KEYWORD |
nonlinear system identification of an aircraft structure
Thesis abroad
keywords DAMAGE DETECTION, MODAL ANALYSIS, STRUCTURAL DYNAMICS, STRUCTURAL HEALTH MONITORING, VIBRATION DIAGNOSTICS
Reference persons MARCO CIVERA
External reference persons Prof Gabriele Dessena, Universidad Carlos III de Madrid, Spain
Thesis type EXPERIMENTAL, NUMERICAL
Description The aim of this thesis is the identification of non-linear dynamics from experimental data collected with an odd random phase multisine (ORPM) excitation technique of a military fighter aircraft.
Required skills Good basics of MATLAB and/or basics of Python (the student will be supported in further developing his/her coding skill during the project)
Notes Required grade average: >=27/30 (qualifying interview with the Spanish supervisor also required); knowledge of English at B2 level (minimum)
Deadline 02/01/2026
PROPONI LA TUA CANDIDATURA