A study on control method of new type UAV

作     者：Kenji Nishigaki Kohei Kawakami Shin- Ichiro Nishida Masaharu Nishimura Kazunori Sakurama Kenji Nishigaki;Kohei Kawakami;Shin-Ichiro Nishida;Masaharu Nishimura;Kazunori Sakurama

作者机构：Department of Mechanical and Aerospace Engineering Tottori University 4 -101 Koyama- M inami Tottori 680 -8552 Japan 

出 版 物：《材料与冶金学报》 (Journal of Materials and Metallurgy)

年 卷 期：2015年第14卷第2期

页      面：149-151,158页

学科分类：08[工学] 080203[工学-机械设计及理论] 0802[工学-机械工程] 

主　　题：stator wing UAV anti-torque control simulator 

摘      要：In late years the use of UAV which is suitable for the observation activities in a dangerous area is pushed forw ard.R otary wing type UAV which can perform vertical takeoff and landing and hovering is used. We propose a compact U AV called SW U M which is without tail rotor. We adopt stator wing as an anti- torque compensation mechanism instead of a tail ***,the attitude control test around yaw axis was performed using the SW UM prototype on a free rotational table. It was confirmed that the attitude of the vehicle around yaw axis by stator wings was controlled well. We studied a control method for translational motion of this vehicle. The horizontal translational motion will be achieved by tilting the body fone of stator *** created the mathematical model of the kinetics of this vehicle,and are performed analysis by the computer simulation.