Multiplatform GMTI radar with adaptive clutter suppression

• US 9,772,402 B2
• Filed: 06/09/2014
• Issued: 09/26/2017
• Est. Priority Date: 06/09/2014
• Status: Active Grant

• Current Assignee: SRC, Inc.
• Original Assignee: SRC, Inc.
• Inventors: Schuman, Harvey K., Li, Ping G.
• Primary Examiner(s): Windrich, Marcus
• Application Number:
  US14/299,399
• Publication Number:
  US 20170102458A1
• Time in Patent Office: 1,205 Days
• Field of Search: 342 17, 342 59, 342160, 342161
• CPC Class Codes: G01S 13/003 Bistatic radar systems; Multistatic radar systems
• CPC Class Codes: G01S 13/5244 Adaptive clutter cancellation specially adapted for airborne MTI, G01S13/5242
• CPC Class Codes: G01S 13/87 Combinations of radar systems, e.g. primary radar and secondary radar
• CPC Class Codes: G01S 7/288 Coherent receivers
• CPC Class Codes: G01S 7/414 Discriminating targets with respect to background clutter

Abstract

The present invention is directed to a ground moving target (GMTI) radar that can detect targets, including dismounts, with very small minimum detectable velocities by combining signals from antennas on different spatially separated platforms in a main beam clutter-suppressing spatially adaptive process without requiring that the relative positions of the antenna phase centers be accurately tracked. The clutter nulling is in addition to that provided by the Doppler filters. The spatial displacement provides a narrow main beam clutter null reducing undesired target suppression. The clutter-suppressing spatially adaptive structure is used in both the sum and delta channels of the monopulse processor so that the beam distortion caused by the spatial nulling is compensated for, and the monopulse look-up process is preserved to maintain angle accuracy. Noncoherent integration is employed to recover signal to noise loss resulting from the uncertain relative locations of the platforms.

Claims

1. A radar system comprising:

a data input portion including a first channel configured to receive first radar return samples from a first GMTI radar receiver disposed on a first mobile platform and at least one second channel configured to receive second radar return samples from at least one auxiliary GMTI radar receiver disposed on at least one second mobile platform, the first mobile platform and the at least one second mobile platform defining a distributed array, the first radar return samples and the second radar return samples corresponding to radar return signals originating from a radar transmitter;

a non-adaptive processing portion coupled to the data input portion, the non-adaptive portion being configured to derive Doppler filtered radar return samples that include a plurality of first clutter signals from the first radar return samples, a plurality of second clutter signals from the second radar return samples and a target signal, the plurality of second clutter signals being characterized by at least one phase delay relative to the plurality of first clutter signals; and

an adaptive processing portion coupled to the non-adaptive processing portion, the adaptive processing portion being configured to calculate a weight value as a function of the plurality of first clutter signals and the plurality of second clutter signals but not the phase delay, the weight value being employed in a weight vector w for a space-time adaptive processing (STAP) filter that applies the weight vector w to a signal vector corresponding to the Doppler filtered radar return samples, the STAP filter implementing an open loop feedback configured to create beam pattern nulls at angles corresponding to a plurality of first interference signals within each of the Doppler bins without substantially tracking a position or velocity of the first airborne platform or the at least one second airborne platform.

2. The system of claim 1, wherein the plurality of first clutter signals and the plurality of second clutter signals include clutter, noise or other interference signals.

3. The system of claim 1, wherein the plurality of first clutter signals and the plurality of second clutter signals substantially correspond to a predetermined range and predetermined Doppler frequency.

4. The system of claim 1, wherein the first mobile platform and the at least one second mobile platforms include an airborne platform or spaceborne platform.

5. The system of claim 1, wherein the at least one second airborne platform includes a plurality of second airborne platforms and the at least one auxiliary GMTI radar receiver includes a plurality of GMTI radar receivers.

6. The system of claim 1, wherein the first airborne platform and the at least one second airborne platforms are separated by a cross range dimension (Δ

Y) that is within a range of about 5-20 wavelengths (λ

) of a transmitted radar signal.

7. The system of claim 1, wherein a potential target range is at least several times the altitude of the first airborne platform or the at least one second airborne platforms.

8. The system of claim 1, wherein a lateral separation dimension (Δ

X) and an altitude separation between the first airborne platform and the at least one second airborne platforms is substantially unconstrained.

9. The system of claim 1, wherein the data input portion is disposed on either the first platform or the at least one second platform.

10. The system of claim 7, wherein the non-adaptive processing portion and the adaptive processing portion are disposed at a location remote from the data input portion, and wherein the data input portion provides the first coherent radar return samples and the second radar return samples via a data link.

11. The system of claim 1, wherein the data input portion, the non-adaptive processing portion and the adaptive processing portion are disposed at a location remote from the first GMTI radar receiver or the at least one auxiliary GMTI radar receiver, and wherein the first coherent radar return samples and the second radar return samples are provided to the data input portion via a data link.

12. The system of claim 1, wherein the radar transmitter is configured as a monostatic radar transmitter or as a bistatic radar transmitter.

13. The system of claim 12, wherein the bistatic radar transmitter is disposed aboard a separate and remote airborne or spaceborne platform.

14. The system of claim 1, wherein the adaptive processing portion is configured to provide a clutter plus noise signal based on a linear combination of the plurality of first interference signals and a plurality of second interference signals.

15. The system of claim 1, wherein a linear combination of the first clutter signal and the second clutter signal is substantially equal to y(θ

_c)=x₁(θ

_c)+w*x₂(θ

_c), where x₁(θ

_c) and x₂(θ

_c) are the plurality of first clutter signals and the plurality of second clutter signals, respectively, and θ

_c denotes the angle of a clutter direction vector relative to the distributed array boresight, and wherein w* is the complex conjugate of the weight vector w that maintains target signal strength while minimizing the mean square value of the clutter signal.

16. The system of claim 15, wherein a target signal in a linear combination of the first channel and the at least one second channel is given by:

y(θ

_t)=e_tf₁(θ

_t)+n₁+w*(e_texp(jψ

_t)f₂(θ

_t)+n₂),

wherein e_t is a complex target spectral component, f₁(θ

_t) and f₂(θ

_t) are complex antenna patterns of the first GMTI radar receiver and the at least one second GMTI radar receiver, respectively, and wherein e_t [exp (jψ

_t)] is a complex target spectral component including the phase delay between the first GMTI radar receiver and the at least one second GMTI radar receiver, and wherein n₁ and n₂ are the first GMTI radar receiver noise and the at least one second GMTI radar receiver noise, respectively.

17. The system of claim 16, wherein the weight vector w is a mean square average given by:

w=−

|x*₁(θ

_c)|²/|x*₂(θ

_c)|² wherein x₁*(θ

_c) and x₂*(θ

_c) are the complex conjugates of x₁(θ

_c) and x₂(θ

_c), respectively.

18. The system of claim 17, wherein the mean square average is approximated by collecting several range cells of the plurality of first clutter signals and the plurality of second clutter signals.

19. The system of claim 16, wherein the wherein the weight vector w is a covariance matrix given by:

w=R<sup>−

1</sup>s

where R denotes the interference plus noise covariance matrix and s denotes the steering vector that need not be matched to the target vector.

20. The system of claim 19, wherein the adaptive processing portion provides an output signal, the output signal being given by:

y=w^Hx for a data vector x under test for a target.

21. The system of claim 1, wherein a relative position or a relative velocity of the first airborne platform or the at least one second airborne platform are known only to within a few range cells and Doppler bins from navigation data.

22. The system of claim 1, wherein the application of the weight vector w to a signal vector automatically coheres the plurality of first clutter signals and the plurality of second clutter signals to substantially cancel the plurality of first clutter signals and the plurality of second clutter signals and maintain the target signal strength.

23. A method for processing radar signals in a distributed array radar that includes a first GMTI radar receiver, disposed on a first airborne platform, configured to receive first radar return samples and at least one auxiliary GMTI radar receiver, disposed on at least one second airborne platform, configured to receive second radar return samples, the first airborne platform and the at least one second airborne platform defining a distributed array, the method including:

obtaining Doppler filtered radar return samples that include a plurality of first clutter signals from the first radar return samples, a plurality of second clutter signals from the second radar return samples and a target signal, the plurality of second clutter signals being characterized by at least one phase delay relative to the plurality of first clutter signals;

calculating a weight value as a function of the plurality of first clutter signals and the plurality of second clutter signals but not the phase delay, the weight value being employed in a weight vector w for a space-time adaptive processing (STAP) filter;

applying the weight vector w to a signal vector corresponding to the Doppler filtered radar return samples; and

implementing an open loop feedback configured to create beam pattern nulls at angles corresponding to a plurality of first interference signals within each of the Doppler bins without substantially tracking a position or velocity of the first airborne platform or the at least one second airborne platform.

24. The method of claim 23, further comprising:

identifying a target characterized by a target range and a target velocity relative to the first airborne platform and a target angle relative to the distributed array; and

receiving the first radar return samples from the first GMTI radar receiver and the second radar return samples from the at least one auxiliary GMTI radar receiver, the first radar return samples and the second radar return samples corresponding to radar return signals originating from one radar transmitter.

25. The method of claim 23, wherein the plurality of first clutter signals and the plurality of second clutter signals include clutter, noise or interference signals.

26. The method of claim 23, wherein the plurality of first clutter signals and the plurality of second clutter signals substantially correspond to a predetermined range and predetermined Doppler frequency.

27. The method of claim 23, wherein the radar transmitter is configured as a monostatic radar transmitter or as a bistatic radar transmitter.

28. The method of claim 23, wherein a clutter signal is provided based on a linear combination of the plurality of first interference signals and the plurality of second interference signals.

29. The method of claim 23, wherein the clutter signal is substantially equal to y(θ

_c)=x₁(θ

_c)+w*x₂(θ

_c), where x₁(θ

_c) and x₂(θ

_c) are the plurality of first clutter signals and the plurality of second clutter signals, respectively, and θ

_c denotes the angle of a clutter direction vector relative to the distributed array boresight, and wherein w* is the complex conjugate of the weight vector w that maintains target signal strength while minimizing the mean square value of the clutter voltage.

30. The method of claim 28, wherein a target signal in a linear combining of the first channel and the at least one second channel is given by:

y(θ

_t)=e_tf₁(θ

_t)+n₁+w*(e_texp(jψ

_t)f₂(θ

_t)+n₂),

wherein e_t is a complex target spectral component, f_t(θ

_t) and f₂(θ

_t) are complex antenna patterns of the first GMTI radar receiver and the at least one second GMTI radar receiver, respectively, and wherein e_t [exp (jψ

_t)] is a complex target spectral component including the phase delay between the first GMTI radar receiver and the at least one second GMTI radar receiver, and wherein n₁ and n₂ are the first GMTI radar receiver noise and the at least one second GMTI radar receiver noise, respectively.

31. The method of claim 29, wherein the weight vector w is a mean square average given by:

w=−

|x*₁(θ

_c)|²/|x*₂(θ

_c)|² wherein x₁*(θ

_c) and x₂*(θ

_c) are the complex conjugates of x₁(θ

_c) and x₂(θ

_c), respectively.

32. The method of claim 30, wherein the mean square average is approximated by collecting several range cells of the plurality of first clutter signals and the plurality of second clutter signals.

33. The method of claim 29, wherein the weight vector w is a covariance matrix given by:

w=R<sup>−

1</sup>s, where R denotes the interference plus noise covariance matrix and s the steering vector that need not be matched to the target vector.

34. The method of claim 29, further comprising the step of providing an output signal, the output signal being given by:

y=^Hx for a data vector x under test for a target.

35. The method of claim 23, wherein a relative position or a relative velocity of the first airborne platform or the at least one second airborne platform are known only to within a few range cells and Doppler bins from navigation data.

36. The method of claim 23, wherein the application of the weight vector w to a signal vector automatically coheres the plurality of first clutter signals and the plurality of second clutter signals to substantially cancel the plurality of first clutter signals and the plurality of second clutter signals and maintain the target signal strength.