Dynamic analysis of a ducted fan UAV in forward flight

被引：1
|
作者：
Zhang Wei [1 ]
Fan Ningjun [1 ]
机构：
[1] Beijing Inst Technol, Sch Mechatron Engn, Beijing 100081, Peoples R China
来源：
INDUSTRIAL DESIGN AND MECHANICAL POWER | 2012年 / 224卷
关键词：
ducted fan UAV; aerodynamic characteristics; dynamic model;
D O I：
10.4028/www.scientific.net/AMM.224.510
中图分类号：
T [工业技术];
学科分类号：
08 ;
摘要：
This paper deals with the dynamic modeling of a ducted fan vertical takeoff and landing (VTOL) unmanned aerial vehicle (UAV) and focuses on the dynamic characteristics analyzing in forward flight. A 6-DOF nonlinear model has been established in terms of the forces and moments and the model can be used in the structure and control system design.
引用
收藏
页码：510 / 513
页数：4
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