Method of generating accurate estimates of azimuth and elevation angles of a target for a phased-phased array rotating radar

• US 20070018882A1
• Filed: 07/19/2005
• Published: 01/25/2007
• Est. Priority Date: 07/19/2005
• Status: Active Grant

• Current Assignee: Raytheon Company (Rtx Corporation)
• Original Assignee: Raytheon Company (Rtx Corporation)
• Inventors: Manoogian, David, Pitstick, Gerald, Cangeme, John
• Granted Patent: US 7,250,902 B2
• Time in Patent Office: Days
• US Class Current: 342/80
• CPC Class Codes: G01S 13/4418 with means for eliminating radar-dependent errors in angle measurements, e.g. multipath effects
• CPC Class Codes: G01S 13/4463 using phased arrays
• CPC Class Codes: G01S 7/2925 by using shape of radiation pattern
• CPC Class Codes: G01S 7/2926 by integration
• CPC Class Codes: G01S 7/4026 Antenna boresight
• CPC Class Codes: G01S 7/403 in azimuth, i.e. in the horizontal plane
• CPC Class Codes: G01S 7/4034 in elevation, i.e. in the vertical plane

Abstract

A method and apparatus for generating accurate estimates of a radar target'"'"'s azimuth and elevation angles for a phased-phased array rotating radar. Scan modulated coherently integrated (SMCI) monopulse curves are generated from a measured one-way transmit antenna pattern and three receive antenna patterns. The SMCI monopulse curves are calculated in advance for the expected beam steers. To utilize the SMCI monopulse curves, two-way Sum, Delta-Azimuth and Delta-Elevation target returns are coherently integrated, the target'"'"'s monopulse ratios calculated, and the SMCI monopulse curves or polynomials used to calculate the target'"'"'s U-offset and V-offset sine-space angles, which are added to the radar'"'"'s beam steer to get an improved estimate of the target'"'"'s sine-space angular position denoted as U_tgt and V_tgt. A coordinate system transformation transforms U_tgt and V_tgt to azimuth and elevation angles in a non-rotating coordinate system.

Claims

1. A method for generating accurate estimates of a radar target'"'"'s azimuth and elevation angles for a rotating monopulse radar comprising the steps of:

measuring an antenna'"'"'s one-way transmit pattern and three receive antenna patterns;

generating two-way Sum, Delta-Azimuth and Delta-Elevation antenna patterns;

translating the coordinates of two-way Sum, Delta-Azimuth and Delta-Elevation antenna patterns to center on a sine-space beam steer;

sampling uniformly the two-way antenna patterns at mid-CPI points of numerous target returns;

coherently integrating over the sine-space trajectories of said target returns;

averaging coherent integration sums of said target returns and plotting said averages at their respective mid-CPI points to produce average gain antenna patterns;

generating U-offset and V-offset scan modulated coherently integrated (SMCI) monopulse curves from average gain patterns;

coherently integrating said two-way Sum, Delta-Azimuth and Delta-Elevation target returns of said antenna patterns;

calculating the target'"'"'s monopulse ratios from said coherently integrated target return measurements;

calculating the target'"'"'s U-offset and V-offset monopulse angles in sine-space using said SMCI monopulse curves;

adding said U-offset and V-offset monopulse angles to a sine-space beam steer to obtain an improved estimate of a target'"'"'s sine-space position denoted as U_tgt and V_tgt; and

transforming said U_tgt and V_tgt to azimuth and elevation angles in a non-rotating coordinate system using coordinate system transformations.

2. The method as recited in claim 1 wherein said step of measuring an antenna'"'"'s one-way transmit pattern and three receive antenna patterns comprises the step of expressing such measurements in a sine-space coordinate system.

3. The method as recited in claim 1, wherein said step of measuring said three receive antenna patterns includes obtaining one-way Sum, Delta-Azimuth, and Delta-Elevation patterns.

4. The method as recited in claim 1 wherein:

said step of transforming said estimates of a target'"'"'s sine-space position, U_tgt and V_tgt, to azimuth and elevation angles in a non-rotating coordinate system comprises the steps of;

calculating W_tgt as

W_tgt=√

{square root over (1−

U_tqt²−

V_tgt²)}

estimating the antenna'"'"'s mid-CPI rotation angle (yaw angle) using resolver transducer measurements taken just prior to the dwell; and

transforming said target'"'"'s sine-space coordinates U_tgt, V_tgt and W_tgt to normalized north-west-up (NWU) coordinates (X_n, Y_n, Z_n) using knowledge of the antennnals rotation and tilt angles at mid-CPI; and

calculating said target'"'"'s NWU azimuth angle (Az_Tgt) and elevation angle (El_Tgt) using the following relationships;

$\mathrm{Az\_Tgt}=\arctan <br><br>\left(\frac{Y_n}{X_n}\right);<br><br>\text{\hspace{1em}<br><br>}<br><br>\mathrm{and}$$\mathrm{El\_Tgt}=\arctan \left(\frac{Z_n}{\sqrt{X_n^2+Y_n^2}}\right).$

5. The method as recited in claim 1 wherein said method comprises the step of fitting polynomials to said monopulse curves using a method of least squares.

6. A method for generating scan modulated coherently integrated (SMCI) monopulse curves comprising the steps of:

measuring an antenna'"'"'s one-way transmit pattern and three receive antenna patterns;

generating two-way Sum, Delta-Azimuth and Delta-Elevation antenna patterns by performing a point by point multiplication of the antenna gain of the one-way transmit pattern with the antenna gains of the three receive patterns;

translating the coordinates of two-way Sum, Delta-Azimuth and Delta-Elevation antenna patterns to center on a sine-space beam steer;

sampling uniformly the two-way antenna patterns at mid-CPI points of numerous target returns;

coherently integrating over the trajectories of said target returns;

averaging coherent integration sums of said target returns and plotting said averages at their respective points; and

generating scan modulated coherently integrated (SMCI) monopulse curves from the Sum, Delta-Azimuth and Delta-Elevation average gain antenna patterns as follows;

generating a U-offset SMCI monopulse curve by taking the real parts of the Delta-Azimuth U-cardinal plane gains divided point-by-point by the Sum U-cardinal plane gains; and

generating a V-offset SMCI monopulse curve by taking the real parts of the Delta-Elevation V-cardinal plane gains divided point-by-point by the Sum V-cardinal plane gains.

7. The method as recited in claim 6 wherein said step of measuring an antenna'"'"'s one-way transmit pattern and three receive antenna patterns comprises the step of expressing such measurements in a sine-space coordinate system.

8. The method as recited in claim 6 wherein said step of measuring said three receive antenna patterns includes obtaining one-way Sum, Delta-Azimuth, and Delta-Elevation patterns.

9. The method as recited in claim 6 wherein said method comprises the step of fitting polynomials to said SMCI monopulse curves using a method of least squares.

10. A method for applying SMCI monopulse polynomials to target returns and determining azimuth and elevation angles in a non-rotating coordinate system comprising the steps of:

coherently integrating two-way Sum, Delta-Azimuth and Delta-Elevation target returns;

calculating the target'"'"'s U-offset and V-offset monopulse ratios from said coherently integrated target return measurements;

calculating the target'"'"'s U-offset and V-offset monopulse angles in sine-space using said SMCI monopulse polynomials;

adding said U-offset and V-offset monopulse angles to a sine-space beam steer to obtain an improved estimate of a target'"'"'s sine-space position denoted as U_tgt and V_tgt; and

transforming said U_tgt and V_tgt to azimuth and elevation angles in a non-rotating coordinate system using knowledge of the antenna'"'"'s yaw and tilt angles and coordinate system transformations.

11. The method as recited in claim 10 wherein:

said step of transforming said estimates of a target'"'"'s sine-space position, U_tgt and V_tgt, to azimuth and elevation angles in a non-rotating coordinate system comprises the steps of;

transforming said target'"'"'s sine-space coordinates to normalized north-west-up (NWU) coordinates (X_n, Y_n, Z_n) and

calculating said target'"'"'s NWU azimuth angle (Az_Tgt) and elevation angle (El_Tgt) using the following relationships;

$\mathrm{Az\_Tgt}=\arctan <br><br>\left(\frac{Y_n}{X_n}\right);<br><br>\text{\hspace{1em}<br><br>}<br><br>\mathrm{and}$$\mathrm{El\_Tgt}=\arctan \left(\frac{Z_n}{\sqrt{X_n^2+Y_n^2}}\right).$

12. A method of producing an average gain pattern for a rotating radar employing coherent integration comprising the steps of:

storing a measured two-way antenna pattern with U and V sine-space coordinates;

translating said antenna coordinates to center on a beam steer;

calculating a W component of said antenna pattern coordinates;

calculating the number of samples in a coherent processing interval (CPI);

calculating a yaw angle scanned in a sampling period;

calculating said yaw angle scanned in said CPI;

calculating a starting yaw angle with respect to the NWU X-axis;

calculating mid-CPI points of numerous target returns in a NWU frame;

coherently integrating over trajectories of said target returns for integration steps one to number of samples in a CPI; and

averaging said coherently integrated pattern of said target returns to obtain an average gain pattern.

13. The method as recited in claim 12 wherein said coherently integrating over trajectories of said target returns comprises the steps of:

determining the antenna yaw angle at each integration step;

calculating sine-space trajectories of said target returns;

interpolating the two-way antenna patterns at said trajectory points; and

coherently integrating by summing the antenna pattern gains at each point in the sine-space trajectories of said target returns and plotting the sums at the mid-CPI points of their respective sine-space trajectories; and

averaging said coherently integrated antenna patterns by dividing the antenna pattern gains by the number of samples in a CPI to produce an average gain two-way antenna pattern.

14. A phased-phased array rotating radar system comprising:

a phased-phased array rotating antenna;

an antenna electronics unit for sending and receiving signals to and from said phased-phased array rotating antenna wherein the direction of radar beams transmitted by said antenna are electronically controlled;

means connected to said antenna electronics unit for processing target return signals and generating transmit command signals;

a signal and data processor for generating estimates of a target azimuth angle and elevation angle including

means for pulse compression of target return signals;

means for coherent integration of compressed pulses;

means for detection processing of said coherently integrated compressed pulses;

means for monopulse processing of detected signals;

means for target tracking;

means for generating array beam steering commands;

a beam steering generator connected to said signal and data processor for generating beam steering commands for said antenna electronics unit;

said signal and data processor for generating estimates of a target azimuth angle and elevation angle comprises means for generating scan modulated monopulse curves from average gain patterns, means for calculating a target'"'"'s monopulse ratios, means for calculating said target'"'"'s U-offset and V-offset monopulse angles, means for adding said U-offset and said V-offset monopulse angles to a sine-space beam steer obtaining estimates of said target'"'"'s angular position (U_tgt and V_tgt); and

means for transforming said estimates U_tgt and V_tgt to said azimuth and elevation angles in a non-rotating coordinate system.