ROBUST IDENTIFICATION AND VIBRATION SUPPRESSION OF A FLEXIBLE STRUCTURE

Citation
Jl. Crassidis et al., ROBUST IDENTIFICATION AND VIBRATION SUPPRESSION OF A FLEXIBLE STRUCTURE, Journal of guidance, control, and dynamics, 17(5), 1994, pp. 921-928
Citations number
25
Categorie Soggetti
Instument & Instrumentation","Aerospace Engineering & Tecnology
ISSN journal
07315090
Volume
17
Issue
5
Year of publication
1994
Pages
921 - 928
Database
ISI
SICI code
0731-5090(1994)17:5<921:RIAVSO>2.0.ZU;2-2
Abstract
A robust vibration suppression design involving the use of H-infinity optimal control theory is studied for a complex flexible structure. Th e digital control architecture involves noncollocated feedback utilizi ng active piezoceramic actuators and position sensor data. The modal p roperties of the multi-input, multi-output structure are first determi ned from experimental data in order to obtain an identified state-spac e model. This model forms the basis for the H-infinity vibration suppr ession design. Performance specifications are developed that obtain ad equate damping in the structure while maintaining controller integrity without the destabilization of higher modes. A controller optimized f or these H-infinity performance specifications is implemented on the a ctual test structure. Experimental structural perturbations are also e xamined in order to determine the robustness of the vibration suppress ion design. The experimental study indicates that the H-infinity desig n substantially increases damping in the targeted frequency region and conforms to predicted analytical simulations.