Nonlinear scanning to optimize sector scan electro-optic reconnaissance system performance

• US 5,481,479 A
• Filed: 12/10/1992
• Issued: 01/02/1996
• Est. Priority Date: 12/10/1992
• Status: Expired due to Term

• Current Assignee: BAE Systems Information and Electronic Systems Integration Incorporated (BAE Systems Plc)
• Original Assignee: Loral Fairchild Corp. (Newell Brands Inc.)
• Inventors: Wolfe, Gregory J., Wight, Ralph H.
• Primary Examiner(s): Voeltz, Emanuel T.
• Assistant Examiner(s): PIPALA, EDWARD J
• Application Number:
  US07/988,837
• Time in Patent Office: 1,118 Days
• Field of Search: 364/514, 364/516, 364/517, 364/423, 364/456, 364/525, 358/113, 358/109, 358/448, 358/451, 348/144, 348/146, 348/147, 348/98, 348/106, 348/135
• US Class Current: 701/223
• CPC Class Codes: G03B 37/02 with scanning movement of lens or cameras
• CPC Class Codes: H04N 3/30 otherwise than with constant velocity or otherwise than in pattern formed by unidirectional, straight, substantially horizontal or vertical lines

Abstract

Long range, non-linear, sector scan panoramic electro-optical reconnaissance of a scene from an airborne craft is performed at increased aircraft velocities with a given detector technology at a desired level of performance. A focal plane array is configured to detect an image of the scene, and to convert the image into electronic charge information representing the image. A main electronics unit that converts the electronic charge representation into an electronic signal which is a digital representation of the image. A lens arrangement is used to focus a narrow slit of the scene onto the focal plane array, and a rotating prism scans the slit across the scene at a non-linear scanning velocity as determined according to the present invention. The electronic signal is transmitted to a ground station where it is processed to provide visual image data and that represents the scene, distortion induced into this data as a result of the non-linear scan velocity is removed to provide a distortion free final image.

Claims

1. A system for performing long range, sector scan panoramic electro-optical reconnaissance of a scene, the reconnaissance performed at increased scan velocities for a given ground resolved distance and forward overlap, comprising:

(1) a focal plane array configured to detect an image of the scene and to convert said image into an electronic charge representation of said image;

(2) a main electronics unit, coupled to said focal plane array, configured to convert said electronic charge representation into a digital image data signal, wherein said digital image data signal is a digital representation of said image;

(3) focusing means, coupled to said focal plane array, for focusing a portion of the scene onto said focal plane array, wherein said portion of the scene is defined by a projection of said focal plane array;

(4) determining means for determining a non-linear scan velocity;

(5) scanning means. coupled to said focusing means for scanning said projection of said focal plane array across the scene at said non-linear scan velocity; and

(6) processing means, coupled to said main electronics unit, for processing said digital image data signal to provide a visual image signal representing a corrected image, said corrected image having a pixel aspect ratio corrected to remove the effects of said non-linear scan velocity.

2. The system of claim 1, wherein said determining means is configured to determine said non-linear scan velocity using an exact solution, and wherein said exact solution determines said non-linear scan velocity such that a cross-track ground sample distance is kept constant throughout the scan.

3. The system of claim 1, wherein said determining means is configured to determine said non-linear scan velocity using a polynomial approximation.

4. The system of claim 1, wherein said focal plane array is a charge coupled device matrix, said focusing means is an optical camera, and said scanning means is a rotating camera barrel.

5. The system of claim 1, further comprising an airborne craft for supporting said focal plane array, said main electronics unit and said focusing means said determining means, said scanning means and said processing means.

6. The system of claim 1, further comprising an air-to-ground data link coupled between said focal plane army and said fourth means, for transmitting said electronic signal from said airborne craft to a ground station.

7. The system of claim 1, further comprising a data base, coupled to said main electronics unit, for storing digital image data signal.

8. The system of claim 1, further comprising means, coupled to said means for displaying said corrected image.

9. The system of claim 1, further comprising fifth means, coupled to said focal plane array, for compressing said digital image data signal to form a compressed digital image data signal, and sixth means, coupled to said fifth means, for decompressing said compressed digital image data to reproduce said digital image data signal.

10. A method for optimizing long range, sector scan panoramic electro-optical reconnaissance of a scene from an airborne craft comprising the steps of:

(1) determining a camera scan rate and a focal plane array read rate for a desired level of operational performance;

(2) determining a non-linear scan velocity if said scan rate is above a threshold level;

(3) scanning the camera across the scene at said non-linear scan velocity determined in step (2);

(4) focusing an image of the scene scanned in said step (3) onto a focal plane array and converting the image into an electronic signal that represents the scene;

(5) processing said electronic signal to generate a digital image of the scene, wherein said processing comprises a step of correcting a pixel aspect ratio of said digital image to remove effects of said non-linear scan velocity.

11. The method of claim 10, further comprising the step of displaying said corrected image.

12. The method of claim 10, wherein said step (1) comprises the steps of:

(a) determining an actual scan time used;

(b) determining a system line rate;

(c) calculating the number of lines in a scan, wherein the calculation is made using said actual scan time determined in said step (a) and said system line rate determined in said step (b); and

(d) determining an end-of-frame time as a ratio of said number of lines in a scan to said line rate.

13. The method of claim 10, wherein said step (1) comprises the steps of:

(a) determining an actual scan time used;

(b) determining a desired number of lines in a scan;

(c) calculating a system line rate as a ratio of said number of lines determined in said step (b) to said actual scan time used determined in said step (a); and

(d) determining an end-of-frame time as a ratio of said number of lines in a scan to said line rate.

14. The method of claim 12, wherein said step for determining said actual scan time used comprises the steps of:

(i) determining a slant range;

(ii) computing an in-track distance in a near-field, wherein said in-track distance is a function of said slant range determined in said step (i)

(iii) computing a cycle time as a fraction of said in-track distance computed in said step (ii), wherein said fraction is determined to provide a desired amount of forward overlap;

(iv) calculating available a scan time as a function of said cycle time; and

(v) calculating said actual scan time used as a function of said available scan time.

15. The method of claim 13, wherein said step for determining said scan time used comprises the steps of:

(i) determining a slant range;

(ii) computing an in-track distance in a near-field, wherein said in-track distance is a function of said slant range determined in said step (i)

(iii) computing a cycle time as a fraction of said in-track distance computed in said step (ii), wherein said fraction is determined to provide a desired amount of forward overlap;

(iv) calculating an available scan time as a function of said cycle time; and

(v) calculating said actual scan time used as a function of said available scan time.

16. The method according to claim 10, wherein said step (2) comprises the steps of:

(a) computing a cross-track ground sample distance;

(b) computing an angular scan velocity needed to keep said

cross-track ground sample distance constant;

(c) calculating a camera depression angle as a function of time based on said angular scan velocity; and

(d) differentiating said depression angle calculated in said step (c) to obtain a non-linear scan velocity.

17. The method according to claim 10, wherein said step (2) comprises the steps of:

(a) calculating a cross-track ground sample distance required to maintain a constant overall ground sample distance;

(b) holding said cross-track ground sample distance constant for large depression angles;

(c) computing an angular scan velocity required to maintain said cross-track ground sample distance;

(d) calculating a camera depression angle as a function of time based on said angular scan velocity; and

(e) differentiating said depression angle calculated in said step (c) to obtain a non-linear scan velocity.

18. The method according to claim 10, wherein said step (2) comprises the step of using a quadratic polynomial approximation to determine a non-linear scanning velocity.

19. The method according to claim 10, wherein said step (5) comprises the steps of:

(a) deriving a correction for said pixel aspect ration of said digital image; and

(b) implementing said correction to correct said pixel aspect ratio.

20. The method according to claim 19, wherein said step (a) comprises the steps of:

(i) computing an averaging factor to produce minified view images;

(ii) computing a line group angle as the product of said averaging factor and a detector angle;

(iii) determining a third-order polynomial approximation of time as a function of an angle scanned since the scan was started; and

(iv) determining a full resolution line group based on said line group angle using said third-order polynomial; and

said step (b) comprises the steps of;

(i) evaluating said full resolution line group;

(ii) rounding said full resolution line group to a nearest integer value; and

(iii) adding the amount of the rounding to a next value for said full resolution line group.

21. A system for performing long range, sector scan panoramic electro-optical reconnaissance of a scene from an airborne craft, the reconnaissance performed at increased scan velocities for a given ground resolved distance, and forward overlap, comprising:

first means for detecting an image of a portion of the scene and converting said image into a digital image data signal, wherein said digital image data signal is a digital representation of said image;

second means, coupled to said first means, for focusing said portion of the scene onto said first means, and for scanning said portion of the scene across the entire scene at a non-linear scan velocity; and

third means, coupled to said first means, for processing said digital image data signal to provide a visual image data signal representing a corrected image, said corrected image having a pixel aspect ratio corrected to remove the effects of said non-linear scan velocity.

22. The system of claim 21, further comprising fourth means, coupled to said second means, configured to use an exact solution to determine said non-linear scan velocity, and wherein said exact solution determines said non-linear scan velocity such that a cross-track ground sample distance is constant throughout the scan.

23. The system of claim 21, further comprising fourth means, coupled to said second means, configured to use a polynomial approximation solution to determine said non-linear scan velocity.

24. The system of claim 21, further comprising fourth means, coupled to said first means, for transmitting said digital image data signal from the airborne craft to the ground.

25. The system of claim 21, further comprising fourth means, coupled to said first means, for storing said digital image data signal.

26. The system of claim 21, further comprising fourth means, coupled to said third means, for displaying said corrected image.

27. The system of claim 21, further comprising fourth means, coupled to said focal plane array, for compressing said digital image data signal to form a compressed digital image data signal, and fifth means, coupled to said fourth means, for decompressing said compressed digital image data signal.

28. A system for performing sector scan reconnaissance of a scene, comprising:

focusing means for focusing a portion of the scene onto a detector, wherein said portion of the scene is defined by a projection of said detector;

determining means for determining a non-linear scan velocity and;

scanning means for scanning said projection across the scene at said determined-non-linear scan velocity.

29. The system of claim 28, wherein said determining means comprises means for determining said non-linear scan velocity using an exact solution.

30. The system of claim 28, wherein said determining means comprises means for determining said non-linear scan velocity using a polynomial approximation.