Guided projectile and countermeasure systems and methods for use therewith

Patent metadata

Field	Value
Publication number	US-11835319-B2
Application number	US-202217664679-A
Country	US
Kind code	B2
Filing date	May 24, 2022
Priority date	Jun 7, 2021
Publication date	Dec 5, 2023
Grant date	Dec 5, 2023

Abstract

A guided projectile including a projectile housing, a first sensor, and an air brake detachably coupled to the projectile housing. The air brake is deployable from a flight configuration to a braking configuration. A processor is configured to monitor, based on data received from the first sensor, a proximity of the at least one intercepting object relative to the guided projectile, wherein the guided projectile is configured to advance towards a target location on a first target trajectory. The processor is also configured to deploy the air brake to cause the guided projectile to veer from the first target trajectory to evade the at least one intercepting object, and detach the air brake from the guided projectile to enable the guided projectile to advance on a second target trajectory that is offset from the first target trajectory, wherein the first target trajectory and the second target trajectory have the same target location.

First claim

What is claimed is:

1. A guided projectile comprising:
a projectile housing;
a first sensor configured to detect approach of an intercepting object;
an air brake detachably coupled to the projectile housing, wherein the air brake is deployable from a flight configuration to a braking configuration; and
a processor configured to:
monitor, based on data received from the first sensor, a proximity of the at least one intercepting object relative to the guided projectile, wherein the guided projectile is configured to advance towards a target location on a first target trajectory;
deploy the air brake when the intercepting object is within a predetermined proximity, to cause the guided projectile to veer from the first target trajectory to establish a separation distance to evade the at least one intercepting object; and
detach the air brake from the guided projectile to enable the guided projectile to advance on a second target trajectory that is offset from the first target trajectory, wherein the first target trajectory and the second target trajectory have the same target location.

2. The guided projectile in accordance with claim 1 , wherein, when deployed to the braking configuration, the air brake causes the guided projectile to decelerate and lose altitude.

3. The guided projectile in accordance with claim 1 , wherein the air brake comprises a plurality of air fins positioned against the projectile housing when in the flight configuration, and oriented at least one of orthogonally or perpendicularly relative to a longitudinal axis of the guided projectile when in the braking configuration.

4. The guided projectile in accordance with claim 3 , wherein the air brake further comprises a base plate coupled to the plurality of air fins, wherein the base plate is detachably coupled to the projectile housing.

5. The guided projectile in accordance with claim 3 , wherein the air brake comprises a release mechanism configured to retain the plurality of air fins against the projectile housing, and configured to selectively release the plurality of air fins for deployment to the braking configuration.

6. The guided projectile in accordance with claim 1 further comprising a second sensor, wherein the processor is further configured to:
monitor, based on data received from the second sensor, at least one of an air speed or an altitude of the guided projectile; and
detach the air brake from the projectile housing when at least one of the air speed or the altitude is reduced to less than a respective minimum threshold.

7. A countermeasure system for use with a guided projectile, the countermeasure system comprising:
a first sensor configured to detect approach of an intercepting object;
an air brake detachably coupled to the guided projectile, wherein the air brake is deployable from a flight configuration to a braking configuration; and
a processor configured to:
monitor, based on data received from the first sensor, a proximity of the at least one intercepting object relative to the guided projectile, wherein the guided projectile is configured to advance towards a target location on a first target trajectory;
deploy the air brake to cause the guided projectile to veer from the first target trajectory to evade the at least one intercepting object; and
detach the air brake from the guided projectile to enable the guided projectile to advance on a second target trajectory that is offset from the first target trajectory, wherein the first target trajectory and the second target trajectory have the same target location.

8. The countermeasure system in accordance with claim 7 , wherein, when deployed to the braking configuration, the air brake causes the guided projectile to decelerate and lose altitude.

9. The countermeasure system in accordance with claim 7 , wherein the air brake comprises a plurality of air fins positioned against the projectile housing when in the flight configuration, and oriented at least one of orthogonally or perpendicularly relative to a longitudinal axis of the guided projectile when in the braking configuration.

10. The countermeasure system in accordance with claim 9 , wherein the air brake further comprises a base plate coupled to the plurality of air fins, wherein the base plate is detachably coupled to the projectile housing.

11. The countermeasure system in accordance with claim 9 , wherein the air brake comprises a release mechanism configured to retain the plurality of air fins against the projectile housing, and configured to selectively release the plurality of air fins for deployment to the braking configuration.

12. The countermeasure system in accordance with claim 7 further comprising a second sensor, wherein the processor is further configured to:
monitor, based on data received from the second sensor, at least one of an air speed or an altitude of the guided projectile; and
detach the air brake from the projectile housing when at least one of the air speed or the altitude is reduced to less than a respective minimum threshold.

13. A method of evading at least one intercepting object, the method comprising:
monitoring, based on data received from a first sensor onboard a guided projectile configured to detect approach of an intercepting object, a proximity of the at least one intercepting object relative to the guided projectile, wherein the guided projectile is configured to advance towards a target location on a first target trajectory;
deploying an air brake onboard the guided projectile to cause the guided projectile to veer from the first target trajectory to evade the at least one intercepting object; and
detaching the air brake from the guided projectile to enable the guided projectile to advance on a second target trajectory that is offset from the first target trajectory, wherein the first target trajectory and the second target trajectory have the same target location.

14. The method in accordance with claim 13 , wherein deploying the air brake comprises deploying the air brake when a distance between the at least one intercepting object and the guided projectile is less than a predetermined threshold.

15. The method in accordance with claim 13 , wherein detaching the air brake comprises:
monitoring a proximity of the guided projectile relative to the at least one intercepting object after the air brake has been deployed; and
detaching the air brake when a distance between the guided projectile and the at least one intercepting object is greater than a predetermined threshold.

16. The method in accordance with claim 13 , wherein detaching the air brake comprises:
determining a kill radius of the at least one intercepting object; and
detaching the air brake when a distance between the guided projectile and the at least one intercepting object is greater than the kill radius.

17. The method in accordance with claim 13 , wherein detaching the air brake comprises:
monitoring a proximity of a first intercepting object and a second intercepting object relative to the guided projectile; and
detaching the air brake based on the proximity of the second intercepting object relative to the guided projectile, wherein detaching the air brake enables the guided projectile to accelerate to evade the second intercepting object.

18. The method in accordance with claim 13 , wherein detaching the air brake comprises detaching the air brake after a predetermined amount of time has elapsed, the predetermined amount of time based on how long the air brake has been deployed.

19. The metho

Assignees

• Boeing Co

Inventors

• Est Brian Edward
• Palmer Leslie Leon

Classifications

• F41G7/224 Primary

  Deceiving or protecting means (jamming or anti-jamming of radio-wave systems in general G01S7/36, G01S7/38; defense installations in general F41H11/02; chaff dispensers F42B12/70) · CPC title

• F42B10/50 Primary

  Brake flaps {, e.g. inflatable} · CPC title