
Fixed wing type UAVs are used for long flight time and high altitude conditions, while helicopter or multi-propeller wingless type UAVs are preferred for short flight, low altitude and high maneuvering tasks. In this case, a mission-specific aircraft developed cannot be used for another mission.
The aim of unmanned aircraft projects is to create an unmanned aircraft protected by intellectual property rights by patent application combining the advantages of two different winged and rotor type aircraft on a single platform. Another aim of the project is that the ease of use of the developed aircraft will be high and the operational costs will be quite low compared to the systems used.
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