摘要
按照飞行器设计的基本原理,完成了某型手掷电动无人机的总体设计,制作了3架采用不同尾翼布局的样机,并对其进行了飞行试验。通过对试验结果的分析可知,不同尾翼型式对高翼台、单尾撑后推式布局的飞机纵向操纵性与稳定性的影响较大。该项研究为此类小型手掷电动无人机的研究提供了参考。
This paper finished the conceptual design of a hand-launched electric-powered unmanned aerial vehicle （UAV） based on its design methodology, and built 3 full-scale prototypes for flight test to examine the flying qualities to research the influence of three different tails on the longitudinal stability-and-control characteristics in order to provide valuable information for designing this type of UAVs.
出处
《飞行力学》
CSCD
北大核心
2010年第2期82-84,88,共4页
Flight Dynamics
关键词
手掷电动无人机
验证试飞
尾容系数
hand-launched electric-powered UAV
validation test flight
tail volume
