System and Method for Correcting Astigmatism Caused by an Aircraft Canopy

• US 20120293861A1
• Filed: 05/18/2011
• Published: 11/22/2012
• Est. Priority Date: 05/18/2011
• Status: Abandoned Application

• Current Assignee: Elbit Systems of America LLC (Elbit Systems Limited)
• Original Assignee: Elbit Systems of America LLC (Elbit Systems Limited)
• Inventors: Harder, James A., Sprague, Michaelene W.
• Application Number:
  US13/110,319
• Publication Number:
  US 20120293861A1
• Time in Patent Office: Days
• US Class Current: 359/356
• CPC Class Codes: G02B 2027/011 comprising device for correcting geometrical aberrations, distortion
• CPC Class Codes: G02B 27/0025 for optical correction, e.g. distorsion, aberration
• CPC Class Codes: G02B 27/0101 characterised by optical features G02B27/0172 takes precedence

Abstract

In a method embodiment, a method for correcting astigmatism caused by an aircraft canopy comprises receiving at a compensator module a plurality of light rays that have been refracted by an aircraft canopy. At least two of the refracted light rays have respective foci different from one another and propagate in respective planes that are substantially perpendicular to one another, such that astigmatism occurs. The method further includes using the compensator module to substantially compensate for the astigmatism by providing astigmatic power to the received plurality of light rays. The method also includes providing the plurality of light rays having the astigmatic power compensation to an imaging module. The imaging module is configured to generate imagery using the plurality of light rays having the astigmatic power compensation.

Claims

1. A method for correcting astigmatism caused by an aircraft canopy, comprising:

determining which one of a plurality of viewing angles through an aircraft canopy corresponds to an optical path of an imaging system configured to be articulated within a cockpit of the aircraft;

accessing data representing an astigmatic power sufficient to substantially compensate for astigmatism associated with the determined one of the plurality of viewing angles through the aircraft canopy, the astigmatism caused by refraction of light by the aircraft canopy; and

providing the astigmatic power to the optical path of the imaging system, the provided astigmatic power substantially correcting the astigmatism caused by the aircraft canopy.

2. The method of claim 1, wherein providing the astigmatic power to the optical path of the imaging system comprises:

determining an orientation angle of a rotatable lens element corresponding to the astigmatic power; and

rotating the lens element until the lens element is oriented at the determined orientation angle.

3. The method of claim 1, wherein providing the astigmatic power to the optical path of the imaging system comprises rotating two lens elements about an axis, the two lens elements configured to rotate with respect to one another such that a difference in the angle of rotation between the two lens elements is within the range of 0 to 90 degrees, inclusively, the 0 and 90 degree differences in the angle of rotation between the two lens elements corresponding to a maximum and a minimum astigmatic power, respectively.

4. The method of claim 1, wherein providing the astigmatic power to the optical path of the imaging system comprises rotating a plurality of lens elements;

and

wherein the provided astigmatic power is substantially equal to twice the maximum power of at least one of the plurality of lens elements.

5. The method of claim 1, wherein providing the astigmatic power to the optical path of the imaging system comprises providing the astigmatic power to the optical path of the helmet-mounted imaging system using a compensator module optically coupled to the helmet-mounted imaging system, the compensator module comprising one or more lens elements each configured to provide a variable amount of astigmatic power to the optical path of the helmet-mounted imaging system.

6. The method of claim 1, wherein the imaging system is coupled to a helmet such that the optical path of the imaging system varies as a function of the orientation of the helmet relative to the aircraft canopy.

7. The method of claim 1, wherein the imaging system is coupled to a goggles such that the optical path of the imaging system varies as a function of the orientation of the goggles relative to the aircraft canopy.

8. The method of claim 1, wherein determining which one of the plurality of viewing angles through the aircraft canopy corresponds to the optical path of the helmet-mounted imaging system is in response to a determination that the optical path of the helmet-mounted imaging system has changed.

9. The method of claim 1, wherein the helmet-mounted imaging system is configured to generate imagery using light rays transmitted along the optical path.

10. A method for correcting astigmatism caused by an aircraft canopy, comprising:

receiving at a compensator module a plurality of light rays that have been refracted by an aircraft canopy, at least two of the refracted light rays having respective foci different from one another and propagating in respective planes that are substantially perpendicular to one another, such that astigmatism occurs;

using the compensator module, substantially compensating for the astigmatism by providing astigmatic power to the received plurality of light rays; and

providing the plurality of light rays having the astigmatic power compensation to an imaging module configured to generate imagery using the plurality of light rays having the astigmatic power compensation.

11. The method of claim 10, wherein the plurality of light rays received at the compensator module each have infrared wavelengths;

and

wherein the imagery generated by the imaging module is night-vision imagery.

12. The method of claim 10, wherein the plurality of light rays received at the compensator module each have wavelengths outside of the visible spectrum comprising 390 nanometers to 750 nanometers, inclusively.

13. The method of claim 10, wherein substantially compensating for the astigmatism by providing astigmatic power to the received plurality of light rays comprises rotating a lens element of the compensator module until the lens element is oriented at an angle corresponding to the astigmatic power compensation.

14. The method of claim 10, wherein substantially compensating for the astigmatism by providing astigmatic power to the received plurality of light rays comprises rotating two lens elements about an axis, the two lens elements configured to rotate with respect to one another such that a difference in the angle of rotation between the two lens elements is within the range of 0 to 90 degrees, inclusively, the 0 and 90 degree differences in the angle of rotation between the two lens elements corresponding to a maximum and a minimum astigmatic power, respectively.

15. The method of claim 10, wherein substantially compensating for the astigmatism by providing astigmatic power to the received plurality of light rays comprises rotating a plurality of lens elements of the compensator module;

and

wherein the astigmatic power compensation provided to the plurality of light rays is substantially equal to twice the maximum power of at least one of the plurality of lens elements.

16. The method of claim 10, wherein substantially compensating for the astigmatism by providing astigmatic power to the received plurality of light rays comprises providing the astigmatic power to the optical path of the helmet-mounted imaging system using a compensator module optically coupled to the helmet-mounted imaging system, the compensator module comprising one or more lens elements each configured to provide a variable amount of astigmatic power to the optical path of the helmet-mounted imaging system.

17. The method of claim 10, wherein the imaging module is fixed to the aircraft such that an optical path of the imaging module is fixed relative to the aircraft canopy.

18. The method of claim 10, wherein the imaging module is not fixed to the aircraft such that an optical path of the imaging module is changeable relative to the aircraft canopy.

19. A system for correcting astigmatism caused by an aircraft canopy, comprising:

a compensator module comprising at least one rotatable lens element, the compensator module configured to;

determine which one of a plurality of viewing angles through an aircraft canopy corresponds to an optical path of an imaging system;

access data representing an astigmatic power sufficient to substantially compensate for astigmatism associated with the determined one of the plurality of viewing angles through the aircraft canopy, the astigmatism caused by refraction of light by the aircraft canopy; and

provide the astigmatic power to the optical path of the imaging system using the plurality of rotatable lens elements, the provided astigmatic power substantially correcting the astigmatism caused by the aircraft canopy.

20. The system of claim 19, wherein the compensator module is further configured to modify the astigmatic power provided by the at least one lens element based at least in part on a determination that the optical path of the imaging system has changed such that a different one of the plurality of viewing angles though the aircraft canopy corresponds to the changed optical path of the imaging system.