Three-dimensional synthetic aperture radar for mine detection and other uses

• US 6,982,666 B2
• Filed: 06/08/2001
• Issued: 01/03/2006
• Est. Priority Date: 06/08/2001
• Status: Expired due to Fees

• Current Assignee: Navy The USA As Represented By The Secretary of The
• Original Assignee: the united states of america as represented by the secretary of the navy
• Inventors: Pavco, John A., Temes, Clifford L.
• Primary Examiner(s): Tarcza, Thomas H.
• Assistant Examiner(s): ALSOMIRI, ISAM A
• Application Number:
  US09/876,137
• Publication Number:
  US 20040118313A1
• Time in Patent Office: 1,670 Days
• Field of Search: 342/22, 342/25, 342/64, 342/179, 342/368, 342/459, 342/465, 244/137.4, 362/470, 343/705
• US Class Current: 342/22
• CPC Class Codes: F41H 11/12 Means for clearing land minefields; Systems specially adapted for detection of landmines

Abstract

A radar system for generating a three-dimensional image includes a radar transmitter which is operable to produce a radar signal of a frequency of at least three gigahertz. A plurality of radar receiving antennas from an antenna array. The antenna array is aerially translatable. For example, in one embodiment, the antenna array is disposed along the wings of an aircraft which, in operation, flies over the intended target area. A three-dimensional image is generated from a reflected radar signal returned from the surface of an object in response to the transmitted radar signal. The radar system may be incorporated into an aircraft and adapted to detect subsurface objects such as mines buried beneath the surface of the ground as the aircraft traverses over a target area.

Claims

1. A radar system comprising:

an aircraft for detecting buried objects from the air, for overflying a target area of interest;

a radar transmitter, carried by the aircraft, for producing a pulsed radar signal having a carrier frequency of at least three gigahertz;

an array of radar receiving antennas, carried by the aircraft for receiving a reflected signal produced by reflection of said radar signal and forming a real aperture for cross track resolution of the objects; and

a processor for generating a three-dimensional image of said object from the reflected signal.

2. The radar system of claim 1, wherein the radar signal carrier frequency is within a range of three to ten gigahertz.

3. The radar system of claim 1, wherein said processor performs synthetic aperture beam processing based on movement of said radar transmitter and said antenna array relative to the target.

4. The radar system of claim 1, wherein said radar transmitter comprises a frequency-stepped pulse compression radar unit.

5. The radar system of claim 1, wherein said radar transmitter comprises an impulse-modulated radar unit.

6. The radar system of claim 1, wherein said aircraft includes wings and said array is disposed along said wings.

7. The radar system of claim 6, further comprising at least one boom extending laterally outwardly from one of said aircraft wings, wherein the array includes radar receiving antennas disposed along the boom.

8. The radar system of claim 6, wherein said aircraft further comprises first and second booms each extending laterally outwardly from one of said aircraft wings, and said array includes radar receiving antennas disposed along each of said booms.

9. The radar system of claim 8, wherein said booms comprise extendable booms.

10. The radar system of claim 1, wherein the signal processor filters out a portion of the reflected signal corresponding to reflection from the surface of the target area.

11. The radar system of claim 10, wherein the signal processor filters out a portion of the reflected signal corresponding to reflection from the earth'"'"'s surface by range-gating.

12. The radar system of claim 1, wherein said processor comprises an on-board processor disposed on the aircraft.

13. The radar system of claim 1, wherein the processor comprises an off-board processor.

14. The radar system of claim 1, wherein the carrier frequency signal is frequency modulated or phase modulated.

15. The radar system of claim 1, wherein the carrier frequency signal is frequency modulated.

16. The radar system of claim 1, wherein the carrier frequency signal is greater than ten gigahertz.

17. A method for detecting a subsurface object in a target area from an aircraft, said method comprising:

transmitting a pulsed radar signal having a carrier frequency of at least three gigahertz using a radar transmitter disposed on the aircraft;

receiving a return of the transmitted signal reflected by the subsurface object with an array of radar receiving antennas disposed on the aircraft, said array forming a real aperture for cross-track resolution; and

generating a three-dimensional image of said subsurface object based on the received return of the transmitted signal.

18. The method of claim 17, wherein the radar signal frequency is within a range of three to ten gigahertz.

19. The method of claim 17, further comprising the step of identifying the object from the three-dimensional image.

20. The method of claim 19, wherein the step of identifying the object comprises the step of comparing the generated three-dimensional image to a stored image.

21. The method of claim 20, wherein the stored image comprises an image identifiable as a mine.

22. The method of claim 20, wherein the stored image comprises an image identifiable as a mine, munition, or other object of interest.

23. The method of claim 17, wherein the step of transmitting a radar signal comprises selecting a desired transmitting frequency to maximize image resolution.

24. The method of claim 17, further comprising a step of filtering out portions of the return signal corresponding to reflection of the target area surface.

25. The method of claim 17, wherein the carrier frequency signal is greater than ten gigahertz.

26. The method of claim 17, wherein the step of transmitting a pulsed radar signal comprises using a plurality of radar transmitters spaced transversely on the aircraft to transmit a plurality of pulsed radar signals.

27. A method according to claim 17, wherein said transmitter and said receivers have an altitude between about forty feet and about two hundred forty feet during said transmitting and said receiving.

28. A radar system for detecting buried objects from an aircraft overflying a target area of interest, the system comprising:

a radar transmitter being carried by the aircraft, the radar transmitter producing a pulsed radar signal having a carrier frequency of at least three gigahertz;

an array of radar receiving antennas being carried by the aircraft for receiving a reflected signal produced by reflection of said radar signal and forming real aperture for cross-track resolution of the objects; and

a processor for generating a three-dimensional image of said buried object from the reflected signal.

29. A radar system according to claim 28, wherein said array comprises at least three radar receivers.

30. A radar system according to claim 28, wherein said array is densely populated.

31. A radar system according to claim 28, wherein the array receivers have a half wavelength spacing.

32. A radar system according to claim 28, wherein said receiver array has a gain of about 32 dB.