DocumentCode
3169978
Title
A robust controller based on adaptive super-twisting algorithm for a 3DOF helicopter
Author
Plestan, F. ; Chriette, A.
Author_Institution
Ecole Centrale de Nantes, LUNAM Univ., Nantes, France
fYear
2012
fDate
10-13 Dec. 2012
Firstpage
7095
Lastpage
7100
Abstract
This paper presents a new controller for a 3D helicopter. The main novelty of this controller is the use of adaptive super-twisting algorithm for the control of each attitude angle. This controller is a second order sliding mode controller, which is robust versus uncertainties and perturbations, ensures finite time convergence, reduces the chattering, increases the accuracy and does not require time derivative of the sliding variable. A very important point comes from its adaptive gain, which allows to design the controller with very reduced knowledge on uncertainties and perturbations. This controller is applied on the three attitude angles of a 3D helicopter, this fact being validated by simulations and experimental results.
Keywords
adaptive control; aircraft control; helicopters; robust control; variable structure systems; 3D helicopter; 3DOF helicopter; adaptive gain; adaptive super-twisting algorithm; attitude angle; controller design; finite time convergence; perturbation robustness; robust controller; second order sliding mode controller; time derivative; uncertainty robustness; Adaptation models; Attitude control; Dynamics; Helicopters; Mathematical model; Robustness; Trajectory;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control (CDC), 2012 IEEE 51st Annual Conference on
Conference_Location
Maui, HI
ISSN
0743-1546
Print_ISBN
978-1-4673-2065-8
Electronic_ISBN
0743-1546
Type
conf
DOI
10.1109/CDC.2012.6426337
Filename
6426337
Link To Document