Systems and methods for parachute-assisted landing of an unmanned aerial vehicle

Patent metadata

Field	Value
Publication number	US-11459114-B2
Application number	US-202016881684-A
Country	US
Kind code	B2
Filing date	May 22, 2020
Priority date	May 22, 2020
Publication date	Oct 4, 2022
Grant date	Oct 4, 2022

Abstract

In an example, a system is described. The system comprises an unmanned aerial vehicle (UAV) having a UAV control system to control flight of the UAV. The system also comprises a steerable parachute system for parachute-assisted landing. The steerable parachute system comprises (i) a deployable parachute having steerable parachute cables, (ii) steering actuators, each steering actuator coupled to, and movable to adjust, a respective steerable parachute cable, (iii) a steerable parachute controller, and (iv) one or more parachute system sensors communicatively coupled to the steerable parachute controller and configured to detect physical characteristics of a reachable landing zone for the UAV. The steerable parachute controller is configured to (i) select a safe landing location within the reachable landing zone based on the physical characteristics and (ii) control movement of the steering actuators to steer the parachute to land the UAV at the safe landing location.

First claim

What is claimed is:

1. A system comprising:
an unmanned aerial vehicle (UAV) having a UAV control system to control flight of the UAV, wherein the UAV control system comprises a UAV controller; and
a steerable parachute system for parachute-assisted landing, comprising (i) a deployable parachute having a plurality of steerable parachute cables, (ii) a plurality of steering actuators, each steering actuator coupled to a respective steerable parachute cable and movable to adjust the respective steerable parachute cable, (iii) a steerable parachute controller, and (iv) one or more parachute system sensors communicatively coupled to the steerable parachute controller and configured to detect physical characteristics of a reachable landing zone for the UAV,
wherein the steerable parachute controller is separate from the UAV controller and configured to (i) select a safe landing location within the reachable landing zone based on the physical characteristics detected with the one or more parachute system sensors and (ii) control movement of the plurality of steering actuators to steer the deployable parachute to land the UAV at the safe landing location.

2. The system of claim 1 , wherein the steerable parachute system operates independently from the UAV control system.

3. The system of claim 1 , wherein the UAV control system further comprises one or more UAV sensors, and
wherein the one or more UAV sensors are separate from the one or more parachute system sensors of the steerable parachute system.

4. The system of claim 1 , wherein the UAV control system comprises a UAV power source and the steerable parachute system further comprises a parachute system power source, and
wherein the parachute system power source is separate from the UAV power source.

5. The system of claim 1 , wherein the one or more parachute system sensors are attached to the UAV.

6. The system of claim 1 , wherein the plurality of steering actuators comprises a first steering actuator and a second steering actuator,
wherein the plurality of steerable parachute cables comprises a first steerable parachute cable attached to a first end of the deployable parachute and a second steerable parachute cable attached to a second end of the deployable parachute, opposite the first end, and
wherein the first steering actuator is movable to adjust the first steerable parachute cable and the second steering actuator is movable to adjust the second steerable parachute cable.

7. The system of claim 6 , wherein the first steerable parachute cable is attached to a first aft corner of the deployable parachute and the second steerable parachute cable is attached to a second aft corner of the deployable parachute.

8. The system of claim 1 , wherein each steering actuator comprises a pulley coupled to a motor, and
wherein controlling the movement of the plurality of steering actuators to steer the deployable parachute to land the UAV at the safe landing location comprises controlling the motor to cause the pulley to adjust the respective steerable parachute cable.

9. The system of claim 1 , wherein the steerable parachute system further comprises a housing within which the deployable parachute is releasably disposed, the plurality of steering actuators is disposed, and the steerable parachute controller is disposed, and
wherein the deployable parachute further comprises a plurality of static cables attached to the housing.

10. A method for parachute-assisted landing of an unmanned aerial vehicle (UAV), the method comprising:
detecting, by a steerable parachute controller of a steerable parachute system for the UAV and using one or more parachute system sensors of the steerable parachute system that are communicatively coupled to the steerable parachute controller, physical characteristics of a reachable landing zone for the UAV, wherein steerable parachute system further comprises (i) a deployable parachute having a plurality of steerable parachute cables and (ii) a plurality of steering actuators, each steering actuator coupled to a respective steerable parachute cable and movable to adjust the respective steerable parachute cable, wherein the UAV comprises a UAV control system having a UAV controller, and wherein the steerable parachute controller is separate from the UAV controller;
selecting, by the steerable parachute controller, a safe landing location within the reachable landing zone based on the physical characteristics; and
controlling, by the steerable parachute controller, movement of the plurality of steering actuators to steer the deployable parachute to land the UAV at the safe landing location.

11. The method of claim 10 , further comprising:
detecting a trigger for a parachute-assisted landing; and
responsive to detecting the trigger, controlling, by the steerable parachute controller, the steerable parachute system to deploy the deployable parachute,
wherein the detecting of the physical characteristics of the reachable landing zone for the UAV comprises detecting the physical characteristics of the reachable landing zone for the UAV responsive to deploying the deployable parachute.

12. The method of claim 10 , wherein controlling the movement of the plurality of steering actuators to steer the deployable parachute to land the UAV at the safe landing location comprises:
controlling a first steering actuator of the plurality of steering actuators to pull on a first steerable parachute cable of the plurality of steerable parachute cables that is attached to a first aft corner of the deployable parachute, wherein pulling on the first steerable parachute cable causes the UAV to steer left; and
controlling a second steering actuator of the plurality of steering actuators to pull on a second steerable parachute cable of the plurality of steerable parachute cables that is attached to a second aft corner of the deployable parachute, wherein pulling on the second steerable parachute cable causes the UAV to steer right.

13. The method of claim 12 , wherein controlling the first steering actuator to pull on the first steerable parachute cable comprises controlling a first motor to cause a first pulley coupled to the first motor to pull the first steerable parachute cable, and
wherein controlling the second steering actuator to pull on the second steerable parachute cable comprises controlling a second motor to cause a second pulley coupled to the second motor to pull on the second steerable parachute cable.

14. The method of claim 12 , wherein controlling the first steering actuator to pull on the first steerable parachute cable comprises controlling a first mechanical arm to pull the first steerable parachute cable, and
wherein controlling the second steering actuator to pull on the second steerable parachute cable comprises controlling a second mechanical arm to pull on the second steerable parachute cable.

15. The method of claim 10 , wherein the steerable parachute system operates independently from the UAV control system of the UAV such that the detecting, the selecting, and the controlling are performed independently from operations performed by the UAV control system.

16. A system comprising:
an unmanned aerial vehicle (UAV) having a UAV control system to control flight of the UAV, the UAV control system comprising one or more UAV sensors attached to the UAV; and
a steerable parachute system for parachute-assisted landing, comprising (i) a housing, (ii) a deployable parachute releasably disposed within the housing, the deployable parachute having a plurality of steerable parachute cables and a plurality of static cab

Assignees

• Boeing Co

Inventors

• Jarvis Joshua B

Classifications

• B64U2201/10

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

• B64U2201/00

  UAVs characterised by their flight controls · CPC title

• B64D17/34

  adapted to control direction or rate of descent · CPC title

• B64D17/80 Primary

  in association with aircraft, e.g. for braking thereof · CPC title

• B64C2201/185

  Operations & Transport · mapped topic