Applied aerospace systems and control research
Rotorcraft and tiltrotor attitude control
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.
Path planning, collision avoidance and path following for UAV formations
