DocumentCode
234292
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
fYear
2014
fDate
28-30 July 2014
Firstpage
2095
Lastpage
2100
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);
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference (CCC), 2014 33rd Chinese
Conference_Location
Nanjing
Type
conf
DOI
10.1109/ChiCC.2014.6896954
Filename
6896954
Link To Document