一种微型仿昆扑翼飞行器扑翼操控机制

提出了一种扑翼操控机制,用于解决微型仿昆扑翼飞行器悬停飞行的飞行动力问题。通过对扑翼运动参数对气动力及空气动力矩的作用进行理论和仿真分析,设计了一种采用可变幅值的周期函数调节扑翼运动的扑打角和旋转角变化的方法,实现对气动力和气动力矩进行独立控制的操控机制。仿真结果验证了此操控机制可以较好地解决仅一对翼的仿昆扑翼飞行器飞行动力问题。

Flapping control mechanism for insect-like flapping micro aerial vehicles

This dissertation proposes a flapping control mechanism to solve the flight power problems in hovering flight control of the insect-like flapping micro aerial vehicles(IFMAVs).By analyzing and simulating the relationship among flapping kinematic parameters and aerodynamic forces and moments it designs a flapping control mechanism by using the vaviable breadth periodic functions to adjust the stroke angle and rotation angle,which can realize the control of the aerodynamic forces and moments independently.The...