DocumentCode
577727
Title
Active disturbance rejection control for the yaw tracking for unmanned helicopter
Author
Jiang, Zhe
Author_Institution
Key Lab. of Syst. & Control, Beijing, China
fYear
2012
fDate
6-8 July 2012
Firstpage
1915
Lastpage
1919
Abstract
The yaw dynamics of helicopter involve input nonlinearity, time-varying parameters and the couplings between main and tail rotor. With respect to such a complicated dynamics, the normal control is difficult to realize good tracking performance while maintaining stability and robustness simultaneously. In this paper, an active disturbance rejection control(ADRC) method is proposed. we design an extended state observer (ESO) to estimate the impact from parametric uncertainties and disturbances, and realize online compensations. Time-varying parameters and other uncertainties in the helicopter dynamics can be rejected by active disturbance rejection control to achieve small tracking error. The simulations results with respect to the dynamics identified from a real helicopter-on-arm testbed are presented. The simulation results are further demonstrated the improvements of the proposed algorithm under the time-varying parameters and other uncertainties.
Keywords
autonomous aerial vehicles; compensation; helicopters; nonlinear control systems; observers; robust control; time-varying systems; uncertain systems; ADRC; ESO; active disturbance rejection control; extended state observer; helicopter dynamics; helicopter-on-arm testbed; nonlinearity; online compensation; parametric disturbance; parametric uncertainty; robustness; stability; time-varying parameter; unmanned helicopter; yaw tracking; Aerodynamics; Educational institutions; Helicopters; Simulation; Uncertainty; Vehicle dynamics; Active disturbance rejection control; Input nonlinearity; Yaw control;
fLanguage
English
Publisher
ieee
Conference_Titel
Intelligent Control and Automation (WCICA), 2012 10th World Congress on
Conference_Location
Beijing
Print_ISBN
978-1-4673-1397-1
Type
conf
DOI
10.1109/WCICA.2012.6358189
Filename
6358189
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