CALCULATION OF THRUSTS OF UNMANNED AERIAL VEHICLE MOTORS AND COMPARATIVE ANALYSIS

H.G. DARBINYAN; G.I. YENGIBARYAN; A.G. ARAKELYAN; B.K. ABRAHAMYAN; R.K. SIMONYAN

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H.G. DARBINYAN National Polytechnic University of Armenia Author
G.I. YENGIBARYAN National Polytechnic University of Armenia Author
A.G. ARAKELYAN National Polytechnic University of Armenia Author
B.K. ABRAHAMYAN National Polytechnic University of Armenia Author
R.K. SIMONYAN National Polytechnic University of Armenia Author

Keywords:

thrust, hexacopter, kinematic scheme, UAV

Abstract

The kinematic features of the UAV, transporting up to 2 litres of liquid material are studied, and the thrust forces are calculated. Through RCbenchmark 1580 test stand, the thrust of T-Motor U3 motor with four different propellers are tested. A comparative analysis of the obtained results and the data given in the datasheet of the tested motor is carried out. The choice of hexacopter-UAV motors is proved.

CALCULATION OF THRUSTS OF UNMANNED AERIAL VEHICLE MOTORS AND COMPARATIVE ANALYSIS

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