阅读说明：本技术 无人机的动力输出检测方法和设备 (Power output detection method and equipment for unmanned aerial vehicle ) 是由 王晓亮 吕熙敏 商志猛 于 2020-05-07 设计创作，主要内容包括：无人机(110,201,1400,1601)的动力输出检测方法和设备,方法包括：获取电机(152,1412)的控制指令,电机(152,1412)的控制指令用于指示电机(152,1412)的期望转速(S301,S801,S1201)；根据电机(152,1412)的期望转速、无人机(110,201,1400,1601)的角速度和线加速度,获得无人机(110,201,1400,1601)的动力系统(150,1410)的动力输出状况(S302,S803)。无需电机(152,1412)的测量转速也能得到动力系统(150,1410)的动力输出状况,确保在电调(151,1411)出现故障时也能检测动力系统(150,1410)的动力输出状况,以便在出现动力失效时,做好对无人机(110,201,1400,1601)的控制措施,避免无人机(110,201,1400,1601)坠机。(Method and apparatus for power output detection of a drone (110, 201, 1400, 1601), the method comprising: acquiring a control instruction of the motor (152, 1412), wherein the control instruction of the motor (152, 1412) is used for indicating a desired rotating speed (S301, S801, S1201) of the motor (152, 1412); obtaining a power output condition (S302, S803) of a power system (150, 1410) of the unmanned aerial vehicle (110, 201, 1400, 1601) according to a desired rotation speed of the motor (152, 1412), an angular velocity and a linear acceleration of the unmanned aerial vehicle (110, 201, 1400, 1601). The power output condition of the power system (150, 1410) can be obtained without the measured rotating speed of the motor (152, 1412), the power output condition of the power system (150, 1410) can be detected when the electric speed regulator (151, 1411) breaks down, so that control measures for the unmanned aerial vehicle (110, 201, 1400, 1601) are made when power failure occurs, and the unmanned aerial vehicle (110, 201, 1400, 1601) is prevented from falling down.)