• 제목/요약/키워드: Correction coefficient method

검색결과 183건 처리시간 0.021초

조직 정량화를 위한 의용 초음파 영상 기술 개발(감쇠계수 측정에서 회질 영향의 보정법) (Development of Medical Ultrasound Imaging Techniques for Tissue Characterization (The Correction Method of Diffraction Effect in Measurements of Attenuation Coefficient))

  • 한성현;이강호;최종호;최종수
    • 대한전자공학회논문지
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    • 제27권12호
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    • pp.1925-1932
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    • 1990
  • In this paper, we consider the effect of diffraction due to the finite-sized aperture and propose the new correction method of errors in measurements of attenuation coefficient owing to the diffraction effect. In the existing correction method, we obtained the attenuation coefficient after correct the spectrum at each depth. However, this paper obtain the attenuation coefficient using lg-spectral difference approach and then correct errors. As a proposed method is not correction for the spectrum at each depth but the difference spectrum, we reduce the calculation. Also the correction is performed through the total frequency range, the accurate attenuation coefficient in whole bandwidth is produced.

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초소형 비행체 하중해석을 위한 공력보정 (Aerodynamic Corrections for Load Analysis of Micro Aerial Vehicle)

  • 구교남
    • 한국항공우주학회지
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    • 제33권6호
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    • pp.31-38
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    • 2005
  • 하중해석을 위한 선형 패널법에서 압력과 다운워시와의 관계는 공력영향계수로 표현되며 점성 효과는 무시되고 천음속 영역에서 압축성 효과를 적절히 표현하지 못한다. 공력영향계수는 공력면의 평면형상에 의해 결정되므로 저 레이놀즈 수의 유동의 특성을 나타내는 데는 한계가 있다. 따라서 공력계수의 시험치를 구속조건으로 하여 압력분포를 직접 보정하거나 다운워시를 보정하여 유효 캠버나 두께를 반영하여 압력분포를 보정하게 된다. 본 논문에서는 전승보정방법과 후승보정방법을 초소형 비행체의 균형해석 및 하중해석을 위한 공기력 보정에 적용하였다. 이론적인 공기력은 패널법을 이용하였으며 단일 구속조건과 이중 구속조건을 적용하여 보정행렬과 보정된 압력계수를 구하였다. 초소형 비행체의 공력보정에 있어서 비행영역의 특성으로 인해 후승보정방법이 보다 나은 결과를 나타내었다.

COMPARISON OF ATMOSPHERIC CORRECTION ALGORITHMS FOR DERIVING SEA SURFACE TEMPERATURE AROUND THE KOREAN SEA AREA USING NOAA/AVHRR DATA

  • Yoon, Suk;Ahn, Yu-Hwan;Ryu, Joo-Hyung;Won, Joong-Sun
    • 대한원격탐사학회:학술대회논문집
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    • 대한원격탐사학회 2007년도 Proceedings of ISRS 2007
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    • pp.518-521
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    • 2007
  • To retrieve Sea Surface Temperature(SST) from NOAA-AVHRR imagery the spilt window atmospheric correction algorithm is generally used. Recently, there have been various new algorithms developed to process these data, namely the variable-coefficient split-window, the R54 transmittance-ratio method, fixed-coefficient nonlinear algorithm, dynamic water vapour (DWV) correction method, Dynamic Water Vapour and Temperature algorithm (DWVT). We used MCSST (Multi-Channel Sea surface temperature) and NLSST(Non linear sea surface temperature) algorithms in this study. The study area is around the Korea sea area (Yellow Sea). We compared and analyzed with various methods by applying each Ocean in-situ data and satellite data. The primary aim of study is to verify and optimize algorithms. Finally, this study proposes an optimized algorithm for SST retrieval.

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아음속 익형 풍동시험 전산해석 (CFD ANALYSIS OF SUBSONIC AIRFOIL WIND TUNNEL TEST)

  • 김철완;이융교
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2007년도 추계 학술대회논문집
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    • pp.167-170
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    • 2007
  • In the present paper, wall correction method is reviewed and applied to the numerical experimental results obtained at the wind tunnel condition. The corrected lift coefficient agrees well with the reference data generated from the grid having very far boundary. However the corrected drag coefficient presents some deviation from the reference data.

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최적화기법을 이용한 고속 탄성회전체의 밸런싱 (An Optimal Correction Balancing of A High-Speed Flexible Rotor)

  • 이용복;이동수;최동훈
    • 대한기계학회논문집
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    • 제19권6호
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    • pp.1402-1410
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    • 1995
  • An influence coefficient method with an optimal correction balancing algorithm is developed for balancing a high-speed flexible rotor system. Conventional flexible balancing algorithms such as least square and weighted least square algorithms may not satisfy allowable residual vibration levels in certain speed ranges, while the optimal correction balancing method can be more effective in controlling vibration levels in a target speed. Related analyses were reviewed and applied to a test rig to show the effectiveness of the optimal correction balancing method.

폐쇄형 풍동 시험부 내의 비정상 흐름에 대한 Blockage 보정 기법 연구 (Blockage-Correction Method for Unsteady Flows in a Closed Test-Section Wind Tunnel)

  • 강승희;권오준;안승기
    • 한국항공우주학회지
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    • 제34권12호
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    • pp.67-74
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    • 2006
  • 아음속풍동 폐쇄형 시험부내의 비정상 벽면효과 보정 연구의 일환으로 시험부 벽면압력을 사용하는 비정상 흐름에 대한 blockage 보정 기법을 개발하였다. 시험부 벽면압력은 프리에 급수로 전개하고, 전개된 각 계수를 벽면압력측정 방법을 사용하여 전 주기에 대해 일괄적으로 보정하는 준 정상상태 보정 방법을 제시하였다. 본 연구에서 제시된 방법을 검증하기 위해 수치적으로 계산된 폐쇄형 시험부내의 원형실린더 및 강제 진동하는 익형의 비정상 흐름에 적용하였다. 그 결과 본 연구에서 제시된 방법은 자유흐름 상태와 일치되는 blockage 보정 결과를 보임을 확인하였다.

Ricean Bias Correction in Linear Polarization Observation

  • Sohn, Bong-Won
    • Journal of Astronomy and Space Sciences
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    • 제28권4호
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    • pp.267-271
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    • 2011
  • I developed an enhanced correction method for Ricean bias which occurs in linear polarization measurement. Two known methods for Ricean bias correction are reviewed. In low signal-to-noise area, the method based on the mode of the equation gives better representation of the fractional polarization. But a caution should be given that the accurate estimation of noise level, i.e. ${\sigma}$ of the polarized flux, is important. The maximum likelihood method is better choice for high signal-to-noise area. I suggest a hybrid method which uses the mode of the equation at the low signal-to-noise area and takes the maximum likelihood method at the high signal-to-noise area. A modified correction coefficient for the mode solution is proposed. The impact on the depolarization measure analysis is discussed.

유전 알고리즘을 이용한 회전기계의 최적 현장평형잡이 (Optimum Field Balancing of Ratating Machinery Using Genetic Algorithm)

  • 최원호;양보석;주호진
    • 대한기계학회논문집A
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    • 제20권6호
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    • pp.1819-1826
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    • 1996
  • This paper present the claculating method of optimum correction mass within permissible vibration linits for ratating machinery in two-plane field balancing. Basic technique of this method is based on influence coefficient method, and grphic vector composition that the resultant of two influence vectors obtained by trial mass have to be equilibrium with initial vibration vector in the each correction plane. Genetic algorithm which is a search algorithm based on the mechanism of natural selection and natural genetics is sued for vector composition, and SUMT method is used to objective function which seeks optimum correction mass for balancing a rotor.

유전 알고리즘을 이용한 회전기계의 최적 평형잡이 (Optimum Balancing of Rotating Machinery Using Genetic Algorithm)

  • 주호진;최원호;양보석
    • 한국지능시스템학회:학술대회논문집
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    • 한국퍼지및지능시스템학회 1995년도 추계학술대회 학술발표 논문집
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    • pp.195-202
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    • 1995
  • This paper presents the calculating method of optimum correction mass within permissible vibration limits for rotating machinery in two-plane field balancing. Basic technique of this method based on influence coefficient method, is graphic vector composition that the resultant of two influence vectors obtained by trial mass have to be equilibrium with initial vibration vector in the each correction plane. Genetic algorithm which is a search algorithm based on the mechanics of natural selection and natural genetics is used for vector composition, and SUMT method is used to objective function which seeks optimum correction mass for balancing a rotor.

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수정된 방사 에너지법과 단파장 영역 보정법을 이용한 파랑 중 부가저항 추정에 관한 연구 (A Study on Estimation of Added Resistance in Waves Using Modified Radiated Energy Method and Short Wave Correction Method)

  • 오승훈;양진호
    • 대한조선학회논문집
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    • 제53권1호
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    • pp.62-68
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    • 2016
  • A simple calculation tool for added resistance in waves is developed to utilize for initial design or embedded module for navigation support system. In order to select an appropriate calculation method for added resistance in waves, three methods (drift method, integrated pressure method, radiated energy method) based on strip method are applied to Wigley I and KVLCC2. The methods for added resistance in waves give the underestimated results because it is difficult to consider nonlinear effects due to reflected wave. We apply asymptotic (Faltinsen's method) and empirical formula (NMRI's method) to improve the accuracy for short wave length region. In comparison with experimental results, the combination of radiated energy method and short wave correction method of NMRI is the most reasonable. However, a simple sum of results calculated by two methods gives rise to the overestimation of added resistance for short wave length region because added resistance of radiated energy method exits in total reflection region. To overcome this problem, modified radiated energy method is proposed using correction coefficient defined by reflection coefficient of NMRI's method. Finally, added resistance in regular waves is composed of added resistance of modified radiated energy method and that of short wave correction method of NMRI. Estimated added resistance in regular waves is validated by comparison with experimental results of other research groups.