High-fidelity modeling and performance analysis of electro-hydraulic flight control actuators in presence of degradations within the spherical rod-ends.
Research Groups 14-Meccatronica e servosistemi
Thesis type MODELING AND DATA ANALYSIS
Description The student will be tasked to model the dynamic behavior of an electro-hydraulic flight control actuatos for wide-body aircrafts to evaluate its performances in degraded health conditions.
The student will also be responsible of the analysis of the simulated data and will work to design novel diagnostic/prognostic algorithms.
Deadline 04/02/2023 PROPONI LA TUA CANDIDATURA