Title :
Modelling and attitude control simulation of Multi-rotor Helicopter
Author :
He Zhi Chao ; You An Hua ; Ma Guo Liang ; Zhang Yong
Author_Institution :
Sch. of Autom., Nanjing Univ. of Sci. & Technol., Nanjing, China
Abstract :
In this paper, a nonlinear dynamic model and multi attitude controllers are developed for Multi-rotor Helicopter. First, different type of Multi-rotor Helicopter and its flight theory is introduced. Secondly, based on the forces and moments on the Multi-rotor Aircraft during its flight, kinematic and dynamic model is founded. Then, the mathematical model is simplified to design attitude controllers. Finally, the model and attitude controllers are established in Simulink, and the controllers are proved to be effective.
Keywords :
aircraft control; attitude control; control system synthesis; helicopters; nonlinear dynamical systems; vehicle dynamics; Simulink; aircraft; attitude control design; flight theory; kinematic model; mathematical model; multirotor helicopter; nonlinear dynamic model; Atmospheric modeling; Attitude control; Educational institutions; Electronic mail; Helicopters; Mathematical model; Xenon; Attitude Control; Dynamical Model; Multi-rotor; Unmanned Aerial Vehicle (UAV);
Conference_Titel :
Control Conference (CCC), 2014 33rd Chinese
Conference_Location :
Nanjing
DOI :
10.1109/ChiCC.2014.6896954
