DocumentCode
582306
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
fYear
2012
fDate
25-27 July 2012
Firstpage
4389
Lastpage
4395
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;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference (CCC), 2012 31st Chinese
Conference_Location
Hefei
ISSN
1934-1768
Print_ISBN
978-1-4673-2581-3
Type
conf
Filename
6390697
Link To Document