Review Article
A Review on Vertical Take-Off and Landing (VTOL) Tilt-Rotor and Tilt Wing Unmanned Aerial Vehicles (UAVs)
Table 4
Modeling, design, and analysis done by various teams.
| Team | Innovation carried | Software/technique used | Remarks |
| N Amiri | Simulations to find pitch and yaw moments | CFD, propulsion, and sensors | The lift fan OAT mechanism has the capability of being efficient, providing high cruise speed and high manoeuvrability | Mahmoud Elfeky | A new concept of quad-rotor design with four rotors and each rotor having two axes of tilt | Prototype was tested | The mechanism gives a big boost to the manoeuvrability and agility of the quadcopter and enhances the fault tolerance of the UAV | Duc Anh Ta | Tilt tri-UAV configuration | Newton–Euler equations combined with an aerodynamic formula for a mathematical model | Demonstrated a basic control strategy and how it can achieve a longitudinal path | Muhammad R | Analysis of flight dynamics and tilt-rotor in a VTOL aircraft during the transition stage | MATLAB Simulink software | Further need for corrections and improvements to the dynamic model | D.F. Finger | A supplementary electric propulsion system | Prototype was tested | Demonstrates the various sizing possibilities depending upon the configuration requirements |
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