CPC G05D 1/106 (2019.05) [B64C 39/024 (2013.01); G01S 19/42 (2013.01); G05D 1/104 (2013.01); B64U 10/13 (2023.01); B64U 2201/10 (2023.01)] | 15 Claims |
1. An unmanned aerial vehicle (UAV) control system comprising:
a first UAV;
a second UAV that flies near the first UAV during a flight of the first UAV and is configured to obtain present wind information; and
at least one processor configured to:
control the flight of the first UAV based on the wind present information obtained by the second UAV;
obtain first position information about a position of the first UAV;
obtain second position information about a position of the second UAV;
control the flight of the first UAV further based on the first position information and the second position information; and
control the flight of the first UAV based on the present wind information when the second UAV is on a windward side of the first UAV;
wherein the windward side is upwind of the first UAV.
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