Beamspace-frequency adaptive processing for satellite communications

• US 9,876,562 B2
• Filed: 01/14/2014
• Issued: 01/23/2018
• Est. Priority Date: 01/15/2013
• Status: Expired due to Fees

• Current Assignee: Empire Technology Development LLC (Allied Inventors Management, LLC)
• Original Assignee: Empire Technology Development LLC (Allied Inventors Management, LLC)
• Inventors: Hall, James Stroman
• Primary Examiner(s): Orgad, Edan
• Assistant Examiner(s): Mansoury, Nourali
• Application Number:
  US14/760,951
• Publication Number:
  US 20150341110A1
• Time in Patent Office: 1,470 Days
• CPC Class Codes: H04B 7/0421 utilizing implicit feedback, e.g. steered pilot signals
• CPC Class Codes: H04B 7/0617 for beam forming
• CPC Class Codes: H04B 7/068 using space frequency diversity space-frequency coding H04L1/0606
• CPC Class Codes: H04B 7/18513 Transmission in a satellite or space-based system
• CPC Class Codes: H04B 7/18519 Operations control, administration or maintenance
• CPC Class Codes: H04B 7/2041 Spot beam multiple access

Abstract

Systems and methods to generate virtual spot beams are provided. The system includes a first antenna that provides a first physical spot beam that represents a radio frequency (RF) signal received from a remote source. The system also includes a second antenna that provides a second physical spot beam that represents the RF signal received from the remote source. The system further includes a beam formation module that is communicatively to the first and second antennas and that performs a beam formation operation on the first and second physical spot beams to generate one or more virtual spot beams.

Claims

1. A satellite system to generate a plurality of beamformed outputs from one or more input antenna signals, the satellite system comprising:

a plurality of channel breakout modules configured to receive respective unique input antenna signals that represent channels of a common radio frequency (RF) signal received from a remote source and to break each unique input antenna signal into a plurality of channel components;

a switch module coupled to the plurality of channel breakout modules and configured to receive the plurality of channel components from the plurality of channel breakout modules and to match equivalent channel components from each of the unique input antenna signals; and

a plurality of beam formation operation modules coupled to the switch module, wherein each beam formation operation module is configured to receive a set of equivalent channel components that have been matched by the switch module and to perform a beam formation operation on the set of equivalent channel components to generate a beamformed output for the set of equivalent channel components.

2. The satellite system of claim 1, further comprising:

one or more antennas coupled to at least one of the plurality of channel breakout modules and configured to receive one of the unique input antenna signals from the remote source.

3. The satellite system of claim 2, wherein the one or more antennas include phased array antennas.

4. The satellite system of claim 2, further comprising:

a down converter coupled to the one or more antennas and configured to down convert each of the unique input antenna signals to a digital baseband signal prior to the unique input antenna signals being received by the plurality of channel breakout modules.

5. The satellite system of claim 1 further comprising:

a reconstruction module coupled to the plurality of beam formation operation modules and configured to receive the generated beamformed output from each beam formation operation module and to place the plurality of beamformed outputs into a form that is usable by other components of the satellite system, wherein the plurality of beamformed outputs include digital baseband signals.

6. The satellite system of claim 1, wherein the beam formation operation comprises a space-frequency adaptive processing operation.

7. The satellite system of claim 1, wherein each beam formation operation module is configured to perform the beam formation operation in a frequency domain.

8. The satellite system of claim 7, wherein each beam formation operation module is configured to perform multiple frequency-specific weighted summations as part of the beam formation operation in the frequency domain.

9. The satellite system of claim 8, wherein each beam formation module is configured to perform each weighted summation by use of weight coefficients that are obtained using an adaptive beaming formation operation.

10. The satellite system of claim 9, wherein the adaptive beaming formation operation includes one of a minimum power distortionless response or a minimum variance distortionless response.

11. The satellite system of claim 9, wherein each beam formation operations module is configured to use steerage vectors to compute the weight coefficients, and wherein the weight coefficients are determined based on the input antenna signals.

12. The satellite system of claim 1, wherein the plurality of beam formation operation modules comprises:

a plurality of first modules configured to receive the set of equivalent channel components that have been matched by the switch module and to break each channel component into a plurality of frequency components that comprise each channel component;

a plurality of frequency-specific beamformer modules coupled to a plurality of second modules and configured to receive a given one of the plurality of frequency components from each channel component and to perform the beam formation operation; and

a second module coupled to the plurality of frequency-specific beamformer modules and configured to receive outputs from each of the plurality of frequency-specific beamformer modules and to combine the outputs to generate the beamformed output.

13. The satellite system of claim 12, wherein the plurality of first modules include fast Fourier transform (FFT) modules configured to convert the equivalent channel components into frequency domain components.

14. The satellite system of claim 12, wherein the second module includes an inverse fast Fourier transform (iFFT) module.

15. A method to generate a plurality of virtual beamformed outputs from one or more input antenna signals, the method comprising:

receiving a plurality of physical input antenna signals that represent a common radio frequency (RF) signal from a remote source;

dividing the physical input antenna signals into a plurality of channel components;

matching equivalent channel components from each input antenna signal with like channel components; and

performing a beam formation operation on the equivalent channel components to generate the plurality of virtual beamformed outputs for each channel component.

16. The method of claim 15, wherein the generation of the plurality of virtual beamformed outputs includes generation of digital baseband signals.

17. The method of claim 15, further comprising:

combining the plurality of virtual beamformed outputs into one or more new physical antenna signals that are configurable to be further processed.

18. The method of claim 15, wherein the beam formation operation is performed in a frequency domain, wherein the beam formation operation in the frequency domain comprises multiple frequency-specific weighted summations, wherein each weighted summation includes weight coefficients that are obtained using an adaptive beaming formation operation, wherein the adaptive beaming formation operation includes a minimum power distortionless response, wherein the input antenna signal is used to determine steerage vectors, and wherein the steerage vectors are used to compute the weight coefficients.

19. The method of claim 15, wherein the beam formation operation includes a minimum variance distortionless response.

20. The method of claim 15, further comprising:

dividing each channel component into a plurality of frequency components that comprise each channel component;

subjecting each frequency component to the beam formation operation; and

combining each of the plurality of frequency components that have been subjected to the beam formation operation to generate a virtual beamformed output.

21. A system to generate a plurality of virtual spot beams from one or more physical spot beams, the system comprising:

a first antenna configured to provide a first physical spot beam that represents an radio frequency (RF) signal received from a remote source;

a second antenna configured to provide a second physical spot beam that represents the RF signal received from the remote source; and

a beam formation module communicatively coupled to the first and second antennas and configured to perform a beam formation operation on the first and second physical spot beams to generate one or more virtual spot beams.

22. The system of claim 21, wherein the first and second antennas include phase array antennas.

23. The system of claim 21, wherein the beam formation operation comprises a space-frequency adaptive processing operation, wherein the beam formation module is configured to perform the beam formation operation in a frequency domain, wherein the beam formation module is configured to perform multiple frequency-specific weighted summations as part of the beam formation operation in the frequency domain, wherein the beam formation module is configured to perform each weighted summation by use of weight coefficients that are obtained by use of an adaptive beaming formation operation, wherein the adaptive beaming formation operation includes a minimum power distortionless response, wherein the beam formation module is configured to use steerage vectors to compute the weight coefficients, wherein the weight coefficients are determined based on the first and second physical spot beams, and wherein the first and second physical spot beams include digital baseband signals prior to being received by the beam formation module.

24. The system of claim 21, wherein the beam formation operation includes a minimum variance distortionless response.

25. The system of claim 21, wherein the beam formation module comprises:

a plurality of first modules configured to break the first and second physical spot beams into a plurality of frequency components;

a plurality of frequency-specific beam formation modules coupled to the plurality of first modules and configured to receive a given one of the frequency components and to perform the beam formation operation; and

a second module coupled to the plurality of frequency-specific beam formation modules and configured to receive outputs from each of the plurality of frequency-specific beam formation modules and to combine the outputs to generate the one or more virtual spot beams.

26. A method to generate a plurality of virtual spot beams from one or more physical spot beams, the method comprising:

receiving a common radio frequency (RF) signal from one or more remote sources at a plurality of antennas;

providing a first physical spot beam from a first antenna of the plurality of antennas to a beam formation module, wherein the first physical spot beam is representative of all common RF signals;

providing at least a second physical spot beam from a second antenna of the plurality of antennas to the beam formation module, wherein the second physical spot beam is also representative of the common RF signals; and

performing a beam formation operation by the beam formation module to generate one or more virtual spot beams.

27. The method of claim 26, wherein providing the first physical spot beam from the first antenna and providing the at least second physical spot beam from the second antenna comprise providing the first physical spot beam and the at least second physical spot beam from phase array antennas.

28. The method of claim 26, wherein the beam formation operation is performed in a frequency domain, wherein the beam formation operation in the frequency domain comprises multiple frequency-specific weighted summations, wherein each weighted summation involves weight coefficients that are obtained using an adaptive beaming formation operation, wherein the adaptive beaming formation operation includes a minimum power distortionless response, wherein steerage vectors are used to compute the weight coefficients, and wherein the weight coefficients are determined based on the first and the at least second physical spot beams.

29. The method of claim 26, wherein the beam formation operation includes a minimum variance distortionless response.

30. A method to generate a new spot beam, the method comprising:

receiving a first spot beam from a first antenna, wherein the first spot beam comprises a plurality of first communication channels to communicate data from a remote source;

receiving a second spot beam from a second antenna, wherein the second spot beam is different from the first spot beam, and wherein the second spot beam comprises a plurality of second communication channels to communicate data from the remote source;

dividing the first spot beam into first communication channel components, wherein each first communication channel component comprises a plurality of first frequency components;

dividing the second spot beam into second communication channel components, wherein each second communication channel component comprises a plurality of second frequency components;

matching the first communication channel components with corresponding second communication channel components;

performing a beam formation operation on each first frequency component and second frequency component of each corresponding matched first and second communication channel components, wherein the beam formation operation includes filtering signal components from each of the first and second frequency components; and

combining the output of the beam formation operation of each first frequency component and second frequency component to generate the new spot beam, wherein the new spot beam comprises one or more signal channels and is substantially more focused on a target than the first and second spot beams.

31. The method of claim 30, wherein the beam formation operation is performed in a frequency domain, wherein the beam formation operation in the frequency domain comprises multiple frequency-specific weighted summations, wherein each weighted summation includes weight coefficients that are obtained using an adaptive beaming formation operation, wherein the adaptive beaming formation operation includes a minimum power distortionless response, wherein steerage vectors are used to compute the weight coefficients, and wherein the weight coefficients are determined based on the first and the second spot beams.

32. The method of claim 30, wherein the beam formation operation includes a minimum variance distortionless response.

33. The method of claim 30, wherein receiving the first spot beam from the first antenna and receiving the second spot beam from the second antenna comprise receiving the first spot beam and the second spot beam from phase array antennas.