• 한국기술혁신학회:학술대회논문집
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• 한국기술혁신학회 2013년도 추계 학술대회 초록집
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• pp.88-97
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• 2013

• 전기전자학회논문지
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• 제23권4호
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• pp.1295-1301
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• 2019

본 논문에서는 어텐션 기법을 적용한 양방향 순환신경망을 이용하여 새로운 휴먼 모션 디노이징 방법을 제안한다. 본 방법을 이용하면, 단일 3D 깊이 센서 카메라에서 캡처된 노이즈가 포함된 사람의 움직임이 잘 교정된 자연스러운 움직임으로 자동 조정된다. 양방향 순환신경망에 어텐션 기법을 도입하면, 입력으로 들어온 움직임을 인코딩할 때 여러 자세 중에 더 중요한 자세가 있는 프레임에 더 높은 어텐션 가중치를 부여함으로써, 다른 딥 러닝 네트워크와 비교해 더 나은 최적화 결과와 더 높은 정확도를 보인다. 실험을 통해 본 논문에서 제시한 방법이 다양한 스타일의 움직임과 노이즈를 효과적으로 처리함을 확인하였으며, 제시한 방법은 모션 캡처 후처리 단계의 애플리케이션으로 충분히 사용 가능할 것으로 기대된다.

• 천문학회보
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• 제37권1호
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• pp.85.2-85.2
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• 2012

In this paper, we introduce the 3D modeling of the coronal magnetic field in the solar active region by extrapolating from the 2D observational data numerically. First, we introduce a nonlinear force-free field (NLFFF) extrapolation code based on the MHD-like relaxation method implementing the cleaning a numerical error for Div B proposed by Dedner et al. 2002 and the multi-grid method. We are able to reconstruct the ideal force-free field, which was introduced by Low & Lou (1990), in high accuracy and achieve the faster speed in the high-resolution calculation (512^3 grids). Next we applied our NLFFF extrapolation to the solar active region NOAA 10930. First of all, we compare the 3D NLFFF with the flare ribbons of Ca II images observed by the Solar Optical Telescope (SOT) aboard on the Hinode. As a result, it was found that the location of the two foot-points of the magnetic field lines well correspond to the flare ribbon. The result indicates that the NLFFF well capture the 3D structure of magnetic field in the flaring region. We further report the stability of the magnetic field by estimating the twist value of the field line and finally suggest the flare onset mechanism.

• International Journal of Aeronautical and Space Sciences
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• 제16권4호
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• pp.560-570
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• 2015

We present a simulation of a hybrid Reynolds-averaged Navier Stokes / Large Eddy Simulation (RANS/LES) based on detached eddy simulation (DES) for a Burrows and Kurkov supersonic planar mixing experiment. The preliminary simulation results are checked in order to validate the numerical computing capability of the current code. Mesh refinement studies are performed to identify the minimum grid size required to accurately capture the flow physics. A detailed investigation of the turbulence/chemistry interaction is carried out for a nine species 19-step hydrogen-air reaction mechanism. In contrast to the instantaneous value, the simulated time-averaged result inside the reactive shear layer underpredicts the maximum rise in $H_2O$ concentration and total temperature relative to the experimental data. The reason for the discrepancy is described in detail. Combustion parameters such as OH mass fraction, flame index, scalar dissipation rate, and mixture fraction are analyzed in order to study the flame structure.