Satellite communications system using transceiver arrays

1. A system comprising:

a first transceiver circuit, a second transceiver circuit, and a first data bus, wherein the first transceiver circuit and the second transceiver circuit are unsynchronized, and wherein:

said first transceiver circuit is configured to:

receive a first plurality of signals from a first plurality of antenna elements;

beamform said first plurality of signals to generate a first beamformed signal;

downconvert said first beamformed signal as part of generation of a first downconverted beamformed signal; and

transmit said first downconverted beamformed signal onto said first data bus; and

said second transceiver circuit is configured to:

receive a second plurality of signals from a second plurality of antenna elements;

beamform said second plurality of signals to generate a second beamformed signal;

downconvert said second beamformed signal as part of generation of a second downconverted beamformed signal;

receive said first downconverted beamformed signal via said first data bus; and

combine said first downconverted beamformed signal and said second downconverted beamformed signal to generate a combined signal for demodulation, wherein said first downconverted beamformed signal is combined with said second downconverted beamformed signal according to a time offset that is determined from a correlation of said first downconverted beamformed signal against said second downconverted beamformed signal.

2. The system of claim 1 , wherein:

a first subset of a plurality of beamforming coefficients are used for said beamforming of said plurality of signals from said first plurality of antenna elements;

a second subset of said plurality of beamforming coefficients are used for said beamforming of said plurality of signals from said second plurality of antenna elements; and

said beamforming coefficients are such that a signal from a first source that is incident on both said first plurality of antenna elements and said second plurality of antenna elements is reinforced, and a signal from a second source that is incident on both said first plurality of antenna elements and said second plurality of antenna elements is suppressed.

3. The system of claim 2 , wherein:

said first source is a satellite;

one or both of said first transceiver circuit and said second transceiver circuit is operable to:

recover an identifier of said satellite carried in said plurality of signals; and

determine a location of said satellite relative to said first plurality of antenna elements based on said identifier.

4. The system of claim 3 , wherein said one or both of said first transceiver circuit and said second transceiver is operable to:

determine an angle of incidence of said signal from said first source based on said location of said satellite; and

compensate one or more local oscillators and/or one or more of said plurality of beamforming coefficients based on said determined angle of incidence.

5. The system of claim 3 , wherein said determination of said location of said satellite comprises communication with a satellite tracking database.

6. The system of claim 1 , wherein each of said first transceiver circuit and said second transceiver circuit comprises a CMOS die with an on-chip power amplifier.

7. The system of claim 1 , wherein said first transceiver circuit comprises an expansion interface for coupling to a third transceiver circuit.

8. The system of claim 1 , comprising a second data bus and a third transceiver circuit, wherein:

said third transceiver circuit is configured to:

receive a third plurality of signals from a third plurality of antenna elements;

beamform said third plurality of signals to generate a third beamformed signal;

downconvert said third beamformed signal to generate a third downconverted beamformed signal; and

transmit said first downconverted beamformed signal onto said second data bus;

said first transceiver circuit is configured to receive said third downconverted beamformed signal via said second data bus; and

said generation of said first downconverted beamformed signal comprises combining of:

a signal resulting from said downconversion said first beamformed signal; and

said third downconverted beamformed signal.

9. The system of claim 1 , wherein said first plurality of antennas comprises a plurality of molded-plastic horn antennas with a metal coating.

10. The system of claim 1 , comprising a third plurality of antenna elements, wherein:

said first transceiver comprises a plurality of receive front end circuits coupled to said first plurality of antenna elements for said reception of said first plurality of signals;

said first transceiver comprises a plurality of transmit front end circuits coupled to said third plurality of antenna elements.

11. The system of claim 1 , wherein:

a plurality of receive front end circuits are not coupled to a third plurality of antenna elements; and

said plurality of transmit front end circuits are not coupled to said first plurality of antenna elements.

12. A method comprising:

receiving, by a first transceiver circuit, a plurality of signals from a corresponding first plurality of antenna elements;

beamforming, by said first transceiver circuit, said plurality of signals to generate a first beamformed signal;

downconverting, by said first transceiver circuit, said first beamformed signal as part of generating a first downconverted beamformed signal;

receiving, by a second transceiver circuit, a plurality of signals from a corresponding second plurality of antenna elements, wherein the first transceiver circuit and the second transceiver circuit are unsynchronized;

beamforming, by said second transceiver circuit, said plurality of signals to generate a second beamformed signal;

downconverting, by said second transceiver circuit, said second beamformed signal as part of generating a second downconverted beamformed signal;

conveyeing, by said first transceiver circuit via a data bus, said first downconverted beamformed signal to said second transceiver circuit; and

combining, by said second transceiver circuit, said first downconverted beamformed signal and said second downconverted beamformed signal to generate a combined signal to be demodulated, wherein said combining of said first downconverted beamformed signal and said second downconverted beamformed signal is based on to a time offset that is determined from a correlation of said first downconverted beamformed signal against said second downconverted beamformed signal.

13. The method of claim 12 , comprising calculating a plurality of beamforming coefficients wherein:

a first subset of said beamforming coefficients are used for said beamforming said plurality of signals from said first plurality of antenna elements;

a second subset of said beamforming coefficients are used for said beamforming said plurality of signals from said second plurality of antenna elements; and

said beamforming coefficients are such that electromagnetic energy from a first source that is incident on both said first plurality of antenna elements and said second plurality of antenna elements is reinforced, and electromagnetic energy from a second source that is incident on both said first plurality of antenna elements and said second plurality of antenna elements is suppressed.

14. The method of claim 12 , wherein a first source is a satellite and comprising:

recovering, by one or both of said first transceiver circuit and said second transceiver circuit, an identifier of said satellite carried in said plurality of signals; and

determining, by said one or both of said first transceiver circuit and said second transceiver circuit, a location of said satellite relative to said first plurality of antennas based on said identifier.

15. The method of claim 14 , comprising:

determining, by said one or both of said first transceiver circuit and said second transceiver circuit, an angle of incidence of said signal from said first source based on said location of said satellite; and

compensating, by said one or both of said first transceiver circuit and said second transceiver circuit, one or more local oscillators and/or one or more of said plurality of beamforming coefficients based on said determined angle of incidence.

16. The method of claim 14 , wherein said determining said location of said satellite comprises communicating with a satellite tracking database.

17. The method of claim 12 , wherein each of said first transceiver circuit and said second transceiver circuit comprises a CMOS die with an on-chip power amplifier.

18. The method of claim 13 , wherein said first transceiver circuit comprises an expansion interface for coupling to a third transceiver circuit.

19. The method of claim 12 , comprising:

receiving, by a third transceiver circuit, a third plurality of signals from a third plurality of antenna elements;

beamforming, by said third transceiver circuit, said third plurality of signals to generate a third beamformed signal;

downconverting, by said third transceiver circuit, said third beamformed signal as part of generating a third downconverted beamformed signal;

transmitting, by said third transceiver circuit, said first downconverted beamformed signal onto a second data bus;

receiving, by said first transceiver circuit, said third downconverted beamformed signal via said second data bus; and

as part of said generating said first downconverted beamformed circuit by said first transceiver circuit, combining:

a signal resulting from said downconverting said first beamformed signal; and

said third downconverted beamformed signal.

20. The method of claim 12 , wherein said first plurality of antennas comprises a plurality of molded-plastic horn antennas with a metal coating.

21. The method of claim 12 , comprising dynamically powering up and powering down said first transceiver circuit based on a power consumption budget.

22. The method of claim 12 , comprising dynamically powering up and powering down said first transceiver circuit based on a receiver performance metric.