Flexibility of flapping wing and its effect on aerodynamic characteristic 扑翼柔性及其对气动特性的影响
The development and test on wing type of a bionic flying micro - robot 仿生扑翼飞行机器人翅型的研制与实验研究
Aerospace series . rowings . measurement of the equitension of the base strands 航空航天系列.扑翼机.底板绞线的等拉伸力的测量
Status and prospects of driving mode about the wing for the bionics flapping aerocraft 仿生扑翼飞行器翅翼驱动方式的研究现状及展望
Attitude tracking control for flapping wing micro aerial vehicle based on feedback compensation 基于反馈补偿的扑翼微型飞行器姿态跟踪控制
The bionic flying micro - robot is a complicated intelligent robot , i . e . and a micro aerial vehicle 摘要微型仿生扑翼飞行器是一种新概念的微型飞行器。
The modeling and analysis method , as well as the conclusions are helpful to the design , fabrication and application of fmav 文中的建模、分析方法及所得结论为微扑翼飞行器机翼的设计、制作和应用提供了一定的理论依据。
Applying this dissertation , the aerodynamic characteristics of flapping wing can be calculated , the effects of every factor can be analyzed and some qualitative instructions can be given 运用本文可以计算扑翼的气动特性及分析各参数对扑翼气动特性的影响,进而指导扑动翼微型飞机的初期设计。
5 . effects of unsteady flows on the aerodynamic characteristics are also analyzed . the results of this dissertation are useful for the further investigations of three - dimensional flapping wing 对于非定常不可压流动,分析了运动参数对翼型气动特性的影响,为进一步研究绕三维扑翼的非定常流动打下基础。
The design and fabrication of high efficient biomimetic wings with good dynamic characteristics are the keys of fmav . meanwhile , it ’ s also a very challenging research topic at present 设计和制造具有良好动力学特性的高效仿生翼,是仿生微扑翼飞行器研究中的一个关键环节,同时也是目前非常富有挑战性的研究难题。