Feedforward decision-free pilot-aided phase noise estimation for coherent optical M-QAM systems
An apparatus includes an electronic digital signal processor having electrical inputs for receiving a first sequence of measurements of values of a transmitted modulated optical carrier received in a coherent optical receiver and having electrical outputs for a stream of determined transmitted data values demodulated therein from the first sequence. The electronic digital signal processor has first circuitry to determine phase offsets of received pilot values from the first sequence. Additionally, the electronic digital signal processor has second circuitry to correct phase offsets of received ones of the data values from the determined phases of pilot values and data values being temporally interleaved in the transmitted modulated optical carrier. A system and a method are also included.
1. An apparatus comprising:
an electronic digital signal processor having electrical inputs for receiving a first sequence of measurement values of a transmitted modulated optical carrier received in a coherent optical receiver and having electrical outputs for a stream of determined transmitted data symbol values demodulated therein from the first sequence, and
wherein the electronic digital signal processor has first circuitry to determine phase offsets of received pilot symbol values from the first sequence;
wherein the electronic digital signal processor calculates pilot transform coefficients utilizing received pilot symbol phase angles; and
wherein the electronic digital signal processor has second circuitry to correct phase offsets of received ones of the data symbol values from the determined phase offsets of the received pilot symbol values, utilizing the pilot transform coefficients, and wherein the pilot symbol values are temporally inserted between groups of the data symbol values in the transmitted modulated optical carrier.
2. The apparatus of claim 1 , wherein the electronic digital signal processor includes a memory to store information indicative of a transmitted sequence of the received pilot symbol values.
3. The apparatus of claim 2 , wherein the electronic digital signal processor is configured to estimate phase offsets of some of the data symbol values by interpolating between the determined phase offsets of the received pilot symbol values.
4. The apparatus of claim 3 , further comprising the optical coherent receiver having an optical local oscillator therein and having one or more optical hybrids connected to interfere light of the transmitted modulated optical carrier received with light of the optical local oscillator.
5. The apparatus of claim 4 , wherein the electronic digital signal processor has third circuitry configured to estimate a frequency offset between the local optical oscillator and an optical carrier frequency of the transmitted modulated optical carrier received by measuring a temporal rotation of a constellation of the data symbol values from the first sequence of measurement values.
6. The apparatus of claim 1 , wherein the electronic digital signal processor is configured to estimate phase offsets of some of the data symbol values by interpolating between the determined phase offsets of the received pilot symbol values.
7. The apparatus of claim 1 , further comprising the optical coherent receiver having an optical local oscillator therein and having one or more optical hybrids connected to interfere light of the transmitted modulated optical carrier received with light of the optical local oscillator.
8. The apparatus of claim 7 , wherein the electronic digital signal processor has third circuitry configured to estimate a frequency offset between the local optical oscillator and an optical carrier frequency of the transmitted modulated optical carrier received by measuring a temporal rotation of a constellation of the data symbol values from the first sequence of measurement values.
9. The apparatus of claim 7 , wherein the electronic digital signal processor is configured to demodulate a stream of data symbol values transmitted in a quadrature amplitude modulation constellation.
10. The apparatus of claim 9 , wherein the quadrature amplitude modulation constellation has more than 16 symbol values.
11. The apparatus of claim 9 , wherein the quadrature amplitude modulation constellation has more than 64 symbol values.
12. The apparatus of claim 1 , wherein the electronic digital signal processor is configured to demodulate a stream of data symbol values transmitted in a quadrature amplitude modulation constellation.
13. The apparatus of claim 1 , wherein the pilot transform coefficients are pilot discrete cosine transform coefficients and are determined based on the pilot symbol phase angles.
14. A method, comprising:
in a coherent optical receiver, receiving optical transmission frames having pilot symbols and data symbols arranged in a pattern;
comparing the pilot symbols received with one or more reference pilot symbols to determine received pilot symbol phase angles;
calculating discrete transform coefficients based on the received pilot symbol phase angles; and
estimating a reception phase noise of each optical transmission frame based on the discrete transform coefficients.
15. The method as recited in claim 14 further comprising determining a mean value for the reception phase noise of the optical transmission frames to provide initial phase noise angles for de-rotation of the received data symbols.
16. The method as recited in claim 14 further comprising processing initial phase noise angles iteratively to improve an accuracy of the initial phase noise angles for de-rotation of received data symbols.
17. The method as recited in claim 14 wherein each optical transmission frame contains a total of N symbols with P pilot symbols periodically inserted within the data symbols such that N is an odd number integer multiple of P.
18. The method as recited in claim 14 , wherein the calculating discrete transform coefficients is additionally based on received pilot symbol discrete cosine transform basis functions.
19. A system, comprising:
a digital signal processor (DSP), of a coherent optical receiver, wherein the DSP comprises:
a frame comparator circuit to compare received pilot symbols of an optical transmission frame with a reference pilot symbol to determine pilot phase angles between the received pilot symbols and reference pilot symbols;
a pilot processor circuit that generates pilot transform coefficients based on the pilot phase angles; and
a frame processor circuit to determine a received phase noise value for the optical transmission frame based on the pilot transform coefficients.
20. The system as recited in claim 19 wherein the pilot transform coefficients are pilot discrete cosine transform coefficients that are based on the phase angles between the received pilot symbols and reference pilot symbols.
21. The system as recited in claim 20 wherein each optical transmission frame contains a total of N symbols with P pilot symbols periodically inserted within data symbols such that N is an odd number integer multiple of P.
22. The system as recited in claim 19 further comprising the frame processor determining a mean value of the received phase noise value for the optical symbol frame to provide an initial phase noise angle for de-rotation of received data symbols.
23. The system as recited in claim 19 , wherein the pilot processor circuit additionally utilizes pilot transform basis functions.