The invention relates to the technical field of unmanned aerial vehicle launching, in particular to a fixed-wing unmanned aerial vehicle launcher and a launching method.The fixed-wing unmanned aerial vehicle launcher comprises an unmanned aerial vehicle supporting plate, a friction wheel launching mechanism, a chassis, an angle adjusting mechanism, a pitching adjusting mechanism, an industrial camera and a controller, a transmitting channel is formed between the two groups of friction wheels, and the rotating speed of the friction wheels is adjustable; the industrial camera is used for capturing flying objects in the air in real time, the angles needing to be adjusted by the angle adjusting mechanism and the pitching adjusting mechanism and the launching speed of the friction wheel launching mechanism are calculated in combination with an algorithm, and the launching direction, the launching pitching angle and the launching speed are adjusted in real time. The unmanned aerial vehicle is launched to a preset position in the air at a set launching direction, a launching pitch angle and a speed through multiple groups of friction wheels, so that unmanned aerial vehicle formation is quickly completed, and the difficulty of unmanned aerial vehicle air formation is reduced.
本发明涉及无人机发射技术领域,具体涉及一种固定翼无人机发射架及发射方法,包括:无人机托板、摩擦轮发射机构、底盘、角度调节机构、俯仰调节机构、工业摄像机和控制器,其中,所述摩擦轮发射机构包括两组摩擦轮,使得两组所述摩擦轮之间形成发射通道,所述摩擦轮设置为转速可调;利用工业摄像机实时捕捉空中飞行物,结合算法计算出角度调节机构、俯仰调节机构所需要调整的角度,以及摩擦轮发射机构的发射速度,并实时调整发射方向、发射俯仰角和发射速度,通过多组摩擦轮将无人机以设定发射方向、发射俯仰角以及速度发射至空中的预定位置,快速完成无人机编队,降低无人机空中编队的难度。
Fixed-wing unmanned aerial vehicle launcher and launching method
固定翼无人机发射架及发射方法
2024-06-14
Patent
Electronic Resource
Chinese
IPC: | B64U |
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