A Review on Vertical Take-Off and Landing (VTOL) Tilt-Rotor and Tilt Wing Unmanned Aerial Vehicles (UAVs)

Table 8

Prototyping analysis done by various teams.

Team	Innovation carried	Software/technique used	Remarks
B. V. Sandilya	Tilt quad rotor aircraft have features of both fixed-wing UAV	3D modeling	Further need to control the UAV using a fully autonomous system is required for a more efficient
Seunghee Yu	Lighter than Tr-100 and has easy manoeuvrability	Prototype built	Summarizes a comparison report in terms of performance and applications
D. F. Finger	Balancing electric propulsion system	Tool by institute of aircraft engineering of FH aachen	Fully electric aircraft are still too heavy and hybrid electric provide no clear advantage over other systems
D.F Finger	Various configurations are tested with different forward and vertical motors	3D modeling	VTOL aircraft are certainly very feasible; their design remains challenging, but the advantages are still highly beneficial