DocumentCode
3724271
Title
Aircraft Autopilot Pitch Control Based on Fuzzy Active Disturbance Rejection Control
Author
Di We;Hejin Xiong;Jian Fu
Author_Institution
Sch. of Autom., Wuhan Univ. of Technol., Wuhan, China
fYear
2015
Firstpage
144
Lastpage
147
Abstract
Considering the high demands of modern flight control system and the existence of various uncertain disturbances in flight, an active disturbance rejection control (ADRC) strategy based on fuzzy control is proposed, so as to realize the high performance of aircraft pitch control. The nonlinear active disturbance rejection controller is designed to improve the ability of anti-interference, meanwhile, fuzzy control is adopted to adjust the ADRC parameters online, which makes control performance better. Simulation results show that compared with conventional PID the Fuzzy-ADRC strategy can suppress the disturbances quickly and efficiently, with higher control accuracy, stronger robustness and so on. The results are of important value for aircraft pitch control in practice.
Keywords
"Aircraft","Aerospace control","Pitch control (position)","Atmospheric modeling","Mathematical model","Fuzzy control"
Publisher
ieee
Conference_Titel
Industrial Informatics - Computing Technology, Intelligent Technology, Industrial Information Integration (ICIICII), 2015 International Conference on
Type
conf
DOI
10.1109/ICIICII.2015.119
Filename
7373807
Link To Document