DocumentCode
2777741
Title
Experimental study of active vibration control for flexible beam by using a Stewart platform manipulator
Author
Luo, Bo ; Li, Weipeng ; Huang, Hai
Author_Institution
Sch. of Astronaut., Beihang Univ., Beijing, China
fYear
2011
fDate
7-10 Aug. 2011
Firstpage
1465
Lastpage
1470
Abstract
Experiments of active vibration control for flexible beam are studied, with a Stewart platform manipulator (SPM) employed as an active equipment at the bottom of the beam. The dynamic modal of the rigid-flexible coupling system composed of the upper platform of the SPM and the flexible beam is built, and an auto disturbances rejection controller (ADRC) is designed. Then based on the dSPACE real-time simulation system, the control test system for the beam is built, on which the auto disturbances rejection control experiments are carried out. Experimental results show the rate of amplitude attenuation using ADRC is almost 10 times faster than the free attenuation. For comparison purpose, a classic LQG controller is applied in another experiment on the same test system. The results of the two experiments show that ADRC has a better performance than LQG controller for the nonlinear system. At the same time, the results verify the effectiveness of the control conducted by SPM at the bottom of the beam.
Keywords
beams (structures); flexible structures; linear quadratic Gaussian control; manipulators; nonlinear control systems; shear modulus; vibration control; ADRC; LQG controller; active vibration control; amplitude attenuation; auto disturbances rejection control; dSPACE real-time simulation system; flexible beam; nonlinear system; platform manipulator; rigid flexible coupling system; Attenuation; Damping; Manipulators; Real time systems; Space vehicles; Vibration control; Vibrations; ADRC; flexible beam; nonlinear system; vibration control;
fLanguage
English
Publisher
ieee
Conference_Titel
Mechatronics and Automation (ICMA), 2011 International Conference on
Conference_Location
Beijing
ISSN
2152-7431
Print_ISBN
978-1-4244-8113-2
Type
conf
DOI
10.1109/ICMA.2011.5985966
Filename
5985966
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