| KEYWORD |
15-Modellazione, simulazione e controllo di velivoli
ANALYSIS AND DEVELOPMENT OF CONTROL SYSTEMS FOR AERONAUTICAL REDUNDANT ELECTROMECHANICAL ACTUATORS
Parole chiave ACTUATOR, CONTROL SYSTEMS
Riferimenti MANUELA BATTIPEDE
Gruppi di ricerca 15-Modellazione, simulazione e controllo di velivoli
Descrizione Aim of this thesis is to develop the control laws of a redundant electromechanical actuator for aeronautical applications.
- Study of the state of the art of redundant electromechanical actuation systems and their relative control strategies.
- Identification of key performance indicators depending on the task of the redundant actuator within an aircraft flight control system.
- Development, analysis, and comparative study of a set of suitable control laws.
The thesis is carried out in cooperation with an experienced development team.
Note Tesi retribuita da svolgere con presenza full time in Mecaer Aviation group
Scadenza validita proposta 24/10/2024
PROPONI LA TUA CANDIDATURA