POLARIZATION MODE DISPERSION COMPENSATOR BASED ON DEGREE OF POLARIZATION

Abstract: The degree of polarization of an optical signal is measured by a polarimeter and used for providing a feedback signal to adjust adaptive optics of a polarization mode dispersion compensator. The polarization properties of the polarimeter are determined with high accuracy to match the polarimeter through calibration and used to produce the feedback signal.

Description: DESCRIPTION POLARIZATIONMODE DISPERSIONCOMPENSATORBASED ONDEGREE OF POLARIZATION Technical Field The present invention relates to a polarization mode dispersion compensator for analyzing signal distortiondue topolarizationmode dispersion inoptical transmission systems and therefore providing a feedback signal to adjust adaptive optics used for mitigating polarization mode dispersion. Background Art The higher the bit rate of an optical transmission system, the more a specific amount of polarization mode dispersion of an optical fiber distorts the transmitted signal . Due to polarization mode dispersion, the two modes in a so called single-mode fiberpropagate with different velocities. Αn initial pulse splits its energy into the two modes . The two modes experience a differential delay during propagation. This leads to pulse spreading at the end of the fiber. The more the differential delay between the two modes is in the order of the bit duration, the more neighboring pulses will overlap, which leads at least to an increasing bit-error rate or makes it even impossible to differentiate the pulses. Polarization mode dispersion is due to internal birefringence (e.g. fiber core geometry irregularities) or externally induced birefringence (e.g. bending, squeezing, etc.) . Because in a long single-mode fiber, polarization mode coupling occurs at randomly varying locations with randomly fluctuating strength due to e.g. environmental changes like temperature, polarization mode dispersion itself varies over time. It is well known, that the instantaneous differential group delay between theprincipal states ofpolarization follows aMaxwellian probability density function . The mean of the Maxwellian distributed instantaneous differential group delay is known as the average differential group delay, or the polarization mode dispersion value (PMD) of the fiber. The polarization mode dispersion value is, for long single-mode fibers with highpolarizationmode coupling, proportional to the square root of the fiber length. To mitigate signal distortion due to polarization mode dispersion, optical elements introducing a similar amount of differential group delay as in the fiber but with an opposite sign, can be placed at the end of the fiber. Due to the random nature of the instantaneous differential group delay and the principal states of polarization in a long optical fiber, the optical elements used for compensating polarization mode dispersion must be adaptively adjusted to the momentary fiber conditions. A closed loop design, polarization mode dispersion compensator consequently consists of: 1. adaptively adjustable optical elements (adaptive optics) 2. distortion analyzer 3. control logic as depicted in Fig. 1. In Fig. 1, the distortion analyzer 12 provides a measure of signal distortion for the control logic 13 to adaptively adjust the adaptive optics 11, such that they best match the momentary polarization mode dispersion conditions of the optical fiber. Beside methods like for example spectral hole burning (SHB) , direct eye-opening analyzing, etc., the degree of polarization (DOP) can be used for analyzing signal distortion ' due to polarization mode dispersion. For those who are skilled in the art, it is well known that a light beam experiences depolarization if the coherence length, which is inversely proportional to the spectral width, is in the order of the differential group delay. The higher the differential group delay becomes compared to the coherence length, the more the beam gets depolarized and its degree of polarization decreases. This well known physical effect is straightforward to be used as a feedback signal to adaptively control optical elements of a polarization mode dispersion compensator. Derivation of the depolarization of an optical signal due to fiber anisotropies as a functionof signal spectrum (bandwidth, form) , differential group delay and state of input polarization is shown in the following reference. "Degree of Polarization in Anisotropic Single-Mode Optical Fibers : Theory", Jun-ichi Sakai, SusumuMachida, Tatsuya Kimura, IEEE Journal of Quantum Electronics, Vol.QE-18, No.4, pp.488-495, 1982 Compared to spectral hole burning, measuring directly the eye-opening or bit-error rate detection, the advantages of using degree of polarization as a feedback signal for adaptive polarization mode dispersion compensation are: 1. independent of bit rate 2. applicable to anymodulation format without requiring modifications 3. insensitive to chromatic dispersion, such that degree of polarization provides a good measure of signal distortion due to only polarization mode dispersion Depicted in Fig. 2 are as a function of instantaneous differential group delay the degree of polarization and Q-penalty of a transmitted signal, non-return to zero (NRZ) format modulated with a bit rate of 48Gbit/s. The Q-penalty is defined here as: „ Λ , Eye - opening of received signal Q-penalty = 20 • log — . Back - to - back eye - opening (1) For reference, also shown in Fig. 2 is the power of the 24GHz (half the bit rate) spectral component as a function of instantaneous differential group delay. The spectral component at half the bit rate has been proved to show the strongest dependence on instantaneous differential group. Contrary to the degree of polarization which shows only one maximum if the instantaneous differential group delay vanishes, the 24GHz spectral component shows a periodic behaviour. Therefore, in cases where the instantaneous differential group delay is expected to exceed on bit duration, at least one more spectral component, namely the 12GHz (quarter of the bit rate) must be additionally tested to avoid an ambiguity. The details of degree of polarization and the power of spectral components at 24GHz (half the bit rate) , 12GHz (quarter of the bit rate) and 6GHz (eighth the bit rate) are depicted in Fig. 3 for small values of the instantaneous differential group delay. Of critical importance in the application of degree of polarization as a feedback signal in an adaptive polarization mode dispersion compensator, is the accuracy (particularly the variance of the measured degree of polarization with the input state of polarization) with which the degree of polarization can be measured. As canbe seen fromFig.2, if for example aQ-penalty of 0.5dB must not be exceeded, the dynamic range of the degree of polarization is ±5%. The uncertainty, with which the degree of polarization is measured, must therefore not exceed 5%. An adaptive control algorithm of a polarization mode dispersion compensator needs to sample the degree of polarization in the environment of the optimumpoint inorder to track the randomlyvarying differential group delay and principal states of polarization. Because of the required sampling by slightly mismatching the optical elements with respect to the polarization mode dispersion conditions in the optical fiber, the required accuracy with which the degree of polarization can be measured is much more stringent. A common approach for realizing the required accuracy is to mechanically align the optical components of a polarimeter in a distortion analyzer with high accuracy to predefined angles. However, this is a very tedious andtherefore cost intensive wayof construction. Disclosure of Invention It is an object of the present invention to provide a polarization mode dispersion compensator based on degree of polarization, which does not require a tedious and cost intensive way of construction. The polarization mode dispersion compensator according to the present invention comprises an optical unit, a distortion analyzer and a controller . The optical unit receives an input optical signal and outputs an output optical signal. The distortion analyzer includes a polarimeter, analyzes the output optical signal and produces a feedback signal, which represents degree of polarization of the output optical signal, by using a polarization property of the polarimeter. The polarizationproperty is determined through calibration using intensity signals output from the polarimeter. The controller produces a control signal to adjust the optical unit, based on the feedback signal. The optical unit corresponds to adaptive optics and includes one or more optical elements . the controller corresponds to control logic which controls the optical unit using the degree ofpolarization as a feedback signal . The polarization property of the polarimeter is determined in advance to match the actual polarimeter through calibration. The distortion analyzer analyzes the output optical signal from the optical unit, produces the feedback signal by using the obtained polarization property and outputs it to the controller. Because the polarization property is measured after the polarimeter is completely assembled, the requirements on mechanical alignment accuracy are drastically relaxed. Tedious, highly-accurate mechanical alignment is no longer necessary, which can lead to a drastic cost reduction. Brief Description of Drawings Fig. 1 shows a configuration of a conventional polarization mode dispersion compensator. Fig.2 shows degree of polarization, Q-penalty and a spectral component as a function of instantaneous differential group delay. Fig. 3 shows detail of degree of polarization, Q-penalty and a spectral component as a function of instantaneous differential group delay. Fig. 4 shows a configuration of a distortion analyzer. Fig. 5 shows a model of a division of amplitude type polarimeter. Fig. 6 shows representation of polarization properties of a division of amplitude type polarimeter in a Poincare sphere. Fig. 7 shows parameters of the elliptical retarders . Fig.8 shows a setup for calibration of a division of amplitude type polarimeter. Fig. 9 shows a parametric plot of two intensity signals. Fig. 10 shows a scaled parametric plot of two intensity signals. Fig. 11 shows a location of the first equivalent analyzer polarization on a Poincare sphere. Fig. 12 shows a circle indicating possible locations of the secondequivalent analyzerpolarization on a Poincare sphere. Fig. 13 shows a cross point of circles indicating a possible location of the third equivalent analyzer polarization on a Poincare sphere. Fig.14 shows an orthogonal type configuration of a division of amplitude type polarimeter. Fig. 15 shows equivalent analyzer polarizations of an orthogonal type configuration on a Poincare sphere . Fig.16 shows dependence of DOP accuracy on noise and angular uncertainty for an orthogonal type configuration . Fig. 17 shows a variant configuration of an orthogonal type polarimeter. Fig. 18 shows a tetragonal type configuration of a division of amplitude type polarimeter. Fig. 19 shows equivalent analyzer polarizations of a tetragonal type configuration on a Poincare sphere. Fig.20 shows dependence of DOP accuracy on noise and angular uncertainty for a tetragonal type configuration . Fig. 21 shows a variant configuration of a tetragonal type polarimeter. Fig. 22 shows a diamond type configuration of a division of amplitude type polarimeter. Fig. 23 shows equivalent analyzer polarizations of a diamond type configuration on a Poincare sphere. Fig.24 shows dependence of DOP accuracy on noise andangularuncertainty for a diamondtype configuration. Fig.25 shows a variant configuration of a diamond type polarimeter. Fig. 26 shows another variant configuration of a diamond type polarimeter. Fig.27 shows a variant configuration of a division of amplitude type polarimeter for autonomous calibration. Fig. 28 shows another variant configuration of a division of amplitude type polarimeter for autonomous calibration. Fig. 29 shows a polarization mode dispersion compensator using degree of polarization and a state of polarization as feedback signals. Fig. 30 shows a polarization mode dispersion compensator using degree of polarization and/or a state of polarization and a bit-error rate as feedback signals . Best Mode for Carrying Out the Invention Hereinafter, preferred embodiments according to the present invention will be described in detail by referring to the drawings. As a physical property of light, the degree of polarization is used for providing a feedback signal to adjust adaptive optics of a polarization mode dispersion compensator. To measure the degree of polarization, an incident beam of light is split into four or more beams, each of which passes through individually arranged retardation and polarizing optics. This type of polarization measurement system can be called a division of amplitude type polarimeter. From the intensities of those beams, the state of polarization and the degree of polarization can be calculated if, and only if, the polarization properties of the paths each beam travels are known. The accuracy with which the state of polarization and degree of polarization can be measured by such an instrument, depends strongly on the accuracy with which the polarization properties of each path, particularly e. g. polarizer angle, retardance of a path, etc. are known. In the following, an advantageous solution for measuring the polarization properties with high accuracy of each of the split beams is described. Fig. 4 shows an example of the configuration of a distortion analyzer which measures the degree of polarization and/or the state of polarization. The polarimeter 21 splits a light beam into several beams and outputs intensity signals of those beams. The intensity signals are amplified by the amplifier 22 and converted into digital signals by the analog-to-digital (A/D) converter 23. The central processing unit (CPU) 24 calculates the degree ofpolarization and/or the state of polarization using the values of the digital signals and outputs the obtained result as a feedback signal. In the following, variousmethods willbe described to applying degree of polarization as a feedback signal to adaptive polarization mode dispersion compensators. The describedmethods include advantageous construction of polarimeters with respect to degree of polarization measurement accuracy. To relax the stringent requirements onhowexact optical components are aligned, or their orientation is at least known, calibration methods will be described including adapted variations of polarimeter constructions. As mentioned above, a division of amplitude type polarimeter refers to a polarimeter in which an incoming light beam is split into several beams. Each beam is then individually guided through optical components like polarizer (analyzer) and retarder. From the measured intensities, the state ofpolarizationcanbe calculated. A division of amplitude type polarimeter can be modeled as depicted in Fig. 5. An incoming light beam S is split into fourbeams (more than fourbeams possible, four beams selected for description for clarity reasons) by beam splitter 31. Each of the split beams propagates through a combination of retarder 32 and polarizer 33 and their respective intensities I 0 , Ii, I 2 and I 3 , are detected by photodiodes 34. The retarder/polarizer combination represents an elliptical polarizer, characterized by an azimut θ, an ellipticity ε and an extinction ratio ER. The extinction ratio is the relation between the minimum, x m i n , and maximum, τ max , transmitted intensity for all possible input states of polarization . The polarization properties each beam experiences while propagating from the input through the beam splitter 31 until it reaches the polarizer 33, are incorporated in this model by the respective retarder/polarizer combination. The relation between the detected intensities I 0 , Iχ, I 2 and I 3 , and the polarization of light at the input of the beam splitter 31 (Stokes vector S) can be given as : 2ε 0 τ d0 sin 2ε 0 2z x τ dl sin 2ε, τ "d,,2 s k3 i J -n α - t 2ε°,2 2ε,. τ "„d.3 sin 2ε 3 The angles θ 0 , θi, θ 2 , 63, and ε 0 , εi, ε 2 , ε 3 describe the elliptical retarder properties of each retarder/polarizer combination. The coefficients x a0 , tai t a2 and τ a 3, and t d o, idi r τ d2 and x d 3 are related to the minimum, τ m i n , and maximum, τ max , transmitted intensity (transmission coefficient) for all possible input states of polarization by: Ε a — ( max "r min) ) ^d — (^max — min ) / -- • { I Each row of the instrument matrix Z can be thought of in the same way as a Stokes vector, describing a state of polarization with azimut θ and ellipticity ε. Consequently, the retarder/polarizer combination each beampasses, canbe representedby a point on the Poincare sphere as depicted in Fig. 6. The representation in the Poincare sphere of the polarization properties each beam experiences, can be called equivalent analyzer polarization. The depicted example of equivalent analyzer polarizations AO, Al, A2 and A3 shows the situation for a division of amplitude type polarimeter, whereas the parameters of the elliptical retarders (equivalent analyzers) are as shown in Fig. 7. In the case the equivalent analyzer polarizations and respective extinction ratios are known, the division of amplitude polarimeter is fully characterized with respect to its polarization properties. The instrument matrix Z can be calculated and the Stokes vector S at the input of the polarimeter can be calculated from the detected intensities I 0 , Ii, I 2 and I 3 at the photodiodes 34. A conventional procedure is to first select values for the equivalent analyzer polarizations and then assembling the optical components such that their mechanical alignment match the preselected instrument matrix. Depending on required accuracy, the alignment must be very precise. This leads to a tedious and cost intensive assembling. A different approach, outlined in the following, provides a procedure to measure the equivalent analyzer polarizations and respective extinction ratios withhigh accuracy. The optical components can therefore be assembled with relaxed requirements on alignment precision. This leads to an improved performance while at the same time providing a way of cost reduction for assembling. Fig. 8 shows a setup for autonomous calibration of a division of amplitude type polarimeter. The calibration procedure starts by measuring an assemble of intensity vectors lo, Ii, I 2 and I 3 for different states of input polarization. The different states of input polarization are provided by narrow-bandwidth laser 41 launching fully polarized light (DOP = 100%) into polarization converter 42 with negligible or at least very low variation of its insertion loss. The free-running or by means of external signals controlled polarization converter 42 launches states of polarization into the, to be calibrated, division of amplitude polarimeter 43 such that the Poincare sphere is fully covered. In the case the input polarization is modulated in this way, a parametric plot of any two out of the four intensity signals leads always to points in a plane surrounded by an ellipse as depicted in Fig.9. The left, right, lower and upper bounds of the ellipse equal the minimum, m± and maximum, x m ax / transmission coefficients of the respective analyzers. After scaling the intensity signals such that the ellipse fits into a square with length of the sides of 1 (multiplication of the intensity signals with factors aandb) as depicted in Fig.10, the ellipticityε equals, in Poincare sphere representation, half of the angular spacing oi between the two equivalent analyzer polarizations for which the parametric plot was drawn. In the following reference, construction of an all-fiber optical in-line and off-line polarization analyzer is shown and application of a setup in which a device under test is placed between in-line and off-line polarimeter to characterize its polarization transfer function is described. Measurable parameters are polarization dependent loss, retardation, differential group delay and depolarization. Further included applications are fiber-optical polarimetric sensors, particularly temperature sensors. Especially, mathematics related to properties of intensity vectors of a division of amplitude type polarimeter is described on pages 46 through 51. "Selbstkalibrierender faseroptischer Polarisationsanalysator", Jens C. Rasmussen, Ph.D thesis, R TH Aachen (Germany) , Shaker Verlag, ISBN 3-8265-4450-1, 1998 After the relative angular distances ε 0 ι, ε 0 2/ So3 εi 2 and ε i between the equivalent analyzer polarizations are known, the absolute positions are derived as follows . The measurement of the degree of polarization is invariant to a rotation of the reference frame (rotation of the Poincare sphere in both possible directions) for which the state of polarization is measured. Even for the measurement of the state of polarization itself, a rotation of the reference frame always happens during light propagates through an optical fiber due to internal and externally introduced birefringence. The absolute orientation of the reference frame (angular orientation of the Poincare sphere) is therefore not important in cases, like here, polarization of light is measured, which has passed through an optical fiber. The first equivalent analyzer polarization AO can therefore be located at an arbitrary position on the Poincare sphere as depicted in Fig.11. It is fixed here to (azi ut, ellipticity) = (0, 0) . The second equivalent analyzer polarization Al is located with an angular distance εoi from the first equivalent analyzer polarization A0 on the Poincare sphere. Possible locations describe therefore a circle around the first equivalent analyzer polarization A0. Due to the previously described rotational invariance, the cross point of the circle of possible locations and the equator of the Poincare sphere is selected as depicted in Fig. 12. The third equivalent analyzer polarization A2 is located with an angular distance ε 02 from the first equivalent analyzer polarizationA0, andwith an angular distance βι 2 from the second equivalent analyzer polarization Al, on the Poincare sphere. Possible locations are therefore the two cross points of the circles around the first and second equivalent analyzer polarizations AO and Al . From those two possible locations of the third equivalent analyzer polarization A2 one can be selected as depicted in Fig. 13. The fourth equivalent analyzer polarization A3 is located with an angular distance εo3 from the first equivalent analyzer polarization AO, with an angular distance ει from the second equivalent analyzer polarization Al, and with an angular distance ε 2 3 from the third equivalent analyzer polarization A2 on the Poincare sphere. Possible locations are therefore the two cross points of the circles around the first, second and third equivalent analyzer polarizations AO, Al and A2. From those possible locations of the fourth equivalent analyzer polarizationA3 one can be selected. In the following, the mathematics used to derive the calibration procedure is shown. Each analyzer of a division of amplitude type polarimeter canbe described with respect to a common, arbitrary reference plane by an elliptical polarizer. The intensity I n (n=0,l,2,3) which can be detected by the n-th analyzer is: I n = τ an +x dn (cos2θ n cos2ε n Sι+sin2θ n cos2εnS2+sin2εnS 3 ) . (5) The polarization in the reference plane is described by the Stokes parameters SO, SI, S2 and S3. The equivalent analyzerpolarization of the n-th analyzer is characterized by an azimut θ n and an ellipticity ε n . The factors x an and x dn can be calculated from the transmission coefficients x maX n = Imaxn and x minn = Iminr,: 'Can (Tmaxn "■" Xminn) / <-• (6) T-dn IX axn — Xminn/ / -- (7) Looking at three analyzers which detect the intensities lo, Iιandl , leads to the following equation: ϊ' = Z' • S' , ( 8 ) τ M cos 2Θ 0 cos 2ε 0 τ d0 sin 2Θ 0 cos 2ε 0 τ d0 sin Z' = τ d] cos 2θ j cos 2ε, τ dl sin 2Θ, cos 2ε, τ d] sin τ d3 cos 2Θ, cos 2ε τ rt , sin 2θ τ cos 2ε, τ ri , sin Assuming a constant degree of polarization p = (Sι 2 +S 2 2 +S 3 2 ) 1/2 , each state of polarization described by the vector S' = (Si, S 2 , S 3 ) τ satisfies: S' τ • E ■ S' = p 2 , (9) E: unit matrix. This equation describes a sphere in the variables of the vector components of S' with a radius p. Combining equations (8) and (9) leads to: p 2 = S' τ S' ( 10 ) = (z'- ϊ') τ E • Z I' ( 11 ) 1 (Z' τ • ϊ') τ • E Z' τ • ϊ' ( 12 ) det (Z') det (Z') => ϊ' τ • Z' • E • Z' τ • ϊ' = p 2 (det (Z') ) ( 13 ) The resultant equation describes a second order plane in the variables of the components of the vector in three dimensions . Afurther classification ispossible . All eigenvalues of the symmetric matrix Z' -E- Z' τ are real and positive. The term p 2 (det (Z' )) 2 is also always positive. The equation (13) describes therefore an ellipsoid, under the assumption of regularity of the matrix Z' and all its column vectors are linear independent. The physical meaning is, that all analyzers are polarizer (x dn > 0) and the equivalent analyzer polarization are not pairwise identical. Normalizing the components of the intensity vector ϊ' , the vectors ( 14 ) describe an ellipsoid, which is inscribed into a cube with the length of all sides equal to one. The possible values for each component of the intensity vector ϊ" is now limited to -0.5 < I n " < 0.5. The first analyzer detects a maximum intensity I 0 " = 0.5 if the polarization in the reference plane equals the equivalent analyzer polarization. For the first analyzer, the detected intensity I 0 ": S x = cos 2Θ, cos 2ε 1 lo 0.5 therefore maximum for 5 2 = cos 2Θ, cos 2ε, 5 3 = sin 2ε, (15) The second analyzer detects at the same polarization at which the first analyzer detect the maximum intensity, an intensity Ii" with: 2Iι"(I 0 " = 0.5) = cos2θ 0 cos2ε 0 cos2θιcos2ει +sin2θ 0 cos2ε 0 sin2θιcos2ει +sin2εosin2ει. (16) The right side of equation (16) is equal to the cosine of the angle ^ Ana oP Ana i between the equivalent analyzer polarizations of the first P Ana0 and second P Ana] analyzer, because co U st. " (17) The orthogonal projection of the ellipsoid composed of the vectors ϊ" on the coordinate plane Io"j Ii" leads to a plane with an elliptical shape. For the length of the main axis a and b and the ellipticity ε of the elliptically shaped plane and for the value Ii"(Io"max)/ the following relations apply: tanε = -, (18) a cosδ = 2 i^' do"^) , ( is; a 2 + b 2 Lemma of Apollonius . ( 20] ± ab sin δ From this, the relation of the angle between the equivalent analyzer polarizations P Ana0 , P Anal and the ellipticity ε can be derived. From equations (18) -(20): 2ab = ±sinδ + b z _ 2 tan ε 1 + tan 2 ε = sin2ε => δ = ±2ε. (21) With equations (16), (17) and (19) the relation of the angle ZP Anan P Anam between two equivalent analyzer polarizations P Anan , P Anam and the ellipticity ε nm calculates to: cos (ZP Anan P Ana = 2I" m ( I n " max ) = cosδ nm = cos2ε nm (22 ) = ^ Ana A nam = 2 Snm . ( 23 ) This applies to each possible pair of analyzers Next, with respect to the principle measurement accuracy of the degree of polarization, three configurations and possible variations of a division of amplitude type polarimeter are discussed. Those configurations are named "Orthogonal", "Tetragonal" and "Diamond". They differ in the number and arrangement of utilized optical components. The "Orthogonal" scheme is used in the following reference. "A study for wavelength dependency of Polarization Analysis Module", T. Miyakoshi, S. Shikii, Y. Hotta, S. Boku, Institute of Electronics, Information and Communication Engineers, sougou taikai B-10-95, p.528, 2001 In this .reference, a division of amplitude type polarimeter, composed of three beam-splitters, four polarizers, one quarter-wave retarder, four photodiodes and data acquisition electronics are described. "Tetragonal" is a compromise between complexity and realizable accuracy. "Diamond" is with respect to DOP accuracy and sensitivity to noise an ideal configurationbut requires themost complex arrangement . To compare the principal performance of a specific arrangement, the condition number of the 4x4 instrument matrix, describing the relationbetweenmeasuredoptical intensities and the Stokes vector, can be used. The condition numbers (calculated according to Hadamard) of the schemes "Orthogonal", "Tetragonal" and "Diamond" are 2.0, 1.5 and 1.3, respectively. In order to numerically investigate the dependence of the principal DOP accuracy on angular misalignment of optical components, the difference between real and supposed polarizer angles has been varied through the values 0°, 0.1°, 0.5°, 1° up to 2°. Those values where alternatively added to and subtracted from the four polarizer angles, which can be supposed to be approximately the worst case. To take further into account noise, the quantification noise due to A/D conversion of the photodiode currents is supposed to be the main source. The resolution of A/D conversion has been varied through the values 8, 10, 12, 14 up to 16bit. The offsets due to photodiode dark currents and amplifiers are supposed to be zero. Signals are supposed to fully cover the dynamic range of the A/D conversion. Extinction ratios of the polarizers are supposed to be arbitrary high. Incorporated retardations are supposed to be fixed. An "Orthogonal" type configuration of a division of amplitude type polarimeter is depicted in Fig. 14. Abasic configuration of this polarimeter includes three beam splitters 51, 52 and 53, four polarizers 54, 55, 56 and 57, and one retarder 58 with retardation of a quarter of a wavelength. Angles of the polarizers 54 and 57 are 0° and angles of the polarizers 55 and 56 are 45° and -45°, respectively. As shown in Fig. 15, the components are arranged suchthat the equivalent analyzer polarizations (AO, Al, A2, A3) are mutually orthogonal on a Poincare sphere. The dependence of the principal DOP accuracy [%] on noise (A/D resolution [bit] ) and angular uncertainty [°] is shown for exemplified values in Fig. 16. A variant configuration of the "Orthogonal" type polarimeter is depicted in Fig. 17. This polarimeter includes three beam splitters 61, 62 and 63, four polarizers 64, 65, 66 and 67, and one retarder 68 with retardation of a quarter of a wavelength. Angles of the polarizers 64 and 65 are 0° and angles of the polarizers 66 and 67 are 45° and -45°, respectively. A "Tetragonal" type configuration of a division of amplitude type polarimeter is depicted in Fig. 18. Abasic configuration of this polarimeter includes three beam splitters 71, 72 and 73, four polarizers 74, 75, 76 and 77, and one retarder 78 with retardation of a quarter of a wavelength. Angles of the polarizers 74 and 77 are 0° and angles of the polarizers 75 and 76 are 60° and -60°, respectively. As shown in Fig. 19, the components are arrangedsuch that the equivalent analyzer polarizations (A0, Al, A2, A3) are angular spaced by 120° on a Poincare sphere. A3 is orthogonal to all other equivalent analyzer polarizations. The dependence of the principal DOP accuracy on noise and angular uncertainty is shown for exemplified values in Fig.20. A variant configuration of the "Tetragonal" type polarimeter is depicted in Fig. 21. This polarimeter includes three beam splitters 81, 82 and 83, four polarizers 84, 85, 86 and 87, and one retarder 88 with retardation of a quarter of a wavelength. Angles of the polarizers 84 and 85 are 0° and angles of the polarizers 86 and 87 are 60° and -60°, respectively. A "Diamond" type configuration of a division of amplitude type polarimeter is depicted in Fig. 22. A basic configuration of this polarimeter includes three beam splitters 91, 92 and 93, four polarizers 94, 95, 96 and 97, and four retarders 98, 99, 100 and 101. Angles of the polarizers 94 and 97 are 0° and angles of the polarizers 95 and 96 are 60° and -60°, respectively. Retardation of the retarders 98, 99 and 100 is 1/18.48 of a wavelength and that of the retarder 101 is a quarter of a wavelength. As shown in Fig. 23, the components are arranged such that the equivalent analyzer polarizations (AO, Al, A2, A3) form a structure like atoms in a diamond on a Poincare sphere. The dependence of the principal DOP accuracy on noise and angular uncertainty is shown for exemplified values in Fig.24. A variant configuration of the "Diamond" type polarimeter is depicted in Fig. 25. This polarimeter includes three beam splitters 111, 112 and 113, four polarizers 114, 115, 116 and 117, and four retarders 118, 119, 120 and 121. Angles of the polarizers 114 and 115 are 0° and angles of the polarizers 116 and 117 are 60° and -60°, respectively. Retardation of the retarder 118 is a quarter of a wavelength and that of the retarders 119, 120 and 121 is 1/18.48 of a wavelength. Fig.26 shows another variant configuration of the "Diamond" type polarimeter. This polarimeter includes three beam splitters 131, 132 and 133, four polarizers 134, 135, 136 and 137, and two retarders 138 and 139. Angles of the polarizers 134 and 135 are 0° and angles of thepolarizers 136 andl37 are 60° and-60°, respectively. Retardation of the retarder 138 is 1/18.48 subtracted from a quarter of a wavelength and that of the retarder 139 is 1/18.48 of a wavelength. In the above described configurations, the angles of the polarizers and the retardation of the retarders are not limited to the respective theoretical values themselves but can be within a given tolerance range (±5% for example) of the values. The autonomous calibration procedure requires besides a constant degree of polarization of the light source, which is easy to realize, a constant input power . This can be realized by either using polarization converters for polarization modulation with low dependence of the insertion loss on polarization like crystal based or fiber based devices. In the case a polarization converter with untolerable high dependence of insertion loss on polarization is used, like multi stages of variable birefringent plates or integrated optical realizations, the power of the light wave must be measured simultaneous with the intensities of the polarimeter to be calibrated. Simultaneous power measurement can be either realized by a 1x2 coupler, whereas one arm is used for power monitoring and the other for the polarimeter to be calibrated. Analternative is to realize adivisionof amplitude type polarimeter where only three polarizers are used and one of the four light beams is used for the power monitoring as depicted in Fig. 27. The configuration shown in Fig. 27 is obtained by removing the polarizer 67 from the configuration shown in Fig. 17. Another realizationpossibility is depicted in Fig. 28, in which the light beam is split into five beams. The configuration shown in Fig. 28 is obtained by inserting an additional beam splitter 140 into the configuration shown in Fig.26. While four of the beams are transmitted through optics as described above, the fifth beam from the beam splitter 140 is used for power monitoring. In the application of a division of amplitude type polarimeter for an adaptive polarizationmode dispersion compensator as a distortionmonitor, one of the described variants can be used, whereas the required accuracy for the degree of polarization measurement is provided after the described calibration procedure (measurement of the instrument matrix Z) has been applied. The basic algorithm for adjusting the adaptive optics of a polarization mode dispersion compensator, is provided bymeans of a gradient search algorithm assuring amaximum degree of polarization. In order to improve the speed with which the adaptive optics of a polarization mode dispersion compensator canbe controlledand/or to avoidambiguities of the correlation between degree of polarization and signal distortion due to polarization mode dispersion, in the following other variants are described. While it is possible to adaptively control a polarization mode dispersion compensator by tracking the maximum degree of polarization, the principal realizable tracking speed could be improved by including the measured state of polarization. In general, the measured state of polarization is very sensitive to variations of the polarization transfer function of an optical fiber, while the degree of polarization shows only moderate sensitivity which can be covered by the limited measurement accuracy even if it is in the order of 1% or better. Monitoring beside the degree of polarization also the state of polarization as depicted in Fig. 29 leads to the possibility of a more sophisticated algorithm. The polarization mode dispersion compensator shown in Fig.29 includes adaptive optics 141, distortion analyzer 142 and control logic 143. The distortion analyzer 142 provides beside the degree of polarization as a measure of signal distortion also the state of polarization to the control logic 143 as feedback signals. The control logic 143 receives the feedback signals and produces a control signal for the adaptive optics 141 based on the received signals. As long as the state of polarization shows only small variations, the polarization mode dispersion properties of the optical transmission system also only vary slightly and readjustment of the adaptive optics 141 is not required during this time. This idle time can be advantageously used to perform other operations like readjusting or rewinding components of a polarization converter to their main operating point. In the case the state of polarization changes, the polarization mode dispersion properties of the optical transmission system have changed and readjustment of the adaptive optics 141 is necessary. The angular change and speedwithwhich the state ofpolarizationhas changed, can be used as a measure of how strong the conditions of the adaptive optics 141 must be readjusted. To avoid ambiguities, i.e. cases in which amaximum degree of polarization does not correspond to minimum signal distortion, a combination of degree of polarization as a fast feedback signal, and a bit-error rate as provided by e.g. forward-error-correcting electronics as an ultimate measure of signal distortion can be used as depicted in Fig. 30. The polarization mode dispersion compensator shown in Fig.30 has a similar configuration to that shown in Fig. 29. The distortion analyzer 142 provides the control logic 143 with only the degree of polarization or the combination of the degree of polarization and the state of polarization. Receiver 144 includes forward-error-correcting electronics and outputs a bit-error rate as a feedback signal. The control logic 143 receives the feedback signals from the distortion analyzer 142 and the receiver 144 and produces a control signal for the adaptive optics 141 based on the received signals. While fast changes of the polarization mode dispersion properties of an optical transmission system require a fast feedback signal as provided by the measurement of the degree of polarization, for fine tuning purposes the bit-error rate as provided by the forward-error-correcting electronics at the receiver 144 is used. As described in detail above, according to the present invention, the requirements on mechanical alignment accuracy for a polarimeter are drastically relaxed since the polarization properties are measured after the polarimeter is assembled. Therefore, tedious and cost intensive mechanical alignment is not required.

Claims: CLAIMS 1. A polarization mode dispersion compensator comprising: an optical unit receiving an input optical signal and outputting an output optical signal; a distortion analyzerwhich includes apolarimeter, analyzing the output optical signal and producing a feedback signal, which represents degree ofpolarization of the output optical signal, by using a polarization property of the polarimeter, the polarization property determined through calibration using a plurality of intensity signals output from the polarimeter; and a controller producing a control signal to adjust said optical unit, based on the feedback signal. 2. A polarization mode dispersion compensator according to claim 1, wherein: said polarimeter includes a plurality of optical components to produce the intensity signals; said distortion analyzer produces the feedback signal by using information of an instrument matrix of the polarimeter as the polarization property; and the information of the instrument matrix is obtained by inputting light with different states of polarization into the polarimeter such that a Poincare sphere is fully covered and measuring the intensity signals output from the polarimeter. 3. A polarization mode dispersion compensator according to claim 2, wherein the information of the instrument matrix is obtained by plotting two of the intensity signals on a plane for the different states of polarization and determining an azimut and an ellipticity of an ellipse which surrounds plotted points. 4. A polarization mode dispersion compensator according to claim 3, wherein maximumandminimumintensityof theplottedpoints are further determined for each of the two of the intensity signals and used, together with the azimut and ellipticity, as the informationof the instrumentmatrix. 5. A polarization mode dispersion compensator according to claim 1, wherein: said polarimeter includes a plurality of optical components forming four analyzers to produce four intensity signals; and the optical components are arranged such that equivalent analyzer polarizations of three of the four analyzers are angular spaced by 120 degrees on a Poincare sphere andan equivalent analyzerpolarizationof another of the four analyzers is orthogonal to the equivalent analyzer polarizations of the three analyzers on the Poincare sphere. 6. A polarization mode dispersion compensator according to claim 1, wherein: said polarimeter includes a plurality of optical components forming four analyzers to produce four intensity signals; and the optical components are arranged such that equivalent analyzer polarizations of the four analyzers form a structure like atoms in a diamond on a Poincare sphere . 7. A polarization mode dispersion compensator according to claim 1, wherein: said distortion analyzer produces a feedback signal which represents a state of polarization of the output optical signal; and said controller produces the control signal based on both the feedback signal representing the degree of polarization and the feedback signal representing the state of polarization. 8. A polarization mode dispersion compensator according to claim 1, wherein said controller receives a feedback signal which represents a bit-error rate of the output optical signal andproduces the control signal basedonboth the feedback signal representing the degree of polarization and the feedback signal representing the bit-error rate. 9. A polarization mode dispersion compensator according to claim 1, wherein: said distortion analyzer produces a feedback signal which represents a state of polarization of the output optical signal; and said controller receives a feedback signal which represents a bit-error rate of the output optical signal and produces the control signal based on the feedback signal representing the degree of polarization, the feedback signal representing the state of polarization and the feedback signal representing the bit-error rate . 10. A distortion analyzer comprising: apolarimeterwhich includes apluralityof optical components to produce a plurality of intensity signals from an input optical signal; and a processor producing a feedback signal, which represents degree of polarization of the input optical signal, for polarization mode dispersion compensation from the intensity signals by using a polarization property of the polarimeter, the polarization property determined through calibration using intensity signals output from the polarimeter. 11. A polarimeter comprising: three beam splitters; two polarizers within a given tolerance range of zero degrees; a polarizer within a given tolerance range of 60 degrees; a polarizer within a given tolerance range of -60 degrees; and a retarder within a given tolerance range of a quarter of a wavelength, wherein the beam splitters, the polarizers and the retarder form four analyzers to produce four intensity signals, and are arranged such that equivalent analyzer polarizations of three of the four analyzers are angular spaced by 120 degrees on a Poincare sphere and an equivalent analyzer polarization of another of the four analyzers is orthogonal to the equivalent analyzer polarizations of the three analyzers on the Poincare sphere. 12. A polarimeter comprising: three beam splitters; two polarizers within a given tolerance range of zero degrees; a polarizer within a given tolerance range of 60 degrees; a polarizer within a given tolerance range of -60 degrees; a retarder within a given tolerance range of a quarter of a wavelength; and three retarders within a given tolerance range of 1/18.48 of a wavelength, wherein the beam splitters, the polarizers and the retarders form four analyzers to produce four intensity signals, and are arranged such that equivalent analyzer polarizations of the four analyzers form a structure like atoms in a diamond on a Poincare sphere. 13. A polarimeter comprising: three beam splitters; two polarizers within a given tolerance range of zero degrees; a polarizer within a given tolerance range of 60 degrees; a polarizer within a given tolerance range of -60 degrees; a retarderwithin a giventolerance range of 1/18. 8 subtracted from a quarter of a wavelength; and a retarderwithin a giventolerance range of 1/18.48 of a wavelength, wherein the beam splitters, the polarizers and the retarders form four analyzers to produce four intensity signals, and are arranged such that equivalent analyzer polarizations of the four analyzers form a structure like atoms in a diamond on a Poincare sphere. 14. A method of polarization mode dispersion compensation, comprising: determining a polarization property of a polarimeter through calibration using a plurality of intensity signals output from a polarimeter; producing an output optical signal through an optical unit from an input optical signal; analyzing the output optical signal and producing a feedback signal, which represents degree of polarization of the output optical signal, by using the polarization property of the polarimeter; and adjusting said optical unit according to the feedback signal .

Inventors: ISHIKAWA GEORGE, OOI HIROKI, RASMUSSEN JENS C, TERAHARA TAKAFUMI, ISHIKAWA, GEORGE, OOI, HIROKI, RASMUSSEN, JENS, C., TERAHARA, TAKAFUMI
Applicants: FUJITSU LTD, ISHIKAWA GEORGE, OOI HIROKI, RASMUSSEN JENS C, TERAHARA TAKAFUMI, FUJITSU LIMITED, ISHIKAWA, GEORGE, OOI, HIROKI, RASMUSSEN, JENS, C., TERAHARA, TAKAFUMI
Application year: 2001
Main classification: H04B10
IPC codes: G01J4, G02F1, H04B10