METHOD AND SYSTEM FOR MAPPING A TARGET SCENE USING SCANNING RADAR

• US 20090231185A1
• Filed: 03/29/2006
• Published: 09/17/2009
• Est. Priority Date: 03/29/2005
• Status: Active Grant

• Current Assignee: Saab AB
• Original Assignee: Saab AB
• Inventors: Hämäläinen, Mikael
• Granted Patent: US 7,586,434 B1
• Time in Patent Office: Days
• US Class Current: 342/25.R
• CPC Class Codes: G01S 13/9019 Auto-focussing of the SAR signals
• CPC Class Codes: G01S 13/9043 Forward-looking SAR

Abstract

A system and method for mapping a target scene by means of scanning radar utilizing the Doppler effect that arises in the event of movement between radar and target scene, where the movement of a platform upon which the radar'"'"'s antenna is mounted is calculated utilizing navigation data obtained for the platform. The system and method can generate high-resolution radar images in an almost forward-looking application. This is achieved by introducing an approach compensation (7), in which the signal quantity received by the radar which is related to transmitted pulses is transformed pulse by pulse to a corresponding movement-corrected signal quantity by displacement in time and phase, dependent upon the platform'"'"'s movement along an imaginary platform movement directed in such a way that the antenna'"'"'s momentary direction is essentially 90° to the direction of the movement of the imaginary platform.

Claims

1-12. -12. (canceled)

13. A method for mapping a target scene from a moving platform, the method comprising:

providing a scanning Doppler radar sensitive to a relative movement between the radar and the target scene;

calculating a movement of a platform on which a radar antenna is mounted utilizing navigation data obtained for the platform; and

approach compensating a radar return signal,

wherein, for approach compensation, a signal quantity related to pulses transmitted and received by the radar is transformed pulse by pulse to a corresponding movement-corrected signal quantity by displacement in time and phase, dependent upon a movement of the platform along an imaginary platform movement direction oriented in such a way that a momentary direction of a radar antenna is oriented at essentially 90°

with respect to a direction of the movement of the imaginary platform.

14. The method of claim 13, wherein said approach compensating is carried out in a frequency plane, and wherein a size in time T and phase G is obtained, respectively, by the correlations:

T=2R/c and

Θ

=(4π

/λ

_c)R,

where R is a distance a respective echo is to be displaced, c is a propagation speed, and λ

_c is a wavelength of the radar return signal.

15. The method of claim 13, wherein the signal quantity is pulse compressed, suitably in combination with a transformation to a movement-corrected signal quantity.

16. The method of claim 13, further comprising:

creating a reference function by;

placing a reference target in a direction of travel of the platform;

illuminating the reference target throughout a whole of a movement of the platform and across all antenna angles;

calculating a phase variation Θ

_ref that has arisen;

creating a reference signal according to S_ref=exp(jΘ

_ref); and

approach compensating S_ref,

wherein the signal quantity is demodulated by multiplication with a conjugate of the reference function.

17. The method of claim 16, wherein the demodulated signal quantity is angle focused by using a calculation-efficient Fourier transform (FFT).

18. The method of claim 17, wherein the angle-focused signal quantity is projected onto a linear frequency scale.

19. The method of claim 13, wherein a scan rate of the scanning radar is kept constant.

20. The method of claim 13, wherein a scan rate of the scanning radar is varied in order to obtain a constant resolution within a scan area.

21. The method of claim 20, wherein the scan rate of the radar ω

_s is determined from the correlation;

${\mathrm{\omega <br><br>}}_s=\frac{2<br><br>{\mathrm{\lambda <br><br>\upsilon <br><br>}}_p}{R_{\mathrm{FSAR}}<br><br>l^2}<br><br>\sin <br><br>\left(\mathrm{\phi <br><br>}\right),$

where λ

corresponds to a wavelength of the signal, v_p is a platform speed, R_FSAR is a beam sharpening factor, l is a physical size of the radar antenna, and φ

is an antenna angle.

22. The method of claim 13, further comprising mapping the target scene within an angular range of approximately ±

30°

during an approach towards a target scene.

23. The method of claim 13, wherein said utilizing navigation data obtained for the platform utilizes data obtained from an INU (IMU+INS) system connected to the platform.

24. The method of claim 13, further comprising utilizing an additional radar-based mapping technique in a portion of a range to be mapped.

25. A system for mapping a target scene from a moving platform, the system comprising:

a scanning Doppler radar and antenna mounted on the moving platform adapted to detect a relative movement between the radar and the target scene;

a navigation circuit on the moving platform;

a movement calculating circuit that calculates a movement of the moving platform utilizing navigation data provided by the navigation circuit, and

a compensating circuit that approach compensates a signal quantity related to pulses transmitted and received by the radar by pulse by pulse transformation to a corresponding movement-corrected signal quantity by displacement in time and phase, dependent upon the movement of the platform along an imaginary platform movement directed in such a way that a momentary direction of the radar antenna is oriented at essentially 90°

with respect to a direction of the movement of the imaginary platform.

26. The system of claim 25, wherein said compensating circuit operates in a frequency plane, and wherein a size in time T and phase G is obtained, respectively, by the correlations:

T=2R/c and

Θ

=(4π

/λ

_c)R,

where R is a distance a respective echo is to be displaced, c is a propagation speed, and λ

_c is a wavelength of the radar return signal.

27. The system of claim 25, further comprising a pulse compression circuit that pulse compresses the signal quantity, suitably in combination with a transformation to a movement-corrected signal quantity.

28. The system of claim 25, further comprising a reference function generating circuit that creates a reference function by:

placing a reference target in a direction of travel of the platform;

illuminating the reference target throughout a whole of a movement of the platform and across all antenna angles;

calculating a phase variation Θ

_ref that has arisen;

creating a reference signal according to S_ref=exp(jΘ

_ref); and

approach compensating S_ref,

wherein the reference function generating circuit demodulates the signal quantity by multiplying a conjugate of the reference function.

29. The system of claim 25, further comprising a Fourier Transform circuit, wherein the FFT circuit angle focuses the demodulated signal quantity by using a calculation-efficient Fourier transform (FFT).

30. The system of claim 25, wherein a scan rate of the scanning radar is kept constant.

31. The system of claim 25, wherein a scan rate of the scanning radar is varied in order to obtain a constant resolution within a scan area.

32. The system of claim 25, wherein said navigation circuit on the moving platform comprises an inertial navigation unit (INU) including an inertial measurement unit (IMU) and an inertial navigation system (INS) system connected to the platform.