AUTONOMOUS AIRBAG SYSTEM FOR UNMANNED AERIAL VEHICLES

• US 20160272333A1
• Filed: 03/17/2015
• Published: 09/22/2016
• Est. Priority Date: 03/31/2014
• Status: Abandoned Application

• Current Assignee: Sharper Shape Oy (Sharper Shape, Inc.)
• Original Assignee: Sharper Shape Oy (Sharper Shape, Inc.)
• Inventors: Heinonen, Tero
• Application Number:
  US14/660,165
• Publication Number:
  US 20160272333A1
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: B64C 39/024 of the remote controlled vehicle type, i.e. RPV
• CPC Class Codes: B64D 2201/00 Airbags mounted in aircraft for any use
• CPC Class Codes: B64U 70/87 using inflatable cushions

Abstract

The present disclosure is related to an autonomous airbag unit (AAU) for an unmanned aerial vehicle (UAV). The AAU includes a first sensor configured to determine a speed of the UAV, a second sensor configured to determine a relative speed of the UAV in relation to an object with which the UAV is likely to collide, an airbag cushion, an inflator connected to the airbag cushion, and an airbag control unit, connected to the first and second sensors and inflator. The airbag control unit is configured to estimate a momentum of the UAV based on a speed of the UAV, determine if the momentum of the UAV exceeds a threshold momentum value, determine if the relative speed of the UAV in relation to the object exceeds a threshold relative speed, and enable the inflator to inflate the airbag cushion when the momentum and the relative speed exceeds respective threshold limits.

Claims

1. An autonomous airbag unit for an unmanned aerial vehicle comprising

a first sensor configured to determine a speed of the unmanned aerial vehicle;

a second sensor configured to determine a relative speed of the unmanned aerial vehicle in relation to an object with which the unmanned aerial vehicle is likely to collide;

an airbag cushion;

an inflator connected to the airbag cushion, and configured to generate gas to inflate the airbag cushion; and

an airbag control unit, connected to the first sensor, the second sensor and the inflator, and configured to;

estimate a momentum of the unmanned aerial vehicle based on a mass of the unmanned aerial vehicle and the speed determined by the first sensor;

determine if the momentum of the unmanned aerial vehicle exceeds a threshold momentum value;

determine if the relative speed of the unmanned aerial vehicle in relation to the object exceeds a threshold relative speed; and

enable the inflator to inflate the airbag cushion when the momentum and the relative speed exceed respective threshold limits.

2. The autonomous air bag unit of claim 1, wherein the first sensor is an inertial measurement unit, a global positioning system receiver or a global navigation satellite system receiver.

3. The autonomous air bag unit of claim 1, wherein the second sensor is an ultrasound sensor, a light detection and ranging sensor, an infrared sensor or a laser distance meter unit.

4. The autonomous air bag unit of claim 1, wherein the airbag control unit is further configured to automatically deploy the airbag cushion, due to at least one of:

a mechanical failure in the unmanned aerial vehicle, an electrical failure in the unmanned aerial vehicle, a communication error, a software error, a remote pilot failure, and a remote pilot intentional act.

5. The autonomous air bag unit of claim 1, wherein the airbag control unit is further configured to inflate the airbag cushion when the unmanned aerial vehicle is about to collide with an object, even if the momentum of the unmanned aerial vehicle is below the threshold momentum value.

6. The autonomous air bag unit of claim 1, wherein the airbag control unit is further configured to deflate the airbag cushion after expiry of a predetermined time period from the collision.

7. The autonomous air bag unit of claim 1, further comprising at least one of an accelerometer and a pressure sensor.

8. An unmanned aerial vehicle comprising at least one autonomous airbag unit according to claim 1.

9. The unmanned aerial vehicle of claim 8, comprising at least two autonomous airbag units, each provided with communication means for interacting with each other.

10. A method for controlling an autonomous airbag unit of an unmanned aerial vehicle comprising

determining a speed of the unmanned aerial vehicle with a first sensor;

determining a relative speed of the unmanned aerial vehicle in relation to an object with which the unmanned aerial vehicle is likely to collide, with a second sensor;

estimating a momentum of the unmanned aerial vehicle based on a mass of the unmanned aerial vehicle and the speed determined by the first sensor;

determining if the momentum of the unmanned aerial vehicle exceeds a threshold momentum value;

determining if the relative speed of the unmanned aerial vehicle in relation to the object exceeds a threshold relative speed; and

enabling an inflator to inflate an airbag cushion of the airbag unit when the momentum and the relative speed exceed respective threshold limits.