Technique for sharing radio frequency spectrum in multiple satellite communication systems

• US 5,995,841 A
• Filed: 08/22/1997
• Issued: 11/30/1999
• Est. Priority Date: 08/22/1997
• Status: Expired due to Fees

• Current Assignee: Hanger Solutions, LLC (IP Investments Group LLC)
• Original Assignee: Teledesic, LLC (Michael J. Larson, MBA)
• Inventors: Sturza, Mark A., King, Janet L., Deininger, Richard C., Grzemski, Kenneth C., Hayden, Thomas L.
• Primary Examiner(s): Chin, Wellington
• Assistant Examiner(s): Woldetatios, Yemane
• Application Number:
  US08/918,499
• Time in Patent Office: 830 Days
• Field of Search: 455/427, 455/450, 455/454, 455/12.1, 455/13.1, 455/62, 455/63, 455/428, 455/429
• US Class Current: 455/454
• CPC Class Codes: H04B 7/18513 Transmission in a satellite or space-based system
• CPC Class Codes: H04B 7/195 Non-synchronous stations

Abstract

A technique for sharing radio frequency spectrum in a multiple communication satellite system with a plurality of satellites in each of a plurality of non-geostationary (non-GSO) Earth orbits. A first satellite communication system uses a plurality of predefined non-GSO Earth orbits and a second satellite communication system uses a plurality of predefined orbits that are interleaved with the orbital planes of the first satellite communication system. In this manner, it is possible to achieve satisfactory discrimination between satellites and Earth-based stations. With near polar orbits, the topocentric separation between satellites decreases as the latitude of the Earth-based stations increases due to the convergence of orbital planes near the poles. To compensate for the decreased topocentric separation, the system utilizes one or more mitigation techniques to select one of a plurality of possible satellites to communicate with the Earth-based station in order to effectively increase topocentric separation.

Claims

1. A system for sharing a radio frequency spectrum between first and second satellite communication systems, the system comprising:

a first plurality of Earth-based communication stations operating as an Earth-bound portion of the first satellite communication system;

a second plurality of Earth-based communication stations operating as an Earth-bound portion of the second satellite communication system;

a first plurality of satellites in non-geostationary low-Earth orbits and operating as a satellite portion of the first satellite communication system to communicate with said first plurality of Earth-based communication stations and not communicating with said second plurality of Earth-based stations, each of said satellites in said first plurality of satellites orbiting the Earth in one of a first plurality of near polar orbital planes; and

a second plurality of satellites in non-geostationary low-Earth orbits and operating as a satellite portion of the second satellite communication system to communicate with said second plurality of Earth-based communication stations and not communicating with said first plurality of Earth-based stations, each of said satellites in said second plurality of satellites orbiting the Earth in one of a second plurality of near polar orbital planes different from said first plurality of near polar orbital planes, each of said second plurality of near polar orbital planes being located interleaved with said first plurality of near polar orbital planes, whereby said satellites of one of the first and second satellite communication systems and said Earth-based communication stations of the other system share the radio frequency spectrum by interleaving said near polar orbital planes of said first and second pluralities of satellites while maintaining interference between the satellite communication systems at an acceptable level.

2. The system of claim 1, further including a directional antenna coupled to each of said satellites in said first and second pluralities of satellites, said antenna of a particular satellite of said first plurality of satellites being oriented to direct radio beams between said particular satellite and a particular one of said first plurality of Earth-based communication stations and to thereby minimize direction of radio beams received by said second plurality of Earth-based communication stations.

3. The system of claim 1, further including a directional antenna coupled to each of said first and second plurality of Earth-based communication stations, said antenna of a particular one of said first plurality of Earth-based communication stations being oriented to direct radio beams between said particular Earth-based communication station and a particular satellite of said first plurality of satellites and to thereby minimize direction of radio beams received by said second plurality of satellites.

4. The system of claim 3 wherein said antenna of said particular Earth-based communication station is capable of communicating with a plurality of said satellites in said first plurality of satellites, said particular Earth-based communication station communicating with a selected satellite of said first plurality of satellites having a minimum acceptable topocentric separation between said selected satellite and said satellites of said second plurality of satellites.

5. The system of claim 4 wherein said satellite selection is based on an increased topocentric separation greater than said minimum acceptable topocentric separation.

6. The system of claim 4 wherein said satellite selection is further based on a communication traffic load in said plurality of satellites in said first plurality of satellites.

7. The system of claim 3 wherein said antenna of said particular Earth-based communication station is capable of communicating with a plurality of said satellites in said first plurality of satellites, said particular Earth-based communication station communicating with a selected satellite of said first plurality of satellites having a lowest slant range.

8. A system for sharing a radio frequency spectrum between first and second satellite communication systems, the system comprising:

a first plurality of Earth-based communication stations operating as an Earth-bound portion of the first satellite communication system;

a second plurality of Earth-based communication stations operating as an Earth-bound portion of the second satellite communication system;

a first plurality of satellites in non-geostationary Earth orbits and operating as a satellite portion of the first satellite communication system to communicate with said first plurality of Earth-based communication stations and not communicating with said second plurality of Earth-based stations, each of said satellites in said first plurality of satellites orbiting the Earth in one of a first plurality of orbital planes; and

a second plurality of satellites in non-geostationary Earth orbits and operating as a satellite portion of the second satellite communication system to communicate with said second plurality of Earth-based communication stations and not communicating with said first plurality of Earth-based stations, each of said satellites in said second plurality of satellites orbiting the Earth in one of a second plurality of orbital planes different from said first plurality of orbital planes, each of said second plurality of orbital planes being located interleaved with said first plurality of orbital planes.

9. The system of claim 8 wherein said first and second pluralities of satellites are in low-Earth orbits.

10. The system of claim 8 wherein said first and second pluralities of orbital planes are inclined at substantially 90°

with respect to the Earth'"'"'s equator, whereby said fist and second pluralities of satellites are in non-geostationary near-polar orbits.

11. A system for sharing a radio frequency spectrum between first and second satellite communication systems, the system comprising:

a first Earth-based communication station operating as an Earth-bound portion of the first satellite communication system;

a second Earth-based communication station operating as an Earth-bound portion of the second satellite communication system;

first and second satellites in a non-geostationary Earth orbit and operating as a satellite portion of the first satellite communication system to communicate with said first Earth-based communication station and not communicating with said second Earth-based communication station, said first and second satellites being placed in an Earth orbit in first and second predetermined planes, respectively; and

a third satellite in a non-geostationary Earth orbit and operating as a satellite portion of the second satellite communication system to communicate with said second Earth-based communication station and not communicating with said first Earth-based communication station, said third satellite being placed in an Earth orbit in a third predetermined plane located intermediate said first and second predetermined planes.

12. The system of claim 11 wherein said first, second and third satellites are in low-Earth orbits.

13. The system of claim 11 wherein said first, second and third orbits are inclined at substantially 90°

with respect to the Earth'"'"'s equator, whereby said first, second and third satellites are in near-polar orbits.

14. The system of claim 11, further including first, second and third directional antennas coupled to said first, second and third satellites, respectively, said first antenna being oriented to direct radio beams between said first satellite and said first Earth-based communication station and to thereby minimize direction of radio beams received by said second Earth-based communication station.

15. The system of claim 11, further including a first directional antenna coupled to said first Earth-based communication station, said antenna coupled to said first Earth-based communication station being oriented to direct radio beams between said first satellite and said first Earth-based communication station and to thereby minimize direction of radio beams received by said third satellite.

16. The system of claim 15 wherein said first antenna is capable of communicating with both said first and second satellites, said first Earth-based communication station communicating with a selected one of said first and second satellites based on a minimum acceptable topocentric separation between said selected satellite and said third satellite.

17. The system of claim 16 wherein said satellite selection is based on an increased topocentric separation greater than said minimum acceptable topocentric separation.

18. The system of claim 16 wherein said satellite selection is further based on a communication traffic load in said satellites of said first satellite communication system.

19. The system of claim 15 wherein said first antenna is capable of communicating with both said first and second satellites, said first Earth-based communication station communicating with a selected one of said first and second satellites based on a lowest slant range.

20. A system for sharing a radio frequency spectrum between a plurality of satellite communication systems, the system comprising:

an Earth-based communication station for each of the plurality of satellite communication systems and operating as an Earth-bound portion of the respective satellite communication system;

a set of orbital planes for each of the plurality of satellite communications systems, each of said set of orbital planes being interleaved in an ordered repetitive sequence; and

a satellite in non-geostationary Earth orbit in each of the orbital planes in each of said set of orbital planes, said satellites in each of said sets of orbital planes operating as a satellite portion of the respective satellite communication system to communicate only with said Earth-based communication station corresponding to the respective satellite communication system.

21. A method for sharing a radio frequency spectrum between first and second satellite communication systems, the method comprising the steps of:

operating a first plurality of Earth-based communication stations as an Earth-bound portion of the first satellite communication system;

operating a second plurality of Earth-based communication stations as an Earth-bound portion of the second satellite communication system;

operating a first plurality of satellites in non-geostationary Earth orbits as a satellite portion of the first satellite communication system to communicate with said first plurality of Earth-based communication stations and not communicating with said second plurality of Earth-based stations, each of said satellites in said first plurality of satellites orbiting the Earth in one of a first plurality of orbital planes; and

operating a second plurality of satellites in non-geostationary Earth orbits as a satellite portion of the second satellite communication system to communicate with said second plurality of Earth-based communication stations and not communicating with said first plurality of Earth-based stations, each of said satellites in said second plurality of satellites orbiting the Earth in one of a second plurality of orbital planes different from said first plurality of orbital planes, each of said second plurality of orbital planes being located interleaved with said first plurality of orbital planes.

22. The method of claim 21 wherein said first and second pluralities of satellites are in low-Earth orbits.

23. The method of claim 21 wherein said first and second pluralities of orbital planes are inclined at substantially 90°

with respect to the Earth'"'"'s equator, whereby said first and second pluralities of satellites are in near-polar orbits.

24. A method for sharing a radio frequency spectrum between first and second satellite communication systems wherein the first satellite communication system operates a first Earth-based communication station and first and second satellites in non-geostationary orbits to communicate with the first Earth-based communication station, the first and second satellites being placed in an Earth orbit in first and second predetermined planes, respectively, the method comprising:

operating a second Earth-based communication station as an Earth-bound portion of the second satellite communication system; and

operating a third satellite in a non-geostationary Earth orbit as a satellite portion of the second satellite communication system to communicate with said second Earth-based communication station and not communicating with the first Earth-based communication station, said third satellite being placed in an Earth orbit in a third predetermined plane located intermediate said first and second predetermined planes.

25. The method of claim 24 wherein said first, second and third satellites are in low-Earth orbits.

26. The method of claim 24 wherein said first, second and third orbits are inclined at substantially 90°

with respect to the Earth'"'"'s equator, whereby said first, second and third satellites are in near-polar orbits.

27. The method of claim 24 wherein said first Earth-based communication station is capable of communicating with both said first and second satellites, said step of operating said first Earth-based communication station including communicating with a selected one of said first and second satellites selected to have at least a minimum acceptable topocentric separation between said selected satellite and said third satellite.

28. The method of claim 27 wherein said satellite selection is based on an increased topocentric separation greater than said minimum acceptable topocentric separation.

29. The method of claim 27 wherein said satellite selection is further based on a communication traffic load in said satellites of said first satellite communication system.

30. A method for sharing a radio frequency spectrum between first and second satellite communication systems including a first Earth-based communication station as an Earth-bound portion of the first satellite communication system and a second Earth-based communication station as an Earth-bound portion of the second satellite communication system, the method comprising the steps of:

inserting a first satellite into a first non-geostationary Earth orbit as a satellite portion of the first satellite communication system to communicate with the first Earth-based communication station and not communicating with the second Earth-based communication station, said first Earth orbit having a first predetermined orbital plane;

inserting a second satellite into a second non-geostationary Earth orbit as a satellite portion of the first satellite communication system to communicate with the first Earth-based communication station and not communicating with the second Earth-based communication station, said second Earth orbit having a second predetermined orbital plane different from said first predetermined orbital plane; and

inserting a third satellite into a third non-geostationary Earth orbit as a satellite portion of the second satellite communication system to communicate with the second Earth-based communication station and not communicating with the first Earth-based communication station, said third Earth orbit having a third predetermined orbital plane different from said first and second predetermined orbital planes located intermediate said first and second predetermined orbital planes.

31. The method of claim 30 wherein said steps of inserting said first, second and third satellites includes insertion of said first, second and third satellites into low-Earth orbits.

32. The method of claim 30 wherein said steps of inserting said first, second and third satellites includes insertion of said first, second and third satellites into said first, second and third predetermined orbital planes, respectively, such that said first, second and third orbits are inclined at substantially 90°

with respect to the Earth'"'"'s equator, whereby said first, second and third satellites are in near-polar orbits.

33. The method of claim 30 wherein said first Earth-based communication station is capable of communicating with both said first and second satellites, said step of operating said first Earth-based communication station including communicating with a selected one of said first and second satellites selected to have at least a minimum acceptable topocentric separation between said selected satellite and said third satellite.

34. The method of claim 33 wherein said satellite selection is based on an increased topocentric separation greater than said minimum acceptable topocentric separation.

35. The method of claim 33 wherein said satellite selection is further based on a communication traffic load in said satellites of said first satellite communication system.

36. A system for sharing a radio frequency spectrum between first and second satellite communication systems, the system comprising:

a first Earth-based communication station operating as an Earth-bound portion of the first satellite communication system;

a second Earth-based communication station operating as an Earth-bound portion of the second satellite communication system;

first and second satellites in a non-geostationary Earth orbit and operating as a satellite portion of the first satellite communication system to communicate with said first Earth-based communication station, said first and second satellites being placed in an Earth orbit in first and second predetermined planes, respectively;

a third satellite in a non-geostationary Earth orbit and operating as a satellite portion of the second satellite communication system to communicate with said second Earth-based communication station, said third satellite being placed in an Earth orbit in a third predetermined plane located intermediate said first and second predetermined planes; and

a first directional antenna coupled to said first Earth-based communication station, said antenna coupled to said first Earth-based communication station being capable of communicating with both said first and second satellites and oriented to communicate with a selected one of said first and second satellites based on a minimum acceptable topocentric separation between said selected satellite and said third satellite to thereby minimize direction of radio beams received by said third satellite.

37. The system of claim 36 wherein said satellite selection is based on an increased topocentric separation greater than said minimum acceptable topocentric separation.

38. The system of claim 36 wherein said satellite selection is further based on a communication traffic load in said satellites of said first satellite communication system.

39. The system of claim 36 wherein the first and second satellite communication systems are portions of a common communication system, said first, second and third satellites being portions of said common communication system.

40. A system for sharing a radio frequency spectrum between first and second satellite communication systems, the system comprising:

a first Earth-based communication station operating as an Earth-bound portion of the first satellite communication system;

a second Earth-based communication station operating as an Earth-bound portion of the second satellite communication system;

first and second satellites in a non-geostationary Earth orbit and operating as a satellite portion of the first satellite communication system to communicate with said first Earth-based communication station, said first and second satellites being placed in an Earth orbit in first and second predetermined planes, respectively;

a third satellite in a non-geostationary Earth orbit and operating as a satellite portion of the second satellite communication system to communicate with said second Earth-based communication station, said third satellite being placed in an Earth orbit in a third predetermined plane located intermediate said first and second predetermined planes; and

a first directional antenna coupled to said first Earth-based communication station, said first directional antenna coupled to said first Earth-based communication station being capable of communicating with both said first and second satellites and oriented to communicate with a selected one of said first and second satellites based on a lowest slant range.

41. A method for sharing a radio frequency spectrum between first and second satellite communication systems, the method comprising:

operating a first Earth-based communication station as an Earth-bound portion of the first satellite communication system;

operating a second Earth-based communication station as an Earth-bound

portion of the second satellite communication system;

operating first and second satellites in a non-geostationary Earth orbit as a satellite portion of the first satellite communication system to communicate with said first Earth-based communication station, said first and second satellites being placed in an Earth orbit in first and second predetermined planes, respectively; and

operating a third satellite in a non-geostationary Earth orbit as a satellite portion of the second satellite communication system to communicate with said second Earth-based communication station, said third satellite being placed in an Earth orbit in a third predetermined plane located intermediate said first and second predetermined planes, wherein said first Earth-based communication station is capable of communicating with both said first and second satellites, said act of operating said first Earth-based communication station comprising communicating with a selected one of said first and second satellites selected to have at least a minimum acceptable topocentric separation between said selected satellite and said third satellite.

42. The method of claim 41 wherein said satellite selection is based on an increased topocentric separation greater than said minimum acceptable topocentric separation.

43. The method of claim 41 wherein said satellite selection is further based on a communication traffic load in said satellites of said first satellite communication system.

44. The method of claim 41 wherein the first and second satellite communication systems are portions of a common communication system, said first, second and third satellites being portions of said common communication system.

45. A method for sharing a radio frequency spectrum between first and second satellite communication systems including a first Earth-based communication station as an Earth-bound portion of the first satellite communication system and a second Earth-based communication station as an Earth-bound portion of the second satellite communication system, the method comprising the steps of:

inserting a first satellite into a first non-geostationary Earth orbit as a satellite portion of the first satellite communication system to communicate with the first Earth-based communication station, said first Earth orbit having a first predetermined orbital plane;

inserting a second satellite into a second non-geostationary Earth orbit as a satellite portion of the first satellite communication system to communicate with the first Earth-based communication station, said second Earth orbit having a second predetermined orbital plane different from said first predetermined orbital plane; and

inserting a third satellite into a third non-geostationary Earth orbit as a satellite portion of the second satellite communication system to communicate with the second Earth-based communication station, said third Earth orbit having a third predetermined orbital plane different from said first and second predetermined orbital planes located intermediate said first and second predetermined orbital planes wherein said first Earth-based communication station is capable of communicating with both said first and second satellites, said act of operating said first Earth-based communication station comprising communicating with a selected one of said first and second satellites selected to have at least a minimum acceptable topocentric separation between said selected satellite and said third satellite.

46. The method of claim 45 wherein said satellite selection is based on an increased topocentric separation greater than said minimum acceptable topocentric separation.

47. The method of claim 45 wherein said satellite selection is further based on a communication traffic load in said satellites of said first satellite communication system.