CPC G08G 5/0069 (2013.01) [B64U 30/20 (2023.01); B64U 10/14 (2023.01); B64U 50/19 (2023.01); B64U 2201/20 (2023.01)] | 20 Claims |
1. A control method for an aerial vehicle comprising:
generating, before the aerial vehicle takes off, a control signal that controls multiple actuators of the aerial vehicle each including a corresponding one of multiple propellers, the multiple propellers being configured to be mounted in the multiple actuators, respectively;
controlling the multiple actuators to operate based on the control signal;
obtaining status information of the aerial vehicle when the multiple actuators are operating in response to the control signal; and
determining whether at least one of the multiple propellers is abnormally mounted according to the status information.
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