A control method of an unmanned aerial vehicle comprises determining a power demand for the unmanned aerial vehicle to perform an action (S110); determining the power output capability of the battery assembly according to the attribute information of the action and the state parameter of the battery assembly (S120); and controlling the unmanned aerial vehicle to perform a corresponding operation according to the power demand of the action and the power output capability of the battery assembly (S130). The invention also provides a battery power state management method, an unmanned aerial vehicle, electronic equipment and a storage medium.
一种无人飞行器的控制方法,包括:确定无人飞行器执行一动作的功率需求(S110);根据动作的属性信息和电池组件的状态参数确定电池组件的功率输出能力(S120);根据动作的功率需求和电池组件的功率输出能力,控制无人飞行器执行相应的操作(S130)。还提供了电池功率状态管理方法、无人飞行器、电子设备和存储介质。
Unmanned aerial vehicle, control method, electronic equipment and battery power state management method
无人飞行器及控制方法、电子设备及电池功率状态管理方法
2021-05-04
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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