The invention belongs to the technical field of flapping wing aircrafts, and relates to a hovering tailless flapping wing aircraft and a control method thereof.The aircraft comprises a carbon rod framework, flapping wing assemblies, a control assembly and a steering engine direction changing assembly, and the flapping wing assemblies are symmetrically installed on the two sides of the carbon rod framework; the control assembly is fixedly installed on the carbon rod framework and connected with and controls the steering engine turning assembly through a signal line, the steering engine turning assembly comprises an upper steering engine and a lower steering engine which are installed on the head portion and the tail portion of the carbon rod framework respectively, and rotation of the pitch angle of the aircraft is controlled by adjusting the angle of the upper steering engine. And the yaw angle rotation of the aircraft is controlled by adjusting the angle of the lower steering engine. According to the aircraft, the hovering and autonomous control functions are achieved, manufacturing is easy, the structure is compact, low noise and flight safety in the flight process are guaranteed through the flexible wings, and the aircraft has great potential in application scenes such as aerial inspection and reconnaissance.
本发明属于扑翼飞行器技术领域,涉及一种可悬停的无尾扑翼飞行器及其控制方法,该飞行器包括碳杆骨架、扑翼组件、控制组件、舵机变向组件,所述扑翼组件对称安装在碳杆骨架两侧,控制组件固定安装在碳杆骨架上并通过信号线连接控制舵机变向组件,舵机变向组件包括分别安装在碳杆骨架头部和尾部的上方舵机和下方舵机,通过调整上方舵机角度控制飞行器俯仰角的转动,通过调整下方舵机角度控制飞行器偏航角的转动。本发明的飞行器实现了空中悬停和自主控制功能,且制作简单,结构紧凑,柔性翅膀保证了飞行过程的低噪声和飞行安全性,在空中巡检、侦察等应用场景中拥有较大潜力。
Tailless flapping-wing aircraft capable of hovering and control method thereof
一种可悬停的无尾扑翼飞行器及其控制方法
2024-07-05
Patent
Electronic Resource
Chinese
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