In-flight antenna optimization
First Claim
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.
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Accused Products
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.
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Citations
17 Claims
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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:
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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. - View Dependent Claims (2, 3, 4, 5, 6)
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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:
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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.
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8. An aircraft phased array radar system comprising:
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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. - View Dependent Claims (9, 10, 11, 12)
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13. An aircraft phased array radar system comprising:
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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.
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14. An aircraft phased array radar system operative to produce a main beam, comprising:
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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. - View Dependent Claims (15)
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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:
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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.
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17. An aircraft phased array radar system comprising:
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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.
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Specification