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

fYear

2011

fDate

23-26 Nov. 2011

Firstpage

74

Lastpage

78

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;

fLanguage

English

Publisher

ieee

Conference_Titel

Ubiquitous Robots and Ambient Intelligence (URAI), 2011 8th International Conference on

Conference_Location

Incheon

Print_ISBN

978-1-4577-0722-3

Type

conf

DOI

10.1109/URAI.2011.6145936

Filename

6145936