DocumentCode
2241859
Title
Attitude stability control of Quad-rotor aerial robot base on controlled Lagrangian method
Author
Xun, Gong ; Dongfu, Xu
Author_Institution
Changchun Institute of Optics, Fine Mechanics and Physics, Chinese Academy of Sciences, Changchun 130033, P.R. China
fYear
2015
fDate
28-30 July 2015
Firstpage
963
Lastpage
966
Abstract
Over the last decade, a kind of Quad-rotor aerial robot, with its characteristics such as simple structure and flexible control, has become the hotspot in the field of small aerial robots research content. In this paper, based on the energy shaping theory, the controlled Lagrangians method will be introduced into the attitude stability control system of Qaud-rotor aerial robot in order to predigest the design procedure and guarantee the exact tracking to the desired angle signals. At finally, the availability of the proposed scheme is verified through numerical simulation with different initial state.
Keywords
Aircraft; Angular velocity; Attitude control; Control systems; DC motors; Stability analysis; Controlled Lagrangians; Energy Shaping; Quad-rotor Robot;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference (CCC), 2015 34th Chinese
Conference_Location
Hangzhou, China
Type
conf
DOI
10.1109/ChiCC.2015.7259764
Filename
7259764
Link To Document