DocumentCode
176874
Title
Attitude control of coaxial tri-rotor UAV based on Linear Extended State Observer
Author
Zhimin Chen ; Zhihong Peng ; Fan Zhang
Author_Institution
Sch. of Autom., Beijing Inst. of Technol., Beijing, China
fYear
2014
fDate
May 31 2014-June 2 2014
Firstpage
4204
Lastpage
4209
Abstract
A novel dynamic decoupling control method based on Linear Extended State Observer(LESO) for attitude stabilization of coaxial tri-rotor UAV is presented. Coaxial tri-rotor UAV system is a strong coupling, susceptible to disturbance, and multi-input multi-output (MIMO) system. High performance stabilization of such UAV is effected by virous uncertainties and disturbances which are difficult to measure. For this reason, we adopt Active Disturbance Rejection Control (ADRC) based on (LESO) and a linear feedback control law to estimate the dynamic disturbances and reject them out in real time to achieve desirable flight performance. The high performance of low overshoot, high accuracy, and strong robustness are demonstrated by the simulation results.
Keywords
MIMO systems; aircraft control; attitude control; autonomous aerial vehicles; feedback; helicopters; linear systems; observers; stability; ADRC; LESO; MIMO system; active disturbance rejection control; attitude control; attitude stabilization; coaxial trirotor UAV system; dynamic decoupling control method; dynamic disturbance estimation; flight performance; high performance stabilization; linear extended state observer; linear feedback control law; multiinput multioutput system; Aircraft; Attitude control; Couplings; Dynamics; Equations; Mathematical model; Rotors; LESO; PD controller; attitude stabilization; coaxial tri-rotor UAV; dynamic decoupling;
fLanguage
English
Publisher
ieee
Conference_Titel
Control and Decision Conference (2014 CCDC), The 26th Chinese
Conference_Location
Changsha
Print_ISBN
978-1-4799-3707-3
Type
conf
DOI
10.1109/CCDC.2014.6852918
Filename
6852918
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