The focuses of this paper are on flight environment simulation and high span - chord ratio uav model 本文的工作就是圍繞飛行環(huán)境模擬和無人機(jī)動力學(xué)仿真展開。
For the first time , flight simulation related to high span - chord ratio uav based on variable windfield is executed , the facticity of windfield and its influence to flight performance curve are analyzed . 5 首次針對大展弦比無人機(jī),進(jìn)行變化風(fēng)場中飛行仿真,討論各風(fēng)場模型的真實性及其對飛行性能曲線的影響; 5