@thesis{thesis,
		author={Saputra  Enggal},
		title ={RANCANG BANGUN ALAT UJI ELECTRIC DUCTED FAN (EDF) BERBASIS MIKROKONTROLER},
		year={2023},
		url={http://eprints.stta.ac.id/1105/},
		abstract={Electric Ducted Fan (EDF) is a type of motor that is currently popular, 
especially in the aerospace field. EDF can generate thrust through the ability of a 
rotating fan, EDF is often used in unmanned aerial vehicles (UAV). The 
development of UAVs is very rapid because they are needed for various needs, one 
example as a reconnaissance tool in military activities. The type of UAV being 
developed is high-speed UAV, high-speed UAV requires a large driving force to 
maximize the speed of the UAV. Using EDF as an engine for UAVs is a way to 
maximize speed for UAVs. EDF is made of plastic or aluminum and is designed 
with aerodynamics in mind. In this research, a microcontroller-based EDF test 
device was created which used an infrared sensor for calculating RPM, a load cell 
sensor for calculating thrust. The sensors were decoded using Arduino, and the 
results will be displayed on the LCD display. Of the 3 tests, the maximum thrust 
was found to be 212.666 gr, 11.07 V, 6.96 A, 76.9 W and 22533 RPM. Where each 
test is carried out with the same time, namely 30 seconds and the same battery. 
EDF maximum testing requires large and high resources so that EDF can achieve 
maximum results.}
		}