Dynamic analysis of a ducted fan UAV in forward flight

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.

关键词： ducted fan UAV aerodynamic characteristics dynamic model

作者: Zhang Wei Fan Ningjun

作者单位: School of Mechatronical Engineering, Beijing Institute of Technology, Beijing 100081, China

会议类型: 国际会议

会议名称: 2012 International Conference on Industiial Design and Mechanical Power(2012工业设计与机械动力国际会议 ICIDMP 2012)

会议地点: 黄山

会议语种:英文

页码: 510-513

在线出版日期: 2012-07-10（万方平台首次上网日期，不代表论文的发表时间）