Thermal imaging of aircraft

1. A thermal imaging system to analyze aircraft, comprising:

one or more thermal imaging devices; and

a turn event controller in operative communication with the one or more thermal imaging devices, the turn event controller configured to:

receive an aircraft identifier associated with an aerial vehicle received proximate to the thermal imaging system, the aircraft identifier indicating equipment onboard the aerial vehicle and a model or configuration of the aerial vehicle;

obtain one or more vehicle parameters associated with the received aircraft, the one or more vehicle parameters including equipment information associated with the equipment onboard the aerial vehicle;

obtain, from the one or more thermal imaging devices positioned offboard of the received aerial vehicle, one or more thermal images that capture at least a portion of the aerial vehicle associated with the equipment onboard the aerial vehicle during at least one phase of a turn of the aerial vehicle at an airport;

receive, from a data store communicatively coupled with the turn event controller, expected thermal signature information associated with the equipment onboard the aerial vehicle;

detect one or more anomalies associated with the turn of the aerial vehicle based on the one or more thermal images and the expected thermal signature information; and

generate, in response to detecting the one or more anomalies, one or more signals indicative of the one or more anomalies.

2. The system of claim 1 , wherein the one or more thermal imaging devices comprise thermal imaging cameras.

3. The system of claim 1 , further comprising a thermal imaging processor in operative communication with the turn event controller and the one or more thermal imaging devices, wherein the thermal imaging processor is configured to analyze thermal images to determine whether a first thermal image depicts a thermal anomaly.

4. The system of claim 1 , wherein:

the one or more vehicle parameters include an identifier of a potential icing location on the aerial vehicle; and

detecting the one or more anomalies associated with the turn of the aerial vehicle based on the one or more thermal images and the expected thermal signature information comprises determining a temperature based on correlating the potential icing location with a particular portion of each of the one or more thermal images.

5. The system of claim 1 , wherein:

the one or more vehicle parameters include an identifier of a fuel tank location of a fuel tank of the aerial vehicle,

wherein the obtained one or more thermal images comprise one or more thermal images of the fuel tank captured by the one or more thermal imaging devices based on the fuel tank location, and

detecting the one or more anomalies associated with the turn of the aerial vehicle based on the one or more thermal images and the expected thermal signature information comprises determining a fuel level of fuel within the fuel tank based on the one or more thermal images of the fuel tank.

6. The system of claim 1 , wherein:

the one or more vehicle parameters include an identifier of a tire location of a tire of the aerial vehicle;

wherein the obtained one or more thermal images comprise one or more thermal images of the tire of the aerial vehicle captured by the one or more thermal imaging devices, and

detecting the one or more anomalies associated with the turn of the aerial vehicle based on the one or more thermal images and the expected thermal signature information comprises determining whether a temperature of the tire exceeds a target temperature.

7. The system of claim 1 , wherein the one or more thermal imaging devices are mobile thermal imaging devices that are movable relative to the aerial vehicle.

8. The system of claim 1 , wherein the turn event controller is further configured to verify that a heating-ventilation-and-air-conditioning (HVAC) system of the aircraft has been serviced by comparing the one or more thermal images and the expected thermal signature information.

9. The system of claim 1 , wherein the turn event controller is further configured to determine whether there is any external danger from fire or potential ignition sources proximate the aircraft by comparing the one or more thermal images and the expected thermal signature information.

10. The system of claim 1 , wherein the turn event controller is further configured to determine an approximate number and location of people on board the aircraft.

11. The system of claim 10 , wherein the turn event controller is further configured to determine if the approximate number of people on board the aircraft indicates illegal activity.

12. The system of claim 1 , wherein the turn event controller is further configured to issue a warning or alarm based on the one or more signals.

13. The system of claim 1 , wherein the turn event controller is further configured to prohibit the aerial vehicle from becoming airborne based on the one or more signals.

14. The system of claim 1 , wherein detecting the one or more anomalies associated with the turn of the aerial vehicle based on the one or more thermal images and the expected thermal signature information comprises comparing the one or more thermal images against the expected thermal signatures to identify the anomalies.

15. A computer-implemented method to analyze aircraft, comprising:

receiving an aircraft identifier associated with an aerial vehicle received proximate to one or more thermal imaging devices of a thermal imaging system, the aircraft identifier indicating equipment onboard the aerial vehicle and a model or configuration of the aerial vehicle;

obtaining one or more vehicle parameters associated with the aerial vehicle;

obtaining, from the one or more thermal imaging devices mounted offboard to the aerial vehicle, one or more thermal images associated with the aerial vehicle;

processing the one or more thermal images based on the one or more vehicle parameters to detect anomalies associated with an event associated with the aerial vehicle;

generating, in response to detecting one or more anomalies, one or more signals indicative of the one or more anomalies; and

issuing, based on the one or more signals, one or more warning messages based on the one or more signals.

16. The method of claim 15 , the one or more thermal imaging devices are mobile thermal imaging devices that are movable relative to the aerial vehicle.

17. The method of claim 15 , further comprising:

prohibiting the aerial vehicle from becoming airborne based on the one or more signals.

18. A thermal imaging system to analyze aircraft, comprising:

one or more thermal imaging devices; and

a turn event controller in operative communication with the one or more thermal imaging devices, the turn event controller configured to:

receive identifying information associated with an aerial vehicle to be analyzed by the thermal imaging system, the identifying information indicating equipment onboard the aerial vehicle;

obtain one or more thermal images that capture portions of the aerial vehicle associated with the equipment onboard the aerial vehicle during at least one phase of a turn of the aerial vehicle at an airport;

receive, from a data store communicatively coupled with the turn event controller, expected thermal signature information associated with the equipment identified onboard the aerial vehicle;

detect one or more anomalies associated with the turn of the aerial vehicle based on the obtained one or more thermal images and the expected thermal signature information; and

generate, in response to detecting the one or more anomalies, one or more signals indicative of the one or more anomalies.

19. The system of claim 18 , the one or more thermal imaging devices are mobile thermal imaging devices that are movable relative to the aerial vehicle.

20. The system of claim 18 , wherein the turn event controller is configured to:

obtain at least one of a passenger manifest, a flight crew manifest, and a cargo manifest associated with the aerial vehicle, and

obtain one or more interior thermal images associated with an interior of the aerial vehicle, and

wherein in detecting the one or more anomalies associated with the turn of the aerial vehicle, the turn event controller is configured to determine whether a mismatch between an actual heat signature of the interior of the aerial vehicle and an expected heat signature of the interior of the aerial vehicle is present based on the obtained one or more interior thermal images and the expected thermal signature information.