DocumentCode :
574496
Title :
A gust-attenuation robust H output-feedback control design for unmanned autonomous helicopters
Author :
Jun Wang ; Hailong Pei ; Weizhou Su ; Yuebang He
Author_Institution :
Coll. of Autom. Sci. & Eng., South China Univ. of Technol., Guangzhou, China
fYear :
2012
fDate :
27-29 June 2012
Firstpage :
3260
Lastpage :
3265
Abstract :
This paper presents a hierarchical inner-outer loop-based approach to the longitudinal and lateral control of a small unmanned helicopter in the presence of parameter uncertainties and exogenous disturbances. The outer loop employs robust H output feedback to attenuate the wind disturbance and track the reference trajectory, while the inner loop controller is proposed to solve the parameter uncertainties problems using robust H static output feedback. The obtained control method takes advantage of the feature of hierarchical structure ensuring the stability of the flight attitude. Finally, the validity of the proposed control strategy is verified through simulation results.
Keywords :
H control; attitude control; autonomous aerial vehicles; control system synthesis; feedback; helicopters; robust control; control strategy; exogenous disturbances; flight attitude stability; gust-attenuation robust H∞ output-feedback control design; hierarchical inner-outer loop-based approach; hierarchical structure; inner loop controller; lateral control; longitudinal control; parameter uncertainties problems; reference trajectory; robust H∞ output feedback; robust H∞ static output feedback; small unmanned helicopter; unmanned autonomous helicopters; wind disturbance; Aerodynamics; Helicopters; Mathematical model; Output feedback; Robustness; Rotors; Vectors;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference (ACC), 2012
Conference_Location :
Montreal, QC
ISSN :
0743-1619
Print_ISBN :
978-1-4577-1095-7
Electronic_ISBN :
0743-1619
Type :
conf
DOI :
10.1109/ACC.2012.6315081
Filename :
6315081
Link To Document :
بازگشت