Compensating for a non-ideal surface of a reflector in a satellite communication system

• US 9,293,820 B2
• Filed: 03/13/2013
• Issued: 03/22/2016
• Est. Priority Date: 03/13/2013
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Koduru, Chandra S., Suh, Kihyun Kevin, Veysoglu, Murat E., Busche, Greg
• Primary Examiner(s): Liu, Harry
• Application Number:
  US13/798,342
• Publication Number:
  US 20140266870A1
• Time in Patent Office: 1,105 Days
• Field of Search: 342/354
• US Class Current: 1/1
• CPC Class Codes: H01Q 1/288 Satellite antennas
• CPC Class Codes: H01Q 15/14 Reflecting surfaces; Equivalent structures electromagnetic shields H01Q1/526
• CPC Class Codes: H01Q 15/148 with means for varying the reflecting properties H01Q15/147 takes precedence
• CPC Class Codes: H01Q 3/2605 Array of radiating elements provided with a feedback control over the element weights, e.g. adaptive arrays
• CPC Class Codes: H01Q 3/2658 Phased-array fed focussing structure
• CPC Class Codes: H01Q 3/40 with phasing matrix
• CPC Class Codes: H01Q 5/50 Feeding or matching arrangements for broad-band or multi-band operation
• CPC Class Codes: H04B 7/1851 Systems using a satellite or space-based relay H04B7/18508, H04B7/18521 take precedence; providing specific services H04B7/18523 - H04B7/18576
• CPC Class Codes: H04B 7/2041 Spot beam multiple access

Abstract

A method is provided that includes measuring amplitudes and phases of signals reflected off a reflector of a satellite, with the amplitudes and phases forming a first set of measurements. The method includes calculating an element correlation matrix as a function of the first set of measurements. The element correlation matrix represents a radiated feed element pattern off the reflector. And the method includes adjusting a formed beam pattern of a beamformer based on the element correlation matrix to thereby compensate for a non-ideal surface of the reflector.

Claims

1. A system comprising:

a beamformer configured to measure amplitudes and phases of signals reflected off a reflector of a satellite, the amplitudes and phases forming a first set of measurements; and

a computing apparatus configured to calculate an element correlation matrix as a function of the first set of measurements, the element correlation matrix representing a radiated feed element pattern off the reflector,

wherein the beamformer is configured to generate a formed beam pattern adjusted based on the element correlation matrix.

2. The system of claim 1, wherein the formed beam pattern is a function of a feed pattern and beam weights, and the beamformer is configured to generate the formed beam pattern as a function of the beam weights adjusted based on the element correlation matrix.

3. The system of claim 1, wherein the beamformer is configured to measure the amplitudes and phases as the satellite is slewed at a predetermined rate over a predetermined range.

4. The system of claim 1, wherein the beamformer is further configured to forward the signals to the satellite for reflection off the reflector, the satellite being configured to receive the signals over feeder links at a feeder-link antenna, and

wherein the feeder-link antenna is counter-slewed as the satellite is slewed.

5. The system of claim 1, wherein the satellite is configured to receive the signals over feeder links,

wherein the beamformer includes first and second beamformers, the first beamformer being configured to measure the amplitudes and phases of the signals reflected off a reflector, and the second beamformer being configured to measure the amplitudes and phases of the signals passed through a communication platform of the satellite and returned back over the feeder links independent of the reflector, the respective amplitudes and phases forming a second set of measurements, and

wherein the computing apparatus is configured to calculate the element correlation matrix further as a function of the second set of measurements.

6. The system of claim 1, wherein the beamformer includes first and second beamformers, the first beamformer being configured to measure the amplitudes and phases of the signals reflected off a reflector,

wherein the first and second beamformers are configured to measure first and second amplitudes and phases of second signals received at respective ones of the first and second beamformers from the satellite over feeder links, the satellite having received the second signals over the feeder links independent of the reflector, the respective first and second amplitudes forming first and second second sets of measurements,

wherein the computing apparatus is configured to calculate a difference measurement as a function of the difference between the first and second second sets of measurements, and calculate the element correlation matrix further as a function of the first second set of measurements and difference measurement.

7. A method comprising:

measuring amplitudes and phases of signals reflected off a reflector of a satellite, the amplitudes and phases forming a first set of measurements;

calculating an element correlation matrix as a function of the first set of measurements, the element correlation matrix representing a radiated feed element pattern off the reflector; and

adjusting a formed beam pattern of a beamformer based on the element correlation matrix.

8. The method of claim 7, wherein the formed beam pattern is a function of a feed pattern and beam weights, and adjusting the formed beam pattern includes adjusting the beam weights based on the element correlation matrix.

9. The method of claim 7, wherein the amplitudes and phases are measured as the satellite is slewed at a predetermined rate over a predetermined range.

10. The method of claim 7 further comprising:

forwarding the signals to the satellite for reflection off the reflector, the satellite receiving the signals over feeder links at a feeder-link antenna,

wherein the feeder-link antenna is counter-slewed as the satellite is slewed.

11. The method of claim 7, wherein the satellite receives the signals over feeder links, wherein the method further comprises:

measuring the amplitudes and phases of the signals passed through a communication platform of the satellite and returned back over the feeder links independent of the reflector, the respective amplitudes and phases forming a second set of measurements, and

wherein the element correlation matrix is calculated further as a function of the second set of measurements.

12. The method of claim 7, wherein the beamformer includes first and second beamformers, wherein the method further comprises:

measuring first and second amplitudes and phases of second signals received at respective ones of the first and second beamformers from the satellite over feeder links, the satellite having received the second signals over the feeder links independent of the reflector, the respective first and second amplitudes forming first and second second sets of measurements; and

calculating a difference measurement as a function of the difference between the first and second second sets of measurements,

wherein the element correlation matrix is calculated further as a function of the first second set of measurements and difference measurement.

13. A method comprising:

measuring amplitudes and phases of signals received by a satellite over feeder links, passed through a communication platform and reflected off a reflector of the satellite in a forward direction, the amplitudes and phases forming a first set of measurements;

measuring the amplitudes and phases of the signals passed through the communication platform and returned back over the feeder links independent of the reflector, the respective amplitudes and phases forming a second set of measurements;

calculating an element correlation matrix as a function of the first and second sets of measurements, the element correlation matrix representing a radiated feed element pattern off the reflector; and

adjusting a formed beam pattern of a beamformer based on the element correlation matrix.

14. The method of claim 13, wherein the formed beam pattern is a function of a feed pattern and beam weights, and adjusting the formed beam pattern includes adjusting the beam weights based on the element correlation matrix.

15. The method of claim 13, wherein the amplitudes and phases are measured as the satellite is slewed at a predetermined rate over a predetermined range.

16. The method of claim 13 further comprising:

forwarding the signals to the satellite for reflection off the reflector, the satellite receiving the signals over feeder links at a feeder-link antenna,

wherein the feeder-link antenna is counter-slewed as the satellite is slewed.

17. A method comprising:

measuring amplitudes and phases of signals reflected off a reflector of a satellite, and forwarded by the satellite to a beamformer in a return direction, the beamformer including first and second beamformers, and the amplitudes and phases forming a first set of measurements;

measuring first and second amplitudes and phases of second signals received at respective ones of the first and second beamformers from the satellite over feeder links, the satellite having received the second signals over the feeder links independent of the reflector, the respective first and second amplitudes forming first and second second sets of measurements;

calculating a difference measurement as a function of the difference between the first and second second sets of measurements;

calculating an element correlation matrix as a function of the first set of measurements, first second set of measurements and difference measurement, the element correlation matrix representing a radiated feed element pattern off the reflector; and

adjusting a formed beam pattern of a beamformer based on the element correlation matrix.

18. The method of claim 17, wherein the formed beam pattern is a function of a feed pattern and beam weights, and adjusting the formed beam pattern includes adjusting the beam weights based on the element correlation matrix.

19. The method of claim 17, wherein the amplitudes and phases are measured as the satellite is slewed at a predetermined rate over a predetermined range.

20. The method of claim 17 further comprising:

forwarding the signals to the satellite for reflection off the reflector, the satellite receiving the signals over feeder links at a feeder-link antenna,

wherein the feeder-link antenna is counter-slewed as the satellite is slewed.