DocumentCode :
3177482
Title :
The Furuta´s pendulum stabilization without the use of a mathematical model: Attractive Ellipsoid Method with KL-adaptation
Author :
Ordaz, Patricio ; Poznyak, Alexander
Author_Institution :
Centro de Investig. y Estud. Av. Del Inst., Politec. Nac. (CINVESTAV-IPN), Mexico City, Mexico
fYear :
2012
fDate :
10-13 Dec. 2012
Firstpage :
7285
Lastpage :
7290
Abstract :
This paper presents a development of adaptive state estimator and output controller based on Attractive Ellipsoid Method (AEM) for the stabilization of the Furuta´s pendulum. The proposed method guaranties that the controlled system trajectories are stabilized within an ellipsoid of a “minimal size”. We expand the classical AEM without adaptation to a class of observer and controller compensator with time varying gain matrices K and L adjusted on-line by specific adaptation procedure, that guaranties the convergence of the trajectories to an ellipsoid of less size compared to one without adaptation. In the case of the considered pendulum the incorporated adaptation procedures provides a stabilization in the vertical position practically with negligible vibrations, or in other words, without any “chattering effect”.
Keywords :
convergence; mathematical analysis; matrix algebra; observers; pendulums; stability; time-varying systems; trajectory control; vibrations; AEM; Furuta pendulum stabilization; KL-adaptation; adaptation procedure; adaptive state estimator; attractive ellipsoid method; controlled system trajectories; controller compensator; incorporated adaptation procedures; mathematical model; observers; output controller; time varying gain matrices; Adaptive systems; Ellipsoids; Mathematical model; Observers; Optimization; 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.2012.6426722
Filename :
6426722
Link To Document :
بازگشت