| KEYWORD |
ANALYSIS AND DEVELOPMENT OF CONTROL SYSTEMS FOR AERONAUTICAL REDUNDANT ELECTROMECHANICAL ACTUATORS
keywords ACTUATOR, CONTROL SYSTEMS
Reference persons MANUELA BATTIPEDE
Research Groups 15-Modellazione, simulazione e controllo di velivoli
Description 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.
Notes Tesi retribuita da svolgere con presenza full time in Mecaer Aviation group
Deadline 24/10/2024
PROPONI LA TUA CANDIDATURA