Methods and systems for satellite communications employing ground-based beam forming with spatially distributed hybrid matrix amplifiers

• US 9,014,619 B2
• Filed: 05/22/2007
• Issued: 04/21/2015
• Est. Priority Date: 05/30/2006
• Status: Active Grant

• Current Assignee: ATC Technology Corporation (FedEx Corporation)
• Original Assignee: ATC Technology Corporation (FedEx Corporation)
• Inventors: Benjamin, Ted, Griffin, Matthew, Chapman, William W.
• Primary Examiner(s): Pan, Yuwen
• Assistant Examiner(s): Tran, Paul P
• Application Number:
  US11/751,701
• Publication Number:
  US 20070281612A1
• Time in Patent Office: 2,891 Days
• Field of Search: 455/12.1, 455/3.04, 455/3.05, 455/13.1, 455/13.3, 455/13.4, 455/427, 455/13.2, 455/63.1, 455/456.1, 455/11.1, 455/15, 455/39, 455/63.4, 455/67.15, 455/67.16, 455/73, 455/101, 455/102, 455/121, 455/1, 455/29, 455/269, 455/273, 455/277.1, 455/424, 455/436, 455/446, 455/447, 455/450, 455/456.2, 455/458, 455/507, 455/517, 455/522, 455/525, 455/553.1, 455/561, 455/562.1, 455/575.7, 333/2, 333/124.D, 333/124.R, 333/117, 333/149, 333/295, 342/352, 342/373, 342/442, 342/70, 342/140, 342/157, 342/158, 342/202, 342/354, 342/356, 342/368, 342/371, 342/372, 342/159, 342/161, 342/367, 342/374, 342/375, 342/377, 342/378, 342/4, 342/24, 370/18, 370/104, 370/315, 370/316, 370/325, 370/326, 370/328, 370/319, 370/480, 370/535, 370/334, 370/343, 370/203, 370/252, 370/278, 370/280, 370/312, 370/321, 370/329, 370/335, 370/336, 370/337, 370/338, 370/345, 370/411, 375/1, 375/267, 375/140, 375/144, 375/148, 375/232, 375/262, 375/292, 375/296, 375/298, 375/299, 375/346, 375/354, 330/2, 330/124.D, 330/124.R, 330/117, 330/149, 330/286, 330/295, 275/1, 275/267, 275/316, 343/700.MS, 343/705, 343/711, 343/754, 343/755, 343/756, 343/757, 343/770, 343/771, 343/775, 343/781.CA, 343/78, 343/6, 343/792.5, 343/836, 343/844, 343/853, 343/876, 343/893
• US Class Current: 455/12.1
• CPC Class Codes: H04B 7/18515 Transmission equipment in satellites or space-based relays
• CPC Class Codes: H04B 7/2041 Spot beam multiple access

Abstract

A satellite communications system includes a satellite configured to communicate with terminals, a station configured to communicate signals intended for the terminals to the satellite via a plurality of feeder links and a beamformer including an input multi-port hybrid matrix (MPHM) and a complementary output MPHM in a signal path with the plurality of feeder links. The output MPHM is positioned at the satellite and coupled to the input MPHM via the plurality of feeder links. For example, the input MPHM may be positioned at a ground-based satellite gateway. The input and output MPHMs may be configured to implement fully populated signal transformation matrices that collectively provide a substantially diagonal signal transformation matrix.

Claims

1. A satellite communications system comprising:

a satellite configured to communicate with terminals;

a station configured to communicate signals intended for the terminals to the satellite via a plurality of feeder links; and

a beamformer comprising an input multi-port hybrid matrix (MPHM) and a complementary output MPHM in a signal path with the plurality of feeder links, the output MPHM positioned at the satellite and coupled to the input MPHM via the plurality of feeder links.

2. The system of claim 1, wherein the input and output MPHMs implement fully populated signal transformation matrices that collectively provide a substantially diagonal signal transformation matrix.

3. The system of claim 1, wherein the satellite comprises a partial hybrid matrix amplifier (HMA) comprising the output MPHM and a plurality of amplifiers coupled to respective input ports thereof.

4. The system of claim 1, further comprising:

a feeder link compensation unit in the signal path; and

a calibration unit configured to adjust the feeder link compensation unit responsive to feedback from a receiving station receiving a calibration signal injected into the signal path.

5. The system of claim 4, further comprising a calibration signal injection unit configured to inject the calibration signal into the signal path on an input MPHM side of the feeder links.

6. The system of claim 4, further comprising the receiving station.

7. The system of claim 4, where the calibration unit comprises a first calibration unit and wherein the system further comprises:

an antenna geometry compensation unit coupled to the input MPHM; and

a second calibration unit configured to adjust the antenna geometry compensation unit responsive to feedback from a receiving station receiving a calibration signal injected into the signal path.

8. The system of claim 7, further comprising a calibration signal injection unit configured to inject the calibration signal into the signal path on an input MPHM side of the feeder links.

9. The system of claim 7, further comprising the receiving station.

10. The system of claim 1, wherein the input and output MPHMs comprise respective Butler matrices.

11. The system of claim 1, wherein the input MPHM is positioned at a ground-based satellite gateway.

12. A communications satellite comprising:

a feeder link antenna configured to receive signals from a station via a plurality of feeder links;

a phased array antenna configured to communicate the received signals to terminals; and

a processing unit coupled between the feeder link antenna and the phased array antenna and comprising an output MPHM configured to complement an input MPHM coupled to the satellite via the plurality of feeder links.

13. The satellite of claim 12, wherein the input and output MPHMs implement fully populated signal transformation matrices and provide a composite effect substantially corresponding to a diagonal signal transformation matrix.

14. The satellite of claim 12, wherein the processing unit comprises a partial hybrid matrix amplifier (HMA) comprising the output MPHM and a plurality of power amplifiers coupled to respective input ports thereof.

15. The satellite of claim 14, wherein the processing unit further comprises:

a plurality of low noise amplifiers (LNAs) having inputs coupled to respective elements of the feeder link antenna;

a demultiplexer having inputs coupled to outputs of the LNAs;

a channelizer/element signal combiner having inputs coupled to outputs of the demultiplexer and outputs coupled to inputs of the power amplifiers; and

a plurality of diplexers coupling respective outputs of the output MPHM to respective elements of the phased array antenna.

16. The satellite of claim 12, wherein the output MPHM comprises a Butler matrix.

17. An apparatus for supporting satellite communications between a satellite and terminals, the apparatus comprising:

a feeder link antenna configured to communicate signals intended for the terminals to the satellite via a plurality of feeder links; and

a signal processing unit comprising an input multi-port hybrid matrix (MPHM) configured to complement an output MPHM positioned at the satellite.

18. The apparatus of claim 17, wherein the input and output MPHMs implement fully populated signal transformation matrices and provide a composite effect substantially corresponding to a diagonal signal transformation matrix.

19. The apparatus of claim 17, wherein the signal processing unit further comprises a feeder link compensation unit in a signal path of the input MPHM, the output MPHM and the intervening feeder links and wherein the apparatus further comprises a calibration unit configured to adjust the feeder link compensation unit responsive to feedback from a receiving station receiving a calibration signal injected into the signal path.

20. The apparatus of claim 19, wherein the signal processing unit further comprises a calibration signal injection unit configured to inject the calibration signal into the signal path on an input MPHM side of the feeder links.

21. The apparatus of claim 19, where the calibration unit comprises a first calibration unit, wherein the signal processing unit further comprises an antenna geometry compensation unit in the signal path and wherein the apparatus further comprises a second calibration unit configured to adjust the antenna geometry compensation unit responsive to feedback from a receiving station receiving a calibration signal injected into the signal path.

22. The apparatus of claim 21, further comprising a calibration signal injection unit configured to inject the calibration signal into the signal path on an input MPHM side of the feeder links.

23. The apparatus of claim 17, wherein the input MPHM comprises a Butler matrix.

24. The apparatus of claim 17 positioned at a ground-based satellite gateway.

25. A method of operating a satellite communications system comprising a satellite configured to communicate with terminals and a station configured to communicate signals intended for the terminals to the satellite via a plurality of feeder links, the method comprising:

beam forming for communications between the satellite and terminals using an HMA including an output MPHM positioned at the satellite and a complementary input MPHM coupled to the output MPHM via the plurality of feeder links.

26. The method of claim 25, wherein the input and output MPHMs implement fully populated signal transformation matrices that collectively provide a substantially diagonal signal transformation matrix.

27. The method of claim 25, further comprising adjusting a feeder link compensation unit in a signal path of the HMA responsive to feedback from a receiving station receiving a calibration signal injected into the signal path.

28. The method of claim 27, further comprising adjusting an antenna geometry compensation unit coupled to the input MPHM responsive to feedback from a receiving station receiving a calibration signal injected into the signal path.

29. The method of claim 25, where the input and output MPHMs comprise respective Butler matrices.

30. The method of claim 25, wherein the input MPHM is positioned at a ground-based satellite gateway.