Synthetic aperture radar system having a third order tuned auto compensator for residual antenna motion and method for its use

• US 5,012,249 A
• Filed: 11/28/1989
• Issued: 04/30/1991
• Est. Priority Date: 11/28/1989
• Status: Expired due to Term

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Chan, Yuen-Kwok
• Primary Examiner(s): Barron, Jr., Gilberto
• Application Number:
  US07/442,242
• Time in Patent Office: 518 Days
• Field of Search: 342/25
• US Class Current: 342/25.00A
• CPC Class Codes: G01S 13/9019 Auto-focussing of the SAR signals

Abstract

In a SAR system a method is provided for compensating for antenna residual motion relative to a motion sensor, wherein such residual motion causes phase corruption in a radar image produced by the SAR system. Residual motion compensation is provided by first correlating a received radar signal to a range line having a plurality of azimuth positions. Such signal is transformed into a frequency spectrum indicating the reflectivity of point reflectors at the various azimuth positions. Then, the range line is sampled for symmetric sets of sequential point reflectors positioned along the range line at a consecutive distance from each other corresponding to a specified frequency associated to a mode of residual vibration of the antenna. The amplitude and phase angle of said mode of the antenna residual motion may be obtained from such symmetric sets.

Claims

1. In a SAR system that receives reflections of radar signals from a target region, wherein such signals are combined with position signals from a motion sensor indicating antenna position, with the reflected signals and the position signals being integrated into range lines that may be combined to form a radar image, and wherein there may be residual motion between the antenna and the motion sensor, a method of correcting the position signals from the motion sensor to compensate for the amplitude and phase of antenna residual motion that may cause phase corruption in the radar image, the method comprising the steps of:

a. transforming a received radar signal into a range line having a plurality of azimuth positions,

b. transforming said received signal into a frequency spectrum f indicating the reflectivity of point reflectors at said azimuth positions, wherein one point reflector is located at each azimuth position, and wherein each point reflector is represented by a complex number having a certain magnitude and phase angle;

c. sampling the range line for substantially symmetric sets of point reflectors separated consecutively from each other by a distance corresponding to a frequency θ

, wherein said frequency corresponds to a mode of residual vibration of the antenna, and wherein said substantially symmetric set includes a main lobe point reflector, a pair of first order point reflectors, and a pair of second order point reflectors, each of said point reflectors being represented by a complex number, with said main lobe point reflector being centrally positioned between said pairs of first and second order point reflectors,

d. calculating a product of a predetermined threshold with the greater magnitude of the two complex numbers f(x-θ

) and f(x+θ

), representing the pair of first order point reflectors,

e. comparing the product with the magnitude of the complex number f(x) representing the main lobe point reflector,

f. establishing first and second criteria of a symmetry relation, depending upon whether the magnitude of the complex number representing the main lobe point reflector is greater or less than the product of the predetermined threshold with the greater magnitude of the two complex numbers representing the pair of first order point reflectors,

g. determining whether the complex numbers representing the main lobe point reflector, the pair of first order point reflectors, and the pair of second order point reflectors meet the first or second symmetry relation, depending upon the result of the comparison of step e,

h. calculating estimates of the amplitude and phase of the antenna residual motion, depending upon the result of the comparison of step e,

i. generating an antenna residual motion signal therefrom, and

j. combining the antenna residual motion signal with the position signals from the motion sensor, to correct for antenna residual motion between the motion sensor and the antenna.

2. The method of claim 1 wherein the first criterion is that -f(x-θ

) and f(x+θ

) are approximately mirror images of each other relative to a line in the complex plane through the origin and f(x).

3. The method of claim 1 wherein the second criterion is the simultaneous satisfaction of the following approximate equivalances:

(i) |f(x-θ

)|˜

|f(x+θ

)|,

(ii)|f(x-2θ

)|˜

|f(x+2θ

),

(iii) Angle of -f(x-θ

)-f(x-2θ

)˜

angle of f(x+2θ

)-f(x+θ

), and

(iv) Angle of f(x+θ

)-f(x-θ

)˜

twice the angle of f(x+2θ

)-f(x+θ

),

where, for two numbers u and v, the symbol u˜

v means |u-v|<

ε

1 (1+|u|+|v|) for some threshold ε

₁, and where all angles take values in the interval [0,2π

).

4. The method of claim 3 wherein the first criterion is that -f(x-θ

) and f(x+θ

) are approximately mirror images of each other relative to a line in the complex plane through the origin and f(x).

5. The method of claim 2 wherein estimates G_k are produced, the G_k being estimates for J_k (z)exp(jka)/J₀ (z) and being averaged from values of f(x+kθ

)/f(x), the phase angle a is estimated from the angle of G₁ -G₀,G₀ -G_-1, -G₁ -G_-2, or G₂ -G₁, or from a combination of these angles, and the magnitude z is estimated by z=2G₁ exp (-ja)/[1+G₂ exp (-2ja)] when 1+G₂ exp (-2ja) is not approximately zero, or by z=4G₂ exp (-ja)/(G₁ +G₃ exp (-2ja)) if 1+G₂ exp (-2ja) is approximately zero.

6. The method of claim 3 wherein estimates h_k are produced, the h_k being the respective estimates h_k for J_k (z)exp(jka)/J₀ (z) (k=-2, -1, 0, 1, 2) are being generated by dividing the symmetric quintuple set f(x-2θ

), f(x-θ

), f(x), f(x+θ

), and f(x+2θ

) by f(x+θ

) and rotating the resulting complex numbers by the angle given in condition iii), the phase angle a is estimated from the angles of -H_-1 -H_-2, or half the angle of H₁ +H_-1, or the angle of H₂ -H₁, or from a combination of these angles, and the magnitude z is estimated by

space="preserve" listing-type="equation">z=2/(H.sub.o +H.sub.2 exp (-2ja)).

7. An autocompensator for an SAR system that receives reflections of radar signals from a target region, wherein such signals are combined with position signals from a motion sensor indicating antenna position, with the reflected signals and the position signals being integrated into range lines that may be combined to form a radar image, and wherein there may be residual motion between the antenna and the motion sensor, the autocompensator comprising:

means for transforming a received radar signal into a range line having a plurality of azimuth positions,

means for transforming said received signal into a frequency spectrum f indicating the reflectivity of point reflectors at said azimuth positions, wherein one point reflector is located at each azimuth position, and wherein each point reflector is represented by a complex number having a certain magnitude and phase angle;

means for sampling the range line for substantially symmetric sets of point reflectors separated consecutively from each other by a distance corresponding to a frequency θ

, wherein said frequency corresponds to a mode of residual vibration of the antenna, and wherein said substantially symmetric set includes a main lobe point reflector, a pair of first order point reflectors, and a pair of second order point reflectors, each of said point reflectors being represented by a complex number, with said main lobe point reflector being centrally positioned between said pairs of first and second order point reflectors,

means for calculating a product of a predetermined threshold ε

with the greater magnitude of the two complex numbers f(x-θ

) and f(x+θ

), representing the pair of first order point reflectors,

means for comparing the product with the magnitude of the complex number f(x) representing the main lobe point reflector,

means for establishing first and second criteria of a symmetry relation, depending upon whether the magnitude of the complex number representing the main lobe point reflector is greater or less than the product of the predetermined threshold with the greater magnitude of the two complex numbers representing the pair of first order point reflectors,

means for determining whether the complex numbers representing the main lobe point reflector, the pair of first order point reflectors, and the pair of second order point reflectors meet the first or second symmetry relation, depending upon the result of the comparison of the product with the magnitude of the complex number f(x) representing the main lobe point reflector,

means for calculating estimates of the amplitude and phase of the antenna residual motion, depending upon the result of the comparison of the product with the magnitude of the complex number f(x) representing the main lobe point reflector, and

means for generating an antenna residual motion signal therefrom,

wherein the autocompensator corrects the position signals from the motion sensor to compensate for the amplitude and phase of antenna residual motion that may cause phase corruption in the radar image.

8. The autocompensator of claim 7 wherein the means for transforming said received signal into a frequency spectrum f is a means for performing a discrete Fourier transform.

9. The autocompensator of claim 8 wherein the means for performing a discrete Fourier transform is a means for performing a fast Fourier transform.

10. The autocompensator of claim 7 wherein the means for sampling the range line, the means for calculating a product of a predetermined threshold ε

with the greater magnitude of the two complex numbers f(x-θ

) and f(x+θ

), the means for comparing the product with the magnitude of the complex number f(x) representing the main lobe point reflector, the means for establishing first and second criteria of a symmetry relation, the means for determining whether the complex numbers representing the main lobe point reflector, the pair of first order point reflectors, and the pair of second order point reflectors meet the first or second symmetry relation, the means for calculating estimates of the amplitude and phase of the antenna residual motion, and the means for generating an antenna residual motion signal are a programmed computer.

11. An SAR system, comprising:

means for transmitting radar signals to a target region;

means for receiving the reflections of the radar signals from the target region;

means for producing position signals from a motion sensor indicating antenna position;

an autocompensator comprising;

means for transforming a received radar signal into a range line having a plurality of azimuth positions,

means for transforming said received signal into a frequency spectrum f indicating the reflectivity of point reflectors at said azimuth positions, wherein one point reflector is located at each azimuth position, and wherein each point reflector is represented by a complex number having a certain magnitude and phase angle,

means for sampling the range line for substantially symmetric sets of point reflectors separated consecutively from each other by a distance corresponding to a frequency θ

, wherein said frequency corresponds to a mode of residual vibration of the antenna, and wherein said substantially symmetric set includes a main lobe point reflector, a pair of first order point reflectors, and a pair of second order point reflectors, each of said point reflectors being represented by a complex number, with said main lobe point reflector being centrally positioned between said pairs of first and second order point reflectors,

means for calculating a product of a predetermined threshold ε

with the greater magnitude of the two complex numbers f(x-θ

) and f(x+θ

), representing the pair of first order point reflectors,

means for comparing the product with the magnitude of the complex number f(x) representing the main lobe point reflector,

means for establishing first and second criteria of a symmetry relation, depending upon whether the magnitude of the complex number representing the main lobe point reflector is greater or less than the product of the predetermined threshold with the greater magnitude of the two complex numbers representing the pair of first order point reflectors,

means for determining whether the complex numbers representing the main lobe point reflector, the pair of first order point reflectors, and the pair of second order point reflectors meet the first or second symmetry duct with the magnitude of the complex number f(x) representing the main lobe point reflector,

means for calculating estimates of the amplitude and phase of the antenna residual motion, depending upon the result of the comparison of the product with the magnitude of the complex number f(x) representing

means for generating an antenna residual motion signal therefrom; and

means for correcting the position signals from the motion sensor to compensate for the amplitude and phase of antenna residual motion that may cause phase corruption in the radar image.

12. The SAR of claim 11, further comprising means for forming a radar image from the position signals which have been compensated for the amplitude and phase of the antenna residual motion.

13. The SAR of claim 11 wherein the means for transmitting radar signals to a target region comprises oscillator means for generating a stable frequency, transmitter means for modulating a carrier signal at the stable frequency to produce the radar signals, duplexer means connected to the transmitter means for transmitting the radar signal, and antenna means connected to the duplexer means for transmitting the radar signal to the target region.

14. The SAR of claim 11 wherein the means for receiving radar signals from the target region comprises oscillator means for generating a stable frequency, antenna means for receiving the radar signal from the target region, duplexer means connected to the antenna means for transmitting the received radar signal, and receiver means connected to the duplexer means and the oscillator means for producing signals representing the reflections of the radar signals from the target region.

15. The SAR of claim 11 wherein the means for producing position signals from the motion sensor is an inertial navigation system.