As micro flapping flight is investigated further, its control is paid more attention to.
随着微扑翼飞行器研究的不断深入，对其控制问题研究已引起了人们的重视。
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).
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。
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