Granted Patent B2

US 12,212,403 · App. 17/704,784 · Granted Jan 28, 2025

Inventors: Kumud Patel (Clarksburg, MD); Jack Edwin Lundstedt, Jr. (Monrovia, MD); Walter Kepley (Gaithersburg, MD)

Assignee: Hughes Network Systems, LLC

H04B7/18519

Abstract

Claims (60)

1. A satellite gateway comprising:

a first radiofrequency chain configured to transmit or receive information on a first channel;

a second radiofrequency chain configured to transmit or receive information on a second channel;

a third radiofrequency chain configured to operate in a standby mode while the first radiofrequency chain and second radiofrequency chain are operational;

radiofrequency switches configured to (i) switch between coupling the first radiofrequency chain and the third radiofrequency chain to a first antenna feed port for the first channel, and (ii) switch between coupling the second radiofrequency chain and the third radiofrequency chain to a second antenna feed port for the second channel; and

a controller configured to monitor a status of the radiofrequency chains, to detect failures of the radiofrequency chains based on the monitoring, and to instruct the radiofrequency switches to (i) couple the third radiofrequency chain to the first antenna feed port when a failure is detected for the first radiofrequency chain, and (ii) couple the third radiofrequency chain to the second antenna feed port when a failure is detected for the second radiofrequency chain.

2. The satellite gateway of claim 1 , wherein the first channel is first physical channel in which communication occurs over a particular frequency band with a left-hand circular polarization;

wherein the second channel is second physical channel in which communication occurs over the particular frequency band with a left-hand circular polarization; and

wherein the first antenna feed port is coupled to a right-hand circular polarized antenna and is configured to receive signals for transmission with a right-hand circular polarization, and wherein the second antenna feed port is coupled to a left-hand circular polarized antenna and is configured to receive signals for transmission with a left-hand circular polarization.

3. The satellite gateway of claim 1 , wherein the first radiofrequency chain, the second radiofrequency chain, and the third radiofrequency chain are each transmit chains.

4. The satellite gateway of claim 3 , wherein the first radiofrequency chain includes a first up-converter and a first power amplifier;

wherein the second radiofrequency chain includes a second up-converter and a second power amplifier; and

wherein the third radiofrequency chain includes a third up-converter and a third power amplifier.

5. The satellite gateway of claim 4 , wherein the first radiofrequency chain includes a first modulator;

wherein the second radiofrequency chain includes a second modulator; and

wherein the third radiofrequency chain includes a third modulator.

6. The satellite gateway of claim 4 , wherein the radiofrequency switches are placed between the power amplifiers and the antenna feed ports to selectively provide outputs of the power amplifiers to the antenna feed ports.

7. The satellite gateway of claim 1 , wherein the first radiofrequency chain, the second radiofrequency chain, and the third radiofrequency chain are each receive chains.

8. The satellite gateway of claim 7 , wherein the first radiofrequency chain includes a first amplifier and a first down-converter;

wherein the second radiofrequency chain includes a second amplifier and a second down-converter; and

wherein the third radiofrequency chain includes a third amplifier and a third down-converter.

9. The satellite gateway of claim 8 , wherein the first radiofrequency chain includes a first demodulator;

wherein the second radiofrequency chain includes a second demodulator; and

wherein the third radiofrequency chain includes a third demodulator.

10. The satellite gateway of claim 8 , wherein the radiofrequency switches are placed between the antenna feed ports and the amplifiers to selectively provide input from the antennas to the amplifiers of the receive chains.

11. The satellite gateway of claim 1 , wherein the radiofrequency switches comprise two radiofrequency switches, including (i) a first switch arranged to switch the first radiofrequency chain and the third radiofrequency chain between the first antenna feed port and a termination, and (ii) a second switch arranged to switch the second radiofrequency chain and the third radiofrequency chain between the second antenna feed port and a termination.

12. The satellite gateway of claim 1 , wherein the radiofrequency switches comprise four radiofrequency switches arranged to selectively (i) couple one of the antenna feed ports with one of the radiofrequency chains, (ii) couple two of the antenna feed ports to different radiofrequency chains, or (iii) couple none of the antenna feed ports to any of the radiofrequency chains.

13. The satellite gateway of claim 1 , wherein each of the first radiofrequency chain, the second radiofrequency chain, and the third radiofrequency chain has a coupling port between the radiofrequency chain and the radiofrequency switches; and

wherein the controller is configured to receive, for each of the radiofrequency chains, data indicating a status of signals on the radiofrequency chain that is based on the signals on the coupling port for the radiofrequency chain.

14. The satellite gateway of claim 1 , wherein the first radiofrequency chain, the second radiofrequency chain, and the third radiofrequency chain are transmit chains;

wherein the radiofrequency switches are placed between outputs of the transmit chains and the antenna feeds to (i) switch between coupling the output of the first radiofrequency chain and the output of the third radiofrequency chain to the first antenna feed port for the first channel, and (ii) switch between coupling the output of the second radiofrequency chain and the output of the third radiofrequency chain to the second antenna feed port for the second channel; and

wherein the first channel and the second channel each involve communication over a same particular frequency band using different polarizations, such that the radiofrequency switches are configured to selectively couple the output of the third radiofrequency chain to (i) the first antenna feed port for transmission using a first polarization of the different polarizations and (ii) the second antenna feed port for transmission using a second polarization of the different polarizations.

15. The satellite gateway of claim 14 , further comprising:

a first coupling port placed to provide output signals at the output of the first radiofrequency chain;

a second coupling port placed to provide output signals at the output of the second radiofrequency chain;

a third coupling port placed to provide output signals at the output of the third radiofrequency chain; and

a spectrum analyzer configured to determine properties of the output signals;

wherein the controller is configured to monitor the status of the radiofrequency chains based on the properties indicated by the spectrum analyzer.

16. The satellite gateway of claim 1 , wherein the controller is configured to monitor the status of the radiofrequency chains by detecting whether output of the radiofrequency chains deviate from a predetermined set of reference properties.

17. A method comprising:

operating, by a controller in a gateway of a satellite communication system, (i) a first radiofrequency chain configured to transmit or receive information on a first channel, (ii) a second radiofrequency chain configured to transmit or receive information on a second channel, and (iii) a third radiofrequency chain in a standby mode in which the third radiofrequency chain does not transmit or receive information in the satellite communication system, wherein the gateway includes radiofrequency switches configured to (i) switch between coupling the first radiofrequency chain and the third radiofrequency chain to a first antenna feed port for the first channel, and (ii) switch between coupling the second radiofrequency chain and the third radiofrequency chain to a second antenna feed port for the second channel;

monitoring, by a controller in a gateway of a satellite communication system, a status of the first radiofrequency chain and the second radiofrequency chain;

based on the monitoring, detecting, by the controller, a failure in the first radiofrequency chain or the second radiofrequency chain; and

in response to detecting the failure, causing, by the controller, the radiofrequency switches to couple the third radiofrequency chain to one of the antenna feed ports in place of the radiofrequency chain in which the failure is detected.

18. The method of claim 17 , further comprising:

providing a test input to the third radiofrequency chain;

receiving a test output that the third radiofrequency chain produced in response to the test input; and

determining, based on the test output, that the third radiofrequency chain is operating correctly;

wherein causing the radiofrequency switches to couple the third radiofrequency chain to one of the antenna feed ports is based on determining that the third radiofrequency chain is operating correctly.

19. The method of claim 17 , wherein the first radiofrequency chain, the second radiofrequency chain, and the third radiofrequency chain are each transmit chains;

wherein the first radiofrequency chain includes a first modulator, a first up-converter, and a first power amplifier;

wherein the second radiofrequency chain includes a second modulator, a second up-converter, and a second power amplifier;

wherein the third radiofrequency chain includes a third modulator, a third up-converter, and a third power amplifier;

wherein causing the radiofrequency switches to couple the third radiofrequency chain to one of the antenna feed ports comprises causing the radiofrequency switches to couple the third radiofrequency chain to the first antenna feed port in place of the first radiofrequency chain; and

wherein the method further comprises routing data to be transmitted on the first channel to the third modulator instead of to the first modulator.

20. One or more non-transitory computer-readable storage media coupled to one or more processors and having instructions stored thereon which, when executed by the one or more processors, cause the one or more processors to perform operations comprising:

operating, by a controller in a gateway of a satellite communication system, (i) a first radiofrequency chain configured to transmit or receive information on a first channel, (ii) a second radiofrequency chain configured to transmit or receive information on a second channel, and (iii) a third radiofrequency chain in a standby mode in which the third radiofrequency chain does not transmit or receive information in the satellite communication system, wherein the gateway includes radiofrequency switches configured to (i) switch between coupling the first radiofrequency chain and the third radiofrequency chain to a first antenna feed port for the first channel, and (ii) switch between coupling the second radiofrequency chain and the third radiofrequency chain to a second antenna feed port for the second channel;

monitoring, by a controller in a gateway of a satellite communication system, a status of the first radiofrequency chain and the second radiofrequency chain;

based on the monitoring, detecting, by the controller, a failure in the first radiofrequency chain or the second radiofrequency chain; and

in response to detecting the failure, causing, by the controller, the radiofrequency switches to couple the third radiofrequency chain to one of the antenna feed ports in place of the radiofrequency chain in which the failure is detected.

Assignments (2)

Continuity (3)

References Cited (75)

Cited By (1)

US 12,335,025