flying-wing uav

基本解釋

Then the math model is built using flight dynamics theory and the flight quality of flying-wing UAV is analyzed.
然后利用飛行力學(xué)理論建立了飛翼無(wú)人機(jī)運(yùn)動(dòng)的數(shù)學(xué)模型，分析了飛翼無(wú)人機(jī)的飛行品質(zhì)特性；
So many countries focus on the development of HALE UAV. Flying-wing HALE UAV has high ratio of lift and drag and low level of detective.
飛翼式高空長(zhǎng)航時(shí)無(wú)人偵察機(jī)在具有高升阻比、低可探測(cè)性等優(yōu)勢(shì)的同時(shí)，具有裝載特性好等諸多獨(dú)特的技術(shù)優(yōu)勢(shì)，使其成為研究的焦點(diǎn)。
Finally, main methods and characteristics of flying-wing UAV's control system design are analyzed based on nonlinear simulation results and some advice for improvement is presented.
最后，根據(jù)仿真結(jié)果分析總結(jié)了飛翼布局無(wú)人機(jī)的控制系統(tǒng)設(shè)計(jì)方法和設(shè)計(jì)特點(diǎn)，并提出一些具體的建議，為飛翼無(wú)人機(jī)總體設(shè)計(jì)提供了一定的依據(jù)。