Managing power of aerial vehicles

1. A system for managing power of an aerial vehicle, the system comprising:

an aerial vehicle including:

a power storage module, and

at least one component; and

a computing device communicatively coupled to the aerial vehicle, the computing device including a processor and a memory storing instructions which, when executed by the processor, cause the computing device to:

receive data indicating a state of charge of the power storage module,

receive data indicating a location of the aerial vehicle,

determine a time until sunrise based on the data indicating the location of the aerial vehicle,

receive data indicating a rate of power consumption of the at least one component,

generate, based on the determined time until sunrise and at least one of the state of charge of the power storage module or the rate of power consumption of the at least one component, a power command to switch the at least one component to a power-saving state, and

transmit the power command to the aerial vehicle.

2. The system according to claim 1 , wherein the instructions, when executed by the processor, further cause the computing device to:

determine, based on the data indicating the state of charge of the power storage module and the data indicating the rate of power consumption of the at least one component, that the state of charge of the power storage module is insufficient to provide power to the at least one component until sunrise, and

wherein the generation of the power command is further based on the determination that the state of charge of the power storage module is insufficient to provide power to the at least one component until sunrise.

3. The system according to claim 2 , wherein the instructions, when executed by the processor, further cause the computing device to determine whether the rate of power consumption is greater than a threshold.

4. The system according to claim 3 , wherein the determination whether the state of charge of the power storage module is insufficient to provide power to the at least one component is further based on the determination whether the rate of power consumption is greater than the threshold.

5. The system according to claim 2 , wherein the instructions, when executed by the processor, further cause the computing device to determine an expected amount of power required to provide power to the at least one component until sunrise based on the data indicating the rate of power consumption of the at least one component.

6. The system according to claim 5 , wherein the determining that the state of charge of the power storage module is insufficient to provide power to the at least one component until sunrise is further based on the determined expected amount of power required to provide power to the at least one component until sunrise.

7. The system according to claim 1 , wherein the at least one component includes at least one flight-related component,

wherein the data indicating the rate of power consumption of the at least one component includes at least a rate of power consumption of the at least one flight-related component, and

wherein the instructions, when executed by the processor, further cause the computing device to determine, based on the data indicating the rate of power consumption of the at least one flight-related component and the determined time until sunrise, an expected amount of power required to provide power to the at least one flight-related component until sunrise.

8. The system according to claim 7 , wherein the instructions, when executed by the processor, further cause the computing device to determine, based on the data indicating the state of charge of the power storage module and the expected amount of power required to provide power to the at least one flight-related component until sunrise, that the state of charge of the power storage module is greater than the expected amount of power required to provide power to the at least one flight-related component until sunrise.

9. The system according to claim 8 , wherein the instructions, when executed by the processor, further cause the computing device to determine an expected amount of allocable power, the expected amount of allocable power corresponding to a difference between the state of charge of the power storage module and the expected amount of power required to provide power to the at least one component until sunrise.

10. The system according to claim 9 , wherein the instructions, when executed by the processor, further cause the computing device to generate a power allocation plan based on the expected amount of allocable power.

11. The system according to claim 10 , wherein the at least one component further includes at least one non-flight-related component,

wherein the data indicating the rate of power consumption of the at least one component further includes at least a rate of power consumption of the at least one non-flight-related component, and

wherein the instructions, when executed by the processor, further cause the computing device to determine, based on the data indicating the rate of power consumption of the at least one non-flight-related component and the determined time until sunrise, an expected amount of power required to provide power to the at least one non-flight-related component until sunrise, and

wherein the generation of the power allocation plan is further based on the determined expected amount of power required to provide power to the at least one non-flight-related component until sunrise.

12. The system according to claim 10 , wherein the at least one component further includes at least a first non-flight-related component and a second non-flight-related component,

wherein the data indicating the rate of power consumption of the at least one component further includes at least a rate of power consumption of the first non-flight-related component and the second non-flight-related component, and

wherein the instructions, when executed by the processor, further cause the computing device to determine, based on the data indicating the rate of power consumption of the first non-flight-related component and the rate of power consumption of the second non-flight-related component and the determined time until sunrise, an expected amount of power required to provide power to the first non-flight-related component and the second non-flight-related component until sunrise,

wherein the generation of the power allocation plan is further based on the determined expected amount of power required to provide power to the first non-flight-related component and the second non-flight-related component until sunrise.

13. The system according to claim 12 , wherein the power allocation plan includes an instruction to switch one of the first non-flight-related component or the second non-flight-related component to a power-saving state.

14. The system according to claim 13 , wherein the rate of power consumption of the first non-flight-related component is different from the rate of power consumption of the second non-flight-related component, and

wherein the instruction to switch one of the first non-flight-related component or the second non-flight-related component to a power-saving state is based on the difference in the rate of power consumption of the first non-flight-related component and rate of power consumption of the second non-flight-related component.

15. The system according to claim 13 , wherein the first non-flight-related component has a different function from the second non-flight-related component, and

wherein the instruction to switch one of the first non-flight-related component or the second non-flight-related component to a power-saving state is based on the difference in function between the first non-flight-related component and the second non-flight-related component.

16. The system according to claim 1 , wherein the at least one component includes at least one flight-related component and at least one non-flight-related component, and

wherein the non-flight-related component is the at least one component switched to a power-saving state.

17. The system according to claim 1 , wherein the aerial vehicle includes a balloon.

18. A method for managing power of an aerial vehicle, the method comprising:

receiving data indicating a state of charge of a power storage module of the aerial vehicle;

receiving data indicating a location of the aerial vehicle;

determining a time until sunrise based on the data indicating the location of the aerial vehicle;

receiving data indicating a rate of power consumption of at least one component of the aerial vehicle;

generating, based on the determined time until sunrise and at least one of the state of charge of the power storage module or the rate of power consumption of the at least one component, a power command to switch the at least one component to a power-saving state; and

transmitting the power command to the aerial vehicle.

19. A non-transitory computer-readable storage medium storing instructions which, when executed by a processor, cause a computing device to:

receive data indicating a state of charge of a power storage module of an aerial vehicle;

receive data indicating a location of the aerial vehicle;

determine a time until sunrise based on the data indicating the location of the aerial vehicle;

receive data indicating a rate of power consumption of at least one component of the aerial vehicle;

generate, based on the determined time until sunrise and at least one of the state of charge of the power storage module or the rate of power consumption of the at least one component, a power command to switch the at least one component to a power-saving state; and

transmit the power command to the aerial vehicle.

20. The method according to claim 18 , further comprising:

determining, based on the data indicating the state of charge of the power storage module and the data indicating the rate of power consumption of the at least one component, that the state of charge of the power storage module is insufficient to provide power to the at least one component until sunrise, and

wherein the generating of the power command is further based on the determination that the state of charge of the power storage module is insufficient to provide power to the at least one component until sunrise.