| KEYWORD |
15-Modellazione, simulazione e controllo di velivoli
Theses at Politecnico
ANALYSIS AND DEVELOPMENT OF FORCE CONTROL SYSTEMS FOR AERONAUTICAL ELECTROMECHANICAL ACTUATORS
keywords ACTUATOR, CONTROL SYSTEMS, HAPTIC FUNCTIONALITIES
Reference persons MANUELA BATTIPEDE
Research Groups 15-Modellazione, simulazione e controllo di velivoli
Thesis type THESIS WITH COMPANY STAGE
Description Aim of this thesis is to develop the control laws of an electromechanical actuator for aeronautical applications tasked with providing haptic functionalities.
- Study of the state of the art of haptic technology and its relative control strategies, focusing on the aeronautical field.
- Identification of key performance indicators.
- Development, analysis, and comparative study of a set of suitable control laws.
- Analysis on the integration of the haptic interface and its control system with instrumented aircraft flight controls.
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