Imaging seeker for a spin-stabilized projectile

Patent metadata

Field	Value
Publication number	US-10877489-B2
Application number	US-201815935647-A
Country	US
Kind code	B2
Filing date	Mar 26, 2018
Priority date	Mar 26, 2018
Publication date	Dec 29, 2020
Grant date	Dec 29, 2020

Abstract

Apparatus and associated methods relate to determining a course-correction signal for a spin-stabilized projectile based on a time sequence of images of a scene aligned with and obtained by a forward-looking imager coupled to the projectile. As the projectile rotates, the aligned scenes captured in the images obtained by the forward-looking imager are rotated. The rotation angle of each of the captured scenes corresponds to the spin angle of the projectile at the time of image exposure. Objects in the captured scenes will circle about a rotation center of the time-sequence images. The distances from a rotation center to the objects in the captured scenes, as well as the rotation angles of the captured scenes can be used to generate a course-correction signal so that the projectile can be guided to a target selected from the objects in the captured scene.

First claim

The invention claimed is:

1. An imaging seeker for a spin-stabilized projectile, the imaging seeker comprising:
a forward-looking imager configured to obtain a time-sequence of images of a scene aligned along an optical axis of the forward-looking imager, wherein each of the time-sequence of images is obtained at a capture time and has an image-rotation angle corresponding to a spin angle of the projectile at the capture time;
an image processor configured, for each of the time-sequence of images, to identify a target captured therein, and to determine relative position of the identified target with respect to rotation-center pixel coordinates, the relative position including an image rotation angle;
a signal generator configured to generate, based at least in part on the determined relative position of the identified target with respect to the rotation-center pixel coordinates, a course-correction signal configured to cause the projectile to correct course toward the target; and
a controller configured to control, based on the image-rotation angle(s) of an earlier image(s) of the time sequence of images, the capture time corresponding to a later image of the time-sequence of images so as to control the image-rotation angle of the later image of the time sequence of images.

2. The imaging seeker of claim 1 , wherein the controller is further configured to control the capture time corresponding to the later image of a time-sequence of images such that a difference between the imager-rotation angle of the later image of the time-sequence of images and the image-rotation angle of an earlier image(s) of the time-sequence of images is less than 15 degrees.

3. The imaging seeker of claim 1 , wherein the image processor is further configured to determine whether the identified target is within a guidable range of the projectile.

4. The imaging seeker of claim 1 , wherein the image processor is further configured to identify objects that are within a guidable range of the projectile, and to determine pixel coordinates corresponding to the identified objects.

5. The imaging seeker of claim 4 , wherein the image processor is further configured to assign target priority weights to the identified objects within the guidable range of the projectile.

6. The imaging seeker of claim 5 , wherein the image processor selects the target based on the assigned target priority weights.

7. The imaging seeker of claim 6 , wherein the selected target corresponds to the object assigned with the greatest target priority weight.

8. A method for generating a course-correction signal for a spin-stabilized projectile, the method comprising:
receiving a first image that is obtained at a first capture time, wherein the first image has a first image-rotation angle;
receiving a second image that is obtained at a second capture time subsequent to the first capture time, wherein the second image has a second image-rotation angle;
identifying a target captured within both the first and second images;
determining, for the identified target, relative position of the identified target with respect to rotation-center pixel coordinates for each of the first and second images, the relative position including the first and second image rotation angles, respectively;
generating a course-correction signal based at least in part on the determined relative position of the identified target with respect to the rotation-center pixel coordinates; and
controlling, based on the first capture time and the first image-rotation angle, the second capture time so as to control the second image-rotation angle.

9. The method of claim 8 , further comprising:
controlling the second capture time such that a difference between the first image-rotation angle and the second image-rotation angle is less than 15 degrees.

10. The method of claim 8 , further comprising:
determining whether the identified target is within a guidable range of the projectile.

11. The method of claim 8 , further comprising:
identifying image features that are common to both the first and second images; and
selecting the target from the identified common image features.

12. The method of claim 10 , further comprising:
determining whether each of the identified common image features are within a guidable range of the projectile.

13. The method of claim 12 , further comprising:
assigning target priority weights to the common image features determined to be within the guidable range of the projectile; and
selecting the object assigned with the greatest target priority weight as the target.

14. A system comprising:
a forward-looking imager disposed on a projectile;
a guidance, navigation and control unit (GNC) disposed on the projectile;
one or more processors; and
computer-readable memory encoded with instructions that, when executed by the one or more processors, cause the system to:
receive a first image that is obtained at a first capture time, wherein the first image has a first image-rotation angle;
receive a second image that is obtained at a second capture time subsequent to the first capture time, wherein the second image has a second image-rotation angle;
identify a target captured within both the first and second images;
determine, for the identified target, relative position, including the first and second image rotation angles, of the identified target with respect to rotation-center pixel coordinates for each of the first and second images, respectively;
generate a course-correction signal based at least in part on the determined relative position of the identified target with respect to the rotation-center pixel coordinates; and
control, based on the first capture time and the first image-rotation angle, the second capture time so as to control the second image-rotation angle.

15. The system of claim 14 , wherein the computer-readable memory encoded with instructions that, when executed by the one or more processors, cause the system to:
determine whether the identified target is within a guidable range of the projectile.

16. The system of claim 14 , wherein the computer-readable memory encoded with instructions that, when executed by the one or more processors, cause the system to:
identify image features that are common to both the first and second images; and
select the target from the identified common image features.

17. The system of claim 14 , wherein the computer-readable memory encoded with instructions that, when executed by the one or more processors, cause the system to:
assign target priority weights to the common image features determined to be within the guidable range of the projectile; and
select the selecting the object assigned with the greatest target priority weight as the target.

Assignees

• Simmonds Precision Products

Inventors

• Durand William
• Ell Todd Anthony

Classifications

• F41G7/222

  for spin-stabilized missiles · CPC title

• F41G7/008

  Combinations of different guidance systems · CPC title

• F41G7/2293 Primary

  using electromagnetic waves other than radio waves · CPC title

• F41G7/226

  Semi-active homing systems, i.e. comprising a receiver and involving auxiliary illuminating means, e.g. using auxiliary guiding missiles · CPC title

• F41G7/2253

  Passive homing systems, i.e. comprising a receiver and do not requiring an active illumination of the target · CPC title