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SYSTEM AND METHOD FOR AUTONOMOUS LANDING OF ROTOR TYPE UNMANNED AREIAL VEHICLE

机译:转子式无人飞行器自动着陆的系统和方法

摘要

According to an embodiment of the present invention, an automatic landing system for a rotary-wing unmanned aircraft includes: a vision sensor part sensing a beam generated from a marker indication part prepared on a landing point of a rotary-wing unmanned aircraft; a horizontal error calculating part calculating a horizontal distance error between the marker indication part and the vision sensor part; a vertical velocity calculating part calculating the vertical velocity of the rotary-wing unmanned aircraft by receiving a horizontal position of the rotary-wing unmanned aircraft from the vision sensor part; an altitude estimating part estimating a desired altitude of the rotary-wing unmanned aircraft by receiving the vertical velocity from the vertical velocity calculating part; a vertical controller controlling the thrust of the rotary-wing unmanned aircraft by receiving the desired altitude of the rotary-wing unmanned aircraft from the altitude estimating part; a horizontal controller generating a target posture of the rotary-wing unmanned aircraft by receiving the horizontal position and horizontal velocity of the rotary-wing unmanned aircraft from the vision sensor part or horizontal error calculating part; and a purge control part connected to the horizontal error calculating part and the vertical velocity calculating part to adjust the vertical velocity which is dependent on the horizontal distance error.
机译:根据本发明的实施例,一种用于旋转翼无人飞行器的自动着陆系统包括:视觉传感器部分,其感测从在旋转翼无人飞行器的着陆点上准备的标记指示部分产生的光束;水平误差计算部分计算标记指示部分和视觉传感器部分之间的水平距离误差;垂直速度计算部分通过从视觉传感器部分接收旋转翼无人机的水平位置来计算旋转翼无人机的垂直速度;高度估计部通过从垂直速度计算部接收垂直速度来估计旋翼无人机的期望高度;垂直控制器,其通过从高度估计部接收期望的旋翼无人机的高度来控制旋翼无人机的推力;水平控制器通过从视觉传感器部分或水平误差计算部分接收旋转翼无人机的水平位置和水平速度来产生旋转翼无人机的目标姿态;吹扫控制部,其与水平误差计算部和垂直速度计算部连接,以调整取决于水平距离误差的垂直速度。

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