Small caliber guided projectile

• US 7,781,709 B1
• Filed: 09/30/2008
• Issued: 08/24/2010
• Est. Priority Date: 05/05/2008
• Status: Active Grant

• Current Assignee: National Technology & Engineering Solutions Of Sandia LLC (Honeywell International Inc.)
• Original Assignee: Sandia Corporation (Martin Marietta Corporation)
• Inventors: Kniskern, Marc W., Rose, Scott E., Jones, James F., Woods, James W., Kast, Brian A., Rohrer, Brandon R., Greene, Ronald W.
• Primary Examiner(s): Gregory; Bernarr E
• Application Number:
  US12/241,410
• Time in Patent Office: 693 Days
• Field of Search: 244 31- 33, 89/11.1, 102/382, 102/384, 102/430, 102/439
• US Class Current: 244/3.16
• CPC Class Codes: F41G 7/226 Semi-active homing systems, i.e. comprising a receiver and involving auxiliary illuminating means, e.g. using auxiliary guiding missiles
• CPC Class Codes: F41G 7/2293 using electromagnetic waves other than radio waves
• CPC Class Codes: F42B 10/60 Steering arrangements F42B19/01 takes precedence
• CPC Class Codes: F42B 10/64 of fins
• CPC Class Codes: F42B 30/02 Bullets

Abstract

A non-spinning projectile that is self-guided to a laser designated target and is configured to be fired from a small caliber smooth bore gun barrel has an optical sensor mounted in the nose of the projectile, a counterbalancing mass portion near the fore end of the projectile and a hollow tapered body mounted aft of the counterbalancing mass. Stabilizing strakes are mounted to and extend outward from the tapered body with control fins located at the aft end of the strakes. Guidance and control electronics and electromagnetic actuators for operating the control fins are located within the tapered body section. Output from the optical sensor is processed by the guidance and control electronics to produce command signals for the electromagnetic actuators. A guidance control algorithm incorporating non-proportional, “bang-bang” control is used to steer the projectile to the target.

Claims

1. A non-spinning projectile self-guided to a laser designated target, the projectile having a center of gravity, a center of pressure and a length, the projectile comprising:

an optical sensor operatively arranged to detect light reflected from the laser designated target;

a counterbalance mass operatively arranged to cause the center of gravity of the projectile to be located forward of the center of pressure of the projectile;

a plurality of stabilizing strakes rigidly affixed to an exterior surface of the projectile, each of the plurality extending longitudinally along a portion of the projectile'"'"'s length;

a plurality of control fins each pivotally mounted adjacent to a trailing edge of one of the plurality of stabilizing strakes, one or more of the plurality of control fins attached to each of one or more rotatable shafts, each rotatable shaft having an actuation lever and an opposed actuation lever;

a plurality of electromagnetic actuators each magnetically coupleable to one of the actuation lever and the opposed actuation lever of each rotatable shaft; and

,

a control and guidance electronics module operatively arranged to receive a signal from the optical sensor and generate therefrom, a control command for each of the plurality of electromagnetic actuators, causing the control fins to pivot in a controlled manner thereby guiding the projectile towards the target.

2. The projectile of claim 1 wherein the control command for each of the plurality of electromagnetic actuators consists of one of a power off command and a power on command, thereby providing non-proportional control of the plurality of control fins.

3. The projectile of claim 1 further comprising a sabot, the sabot operatively arranged to interface the projectile to a smooth bore gun barrel thereby preventing damage to the stabilizing strakes and control fins upon firing.

4. The projectile of claim 3 wherein the projectile and the sabot are operatively configured to comprise a combined diameter equal to or less than thirteen millimeters.

5. The projectile of claim 1 wherein the length is equal to or less than approximately four inches.

6. The projectile of claim 1 wherein the plurality of control fins are operatively arranged to be pivotable through approximately six degrees of rotation.

7. A non-spinning projectile self-guided to a laser designated target, the projectile having a center of gravity, a center of pressure, a length and fore and aft ends, the projectile comprising:

an infrared optical sensor operatively arranged to detect light reflected from the laser designated target, the optical sensor fixedly mounted proximal to the fore end of the projectile;

a counterbalance mass operatively arranged to cause the center of gravity of the projectile to be located forward of the center of pressure of the projectile, the counterbalance mass operatively connected to and aft of the optical sensor;

a plurality of stabilizing strakes rigidly affixed to an exterior surface of the projectile, each of the plurality extending longitudinally along a portion of the projectiles length and terminating proximal to the aft end of the projectile;

a plurality of control fins each pivotally mounted adjacent to a trailing edge of one of the plurality of stabilizing strakes, one or more of the plurality of control fins attached to each of one or more rotatable shafts, each rotatable shaft having an actuation lever and an opposed actuation lever attached thereto;

an actuation module disposed at the aft end of the projectile, the actuation module comprising a plurality of electromagnetic actuators each magnetically coupleable to one of the actuation lever and the opposed actuation lever of each rotatable shaft;

a control and guidance electronics module operatively arranged to receive a signal from the optical sensor and generate therefrom, a control command for each of the plurality of electromagnetic actuators, causing the control fins to pivot in a controlled manner thereby guiding the projectile towards the target; and

,

a sabot encasing a portion of the exterior surface of the projectile, the sabot operatively arranged to interface the projectile to a smooth bore gun barrel and prevent damage to the stabilizing strakes and control fins upon firing.

8. The projectile of claim 7 wherein the plurality of control fins comprises four control fins operatively arranged as a first pair and a second pair, the first pair of control fins commonly attached to a first rotatable shaft, second pair of control fins commonly attached to a second rotatable shaft, the first pair of control fins oriented substantially orthogonal to the second pair of control fins, thereby providing pitch and yaw control of the projectile'"'"'s trajectory.

9. The projectile of claim 8 wherein the plurality of electromagnetic actuators comprises four electromagnetic actuators configured as a first pair of actuators operatively arranged to control the first pair of control fins and a second pair of actuators operatively arranged to control the second pair of control fins.

10. The projectile of claim 9 wherein each actuation lever and each opposed actuation lever attached to each rotatable shaft comprises a magnetically coupling portion to coupling to each associated electromagnetic actuator.

11. The projectile of claim 7 wherein the counterbalance mass comprises one or more selected from a tungsten counterbalance mass and a depleted uranium counterbalance mass.

12. The projectile of claim 7 wherein the control and guidance electronics module comprises one or more batteries.

13. The projectile of claim 12 wherein the one or more batteries comprises one or more selected from a lithium ion battery and a shock activated battery.