• 한국정보통신학회논문지
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• 제13권10호
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• pp.2147-2153
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• 2009

저가격형으로 프로토타잎 하이브리드형 리니어 펄스 모터(LPM)가 편측형으로 설계되었다. 모터의 정특성 및 동특성 측정위한 측정기기를 설계 제안하였다. 실험측정결과 프로토타잎 리니어 펄스 모터의 정특성 및 동특성을 구체적인 추력의 값으로 확인하였다. 프로트타잎 리니어 펄스 모터를 구형파와 마이크로스텝 구동으로 구동하여 각각의 경우의 추력의 변화를 확인하였다. 실험결과 마이크로스텝구동방식에서 추력리플이 현저히 줄어든 것을 확인할 수 있었다.

• 한국정밀공학회지
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• 제15권11호
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• pp.9-20
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• 1998

In recent manufacturing process, the increase of productivity has been attempted by reducing machining time with the increase of cutting force. However, the excessive increase of cutting force can cause tool breakage and have a bad effect on both manufacturing machine and workpiece. Thus, it is necessary to estimate and control the cutting force in real time during the process. In this study, use of disturbance observer is proposed for the indirect cutting force estimation. The estimated cutting force is used for the real-time control of feedrate, making the actual cutting force follow the reference force command. Since the suggested method does not need an expensive sensor like a dynamometer, the method is expected to be used practically. Since the actual cutting force follow the reference force, resulting the reducing of the machining time the increase of productivity are also expected, and the quality of cutting surface has been improved due to the adjusted feedrate. Besides, an actual constant cutting force guarantees the prevention of tool breakage. To show the effectiveness of the suggested cutting force control method, an experimental setup has been made without sensor and applied to several workpieces. Experiments show that the suggested method is effective to cutting force control of a CNC machining center.

• 제어로봇시스템학회논문지
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• 제20권5호
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• pp.563-569
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• 2014

This article focuses on a hemispherical resonator gyro driven by the Coriolis effect. A hemispherical shell, called a resonator, is maintained in the resonance state by amplitude control and phase locking control. Parametric excitation has been used to control the amplitude. For rate measurement mode or FTR mode, nodal points have been kept to an amplitude of zero. Angular rate measurement has been demonstrated by rotating a resonator. Frequency mismatch between two stiffness principal axes is a major cause of low performance: vibrating pattern drift and reduced control effectiveness. This mismatch has been reduced significantly by the addition of small mass. A negative spring effect, which lowers resonance frequencies, has been verified experimentally.

• Journal of Astronomy and Space Sciences
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• 제28권4호
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• pp.311-317
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• 2011

Momentum changing actuators like reaction wheels and control moment gyros are generally used for spacecraft attitude control. This type of actuators produces force and torque disturbances. These disturbances must be reduced since they degrade the quality of spacecraft attitude control. Major disturbances are mainly due to static and dynamic imbalances. This paper gives attention to the reduction of the static and dynamic imbalance. Force/torque measurement system is used to measure the disturbance of the test reaction wheel. An identification method for the location and magnitude of the imbalance is suggested, and the corrections of the imbalance are performed using balancing method. Through balancing, the static and dynamic imbalance is remarkably reduced.

• International Journal of Aeronautical and Space Sciences
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• 제8권2호
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• pp.98-106
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• 2007

The vortex flow characteristics of a double-delta wing, which can change the incidence angle of its apex strake was investigated through the wing-surface pressure measurement and the particle image velocimetry(PIV) measurement of the wing-leeward flow region. The apex strake has sharp edges and can change its incidence angle with a hinge line at the 23% chord position measured from the apex of the main wing. The present study revealed that the incidence-angle change of the apex strake could greatly alter the vortex flow pattern around the double-delta wing and the wing-surface pressure distribution, which suggested that the apex strake could be used as an effective device for the active control of delta-wing vortex flow.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2000년도 추계학술대회 논문집
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• pp.31-35
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• 2000

A cantilever deflection measurement system for AFM(atomic force microscope) was constructed by the laser deflection method using LEP type PSD. Design process including sensitivity analysis was presented and the performance of the system was demonstrated by several experiments using a sample specimen with 50nm-step on the surface. The measured displacement-amplification-factor showed good agreement with the expected one with about 8% deviation. The step height measurement data were compared to what were acquired by commercial AFM, and the result showed that there were about 5nm-deviation between the two data. These results satisfies our expectation in the stage of system design.

• 한국소성가공학회:학술대회논문집
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• 한국소성가공학회 2008년도 춘계학술대회 논문집
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• pp.305-308
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• 2008

In this paper, the magnetic domain states and recordability of the molded magnetic nanopillars were examined and analyzed by magnetic force microscopy (MFM) measurement. We focused on the some of the technical issues for MFM measurement regarding the lift height and geometry of the MFM tip. The effects of MFM tip shape and lift height on the MFM resolution were analyzed. Finally, we showed that the magnetic film on each molded nanopillars has a single magnetic domain state.

• 한국융합학회논문지
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• 제8권11호
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• pp.49-56
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• 2017

컬링 스위핑 동작은 컬링 스톤의 위치를 조절하는 중요한 동작 중 하나이며, 스위핑 속도와 브룸 패드에 가해지는 힘이 중요한 연구 대상이다. 본 연구에서는 컬링 스위핑 동작에서 컬링 브룸 패드에 가해지는 힘을 측정할 수 있는 장비를 개발하였으며, 두 개의 로드셀을 브룸 패드와 패드 홀더 사이에 장착하는 구조를 이용하였다. 로드셀에서 발생되는 아날로그 신호는 마이크로 제어기를 이용하여 초당 약 300회의 속도로 샘플링을 수행한 후 10 bit 디지털 신호로 변환하였다. 3개의 M1 급 분동을 이용하여 로드셀의 교정과 측정된 전기 신호를 질량(힘)으로 환산하는 회귀 방정식을 추출하였으며, 브룸의 무게 증가를 최소화하기 위해서 웨어러블 장비로 구성하였다. 스포츠 분야에서 힘 측정 시 기준 장비로 사용하는 지면 반력기와 개발된 장비에 동일한 힘을 가하면서 측정된 측정값 차이는 약 $0.909{\pm}1.375N$ (평균과 표준 편차)로 측정되었다. 개발된 장비는 스위핑 동작과 유사한 힘 측정을 필요로 하는 다른 종류의 연구에도 적용이 가능할 것으로 판단된다.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2007년도 추계학술대회 논문집
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• pp.131-132
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• 2007

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2012년도 춘계학술대회 논문집
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• pp.853-854
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• 2012