Applied aerospace systems and control research

Rotorcraft and tiltrotor attitude control:

Rotorcraft and tiltrotor1Rotorcraft and tiltrotor2

Helicopter vibration and noise – identification and control:

Reduction of main rotor vibration using robust harmonic control at blade-passing frequency


Identification and control for multi-rotor UAVs:

Model identification using both continuous and discrete time methods;
Control tuning based on robust methods.

control tuning

multi rotor UAVs

Path planning, collision avoidance and path following for UAV formations:

planning collision

Designed by sofos LAB srl