Unmanned aerial vehicle low-power operation

Patent metadata

Field	Value
Publication number	US-9778660-B2
Application number	US-201514855434-A
Country	US
Kind code	B2
Filing date	Sep 16, 2015
Priority date	Sep 16, 2015
Publication date	Oct 3, 2017
Grant date	Oct 3, 2017

Abstract

Methods, devices, and systems of various embodiments are disclosed for operating a UAV having insufficient power to operate normally. Various embodiments include determining whether an emergency-recovery state of a battery of the UAV has been reached while the UAV is flying. An emergency recovery mode may be activated in response to determining that the emergency-recovery state has been reached. The emergency recovery mode may switch the rotors from drawing energy from the battery to generate propulsion to harvesting energy from airflow that is used to recharge a battery of the UAV. A braking mode may be activated in response to determining that a braking altitude has been reached. The braking mode may switch the rotors from energy harvesting to drawing energy from the battery to generate propulsion in order to reduce a descent rate of the UAV.

First claim

What is claimed is:

1. A method of operating an unmanned aerial vehicle (UAV) using rotors for propulsion, the method comprising:
determining, in a processor while the UAV is flying, whether an emergency-recovery state of a battery of the UAV has been reached, wherein:
the emergency-recovery state is a battery charge state in which the battery has insufficient energy stored therein to enable the UAV to conduct a normal landing from a current altitude; and
the emergency-recovery state is defined by a total amount of stored energy needed to land the UAV minus an amount of energy estimated to be harvested by the rotors during the emergency recovery mode before reaching a braking altitude;

activating an emergency recovery mode in response to determining that the emergency-recovery state has been reached, wherein the emergency recovery mode switches the rotors from drawing power from the battery for generating propulsion to harvesting energy from airflow that is used to recharge the battery;
determining, in the processor, whether the braking altitude has been reached; and
activating a braking mode in response to determining the braking altitude has been reached, wherein the braking mode switches the rotors from energy harvesting to drawing power from the battery to generate propulsion in order to reduce a descent rate of the UAV.

2. The method of claim 1 , wherein the braking mode includes regulating an amount of energy generated by the rotors in order to adjust an amount of drag generated by each rotor in order to control UAV attitude.

3. The method of claim 1 , further comprising:
receiving, in the processor, a signal commanding the UAV to use an extended flight protocol that includes the emergency recovery mode.

4. The method of claim 1 , wherein the emergency-recovery state is a battery charge state in which the battery has insufficient energy stored therein to enable the UAV to maintain level flight.

5. The method of claim 1 , wherein the emergency-recovery state is measured from a voltage level of the battery.

6. The method of claim 1 , wherein the emergency-recovery state is a predetermined rate of change of a stored energy capacity of the battery.

7. The method of claim 1 , further comprising:
determining, in the processor while the UAV is flying, whether a warning state of the UAV has been reached, wherein the warning state is a battery charge state in which the battery has stored a predetermined percentage of a maximum stored energy of the battery and provides an indication that the UAV should initiate a landing;
detecting whether the UAV should use an extended flight protocol in response to determining that the warning state of the UAV has been reached; and
maintaining the rotors in an energy consumption mode for propulsion in response to determining that the UAV should use the extended flight protocol.

8. The method of claim 1 , wherein the emergency recovery mode comprises using at least one motor controlling at least one of the rotors to maintain a stable attitude by regulating an amount of energy generated by the at least one motor in order to adjust an amount of drag generated by the rotors.

9. An unmanned aerial vehicle (UAV), comprising:
a battery;
a rotor configured to be able to draw power from the battery to generate propulsion and to harvest energy from airflow to recharge the battery;
means for determining whether an emergency-recovery state of a battery of the UAV has been reached while the UAV is flying, wherein:
the emergency-recovery state is a battery charge state in which the battery has insufficient energy stored therein to enable the UAV to conduct a normal landing from a current altitude; and
the emergency-recovery state is defined by a total amount of stored energy needed to land the UAV minus an amount of energy estimated to be harvested by the rotors during the emergency recovery mode before reaching a braking altitude;

means for activating an emergency recovery mode in response to determining that the emergency-recovery state has been reached, wherein the emergency recovery mode switches the rotor from drawing power from the battery for generating propulsion to harvesting energy from airflow that is used to recharge the battery;
means for determining whether the braking altitude has been reached; and
means for activating a braking mode in response to determining the braking altitude has been reached, wherein the braking mode switches the rotor from energy harvesting to drawing power from the battery to generate propulsion in order to reduce a descent rate of the UAV.

10. An unmanned aerial vehicle (UAV), comprising:
a rotor;
a motor configured to drive the rotor for propulsion;
a battery configured to supply power to the motor; and
a processor couple to the battery and configured with processor-executable instructions to:
determine whether an emergency-recovery state of the battery has been reached while the UAV is flying, wherein:
the emergency-recovery state is a battery charge state in which the battery has insufficient energy stored therein to enable the UAV to conduct a normal landing from a current altitude; and
the emergency-recovery state is defined by a total amount of stored energy needed to land the UAV minus an amount of energy estimated to be harvested by the rotors during the emergency recovery mode before reaching a braking altitude;

activate an emergency recovery mode in response to determining that the emergency-recovery state has been reached, wherein the emergency recovery mode switches the rotor from drawing power from the battery for generating propulsion to harvesting energy from airflow that is used to recharge the battery;
determining whether the braking altitude has been reached; and
activating a braking mode in response to determining the braking altitude has been reached, wherein the braking mode switches the rotor from energy harvesting to drawing power from the battery to generate propulsion in order to reduce a descent rate of the UAV.

11. The UAV of claim 10 , wherein the processor is configured with the processor-executable instructions such that the braking mode includes regulating an amount of energy generated by the rotor in order to adjust an amount of drag generated by the rotor in order to control UAV attitude.

12. The UAV of claim 10 , wherein the processor is further configured with the processor-executable instructions to:
receive a signal commanding the UAV to use an extended flight protocol that includes the emergency recovery mode.

13. The UAV of claim 10 , wherein the processor is configured with the processor-executable instructions such that the emergency recovery mode comprises using at least one motor controlling at least one of the rotor to maintain a stable attitude by regulating an amount of energy generated by the at least one motor in order to adjust an amount of drag generated by the rotor.

14. The UAV of claim 10 , wherein the processor is configured with the processor-executable instructions such that the emergency-recovery state is a battery charge state in which the battery has insufficient energy stored therein to enable the UAV to maintain level flight.

15. The UAV of claim 10 , wherein the processor is configured with the processor-executable instructions such that the emergency-recovery state is measured from a voltage level of the battery.

16. The UAV of claim 10 , wherein the processor is configured with the processor-executable instructions such that the emergency-recovery state is a predetermined rate of change of a stored energy capacity of the battery.

Assignees

• Qualcomm Inc

Inventors

• Von Novak William Henry

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

• G05D1/0088

  characterized by the autonomous decision making process, e.g. artificial intelligence, predefined behaviours (using knowledge based models G06N5/00) · CPC title

• B64C2201/108

  Operations & Transport · mapped topic

• B64C2201/141

  Operations & Transport · mapped topic