High-bandwidth optical communications relay payload

• US 8,953,946 B2
• Filed: 07/13/2012
• Issued: 02/10/2015
• Est. Priority Date: 07/13/2012
• Status: Active Grant

• Current Assignee: Raytheon Company (Rtx Corporation)
• Original Assignee: Raytheon Company (Rtx Corporation)
• Inventors: Coleman, Gary D., Hastings, C. Thomas Jr., Smith, Duane, Filgas, David
• Primary Examiner(s): Phan, Hanh
• Application Number:
  US13/549,177
• Publication Number:
  US 20140016932A1
• Time in Patent Office: 942 Days
• Field of Search: 398/118, 398/119, 398/120, 398/121, 398/122, 398/123, 398/124, 398/125, 398/128, 398/129, 398/130, 398/131, 398/135, 398/136, 398/115, 398/45, 398/48, 398/158, 398/159, 398/160, 398/126, 398/173, 398/175, 398/180, 455/12.1, 455/13.2, 455/13.3, 455/13.1, 455/3.02, 455/426, 455/427, 455/428, 455/430, 370/316, 370/317, 370/318, 370/310, 370/338, 370/326
• US Class Current: 398/121
• CPC Class Codes: H04B 10/118 specially adapted for satellite communication
• CPC Class Codes: H04B 7/18513 Transmission in a satellite or space-based system
• CPC Class Codes: H04B 7/18515 Transmission equipment in satellites or space-based relays
• CPC Class Codes: H04B 7/18521 Systems of inter linked satellites, i.e. inter satellite service for optical links between satellites H04B10/118

Abstract

A free space optical communication system (100) and method including: several optical beam expanders (414) for receiving incoming optical signals from ground sites and neighboring satellites; several optical preamplifiers (412) for preamplifying the received optical signals; one or more optical main amplifiers (404) for amplifying the preamplified optical signals; and an optical switch (408) for directing respective amplified optical signals to respective destinations via a respective optical beam expander. The respective amplified optical signals are inputted to a respective optical beam expander (414) for transmission to said respective destinations, as outgoing optical signals.

Claims

1. A free space optical communication system comprising:

a plurality of optical beam expanders for receiving incoming optical signals from and transmitting outgoing optical signals to ground sites and neighboring satellites;

a plurality of optical preamplifiers for preamplifying the received optical signals;

one or more optical main amplifiers for amplifying the preamplified optical signals; and

an optical switch for directing respective amplified optical signals to respective destinations via a respective optical beam expander,

wherein respective amplified optical signals are inputted to a respective optical beam expander for transmission to said respective destinations, as said outgoing optical signals, and wherein four optical beam expanders perform optical communication with two nearest neighboring satellites, one of each side, and two next nearest neighboring satellites, one on each side.

2. The system of claim 1, further comprising:

an optical multiplexer for combining the preamplified optical signals and outputting the combined optical signals to a single optical main amplifier for amplifying the combined optical signals; and

a demultiplexer for demultiplexing the amplified combined optical signals for outputting to the optical switch.

3. The system of claim 1, further comprising a plurality of optical power amplifiers optically coupled to the optical switch and respective optical beam expanders for amplifying the outgoing optical signals.

4. The system of claim 3, wherein each of the optical preamplifiers, optical main amplifiers and optical power amplifiers include one or more optical filters to reduce signal noise included in an optical signal from a previous stage.

5. The system of claim 3, wherein the optical preamplifiers, optical main amplifiers and optical power amplifiers are selected from a group consisting of one or more of Erbium-Doped Fiber Amplifiers (EDFAs), Planar Waveguides (PWGs), Semi-Guiding High Aspect Ratio Core (SHARC) fiber laser, and Raman amplifiers.

6. The system of claim 3, wherein the optical preamplifiers, optical main amplifiers and optical power amplifiers are low noise amplifiers, such that photon shot noise in the optical signals is the dominant noise source.

7. The system of claim 1, wherein each of the plurality of optical beam expanders associated with optical communications with the ground sites is configured to utilize Dense Wavelength Diversity Multiplexing (DWDM) to provide bi-directional links with a capability of at least 100 Gbps bandwidth with each ground site.

8. The system of claim 7, wherein each of the plurality of optical beam expanders associated with optical communications with the ground sites is further configured to utilize one or more of polarization and wavelength diversity to isolate two data streams in a bi-directional link.

9. The system of claim 1, wherein one or more of the plurality of optical beam expanders are associated with optical communications with the ground sites and are configured to track at least two ground terminals of a given ground site and send data to a ground terminal with the clearest line of sight to a satellite, in which the free space optical communication system is disposed, as said satellite passes the given ground site.

10. The system of claim 1, wherein the incoming optical signals and the outgoing optical signals are within a C-band or an L-band spectral bands.

11. The system of claim 1, wherein the incoming optical signals and the outgoing optical signals are optically reshaped and re-phased.

12. The system of claim 1, wherein the plurality of optical beam expanders associated with optical communications with ground sites are capable of providing a bi-directional throughput of at least 800 Gbps to the ground sites.

13. The system of claim 1, wherein the plurality of optical beam expanders associated with optical communications with the neighboring satellites are capable of providing a bi-directional throughput of at least 1,600 Gbps of data to and from neighboring satellites.

14. The system of claim 1, further comprising one or more lasers configured to amplify one or more of the optical signals.

15. The system of claim 1, wherein the optical switch includes piezoelectric actuators or Microelectromechanical systems (MEMS) with multiple small mirrors tilting as commanded to connect each optical signal from its input to the respective destinations.

16. The system of claim 1, further comprising a power interface configured to connect to a power bus of a satellite.

17. A method of free space optical communication in a constellation of a plurality of satellites utilizing the system of claim 1.

18. A method for free space optical communication, the method comprising:

receiving incoming optical signals from ground sites and neighboring satellites;

optically preamplifying the received optical signals;

optically amplifying the preamplified optical signals;

optically directing respective amplified optical signals to respective destinations via a respective optical beam expander; and

using four optical beam expanders for optical communication associated with two nearest neighboring satellites, one of each side, and two next nearest neighboring satellites, one on each side,

wherein respective amplified optical signals are inputted to a respective optical beam expander for transmission to said respective destinations, as outgoing optical signals.

19. The method of claim 18, further comprising:

combining the preamplified optical signals and outputting the combined optical signals to a single optical main amplifier for amplifying the combined optical signals; and

demultiplexing the amplified combined optical signals for outputting to an optical switch directing respective amplified optical signals to respective destinations.