Design of an electrically powered dual motor Tilt-Wing UAV to investigate and develop an automated stability system for pitch and roll control in takeoff, hover and landing flight modes/
Rudolph, Devan Jessie Aaron.
Design of an electrically powered dual motor Tilt-Wing UAV to investigate and develop an automated stability system for pitch and roll control in takeoff, hover and landing flight modes/ Devan Jessie Aaron Rudolph; Prof. Dr. Suleyman Tolun. - Kyrenia: University of Kyrenia, 2023. - 83 p.: fig.; 30 cm.
Master (Thesis).
Uncludes references (58-59 p.)
In English.
Unmanned Aerial Vehicle (UAV)
PID Controller
Tilt-Wing
Vertical Takeoff and Landing
Institute of Graduate Studies - Department of Aviation Science
TL685
Design of an electrically powered dual motor Tilt-Wing UAV to investigate and develop an automated stability system for pitch and roll control in takeoff, hover and landing flight modes/ Devan Jessie Aaron Rudolph; Prof. Dr. Suleyman Tolun. - Kyrenia: University of Kyrenia, 2023. - 83 p.: fig.; 30 cm.
Master (Thesis).
Uncludes references (58-59 p.)
In English.
Unmanned Aerial Vehicle (UAV)
PID Controller
Tilt-Wing
Vertical Takeoff and Landing
Institute of Graduate Studies - Department of Aviation Science
TL685