Intersatellite communications systems

• US 5,825,325 A
• Filed: 09/17/1996
• Issued: 10/20/1998
• Est. Priority Date: 12/21/1995
• Status: Expired due to Term

• Current Assignee: Com Dev Limited (Honeywell International Inc.)
• Original Assignee: Com Dev Limited (Honeywell International Inc.)
• Inventors: O'Donovan, Val, Peach, Robert, Beauchamp, Gary
• Primary Examiner(s): Issing, Gregory C.
• Application Number:
  US08/715,065
• Time in Patent Office: 763 Days
• Field of Search: 342/352, 342/353, 342/354, 455/13.1, 455/13.3, 455/12.1, 370/316, 370/323, 370/325, 370/326
• US Class Current: 342/353
• CPC Class Codes: H04B 7/18521 Systems of inter linked satellites, i.e. inter satellite service for optical links between satellites H04B10/118

Abstract

An improved multi-beam bent-pipe communications satellite system and method includes a subchannel switching processor for extracting and switching subchannels of information to and from a plurality of uplink and downlink beams and an intersatellite link for routing certain of the extracted subchannels to another satellite in the system. The subchannel switching processor preferably employs a partial subchannelization processor that combines a coaxial switching network for switching some of the uplink channels at the channel level with an analog or digital transparent subchannel switching network connected to a portion of the uplink channels for extracting and switching at the subchannel level. The switched subchannels are combined to form channels, and then routed to either the downlink beams (where they are combined with other switched channels), or to the intersatellite link for transmission to another satellite. The system of the present invention could be a constellation of satellites, each satellite in the constellation connected to a plurality of other satellites using a plurality of intersatellite links.

Claims

1. A satellite communications system utilizing a multi-beam bent-pipe architecture including:

a first communications satellite including means for receiving M electromagnetic radiation beams from each of M information sources;

a second communications satellite including means for transmitting N electromagnetic radiation beams to each of N information destinations;

where M and N are natural numbers and the sum of M and N is equal to or greater than 3;

means in said first satellite for transmitting an intersatellite electromagnetic radiation beam to said second satellite;

means in said second satellite for receiving the intersatellite electromagnetic radiation beam from said first satellite;

said intersatellite beam including at least one intersatellite communication channel comprising a plurality of intersatellite subchannels;

each of said M electromagnetic radiation beams including one or more incoming communication channels, at least one of said incoming communication channels in each of said M beams including a plurality of incoming subchannels;

each of said N electromagnetic radiation beams including one or more outgoing communication channels, at least one of said outgoing communication channels in each of said N beams including a plurality of outgoing subchannels;

interbeam switching means in said first satellite for directing the information contents of a plurality of incoming subchannels into respective ones of said plurality of intersatellite subchannels;

interbeam switching means in said second satellite for directing the information contents of said plurality of intersatellite subchannels into respective outgoing subchannels of said N outgoing channels;

whereby information contained in incoming subchannels associated with said M beams received from said M information sources served by said first communications satellite is interbeam-switched and transmitted in outgoing subchannels associated with said N beams transmitted to said N information destinations served by said second satellite.

2. The communications system of claim 1 wherein M equals 1 and N equals 2 and said second satellite contains means to interbeam switch subchannels.

3. The communications system of claim 1 wherein M equals 2 and N equals 1 and said first satellite contains means to interbeam switch subchannels.

25. The satellite communications system of claim 1, wherein at least one of the interbeam switching means comprises a partial subchannelization processor.

26. The satellite communications system of claim 25, wherein the partial subchannelization processor includes channel switching circuitry that interbeam switches the communication channels, and subchannel switching circuitry connected to some, but not all of the channels that selects the subchannel information and interbeam switches the subchannel information.

4. An intersatellite communications system utilizing bent-pipe multi-beam architecture including:

means in a first communications satellite to receive a first incoming beam containing a first incoming channel from a first information source and a second incoming beam containing a second incoming channel from a second information source, said first incoming channel containing a first plurality of incoming subchannels and said second incoming channel containing a second plurality of incoming subchannels, one of said first plurality of incoming subchannels containing first communications information and one of said second plurality of incoming subchannels containing second communications information;

means in said first satellite to combine said subchannels containing said first and second communication information respectively and to place said combined subchannels in a single channel in an electromagnetic beam carrier;

means to transmit said carrier to a second communications satellite;

means in said second satellite to receive said carrier and to separate the combined subchannels in said single channel in said carrier;

means in said second communications satellite to transmit a first outgoing beam containing a first outgoing channel to a first information destination and a second outgoing beam containing a second outgoing channel to a second information destination, said first outgoing channel containing a first plurality of outgoing subchannels and said second outgoing channel containing a second plurality of outgoing subchannels;

means in said second communications satellite to place said first communications information contained in one of said separated subchannels in one of said first plurality of outgoing subchannels;

and means in said second communication satellite to place said second communications information contained in the other of said separated subchannels in one of said second plurality of outgoing subchannels.

5. The system of claim 4 in which said first and second incoming beams are microwave-frequency radio beams from respective terrestrial information sources.

6. The system of claim 4 in which said first incoming beam is a microwave-frequency radio beam from a terrestrial source and said second incoming beam is an electromagnetic beam from a third satellite.

7. The system of claim 6 in which said electromagnetic beam is a microwave-frequency radio beam.

8. The system of claim 6 in which said electromagnetic beam is an optical-wavelength carrier beam.

27. The intersatellite communications system of claim 4, wherein the means to combine comprises a partial subchannelization processor.

28. The satellite communications system of claim 27, wherein the partial subchannelization processor includes channel switching circuitry that interbeam switches the incoming channels, and subchannel switching circuitry connected to some, but not all of the channels that selects the incoming subchannels, interbeam switches the subchannels, and combines the incoming switched subchannels.

9. A multi-beam bent-pipe satellite comprising:

a plurality of receivers for receiving incoming information beams from the ground, wherein the incoming information beams include channels of information, and at least one channel in each of the incoming information beams further includes subchannels of information;

a partial subchannelizing processor connected to the plurality of receivers, said partial subchannelizing processor including a coaxial switching network for switching the channels of information, a subchannel switching network connected to some, but not all of the channels of information that extracts the subchannel information from the incoming information beams and inter-beam switches the subchannel information, and means for combining the switched subchannel information and the switched channel information into a plurality of outgoing information beams;

a plurality of transmitters connected to the outgoing information beams for transmitting the outgoing beams to the ground; and

an intersatellite link connected to at least one of said outgoing information beams, wherein the intersatellite link transmits the outgoing information to another satellite.

10. The bent-pipe satellite of claim 9, wherein each receiver includes a corresponding antenna to capture the incoming information beam.

11. The bent-pipe satellite of claim 9, where the plurality of receivers are connected to a single multi-feed orthogonally polarized antenna which captures all of the incoming information beams.

12. The bent-pipe satellite of claim 9, wherein the subchannelizing processor circuitry that extracts the subchannel information from the incoming information beams includes Surface Acoustic Wave (SAW) filters.

13. The bent-pipe satellite of claim 9, wherein the subchannelizing processor circuitry that interbeam switches the subchannel information comprises a solid-state switching matrix.

14. The bent-pipe satellite of claim 9, wherein the subchannelizing processor circuitry that interbeam switches the subchannel information comprises a transparent digital processor.

15. The bent-pipe satellite of claim 14, wherein the transparent digital processor includes digital filters and a digital switching network.

16. The bent-pipe satellite of claim 9, wherein the incoming information beams are microwave-frequency beams.

17. The bent-pipe satellite of claim 9, wherein the intersatellite link is a microwave-frequency beam.

18. The bent-pipe satellite of claim 9, wherein the intersatellite link is an optical-wavelength beam.

19. The bent-pipe satellite of claim 9, wherein the outgoing information beam connected to the intersatellite link includes subchannel information from more than one incoming information beam.

20. An improved multi-beam bent-pipe satellite of the kind that receives a plurality of incoming beams of information and transmits a plurality of outgoing beams of information, wherein the incoming and outgoing beams include channels of information, and at least one of the channels in each beam further includes subchannels of information, the improvement comprising:

a partial subchannelizing processor including channel switching circuitry that interbeam switches the channels of information, and subchannel switching circuitry in parallel with the channel switching circuitry that selects the subchannel information from the incoming beams, and interbeam switches the subchannel information onto a plurality of outgoing channels, said outgoing channels being further combined with the switched channels into outgoing beams; and

an intersatellite link connected to at least one outgoing beam that includes the subchannel switched information, wherein the intersatellite link transmits the outgoing beam to another satellite.

21. The improved bent-pipe satellite of claim 20, wherein the subchannelizing processor includes SAW filters and a solid-state switching network.

22. The improved bent-pipe satellite of claim 20, wherein the subchannelizing processor includes a transparent digital processor.

23. The improved bent-pipe satellite of claim 22, wherein the transparent digital processor includes digital filters and a digital switching matrix.

24. The improved multi-beam bent-pipe satellite of claim 20, wherein the channel switching circuitry includes a coaxial switching network.