In-flight antenna optimization

• US 5,929,810 A
• Filed: 12/19/1997
• Issued: 07/27/1999
• Est. Priority Date: 12/19/1997
• Status: Expired due to Term

• Current Assignee: Northrop Grumman Systems Corporation (Northrop Grumman Corporation)
• Original Assignee: Northrop Grumman Corporation
• Inventors: Koutsoudis, Theodore, Cermignani, Justine D.
• Primary Examiner(s): Issing, Gregory C.
• Assistant Examiner(s): PHAN, DAO LINDA
• Application Number:
  US08/994,809
• Time in Patent Office: 585 Days
• Field of Search: 342/81, 342/174, 342/154, 342/368, 342/372, 342/373
• US Class Current: 342/373
• CPC Class Codes: H01Q 3/2605 Array of radiating elements provided with a feedback control over the element weights, e.g. adaptive arrays
• CPC Class Codes: H01Q 3/267 Phased-array testing or checking devices

Abstract

A method and system for phased array radar antenna calibration to be made in flight employs a synthesized initial transmission signal having a notch in the main direction of beam. This has the effect of returning reflected receiver signals that are main lobe clutter free, but contain clutter returned solely from the sidelobe radiation. The received clutter data is processed to yield a set of coefficients that, when combined with subsequent radar signal return resulting from a signal having a main lobe, provides a return signal that is free from aircraft induced distortions and misalignments that can result in sidelobe induced false alarms. All data processing is conducted in the time domain rather than the frequency domain, thus, avoiding Doppler frequency foldover problems due to ambiguities from signals received at multiple aspect angles.

Claims

1. A method for optimizing an aircraft phased array radar system, the system being operative to produce a transmit radiation pattern having a main lobe in a desired direction, the method comprising the steps of:

synthesizing a first RF transmission signal having a notch in the desired direction;

transmitting said first transmission signal through the phased array antenna;

receiving through the antenna first RF return signal;

processing said first return signal to compute a set of feeding coefficients having a single feeding coefficient for each element of the array, said processing including the forming of an inverse radiation pattern having the main lobe in place of the notch;

transmitting a second signal having said transmit radiation pattern with said main lobe; and

applying said coefficients to subsequently received return signals to correct for aircraft induced distortions and misalignments.

2. A method as set forth in claim 1, wherein the first transmission signal comprises a single transmit pulse.

3. A method as set forth in claim 1, further comprising the step of placing the notch in the desired location.

4. A method as set forth in claim 1 comprising the further step of superimposing feeding coefficients of one or more scanned sum patterns with one pattern at the boresight, subtracting from each sum pattern an unscanned boresight pattern and computing therefrom a single feeding coefficient for each element of the antenna array.

5. A method as set forth in claim 1, wherein the processing includes collecting one or more received analog signals representing different return ranges and inputting the signals into a optimization adaptive processor for computing the feeding coefficients.

6. A method as set forth in claim 1, wherein the processing is conducted in the time domain thus, avoiding Doppler frequency foldover problems.

7. A method for optimizing an aircraft phased array radar system, the system being operative to produce a transmit radiation pattern having a main lobe in a desired direction, the method comprising the steps of:

synthesizing a first RF transmission signal having a notch in the desired direction;

transmitting said first transmission signal through the phased array antenna;

receiving through the antenna first RF return signal;

processing said first return signal to compute a set of feeding coefficients having a single feeding coefficient for each element of the array;

transmitting a second signal having said transmit radiation pattern with said main lobe; and

applying said coefficients to subsequently received return signals to correct for aircraft induced distortions and misalignments;

wherein the processing includes collecting one or more received analog signals representing different return ranges and inputting the signals into a optimization adaptive processor for computing the feeding coefficients;

utilizing the optimization adaptive processor for computing the feeding coefficients includes the steps of forming a covariance matrix, applying a modified Weiner-Hopf algorithm, computing cross correlation terms, inverting the matrix and post multiplying the matrix by a steering vector for each element in the antenna array.

8. An aircraft phased array radar system comprising:

a means to synthesize an RF transmission signal having a notch in the main beam;

a transmitting means to transmit said signal through the phased array antenna;

a receiving means to receive through the antenna an RF return signal;

a processing means to compute a single feeding coefficient for each element of the array based upon said return signal, said processing means including matrix-forming means operative to provide an inverse radiation pattern having the main lobe in place of the notch;

a means for applying said coefficients to subsequently received return signals to correct for aircraft induced distortions and misalignments.

9. The aircraft phased array radar system as set forth in claim 8, wherein the radar transmission signal is a single transmit pulse.

10. The aircraft phased array radar system as set forth in claim 8, wherein the notch is placed directly about the desired pointing angle.

11. The aircraft phased array radar system as set forth in claim 8, wherein the means to synthesize a transmit pulse includes a means for superimposing feeding coefficients of one or more scanned sum patterns with one pattern at the boresight, a means for subtracting from each sum pattern an unscanned boresight pattern and a means for computing therefrom a single feeding coefficient for each element of the antenna array.

12. The aircraft phased array radar system as set forth in claim 8, wherein the process includes one or more received analog signals representing different return ranges and an optimization adaptive processor utilizing the signals to compute a set of feeding coefficients.

13. An aircraft phased array radar system comprising:

a means to synthesize an RF transmission signal having a notch in the main beam;

a transmitting means to transmit said signal through the phased array antenna;

a receiving means to receive through the antenna an RF return signal;

a processing means to compute a single feeding coefficient for each element of the array based upon said return signal;

a means for applying said coefficients to subsequently received return signals to correct for aircraft induced distortions and misalignments;

wherein the process includes one or more received analog signals representing different return ranges and an optimization adaptive processor utilizing the signals to compute a set of feeding coefficients;

the optimization adaptive processor includes a means for forming a covariance matrix, a means for applying a modified Weiner-Hopf algorithm, a means for computing cross correlation terms, a means for inverting the matrix and means for post multiplying the matrix by a steering vector for each element in the antenna array.

14. An aircraft phased array radar system operative to produce a main beam, comprising:

a means to transmit an RF signal through a phased array antenna with a radiation pattern having a notch;

a means to receive through the antenna an RF return signal;

means to form an inverse radiation pattern having the main lobe in place of the notch; and

a means to apply a set of coefficients to the return signal to correct for aircraft induced distortions and misalignments.

15. The aircraft phased array radar system as set forth in claim 14, wherein the means to apply a set of coefficients include a storage device having stored coefficients for optimization therein, an analog to digital converter to convert the received signal to a digital signal and a means for combining the coefficients and the digital signal to produce a beam formed output with controlled sidelobe response.

16. A method for optimizing an aircraft phased array radar system, the system being operative to produce a transmit radiation pattern having a main lobe in a desired direction, the method comprising the steps of:

synthesizing a first RF transmission signal;

transmitting said first transmission signal through the phased array antenna via a radiation pattern having a notch in the desired direction;

receiving through the antenna a first RF return signal;

processing said first return signal to compute a set of feeding coefficients having a single feeding coefficient for each element of the array, said processing including a time-averaging of said first return signal, a formation of a covariance matrix of the first return signal, and an inversion of the covariance matrix to obtain an inverse radiation pattern having the main lobe in the place of the notch;

transmitting a second signal having said transmit radiation pattern with said main lobe; and

applying said coefficients to subsequently received return signals to correct for aircraft induced distortions.

17. An aircraft phased array radar system comprising:

a means to synthesize an RF transmission signal having a notch in the main beam;

a transmitting means to transmit said signal through the phased array antenna;

a receiving means to receive through the antenna an RF return signal;

a processing means to compute a single feeding coefficient for each element of the array based upon said return signal, said processing including means for time-averaging said return signal, means for forming a covariance matrix of the return signal, and means for inverting the covariance matrix to obtain an inverse radiation pattern having the main lobe in the place of the notch; and

means for applying said coefficients to subsequently received return signals to correct for aircraft induced distortions.