The invention relates to the field of unmanned aerial vehicles, and particularly relates to a tandem unmanned aerial vehicle control method. An unmanned aerial vehicle is a double-rotor-wing unmannedaerial vehicle, a front rotor wing and a rear rotor wing comprise cross plates respectively, each cross plate is a front cross plate or a rear cross plate, the front cross plates and the rear cross plates rotate clockwise and anticlockwise, and each cross plate is controlled by three steering engines to achieve flight. The front cross plate comprises M1 to M3 groups of steering engines, and the rear cross plate comprises M4 to M6 groups of steering engines; an engine provides a power source for the double-rotor-wing unmanned aerial vehicle, namely the tandem double-propeller unmanned aerial vehicle, and an attitude of the unmanned aerial vehicle is controlled by controlling a rotor wing system; and each cross plate is provided with three steering engines which are controlled through a constant-speed variable-pitch mode, the rotating speeds of the two paddles are constant in the flying process, the rotating speed directions are opposite, and torsion of the two paddles in the rotating process is overcome.
本发明涉及无人机领域,尤其涉及一种纵列式无人机控制方法无人机为双旋翼无人机,前后两个旋翼分别包含一个十字盘,十字盘为前十字盘或者后十字盘,前后十字盘逆顺时针旋转,每个十字盘由3个舵机控制,实现飞行;前十字盘包含M1到M3三组舵机,后十字盘包含M4到M6三组舵机;双旋翼无人机即纵列式双桨无人机由一个发动机提供动力源,通过控制旋翼系统来控制飞机的姿态;每个十字盘有3个舵机通过定速变距的模式来控制,飞行时两副浆的转速恒定,转速方向相反,克服了两幅浆在旋转时的扭力。
Tandem unmanned aerial vehicle control method
一种纵列式无人机控制方法
2020-11-27
Patent
Electronic Resource
Chinese
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