IP Library › Granted Patent US 11,838,057
Granted Patent B2
US 11,838,057 · App. 17/555,343 · Granted Dec 5, 2023

Optical communication using double sideband suppressed carrier modulation

Inventor: James D. Franklin (Manhattan Beach, CA)
Assignee: THE BOEING COMPANY
H04B10/5165H04B10/25073H04B10/54H04B10/5561
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Quick Facts
Patent No.
US 11,838,057
App. No.
17/555,343
Granted
Dec 5, 2023
Kind
B2
Abstract

A method for operating an optical modulator includes receiving a narrowband radio frequency (“RF”) signal. The method further including, responsive to receiving the narrowband RF signal, modulating the narrowband RF signal using a double sideband suppressed carrier (“DSBSC”) modulation scheme to generate a DSBSC optical signal. The method further including transmitting the DSBSC optical signal to an optical transmitter.

Claims (59)

1. A method of operating an optical modulator, the method comprising:

receiving a narrowband radio frequency (“RF”) signal; and

responsive to receiving the narrowband RF signal, modulating the narrowband RF signal using a double sideband suppressed carrier (“DSBSC”) modulation scheme to generate a DSBSC optical signal,

wherein modulating the narrowband RF signal further comprising;

inputting an optical source laser signal into a first fast phase arm of the optical modulator and a second fast phase arm of the optical modulator;

passing an output of the first fast phase arm through a first slow phase arm of the optical modulator;

passing an output of the second fast phase arm through a second slow phase arm of the optical modulator; and

generating an optical output at an output of the optical modulator by combining an output of the first slow phase arm and an output of the second slow phase arm.

2. The method of claim 1 , wherein modulating the narrowband RF signal to generate the DSBSC optical signal further comprises:

receiving the optical source laser signal.

3. The method of claim 1 , wherein modulating the narrowband RF signal to generate the DSBSC optical signal further comprises:

generating a 0 degree phase shifted RF signal and a 180 degree phase shifted RF signal based on the narrowband RF signal using a 180 degree inverting amplifier;

inputting the 0 degree phase shifted RF signal into an electro-optical (“EO”) crystal of the first fast phase arm of the optical modulator; and

inputting the 180 degree phase shifted RF signal into an EO crystal of the second fast phase arm of the optical modulator.

4. The method of claim 3 , wherein modulating the narrowband RF signal to generate the DSBSC optical signal further comprises:

feeding back the optical output of the optical modulator through an EO detector into a bias controller that generates a voltage that causes a 180 degree phase shifted output;

inputting the 180 degree phase shifted output of the bias controller into an EO crystal of the second slow phase arm; and

outputting the DSBSC optical signal at the output of the optical modulator.

5. The method of claim 4 , wherein the optical modulator is a Mach-Zehnder modulator.

6. The method of claim 1 , wherein the narrowband RF signal is a narrowband phase modulated (“PM”) RF signal.

7. The method of claim 1 , wherein the narrowband RF signal is a narrowband amplitude modulated (“AM”) RF signal.

8. The method of claim 1 , wherein the optical modulator and optical transmitter are on a satellite in low earth orbit (“LEO”) or geosynchronous orbit (“GEO”).

9. The method of claim 1 , wherein the optical modulator is separate from an optical transmitter,

the method further comprising:

transmitting the DSBSC optical signal to the optical transmitter.

10. The method of claim 1 , wherein the optical modulator is included in an optical transmitter,

the method further comprising:

transmitting the DSBSC optical signal to at least one of:

a receiver via an optical fiber; and

an optical telescope system.

11. An optical modulator comprising:

an input port configured to receive a narrowband radio frequency (“RF”) signal;

an output port configured to output a double sideband suppressed carrier (“DSBSC”) signal; and

circuitry configured to modulate the narrowband RF signal using a DSBSC modulation scheme to generate a DSBSC optical signal, the circuitry comprising;

a first fast phase arm;

a second fast phase arm;

a first slow phase arm having an input coupled to an output of the first fast phase arm; and

a second slow phase arm having an input coupled to an output of the second fast phase arm,

wherein the output port is coupled to an output of the first slow phase arm and the second slow phase arm and further configured to generate an optical output by combining a first signal output by the first slow phase arm and a second signal output by the second slow phase arm.

12. The optical modulator of claim 11 , wherein the circuitry further comprises:

an optical laser signal source having an output coupled to an input of the first phase arm and an input of the second phase arm, the optical laser signal source configured to input an optical source laser signal into the first fast phase arm and into the second fast phase arm.

13. The optical modulator of claim 11 , wherein the circuitry further comprises:

a 180 degree inverting amplifier including an input coupled to the input port of the optical modulator and configured to generate a 0 degree phase shifted RF signal at a first output based on the narrowband RF signal and a 180 degree phase shifted RF signal at a second output based on the narrowband RF signal,

wherein the first fast phase arm includes an EO crystal coupled to the first output of the 180 degree inverting amplifier, and

wherein the second fast phase arm includes an EO crystal coupled to the second output of the 180 degree inverting amplifier.

14. The optical modulator of claim 13 , wherein the circuitry further comprises:

an EO detector including an input coupled to the output port; and

a bias controller including an input coupled to an output of the EO detector and configured to phase shift a signal at the output of the EO detector by 180 degrees,

wherein an EO crystal of the second slow phase arm is coupled to an output of the bias controller.

15. The optical modulator of claim 11 , wherein the optical modulator is a Mach-Zehnder modulator.

16. The optical modulator of claim 11 , wherein the narrowband RF signal is a narrowband phase modulated (“PM”) RF signal.

17. The optical modulator of claim 11 , wherein the narrowband RF signal is a narrowband amplitude modulated (“AM”) RF signal.

18. The optical modulator of claim 11 , wherein the optical modulator and optical transmitter are on a satellite in low earth orbit (“LEO”) or geosynchronous orbit (“GEO”).

19. The optical modulator of claim 11 , wherein the optical modulator is separate from the optical transmitter, and

wherein the circuitry is further configured to transmit the DSBSC optical signal to an optical transmitter.

20. The optical modulator of claim 11 , wherein the optical modulator is included in an optical transmitter, and

wherein the circuitry is further configured to transmit the DSBSC optical signal to at least one of:

a receiver via an optical fiber; and

an optical telescope system.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 17, 2021
From: FRANKLIN, JAMES D.
To: THE BOEING COMPANY
Reel/Frame 058424/0847 →
Continuity (1)
Related Publication 20230198624A1 · Jun 22, 2023