Method for cancelling azimuth ambiguity in a SAR receiver

• US 4,853,699 A
• Filed: 11/13/1987
• Issued: 08/01/1989
• Est. Priority Date: 11/13/1987
• Status: Expired due to Fees

• Current Assignee: Hughes Aircraft Company (Rtx Corporation)
• Original Assignee: Hughes Aircraft Company (Rtx Corporation)
• Inventors: Easton, James K.
• Primary Examiner(s): Tarcza, Thomas H.
• Assistant Examiner(s): Hellner, Mark
• Application Number:
  US07/119,938
• Time in Patent Office: 627 Days
• Field of Search: 342/25
• US Class Current: 342/25.00C
• CPC Class Codes: G01S 13/90 using synthetic aperture techniques , e.g. synthetic aperture radar [SAR] techniques
• CPC Class Codes: G01S 13/9092 combined with monopulse techniques

Abstract

A method for cancelling azimuth, i.e., doppler ambiguity, in a SAR receiver on board a moving craft, e.g., an aircraft, which permits a lower PRF, without causing range ambiguity. Radar returns are received on board the craft with an antenna having first and second apertures to produce corresponding first and second return signals. The first return signal is processed over a given time period to generate a first series of component SAR signals representing radar returns from respective cells of an azimuth-range grid. The second return signal is processed over the given time period to generate a second series of component SAR signals representing radar returns from the respective cells of the azimuth-range grid. The component signals, individually weighted, are additively combined to produce a third series of resultant SAR signals representing the radar returns from the respective cells of the azimuty-range grid. The weighted additive combination of the component signals resolves azimuth ambiguity, even though the PRF is less than the minimum PRF prescribed by conventional wisdom.

Claims

1. A method for cancelling azimuth ambiguity in a SAR receiver obtaining radar return signals from cells of an azimuth-range grid on board a moving craft comprising the steps of:

transmitting radar pulses toward the grid at a pulse repetition rate less than (2v)/l sin φ

, where v is the speed of the craft, l is the total antenna length, and φ

is a squint angle between the direction of craft motion and the direction of transmission;

receiving on board the craft radar returns with an antenna having first and second apertures to produce corresponding first and second return signals;

processing the first return signal over a given time period to generate a first series of component SAR signals representing radar returns from the respective cells of said azimuth-range grid;

processing the second return signal over a given time period to generate a second series of component SAR signals representing the radar returns from the respective cells of the grid;

additively combining the respective component signal individually weighted to produce a third signal component SAR signals representing the radar returns from the respective cells of the grid; and

visually displaying the third series of resultant SAR signals in the form of the azimuthrange grid.

2. Apparatus for resolving azimuth ambiguity in a SAR receiver obrtaining radar return signals from cells of an azimith-range grid on board a moving craft comprising:

means for transmitting radar pulses toard the grid at a pulse repetition rate less than (2v)/l sin φ

, where v is the speed of the craft, l is the total antenna length, and φ

is a squint angle between the direction of craft motion and the direction of transmission;

means for receiving on board the craft radar returns with an antenna having first and second apertures to produce corresponding first and second return signals;

means for processing the first return signal over a given time period to generate a first series of component SAR signals representing radar returns from the respective cells of said azimuth-range grid;

means for processing the second return signal over the given time period to generate a second series of component SAR signals representing the radar returns from the respective cells of the grid;

means for visually displaying the third series of resultant SAR signals in the form of the azimuthrange grid.

3. A method for cancelling azimuth ambiguity in a SAR receiver obtaining radar return signals from cells on an azimuth-range grid on board a moving craft comprising the steps of:

transmitting radar pulses toward the grid at a pulse repetition rate of about (4v/3l) sin φ

, where v is the speed of the craft, l is the total antenna length, and φ

is a squint angle between the direction of craft motion and the direction of transmission;

receiving on board the craft radar returns with an N-antenna having first and second apertures to produce corresponding first and second return signals, with N being the number of antenna apertures;

processing the first return signal over a given time period to generate a first series of component SAR signals representing radar returns from the respective cells of said azimuth-range grid;

processing the second return signal over a given time period to generate a second series of component SAR signals representing the radar returns from the respective cells of the grid;

additively combining the respective component signal individually weighted to produce a third signal component SAR signals representing the radar returns from the respective cells of the grid, in which the first and second series, and no others, are combined to produce the third series; and

visually displaying the third series of resultant SAR signals in the form of the azimuth-range grid.

4. Apparatus for resolving azimuth ambiguity in a SAR receiver obtaining radar return signals from cells of an azimuth-range grid on board a moving craft comprising:

means for transmitting radar pulses toward the grid at a pulse repetition rate of about (4v/3l) sin φ

, where v is the speed of the craft, l is the total antenna length, and φ

is a squint angle between the direction of craft motion and the direction of transmission;

means for receiving on board the craft radar returns with an antenna having first and second apertures to produce corresponding first and second return signals;

means for processing the second return signal over the given time period to generate a second series of component SAR signals representing the radar returns from the respective cells of the grid;

means for additively combining the respective component signals individually weighted to produce a third series of component SAR signals representing the radar returns from the respective cells of the grid in which the first and second series, and no others, are combined to produce the third series; and

means for visually displaying the third series of resultant SAR signals in the form of the azimuth-range grid.