DocumentCode
550163
Title
The control method within wind disturbance for MAV based on nonlinear model
Author
Miao Cunxiao ; Fang Jiancheng ; Sun Dingsheng ; Gao Yanhao
Author_Institution
Sch. of Instrum. Sci. & Opto-Electron. Eng., BeiHang Univ., Beijing, China
fYear
2011
fDate
22-24 July 2011
Firstpage
3896
Lastpage
3901
Abstract
To solve the issues of nonlinear model and wind disturbance, it was proposed that the sliding mode control method based on vector field. Firstly, the nonlinear model for MAV(Micro Aerial Vehicle) was constructed. Secondly, the complexity tracking decomposed into straight line and arc segment by the proposed control method, the stable and convergent control law was constructed, and then the simulation experiment shows that MAV can complete the task of tracking in the windy condition through the navigation information. Finally, the proposed control method was compared with the traditional PID controller by flight experiments, and experimental results show that the proposed control method can guarantee the flight path control accuracy in the wind field for MAV.
Keywords
aerospace control; nonlinear control systems; space vehicles; three-term control; variable structure systems; MAV based on nonlinear model; PID controller; arc segment; complexity tracking; convergent control; micro aerial vehicle; navigation information; sliding mode control method; straight line; vector field; wind disturbance; Control systems; Electronic mail; Global Positioning System; Micromechanical devices; Nonlinear dynamical systems; Vehicles; Wind; Micro Aerial Vehicle; Nonlinear dynamics model; Sliding mode; Vector field; Wind disturbance;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference (CCC), 2011 30th Chinese
Conference_Location
Yantai
ISSN
1934-1768
Print_ISBN
978-1-4577-0677-6
Electronic_ISBN
1934-1768
Type
conf
Filename
6000500
Link To Document