Emergency unmanned aerial vehicle and method for deploying an unmanned aerial vehicle

• US 9,834,306 B2
• Filed: 02/09/2016
• Issued: 12/05/2017
• Est. Priority Date: 02/09/2016
• Status: Expired due to Fees

• Current Assignee: Abdullah Almasoud
• Original Assignee: Abdullah Almasoud
• Inventors: Almasoud, Abdullah
• Primary Examiner(s): Do, Truc M
• Application Number:
  US15/019,551
• Publication Number:
  US 20170225781A1
• Time in Patent Office: 665 Days
• CPC Class Codes: B64U 10/10 Rotorcrafts
• CPC Class Codes: B64U 10/13 Flying platforms
• CPC Class Codes: B64U 10/14 with four distinct rotor axes, e.g. quadcopters
• CPC Class Codes: B64U 2101/00 UAVs specially adapted for particular uses or applications
• CPC Class Codes: B64U 2101/20 for use as communications relays, e.g. high-altitude platforms
• CPC Class Codes: B64U 2101/21 for providing Internet access
• CPC Class Codes: B64U 2101/23 for providing telephone services
• CPC Class Codes: B64U 2201/104 using satellite radio beacon positioning systems, e.g. GPS
• CPC Class Codes: B64U 30/20 Rotors; Rotor supports
• CPC Class Codes: B64U 30/293 Foldable or collapsible rotors or rotor supports
• CPC Class Codes: B64U 50/19 using electrically powered motors
• CPC Class Codes: B64U 50/31 generated by photovoltaics
• CPC Class Codes: B64U 50/34 In-flight charging photovoltaics B64U50/31
• CPC Class Codes: B64U 80/00 Transport or storage specially adapted for UAVs
• CPC Class Codes: B64U 80/60 by wearable objects, e.g. garments or helmets
• CPC Class Codes: G01C 21/20 Instruments for performing navigational calculations G01C21/24, G01C21/26 take precedence
• CPC Class Codes: G07C 5/008 communicating information to a remotely located station transmission systems for measured values G08C
• CPC Class Codes: G07C 5/08 Registering or indicating performance data other than driving, working, idle, or waiting time, with or without registering driving, working, idle or waiting time
• CPC Class Codes: G07C 5/0808 Diagnosing performance data testing of vehicles G01M17/00; testing of electrical installation on vehicles G01R31/005
• CPC Class Codes: G07C 5/085 using electronic data carriers
• CPC Class Codes: G08B 25/009 : Signalling of the alarm condition to a substation whose identity is signalled to a central station, e.g. relaying alarm signals in order to extend communication range
• CPC Class Codes: G08B 25/016 : Personal emergency signalling and security systems emergency non-personal manually actuated alarm activators G08B25/12
• CPC Class Codes: G08G 5/0013 : with a ground station
• CPC Class Codes: G08G 5/0021 : located in the aircraft
• CPC Class Codes: G08G 5/0069 : specially adapted for an unmanned aircraft
• CPC Class Codes: G08G 5/0086 : for monitoring terrain radar or analogous systems specially adapted for terrain avoidance G01S13/935
• CPC Class Codes: G08G 5/0091 : for monitoring atmospheric conditions radar or analogous systems specially adapted for meteorological use G01S13/95; meteorology G01W
• CPC Class Codes: H04B 7/18506 : Communications with or from aircraft, i.e. aeronautical mobile service

Abstract

An emergency unmanned aerial vehicle (UAV) and a method for employing a UAV. The method includes storing a digital elevation model (DEM) and associated data including locations of communication networks, updating the locations of communication networks in the associated data via a wireless transceiver, and storing position information determined by a global navigation satellite system (GNSS) receiver. The method includes detecting a predetermined condition using electronic sensors, determining whether the UAV is within a communications range of any communication network via the wireless transceiver, and determining a path to a communication network using the DEM and the associated data. The method also includes causing the UAV to become airborne and fly along the path, and transmitting a distress message via the wireless transceiver to the communication network, the distress message including position information corresponding to a location where the UAV detected the predetermined condition.

Claims

1. An emergency unmanned aerial vehicle (UAV) comprising:

a wireless transceiver configured to receive and transmit wireless communications;

an inertial measurement unit (EMU) configured with at least one of a three-axis accelerometer, a three-axis gyroscope, and a microelectromechanical magnetometer;

a global navigation satellite system (GNSS) receiver, configured to receive position information via an antenna and determine a position of the UAV; and

circuitry configured to

store a digital elevation model (DEM) and associated data, the associated data including locations of communication networks,

update the locations of communication networks in the associated data via the wireless transceiver,

store position information determined by the GNSS receiver,

detect a predetermined condition,

determine, using at least one of the DEM and the associated data, whether the UAV is within a communications range of any communication network via the wireless transceiver,

determine a path to a communication network using the DEM and the associated data,

cause the UAV to become airborne and fly along the path to the communication network in response to detecting the predetermined condition,

transmit a distress message via the wireless transceiver to the communication network, the distress message including position information corresponding to a location where the UAV detected the predetermined condition,

determine an acceleration of the UAV via the IMU prior to the UAV becoming airborne,

wherein the predetermined condition is detected when the determined acceleration exceeds a predetermined acceleration.

2. The emergency UAV as recited in claim 1, further comprising

a solar panel configured to charge the battery.

3. The emergency UAV as recited in claim 1, wherein the circuitry determines the path to the communication network using an optimal path algorithm.

4. The emergency UAV as recited in claim 1, wherein the circuitry is further configured to

store and update environmental data via the wireless transceiver, the environmental data being included in the associated data.

5. The emergency UAV as recited in claim 4, wherein the circuitry is further configured to:

periodically determine whether a communication network is available prior to the UAV becoming airborne, and

periodically obtain the locations of the communication networks and the environmental data via an available communication network when it is determined that the communication network is available.

6. The emergency UAV as recited in claim 1,

wherein the emergency UAV is configured to couple to a docking station on a vehicle, and

wherein the emergency UAV is configured to charge a battery provided in the UAV from the vehicle when coupled to the docking station on the vehicle.

7. The emergency UAV as recited in claim 6, wherein the circuitry is further configured to

receive sensor information from the vehicle,

wherein detecting the predetermined condition includes detecting the predetermined condition in the received sensor information from the vehicle.

8. The emergency UAV as recited in claim 7, wherein the sensor information from the vehicle includes at least one of a fuel level of the vehicle, a battery charge state of the vehicle, and a tilt angle of the vehicle.

9. The emergency UAV as recited in claim 1,

wherein the associated data includes locations of charging stations, and

wherein the emergency UAV is configured to couple to a charging station and receive charge from the charging station.

10. The emergency UAV as recited in claim 1, wherein the circuitry is further configured to:

cause the emergency UAV to wait a predetermined period of time after detecting the predetermined condition before causing the UAV to fly along the path to the communication network or transmitting the distress message,

receive a signal canceling the detection of the predetermined condition via the wireless transceiver within the predetermined period of time, and

cause the emergency UAV to return to a stand-by location when the signal canceling the activation is received within the predetermined period of time.

11. The emergency UAV as recited in claim 1, wherein the emergency UAV is configured to be folded and stored in a portable pack.

12. The emergency UAV as recited in claim 1, wherein the wireless transceiver is further configured as a multiband transceiver including direct radio communications capability.

13. The emergency UAV as recited in claim 1, further comprising

an Ultrasonic rangefinder,

wherein the circuitry is configured to land the UAV when a charge of the battery decreases to a predetermined threshold charge after the UAV becomes airborne,

wherein the circuitry uses the ultrasonic rangefinder to verify a distance to the ground, and

wherein the circuitry monitors a charge of the battery, and reactivates the UAV when the battery reaches a predetermined charge level.

14. The emergency UAV as recited in claim 1,

wherein the DEM and associated data indicate geographical regions where the UAV is not allowed to fly, and

wherein the circuitry determines the path to the communication network avoiding the indicated regions where the UAV is not allowed to fly.

17. The emergency UAV as recited in claim 1, wherein the circuitry is further configured to

cause the emergency UAV to return to a stand-by location after the UAV transmits the distress message to the communication network,

wherein the stand-by location is a pre-programmed location or the stand-by location is a location where the UAV became airborne.

15. The emergency UAV as recited in 1, wherein the circuitry is further configured to transmit the distress message via the wireless transceiver to a second emergency UAV.

16. The emergency UAV as recited in claim 15, wherein the circuitry is further configured to receive an external distress message via the wireless transceiver prior to the UAV becoming airborne,

wherein the detecting the predetermined condition includes receiving the external distress message via the wireless transceiver.

18. A method for employing an emergency unmanned aerial vehicle (UAV) comprising:

storing a digital elevation model (DEM) and associated data, the associated data including locations of communication networks in on-board circuitry including a memory;

updating the locations of communication networks in the associated data to the DEM via a wireless transceiver configured to receive and transmit wireless communications;

storing position information determined by a global navigation satellite system (GNSS) receiver, configured to receive position information via an antenna and determine a position of the UAV;

detecting a predetermined condition using electronic sensors;

determining whether the UAV is within a communications range of any communication network via the wireless transceiver;

determining a path to a communication network using the DEM and the associated data,

causing the UAV to become airborne and fly along the path to the communication network in response to detecting the predetermined condition, and

transmitting a distress message via the wireless transceiver to the communication network, the distress message including position information corresponding to a location where the UAV detected the predetermined condition,

determining an acceleration of the UAV, via an inertial measurement unit (IMU) configured with at least one of a three-axis accelerometer, a three-axis gyroscope, and a microelectromechanical magnetometer, prior to the UAV becoming airborne,

wherein the predetermined condition is detected when the determined acceleration exceeds a predetermined acceleration.

19. A non-transitory computer readable medium having program instructions stored therein for causing a processor to perform a method for employing an emergency unmanned aerial vehicle (UAV), the method comprising:

storing a digital elevation model (DEM) and associated data, the associated data including locations of communication networks in a memory;

updating the locations of communication networks in the associated data to the DEM via a wireless transceiver configured to receive and transmit wireless communications;

storing position information determined by a global navigation satellite system (GNSS) receiver, the GNSS configured to receive position information via an antenna and determine a position of the UAV;

detecting a predetermined condition via electronic sensors;

determining whether the UAV is within a communications range of any communication network via the wireless transceiver;

determining a path to a communication network using the DEM and the associated data;

causing the UAV to become airborne and fly along the path to the communication network in response to detecting the predetermined condition; and

transmitting a distress message via the wireless transceiver to the communication network, the distress message including position information corresponding to a location where the UAV detected the predetermined condition,

determining an acceleration of the UAV, via an inertial measurement unit (IMU) configured with at least one of a three-axis accelerometer, a three-axis gyroscope, and a microelectromechanical magnetometer, prior to the UAV becoming airborne,

wherein the predetermined condition is detected when the determined acceleration exceeds a predetermined acceleration.