Design and Analysis of High Endurance Fixed Wing Multirotor UAV
International Journal of Scientific Research in Science Engineering and Technology2022pp. 277–287
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Abstract
Current work emphasis on research, design and development of a fixed wing multirotor Unmanned Ariel Vehicle (UAV) which operate under V - TOL configuration. In this investigation an effort is made to develop a high endurance and high payload capacity UAV which can have a payload capacity of 15 Kg and which can serve with the endurance of 2 hrs per cycle.
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