flexibility of flapping wing and its effect on aerodynamic characteristic 撲翼柔性及其對氣動特性的影響
attitude tracking control for flapping wing micro aerial vehicle based on feedback compensation 基于反饋補償?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,只要努力就會有收獲,只要付出就會有回報,只要給我一個施展的平臺,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算程序,使之適應于撲動翼計算的需要。
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 運用本文可以計算撲翼的氣動特性及分析各參數(shù)對撲翼氣動特性的影響,進而指導撲動翼微型飛機的初期設計。