The invention relates to an electronic speed regulator control method and system. The electronic speed regulator control method comprises the following steps: receiving an accelerator signal output by a controller, and correspondingly controlling a left driving motor and a right driving motor to synchronously run; receiving a steering signal output by the controller, wherein the steering signal carries a direction value and a steering value; judging that the direction value is left or right based on the direction value; if the direction value is left, controlling the rotating speed of the left driving motor to be smaller than that of the right driving motor based on the steering value; and if the direction value is right, controlling the rotating speed of the right driving motor to be smaller than that of the left driving motor based on the steering value. When the steering signal output by the controller is received, the left driving motor and the right driving motor are correspondingly controlled to form a rotating speed difference, and a left propeller and a right propeller are correspondingly controlled to have a rotating speed difference, so that leftward or rightward torque is generated on the aircraft, and the steering radius of the aircraft is reduced in cooperation with a tail vane, so that the aircraft can quickly steer.
本申请涉及一种电子调速器控制方法及系统。一种电子调速器控制方法,包括以下步骤:接收控制器输出的油门信号,以对应控制左驱动电机和右驱动电机同步运转;接收控制器输出的转向信号,其中,转向信号中携带有方向值和转向值;基于方向值判断为左或右;若方向值为左,则基于转向值控制左驱动电机的转速小于右驱动电机的转速;若方向值为右,则基于转向值控制右驱动电机的转速小于左驱动电机的转速。接收控制器输出的转向信号时,对应控制左驱动电机和右驱动电机之间形成转速差,左螺旋桨与右螺旋桨之间存在转速差,进而在飞行器上产生向左或向右的力矩,配合尾舵,实现缩小飞行器的转向半径,以便于飞行器快速转向。
Electronic speed regulator control method and system
电子调速器控制方法及系统
2021-08-27
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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