and beat signal dI(t) dQ(t), as described above. The frequencies of each of these components are determined by the dither signals d1 and d2 added to the respective drive signals 34 of each synthesizer. As such, they can be readily isolated by the simple expedient of ensuring that all four of the dither signals (d1A, d2A, d1B and d2B) have unique frequencies. With this arrangement, each component (of both signals 8a and 8b) can be detected by a respective correlator 38. The processor can then use the correlator outputs to drive the respective bias signals b1-b3 for both synthesizers 33.
|ET(t)|2=|ETA(t)|+|ETB(t)|2 (Eq. 6)
Where [ETA(t)]2 and [ETB(t)]2 follow equation 2 above. Because ETA(t) and ETB(t) are orthogonal, each signal will be substantially free of interference components from the other signal. Accordingly, each signal will contain respective first harmonics dI(t) and dQ(t) and beat signal dI(t) dQ(t), as described above. The frequencies of each of these components are determined by the dither signals d1 and d2 added to the respective drive signals 34 of each synthesizer. As such, they can be readily isolated by the simple expedient of ensuring that all four of the dither signals (d1A, d2A, d1B and d2B) have unique frequencies. With this arrangement, each component (of both signals 8a and 8b) can be detected by a respective correlator 38. The processor can then use the correlator outputs to drive the respective bias signals b1-b3 for both synthesizers 33.
[0044] Thus it will be seen that the present invention provides methods and apparatus for synthesizing suppressed carrier optical communications signals. According to the invention, an optical modulator capable of complex modulation of an optical carrier signal is driven (biased) to a bias point near a zero-crossing point of the modulator's E-field response. A complete input signal is then used to drive excursions of the E-field response to impress the input signal onto the optical carrier. The resulting lightwave emerging from the complex modulator exhibits an optical spectrum characterised by a pair of sidebands and a strongly suppressed carrier. Bias control of the complex modulator is implemented on the basis of the optical power detected at the output of the complex modulator. This enables the optical modulator to be treated as a “black box”, in that calculation of the bias signals does not relay on knowledge of the precise performance characteristics of the modulator.
[0045] The embodiment(s) of the invention described above is (are) intended to be exemplary only. The scope of the invention is therefore intended to be limited solely by the scope of the appended claims.
Claims
We claim:
1. A method of synthesizing a suppressed carrier optical communications signal, the method comprising the steps of:
providing an optical modulator adapted for complex modulation of a continuous wave (CW) optical signal;
biasing the optical modulator to a bias point proximal a zero-crossing point of an E-field response of the modulator, wherein the bias point is offset from the zero-crossing point, a magnitude and direction of the offset being selected so as to at least partially cancel leakage of the CW optical signal through the optical modulator; and
driving excursions of the E-field response about the bias point using a complex input signal.
2. A method as claimed in claim 1, wherein the optical modulator comprises a nested Mach-Zehnder architecture capable of independently modulating phase and amplitude of the CW optical signal.
3. A method as claimed in claim 1, wherein the complex input signal comprises a pair of orthogonal signal components.
4. A method as claimed in claim 3, wherein the pair of orthogonal signal components comprise an In-phase signal component VI(t) and a Quadrature signal component VQ(t).
5. A method as claimed in claim 4, wherein the optical modulator comprises an outer Mach-Zehnder modulator having a pair of parallel branches, each branch including a respective branch Mach-Zehnder modulator, and wherein the step of driving excursions of the E-field response comprises a step of driving each of the branch Mach-Zehnder modulators using a respective one of the In-phase and Quadrature signal components.
6. A method as claimed in claim 5, wherein the step of biasing the optical modulator comprises steps of:
inserting a respective dither signal into each of the orthogonal signal components, each dither signal having a respective unique frequency;
detecting signal components of the suppressed carrier optical communications signal corresponding to the dither signals; and
adjusting the bias point of the optical modulator using the detected components.
7. A method as claimed in claim 6, wherein the step of detecting signal components of the suppressed carrier optical communications signal comprises a steps of:
detecting a first signal component [dI(t)]2 having a frequency corresponding to that of a first one of the dither signals;
detecting a first signal component [dQ(t)]2 having a frequency corresponding to that of a second one of the dither signals; and
detecting a beat-frequency component 2Sin(θq)dI(t)dQ(t) having a frequency corresponding to a beat frequency of the first and second dither signals.
8. A method as claimed in claim 7, wherein the step of adjusting the bias point of the optical modulator comprises steps of:
adjusting a phase angle between optical signals traversing the branches of the outer Mach-Zehnder modulator to minimize an optical power of the beat-frequency component;
adjusting respective values of the first and second dither signals to minimize an optical power of the corresponding first and second signal components [dI(t)]2 and [dQ(t)]2.
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