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Archivio digitale delle tesi discusse presso l’Università di Pisa

Tesi etd-09142025-211608


Tipo di tesi
Tesi di laurea magistrale
Autore
AUGELLO, MARIA ESTER
URN
etd-09142025-211608
Titolo
Experimental Design, System Architecture and Test Campaign Evaluation of Direct and Indirect Haptic Aids for Pilot Performance on a 3DOF Sidestick
Dipartimento
INGEGNERIA DELL'INFORMAZIONE
Corso di studi
INGEGNERIA ROBOTICA E DELL'AUTOMAZIONE
Relatori
relatore Prof. Pollini, Lorenzo
Parole chiave
  • Control loading device
  • Direct Haptic Aiding
  • Flight Simulation
  • Guidance Algorthm
  • Haptic Aids
  • Human Factors
  • Human–Automation Interaction
  • Indirect Haptic Aiding
  • Level of Automation
  • Naive Pilots
  • Pilot Performance
  • real-time mission feedback
  • Trajectory Tracking
Data inizio appello
29/09/2025
Consultabilità
Non consultabile
Data di rilascio
29/09/2095
Riassunto
Literature highlights issues in human–automation interaction, stressing the need for continuous communication and preserved pilot authority, with the Level of Automation (LoA) requiring solutions that provide support while maintaining pilot engagement. This thesis investigates the use of haptic assistance systems to support pilots in trajectory tracking tasks within a simulated flight environment. A dedicated system architecture was developed, integrating a haptic joystick, CAN communication, a C++/Simulink framework for real-time error computation and the Aerofly FS2 simulator with a custom 40-gate trajectory. Key features of the proposed controllers include real-time mission feedback and a system identification method to model the dynamics of the aircraft and the joystick. Two control strategies were investigated: Direct Haptic Aiding (DHA), which actively guides the control stick towards corrective actions, and Indirect Haptic Aiding (IHA), which emulates the tactile response of conventional aircraft controls without imposing direct commands. A custom algorithm computes real-time deviations from the predefined path, providing cues for pitch and roll correction. A progressive experimental campaign was designed, starting with exploratory sessions and culminating in a between-subjects study with 40 novice pilots. Performance was evaluated through objective metrics and subjective feedback, including the effect of aid intensity.
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