Optimal vibration control by the use of piezoceramic sensors and actuators
- 1 September 1992
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 15 (5) , 1199-1206
- https://doi.org/10.2514/3.20969
Abstract
No abstract availableKeywords
This publication has 14 references indexed in Scilit:
- Distributed piezoelectric-polymer active vibration control of a cantilever beamJournal of Guidance, Control, and Dynamics, 1985
- Modal-space active damping of a plane grid - Experiment and theoryJournal of Guidance, Control, and Dynamics, 1985
- On the Number and Placement of Actuators for Independent Modal Space ControlJournal of Guidance, Control, and Dynamics, 1984
- Electronic damping of orthogonal bending modes in a cylindrical mast - ExperimentJournal of Spacecraft and Rockets, 1981
- Optimal controller placement in modal control of complex systemsJournal of Mathematical Analysis and Applications, 1980
- Electronic damping of vibrations in optical structuresApplied Optics, 1979
- Basic relations for control of flexible vehiclesAIAA Journal, 1970
- Finite Element Analysis of Flexure-Type Vibrators with Electrostrictive TransducersIEEE Transactions on Sonics and Ultrasonics, 1970
- Linear Piezoelectric Plate VibrationsPublished by Springer Nature ,1969
- Electronic Control of Noise, Vibration, and ReverberationThe Journal of the Acoustical Society of America, 1956