System and method for multiple layer satellite communication

• US 9,391,702 B2
• Filed: 05/15/2013
• Issued: 07/12/2016
• Est. Priority Date: 05/15/2013
• Status: Active Grant

• Current Assignee: WorldVu Satellites Limited
• Original Assignee: WorldVu Satellites Limited
• Inventors: Wyler, Gregory Thane
• Primary Examiner(s): Leung, Danney
• Application Number:
  US13/894,994
• Publication Number:
  US 20140341586A1
• Time in Patent Office: 1,154 Days
• Field of Search: 398/115
• US Class Current: 1/1
• CPC Class Codes: H04B 10/118 specially adapted for satellite communication
• 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 system and method are disclosed that may include a system and method for transmitting user data from an initial satellite in a first constellation located conveniently to an origination user terminal to a destination satellite in the first constellation located conveniently to a destination user terminal, the method including transmitting the user data over an optical link from the initial satellite in the first constellation to a first satellite within a second satellite constellation; conveying the user data over an optical link from the first satellite in the second constellation to a second satellite in the second constellation; and receiving the user data from the second satellite in the second constellation at the destination satellite in the first constellation.

Claims

1. A communication system, comprising:

a first constellation of satellites traveling in an inclined orbit and operable to communicate with earth-based user terminals over respective radio frequency (RF) links;

a processor operable to monitor separation angles between beams of said first constellation of satellites and a GSO beam and maintain each of the separation angles by at least a selected number of degrees by temporarily tilting at least some satellites in the first constellation of satellites to move the beams of the respective RF links away from the GSO beam to avoid an interference with the GSO beam without deviating from the inclined orbit; and

a second constellation of satellites traveling in an inclined orbit at a higher altitude than the first constellation and operable to communicate with selected satellites in said first constellation over respective optical communication links.

2. The communication system of claim 1 wherein satellites in the first constellation orbit at an altitude between 600 and 950 kilometers (km).

3. The communication system of claim 1 wherein satellites in the second constellation orbit at an altitude of between 1100 and 1400 km.

4. The communication system of claim 1 wherein satellites in the second constellation travel along an orbit inclined at an angle between 35 degrees and 60 degrees.

5. The communication system of claim 1 wherein satellites in the first constellation travel along an orbit inclined at an angle between 60 degrees and 90 degrees.

6. The communication system of claim 1 wherein the first constellation includes between 200 and 1500 satellites.

7. The communication system of claim 1 wherein each satellite in the second constellation is able to communicate with at least two satellites in the second constellation and at least two satellites in the first constellation.

8. The communication system of claim 1 wherein each satellite in the first constellation comprises:

multiple RF ports for communication with earth-based user terminals.

9. The communication system of claim 1 wherein each satellite in the first constellation comprises:

at least two optical communication ports for communicating with one or more satellites in the second constellation.

10. The communication system of claim 1 wherein any satellite in the first constellation communicates with any other satellite in the first constellation using the satellites in the second constellation as communication intermediaries.

11. A communications system comprising:

a first satellite constellation in orbit around the earth and operable to communicate with a plurality of user terminals on the earth over radio frequency (RF) links;

a processor operable to monitor separation angles between beams of said first satellite constellation and a GSO beam and maintain each of the separation angles by at least a selected number of degrees by temporarily tilting at least some satellites in the first satellite constellation beams of the respective RF links away from the GSO beam to avoid an interference with the GSO beam; and

a second satellite constellation operable to provide a high-speed communication trunk line between a data-path origination satellite and a data-path destination satellite within said first satellite constellation.

12. The communications system claim 11 wherein a majority of a set of communications links between the first constellation and the second constellation are optical.

13. The communications system of claim 11 wherein a majority of a set of communication links between the satellites of the second constellation are primarily optical.

14. The communications system of claim 11 wherein a majority of the communication links between satellites in the second constellation and user terminals on the earth use radio frequency (RF) communication.

15. The communications system of claim 11 wherein the second constellation orbits at a higher altitude than the first constellation.

16. The communication system of 11 where the satellites of the first constellation include the ability to route traffic between two individual user terminals without passing the data traffic to a satellite in the second constellation.

17. A method for transmitting user data from an initial satellite in a first constellation to a destination satellite in the first constellation, the method comprising the steps of:

(a) transmitting the user data from the first-constellation initial satellite to a first satellite in a second constellation, the second constellation having a different orbit altitude than that of the first constellation, the first and second constellations both including a plurality of satellites and both having non-geostationary orbits;

(b) identifying a second satellite in the second constellation that is most suitable for communication with the first-constellation destination satellite;

(c) transmitting the user data from the first satellite in the second constellation to the identified second satellite in the second constellation;

(d) transmitting the user data from the second satellite in the second constellation to the first-constellation destination satellite; and

(e) monitoring separation angles between beams of said first constellation of satellites and a GSO beam and maintaining each of the separation angles by at least a selected number of degrees by temporarily tilting at least some satellites in the first constellation of satellites to move the beams of the respective RF links away from the GSO beam to avoid an interference with the GSO beam.

18. The method of claim 17 further comprising the steps of:

the first-constellation initial satellite receiving the user data from a first user terminal over a radio frequency (RF) link; and

transmitting the user data from the first-constellation destination satellite to a second user terminal.

19. The method of claim 17 wherein the step of

transmitting the user data from the first-constellation initial satellite to the first satellite in the second constellation is conducted over an optical communications link.

20. The method of claim 17 wherein the step of:

transmitting the user data from the first satellite in the second constellation to the identified second satellite in the second constellation is performed over an optical communications link.

21. The method of claim 17 further comprising:

directing satellites in the first constellation along an orbit having a first inclination angle; and

directing satellites in the second constellation along an orbit having a second inclination angle differing by least five degrees from the first inclination angle.

22. The method of claim 17 wherein said transmitting steps (a), (c), and (d) are operable to alleviate data traffic congestion in said first constellation.

23. A method for transmitting user data from an initial satellite in a first constellation located conveniently to an origination user terminal to a destination satellite in the first constellation located conveniently to a destination user terminal, the method comprising the steps of:

transmitting the user data over an optical link from the initial satellite in the first constellation to a first satellite within a second satellite constellation;

conveying the user data over an optical link from the first satellite in the second constellation to a second satellite in the second constellation;

receiving the user data from the second satellite in the second constellation at the destination satellite in the first constellation; and

monitoring separation angles between beams of said first constellation of satellites and a GSO beam and maintaining each of the separation angles by at least a selected number of degrees by temporarily tilting at least some satellites in the first constellation of satellites to move the beams of the respective RF links away from the GSO beam to avoid an interference with the GSO beam.

24. The method of claim 23 wherein all of the satellites are in non-geostationary orbits.

25. The method of claim 23 further comprising:

receiving the user data from the origination user terminal over a radio frequency (RF) link at an initial satellite within the first satellite constellation.

26. The method of claim 23 further comprising:

transmitting the user data from the destination satellite in the first constellation to the destination user terminal.

27. The method of claim 23 further comprising:

controlling communication at said initial and destination satellites in said first constellation and said first and second satellites in said second constellation using a data center on the earth.

28. The method of claim 23 wherein the steps of transmitting, conveying, and receiving correspond to using the second constellation as a space-based communications trunk line for said first constellation.

29. The method of claim 23 wherein the conveying step comprises:

transmitting the user data through a sequence of satellites within the second constellation located between the first and second satellites in the second constellation.

30. The method of claim 23 wherein the conveying step comprises:

transmitting the user data directly from the first satellite in the second constellation to the second satellite in the second constellation.