Master Thesis (d/m/w) zum Thema: Design Studie eines Präzisionsinstruments für Helikopter Flugsteuerung Kräfte
Core
Design study and development of a precision instrument for measuring helicopter flight control forces to improve measurement accuracy of pilot steering forces.
Role type
Master thesis student (mechatronics/electrical engineering)
Builds
Prototype electromechanical actuator system for force measurement
Domain
Aerospace / Helicopter Flight Control Systems
Required skills
electromechanical actuator design, control theory, Matlab/Simulink modeling, analytical calculations, predictive simulation, component selection, stability analysis, feedback loop optimization
Preferred skills
mechatronic systems understanding, motor/sensor/gearbox knowledge, power electronics
Technologies
Matlab, Simulink
Responsibilities
Conceptualize electromechanical actuator for precision force measurement, model actuator system, perform pre-dimensioning via analytical calculations and simulation, select industrial standard components, simulate system including controller design and stability analysis
Seniority
Student, Master thesis