Method and system for real aperture radar ground mapping

• US 4,978,960 A
• Filed: 12/27/1988
• Issued: 12/18/1990
• Est. Priority Date: 12/27/1988
• Status: Expired due to Fees

• Current Assignee: Northrop Grumman Corporation
• Original Assignee: Westinghouse Electric Company LLC (Brookfield Asset Management Incorporated)
• Inventors: Newcomb, Gary L., Brandt, Timothy E., Stevenson, Joseph, Borden, Scott C.
• Primary Examiner(s): Tarcza, Thomas H.
• Assistant Examiner(s): Sotomayor, John B.
• Application Number:
  US07/290,205
• Time in Patent Office: 721 Days
• Field of Search: 342/22, 342/190, 342/191, 342/25, 342/149, 342/154, 342/158
• US Class Current: 342/25.00C
• CPC Class Codes: G01S 13/4454 phase comparisons monopulse, i.e. comparing the echo signals received by an interferometric antenna arrangement
• CPC Class Codes: G01S 13/89 for mapping or imaging
• CPC Class Codes: G01S 13/895 Side looking radar [SLR]

Abstract

A system for real beam radar ground mapping using a monopulse antennae to determine off-boresight angle of target returns. Off-boresight angle is converted to azimuth bins. After processing, return energy for each contiguous azimuth bin of an illuminated area is dumped during a respective "look" of the antenna.

Claims

1. A method of real aperture radar ground mapping, comprising:

scanning a monopulse antenna having a central boresight, over a ground surface area to be mapped;

transmitting along the boresight a plurality of radar pulses, each having a predetermined angular beamwidth, during each of a plurality of spaced azimuth intervals, each azimuth interval defining an antenna look, the transmitted radar pulses during each look illuminating a total ground area in azimuth corresponding to the beamwidth thereof;

receiving and detecting at the antenna, during each look, return energy of the reflected pulses of the illuminated area at distinct times corresponding to respective range intervals;

calculating a predetermined plurality of distinct off-boresight angles of the return energy for each range interval;

converting each of the plurality of calculated off-boresight angles to a different contiguous azimuth bin for each range interval, each azimuth bin corresponding to a fractional portion in azimuth of the total illuminated ground area during each look;

displaying the detected reflected energy of each distinct azimuth bin in successive azimuth bins of the total illuminated ground area for subsequent antenna looks.

2. The method of claim 1, wherein the offboresight angle is calculated in accordance with the ratio of the sum and difference data of the return energy pulses.

3. The method of claim 2, wherein the denominator of the ratio is used as an index in a look up table for performing the division.

4. The method of claim 3, wherein the lookup table includes at least 1K of twelve bit words scaled into fifteen fractional bits.

5. The method of claim 1, wherein the step of calculating includes monopulse processing of the return energy in the horizontal and vertical dimensions between each look of the antenna to obtain horizontal and vertical data;

generating an automatic gain control command during the collecting of the vertical monopulse data for each look in accordance with the value of the horizontal data for the same look; and

processing the horizontal data for each subsequent look in accordance with said generated command for adding to each bin a value corresponding to the strength of the calculated return energy.

11. The method of claim 1, wherein the step of converting the calculated off-boresight angles includes the substeps of converting the horizontal and vertical monopulse data to antenna coordinates to form azimuth and elevation components;

and converting the antenna coordinates to space coordinates.

12. The method of claim 11, wherein the substep of converting the off-boresight angles to antenna coordinates includes space to body transformation and the body to space transformation;

and monopulse slope and curvature compensation.

13. The method of claim 12, wherein the monopulse slope and curvature compensation data is contained in a lookup table.

17. The method of claim 1, wherein the step of displaying includes displaying the return energy of a single bin during each successive look to the antenna.

6. A system for real aperture radar ground mapping, comprising:

a monopulse antenna having a central boresight;

means for scanning the antenna over a ground surface area to be mapped;

means for transmitted along the boresight a plurality of radar pulses, each having a predetermined angular beamwidth, during each of a plurality of spaced azimuth intervals, each interval defining an antenna look, the radar pulses during each look illuminating a total ground area in azimuth corresponding to the beamwidth thereof;

means for receiving and detecting at the antenna, during each look, return energy of the reflected pulses of the illuminated area at distinct times corresponding to respective range intervals;

means for calculating a predetermined plurality of distinct off-boresight angles of the return energy for each range interval;

means for converting each of the calculated off-boresight angles to a different contiguous azimuth bin for each range interval, each azimuth bin corresponding to a fractional portion in azimuth of the total illuminated ground area during each look; and

display means, for displaying the return energy of each distinct azimuth bin in each successive azimuth bin of the total illuminated ground area for subsequent antenna looks.

7. The system of claim 6, wherein the means for calculating the off-boresight angles includes means for determining the ratio of the SUM and DIFFERENCE data of the return energy.

8. The system of claim 7, wherein the ratio determining means includes a lookup table for performing the division.

9. The system of claim 8, wherein the lookup table includes at least 1 k of twelve bit words scaled to fifteen fractional bits.

10. The system of claim 6, wherein the means for receiving and detecting includes means for monopulse processing of the return energy in the horizontal and vertical dimension during each look of the antenna;

and means for generating an automatic gain control during the collecting of the vertical monopulse data between each look in accordance with the horizontal data for the same look; and

means for controlling the processing of the horizontal data for each subsequent look in accordance with said generated command.

14. The system of claim 6, wherein the means for converting the off-boresight angles include means for converting the horizontal and vertical monopulse data to antenna coordinates to form azimuth and elevation components;

and means for converting the antenna coordinates to space coordinates.

15. The system of claim 14, wherein the means for converting the off-boresight angle to antenna coordinates includes means for compensating for the monopulse slope and curvature of the beam.

16. The system of claim 15, wherein the converting means includes lookup tables having monopulse slope and curvature compensation data.

18. The system of claim 14, wherein the means for displaying includes means for displaying the return energy of a single azimuth bin during each look.