HYSTERESIS AND VIBRATION COMPENSATION FOR PIEZOACTUATORS

Authors
Citation
D. Croft et S. Devasia, HYSTERESIS AND VIBRATION COMPENSATION FOR PIEZOACTUATORS, Journal of guidance, control, and dynamics, 21(5), 1998, pp. 710-717
Citations number
29
Categorie Soggetti
Instument & Instrumentation","Aerospace Engineering & Tecnology
ISSN journal
07315090
Volume
21
Issue
5
Year of publication
1998
Pages
710 - 717
Database
ISI
SICI code
0731-5090(1998)21:5<710:HAVCFP>2.0.ZU;2-5
Abstract
Structural vibrations and hysteresis nonlinearities in piezoactuators have been fundamental limitations when using these actuators for high- speed precision-positioning applications. Positioning speed (bandwidth ) is limited by structural vibrations, typically, to about one tenth t he fundamental vibrational frequency of the piezoprobe. Further, preci sion in positioning is limited by hysteresis nonlinearities, which can result in significant errors for large-range positioning applications . This paper shows that significant improvements in precision and band width can be achieved by using an inversion-based approach to compensa te for hysteresis and vibrations in the piezodynamics. The approach de couples the inversion into 1) inversion of the hysteresis nonlinearity and 2) inversion of the structural dynamics, to find an input voltage profile that achieves precision tracking of a desired position trajec tory The approach is applied to a piezoactuator, and experimental resu lts show that an order of magnitude improvement in positioning speed i s achieved, while maintaining precision tracking of the desired positi on trajectory.