Methods for extended-range, enhanced-precision gun-fired rounds using g-hardened flow control systems

1. A g-hardened munition comprising:

a forebody, an afterbody, at least one independently adjustable activatable or deployable flow effector adapted to extend the range and enhance the precision of the munition, at least one g-hardened actuator adapted to actuate and control the at least one flow effector, a g-hardened sensor suite adapted to measure orientation and spin rate of the munition, and a g-hardened microcontroller comprising an algorithm adapted to generate output commands for range extension and guidance control of the munition through closed-loop feedback from the sensor suite;

wherein the output commands of the algorithm are adapted to signal the actuator to activate or deploy, deactivate or stow, and to reactivate or redeploy the at least one flow effector during flight, and to adjust the at least one deployable flow effector while deployed or activated to adjust trim angle, reorient, and/or despin the munition in order to increase range and provide guidance control of the munition, and

the munition experiences a launch or firing acceleration of more than 10,000 g's.

2. The munition of claim 1 , wherein the sensor suite comprises at least one accelerometer, at least one gyroscope, and at least one infrared (IT) sensor, each sensor having a signal.

3. The munition of claim 1 , wherein the munition is a munition or round from 40 mm to 155 mm in diameter.

4. The munition of claim 2 , wherein the munition, or the sensor suite of the munition, further comprises a video sensor adapted to provide a signal corresponding to orientation of the munition and/or corresponding to a target to identify and track the target, and wherein the algorithm further bases the output commands on the video sensor signal.

5. The munition of claim 2 , wherein the sensor suite further comprises a global positioning system (GPS) sensor having a signal.

6. The munition of claim 4 , wherein the microcontroller is further adapted to determine the munition's relative position with respect to a moving target or target location, the algorithm is further adapted to output commands for guide-to-hit control and to direct the actuator to adjust the at least one flow effector to redirect the munition towards the target or target location.

7. The munition of claim 5 , wherein the sensor suite further comprises a pressure sensor, shear stress sensor or inertial measurement system adapted to measure flow dynamics on a flow surface of the munition, and the flow effectors are independently adjusted based further in part on the measured flow dynamics.

8. A g-hardened munition comprising:

a forebody, an afterbody, at least two independently adjustable activatable or deployable flow effectors adapted to extend the range and enhance the precision of the munition, at least one g-hardened actuator adapted to actuate and control the at least two flow effectors, a g-hardened sensor suite adapted to measure orientation and spin rate of the munition, and a g-hardened microcontroller comprising an algorithm adapted to generate output commands for range extension and guidance control of the munition through closed-loop feedback from the sensor suite; and

wherein the output commands of the algorithm are adapted to signal at least one of the g-hardened actuators to activate or deploy, deactivate or stow, and to reactivate or redeploy at least one of the at least two flow effectors during flight, and to adjust the at least two deployable flow effectors while deployed or activated to adjust trim angle, reorient, and/or despin the munition in order to increase range and provide guidance control of the munition, and

wherein the munition experiences a launch or firing acceleration of more than 10,000 g's.

9. The munition of claim 8 , wherein the sensor suite comprises at least one accelerometer, at least one gyroscope, and at least one infrared (IT) sensor, each sensor having a signal.

10. The munition of claim 8 , wherein the munition is a munition or round from 40 mm to 155 mm in diameter.

11. The munition of claim 9 , the munition, or the sensor suite of the munition, further comprises a video sensor adapted to provide a signal corresponding to orientation of the munition and/or corresponding to a target to identify and track the target, and wherein the algorithm further bases the output commands on the video sensor signal.

12. The munition of claim 9 , wherein the sensor suite further comprises a global positioning system (GPS) sensor having a signal.

13. The munition of claim 11 , wherein the microcontroller is further adapted to determine the munition's relative position with respect to a moving target or target location, the algorithm is further adapted to output commands for guide-to-hit control and to direct the actuator to adjust the flow effectors to redirect the munition towards the target or target location.

14. The munition of claim 12 , wherein the sensor suite further comprises a pressure sensor, shear stress sensor or inertial measurement system adapted to measure flow dynamics on a flow surface of the munition, and the flow effectors are independently adjusted based further in part on the measured flow dynamics.

15. A g-hardened munition comprising:

a forebody, an afterbody, at least two independently adjustable activatable or deployable flow effectors adapted to extend the range and enhance the precision of the munition, at least one g-hardened actuator adapted to actuate and control the at least two flow effectors, a g-hardened sensor suite adapted to measure orientation and spin rate of the munition, and a g-hardened microcontroller comprising an algorithm adapted to generate output commands for range extension and guidance control of the munition through closed-loop feedback from the sensor suite;

wherein the output commands of the algorithm are adapted to signal at least one of the g-hardened actuators to activate or deploy, deactivate or stow, and to reactivate or redeploy at least one of the at least two flow effectors during flight, and to adjust the at least one deployable flow effector while deployed or activated to adjust trim angle, reorient, and/or despin the munition in order to increase range and provide guidance control of the munition, and

the munition experiences a launch or firing acceleration of more than 10,000 g's, and the angles of attack of the at least two flow effectors are independently adjusted or controlled after activation or deployment by a beveled gear reduction mechanism corresponding to each flow effector located inside of the munition body.

16. The munition of claim 15 , wherein the sensor suite comprises at least one accelerometer, at least one gyroscope, and at least one infrared (IT) sensor, each sensor having a signal.

17. The munition of claim 15 , wherein the munition is a munition or round from 40 mm to 155 mm in diameter.

18. The munition of claim 16 , wherein the sensor suite further comprises a global positioning system (GPS) sensor having a signal.

19. The munition of claim 15 , wherein the microcontroller is further adapted to determine the munition's relative position with respect to a moving target or target location, the algorithm is further adapted to output commands for guide-to-hit control and to direct the actuator to adjust the flow effectors to redirect the munition towards the target or target location.

20. The munition of claim 18 , wherein the sensor suite further comprises a pressure sensor, shear stress sensor or inertial measurement system adapted to measure flow dynamics on a flow surface of the munition, and the flow effectors are independently adjusted based further in part on the measured flow dynamics.