DESIGN AND FABRICATION OF SMALL VERTICAL-TAKE-OFF-LANDING UNMANNED AERIAL VEHICLE

Design and Fabrication of Small Vertical-Take-Off-Landing Unmanned Aerial Vehicle

Design and Fabrication of Small Vertical-Take-Off-Landing Unmanned Aerial Vehicle

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Modern UAVs available in the market have well-developed to cater to the countless field of application.UAVs have their own limitations in terms of flight range and manoeuvrability.The traditional fixed-wing UAVs can fly for long distance but require runways or wide-open spaces for take-off and landing.On the other hand, the more Oral Care trending multirotor UAVs are extremely manoeuvrable but cannot be used for long-distance flights because of their slower speeds and relatively higher consumption of energy.This study proposed the implementation of hybrid VTOL UAV which has the manoeuvring advantage of a multirotor UAV while having the ability to travel fast to reach a further distance.

The design methodology and fabrication method are discussed extensively which would be followed by a number of flight tests to prove Double Gas Oven the concept.The proposed UAV would be equipped with quadcopter motors and a horizontal thrust motor for vertical and horizontal flight modes respectively.

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