@thesis{thesis,
		author={LUTHFIE TSAQIF  LAUDZA},
		title ={RANCANG BANGUN BATANG VTOL PADA UAV SKY-BEEJO SEBAGAI
TEMPAT PENEMPATAN PROPULSI UAV VERTICAL TAKE OFF LANDING},
		year={2024},
		url={http://eprints.stta.ac.id/1694/},
		abstract={In research with the theme of adding VTOL rods, of course a lot of changes or overhauls
are needed in the load, structure, materials used, propulsion and also the design of the
UAV itself. Therefore, significant changes will also be made to the VTOL rod itself so that 
it can be adequate so that a UAV can take off and land. The addition of VTOL rods to the 
UAV wing structure, which was previously a Fixed Wing type UAV then changed to a 
UAV that can perform VTOL or Vertical Take off Landing. Using the Margin Of Safety
method. From this research, the results obtained obtained ARM VTOL configuration with 
a length of 85cm using aluminum and placed at a distance of 50cm from the fuselage. 
From the simulation get a margin of safety value of 5.1339.}
		}