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公开(公告)号：KR1020130100566A
公开(公告)日：2013-09-11
申请号：KR1020120021890
申请日：2012-03-02
Abstract: PURPOSE: An unmanned air vehicle is provided to be controlled without the use of a servo motor by controlling the rotation speed of left and right drive motors formed on both sides of a main wing. CONSTITUTION: An unmanned air vehicle comprises a body (10), a main wing (20), left and right drive motors (41, 42), a control unit, and a battery. The body is arranged in a longitudinal direction. The main wing crosses the body and generates lift force. The left and right drive motors are arranged on both sides of the main wing to be extended to the rear of drive shafts (41a, 42a). Propellers (43) are coupled to the ends of the drive shafts. The control unit controls the rotation of the left and right drive motors according to previously inputted data. The battery is connected to the left and right drive motor and supplies power to the body.
Abstract translation: 目的：通过控制主翼两侧形成的左右驱动电机的转速，无需伺服电机就可以控制无人机。 构成：无人驾驶飞行器包括主体（10），主翼（20），左和右驱动马达（41,42），控制单元和电池。 主体沿纵向排列。 主翼横穿身体并产生升力。 左右驱动马达设置在主翼的两侧，以延伸到驱动轴（41a，42a）的后部。 螺旋桨（43）联接到驱动轴的端部。 控制单元根据先前输入的数据控制左右驱动马达的旋转。 电池连接到左右驱动电机，并向机体供电。
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