Hardware-in-the-loop tow missile system simulator

• US 5,224,860 A
• Filed: 03/01/1991
• Issued: 07/06/1993
• Est. Priority Date: 03/01/1991
• Status: Expired due to Fees

• Current Assignee: Electronic Arts Incorporated
• Original Assignee: Electronic Arts Incorporated
• Inventors: Wootton, John R., Waldman, Gary S., Hobson, Gregory L., Holder, David L.
• Primary Examiner(s): Apley, Richard J.
• Assistant Examiner(s): CHENG, JOE H
• Application Number:
  US07/662,936
• Time in Patent Office: 858 Days
• Field of Search: 434/11, 434/12, 434/16, 434/17, 434/19, 434/20, 434/21, 434/23, 434/27, 434/22, 273/312, 273/333, 273/348.1, 358/125, 358/103-105, 340/702, 250/223 B, 250/224, 250/330, 353/98, 353/66, 353/11, 353/12, 356/241, 356/445, 359/641
• US Class Current: 434/21
• CPC Class Codes: F41G 7/006 Guided missiles training or simulation devices

Abstract

A "hardware-in-the-loop" simulator (10) for training people in the use of a missile system to teach target acquisition, missile launch, and missile guidance under simulated battlefield conditions. A battlefield environment (E) including at least one target (T) movable therewithin is created by a simulation module (12). Missile system hardware (H) including the missile acquisition, tracking, and guidance portions is provided. An interface module (20) converts signals produced by the simulating module to an infrared image acceptable by the hardware. The resultant image represents a field-of-view (FOV), including the target, within the battlefield environment. An image module (32) produces a dynamic image representative of the missile'"'"'s position in the field-of-view. This image is observable by the hardware which utilizes it to determine the position of the missile relative to the target. The hardware also determines if a missile guidance signal is to be sent to the missile to guide it to the target. If so, the interface module is responsive to the guidance signal to simulate, in real-time, the response of the missile to the guidance signal.

Claims

1. A "hardware-in-the-loop" simulator for training people in the use of a missile system to teach target acquisition, missile launch, and missile guidance under simulated battlefield conditions comprising:

means simulating a battlefield environment including at least one target movable therewithin, said simulating means including means generating a digital signal representing the battlefield and the target;

hardware means including missile acquisition, tracking, and guidance portions of the missile system, the acquisition portion of the hardware means operating on images in an infrared portion of the light spectrum;

interfacing means for converting signals produced by the simulating means to signals acceptable by the hardware means as representing a field-of-view, including the target, within the battlefield environment, the interfacing means including means responsive to the digital signals from the simulating means for generating and projecting an infrared map representing the field-of-view, and the acquisition portion of the hardware means scanning said map to locate the target therewithin; and

,

image means for producing an image representative of the missile'"'"'s position in the field-of-view, said image being acquirable by the hardware means which utilizes the acquired image to determine the position of the missile relative to the target and if a guidance signal is to be sent to the missile to guide it to the target, wherein the interfacing means is responsive to a guidance signal from the hardware means to simulate, in real-time, a dynamic response of the missile to the guidance signal, the image means comprising means for producing an infrared image of the missile and for superimposing the image on the map whereby the acquisition portion of the hardware means senses the position of the missile in the field-of-view, and the image means further including a blackbody and laser means for irradiating the blackbody to heat it to a temperature at which it emits infrared radiation.

2. The simulator of claim 1 wherein the map is a two-dimensional map.

3. The simulator of claim 1 wherein the image means further includes optic means for integrating the radiant image produced by heating the blackbody into the map.

4. The simulator of claim 3 wherein the optic means includes a collimating lens at which infrared radiation from the blackbody is directed, and a zoom lens at which light focused by the collimating lens is directed.

5. The simulator of claim 4 wherein the collimating lens and zoom lens are mounted in a fixed position relative to the blackbody, and the zoom lens has a fixed focal plane.

6. The simulator of claim 5 wherein the optic means further includes mask means interposed between the blackbody and the collimating lens for defining the image of the missile.

7. The simulator of claim 6 wherein the mask means includes a first mask having a first aperture therein representing the missile image during the initial portion of its flight when an engine of the missile is firing, and a second mask having a second aperture therein representing the missile image during a later portion of its flight when the engine is extinguished and a beacon on the missile is activated.

8. The simulator of claim 7 further including means for rotating the first mask to simulate missile roll during its initial stage of flight.

9. The simulator of claim 6 wherein the optic means further includes light polarizing means interposed between the collimating lens and the zoom lens and means for moving the polarizing means to precisely control the radiance from the blackbody.

10. The simulator of claim 9 wherein the optic means further includes beamsplitter means for imposing the image of the missile on the map for the acquisition portion of the hardware means to sense the presence of the missile image in the simulated field-of-view.

11. The simulator of claim 10 further including filter means for filtering out the laser light.

12. The simulator of claim 11 wherein the simulating means generates images of multiple targets within the field-of-view and the image means further includes means for producing the infrared image of a plurality of missiles.

13. The simulator of claim 11 wherein the image means further includes means for producing the infrared image of a missile countermeasure employed by the target.

14. The simulator of claim 1 wherein the simulating means includes means for generating atmospheric conditions on the battlefield.

15. A missile system simulator for use in training people for target acquisition, missile launch, and missile guidance under simulated battlefield conditions comprising:

simulating means for producing a digital signal representing a simulated battlefield environment including at least one target movable therewithin, the simulating means generating an infrared map representing the field-of-view and the target;

interface means for converting said digital signals to an infrared image;

missile system hardware including the missile acquisition, tracking, and guidance portions thereof, said hardware sensing the infrared image to determine the location of the target in a field-of-view; and

,

image means for generating an infrared image of a missile launched at the target and guided thereto, the image means imposing the missile image onto the field-of-view for the missile hardware to acquire the image of the missile in addition to that of the target, and to generate guidance signals to guide the missile image to the target image, wherein the interfacing means is responsive to a guidance signal from the hardware to simulate, in real-time, the response of the missile to the guidance signal, the image means including a blackbody, laser means for irradiating the blackbody to heat it to a temperature at which it emits infrared radiation, and optic means for integrating the radiant image produced by heating the blackbody into the infrared map.

16. The simulator of claim 15 wherein the optic means comprises a collimating lens at which infrared radiation from the blackbody is directed, a zoom lens at which light focused by the collimating lens is directed, and light polarizing means interposed between the collimating lens and the zoom lens for precisely controlling the radiance from the blackbody.

17. The simulator of claim 16 wherein the optic means further includes mask means comprising a first mask having a first aperture therein representing the missile image during an initial portion of its flight, and a second mask having a second aperture therein representing the missile image during a later portion of its flight.

18. The simulator of claim 17 wherein the optic means further includes beamsplitter means for overlaying the image of the missile onto the map.

19. The simulator of claim 18 further including filter means for filtering out the laser light.

20. A "hardware-in-the-loop" simulator for training people in the use of a missile system to teach target acquisition, missile launch, and missile guidance under simulated battlefield conditions comprising:

means simulating a battlefield environment including at least one target movable therewithin, said simulating means comprises means generating a digital signal representing the battlefield and the target;

hardware means including missile acquisition, tracking, and guidance portions of the missile system, the acquisition portion of said hardware means operating on images in an infrared portion of the light spectrum;

interfacing means for converting signals produced by the simulating means to signals acceptable by the hardware means as representing a field-of-view, including the target, within the battlefield environment, the interfacing means including means responsive to digital signals from the simulating means for generating and projecting an infrared map representing the field-of-view, and the acquisition portion of the hardware means scanning said map to locate the target therewithin; and

,

image means for producing an infrared image representative of the missile'"'"'s position in the field-of-view and for superimposing the image on the map whereby the acquisition portion of the hardware means senses the position of the missile in the field-of-view, said image being acquirable by the hardware means which utilizes the acquired image to determine the position of the missile relative to the target an if a guidance signal is to be sent to the missile to guide it to the target, the image means including a blackbody and laser means for irradiating the blackbody to heat it to a temperature at which it emits infrared radiation, wherein the interfacing means is responsive to a guidance signal from the hardware means to simulate, in real-time, a dynamic response of the missile to the guidance signal.

21. A missile system simulator for use in training people for target acquisition, missile launch, and missile guidance under simulated battlefield conditions comprising:

simulating means for producing a simulated battlefield environment including at least one target movable therewithin and for generating a digital signal representative thereof, the simulating means generating an infrared map representing the field-of-view and the target;

interfacing means for converting said digital signals to an infrared image;

missile system hardware including the missile acquisition, tracking, and guidance portions thereof, said hardware sensing the infrared image to determine the location of the target in a field-of-view; and

,

image means for generating an infrared image of a missile launched at the target and guided thereto, the image means imposing the missile image onto the field-of-view for the missile hardware to acquire the image of the missile in addition to that of the target, and to generate guidance signals to guide the missile image to the target image, the image means including a blackbody, laser means for irradiating the blackbody to heat it to a temperature at which it emits infrared radiation, and optic means for integrating the radiant image produced by heating the blackbody into the infrared map, wherein the interfacing means is responsive to a guidance signal from the hardware to simulate, in real-time, the response of the missile to the guidance signal.