Power management system for air mobility vehicle and operation method thereof

1. A power management system for an air mobility vehicle, the power management system comprising:

a plurality of batteries configured to provide power to a propulsion unit of the air mobility vehicle to propel the air mobility vehicle;

a discharge control unit configured to monitor an operation state and a charge state of each of the plurality of batteries, to determine a discharge mode of each of the plurality of batteries according to the monitored operation state and the monitored charge state, and control whether each of the plurality of batteries is discharged or a discharge rate thereof according to the determined discharge mode; and

a discharge guide unit configured to guide information on the determined discharge mode to a user when the discharge mode of each of the plurality of batteries is determined by the discharge control unit.

2. The power management system of claim 1 ,

wherein the operation state of each of the plurality of batteries includes whether each of the plurality of batteries is in a normal state or a fault state, and

wherein the charge state of each of the plurality of batteries includes a remaining capacity of each of the plurality of batteries and an average remaining capacity of all of the plurality of batteries.

3. The power management system of claim 1 ,

wherein the discharge mode of each of the plurality of batteries includes a single discharge mode, a parallel discharge mode, or an output limit mode, and

wherein the discharge control unit is configured to determine the discharge mode of each of the plurality of batteries considering a flight status of the air mobility vehicle.

4. The power management system of claim 3 , wherein the flight status of the air mobility vehicle includes taking off, ascending, cruising, descending, or landing of the air mobility vehicle.

5. The power management system of claim 1 , wherein the discharge control unit is configured for controlling whether each of the plurality of batteries is discharged or the discharge rate thereof by setting an output of the propulsion unit according to the determined discharge mode and selecting a battery among the plurality of batteries to provide power to the propulsion unit according to the set output.

6. The power management system of claim 5 ,

wherein the discharge mode of each of the plurality of batteries includes a single discharge mode, a parallel discharge mode, or an output limit mode,

wherein the discharge control unit is configured to determine the discharge mode of each of the plurality of batteries considering a flight status of the air mobility vehicle,

wherein the flight status of the air mobility vehicle includes taking off, ascending, cruising, descending, or landing of the air mobility vehicle, and

wherein the single discharge mode, the parallel discharge mode, and the output limit mode are determined according to a remaining capacity of the selected battery.

7. The power management system of claim 1 , wherein the discharge control unit is configured to determine a discharge current and a discharge time of each of the plurality of batteries and is configured to control the discharge rate of each of the plurality of batteries according to the determined discharge current and the determined discharge time.

8. The power management system of claim 1 ,

wherein the discharge control unit is configured to perform discharging of a battery to be discharged by controlling whether each of the plurality of batteries is discharged or the discharge rate thereof, and

wherein the discharge control unit stops discharging the battery to be discharged when a charge state of the battery to be discharged is equal to or less than a predetermined reference.

9. A method of operating a power management system for an air mobility vehicle, the method comprising:

monitoring, by a discharge control unit, an operation state and a charge state of each of a plurality of batteries;

determining, by the discharge control unit, a discharge mode of each of the plurality of batteries according to the determined operation state and the determined charge state of each of the plurality of batteries;

controlling, by the discharge control unit, whether each of the plurality of batteries is discharged or a discharge rate thereof according to the determined discharge mode; and

guiding, by a discharge guide unit, information on the determined discharge mode to a user, when the discharge mode of each of the plurality of batteries is determined.

10. The method of claim 9 ,

wherein the operation state of each of the plurality of batteries includes whether each of the plurality of batteries is in a normal state or a fault state, and

wherein the charge state of each of the plurality of batteries includes a remaining capacity of each of the plurality of batteries and an average remaining capacity of all of the plurality of batteries.

11. The method of claim 9 ,

wherein the discharge mode of each of the plurality of batteries includes a single discharge mode, a parallel discharge mode, or an output limit mode, and

wherein the discharge control unit is configured to determine the discharge mode of each of the plurality of batteries considering a flight status of the air mobility vehicle.

12. The method of claim 11 , wherein the flight status of the air mobility vehicle includes taking off, ascending, cruising, descending, or landing of the air mobility vehicle.

13. The method of claim 9 , further including:

performing, by the discharge control unit, discharge of a battery to be discharged according to whether each of the plurality of batteries is discharged or the discharge rate thereof, after the controlling whether each of the plurality of batteries is discharged or the discharge rate thereof according to the determined discharge mode.

14. The method of claim 13 ,

wherein the discharge mode of each of the plurality of batteries includes a single discharge mode, a parallel discharge mode, or an output limit mode,

wherein the discharge control unit is configured to determine the discharge mode of each of the plurality of batteries considering a flight status of the air mobility vehicle,

wherein the flight status of the air mobility vehicle includes taking off, ascending, cruising, descending, or landing of the air mobility vehicle, and

wherein the single discharge mode, the parallel discharge mode, and the output limit mode are determined according to a remaining capacity of the battery.

15. The method of claim 13 , further including:

stopping, by the discharge control unit, discharging the battery to be discharged when a charge state of the battery to be discharged is equal to or less than a predetermined reference, after the performing discharge of the battery to be discharged.

16. A non-transitory computer readable storage medium on which a program for performing the method of claim 9 is recorded.