Title :
Attitude control system design for a quadrotor flying robot
Author :
Lee, Gigun ; Jeong, Dong Yun ; Khoi, Nguyen Dang ; Kang, Taesam
Author_Institution :
Dept. of Aerosp. Inf. Eng., Konkuk Univ., Seoul, South Korea
Abstract :
This study describes the development of an attitude control system for a quadrotor flying robot. In this paper, we introduces the linearized mathematical model from experimental data using system identification method and design of the optimal control. And then we verify the control system through simulation and performing the experimental tests.
Keywords :
aerospace control; attitude control; autonomous aerial vehicles; control system synthesis; identification; linearisation techniques; mobile robots; optimal control; rotors; attitude control system design; linearized mathematical model; optimal control design; quadrotor flying robot; system identification method; unmanned aerial vehicles; Attitude control; Control systems; Data models; Helicopters; Mathematical model; System identification; Attitude Control; Model Identification; Optimal Control; Prediction Error Minimization method(PEM); Quadrotor Flying Robot;
Conference_Titel :
Ubiquitous Robots and Ambient Intelligence (URAI), 2011 8th International Conference on
Conference_Location :
Incheon
Print_ISBN :
978-1-4577-0722-3
DOI :
10.1109/URAI.2011.6145936
