| CPC A62C 3/025 (2013.01) [B64D 1/02 (2013.01); B64U 2101/47 (2023.01); B64U 2201/10 (2023.01)] | 10 Claims |

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1. A method performed by a control system of an unmanned aerial vehicle (UAV), the method comprising:
actuating, using an ignition system of the UAV, one or more delayed-ignition balls of a plurality of delayed-ignition balls stored in a container of the UAV over a site of a prescribed burn and dropping the actuated one or more delayed-ignition balls from the UAV onto the site of the prescribed burn;
while flying over the site of the prescribed burn, generating a temperature map of at least a portion of the site of the prescribed burn; and
navigating, using the aerial propulsion system, the site of the prescribed burn using the temperature map, wherein navigating the site of the prescribed burn using the temperature map comprises detecting a higher temperature and flying the UAV to a lower temperature to protect the UAV, and
wherein navigating the site of the prescribed burn using the temperature map comprises developing a new ignition pattern by altering an ignition path to keep the UAV over an unburned area of the site of the prescribed burn.
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