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