Abstract
A study of the vibration control of cantilevers exposed to blast pressure signatures is presented. Whereas the structure used in this analysis is in the form of a thin-walled beam of closed cross-section contour, the control is based upon the simultaneous implementation of the adaptive materials technology and the optimal feedback control. Issues related with the influence upon dynamic response of size and location along the beam span of piezoactuator patches are investigated and the efficiency of this combined control methodology is outlined. Other issues related with the minimization of the input power required in the control process, maximization of the sensing voltage output and implications of the limitation of control input voltage on dynamic response are also addressed and pertinent conclusions are outlined.
| Original language | English |
|---|---|
| Title of host publication | Analysis and Design Issues for Modern Aerospace Vehicles |
| Publisher | American Society of Mechanical Engineers (ASME) |
| Pages | 231-248 |
| Number of pages | 18 |
| ISBN (Electronic) | 9780791818350 |
| DOIs | |
| Publication status | Published - 1997 |
| Externally published | Yes |
| Event | ASME 1997 International Mechanical Engineering Congress and Exposition, IMECE 1997 - Analysis and Design Issues for Modern Aerospace Vehicles - Dallas, United States Duration: 1997 Nov 16 → 1997 Nov 21 |
Publication series
| Name | ASME International Mechanical Engineering Congress and Exposition, Proceedings (IMECE) |
|---|---|
| Volume | 1997-I |
Conference
| Conference | ASME 1997 International Mechanical Engineering Congress and Exposition, IMECE 1997 - Analysis and Design Issues for Modern Aerospace Vehicles |
|---|---|
| Country/Territory | United States |
| City | Dallas |
| Period | 97/11/16 → 97/11/21 |
Bibliographical note
Publisher Copyright:© 1997 American Society of Mechanical Engineers (ASME). All rights reserved.
ASJC Scopus subject areas
- Mechanical Engineering