This dissertation proposes a flapping control mechanism to solve the flight power problems in hoveringflight control of the insect-like flapping micro aerial vehicles(IFMAVs).
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。
2
The influences of nonuniform vertical flow on helicopter trim controls and regressive lag modal damping levels were analyzed in hovering and forward flight.