Title :
Active disturbance rejection control for the yaw tracking for unmanned helicopter
Author_Institution :
Key Lab. of Syst. & Control, Beijing, China
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;
Conference_Titel :
Intelligent Control and Automation (WCICA), 2012 10th World Congress on
Conference_Location :
Beijing
Print_ISBN :
978-1-4673-1397-1
DOI :
10.1109/WCICA.2012.6358189