| KEYWORD |
A study on non-linear effects during sine vibration testing of large deployable reflector antenna
Thesis in external company 
Thesis abroad
keywords AEROSPACE STRUCTURES, NONLINEAR DYNAMICS, SIGNAL PROCESSING, VIBRATIONS
Reference persons DARIO ANASTASIO, STEFANO MARCHESIELLO
Research Groups 06-Dinamica dei Sistemi Meccanici e Identificazione
Thesis type EXPERIMENTAL AND NUMERICAL
Description Deployable reflectors are widely used in satellite structures due to their compact size during launch. The thesis aims to study the dynamic behavior of these systems in their folded condition through experimental tests. Specifically, it is required to study, characterize, and quantify the nonlinear effects during vibration testing using dynamic identification techniques. The partner company is Large Space Structures, based in Munich, Germany. See the attachment for further information.
See also mastersthesis_lss_polito.pdf
Required skills Linear structural dynamics; vibration mechanics
Deadline 31/08/2024
PROPONI LA TUA CANDIDATURA