High-bandwidth optical communications relay architecture

• US 8,913,894 B2
• Filed: 07/13/2012
• Issued: 12/16/2014
• 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, Silny, John F.
• Primary Examiner(s): Phan, Hanh
• Application Number:
  US13/549,191
• Publication Number:
  US 20140016941A1
• Time in Patent Office: 886 Days
• Field of Search: 398/121, 398/131, 398/118, 398/119, 398/122, 398/123, 398/124, 398/125, 398/115, 398/135, 398/136, 398/128, 398/129, 398/130, 398/175, 398/173, 398/180, 455/12.1, 455/13.2, 455/427, 455/426, 455/428, 455/13.3, 455/13.1, 455/3.02, 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 a constellation of several satellites (102). Each of satellites including: several inter-satellite optical telescopes (204) for optical communication with multiple neighboring satellites, each inter-satellite optical telescope is capable of adjusting its elevation angle; and several up/down link optical telescopes (206) for optical communication with multiple ground sites. As the constellation passes a given ground site, some of the up/down-link telescopes of a given satellite are configured to track at least two respective ground optical telescopes of the given ground site and send data to the ground optical telescope with the clearest line of sight to the given satellite. Moreover, each of the satellites includes optical circuitry (208, 210, 212, 216) for optically processing and switching incoming and outgoing optical signals without converting the optical signals into electrical signals.

Claims

1. A free space optical communication system comprising:

a constellation of a plurality of satellites, each of the plurality of satellites comprising;

a plurality of inter-satellite optical telescopes for optical communication with multiple neighboring satellites, and wherein each inter-satellite optical telescope is capable of adjusting its elevation angle to accommodate changes in the number of satellites in the constellation, and

a plurality of up/down link optical telescopes for optical communication with multiple ground sites, each ground site having two or more ground optical telescopes,

wherein as the satellite constellation passes a given ground site, one or more of the up/down-link telescopes of a given satellite are configured to track at least two ground optical telescopes of the given ground site, determine a line of site for each of the at least two ground optical telescopes of the given ground site, and send data to a ground optical telescope with the clearest line of sight to the given satellite.

2. The system of claim 1, wherein each inter-satellite optical telescope utilizes circular polarization or spectral diversity to provide dual optical signal paths.

3. The system of claim 1, wherein said one or more of the up/down-link telescopes of a given satellite are configured to continuously and in real time track at least two respective ground optical telescopes of the given ground site.

4. The system of claim 1, wherein said one or more of the up/down-link telescopes of a given satellite are configured to track at least two respective ground optical telescopes of the given ground site, using an optical beacon.

5. The system of claim 1, wherein a single up/down-link telescope of the given satellite is configured to track said at least two respective ground optical telescopes of the given ground site using circular polarization or spectral diversity.

6. The system of claim 1, wherein four inter-satellite optical telescopes are used for optical communication with two nearest neighboring satellites, one of each side, and two next nearest neighboring satellites, one on each side, respectively.

7. The system of claim 6, wherein each optical telescope used for nearest neighboring satellite includes an aperture of about 15 cm in diameter, and each optical telescope used for next nearest neighboring satellite includes an aperture of about 30 cm in diameter.

8. The system of claim 1, wherein each inter-satellite telescope includes an aperture of about 30 cm in diameter.

9. The system of claim 1, wherein the constellation of the plurality of satellites is launched into a common Medium Earth Orbit (MEO) equatorial orbit plane.

10. The system of claim 1, wherein the constellation of the plurality of satellites includes a plurality of Medium Earth Orbit (MEO) satellites and one or more Geostationary Earth Orbit (GEO) satellites.

11. The system of claim 10, wherein each of the plurality of MEO satellites includes one or more GEO-link telescopes with a field of regard sufficiency large such that at least one MEO satellite is always able to communicate with any of the GEO satellites.

12. The system of claim 1, wherein the constellation of the plurality of satellites includes a plurality of Medium Earth Orbit (MEO) satellites and one or more Low Earth Orbit (LEO) satellites.

13. The system of claim 1, wherein each inter-satellite optical telescope includes beam steering mirrors to compensate for jitter and orbit differences of said each inter-satellite optical telescope.

14. The system of claim 1, wherein each up/down link optical telescope includes dual internal steering mirrors to maintain track on said at least two respective ground optical telescopes of the given ground site.

15. The system of claim 1, wherein each up/down link optical telescope is configured to utilize Dense Wavelength Diversity Multiplexing (DWDM) to provide bi-directional links with at least 100 Gbps bandwidth with each ground site.

16. The system of claim 1, wherein each up/down link telescope includes an aperture of about 10 cm in diameter.

17. The system of claim 1, wherein the plurality of up/down link optical telescopes are gimbaled telescopes or telescopes with coelostats on each satellite to track a ground site.

18. The system of claim 1, wherein each of the plurality of satellites further includes one or more main lasers for amplifying the outgoing optical signals.

19. The system of claim 1, wherein each of the plurality of satellites includes multiple amplifier chains capable of reamplifying the incoming optical signal.

20. The system of claim 1, wherein at least one of the plurality of up/down optical telescope is available for optical communication with a ground site when an optical ground connection from a preceding satellite in the constellation is nearing an end, to establish a new connection to a following satellite in the constellation before breaking the optical ground connection from the preceding satellite.

21. A method for free space optical communication in a constellation of a plurality of satellites, the method comprising:

using a plurality of inter-satellite optical telescopes in each of the plurality of satellites to optically communicate with multiple neighboring satellites;

using a plurality of up/down link optical telescopes in each of the plurality of satellites to optically communicate with multiple ground sites, each ground site having two or more ground optical telescopes;

tracking, by a given satellite, at least two ground optical telescopes of a given ground site;

determining a line of site for each of the at least two ground optical telescopes of the given ground site; and

sending data to a ground optical telescope with the clearest line of sight to the given satellite, wherein each of the plurality of satellites optically processes and switches incoming and outgoing optical signals, without converting the optical signals into electrical signals.

22. The method of claim 21, further comprising utilizing circular polarization or spectral diversity to provide dual optical signal paths, by each inter-satellite optical telescope.

23. The method of claim 21, further comprising continuously and in real time tracking at least two respective ground optical telescopes of the given ground site, by one or more of the up/down-link telescopes of the given satellite.

24. The method of claim 21, further comprising using four inter-satellite optical telescopes to optically communicate with two nearest neighboring satellites, one of each side, and two next nearest neighboring satellites, one on each side, respectively.

25. The method of claim 21, wherein the constellation of the plurality of satellites is launched into a common Medium Earth Orbit (MEO) equatorial orbit plane.

26. The method of claim 21, wherein the constellation of the plurality of satellites includes a plurality of Medium Earth Orbit (MEO) satellites, and one or more Geostationary Earth Orbit (GEO) satellites or Low Earth Orbit (LEO) satellites.

27. The method of claim 21, further comprising making available at least one of the plurality of up/down optical telescope for optical communication with a ground site when an optical ground connection from a preceding satellite in the constellation is nearing an end, to establish a new connection to a following satellite in the constellation before breaking the optical ground connection from the preceding satellite.