Radar receiver motion compensation system and method

• US 20050179579A1
• Filed: 12/20/2004
• Published: 08/18/2005
• Est. Priority Date: 12/29/2003
• Status: Abandoned Application

• Current Assignee: Rick Mckerracher, Shane D. Pinder, Stuart Doherty
• Original Assignee: Rick Mckerracher, Shane D. Pinder, Stuart Doherty
• Inventors: Pinder, Shane D., Doherty, Stuart, McKerracher, Rick
• Application Number:
  US11/018,854
• Publication Number:
  US 20050179579A1
• Time in Patent Office: Days
• US Class Current: 342/25.R
• CPC Class Codes: G01S 13/5242 with means for platform motion or scan motion compensation, e.g. airborne MTI
• CPC Class Codes: G01S 7/2926 by integration

Abstract

A motion compensation unit and method for use in a radar system. The motion compensation unit comprises a match filter module for producing filtered range-pulse-sensor data; a motion information module for providing motion information related to motion of the radar system; a motion compensation beamformer module connected to the match filter module and the motion information module for utilizing the motion information to provide motion-compensated range-pulse-azimuth data; and, a Doppler processing module connected to the motion compensation beamformer module to provide motion-compensated range-Doppler-azimuth data.

Claims

1. A motion compensation unit for use in a radar system, wherein the motion compensation unit comprises:

a) a match filter module producing filtered range-pulse-sensor data;

b) a motion information module providing motion information related to motion of the radar system;

c) a motion compensation beamformer module operably coupled to the match filter module and the motion information module, the motion compensation beamformer module utilizing the motion information to provide motion-compensated range-pulse-azimuth data; and

,

d) a Doppler processing module operably coupled to the motion compensation beamformer module, the Doppler processing module providing motion-compensated range-Doppler-azimuth data.

2. The motion compensation unit of claim 1, wherein the motion compensation beamformer module comprises:

i) an uncompensated Doppler processing module receiving the filtered range-pulse-sensor data and providing range-Doppler-sensor data;

ii) a beamformer module operably coupled to the uncompensated Doppler processing module, the beamformer module receiving the filtered range-Doppler-sensor data and providing range-Doppler-azimuth data; and

,

iii) an inverse Doppler module operably coupled to the beamformer module and the motion information module for receiving the motion information and the range-Doppler-azimuth data and providing the motion-compensated range-pulse-azimuth data.

3. The motion compensation unit of claim 2, wherein the inverse Doppler module applies a phase demodulation method based on the motion information to produce the motion-compensated range-pulse-azimuth data.

4. The motion compensation unit of claim 2, wherein the phase demodulation method uses the Hilbert transform.

5. The motion compensation unit of claim 1, wherein the motion compensation beamformer module comprises:

i) a beamformer module receiving the filtered range-pulse-sensor data and providing range-pulse-azimuth data; and

,

ii) a phase demodulation module operably coupled to the beamformer module and to the motion information module, the phase demodulation module receiving the motion information and the range-pulse-azimuth data and applying a phase demodulation method to provide the motion-compensated range-pulse-azimuth data.

6. The motion compensation unit of claim 1, wherein the motion information module comprises an inertial navigational system.

7. A method of motion compensation for a radar system, wherein the method comprises:

a) match filtering radar data for producing filtered range-pulse-sensor data;

b) obtaining motion information related to motion of the radar system;

c) motion-compensated beamforming the filtered range-pulse-sensor data according to the motion information to provide motion compensated range-pulse-azimuth data; and

,

d) Doppler processing the motion compensated range-pulse-azimuth data to provide motion-compensated range-Doppler-azimuth data.

8. The motion compensation method of claim 7, wherein beamforming comprises:

i) Doppler processing the filtered range-pulse-sensor data to provide range-Doppler-sensor data;

ii) beamform processing the filtered range-Doppler-sensor data to provide range-Doppler-azimuth data; and

,

iii) inverse Doppler processing and phase demodulating the range-Doppler-azimuth data based on the motion information to provide the motion-compensated range-pulse-azimuth data.

9. The motion compensation method of claim 8, wherein inverse Doppler processing comprises applying a Hilbert Transform while phase demodulating the range-Doppler-azimuth data based on the motion information to produce the motion-compensated range-pulse-azimuth data.

10. The motion compensation method of claim 7, wherein beamforming comprises:

i) Beamform processing the filtered range-pulse-sensor data to provide range-pulse-azimuth data; and

, ii) Phase demodulating the range-pulse-azimuth data based on the motion information to provide the motion-compensated range-pulse-azimuth data.

11. The motion compensation method of claim 7, wherein the radar system comprises an antenna having at least one antenna element with a phase center, and further comprising:

obtaining, for a desired coherent integration time (CIT) of the radar system, rotation and translation information associated with movement of the radar system over the desired CIT;

determining, using at least a portion of rotation and translation information, a change in the location of the phase center of the antenna element over the CIT; and

computing, based on the change in location of the phase center, a phase correction for the antenna element.

12. The motion compensation method of claim 11, further comprising applying the phase correction to the motion compensated range-pulse-azimuth data.

13. The motion compensation method of claim 11, wherein the phase corrections are applied as part of beamforming.

14. The motion compensation method of claim 11 further comprising acquiring a direction of arrival (DOA) at which a radio frequency (RF) signal is returned to the antenna.

15. The motion compensation method of claim 14, wherein the change in location of the phase center is represented by a set of directional components and wherein computing a phase offset further comprises selecting, from the set of directional components, a directional component that is substantially parallel to the DOA and using at least this selected directional component to compute the phase correction for the antenna element.

16. The motion compensation method of claim 15, further comprising applying the phase correction to the motion compensated range-pulse-azimuth data.

17. The motion compensation method of claim 7, wherein the radar system comprises at least one of a high frequency radar system, a high frequency surface wave radar (HFSWR) and an over the horizon (OTH) radar.

18. The motion compensation method of claim 7, wherein the radar system is capable of operation for at least one frequency in the frequency range of 2 to 40 MHz.

19. The motion compensation method of claim 7, wherein the radar system is operably coupled to a conveyance intended for navigation on water.

20. The motion compensation method of claim 8, wherein the radar system comprises an antenna having at least one antenna element with a phase center, and further comprising:

obtaining, for a desired coherent integration time (CIT) of the radar system, rotation and translation information associated with movement of the radar system over the desired CIT;

determining, using at least a portion of rotation and translation information, a change in the location of the phase center of the antenna element over the CIT; and

computing, based on the change in location of the phase center, a phase correction for the antenna element.

21. The motion compensation method of claim 20, further comprising applying the phase corrections to the range Doppler-azimuth data of (ii).

22. The motion compensation method of claim 20 further comprising acquiring a direction of arrival (DOA) at which a radio frequency (RF) signal is returned to the antenna.

23. The motion compensation method of claim 22, wherein the change in location of the phase center is represented by a set of directional components and wherein computing a phase offset further comprises selecting, from the set of directional components, a directional component that is substantially parallel to the DOA and using at least this selected directional component to compute the phase correction for the antenna element.

24. The motion compensation method of claim 23, further comprising applying the phase correction to the motion compensated range-pulse-azimuth data.

25. The motion compensation method of claim 20, wherein the radar system comprises at least one of a high frequency radar system, a high frequency surface wave radar (HFSWR) and an over the horizon (OTH) radar.

26. The motion compensation method of claim 20, wherein the radar system is operably coupled to a conveyance intended for navigation on water.

27. A method for determining motion compensation for a radar system, the radar system comprising an antenna having at least one antenna element with a phase center, the method comprising:

obtaining, for a desired coherent integration time (CIT) of the radar system, rotation and translation information associated with movement of the radar system over the desired CIT;

determining, using at least a portion of rotation and translation information, a change in the location of the phase center of the antenna element over the CIT; and

computing, based on the change in location of the phase center, a phase correction for the antenna element.

28. The method of claim 27, wherein the rotation and translation information comprises a set of motion information coordinates, the motion information coordinates associated with degrees of freedom of motion of the radar system.

29. The method of claim 28, wherein the set of motion information coordinates comprises at least one of surge displacement, sway displacement, heave displacement, pitch angular displacement, yaw angular displacement, and roll angular displacement.

30. The method of claim 28, further comprising obtaining the displacement of each respective coordinate in the set as a function of time.

31. The method of claim 30, wherein the change in location of the phase center is determined using the displacement of each motion information coordinate as a function of time.

32. The method of claim 27 further comprising acquiring a direction of arrival (DOA) at which a radio frequency (RF) signal is returned to the antenna.

33. The method of claim 32, wherein the computed phase correction is a function of the DOA.

34. The method of claim 33, wherein the change in location of the phase center comprises a set of directional components and wherein computing a phase correction further comprises selecting from the set of directional components a directional component that is substantially parallel to the DOA and using at least this selected direction component to compute the phase correction for the antenna element.

35. The method of claim 27, wherein the radar system comprises at least one of a high frequency radar system, a high frequency surface wave radar (HFSWR) and an over the horizon (OTH) radar.

36. The method of claim 27, wherein the radar system is capable of operation for at least one frequency in the frequency range of 2 to 40 MHz.

37. The method of claim 27, wherein the radar system is operably coupled to a vessel intended for navigation on water.

38. A motion compensation unit for use in a radar system, the radar system comprising an antenna having at least one antenna element with a phase center, wherein the motion compensation unit comprises:

a match filter module producing filtered range-pulse-sensor data;

a motion information module providing motion information related to the motion of the radar system, wherein the motion information further comprises phase correction information associated with movement of the phase center of the antenna element;

a motion compensation beamformer module operably coupled to the match filter module and to the motion information module, the motion compensation beamformer module using the motion information to provide motion-compensated range-pulse-azimuth data; and

a Doppler processing module operably coupled to the motion compensation beamformer module, the Doppler processing module providing motion-compensated range-Doppler-azimuth data.

39. A high frequency radar system adapted for use on a vessel, the radar system comprising:

an antenna comprising at least one element, the element having a phase center;

a high frequency receiver operably coupled to the antenna;

a match filter operably coupled to the receiver, the match filter producing filtered range-pulse-sensor data;

a motion information module providing motion information related to motion of the radar system, wherein the motion information comprises phase correction information associated with movement of the phase center of the antenna element;

a motion compensation beamformer operably coupled to the match filter and to the motion information module, the motion compensation beamformer using the motion information to provide motion-compensated range-pulse-azimuth data; and

a Doppler processor operably coupled to the motion compensation beamformer, the Doppler processor providing motion-compensated range-Doppler-azimuth data.

40. The high frequency radar system of claim 39, further comprising an inertial navigation system operably coupled to the motion compensation beamformer.

41. A motion compensation system for use with a radar system, the radar system comprising an antenna having at least one antenna element with a phase center, wherein the motion compensation system comprises:

means for providing filtered range-pulse-sensor data;

means for providing phase correction information associated with movement of the phase center of the antenna element;

means for providing motion-compensated range-pulse-azimuth data based on the filtered range-pulse-sensor data and the phase correction information; and

means for providing motion-compensated range-Doppler-azimuth data based on the motion-compensated range-pulse-azimuth data.