Aerial vehicle control using ballast
A system for controlling an aerial vehicle includes an aerial vehicle, a ballast coupled to the aerial vehicle, a server including a processor and a memory, and a wireless communication link that communicatively couples the aerial vehicle and the server. the memory stores instructions that, when executed by the processor, cause the server to receive weather data, determine, based on the weather data, that the aerial vehicle is experiencing, or is expected to experience, weather that satisfies a predetermined criterion, and cause the aerial vehicle to decouple at least a portion of the ballast based on a result of the determination.
1. A system for controlling an aerial vehicle, the system comprising:
an aerial vehicle;
a ballast coupled to the aerial vehicle; and
a server communicatively coupled to the aerial vehicle by means of a wireless communication link, the server including a processor and a memory storing instructions which, when executed by the processor, cause the server to:
receive weather data comprising one or both of a current and predicted future weather condition,
determine that an aspect of the weather data satisfies a predetermined criterion, and
cause the aerial vehicle to decouple at least a portion of the ballast based on the determination that the aspect of the weather data satisfies the predetermined criterion.
2. The system according to claim 1 , wherein the determining that the aspect of the weather data satisfies the predetermined criterion includes determining that a temperature metric included in the weather data is below a predetermined threshold.
3. The system according to claim 2 , wherein the instructions, when executed by the processor, further cause the server to determine the portion of the ballast to decouple based on an amount by which the temperature metric is below the predetermined threshold.
4. The system according to claim 3 , wherein the determining of the portion of the ballast to decouple is further based on an altitude of the aerial vehicle.
5. The system according to claim 2 , wherein the predetermined threshold is based on an altitude of the aerial vehicle and an amount of gas inside the aerial vehicle.
6. The system according to claim 1 , wherein the determining that the aspect of the weather data satisfies the predetermined criterion includes determining that a temperature of gas inside the aerial vehicle is expected to cause the aerial vehicle to experience zero superpressure.
7. The system according to claim 6 , wherein determining that the temperature of gas inside the aerial vehicle is expected to cause the aerial vehicle to experience zero superpressure includes determining that a level of infrared radiation experienced at an altitude of the aerial vehicle is expected to cause a temperature of the gas inside the aerial vehicle to drop below a predetermined threshold.
8. The system according to claim 7 , wherein the predetermined threshold is determined based on an amount of gas inside the aerial vehicle.
9. The system according to claim 7 , wherein the instructions, when executed by the processor, further cause the server to determine the portion of the ballast to decouple based on an amount of gas inside the aerial vehicle.
10. The system according to claim 9 , wherein the determining of the portion of the ballast to decouple is further based on the altitude of the aerial vehicle.
11. The system according to claim 6 , wherein the instructions, when executed by the processor, further cause the server to determine whether the aerial vehicle is expected to recover from experiencing zero superpressure.
12. The system according to claim 11 , wherein the instructions, when executed by the processor, further cause the server to determine an altitude to which the aerial vehicle is expected to descend while the aerial vehicle experiences zero superpressure.
13. The system according to claim 12 , wherein the instructions, when executed by the processor, further cause the server to determine whether the altitude to which the aerial vehicle is expected to descend while the aerial vehicle experiences zero superpressure is above a minimum altitude.
14. The system according to claim 13 , wherein the instructions, when executed by the processor, further cause the server to cause the aerial vehicle to descend to the ground prior to experiencing zero superpressure in response to a determination that the altitude to which the aerial vehicle is expected to descend while the aerial vehicle experiences zero superpressure is not above the minimum altitude.
15. The system according to claim 1 , wherein the weather data is received from an external source.
16. The system according to claim 1 , wherein the weather data is received from a sensor coupled to the aerial vehicle.
17. The system according to claim 1 , wherein the aerial vehicle includes a balloon.
18. The system according to claim 1 , wherein the ballast is composed of a granular substance.
19. A method for controlling an aerial vehicle, the method comprising:
receiving, by a server, weather data comprising one or both of a current and predicted future weather condition;
determining, by the server, that an aspect of the weather data satisfies a predetermined criterion; and
causing, by the server and a wireless communication link communicatively coupling the server to the aerial vehicle, the aerial vehicle to decouple at least a portion of a ballast coupled to the aerial vehicle based on the determination that the aspect of the weather data satisfies the predetermined criterion.
20. A non-transitory computer-readable storage medium storing instructions which, when executed by a processor, cause a computing device to:
receive weather data comprising one or both of a current and predicted future weather condition;
determine that an aspect of the weather data satisfies a predetermined criterion; and
cause the aerial vehicle to decouple at least a portion of a ballast coupled to the aerial vehicle based on the determination that the aspect of the weather data satisfies the predetermined criterion.