• Title/Summary/Keyword: 비손실 압축

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A Study on Residual U-Net for Semantic Segmentation based on Deep Learning (딥러닝 기반의 Semantic Segmentation을 위한 Residual U-Net에 관한 연구)

  • Shin, Seokyong;Lee, SangHun;Han, HyunHo
    • Journal of Digital Convergence
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    • v.19 no.6
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    • pp.251-258
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    • 2021
  • In this paper, we proposed an encoder-decoder model utilizing residual learning to improve the accuracy of the U-Net-based semantic segmentation method. U-Net is a deep learning-based semantic segmentation method and is mainly used in applications such as autonomous vehicles and medical image analysis. The conventional U-Net occurs loss in feature compression process due to the shallow structure of the encoder. The loss of features causes a lack of context information necessary for classifying objects and has a problem of reducing segmentation accuracy. To improve this, The proposed method efficiently extracted context information through an encoder using residual learning, which is effective in preventing feature loss and gradient vanishing problems in the conventional U-Net. Furthermore, we reduced down-sampling operations in the encoder to reduce the loss of spatial information included in the feature maps. The proposed method showed an improved segmentation result of about 12% compared to the conventional U-Net in the Cityscapes dataset experiment.

An Efficient Transmission Scheme of Aircraft Data (항공데이터의 효율적인 전송 방식)

  • Kang, Min-Woo;Ha, Seok-Wun;Moon, Yong-Ho
    • Journal of the Institute of Electronics Engineers of Korea SC
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    • v.49 no.3
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    • pp.62-68
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    • 2012
  • In this paper, we propose an efficient transmission scheme for flight data. It is important to reduce amount of flight data transmitted effectively for timely transmission in airplane that the safety is very importantly recognized. Thus, this paper shows the improved technique transmitting after compressing flight data by the lossless compression technique. Because the proposed method improves the transmission speed of the flight data effectively. The processing of flight data and handling can be easily performed in the time to be restricted. The simulation results show that the proposed scheme achieves 25% data transfer gain compared to the ARINC 429 based transmission method.

Medical Image Compression in the Wavelet Transform Domain (Wavelet 변환 영역에서 의료영상압축)

  • 이상복;신승수
    • The Journal of the Korea Contents Association
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    • v.2 no.4
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    • pp.23-29
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    • 2002
  • This paper suggest the image compression that is needed to process PACS in medical information system. The image decoding method is used Linear-predictor and Lloyd-Max quantizer(quantization) in the Wavelet transform domain. Wavelet Transform Method is processed the multi-resolution by dividing image into 10 sub-bands of 3 levels. Low frequency domain that is sensitive to human visual characteristic is encoded by DPCM which is lossless encoding methods, and Lloyed-Max quantizer, the optimal quantizer for reducing ringing and aliasing in the image of inter sub-band, is used in the remaining high frequency domain of sub-band. The examination verifies that decompressed images are superior by the result that PSNR is 28.53dB on the input image, 512$\times$152 abdominal CT image and Chest image.

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A Computational Study for the Discharge Coefficient of a Film-Cooling Hole (Film-Cooling Hole의 유출계수에 관한 수치해석적 연구)

  • 김재형;김희동;박경암
    • Journal of the Korean Society of Propulsion Engineers
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    • v.7 no.2
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    • pp.15-22
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    • 2003
  • Computational study using the 2-dimensional, compressible, Navier-Stokes equations is performed to predict the discharge coefficient of air flow through a film-cooling hole. In order to investigate the effect of internal/external flows on discharge coefficient, the present computational results which are obtained for three flow cases, only external flow, only internal flow, and no flow, are compared with experimental ones. It is found that the computational results predict the discharge coefficient of the film-cooling hole in a reasonable accuracy and the external crossflow reduces the discharge coefficient, while the internal crossflow increases the discharge coefficient in a range of momentum flux ratio $I_{c-jet}$ > 1 due to the total pressure loss and boundary layer effect.

Improved Momentum Exchange Theory for Incompressible Regenerative Turbomachines (II) - Loss Model and Performance Prediction - (비압축성 재생형 기계에 대한 개선된 운동량 교환 이론 (II) - 손실 모델 및 성능 예측 -)

  • Park Mu Ryong;Chung Myung Kyoon;Yoo Il Su
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.28 no.10
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    • pp.1247-1254
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    • 2004
  • In momentum exchange theory the loss models for the circulatory flow is critically important. But because of lack of loss model on the circulatory flow, analysis model on regenerative turbomachines is not available in the open literature. In the present study circulatory loss is evaluated by combining bend's losses. Through the comparison with the previous experimental data on linear pressure gradient, a combination factor is suggested in terms of the aspect ratio of a channel. Applying this factor to two kinds of regenerative blowers the predicted results are found to be in good agreement with the experimental data of the overall performance and the head distribution along the rotational direction. Especially, the comparison with the head distribution demonstrates the accuracy of hydraulic model and loss model suggested in the present study. And the comparison with the overall performance confirms the validness of physical models as well as loss models suggested in the present study.

A Study on the Performance of Ramp Tabs Asymmetrically Installed in the Supersonic Nozzle Exit (초음속 노즐 출구에 비대칭적으로 설치한 램프 탭의 성능 연구)

  • Kim, Kyoung-Rean;Ko, Jae-Myoung;Park, Jong-Ho
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.35 no.10
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    • pp.934-939
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    • 2007
  • Thrust vector control(TVC) is the method which generates the side force and moment by controlling the exhausting gas directly from the supersonic nozzle to change the trajectory of a missile quickly. In this paper, performance study on the tapered ramp tabs asymmetrically installed in the supersonic nozzle exhaust for the thurst vector control has been carried out using the supersonic cold flow system. To study the shock wave structure and location of the oblique shock wave produced by the ramp tab, the flow field visualization using the schlieren system is conducted. This paper provides the thrust spoilage, three directional forces and moments and distribution of surface pressure on the region enclosed by the tapered ramp tabs.

An Experimental Study on the Dynamic Characteristics of Rubber Isolator (실험에 의한 방진고무의 동특성에 관한 연구)

  • Kim, W.D.;Kim, K.S.;Kwon, J.D.;Woo, C.S.
    • Elastomers and Composites
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    • v.37 no.3
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    • pp.183-191
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    • 2002
  • Rubber materials with excellent damping property are widely applied for vibration isolators. The dynamic characteristics of the rubber materials for vibration isolators were investigated. Dynamic tests for rubber materials with five different hardness were performed. In dynamic tests for test specimen, non-resonance method was used to obtain the dynamic storage modulus and loss factor. Moreover, the effect of dynamic vibration frequency, strain amplitude and temperature were investigated. As results, the storage modulus and loss factor generally increase when the hardness and frequency increase, and the glass transition temperature is $-50^{\circ}C$ by a large change in modulus and loss factor.

Numerical Study on Flow and Heat Transfer Characteristics of Pipes with Various Shapes (파이프 형상에 따른 내부 열유동 특성과 성능에 관한 수치해석적 연구)

  • Park, Sang Hyeop;Kim, Sang Keun;Ha, Man Yeong
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.37 no.11
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    • pp.999-1007
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    • 2013
  • The present work reports numerical results of the pressure drop and heat transfer characteristics of pipes with various shapes such as circular, elliptical, circumferential wavy and twisted using a three-dimensional simulation. Numerical simulations are calculated for laminar to turbulent flows. The fully developed flow in pipes was modeled using steady incompressible Reynolds-averaged Navier-Stokes (RANS) equations. The friction and Colburn factor of each pipe are compared with those of a circular tube. The overall flow and heat transfer calculations are evaluated by the volume and area goodness factor. Finally, the objective of the investigation is to find a pipe shape that decreases the pressure loss and increases the heat transfer coefficient.

Enhanced Dispersive Packetization Scheme for Reliable Transmission of wavelet Image (신뢰성 있는 웨이블릿 이미지 전송을 위한 패킷타이징 기법)

  • 장신애;이주경;정기동
    • Proceedings of the Korean Information Science Society Conference
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    • 2002.10e
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    • pp.475-477
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    • 2002
  • 이미지 압축을 위한 새로운 기법 중의 하나가 웨이블릿 변환이다. 웨이블릿 변환된 이미지는 이미지 전체의 중요 정보가 한쪽으로 치우치는 경향을 보인다. 그러므로 웨이블 이미지를 순차적으로 네트웍상에 전송한다면 중요 정보가 포함된 패킷에 손실이 발생할 경우 이미지의 품질에 치명적인 영향을 미친다. 본 논문에서는 전송된 웨이블릿 이미지의 품질을 보장하기 위한 새로운 패킷타이징 기법을 제안한다. 즉 주파수 부대역(frequency subband)을 여러 개의 블록으로 나누고, 이 블록들을 서로 다른 패킷에 삽입하여 패킷의 중요도를 분산하는 것이다. 또한 주파수대역이 가장 낮은 부대역 정보를 중복하여 전송함으로써 이미지 전체의 품질을 보장한다. 제안된 기법의 성능을 평가하기 위해 객관적인 성능평가 단위인 PSNR과 주관적인 이미지 분석을 수행하였다. 실험결과 제안된 기법의 성능이 순차적인 블록 패킷 기법에 비하여 PSNR에서 1~4 ㏈ 높았으며, 이미지의 선명도도 높음을 알 수 있었다.

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Development & Operation of Integrated Technical Information System (통합기술정보시스템(ITIS)의 개발 및 운용)

  • Chung, Joon-Young;Lee, Joon-Woo;Kim, Cheon-Young;Lee, Sang-Bum
    • Proceedings of the Korea Information Processing Society Conference
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    • 2003.05b
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    • pp.859-862
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    • 2003
  • 지금까지의 기술자료관리는 수작업의 비효율성과 복잡한 절차로 인해 업무의 시간 손실을 발생시켜 왔다. 대용량 저장장치, 그래픽 디스플레이 및 네트워킹 같은 정보기술 진보는 효과적인 전자문서 처리를 가능하게 했다. 본 논문에서 기술하고자하는 XKO-1의 통합기술 정보시스템 모델은 방대한 문서 데이터베이스를 개발하고 XKO-1 항공기의 도면, 기술문서 및 비행시험 자료의 관리와 처리를 지원하기 위한 기술을 보여주기 위한 것이다. 또한 ITIS 프로그램은 워크플로우를 이용한 문서저장기능과 스캐너를 사용해서 문서를 디지탈화, 전자화, 색인화 및 압축화하여 데이터베이스에 저장할 뿐만 아니라, 프로세스에 따라 검색 및 분배된다.

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