Open AccessAn angle speed and thrust relationship of the rotor system in the quadcopter aircraft
Author(s) -
Al Al,
Arfita Yuana Dewi,
Antonov Bachtiar,
Dwi Harinita
Publication year - 2019
Publication title -
indonesian journal of electrical engineering and computer science
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.241
H-Index - 17
eISSN - 2502-4760
pISSN - 2502-4752
DOI - 10.11591/ijeecs.v13.i2.pp469-474
Subject(s) - thrust , lift (data mining) , propeller , rotor (electric) , rotational speed , quadcopter , physics , control theory (sociology) , engineering , electrical engineering , aerospace engineering , marine engineering , computer science , mechanical engineering , control (management) , artificial intelligence , data mining
Utilizing Quadcopter were still many obstacles such as; plane easy to fall; the battery is not durable; vulnerable to weather conditions and others. The research and development has grown to improve aircraft facilities and capabilities. Many parameters related to aircraft lift capability factors; fly long; flying high; type of motor; the type of propeller: including the sensors and control systems used. This study was to find the relationship between changes in the BLDC motor voltage source to the rotor angle velocity (ω) ; rotor speed to rotor lift (Ft) ; wind speed to rotor lift; push the following rotor (Ct) . Empirical testing was conducted in the laboratory to find the relationship of these parameters. The results data show that; the lift power generated with rotational speed was not proportional, non linearity occurs when the rotor was released from the self and starts pulling the strain gauge when the rotation speed reaches around 65 rps . Once the rotation speed of the rotor is able to reach up to 1.5 Newton lift then the thrust rising trend sharply increasing to increasing of the rotor speed. A motor hade 1200 KV and blade with a radius of 0.12 m , then obtained thrust (Ct) of 1.732.