Multimode unmanned aerial vehicle

Patent metadata

Field	Value
Publication number	US-11555672-B2
Application number	US-201916677348-A
Country	US
Kind code	B2
Filing date	Nov 7, 2019
Priority date	Feb 2, 2009
Publication date	Jan 17, 2023
Grant date	Jan 17, 2023

Abstract

A system comprising an unmanned aerial vehicle (UAV) configured to transition from a terminal homing mode to a target search mode, responsive to an uplink signal and/or an autonomous determination of scene change.

First claim

What is claimed is:

1. An unmanned aerial vehicle (UAV) comprising:
a processing unit which transitions the UAV from a first trajectory to impact a target to a second trajectory to avoid impact of the target by the UAV, wherein the transition is responsive to an indicator generated by onboard processing of the processing unit as an autonomous determination of scene change.

2. The UAV of claim 1 wherein the processing unit maintains a divert trajectory outside of a closed maneuver limit cone while in the first trajectory.

3. The UAV of claim 2 wherein the UAV transfers power from a battery of the UAV to a flight energy of the UAV in the divert trajectory, wherein the divert trajectory transitions the UAV from the first trajectory to the second trajectory, and wherein the UAV achieves at least an altitude in the second trajectory as the altitude at a start of the first trajectory.

4. The UAV of claim 2 wherein the processing unit stores at least one of: a pre-terminal commit point and a return waypoint, wherein the processing unit transitions the UAV to at least one of: the pre-terminal commit point and the return waypoint in response to an external command to transition the UAV from the first trajectory to the second trajectory.

5. The UAV of claim 4 wherein the external command causes the processing unit to transition from the first trajectory to the second trajectory, and wherein the external command is received via an uplink receiver.

6. The UAV of claim 2 further comprising:
one or more sensors, wherein the one or more sensors detect at least one of: a UAV position, a UAV linear velocity, a UAV rotational velocity, a UAV linear acceleration, and a UAV attitude.

7. The UAV of claim 2 wherein the processing unit transitions the UAV from the first trajectory to the second trajectory via the divert trajectory.

8. The UAV of claim 2 wherein the first trajectory further comprises homing on a target to deliver a payload into a target volume.

9. The UAV of claim 8 wherein the second trajectory avoids the UAV impacting the target volume.

10. The UAV of claim 8 wherein the second trajectory avoids the UAV impacting at least one of: the target the UAV is homing on and the ground.

11. The UAV of claim 2 wherein the divert trajectory is outside of a toroidal volume disposed about the UAV.

12. The UAV of claim 1 wherein the processing unit comprises at least one of: a central processing unit configured to execute computer-executable instructions; electrical circuitry; electronic circuitry; and a logical gate array.

13. The UAV of claim 1 wherein the indicator is received autonomously based on one or more image change conditions detected via a UAV onboard targeting sensor.

14. A method comprising:
transitioning, by a processing unit, an unmanned aerial vehicle (UAV) from a first trajectory to impact a target to a second trajectory avoiding impact of the target by the UAV, wherein the transition is responsive to an indicator generated by onboard processing of the processing unit as an autonomous determination of scene change.

15. The method of claim 14 further comprising:
maintaining, by the processing unit, a divert trajectory outside of a closed maneuver limit cone while in the first trajectory.

16. The method of claim 15 further comprising:
transferring power from a battery of the UAV to a flight energy of the UAV in the divert trajectory, wherein the divert trajectory transitions the UAV from the first trajectory to the second trajectory.

17. The method of claim 16 wherein the UAV achieves at least an altitude in the second trajectory as the altitude at a start of the first trajectory.

18. The method of claim 15 wherein the first trajectory further comprises homing on a target to deliver a payload into a target volume, and wherein the second trajectory avoids the UAV impacting at least one of: the target the UAV is homing on and the ground.

19. The method of claim 14 further comprising:
testing, by the processing unit, for the indicator while in the first trajectory.

20. The method of claim 19 further comprising:
receiving the indicator autonomously based on one or more image change conditions detected via a UAV onboard targeting sensor.

Assignees

• Aerovironment Inc

Inventors

• Miralles Carlos Thomas

Classifications

• B64C39/024

  of the remote controlled vehicle type, i.e. RPV · CPC title

• B64C39/00

  Aircraft not otherwise provided for · CPC title

• B64U2201/10

  autonomous, i.e. by navigating independently from ground or air stations, e.g. by using inertial navigation systems [INS] · CPC title

• F41G7/2253

  Passive homing systems, i.e. comprising a receiver and do not requiring an active illumination of the target · CPC title

• F41G9/002

  for guiding a craft to a correct firing position (for bombing control F41G9/02) · CPC title