VIEW-POINT GUIDED WEAPON SYSTEM AND TARGET DESIGNATION METHOD

• US 20130248647A1
• Filed: 03/21/2012
• Published: 09/26/2013
• Est. Priority Date: 03/21/2012
• Status: Active Grant

• Current Assignee: Rosemount Aerospace, Inc. (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Rosemount Aerospace, Inc. (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Ell, Todd A., Rutkiewicz, Robert D.
• Granted Patent: US 8,525,088 B1
• Time in Patent Office: Days
• US Class Current: 244/3.17
• CPC Class Codes: F41G 3/145 using a target illuminator
• CPC Class Codes: F41G 7/007 Preparatory measures taken before the launching of the guided missiles
• CPC Class Codes: F41G 7/2226 comparing the observed data with stored target data, e.g. target configuration data
• CPC Class Codes: F41G 7/2253 Passive homing systems, i.e. comprising a receiver and do not requiring an active illumination of the target
• CPC Class Codes: F41G 7/2293 using electromagnetic waves other than radio waves

Abstract

A passive guidance system including a viewpoint capture system (VCS) including a first processor in communication with first memory and a first SWIR imager for creating a viewpoint image database having a plurality of images, at least one of the images having a target point. A weapon guidance module is in communication with the VCS and coupled to a weapon. The weapon guidance module includes a second processor in communication with second memory and a second SWIR imager for storing the viewpoint image database and correlating in-flight images from the second SWIR imager to provide guidance commands directing the weapon to the target point.

Claims

1. A weapon guidance system for allowing a forward observer to use a target designator in advance of weapon launch comprising:

a) a viewpoint capture system (VCS) including a first processor in communication with first memory and a first shortwave infrared (SWIR) imager for creating a viewpoint image database having a plurality of images, at least one of the images having a target point being indicated by the target designator; and

b) a guidance module for coupling to a weapon including;

i) second memory for storing the viewpoint image database;

ii) a second shortwave infrared (SWIR) imager for creating in-flight images for storage in the second memory; and

iii) a second processor in communication with the second memory for correlating the images in the viewpoint image database with the in-flight images to generate guidance commands directing the weapon to the target point.

2. A weapon guidance system as recited in claim 1, wherein the target designator only designates the target point during capturing the plurality of images for the viewpoint image database and the first SWIR imager has automatic telescopic optical zooming capability.

3. A weapon guidance system as recited in claim 1, wherein the forward observer manually selects the target point.

4. A weapon guidance system as recited in claim 1, wherein the forward observer verifies the target point of the VCS using a third shortwave infrared (SWIR) imager.

5. A method for guiding a weapon comprising the steps of:

creating a viewpoint image database by using an imaging system to capture a plurality of views of a target point at a plurality of focal lengths;

downloading the viewpoint image database to a guidance module on the weapon;

launching the weapon; and

correlating in-flight weapon images from an on-board imaging system with the plurality of views in the viewpoint image database to determine guidance commands for the weapon to hit the target point.

6. A method as recited in claim 5, wherein a minimal magnification setting image in the viewpoint image database approximately matches an initial in-flight weapon image.

7. A method as recited in claim 5, further comprising the step of automatically tagging an individual pixel within at least one view as the target point.

8. A method as recited in claim 5, wherein the weapon determines a relative location in terms of range to target, bore-site angles, and slant angles for guiding the weapon to the target point based on the correlating step.

9. A method as recited in claim 5, further comprising the step of designating the target point with a forward observation designation system.

10. A method as recited in claim 5, wherein the step of designating the target only occurs during the creating step.

11. A method as recited in claim 5, further comprising the step of determining if passive-only flight to target is possible before launching the weapon.

12. A target designation system comprising:

a viewpoint capture system (VCS) including a first processor in communication with first memory and a first shortwave infrared (SWIR) imager for creating a viewpoint image database having a plurality of images at a plurality of magnification levels, each image with a designated target pixel, wherein at least one of the images has a target point; and

a weapon guidance module in communication with the VCS for coupling to a weapon, the weapon guidance module including a second processor in communication with second memory and a second shortwave infrared (SWIR) imager for storing the viewpoint image database and correlating in-flight images from the second SWIR imager to provide guidance commands directing the weapon to the target point.

13. A target designation system as recited in claim 12, wherein an active forward observer manually selects the target point with a laser target designator (LTD) at a high magnification level and the VCS selects target pixels at all other magnification levels.

14. A target designation system as recitied in claim 13, wherein a laser target tracking system pans the first SWIR imager to hold the active forward observer'"'"'s laser designated target in a respective field-of-view.

15. A target designation system as recited in claim 12, wherein a passive forward observer:

verifies that a laser target designator (LTD) has designated a correct target point using a third shortwave infrared (SWIR) imager; and

captures at least one image and selects the target point in the at least one image then sends the at least one image data with the target point to the VCS, then the VCS matches the at least one transmitted image with at least one of the images captured by the VCS.

16. A target designation system as recitied in claim 12, wherein the target point is selected from identified potential targets based on a metric for priority, tracking success and operator input.

17. A method for designating a target comprising the steps of:

creating a viewpoint image database by using an imaging system to capture a plurality of views of a target point at a plurality of magnification settings;

downloading the viewpoint image database to a weapon guidance module on a weapon before weapon launch; and

automatically tagging an individual pixel within each view as the target point.

18. A method as recited in claim 17, wherein a minimal magnification setting image in the viewpoint image database approximately matches an initial in-flight missile image and the target point is designated only during the creating step.

19. A method as recited in claim 17, further comprising the step of estimating probability of tracking success from launch to final target point in passive-only flight and using a metric based upon the tracking success probability to prioritize target points when multiple potential target points are available.

20. A method as recited in claim 17, further comprising the steps of:

locking on to the target point before launch to ensure the weapon has identified the target point before launch; and

minimizing a laser target designator'"'"'s dwell time on a vicinity of the target point by reducing a designation time on the vicinity to a short initial period during viewpoint image capture.