Wide area high resolution SAR from a moving and hovering helicopter

• US 7,728,756 B2
• Filed: 08/20/2007
• Issued: 06/01/2010
• Est. Priority Date: 08/20/2007
• Status: Active Grant

• Current Assignee: Raytheon Company (Rtx Corporation)
• Original Assignee: Raytheon Company (Rtx Corporation)
• Inventors: Rosen, Robert A., Gubala, Michael, Krikorian, Kapriel V.
• Primary Examiner(s): Tarcza; Thomas H
• Assistant Examiner(s): GALT, CASSI J
• Application Number:
  US11/894,069
• Publication Number:
  US 20090051585A1
• Time in Patent Office: 1,016 Days
• Field of Search: 342/25.R, 342 25 A- 25 F, 342 5- 6, 342 61- 65
• US Class Current: 342/25.00A
• CPC Class Codes: G01S 13/904 SAR modes
• CPC Class Codes: G01S 13/9082 Rotating SAR [ROSAR]
• CPC Class Codes: G01S 7/4026 Antenna boresight

Abstract

A hovering helicopter has a radar transmitter/receiver for transmitting radar pulses for illuminating a target for SAR imaging, and rotor blades for generating lift. Radar reflectors are on the rotor blades. The radar reflectors are oriented to reflect the radar pulses from the transmitter to the target as the rotor blades rotate. The radar pulses reflected by the moving reflector from the transmitter are timed to generate the synthetic aperture image using radar returns from the target. The receiver also receives blade returns directly reflected from the moving reflectors attached to the lift rotor blades. The receiver analyzes the blade returns to extract motion details of the reflectors and uses the motion details for motion compensation of target returns for SAR imaging.

Claims

1. A radar system configured to acquire a synthetic aperture image of a target, said radar system comprising:

a radar transmitter affixed to a hovering platform that transmits radar pulses;

a reflector moving relative to said hovering platform, said radar transmitter, and said target along a path, said reflector reflecting said radar pulses from said transmitter to said target as said reflector moves along said path, said radar pulses timed to generate said synthetic aperture image from radar returns from said target,

wherein said synthetic aperture image is generated from said radar returns without any relative motion between said hovering platform and said target.

2. A radar system as described in claim 1 further comprising a receiver for target returns received from illuminating said target with radar pulses reflected from said transmitter.

3. A radar system as described in claim 2 wherein said receiver receives blade returns from said reflector.

4. A radar system as described in claim 3 wherein said receiver analyzes said blade returns to motion compensate said target returns for motion of said reflector.

5. A radar system as described in claim 2 wherein said reflector reflects said radar returns from said target into said receiver.

6. A radar system as described in claim 1 wherein said reflector is mechanically coupled to said hovering platform.

7. A radar system as described in claim 1 wherein said path of said reflector is circular.

8. A radar system as described in claim 1 wherein said path of said reflector is elliptical.

9. A radar system as described in claim 1 wherein said path of said reflector is rectilinear.

10. A helicopter configured to acquire a synthetic aperture image of a target, said helicopter comprising:

a transmitter fixed to a body of said helicopter configured to transmit radar pulses that illuminate said target;

rotor blades, said rotor blades rotating with respect to said body and said transmitter so as to generate lift for said helicopter; and

one or more reflectors on said rotor blades, said one or more reflectors oriented to reflect said radar pulses from said transmitter to said target;

wherein said radar pulses are timed to generate said synthetic aperture image from radar returns from said target.

11. A helicopter as described in claim 10, further comprising a receiver configured to receive target returns reflected by illuminating said target with radar pulses transmitted by said transmitter.

12. A helicopter as described in claim 11 wherein said receiver receives blade returns from said one or more reflectors.

13. A helicopter as described in claim 12 wherein said receiver analyzes said blade returns to motion compensate said target returns for motion of said one or more reflectors.

14. A helicopter as described in claim 12 wherein said one or more reflectors reflect said radar target returns from said target into said receiver.

15. A helicopter as described in claim 10 wherein said one or more reflectors are mechanically coupled to said rotor blades.

16. A method configured to acquire a synthetic aperture image of a target using a radar system, the method comprising:

transmitting radar pulses from a radar transmitter affixed to a non-rotating section of a hovering platform;

illuminating a moving reflector with said radar pulses, said moving reflector moving along a path, said moving reflector reflecting said radar pulses from said transmitter to said target as said moving reflector moves along said path, said radar pulses timed to generate said synthetic aperture image from target returns from said target,

wherein said synthetic aperture image is generated from said radar returns without relative movement between said hovering platform and said target.

17. A method as described in claim 16 further comprising receiving target returns from illuminating said target with radar pulses reflected by said moving reflector.

18. A method as described in claim 17 wherein said receiver receives blade returns reflected from said moving reflector.

19. A method as described in claim 18 wherein said receiver analyzes said blade returns to motion compensate said target returns for motion of said reflector.

20. A method as described in claim 17 wherein said reflector reflects said target returns from said target into said receiver.

21. A method as described in claim 16, wherein said moving reflector is mechanically coupled to said hovering platform.

22. A method as described in claim 16 wherein said path of said moving reflector is circular.

23. A method as described in claim 16 wherein said path of said moving reflector is elliptical.

24. A method as described in claim 16 wherein said path of said moving reflector is rectilinear.

25. A method of operating a hovering helicopter configured to acquire a synthetic aperture image of a target, the method comprising:

transmitting radar pulses from a transmitter fixed to a body of said hovering helicopter;

rotating rotor blades that generate lift for said helicopter;

illuminating one or more reflectors on said rotating rotor blades with said transmitted radar pulses, said one or more reflectors oriented to reflect said transmitted radar pulses from said transmitter to said target as said rotor blades rotate;

timing said transmitted radar pulses reflected by said one or more reflectors to generate said synthetic aperture image from target returns from said target.

26. A method as described in claim 25 further comprising receiving target returns using a receiver, said target returns received from illuminating said target with radar pulses reflected by said one or more reflectors.

27. A method as described in claim 26 wherein said receiver receives blade returns from said one or more reflectors.

28. A method as described in claim 27 wherein said receiver analyzes said blade returns to motion compensate said target returns for motion of said one or more reflectors.

29. A method as described in claim 27 wherein said one or more reflectors reflect said target returns from said target into said receiver.

30. A method as described in claim 25, wherein said one or more reflectors are mechanically coupled to said rotor blades.

31. A helicopter configured to acquire a synthetic aperture image of a target, said helicopter having a longitudinal axis, said helicopter moving with forward motion along said longitudinal axis, said target aligned with said forward motion along said longitudinal axis, said helicopter comprising:

a transmitter fixed to a body of said helicopter that transmits radar pulses that illuminate said target;

rotor blades that rotate to generate lift for said helicopter;

one or more reflectors on said rotor blades, said one or more reflectors oriented to reflect said radar pulses from said transmitter to said target, said radar pulses timed to generate said synthetic aperture image from target returns from said target,

wherein said target is aligned with said forward motion along said longitudinal axis of said helicopter while said synthetic aperture image is generated.

32. A helicopter as described in claim 31, further comprising a receiver configured to receive target returns received after illuminating said target with radar pulses reflected from said transmitter.

33. A helicopter as described in claim 32 wherein said receiver receives blade returns from said one or more reflectors.

34. A helicopter as described in claim 33 wherein said receiver analyzes said blade returns to motion compensate said target returns for motion of said one or more reflectors.

35. A helicopter as described in claim 32 wherein said one or more reflectors reflect said radar returns from said target into said receiver.

36. A helicopter as described in claim 31 wherein said one or more reflectors are mechanically coupled to said rotor blades.

37. A method for acquiring a synthetic aperture image of a target using a helicopter, said helicopter having a longitudinal axis, said helicopter moving with forward motion along said longitudinal axis, said target aligned with said forward motion along said longitudinal axis, said method comprising:

transmitting radar pulses from a body portion of said helicopter to illuminate said target;

rotating rotor blades of said helicopter to generate lift for said helicopter, said rotor blades equipped with one or more reflectors, said one or more reflectors oriented to reflect said radar pulses from said transmitter to said target;

timing said radar pulses from said transmitter to said target as said rotor blades rotate to generate said synthetic aperture image from radar returns received from said target.

38. A method as described in claim 37, further comprising a receiver configured to receive target returns received after illuminating said target with said radar pulses.

39. A method as described in claim 38 wherein said receiver receives blade returns from said one or more reflectors.

40. A method as described in claim 39 wherein said receiver analyzes said blade returns to motion compensate said target returns for motion of said one or more reflectors.

41. A method as described in claim 38 wherein said one or more reflectors reflect said radar returns from said target into said receiver.

42. A method as described in claim 38 wherein said one or more reflectors are mechanically coupled to said rotor blades.