2016 International Conference on Advances in Electrical, Electronic and Systems Engineering (ICAEES) 2016
DOI: 10.1109/icaees.2016.7888114
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Characterization of DC brushless motor for an efficient multicopter design

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Cited by 3 publications
(2 citation statements)
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“…Moreover, their acoustic emissions and thermal signature are high, and the theme of environmental sustainability (due to the shortage of fossil fuels, global warming, and increasing pollution) is a factor to their detriment and pushes toward the adoption of electric propulsion [129]. The choice of electric motors in small-to-medium-sized UAVs is the most common [9,64,100,106], due to their multiple advantages: high efficiency, low noise emission, low thermal dissipation, reliability, no pollutant emission, self-starting, controllability, and high maneuverability. The brushless DC motors' increasing diffusion among electrically actuated UAVs was confirmed by the literature review: indeed, for the totality of the analyzed articles with electric propulsion UAV, the motor used was a brushless DC.…”
Section: Actuation Typesmentioning
confidence: 99%
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“…Moreover, their acoustic emissions and thermal signature are high, and the theme of environmental sustainability (due to the shortage of fossil fuels, global warming, and increasing pollution) is a factor to their detriment and pushes toward the adoption of electric propulsion [129]. The choice of electric motors in small-to-medium-sized UAVs is the most common [9,64,100,106], due to their multiple advantages: high efficiency, low noise emission, low thermal dissipation, reliability, no pollutant emission, self-starting, controllability, and high maneuverability. The brushless DC motors' increasing diffusion among electrically actuated UAVs was confirmed by the literature review: indeed, for the totality of the analyzed articles with electric propulsion UAV, the motor used was a brushless DC.…”
Section: Actuation Typesmentioning
confidence: 99%
“…The papers in the sub-class propulsion were mainly focused on the motor, and almost all were related to the design or characterization of brushless DC motors, as in the following cases. Lee et al [42] put forward the optimal design method for UAVs and interior permanent magnet motors for drones that require high thrust of high rotational speed; Marcolini et al [78] investigated the design of a multiphase coreless axial flux permanent magnet machine with concentrated windings, to obtain very high power and torque densities; Liben et al [84] presented an analytical design method to develop a ring motor that was wrapped around the outer diameter of a propeller; Xu et al [91] presented a novel parameter design method for a DC brushless motor; Parvez Alam et al [98] aimed at the design and development of a small-scale test rig setup for the measurement of the thrust of any brushless DC motor; Zulkipli et al [100] studied the characteristics of a brushless direct current motor for the purpose of multicopter design. A very limited number of works dealt with actuators based on other technologies, such as the work of Mingjun et al [96], who presented a new type of compact smart hydraulic actuator, or of Jims John Wessley [40], who presented the design of major components of a turbojet engine that could produce thrust suitable for medium-altitude UAVs.…”
Section: Design Levelmentioning
confidence: 99%