SYSTEM AND METHOD FOR SATELLITE COMMUNICATION

• US 20100201566A1
• Filed: 04/16/2010
• Published: 08/12/2010
• Est. Priority Date: 10/18/2007
• Status: Abandoned Application

• Current Assignee: O3b Networks Ltd. (SES SA)
• Original Assignee: O3b Networks Ltd. (SES SA)
• Inventors: Wyler, Gregory Thane
• Application Number:
  US12/761,839
• Publication Number:
  US 20100201566A1
• Time in Patent Office: Days
• US Class Current: 342/354
• 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 7/18513 Transmission in a satellite or space-based system

Abstract

A system and method are disclosed which may include providing at least one satellite having a plurality of beamformers configured to provide a plurality of respective beams having a plurality of different respective fixed pitch angles about an axis of the satellite; causing the at least one satellite to move around the earth along a non-geostationary orbit; establishing a data communication path between a first of the beamformers on the satellite and a communication target, the data communication path having a satellite end at the first beamformer and an target end at the communication target; shifting the satellite end of the data communication path through a succession of the beamformers as the satellite moves along its orbit; and at least substantially reducing an amount of RF wave energy directed to beamformers of the plurality of beamformers not forming part of the data communication path.

Claims

1. A method, comprising:

providing at least one satellite having a plurality of beamformers configured to provide a plurality of respective beams having a plurality of different respective fixed pitch angles about an axis of the satellite;

causing the at least one satellite to move around the earth along a non-geostationary orbit;

establishing a data communication path between a first of the beamformers on the satellite and a communication target, the data communication path having a satellite end at the first beamformer and an target end at the communication target;

shifting the satellite end of the data communication path through a succession of the beamformers as the satellite moves along its orbit; and

at least substantially reducing an amount of RF wave energy directed to beamformers of the plurality of beamformers not forming part of the data communication path.

2. The method of claim 1 wherein the plurality of respective beams have a plurality of different respective fixed pitch angles about a lateral axis of the satellite.

3. The method of claim 1 wherein the communication target is a first antenna, at an Earth station, configured to communicate with the satellite along a selected segment of the orbit of the satellite, the first antenna being an Earth end of the data communication path.

4. The method of claim 1 wherein the communication target is another satellite.

5. The method of claim 1 wherein the at least substantially reducing step comprises:

not directing any RF wave energy to beamformers of the plurality of beamformers not forming part of the data communication path.

6. The method of claim 1 wherein the satellite further includes at least one reflector operable to reflect RF wave energy from the plurality of beamformers toward the communication target and to reflect RF wave energy from the communication target toward the plurality of beamformers.

7. The method of claim 1 wherein the orbit is at least substantially equatorial.

8. The method of claim 1 wherein the latitude of the orbit remains between −

10 and +10 degrees latitude.

9. The method of claim 1 wherein the latitude of the orbit remains between −

5 and +5 degrees latitude.

10. The method of claim 1 wherein the altitude of the satellite orbit is between 600 km and 30,000 km.

11. The method of claim 1 wherein the altitude of the satellite orbit is between 5,000 km and 10,000 km.

12. The method of claim 1 wherein the altitude of the satellite orbit is between 7,000 km and 8,000 km.

13. The method of claim 3 further comprising:

the first antenna at the earth station tracking the satellite using a steering mechanism to cause the first antenna to substantially continuously point toward the satellite.

14. The method of claim 3 further comprising:

the first antenna quasi-tracking the satellite by transferring the earth end of the data communication path through a succession of fixed antenna beams, wherein each said antenna beam has a substantially fixed orientation with respect to the surface of the Earth.

15. The method of claim 1 further comprising directing RF wave energy to the beamformer, of the plurality of beamformers, serving as the satellite end of the data communication path.

16. The method of claim 3 further comprising:

maintaining the data communication path between the first antenna and the first beamformer over a range of satellite movement corresponding to a communication alignment range between the beam from the first beamformer and the first antenna.

17. The method of claim 16 further comprising:

commencing communication between the first antenna and the first beamformer when the first antenna and the beam generated by the first beamformer reach an initial communication alignment boundary during movement of the satellite along its orbit; and

concluding communication between the first antenna and the first beamformer when the first antenna and the beam generated by the first beamformer reach a final communication alignment boundary during movement of the satellite along its orbit.

18. The method of claim 17 wherein communication power between the first antenna, at the earth station, and the first beamformer reaches a peak at centroid-to-centroid alignment between the first antenna and the first beamformer.

19. The method of claim 18 wherein the first antenna communicates with the first beamformer while the communication power along the data communication path is equal to or greater than one half the peak communication power.

20. The method of claim 16 wherein the shifting step comprises:

transferring the satellite end of the data communication path from the first beamformer to a second beamformer of the plurality of beamformers once a second antenna at the earth station and a beam from the second beamformer enter into communication alignment range.

21. The method of claim 20 wherein the transferring step comprises:

redirecting RF wave energy, originating from an amplifier on the satellite, from the first beamformer to the second beamformer.

22. The method of claim 21 wherein the redirecting step is performed using a waveguide switch.

23. The method of claim 21 further comprising repeating the steps of transferring and redirecting for the plurality of the beamformers on the satellite so as to maintain operation of the data communication path between the satellite and the earth station throughout the movement of the satellite through the selected segment of the orbit of the satellite.

24. An apparatus, comprising

a satellite having a plurality of beamformers configured to provide a plurality of respective beams having a plurality of different respective fixed pitch angles about an axis of the satellite;

and

a controller operable to direct a data communication path through a first beamformer of the plurality of beamformers,

wherein the controller is further operable to shift the data communication path through a succession of the beamformers.

25. The apparatus of claim 24 wherein the plurality of different respective fixed pitch angles are about a lateral axis of the satellite.

26. The apparatus of claim 24 wherein the controller is operable to redirect the data communication path from the first beamformer to a second beamformer of the plurality of beamformers upon detecting a decline in communication power along the data communication path.

27. The apparatus of claim 24 further comprising an amplifier able to supply RF wave energy to one or more of the plurality of beamformers, wherein the controller is operable to select at least one beamformer, of the plurality of beamformers, to direct the RF wave energy to.

28. The apparatus of claim 24 wherein the plurality of beamformers are disposed in an array on the satellite, having a plurality of rows,

wherein each beamformer row includes a sequence of beamformers configured to illuminate footprints on the Earth over a range of longitude but with substantially similar latitude;

and

wherein the plurality of rows are configured to illuminate respective groups of footprints at a plurality of different respective latitudes.

29. A method, comprising:

providing a first constellation of satellites within a satellite system;

providing at least one additional constellation of satellites to provide a plurality of satellite constellations within the satellite system;

enabling adjacent ones of the satellites in the satellite system to communicate with a single earth station; and

wherein at least one of the satellites in each said constellation has a plurality of beamformers configured to provide a plurality of respective beams having a plurality of different respective fixed pitch angles about a lateral axis of the satellite, and

a controller operable to direct a data communication path through a first beamformer of the plurality of beamformers,

wherein the controller is further operable to shift the data communication path through a succession of the beamformers.

30. The method of claim 29 further comprising:

the adjacent satellites communicating with the earth station employing the same transmission frequency.

31. The method of claim 29 further comprising:

dedicating at least selected ones of the beamformers in the satellite system substantially completely to one of;

transmission; and

reception.

32. The method of claim 30 further comprising:

supplementing the satellite system in a given state with at least one further constellation to provide a modified satellite system without disrupting an operation of the satellite system in the given state.

33. The method of claim 31 further comprising:

dedicating at least selected ones of the satellites in the satellite system substantially completely to one of;

transmission; and

reception.

34. A method, comprising:

conducting a data communication session between a first computing entity and a second computing entity over a communication network,

wherein at least a portion of the data transferred over the communication network during the data communication session is transmitted over a satellite system,

and wherein at least one of the satellites in said satellite system has a plurality of beamformers configured to provide a plurality of respective beams having a plurality of different respective fixed pitch angles about an axis of the satellite; and

a controller operable to direct a data communication path through a first beamformer of the plurality of beamformers,

and wherein the controller is further operable to shift the data communication path through a succession of the beamformers.