| CPC B64D 17/62 (2013.01) [B64U 10/25 (2023.01); B64U 70/83 (2023.01); G05D 1/0011 (2013.01); G05D 1/0094 (2013.01); G05D 1/0202 (2013.01); G05D 1/12 (2013.01); G05D 1/223 (2024.01); G05D 1/686 (2024.01); G05D 1/689 (2024.01); G05D 1/692 (2024.01); B64U 2101/30 (2023.01); B64U 2201/104 (2023.01); B64U 2201/20 (2023.01)] | 19 Claims |

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1. A system for unmanned aerial vehicle (UAV) parachute landing, the system comprising:
a memory storing instructions;
a processor configured to execute the instructions to cause the system to:
determine whether to open a parachute of the UAV in accordance with a criterion; and
responsive to a determination to open the parachute of the UAV:
stop a motor of the UAV that spins a propeller of the UAV,
wait for a specific period after stopping the motor, and
open the parachute of the UAV; and
a detector configured to detect wind direction;
wherein the processor is configured to execute the instructions to cause the system to stop the motor of the UAV when the UAV flies against wind.
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