RECEIVER DUAL-REFLECTOR ANTENNA SYSTEM FOR INTERFERENCE SUPPRESSION ONBOARD SATELLITE

• US 20150123843A1
• Filed: 11/06/2013
• Published: 05/07/2015
• Est. Priority Date: 11/06/2013
• Status: Abandoned Application

• Current Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Original Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Inventors: LIER, Erik, Jacomb-Hood, Anthony Wykeham, Hasan, Moh'd A., Bray, Matthew George, Baker, Russell T.
• Application Number:
  US14/073,759
• Publication Number:
  US 20150123843A1
• Time in Patent Office: Days
• US Class Current: 342/352
• CPC Class Codes: H04B 7/18513 Transmission in a satellite or space-based system
• CPC Class Codes: H04B 7/18515 Transmission equipment in satellites or space-based relays
• CPC Class Codes: H04K 2203/32 including a particular configuration of antennas
• CPC Class Codes: H04K 3/228 Elimination in the received signal of jamming or of data corrupted by jamming interference suppression in receivers H04B1/10

Abstract

A system for interference suppression onboard a satellite may include an antenna that is configured to receive uplink signals from a ground-coverage area and to generate a first signal. A spot-beam antenna may be configured to receive interference signals and to generate a second signal. A processor may be configured to receive the first signal from the antenna and the second signal from the spot-beam antenna and to perform a cross-correlation to generate a composite signal that includes a null at an interference frequency. The antenna may be a shaped reflector antenna and the spot-beam antenna may be a parabolic reflector antenna.

Claims

1. A system for interference suppression onboard a satellite, the system comprising:

an antenna configured to receive uplink signals from a ground-coverage area and to generate a first signal;

a spot-beam antenna configured to receive interference signals and to generate a second signal; and

a processor configured to receive the first signal from the antenna and the second signal from the spot-beam antenna and to generate a composite signal with the interference signals suppressed.

2. The system of claim 1, wherein the processor is configured to filter the first signal from the antenna and the second signal from the spot-beam antenna prior to generating the composite signal with the interference signals suppressed only at selected frequencies, and wherein the processor comprises a digital cross-correlator and summer, and wherein the digital cross-correlator is configured to perform the cross-correlation by comparing the first and the second signals, finding a relative amplitude and phase of the first and the second signals, and wherein the summer is configured to combine the first and the second signals with same amplitudes and a 180 degree relative phase at the interference frequency to create the composite signal with the interference signals suppressed.

3. The system of claim 1, wherein the antenna comprises a shaped reflector antenna, wherein the shaped reflector is configured to provide a shaped beam.

4. The system of claim 1, wherein the spot-beam antenna comprises a parabolic reflector antenna and is configured to provide a spot beam in a direction of an interference source, and wherein the spot-beam reflector antenna is mechanically steerable.

5. The system of claim 4, further comprising an auto-track subsystem configured to facilitate steering of the spot-beam reflector antenna to point the spot beam of the spot-beam reflector antenna in the direction of le interference source and to provide an estimate of the location of a signal source.

6. The system of claim 1, wherein the cross-correlator is configured to provide a digital amplitude of the second signal to an auto-track subsystem, wherein the auto-track subsystem is configured to use the digital amplitude of the second signal to direct a spot-beam of the spot-beam antenna in a direction of an interference source, wherein the interference source comprises a ground jammer, and wherein the system is configured to provide a location of the interference source.

7. The system of claim 1, wherein the spot-beam antenna is configured to scan over a plausible region including an interference source, wherein the system receives information regarding the plausible region and interference frequency data from a ground station.

8. The system of claim 1, further comprising a digital-to-analog converter (DAC) configured to convert the composite signal to an analog signal, and a downlink subsystem configured to transmit down the composite signal toward the ground jammer.

9. The system of claim 1, wherein a composite pattern of antenna and the spot-beam antenna includes a null, and wherein the null is localized to a spot-beam foot-print of the spot-beam antenna, and wherein a narrower null in the composite pattern is achievable by increasing a distance between the antenna and the spot-beam antenna.

10. A method for interference suppression onboard a satellite, the method comprising:

receiving uplink signals from a ground-coverage area and generating a first signal based on the uplink signals;

receiving interference signals and generating a second signal based on the interference signals; and

receiving the first signal and the second signal and generating a composite signal with the interference signals suppressed by performing a weighted sum.

11. The method of claim 10, wherein performing the weighted sum comprises determining weighing factors based on cross-correlation, and further comprising performing cross-correlation using a digital cross-correlator, and wherein performing the cross-correlation comprises comparing the first and the second signals, finding a relative amplitude and phase of the first and the second signals.

12. The method of claim 10, wherein receiving the uplink signals from the ground-coverage area comprises using a shaped reflector antenna, wherein the shaped reflector is configurable to provide a shaped beam.

13. The method of claim 10, wherein receiving interference signals comprises using a spot-beam reflector antenna that comprises a parabolic reflector antenna and is configurable to provide a spot beam in a direction of an interference source, and the method further comprises mechanically steering the spot-beam reflector antenna.

14. The method of claim 13, further comprising facilitating, by using an auto-track subsystem, steering of the spot-beam reflector antenna to point the spot beam of the spot-beam reflector antenna in the direction of the interference source.

15. The method of claim 10, further comprising providing a digital amplitude of the second signal to an auto-track subsystem, configuring the auto-track subsystem to use the digital amplitude of the second signal to direct a spot-beam of the spot-beam antenna in a direction of an interference source, and reporting an estimate of a location of the interference source.

16. The method of claim 10, further comprising receiving information regarding a plausible region and interference frequency data from a ground station, and scanning over the plausible region including an interference source, and wherein scanning over the plausible region includes using an auto-track subsystem.

17. The method of claim 16, further comprising converting the composite signal to an analog signal, and a transmitting down the composite signal.

18. The system of claim 10, wherein a composite pattern of the antenna and the spot-beam antenna includes a null, and wherein the null is localized to a spot-beam foot-print of the spot-beam antenna, and achieving a narrower null in the composite signal by increasing a distance between the antenna and the spot-beam antenna.

19. A satellite system, comprising:

one or more shaped beam antennas;

one or more spot-beam antennas that are mechanically steerable;

a processor configured to perform cross-correlation; and

a payload configured to couple the one or more shaped beam antennas, the one or more spot-beam antennas, and the processor and to facilitate coupling first and second signals generated, respectively, by the one or more shaped beam antennas and the one or more spot-beam antennas to the processor,

wherein the processor is configured to perform a weighted sum to generate composite signals with interference signals suppressed.

20. The satellite system of claim 19, wherein:

the processor comprises a digital cross-correlator and a summer, wherein the digital cross-correlator is configured to perform the cross-correlation by comparing the first and the second signals, finding a relative amplitude and phase of the first and the second signals, and wherein the summer is configured to combine the first and the second signals with same amplitudes and 180 degree relative phases at the interference frequencies to create the composite signal with the interference signals suppressed, and wherein the satellite system further comprises an auto-track subsystem configured to facilitate steering of the one or more spot-beam antennas to point the spot beams of the one or more spot-beam antennas in one or more directions of one or more interference sources and to provide an estimate of the location of one or more signal sources.