• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2001년도 춘계학술대회 논문집
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• pp.1021-1024
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• 2001

Out of all metal-cutting processes, the hole-making process is the most widely used. It is estimated to be more than 30% of the total metal-cutting process. It is therefore desirable to monitor and detect drill wear during the hole-drilling process. In this paper, the vision system of the sensing methods of drill flank wear on the basis of image processing is used to detect the wear pattern by non-contact and direct method and get the reliable wear information about drill. In image processing of acquired image, median filter is applied for noise removal. The vision flank wear area of the drill was measured. Backpropagation neural networks (BPns) were used for no-line detection of drill wear. The neural network consisted of three layers: input, hidden and output. The input vectors comprised of spindle rotational speed, feed rates, vision flank wear, thrust and torque signals. The output was the drill wear state which was either usable or failure. Drilling experiments with various spindle rotational speed and feed rates were carried out. The learning process was peformed effectively by utilizing backpropagation. The detection of the abnormal states using BPNs achieved 96.4% reliability even when the spindle rotational speed and feedrate were changed.

• 재활복지공학회논문지
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• 제10권3호
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• pp.229-236
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• 2016

자기 센서와 액추에이터는 산업과 의료 분야에서 광범위하게 사용되고 있다. 센서와 액추에이터의 기반의 통합시스템은 기계 및 전자 기기들의 일반적인 조합으로써 메카트로닉스로 정의된다. 최근에 자기 무선 센서와 액추에이터가 개발되어지고, 다양한 분야에서 사용되고 있다. 특히 이 메커니즘은 자성 물질 및 물리적 현상에 관한 것으로 자기의 세기의 따라 달라진다. 그러나 이들 연구의 경계는 명확하지 않다. 따라서, 자기 마이크로 로봇, 자기액추에이터 및 센서들을 포함한 새롭고 정확한 정의가 필요하다. 본 연구에서는 의공학 및 재활을 위한 자기 메카트로닉스의 진보되고 확장된 개념을 혈관 재활을 위한 무선 펌프 시스템과 모션 감지 시스템을 중심으로 소개하고자 한다.

• Journal of Biosystems Engineering
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• 제41권4호
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• pp.304-312
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• 2016

Purpose: Soil strength has been measured using a cone penetrometer, which is making it difficult to obtain the spatial data required for precision agriculture. Our objectives were to evaluate real-time horizontal soil strength (RHSS) to measure soil strength in real time while moving across the field. Using the RHSS data, the tillage depth was determined, and the power consumption of a tractor and rotavators were compared. Methods: The horizontal soil-strength index (HSSI) obtained by the RHSS was compared with the cone index (CI), which was measured using a cone penetrometer. Comparison analysis in accordance with the measurement depth that increased at 5-cm interval was conducted using kriged maps at six sensing depths. For tillage control and evaluation of the power consumption, the system was installed with a potentiometer for tillage depth, a torque sensor from the rear axle, and a power take-off (PTO) shaft. Results: The HSSI was lower than the CI, but they were the same at 54.81% of the total grids for the 5-cm depth and at 3.85% for the 10-cm depth. In accordance with the recommended tillage map, tillage operations between 0 and 15 cm left 2.3% and 7% residue cover on the soil, and that between 20 and 10 cm covered a wider utilization of 3% and 18.4%, respectively. When the tillage depth was 15 cm, the comparison result of the power requirements between the PTO and rear axle in terms of control performance revealed that the maximum power requirements of the axle and PTO were 44.63 and 23.24 kW, respectively. Conclusions: An HSSI measurement system was evaluated by comparison with the conventional soil strength measurement system (CI) and applied to a tractor to compare the tillage power consumption. Further study is needed on its application to various farm works using a tractor for precision agriculture.

• 한국항공우주학회지
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• 제46권11호
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• pp.952-960
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• 2018

지구관측용 인공위성에서 고기동성이 많이 요구되고 있다. 고기동성을 만족시키기 위해 고토크 구동기가 인공위성 설계에서 필수적이다. 본 연구에서 고기동 소형위성 설계를 위해 한국항공우주연구원에서 연구되고 있는 5Nm급 소형 제어모멘트자이로(CMG, Control Moment Gyro) 개발 결과를 소개하였다. 구동로직 활용을 위해, 잘 알려진 Elliptic internal singularity를 성공적으로 회피하는 등으로 Singular Direction Avoidance (SDA) 방법에서 향상된 Designated Direction Escape (DDE) CMG 클러스터 구동로직에 대한 간단한 성능 검증과 상세한 로직 방법이 제시되었고, CMG가 피라미드 형태로 장착되었을 경우와 지붕 형태로 장착되었을 경우에 대해 5Nm급 소형 CMG가 고기동 소형위성 설계에 적절한지를 검증하기 위한 시뮬레이션이 수행되었다. 시뮬레이션 결과를 바탕으로 CMG 개발시 고려해야 할 의미있고 중요한 사항들을 제시하였다.