Flexibility of flapping wing and its effect on aerodynamic characteristic 撲翼柔性及其對(duì)氣動(dòng)特性的影響
Attitude tracking control for flapping wing micro aerial vehicle based on feedback compensation 基于反饋補(bǔ)償?shù)膿湟砦⑿惋w行器姿態(tài)跟蹤控制
In fine , as long as effort will include results , as long as pay will have repay , as long as give me a terrace for displaying , i can flap wings to rise high fly 總之,只要努力就會(huì)有收獲,只要付出就會(huì)有回報(bào),只要給我一個(gè)施展的平臺(tái),我就能振翅高飛!
2 . the 3 - d unsteady euler equations are derived . and the computational program based on these equations is developed to adapt for the calculations of flapping wing 2 、推導(dǎo)了非定常情況下的三維歐拉方程,發(fā)展了三維非定常歐拉方程計(jì)算程序,使之適應(yīng)于撲動(dòng)翼計(jì)算的需要。
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 運(yùn)用本文可以計(jì)算撲翼的氣動(dòng)特性及分析各參數(shù)對(duì)撲翼氣動(dòng)特性的影響,進(jìn)而指導(dǎo)撲動(dòng)翼微型飛機(jī)的初期設(shè)計(jì)。