Design and development of innovative monitoring logics for the flap actuation system.
Thesis type NUMERICO-SPERIMENTALE
Description Development of new diagnostic monitoring logics of the flap actuation system and evaluating their performance in flap asymmetry. Comparison between different solutions and evaluation of their behaviors. Study of their interactions with other failures/disturbances (e.g. friction and backlash on the final actuators, supply pressure transitory, servovalve failures).
See also aescte2468.pdf
Required skills Modellazione di servomeccanismi aeronautici, postprocessing di dati in ambiente Matlab, Conoscenza di base del linguaggio di programmazione FORTRAN
Notes La tesi verrą redatta preferenzialmente in lingua inglese.
Deadline 13/03/2024 PROPONI LA TUA CANDIDATURA