Title :
Fuzzy global sliding mode control for flexible manipulators
Author :
LI, Ming-ming ; Fang, Bo ; Huang, Wen-hu
Author_Institution :
Sch. of Astronaut., Harbin Inst. of Technol., Harbin, China
Abstract :
This paper deals with vibration reduction of the flexible manipulators bonded with piezoelectric patch actuator. The flexible manipulators´ dynamic model is established using the theory of Euler-beam. This flexible structure has nonlinear characteristics and must be robust to uncertainties as well as disturbances, so a novel advanced control methodology called fuzzy global sliding mode control (FGSMC) is utilized to reduce the vibration. In this controller, global sliding mode factor is introduced in the design of switching function to make system have global robustness, and fuzzy logic control is employed to estimate the switching gain of control law so as to alleviate the chattering. An experiment for active vibration control of flexible manipulators is performed with the aid of dSPACE Real-Time Simulation System. The experimental results show that FGSMC reduce vibration of the flexible manipulators effectively, even though an inexact model is used to design the controller.
Keywords :
flexible manipulators; fuzzy control; manipulator dynamics; nonlinear control systems; variable structure systems; vibration control; Euler-beam theory; FGSMC; active vibration control; dSPACE; dynamic model; flexible manipulator; fuzzy global sliding mode control; fuzzy logic control; global sliding mode factor; nonlinear characteristic; piezoelectric patch actuator; switching function; vibration reduction; Manipulator dynamics; Mathematical model; Robustness; Switches; Vibrations;
Conference_Titel :
Systems and Control in Aeronautics and Astronautics (ISSCAA), 2010 3rd International Symposium on
Conference_Location :
Harbin
Print_ISBN :
978-1-4244-6043-4
Electronic_ISBN :
978-1-4244-7505-6
DOI :
10.1109/ISSCAA.2010.5633093