Multi-beam satellite network to maximize bandwidth utilization

• US 7,792,070 B1
• Filed: 08/08/2007
• Issued: 09/07/2010
• Est. Priority Date: 04/13/2007
• Status: Active Grant

• Current Assignee: Maxar Space LLC (Galileo Parent, Inc.)
• Original Assignee: Space Systems/Loral Incorporated (Loral Space and Communications Incorporated)
• Inventors: Burr, Douglas
• Primary Examiner(s): LY, ANH VU H
• Application Number:
  US11/891,086
• Time in Patent Office: 1,126 Days
• Field of Search: None
• US Class Current: 370/316
• CPC Class Codes: H04B 7/18582 Arrangements for data linking, i.e. for data framing, for error recovery, for multiple access

Abstract

A communications network (100) for maximizing bandwidth utilization. An embodiment of the invention comprises a spacecraft (11), at least one gateway (12) communicatively coupled to the spacecraft (11) by a feeder link (13) operating within at least one selected frequency band within a bandwidth, at least one user terminal (16) communicatively coupled to the spacecraft (11) by a user link (17), the user link (17) operable at any frequency band within the bandwidth without regard to polarization; and, the communications network (100) adapted to provide for simultaneous operation of at least a portion of the feeder link (13) and a portion of the user link (17) at a common polarization and frequency band within the bandwidth.

Claims

1. A communications network, comprising:

a spacecraft;

at least one gateway communicatively coupled to the spacecraft by a feeder link operating within at least one selected first sub-band of frequencies within a bandwidth;

a first user terminal communicatively coupled to the spacecraft by a first user link, said first user link operable at any frequency band within said first sub-band;

a second user terminal communicatively coupled to the spacecraft by a second user link, said second user link operable at any frequency band within a second sub-band of frequencies within the bandwidth, said second sub-band having no frequency in common with the first sub-band, wherein the communications network is adapted to provide for simultaneous operation of at least a portion of the feeder link and at least a portion of the first user link at a common polarization and frequency within the bandwidth; and

an antenna subsystem disposed on the spacecraft, said antenna subsystem providing a first antenna beam pattern associated with the first user link, and a second antenna beam pattern associated with the second user link, said first and second antenna beam patterns defining respective first and second service regions, wherein every gateway is located within the second service region.

2. The communications network of claim 1, wherein at least a portion of the first user link operates at a common polarization and frequency as at least a portion of the feeder link.

3. The communications network of claim 1, wherein the first and second sub-band together encompass substantially all of the bandwidth.

4. The communications network of claim 1, wherein at least one gateway is located proximate to and communicatively coupled with an Internet backbone.

5. The communications network of claim 1, wherein the spacecraft is a satellite operable in geostationary orbit.

6. The communications network of claim 1, wherein the spacecraft is a satellite operable in non-geostationary orbit.

7. The communications network of claim 1, wherein the user links and the feeder link are operable at Ka band.

8. The communications network of claim 1, wherein at least one antenna beam pattern is configured to provide a plurality of individual spot beams.

9. The communications network of claim 8, wherein at least one antenna beam pattern is configured to provide for frequency re-use in spatially isolated spot beams.

10. The communications network of claim 8, wherein frequency re-use is maximized according to a four color re-use plan wherein a color represents a combination of a frequency sub-band and an antenna polarization.