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Design and analysis of an innovative flapping wing micro aerial vehicle with a figure eight wingtip trajectory

机译:创新泛翼微空中飞行器的设计与分析,具有图8的翼尖轨迹

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A multi-mode flapping wing micro air vehicle?(FWMAV) that uses a figure eight wingtip motion trajectory with wing flapping, rotation, and swing motion is presented in this paper. The flapping wing vehicle achieves three active degrees of freedom?(DOF) wing movements only with one driving micromotor which has a good balance in the mechanism design (that is inspired by natural fliers) and total weight. Owing to these characteristics being integrated into the simple mechanism design, the aerodynamic force is improved. The aerodynamic performance of the thrust force is improved by 64.3?% compared to one that could only flap up and down with one active DOF under the condition of routine flapping frequency.
机译:本文提出了一种多模扇形微型空气车辆?(FWMAV),使用图8的翼尖运动轨迹,旋转,旋转和摆动运动。 漂移的翼车实现了三个活跃的自由度?(DOF)翼移动仅具有一个驱动微电机,其在机构设计中具有良好的平衡(由天然圆锥形的启发)和总重量。 由于这些特性集成到简单的机构设计中,有改善空气动力力。 与一个在常规拍摄频率的条件下,推力的气动性能提高了64.3倍的倍数,其只能在一个活性DOF上向上和下调。

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