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| Team | Innovation carried | Software/technique used | Remarks |
|
| Paul Heslinga et al. | UAVs with a dual-nacelle tilt-rotor | MATLAB simulink | Aims for a low payload with pace and stability. Two prototypes were tested successfully |
| M Ciopcia et al. | Tilt-rotor properties on a fly-by-wire | Lift-drag mathematical model | Worked on steering system combined with transitional state along with efficiency report |
| Ubair Ejaz Butt et al. | Tilt-rotor mechanism | Creo 2.0, mathematical modeling | Test of control of UAV using a rotor |
| N.C. Ajay V et al. | Stability of a tilt-rotor UAV | Prototyping with BLDC motors, servos, mathematical modeling | Analyzed contribution of the wing, fuselage, and tail for stability |
| Carlos A. et al. | Aircraft with tilt-rotor configuration with ducted-fan | XFLR5 and ANSYS FLUENT | A 20% increase in the lift at full thrust was reported. |
| Naman Rawal et al. | Coaxial tilt-rotor design | Structural modeling with performance study and analysis, Dree’s model | Enhancements in maximum cruise velocity, range, endurance, and rate of climb reported |
| Pau Seguí Gascó | Dual-axis tilt quadrotor | Mathematical design and model, Simulink | 20% increase in the efficiency of the new actuator suite |
| G. Flores et al. | Hardware execution of a tilt-rotor aircraft | EFCS | Longitudinal dynamics are derived at hover and forward flight mode |
| Chao Chen et al. | Tri-rotor-copter concept UAV | Mathematical modeling | Tested the flight successfully |
| Liu Zhong et al. | Investigations on tilt-rotor UAVs ranging from dual copter to quadcopter | Investigations of models, features, and algorithms | Concluded that focus should be on robustness and stability |
| Ali B Junaid et al. | Actuation concept for quadcopter UAV | Maple software, MATLAB simulink, 3D printing, and mathematical modeling | Developed UAV with aggressive manoeuvering for congested environments |
| Shishir G et al. | Prototype VTOL UAV quadcopter with four tilt-rotors and a fixed-wing | Prototyping | Successfully carried a payload of 900 grams at 100–150 feet |
| Daeil Jo et al. | Manufactured own hybrid UAV | CAE software, prototyping, FW coding | A prototype was tested successfully and can carry a 3 kg payload |
| Bibek D et al. | Blended wing design for VTOL UAVs | CATIA CAD software | The concept of the blended wing is unique; however, no prototype was made and tested |
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