• 한국항공우주학회지
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• 제39권12호
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• pp.1133-1140
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• 2011

기존의 홀추력기 개념 설계는 비용이 많이 소요되며 과거의 데이터에 기반한 실험적 방법에 근거하고 있다. 본 연구에서는 이러한 홀추력기의 설계 과정을 향상시키기 위해 최근 제안된 수치적 방법에 근거하여 설계 목적에 적합한 설계 공간을 설정하고 이에 대한 설계 공간 탐색을 수행하였다. 설계 공간 탐색의 결과를 통해 기본적으로 주어진 설계 공간에 대한 성능 범위를 결정하였으며 성능간의 관계를 분석하였다. 세부적인 결과 분석을 통해 홀추력기의 주요한 설계 변수로는 양극에서의 질량유량과 방전전압임을 도출하였다.

• 센서학회지
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• 제25권5호
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• pp.310-319
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• 2016

Three types of gap sensors, a capacitive gap sensor, an eddy current gap sensor, and a Hall effect gap sensor are described and evaluated through experiments for the purpose of precise gap sensing for micrometer scale movement, and a novel type of differential hall effect gap sensor is proposed. Each gap sensor is analyzed in terms of resolution and environment dependency including temperature dependency. Furthermore, a transport system for AMOLED deposition is introduced as a typical application of gap sensors, which are recently receiving considerable attention. Based on the analyses, the proposed differential Hall effect gap sensor is found to be the most suitable gap sensor for precise gap sensing, especially for application to a transport system for AMOLED deposition. The sensor shows resolution of $0.63mV/{\mu}m$ for the overall range of the gap from 0 mm to 2.5 mm, temperature dependency of $3{\mu}m/^{\circ}C$ from $20^{\circ}C$ to $30^{\circ}C$, and a monotonic characteristic for the gap between the sensor and the target.

• 한국조명전기설비학회:학술대회논문집
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• 한국조명전기설비학회 2003년도 학술대회논문집
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• pp.315-317
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• 2003

This paper deals with the position control of an AC servo motor using linear hall-effect sensors. The price of these is very low, but it is possible to make position control of motor similar to a control using an encoder. This paper introduces the design of motor using linear hall-effect sensors and shows the results of control.

• 한국재료학회지
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• 제12권3호
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• pp.195-199
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• 2002

Planar Hall effect of ferromagnetic GaMnAs thin films was investigated for the first time. The films were grown in an optimized growth condition via molecular beam epitaxy at low temperatures. For the optimization of the growth conditions, we used reflection high-energy electron diffraction, electrical conductivity, double crystal x-ray diffraction, and superconducting quantum interference device measurements techniques. We observed that the difference between the longitudinal resistance and the transverse resistance matches the planar Hall resistance. The ratio of the planar Hall resistance at saturation magnetic field to that at zero reached above 500%.

• 대한전기학회:학술대회논문집
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• 대한전기학회 1991년도 하계학술대회 논문집
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• pp.187-190
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• 1991

The analytical model to investigate the effects of the drift and diffusion carrier transport upon the Hall effect is presented and applied to the general PN junction structure. The diffusion current effect on the Hall coefficient can not be considered in the conventional model, which produces the conversion of the direction of the induced Hall field between measured and calculated values. The proposed analytical model which considers the diffusion current effect provides the coincident results with the previous experimental results.

• 전기학회논문지
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• 제59권1호
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• pp.70-75
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• 2010

The objective of this paper is to propose a new velocity measurement method for an electro-mechanical fin actuator. The model of the electro-mechanical fin actuator includes uncertainties such as unknown disturbances and parameter variations in flight condition. So, an electro-mechanical fin actuator system needs robust control algorithm which requires not only position information but also velocity information. Usually, analog tachometers have been used for velocity feedback in an electro-mechanical fin actuator. However, using these types of sensors have problems such as the cost, space, and malfunction. These problems lead to propose a new velocity measurement method using linear type Hall-effect sensor. In order to verify the proposed method, several experiments are performed using Model Following Sliding Mode Controller(MFSMC). It is shown that the MFSMC with a new velocity measurement method using linear type Hall-effect sensor can satisfy the requirements without using of velocity sensor.

• Journal of Magnetics
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• 제18권4호
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• pp.454-459
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• 2013

This paper deals with an optimal angle error reduction method of magnetic position sensor using hall effect elements. The angle detection simulation for the magnetic position sensor is performed by 3 dimensional finite element method and Taguchi method, one of the design of experiments. The magnetic position sensor is required to generate ideal sine and cosine waveforms from its hall effect elements according to rotation angle for precise angle information. However, the output signals are easy to include harmonics due to uneven magnetic field distribution from permanent magnet in the air-gap in the vicinity of hall effect elements. For the Taguchi method, three design parameters related to position of hall effect elements and shape of back yoke are selected. The characteristics of optimal magnetic position sensor are compared with those of original one in terms of simulation as well as experiment. Finally, the performances of the motor adopting original model and optimal model are represented for the purpose of verification of motor performance due to signals from magnetic position sensor.

• 대한수학회보
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• 제55권3호
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• pp.735-747
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• 2018

This paper deals with the asymptotic behavior of solutions to the generalized MHD and Hall-MHD systems. Firstly, the upper bound for the generalized MHD and Hall-MHD systems is investigated in $L^2$ space. Then, the effect of the Hall term is analyzed. Finally, we optimize the upper bound of decay and obtain their algebraic lower bound for the generalized MHD system by using Fourier splitting method.

• 한국초전도학회:학술대회논문집
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• 한국초전도학회 2009년도 Korea Superconductivity Society Meeting 2009
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• pp.59-59
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• 2009

• 한국항공우주학회지
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• 제43권4호
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• pp.377-386
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• 2015

본 논문에서는 국내에서 개발된 인공위성 중 최초로 홀 추력기(Hall-effect Thruster)를 탑재한 두바이셋-2(DubiaSat-2)호의 궤도를 분석하여 홀 추력기의 성능을 검증하였다. 두바이셋-2호가 발사된 2013년 11월 21일(UTC) 이후 8개월간의 초기 궤도 운용을 위한 준비 및 수행 결과들에 대해 중점을 두었으며, 임무 수행 기간 중 태양활동이 궤도 변화에 미치는 영향력을 함께 분석하였다. 특히, 증가한 추력에 따른 실제 궤도 변화와 예측된 궤도를 비교하여 분석한 결과 홀 추력기는 지상 실험 결과와 유사한 11 mN 추력을 발생하고 있는 것을 확인하였다. 본 논문에서 정리된 내용은 추후 홀 추력기를 탑재한 인공위성의 초기 및 정상 임무기간 동안 궤도 운용 시 안정성과 효율성을 높이는데 주요 참고자료가 될 것으로 판단된다.