Precision guided munitions

• US 7,999,212 B1
• Filed: 05/01/2009
• Issued: 08/16/2011
• Est. Priority Date: 05/01/2008
• Status: Expired due to Fees

• Current Assignee: EMAG Technologies, Inc.
• Original Assignee: EMAG Technologies, Inc.
• Inventors: Thiesen, Jack H., Brakora, Karl F.
• Primary Examiner(s): Gregory; Bernarr E
• Application Number:
  US12/434,453
• Publication Number:
  US 20110180654A1
• Time in Patent Office: 837 Days
• Field of Search: 342/59, 342 61- 68, 342 73- 75, 342/80, 342/147, 342149-154, 342/175, 342/188, 342165-174, 342/195, 244 31- 33, 89/11.1, 89/6, 89/65, 102/382, 102/384, 102/473, 102/501, 102/513, 174/50
• US Class Current: 244/3.14
• CPC Class Codes: F42B 10/64 of fins

Abstract

A guidance system for actively guiding a projectile, such as a bullet after it has been fired from a gun. The guidance system includes a radar unit that includes a plurality of receiver arrays. An optical scope is also mounted to the gun for optically sighting a target. An inertial measurement unit provided on the gun locks onto the target after it has been sighted by the scope, and provides a reference location at the center of the receiver arrays from which the bullet can be directed. The receiver arrays receive radar monopulse beacon signals from the bullet. The signals from the bullet are used to identify the position of the bullet and the roll of the bullet. The signals sent to the bullet provide flight correction information that is processed on the bullet, and used to control actuators that move steering devices on the bullet.

Claims

1. A guidance system for guiding a bullet to a target after it is fired from a gun, said guidance system comprising:

a radar unit including a plurality of receiver arrays, said receiver arrays emitting radar signals to the bullet and receiving position signals from the bullet;

an optical scope mounted to the gun for optically sighting the target;

an inertial measurement unit provided on the gun, said inertial measurement unit identifying a center location of each receiver array in the radar unit;

an RF transceiver on the bullet, said RF transceiver including an antenna; and

at least one flight actuator on the bullet that controls the direction of the flight of the bullet, wherein the position signals from the bullet received by the radar unit identify the position of the bullet and the radar signal from the radar unit to the bullet provides flight path guidance to change the trajectory of the bullet in response to its position so that the at least one flight actuator directs the bullet towards the target.

2. The system according to claim 1 wherein the inertial measurement unit references the center of the array with respect to the target after it has been optically sighted and wherein the radar unit controls the flight of the bullet using the difference between the position of the bullet relative and the center of the receiver arrays.

3. The system according to claim 1 wherein the position signals from the bullet include signal polarizations that identify the roll of the bullet where the roll of the bullet is determined by comparing amplitudes of polarizations referenced to a linear polarization of a receiver on the bullet.

4. The system according to claim 3 wherein the radar unit calculates flight corrections of the bullet using the roll of the bullet and the position of the bullet.

5. The system according to claim 1 where the radar unit employs sum and difference monopulse tracking to locate the projectile and compute course corrections that control the flight of the bullet.

6. The system according to claim 1 wherein the signals transmitted between the gun and the bullet are encoded.

7. The system according to claim 6 where the encoding is chosen so that a line-of-sight signal and delayed reflected signal have low correlation.

8. The system according to claim 1 further comprising a switch on the gun that activates the inertial measurement unit to track relative motion between the target and the radar before the bullet is fired from the gun and after the target has been acquired.

9. The system according to claim 8 wherein the switch is on a grip of the gun.

10. The system according to claim 8 wherein the switch is provided by a half trigger pull of a trigger on the gun.

11. The system according to claim 1 wherein the radar unit is mounted to the gun.

12. The system according to claim 1 wherein the radar unit is separate from the gun.

13. The system according to claim 1 wherein the bullet includes a fusible switch that causes power to be provided to circuitry on the bullet after it is fired.

14. The system according to claim 1 wherein the bullet is a .50 caliber bullet.

15. The system according to claim 1 wherein the plurality of receiver arrays is two arrays.

16. The system according to claim 1 wherein the plurality of receiver arrays is four arrays.

17. The system according to claim 1 wherein the at least one flight actuator is a plurality of flight actuators that control the trajectory of the bullet.

18. A guidance system for guiding a bullet to a target after it is fired from a gun, said guidance system comprising:

a radar unit mounted to the gun, said radar unit including a plurality of receiver arrays, said receiver arrays emitting radar signals to the bullet and receiving position signals from the bullet;

an optical scope mounted to the gun for optically sighting the target;

an inertial measurement unit provided on the gun, said inertial measurement unit tracking the motion of the center location of each receiver array in the radar unit, wherein the inertial measurement unit corrects for motion between the center of the receiver arrays and the target after it has been optically sighted;

an RF transceiver on the bullet, said RF transceiver including an antenna, wherein the position signals from the bullet include signal polarizations that identify the roll of the bullet where the roll of the bullet is determined by comparing amplitudes of polarizations referenced to a linear polarization of a receiver on the bullet; and

at least one flight actuator on the bullet that controls the direction of the flight of the bullet, wherein the position signals from the bullet received by the radar unit identify the position of the bullet and the radar signal from the radar unit to the bullet provides flight path guidance to change the trajectory of the bullet in response to its position so that the at least one flight actuator directs the bullet towards the target and wherein the radar unit controls the flight of the bullet using the difference between the position of the bullet relative to the center of the receiver arrays, said radar unit calculating flight corrections of the bullet using the roll of the bullet and the position of the bullet and said radar unit employing monopulse radar tracking to compute trajectory information to be sent to the bullet.

19. The system according to claim 18 wherein the signals transmitted between the gun and the bullet are encoded.

20. The system according to claim 19 where the encoding is chosen so that a line-of-sight signal and delayed reflected signal have low correlation.

21. The system according to claim 18 further comprising a switch on the gun that activates the inertial measurement unit to lock onto the target before the bullet is fired from the gun.

22. The system according to claim 18 wherein the bullet includes a fusible switch that causes power to be provided to circuitry on the bullet after it is fired.

23. The system according to claim 18 wherein the bullet is a .50 caliber bullet.

24. A guidance system for guiding a projectile to a target, said guidance system comprising:

a radar unit including a plurality of receiver arrays, said receiver arrays emitting radar signals to the projectile and receiving position signals from the projectile;

an inertial measurement unit identifying a center location of each receiver array in the radar unit;

an RF transceiver on the projectile, said RF transceiver including an antenna; and

at least one flight actuator on the projectile that controls the direction of the flight of the projectile, wherein the position signals from the projectile received by the radar unit identify the position of the projectile and the radar signal from the radar unit to the projectile provides flight path guidance to change the trajectory of the projectile in response to its position so that the at least one flight actuator directs the projectile towards the target.