Optical communication using double sideband suppressed carrier demodulation
A method for operating an optical demodulator includes receiving a double sideband suppressed carrier (“DSBSC”) optical signal. The method further includes passing the DSBSC optical signal through a Costas loop circuit. The method further includes outputting a radio frequency (“RF”) signal from a quadrature port of the Costas loop circuit.
1. A method of operating an optical demodulator, the method comprising:
receiving a double sideband suppressed carrier (“DSBSC”) optical signal;
passing the DSBSC optical signal through a Costas loop circuit including separating data in the DSBSC optical signal into an in-phase (“I”) and a quadrature-phase (“Q”) channel,
wherein passing the DSBSC optical signal through the Costas loop circuit comprises:
passing the DSBSC optical signal to an input of a 3 dB coupler;
passing an output of the 3 dB coupler to an input of an optical/electrical detector;
passing the output of the optical/electrical detector to an input of a Transimpedance Amplifier (“TIA”);
passing an output of the TIA to an input of an electrical amplifier;
passing an output of the electrical amplifier to an input of a quadrature mixer;
passing an output of the quadrature mixer to an input of a first low pass filter (“LPF”) and a second LPF;
passing an output of the first LPF to an input of a discriminator mixer;
passing an output of the second LPF to an input of a splitter;
passing an output of the splitter to an input of the discriminator mixer and an amplifier;
passing an output of the discriminator mixer to an input of a laser diode;
passing an output of the laser diode to an input of the 3 dB coupler as optical input feedback; and
passing an output of the amplifier through a band pass filter to generate a radio frequency (“RF”) signal; and
outputting the RF signal from a quadrature port of the Costas loop circuit.
2. The method of claim 1 , wherein the optical demodulator is coupled to a first satellite in a first orbit.
3. The method of claim 2 , wherein receiving the DSBSC optical signal from a second satellite comprises receiving the DSBSC optical signal from an optical modulator and optical transmitter in the second satellite.
4. The method of claim 2 , wherein the first orbit includes a low earth orbit (“LEO”) or a geosynchronous orbit (“GEO”).
5. The method of claim 2 , wherein receiving the DSBSC optical signal comprises receiving the DSBSC optical signal from a second satellite in a second orbit that is different from the first orbit.
6. The method of claim 1 , wherein the RF signal comprises a narrowband RF signal.
7. The method of claim 6 , wherein the narrowband RF signal is a narrowband phase modulated (“PM”) RF signal.
8. The method of claim 6 , wherein the narrowband RF signal is a narrowband amplitude modulated (“AM”) RF signal.
9. The method of claim 1 , wherein the optical demodulator comprises a bandpass filter, a square-law detector, and the Costas loop circuit.
10. The method of claim 1 , wherein the Costas loop circuit further comprises a laser diode and an optical hybrid.
11. An optical demodulator comprising:
an input port configured to receive a double sideband suppressed carrier (“DSBSC”) optical signal;
a Costas loop circuit having an input coupled to the input port and an output coupled to an output port, the Costas loop circuit configured to demodulate the DSBSC optical signal to generate a radio frequency (“RF”) signal, the Costas loop including a transimpedance amplifier (“TIA”),
wherein the Costas loop circuit is further configured to:
pass the DSBSC optical signal to an input of a 3 dB coupler;
pass an output of the 3 dB coupler to an input of an optical/electrical detector;
pass the output of the optical/electrical detector to an input of the TIA;
pass an output of the TIA to an input of an electrical amplifier;
pass an output of the electrical amplifier to an input of a quadrature mixer;
pass an output of the quadrature mixer to an input of a first low pass filter (“LPF”) and a second LPF;
pass an output of the first LPF to an input of a discriminator mixer;
pass an output of the second LPF to an input of a splitter;
pass an output of the splitter to an input of the discriminator mixer and an amplifier;
pass an output of the discriminator mixer to an input of a laser diode;
pass an output of the laser diode to an input of the 3 dB coupler as optical input feedback; and
pass an output of the amplifier through a band pass filter to generate the RF signal; and
the output port coupled to a quadrature port of the Costas loop circuit and configured to output the RF signal.
12. The optical demodulator of claim 11 , wherein the optical demodulator is coupled to a first satellite in a first orbit.
13. The optical demodulator of claim 12 , wherein the input port is further configured to receive the DSBSC optical signal from an optical modulator and optical transmitter in a second satellite.
14. The optical demodulator of claim 12 , wherein the first orbit includes a low earth orbit (“LEO”) or a geosynchronous orbit (“GEO”).
15. The optical demodulator of claim 12 , wherein the input port is further configured to receive the DSBSC optical signal from a second satellite in a second orbit that is different from the first orbit.
16. The optical demodulator of claim 11 , wherein the RF signal comprises a narrowband RF signal.
17. The optical demodulator of claim 16 , wherein the narrowband RF signal is a narrowband phase modulated (“PM”) RF signal.
18. The optical demodulator of claim 16 , wherein the narrowband RF signal is a narrowband amplitude modulated (“AM”) RF signal.
19. The optical demodulator of claim 11 , wherein the optical demodulator comprises a bandpass filter, a square-law detector, and the Costas loop circuit.
20. The optical demodulator of claim 11 , wherein the Costas loop circuit further comprises a laser diode and an optical hybrid.