• 대한전기학회:학술대회논문집
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• 대한전기학회 2015년도 제46회 하계학술대회
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• pp.884-885
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• 2015

This paper presents the characteristic analysis and experiment of pitching moment in permanent magnet linear synchronous motor (PMLSM) for precision machine tools. In this paper, we define force characteristics of the moment and the moment analysis by the finite element method. Manufacture experiment and we will compare the results of finite element analysis and experimental results.

• 전기학회논문지
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• 제64권12호
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• pp.1695-1702
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• 2015

This paper presents the characteristic analysis and experiment of force characteristics in permanent magnet linear synchronous motor for accuracy prediction of linear motion machine tools. In particular, the pitching moment resulting from attraction force ripple has been analysed and tested. Firstly, we analysed the characteristics of detent force, attraction force, and pitching moment in permanent magnet linear synchronous motor according to the design techniques such as auxiliary teeth, chamfering, and permanent magnet skewing. In addition, we suggested the experimental set for measurement of pitching moment. Finally, the results from measurement shows the good agreement with those obtained from finite element analysis results.

• Journal of Advanced Marine Engineering and Technology
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• 제21권5호
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• pp.503-511
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• 1997

In 3 phase induction motor control system, the speed control using the load torque observer becomes robust against disturbances by means of a feed-forward control of the estimated load torque component. In case of variation of inertia moment, the estimated load torque has error because the observer uses the nominal inertia to estimate the load torque. And so, it is difficult to obtain good speed control characteristics. This paper has two study target strategy. First, we executes feed-forward control with the load torque observer when motor inertia has nominal value and compare it with conventional PI con¬trol. The second strategy estimates inertia moment error using the load torque observer when inertia moment change. The proposed two strategy is confirmed through the computer simulations and the experimental implementations by TMS320C31 microprocessor.

• 한국정밀공학회지
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• 제25권10호
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• pp.115-121
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• 2008

This paper presents bisymmetric dual iron core lineal motor stage for heavy-duty high precision applications such as large area micro-grooving machines or high precision roll die machines. In this stage, two iron core linear motors are installed in laterally symmetric way to cancel out the attractive forces. Main focus was given to analyzing the effect of cogging force and moment for two different layouts, which are symmetric and half-pitch shifted ones. Experimental results showed that the symmetric layout is more adequate for high precision applications because of its clear moment cancellation effect. It was also verified that the effect of the residual cogging moment can be suppressed further by increasing the bearing stiffness. One problem of the symmetric layout is added cogging force which hinders smooth motion, but its effect was relatively small compared with that of moment cancellation.

• 전력전자학회논문지
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• 제10권5호
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• pp.436-442
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• 2005

본 논문에서는 전동기의 고성능 속도제어를 위해 필수적인 상수인 관성을 추정하는 알고리즘을 제안한다. 제안된 알고리즘은 속도관측기에서 발생되는 관성오차의 정보를 포함하고 있는 위치 오차신호를 관측하여 이를 비례적분 제어기를 사용하여 정상상태 오차를 없게 제어함으로써 관성을 추정하므로 특히, 관측기 기반 속도측정법에 쉽게 구현이 가능하다. 모의실험과 실험결과를 제시하여 추정관성이 제안된 방법에 의하여 실제값에 수렴하였으며 이에 파라 관측된 속도 역시 실제 측정된 속도와 일치하게 되었으며, 속도제어기가 설계한 응답특성을 보임을 입증하였다.

• 우주기술과 응용
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• 제3권4호
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• pp.322-332
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• 2023

Satellite attitude-control actuators are equipped with a reaction wheel for three-axis attitude control. The reaction wheel rotates a motor inside the actuator to generate torque in the vector direction. When using the reaction wheel, there are restrictions on the torque values generated as the motor rotates. The torque value of the reaction wheels mounted on small satellites is approximately 10 mNm, and high values are not used. Therefore, three-axis attitude control of a small satellite is possible using a reaction wheel, but this method is not suitable for missions that require rapid attitude control at a specific time. As a technology to overcome the small torque value of the reaction wheel, the control moment gyro (CMG) is currently in wide use as a rapid attitude-control actuator in space satellites. The CMG has an internal gimbal mounted at a right angle to the rotation motor and generates a large torque value. In general, when the gimbal operates, a torque value approximately 100 times greater is generated, making it suitable for rapid posture maneuvering. Currently, we are developing a technology for mounting a controlled moment gyro on a small satellite, and here we share the development status of an 800 mNm CMG.

• 한국항공우주학회지
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• 제43권2호
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• pp.172-178
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• 2015

제어 모멘트 자이로(control moment gyroscope, CMG)는 고토크 발생 장치로서 인공위성 뿐만 아니라 항공, 선박, 자동차, 로봇 등의 다양한 산업분야의 자세안정화와 기동 시스템에 적용될 수 있다. 본 논문은 여러 산업분야에서 적용할 수 있는 100Nm급 CMG 개발 전반에 대한 내용을 다룬다. 이를 위해서 CMG 시스템레벨 요구사항 분석, 모터 서브시스템 설계/제작/조립, 시험장치 구성, 성능시험 및 평가에 대한 개발과정과 결과를 제시한다. 스핀모터와 김벌모터를 설계조건에서 구동하여 CMG의 토크출력이 120Nm 이상 생성됨을 성능시험을 통해 확인한다.

• 한국자동차공학회논문집
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• 제14권1호
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• pp.123-128
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• 2006

The proposed mathematical model of the starter-generator system incorporates the motor speed, battery voltage and the desired current to estimate the moment generation capabilities of the starter-generator and the actual current of the battery system. The fundamentals for this mathematical modeling are the simulated results of the experimental data. These pertinent data are used in establishing the governing equations for the determination of motor moments, actual battery currents and efficiencies of the system's operation at different loading characteristics and speed regions. The derived equations will be used into simulation programs to predict the fuel efficiency, vehicle characteristics of a hybrid electric vehicle equipped with a transmission starter-generator which will be developed.

• 한국자동차공학회논문집
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• 제21권6호
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• pp.40-48
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• 2013

Recently, many types of electric vehicles including a heavy duty vehicle have been developed and released because of the better fuel economy and less gas products. In this study, research about an electric bus which utilizes the wheel motor drive system was conducted. The wheel motor is a motor connected to the wheel directly only with a simple gear so that the developer can utilize the space efficiently and the whole system efficiency will be better because of simple structure. However, because it is different from former types of vehicles which use the differential gear, the development of the integrated control logic is required in order to meet the vehicle stability and driving performance. The developed control logic is composed with direct yaw moment control, regenerative braking control and slip control logics. It is compared to the control logics which does not consist of direct yaw moment control and slip control when the vehicle is exposed in tough situations. For the unification of the control logic, a few maps were developed and applied to determine the output torque of each motor according to the driving status. As a result, it is shown that the developed control logic is more safe and well follow the target speed than the other control logic applied simulations.

• 한국정보통신학회논문지
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• 제2권4호
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• pp.627-634
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• 1998

본 논문에서는 관성 모멘트 동정에 의해 상태관측기의 성능 및 유도전동기의 저속운전 특성을 개선하는 알고리즘을 제안하였다 저속운전 영역에서 저 분해능 엔코더를 사용하는 속도 검출법은 속도 주기내에 펄스수가 너무 적어 정확한 속도정보를 얻을 수 없다 이러한 문제점을 개선하고자 속도와 외란을 추정할 수 있는 고피나스 이론에 근거한 상태관측기를 설계하여, 외란이 제거된 제어를 수행하였다. 또한 추정된 속도와 외란의 오차를 최소화하기 위하여 전동기의 관성 모멘트를 추정하고, 관측기의 공칭 관성 린멘트를 동정하였다. 시뮬레이션과 실험결과로부터 제안된 알고리즘은 6［rpm］ 이하의 저속영역에서 과도응답 특성의 향상을 보여주었다.