DocumentCode
3501411
Title
An active wind gust rejection controller for an autonomous helicopter
Author
Zhang Haoyu ; Huang Jun ; Meng Zhijun ; Xu Wei
Author_Institution
Sch. of Aeronaut. Sci. & Eng., Beihang Univ., Beijing, China
Volume
01
fYear
2013
fDate
16-18 Aug. 2013
Firstpage
742
Lastpage
746
Abstract
This paper proposes a novel wind gust rejection controller for a model helicopter with uncertain parameters. A hybrid of backstepping and active disturbance rejection controller is designed to achieve attitude tracking. The analysis and inclusion of the nature of wind gust disturbances and rotor dynamics yield more practical and reliable disturbance observation. The disturbances are eliminated to the best extent due to real time estimation and compensation, and the robustness against model uncertainties is guaranteed through proper state transformation. The simulation results validate the performance and robustness of proposed controller.
Keywords
aerodynamics; aircraft control; attitude control; autonomous aerial vehicles; control nonlinearities; control system synthesis; helicopters; robust control; wind; active wind gust rejection controller; attitude tracking; autonomous helicopter; compensation; controller performance; controller robustness; hybrid backstepping-active disturbance rejection controller design; model helicopter; model uncertainties; real time estimation; rotor dynamics; state transformation; uncertain parameters; wind gust disturbances; Computational modeling; Noise; Observers; Robustness; TV; active disturbance rejection control; backstepping control; robustness; rotor dynamics; wind gust disturbances;
fLanguage
English
Publisher
ieee
Conference_Titel
Measurement, Information and Control (ICMIC), 2013 International Conference on
Conference_Location
Harbin
Print_ISBN
978-1-4799-1390-9
Type
conf
DOI
10.1109/MIC.2013.6758067
Filename
6758067
Link To Document