Title :
Adaptive Trajectory Linearization Control for a model-scaled helicopter with uncertain inertial parameters
Author :
Bing, Zhu ; Wei, Huo
Author_Institution :
Seventh Res. Div., Beihang Univ., Beijing, China
Abstract :
An adaptive approach based on Trajectory Linearization Control (TLC) is introduced to achieve the trajectory tracking of model-scaled helicopter with constant or slow time-varying model uncertainties. In the procedure of the controller designing, estimated parameters are applied to compensate for the uncertain inertial parameters (such as the mass and the inertial matrix) of the helicopter. Stability of the adaptive control system is proved in both constant and time-varying cases. Performances of the closed-loop system are verified by simulation results.
Keywords :
adaptive control; aircraft control; closed loop systems; control system synthesis; helicopters; linearisation techniques; stability; time-varying systems; trajectory control; uncertain systems; adaptive trajectory linearization control; closed loop system; controller design; model scaled helicopter; stability; time-varying model uncertainty; trajectory tracking; uncertain inertial parameter estimation; Adaptation models; Attitude control; Helicopters; Mathematical model; Rotors; Trajectory; Uncertainty; Trajectory linearization control; adaptive control; helicopter control; nonlinear control;
Conference_Titel :
Control Conference (CCC), 2012 31st Chinese
Conference_Location :
Hefei
Print_ISBN :
978-1-4673-2581-3