near-hovering flight 近悬停状态飞行
hovering flight control system 悬停控制系统
The Mechanics of Hovering Flight 唱片名
hovering and forward flight 悬停与前飞状态
Mainly referring to the study results in the aerodynamics of the FMAV from the University of California at Berkeley, This dissertation takes the size of 10～25mm (wingtip-to-wingtip) FMAV as research object, and takes the hovering flight control as research task.
本论文主要参考美国伯克利大学对扑翼微型飞行器空气动力学的部分研究成果,以实现翼展为10～25mm(翼尖到翼尖)扑翼微型飞行器的悬停飞行控制为研究任务。
参考来源 - 扑翼微型飞行器动力学建模与控制算法研究·2,447,543篇论文数据，部分数据来源于NoteExpress
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。
The influences of nonuniform vertical flow on helicopter trim controls and regressive lag modal damping levels were analyzed in hovering and forward flight.
分析了直升机从悬停到小速度前飞时，定常垂直气流的非均匀分布对直升机平衡操纵以及对系统摆振后退型模态阻尼的影响。
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