Attitude control system design for a quadrotor flying robot

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 s...

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Bibliographic Details
Published in2011 8th International Conference on Ubiquitous Robots and Ambient Intelligence (URAI) pp. 74 - 78
Main Authors Gigun Lee, Dong Yun Jeong, Nguyen Dang Khoi, Taesam Kang
Format Conference Proceeding
LanguageEnglish
Published IEEE 01.11.2011
Subjects
Attitude control
Control systems
Data models
Helicopters
Mathematical model
Model Identification
Optimal Control
Prediction Error Minimization method(PEM)
Quadrotor Flying Robot
System identification
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Summary: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.
ISBN:9781457707223
1457707225
DOI:10.1109/URAI.2011.6145936