• Proceedings of the KIPE Conference
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• 2006.06a
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• pp.501-503
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• 2006

최근 산업 분야에서 리니어모터는 고속, 고정밀도의 요구사항에 따라 회전 모터와 볼 스크류, 벨트를 이용한 직선구동방식보다 빠르고 정확하며, 효율이 높기 때문에 활발히 이루어지고 있다. 리니어모터 중에서 선형 브러시리스 직류 전동기(LBLDCM)는 다른 리니어모터에 비해 소형, 경량이 가능하고, 저속 및 고속의 운전이 용이하며, 기계 가공 정도보다는 엔코더 등과 같은 위치 결정 응용 분야에 적합하며 본 연구에서 사용된 LBLDCM은 코일 가동형으로 영구 자석에 의해 발생된 자계와 가동자 코일에 흐르는 전류 사이에 작용하는 힘을 이용하게 된다. 이와 같은 LBLDCM을 응용분야에 적용하기 위해서는 구동 중에 속도가 변하는 지점에서 발생하는 진동을 줄여야 하며 목표지점까지의 정확한 위치 제어가 필수적이다. 따라서, 본 연구에서는 다양한 속도 프로파일에 따른 진동에 대해 비교 분석한 후, 이동거리에 따른 적합한 속도 프로파일에 대해 알아보았고, 그 결과를 토대로, 목표지점까지의 위치 오차를 저감하면서 정밀한 위치 제어에 적합한 프로파일을 제시하였다.

• Proceedings of the KIEE Conference
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• 1998.11a
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• pp.46-48
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• 1998

In this paper, axial type double rotor brushless DC motor is designed where the rotor is located at the both sides of stator. The rotor uses rare-earth magnets of 16 poles and the stator has 12 coils. The genetic algorithm is used to optimize the efficiency of the designed motor. The characteristics of the design parameters are estimated by varying them for the maximum efficiency.

• Journal of Aerospace System Engineering
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• v.13 no.3
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• pp.1-8
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• 2019

The electromagnetic forces generate a torque on the gimbal motor, and changes in the coil current causes torque ripple. This affects the gimbals' speed and results to unstable satellite attitude. It is therefore essential to reduce the torque ripple of the gimble motor with the aim of improving the attitude control accuracy of the satellite. This paper theoretically analyzes the torque generated from the modeling of a motor for general concentrated winding and distributed winding. The prototype was designed and fabricated through selection of the winding that reduces the torque ripple through simulation results. The results of the magnetic fields' theoretical analysis and the back electromotive force of the prototype were compared with the calibrated results for verification of conformity and manufacture of the design. The low-speed test proved that the torque ripple is reduced by improving the speed stability.

• The Transactions of the Korean Institute of Power Electronics
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• v.21 no.2
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• pp.134-143
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• 2016

This paper proposes a novel asymmetrical interior permanent magnet (IPM) brushless DC (BLDC) motor structure, which utilizes half-type permanent magnet (PM) configuration and has asymmetrical side gaps (slot next to the PMs) for reducing torque ripples. This structure uses 24% less volume of PMs than conventional IPM BLDC motor with a full set of magnets. The characteristics of the proposed motor are compared with three other half-type IPM BLDC motors through finite elements method (FEM) analysis, and the usefulness of the proposed motor was verified through experimental evaluation on prototypes of the conventional motor and proposed motor under various torque load conditions. This research obtained a high-performance IPM BLDC motor while decreasing manufacturing cost at the same time.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.47 no.4
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• pp.300-308
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• 2019

For drones to be used for industrial or agricultural applications, it is necessary to increase the payload and endurance. Currently, the payload and endurance are limited by the battery technology for electric powered drones. In addition, charging or replacing the batteries may not be a practical solution at the field that requires near continuous operation. In this paper, a procedure to optimize the power system of an electric hybrid drone that consists of an internal combustion engine, a generator, a battery, and electric motors is presented. The example drone for crop dusting is sized for easy transportation with a maximum takeoff weight of 200 kg. The two main rotors that are mechanically connected to the internal combustion engine provides most of the lift. The drone is controled by four electric motors that are driven by the generator. By analyzing the flow of the energy, a methodology to select the optimum propeller and motor among the commercially available models is described. Then, a procedure of finding the optimum operational condition along with the proper gear reduction ratios for the internal combustion engine based on the test data is presented.