Abstract
This paper presents the identification process of the electric propulsion system for Unmanned Aerial Vehicles. Prepared identification test rig was described in details. It allows to control the electric motor with a propeller and to measure the parameters like thrust force, torque, current and supply voltage, that were used during identification. The worked out and presented identification test helps to check and verify the electric propulsion properties and to develop more accurate simulation models of UAVs.
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