Dynamic Modeling and Flight Simulation of a Folding Wing-Tip UAV
作者单位：Department of Automation EngineeringNanjing University of Aeronautics and Astronautics Jiangsu Key Laboratory of Internet of Things and Control Technologies
会议名称：《第32届中国控制与决策会议》
会议日期：2020年
学科分类：08[工学] 080203[工学-机械设计及理论] 082503[工学-航空宇航制造工程] 0802[工学-机械工程] 0825[工学-航空宇航科学与技术]
关 键 词：Morphing Aircraft Aerodynamic Modeling Missile DATCOM
摘 要：In this paper,a novel modeling method and the aerodynamic analysis of folding wing-tip UAVs are *** folding wing-tip UAV models are established by treating the aircraft as a single body but relaxing the condition of *** a typical kind of folding wing-tip UAVs,NASA spanwise adaptive wing morphing UAV（SAW） is modeled and analyzed in this *** missile datcom is also applied to analyze the aerodynamic performance during the folding process of wing-tip by establishing the 3 D model of the SAW and conducting numeric simulations.