Technique for sharing radio frequency spectrum in multiple satellite communication systems

• US 6,011,951 A
• Filed: 08/22/1997
• Issued: 01/04/2000
• 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: King, Janet L., Deininger, Richard C., Grzemski, Kenneth C., Hayden, Thomas L., Sturza, Mark A.
• Primary Examiner(s): CUMMING, WILLIAM D
• Application Number:
  US08/916,122
• Time in Patent Office: 865 Days
• Field of Search: 455/12.1, 455/13.1, 455/13.2, 455/456, 455/25, 340/991
• US Class Current: 455/13.2
• CPC Class Codes: H04B 7/1851 Systems using a satellite or space-based relay H04B7/18508, H04B7/18521 take precedence; providing specific services H04B7/18523 - H04B7/18576
• CPC Class Codes: H04B 7/195 Non-synchronous stations

Abstract

A technique for sharing radio frequency spectrum between multiple satellite communication systems. A first and a second satellite communication system each contain a plurality of satellites in a plurality of non-geostationary (non-GSO) Earth orbits. Each of the plurality of non-GSOs has a predefined orbital plane. Within each orbital plane, satellites of the first and second satellite communication systems are alternating, such that each orbital plane contains satellites from each of the satellite systems. In this manner, it is possible to achieve satisfactory discrimination between satellites and Earth-based stations. The Earth-based station of each communication system will communicate with the closest satellite of its respective communication system. In an alternative technique that is particularly useful when an Earth-based station in the first communication system is able to communicate with more than one satellite, a satellite is selected based on the topocentric separation of the satellite from satellites in the second system. The system can also combine alternating satellites within an orbital plane with alternating orbital planes with satellites of each respective communication system.

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 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, each of said satellites of said first plurality of satellites orbiting the Earth in one of a plurality of orbital planes; and

a second plurality of satellites in non-geostationary orbits and operating as a satellite portion of the second satellite communication system to communicate with said second plurality of Earth-based communication stations, each of said satellites of said second plurality of satellites orbiting the Earth in one of said plurality of orbital planes, said satellites of said first and second pluralities of satellites being in alternate positions within at least one of said orbital planes, whereby the first and second satellite communication systems share the radio frequency spectrum by interleaving said satellites of said first and second pluralities of satellites in at least one orbital plane.

2. The system of claim 1, further including a directional antenna coupled to each of said satellites of said first plurality of satellites, said antenna of a particular satellite of said first plurality of satellites being oriented to transmit radio frequency signals from said particular satellite to a particular one of said first plurality of Earth-based communication stations and thereby reduce transmission of radio frequency signals from said particular satellite of said first plurality of satellites to 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 plurality of Earth-based communication stations, said antenna of a particular one of said first plurality of Earth-based communication stations being oriented to transmit radio frequency signals from said particular Earth-based communication station to a particular satellite of said first plurality of satellites and thereby reduce transmission of radio frequency signals from said particular Earth-based communication station of said first plurality of Earth-based communication stations to said second plurality of satellites.

4. The system of claim 1, further including an antenna coupled to each of said first plurality of Earth-based communication stations, said antenna of a particular one of said first plurality of Earth-based communication stations being oriented to communicate 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 selected based on a topocentric separation between said selected satellite and said satellites of said second plurality of satellites.

5. The system of claim 4 wherein said selected satellite of said first plurality of satellites is selected to have a minimum acceptable topocentric separation between said selected satellite and said satellites of said second plurality of satellites.

6. The system of claim 1, further including an antenna coupled to each of said first plurality of Earth-based communication stations, said antenna of a particular one of said first plurality of Earth-based communication stations being oriented to communicate 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 selected based on a lowest slant range.

7. The system of claim 1, further including an antenna coupled to each of said first plurality of Earth-based communication stations, said antenna of a particular one of said first plurality of Earth-based communication stations being oriented to communicate 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 selected based on a communication traffic load in said plurality of satellites in said first plurality of satellites.

8. The system of claim 1 wherein said first and second pluralities of satellites are in low-Earth orbits.

9. The system of claim 1 wherein said plurality 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.

10. 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 in an Earth orbit in a first predetermined plane; 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, said third satellite being in an Earth orbit in said first predetermined plane and positioned intermediate said first and second satellites in said first predetermined plane.

11. The system of claim 10 wherein said first, second and third satellites are in low-Earth orbits.

12. The system of claim 10 wherein said Earth 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.

13. The system of claim 10, further including a directional antenna coupled to said first satellite, said antenna being oriented to transmit radio frequency signals from said first satellite to said first Earth-based communication station and thereby reduce transmission of radio frequency signals from said first satellite to said second Earth-based communication station.

14. The system of claim 10, further including a directional antenna coupled to said first Earth-based communication station and oriented to transmit radio frequency signals from said first Earth-based communication station to said first satellite and thereby reduce transmission of radio frequency signals from said first Earth-based communication station received by said third satellite.

15. The system of claim 10, further including:

a fourth satellite in a non-geostationary Earth orbit in a second predetermined plane different from said first predetermined plane and operating as a portion of said satellite portion of the first satellite communication system to communicate with said first Earth-based communication station; and

a directional antenna coupled to said first Earth-based communication station and oriented to communicate with said first and fourth satellites, said first Earth-based communication station communicating with a selected one of said first and fourth satellites based on a topocentric separation between said first and fourth satellites and a topocentric separation between said third and fourth satellites.

16. The system of claim 15 wherein said selected one of said first and fourth satellites having a minimum acceptable topocentric separation from said third satellite is selected for communication with said first Earth-based communication station.

17. The system of claim 10, further including:

a fourth satellite in a non-geostationary Earth orbit in a second predetermined plane different from said first predetermined plane and operating as a portion of said satellite portion of the first satellite communication system to communicate with said first Earth-based communication station; and

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

18. The system of claim 10, further including:

a fourth satellite in a non-geostationary Earth orbit in a second predetermined plane different from said first predetermined plane and operating as a portion of said satellite portion of the first satellite communication system to communicate with said first Earth-based communication station; and

a directional antenna coupled to said first Earth-based communication station and oriented to communicate with said first and fourth satellites, said first Earth-based communication station communicating with a selected one of said first and fourth satellites based on a communication traffic load in said first and fourth satellites.

19. A system for sharing a radio frequency spectrum in a satellite communication system, the system comprising:

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

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

a third satellite in a non-geostationary Earth orbit and operating as a satellite portion of the satellite communication system to communicate with said second Earth-based communication station, said third satellite being in an Earth orbit in said first predetermined orbital plane and positioned intermediate said first and second satellites in said first predetermined orbital plane.

20. The system of claim 19 wherein said Earth 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.

21. 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;

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 Earth-based communication station, each of said satellites of 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 Earth-based communication station, a portion of said satellites of 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, at least one of said second plurality of satellites being positioned intermediate two adjacent ones of said first plurality of satellites in a selected one of said first plurality of orbital planes.

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

23. The system 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 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 shared by the plurality of satellite communications systems; and

a satellite for each of the respective satellite communication operating as a satellite portion of the respective satellite communication system to communicate with said Earth-based communication station corresponding to the respective satellite communication system, said satellites each being in a non-geostationary Earth orbit and interleaved in an ordered repetitive sequence in each of said set of orbital planes.

25. 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, each of said satellites of said first plurality of satellites orbiting the Earth in a first orbital plane; 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, each of said satellites of said second plurality of satellites orbiting the Earth in one of said plurality of orbital planes in a position intermediate adjacent ones of said satellites of said first plurality of satellites such that each of said orbital planes contains alternating ones of said first and second plurality of satellites.

26. The method of claim 25 wherein said first and second pluralities of satellites are in low-Earth orbits.

27. The method of claim 25 wherein said plurality 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.

29. The method of claim 26 wherein said first, second and third satellites are in low-Earth orbits in said first orbital plane.

30. The method of claim 26 wherein said first orbital plane is inclined at substantially 90°

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

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

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 a first Earth orbit having a first predetermined plane; 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 said first predetermined plane and positioned intermediate said first and second satellites in said first orbital plane.

31. The method of claim 28 for use with a fourth satellite in a non-geostationary Earth orbit and operating as a portion of said satellite portion of the first satellite communication system to communicate with said first Earth-based communication station, said fourth satellite being placed in an Earth orbit in a second predetermined plane different from said first predetermined plane, the method further including the step of selecting said first or fourth satellite for communication with said first Earth-based communication station based on a topocentric separation between said first and fourth satellites and a topocentric separation between said third and fourth satellites.

32. The method of claim 31 wherein said step of selecting selects one of said first and fourth satellites having a minimum acceptable topocentric separation from said third satellite.

33. The method of claim 28 for use with a fourth satellite in a non-geostationary Earth orbit and operating as a portion of said satellite portion of the first satellite communication system to communicate with said first Earth-based communication station, said fourth satellite being placed in an Earth orbit in a second predetermined plane different from said first predetermined plane, the method further including the step of selecting said first or fourth satellite for communication with said first Earth-based communication station based on a lowest slant range.

34. The method of claim 28 for use with a fourth satellite in a non-geostationary Earth orbit and operating as a portion of said satellite portion of the first satellite communication system to communicate with said first Earth-based communication station, said fourth satellite being placed in an Earth orbit in a second predetermined plane different from said first predetermined plane, the method further including the step of selecting said first or fourth satellite for communication with said first Earth-based communication station based on a communications traffic load in said first and fourth satellites.

35. A method for sharing a radio frequency spectrum in a satellite communication system, the method comprising the steps of:

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

operating first and second satellites, each in a non-geostationary Earth orbit, as a satellite portion of the satellite communication system, said first and second satellites being in an Earth orbit in a first predetermined plane and communicating with said first Earth-based communication station; and

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

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

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;

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

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

inserting a third satellite into a non-geostationary Earth orbit in said first predetermined plane as a satellite portion of the second satellite communication system to communicate with said second Earth-based communication station; and

positioning said third satellite intermediate said first and second satellites in said first predetermined plane, the first and second satellite communication systems is minimized by said first, second and third satellites in said first predetermined plane.

37. The method of claim 36 wherein said non-geostationary Earth orbits of said first, second, and third satellites are low-Earth orbits and said steps of inserting said first, second and third satellites includes insertion of said first, second and third satellites into said low-Earth orbits in said first predetermined plane.

38. The method of claim 36 wherein said non-geostationary Earth orbits of said first, second, and third satellites are inclined at substantially 90°

with respect to the Earth'"'"'s equator and said steps of inserting said first, second and third satellites includes insertion of said first, second and third satellites into said first predetermined orbital plane such that said first, second and third satellites are in near-polar orbits in said first predetermined orbital plane.

39. The method of claim 36, further including the steps of inserting a fourth satellite into a non-geostationary Earth orbit in a second predetermined plane different from said first predetermined orbital plane for operation as a portion of said satellite portion of the first satellite communication system to communicate with said first Earth-based communication station, and selecting said first or fourth satellite for communication with said first Earth-based communication station based on a topocentric separation between said first and fourth satellites and a topocentric separation between said third and fourth satellites.

40. The method of claim 39 wherein said step of selecting selects one of said first and fourth satellites having a minimum acceptable topocentric separation from said third satellite.

41. The method of claim 36, further including the steps of inserting a fourth satellite into a non-geostationary Earth orbit in a second predetermined plane different from said first predetermined orbital plane for operation as a portion of said satellite portion of the first satellite communication system to communicate with said first Earth-based communication station, and selecting said first or fourth satellite for communication with said first Earth-based communication station based on a lowest slant range.

42. The method of claim 36, further including the steps of inserting a fourth satellite into a non-geostationary Earth orbit in a second predetermined plane different from said first predetermined orbital plane for operation as a portion of said satellite portion of the first satellite communication system to communicate with said first Earth-based communication station, and selecting said first or fourth satellite for communication with said first Earth-based communication station based on a communication traffic load in said first and fourth satellites.