An Experimental Determinatıon And Numerical Analysis Of A Loiter Munition Unmanned Aerial Vehicle System
Citation
Saraçyakupoğlu T., Delibaş H. D., Özçelik A. D “An Experimental Determination and Numerical Analysis of A Loiter Munition Unmanned Aerial Vehicle System” Int. J. of 3D Printing Tech. Dig. Ind., 6(1): 83-101, (2022).Abstract
This paper experimentally determinates the calculation of an Unmanned Aerial Vehicle (UAV) and
analyzes the design criteria within four different scenarios. The UAV to be designed is a loiter munition
UAV system. A mobile or equipment such as a parachute and/or airbag. The UAV may be operable day
and night conditions, capable of 2-3 hours of flight hours, and will be launched from a catapult. The
UAV navigation system is compact and easily controlled by a personal Global Positioning System
(GPS). The mentioned UAV will have a vast operational capability, especially for defense and border
security activities since it is equipped with advanced avionics and a small physical footprint for covert
operations. As a consequence of this research, it can be claimed that the UAV's mid-wing, twin-tail, and
relatively light body will have three axis stability and offer numerous benefits, particularly in terms of
operational cost.
Volume
6Issue
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