DocumentCode :
3178415
Title :
Modelling and control of oblique cross quadrotors vehicle
Author :
Hao, Wang ; Xiaoxing, Fang ; Zhihao, Cai ; Yingxun, Wang
Author_Institution :
Sch. of Autom. Sci. & Electr. Eng., Beihang Univ., Beijing, China
fYear :
2011
fDate :
8-10 Aug. 2011
Firstpage :
3113
Lastpage :
3117
Abstract :
Oblique cross quadrotors vehicle is a variant of quadrotors, which is more suitable for take photos in the air compared to the conventional cross-shaped quadrotors and the rotary-wing state of Quad Tilt Rotor(QTR) have to take this flight mode. A lot of research work have done about the conventional cross-shaped quadrotors but little about oblique cross quadrotors vehicle. The mathematics model of the oblique cross quadrotors vehicle was built up according Newton-Euler formalism and an experimental identification of dynamic parameters is presented. After that, PD was applied to design the control laws. The simulation results demonstrate that the designed control laws can accurately track the given trajectory and have a good performance.
Keywords :
aircraft control; helicopters; rotors; Newton-Euler formalism; control law design; dynamic parameter identification; flight mode; mathematics model; oblique cross-shaped quadrotor vehicle control; oblique cross-shaped quadrotor vehicle modelling; quad tilt rotor; rotary-wing state; Atmospheric modeling; Helicopters; MATLAB; Mathematical model; Rotors; Stability analysis; Vehicles; PD; identification; model; oblique cross; quadrotors;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Artificial Intelligence, Management Science and Electronic Commerce (AIMSEC), 2011 2nd International Conference on
Conference_Location :
Deng Leng
Print_ISBN :
978-1-4577-0535-9
Type :
conf
DOI :
10.1109/AIMSEC.2011.6010829
Filename :
6010829
Link To Document :
بازگشت