Therefore, the characteristics, the influence on the stability and control, as well as the design theories of the FMAV empennage are studied here.
本文对微型扑翼飞行器尾翼的特性、对稳定性和操纵性的影响以及尾翼的设计理论与方法进行了研究。
Based on statistics and analysis of flying parameters of birds, the biomimetic formulas are brought forth and original FMAV design is carried out.
在对鸟类的飞行参数进行统计分析的基础之上，拟合出扑翼飞行的仿生学公式，并据此进行了微扑翼飞行器的仿生学初步设计。
The evaluation methods and step of the loading for the FMAV are set up so that these Euler angles can be specified to provide wing motions that generate the lift and propulsion for the vehicle.
建立由欧拉角所确定的扑翼飞行器的载荷计算方法和步骤，揭示出扑翼飞行器通过扑翼运动同时产生升力、推力的机理。
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