• 제목/요약/키워드: Residual space

검색결과 303건 처리시간 0.022초

CCD 잔존영상 분석 (A STUDY OF RESIDUAL IMAGE IN CHARGED-COUPLED DEVICE)

  • 진호;이충욱;김승리;강용범;구재림;한원용
    • Journal of Astronomy and Space Sciences
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    • 제22권4호
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    • pp.483-490
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    • 2005
  • CCD 영상센서의 경우 포화 상태를 초과하는 막대한 양의 광자가 조사될 때 $Si-SiO_2$ 접합 면에서 전하가 포획될 순 있으며 이 접합 면에 남아 있는 전하와 관련되어 잔존영상이 보일 수 있다. 이러한 잔존영상은 특히 전면조사 방식의 CCD에서 일어난다. 이 현상이 정밀 측광에 영향을 줄 수 있음에도 불구하고 잔존영상에 대한 정량적인 분석과 보고간 국내에서는 찾아보기 힘들었다. 이에 본 연구에서는 전면조사 방식의 CCD를 사용하는 레몬산천문대 관측자료의 암전자화면에서 잔존영상을 확인하고 잔존영상이 관측에 미칠 수 있는 영향을 분석해 보았다.

버스의 승객안전도 평가방법 연구 (Investigation of Evaluation Method for Bus Occupant Safety)

  • 신재호
    • 자동차안전학회지
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    • 제12권4호
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    • pp.54-60
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    • 2020
  • In a previous study, an investigation of occupant behaviors and injuries (to the head and chest) was performed during vehicle impact loading cases in order to ensure the safety of wheelchair passengers on a bus. The computational results showed overall safety tolerances of wheelchair occupants under different accident configurations. The bus crashworthiness is described as the capability of a bus to protect occupants during rollover loadings. The residual space containing occupants should be undamaged without any intrusions. However it is necessary to evaluate the residual space according to the bus occupant kinematic analysis under the rollover crash simulation. This study focuses on the evaluation of occupant behaviors during rollover loading cases in order to ensure the safety of bus passengers sitting in general seats and wheelchairs and evaluates the residual space of the bus by analyzing the bus occupant kinematics.

Residual Polar Motion excluding Chandler and Annual components

  • Na, Sung-Ho;Baek, Jeong-Ho;Kwak, Young-Hee;Yoo, Sung-Moon;Cho, Jung-Ho;Cho, Sung-Ki;Park, Jong-Uk;Park, Pil-Ho
    • 한국우주과학회:학술대회논문집(한국우주과학회보)
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    • 한국우주과학회 2011년도 한국우주과학회보 제20권1호
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    • pp.22.1-22.1
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    • 2011
  • Two dominant components of polar motion are the Chandler and the annual components. Recently, the existence of 500-day period component in the Earth's polar motion has been manifested. But its existence is not clear on Fourier spectrum. One cause of difficulty involved here is that the amplitudes of the two main components are slightly variable in time by certain amounts (Chandler: 0.15~0.28 arcsec, annual: 0.09~0.15 arcsec). A residual polar motion time series excluding the two main components for a time span between 1962 Jan and 2010 Nov from IERS C04 time series dataset was constructed by least square fitting. For faithful fitting, 43 time segments of 6.8 year length (each starts on January 1st of successive years) were separately acquired and later combined together. The period of dominant peak in the spectrum of this residual polar motion time series is 490 days. Next peaks have their periods as semi-annual, 300~330 days, ~560 days, 670 days, and 1360 days.

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Validation on Residual Variation and Covariance Matrix of USSTRATCOM Two Line Element

  • Yim, Hyeon-Jeong;Chung, Dae-Won
    • Journal of Astronomy and Space Sciences
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    • 제29권3호
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    • pp.287-293
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    • 2012
  • Satellite operating agencies are constantly monitoring conjunctions between satellites and space objects. Two line element (TLE) data, published by the Joint Space Operations Center of the United States Strategic Command, are available as raw data for a preliminary analysis of initial conjunction with a space object without any orbital information. However, there exist several sorts of uncertainties in the TLE data. In this paper, we suggest and analyze a method for estimating the uncertainties in the TLE data through mean, standard deviation of state vector residuals and covariance matrix. Also the estimation results are compared with actual results of orbit determination to validate the estimation method. Characteristics of the state vector residuals depending on the orbital elements are examined by applying the analysis to several satellites in various orbits. Main source of difference between the covariance matrices are also analyzed by comparing the matrices. Particularly, for the Korea Multi-Purpose Satellite-2, we examine the characteristics of the residual variation of state vector and covariance matrix depending on the orbital elements. It is confirmed that a realistic consideration on the space situation of space objects is possible using information from the analysis of mean, standard deviation of the state vector residuals of TLE and covariance matrix.

사진 측량법을 이용한 버스 차체 전복 시험 (Bus Body Rollover Test using Photogrammetry)

  • 정태은;이용래
    • 한국자동차공학회논문집
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    • 제5권6호
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    • pp.28-35
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    • 1997
  • Occupant injuries are always possible in a rollover accident, one of the major accidents in a bus. Thus the structure of body frame should have sufficient strength to protect passengers under accidental loads,. ECE(Economic Commission for Europe) regulation No.66 prescribes that residual space shall be preserved in the passenger compartment during and after the structure has been subjected to the prescribed rollover test. Rollover test on a bus section was completed according to the regulation. The coordinates of body section before and after rollover were measured, and it was checked that the structure still complied with the requirements of residual space. Direct measurement on a bus is difficult because of its large size. Thus photogrammetry by photographing and 3 dimensional digital modeling was introduced, and the coordinates of each point were measured through this method.

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대형 버스의 전복 해석과 측정법 (Rollover Analysis and Measurement of a Large-sized Bus)

  • 정태은
    • 한국자동차공학회논문집
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    • 제5권6호
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    • pp.148-154
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    • 1997
  • The safety problems of buses have been arisen due to the increasing of road traffic. Occupant injuries are always possible in the rollover accident and the frontal impact. Thus the structure of bus should have sufficient strength to protect passengers under accidental loads. ECE(Economic Commission for Europe) regulation No.66 prescribes that the superstructure of the vehicle shall be sufficient strength for passengers' surviving and the residual space shall be preserved in the passenger compartment during and after the standard rollover accident situation. Rollover test and simulation on a large-sized bus was completed according to the regulation. The coordinates of the points on the bus were measured by photogrammetry system. The rollover situation was revived by structural crashes simulation software, PAM-CRASH, and it was checked that the structure still complied with the requirements of residual space during rollover situation. The residual space was preserved during rollover, so it was proved that the structure of the investigated bus had much probability of survival in rollover accidents.

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Experimental Study of Large-amplitude Wavefront Correction in Free-space Coherent Optical Communication

  • Guo, Qian;Cheng, Shuang;Ke, Xizheng
    • Current Optics and Photonics
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    • 제5권6호
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    • pp.627-640
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    • 2021
  • In a free-space coherent optical communication system, wavefront distortion is frequently beyond the correction range of the adaptive-optics system after the laser has propagated through the atmospheric turbulence. A method of residual wavefront correction is proposed, to improve the quality of coherent optical communication in free space. The relationship between the wavefront phase expanded by Zernike polynomials and the mixing efficiency is derived analytically. The influence of Zernike-polynomial distortion on the bit-error rate (BER) of a phase-modulation system is analyzed. From the theoretical analysis, the BER of the system changes periodically, due to the periodic extension of wavefront distortion. Experimental results show that the BER after correction is reduced from 10-1 to 10-4; however, when the closed-loop control algorithm with residual correction is used, the experimental results show that the BER is reduced from 10-1 to 10-7.

Quantification and location damage detection of plane and space truss using residual force method and teaching-learning based optimization algorithm

  • Shallan, Osman;Hamdy, Osman
    • Structural Engineering and Mechanics
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    • 제81권2호
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    • pp.195-203
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    • 2022
  • This paper presents the quantification and location damage detection of plane and space truss structures in a two-phase method to reduce the computations efforts significantly. In the first phase, a proposed damage indicator based on the residual force vector concept is used to get the suspected damaged members. In the second phase, using damage quantification as a variable, a teaching-learning based optimization algorithm (TLBO) is used to obtain the damage quantification value of the suspected members obtained in the first phase. TLBO is a relatively modern algorithm that has proved distinguished in solving optimization problems. For more verification of TLBO effeciency, the classical particle swarm optimization (PSO) is used in the second phase to make a comparison between TLBO and PSO algorithms. As it is clear, the first phase reduces the search space in the second phase, leading to considerable reduction in computations efforts. The method is applied on three examples, including plane and space trusses. Results have proved the capability of the proposed method to precisely detect the quantification and location of damage easily with low computational efforts, and the efficiency of TLBO in comparison to the classical PSO.

잔여추진제 추정을 위한 열질량법의 통계적 불확실성 분석 (Statistical Uncertainty Analysis of Thermal Mass Method for Residual Propellant Estimation)

  • 박응식;박봉규;허환일
    • 한국항공우주학회지
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    • 제43권12호
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    • pp.1116-1123
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    • 2015
  • 정지궤도위성의 수명은 추진제 잔여량에 좌우되고 정확한 잔여추진제량 측정은 조기 수명종료로 야기되는 경제적 손실을 완화시킬 뿐만 아니라 후속위성의 대체나 위성망 운용계획 등에 매우 중요하다. 본 논문에서는 열질량법과 그 불확실성 추정방법에 대한 기본이론에 대해 소개한다. 열질량법 잔여추진제 분석은 무궁화위성 데이터를 기초로 분석하였고 이러한 열질량법 불확실성 분석은 몬테카를로 방법을 사용하여 수행하였다. 이러한 연구 결과를 통해 열질량법을 사용한 잔여추진제 추정의 중요 파라미터를 알 수 있다.

섬유금속적층판의 경화 시 발생하는 열 잔류응력에 관한 연구 (Thermal residual stress behavior in fiber metal laminates)

  • 김세영;최원종;박상윤;문초록
    • 한국항공우주학회지
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    • 제33권6호
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    • pp.39-44
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    • 2005
  • 섬유금속적층판(Fiber Metal Laminates, 이하 FML)에서 알루미늄과 유리섬유/에폭시 복합재료 사이의 열팽창 계수의 차이는 경화공정 시 FML내부에 열 잔류응력을 남기게 되며, 이러한 열 잔류응력은 FML의 피로특성과 항복강도에 영향을 주게 된다. 잔류응력을 예측하기 위해 두 가지 실험법이 제안 되었으며, 이론식을 통해 그 결과를 예측하고, 실제 실험을 수행하여 그 값을 확인 하였다. 또한, 열 잔류응력의 제거 및 응력의 역전을 위하여 후-인발 가공이 수행 되었으며, 가공 이후 발생한 FML내의 잔류응력이 측정 되었다. 예측된 열 잔류응력 결과와 실험을 통한 값이 일치함을 보이며, 후-인발 가공을 통하여 열 잔류응력 제거 및 항복강도의 증가가 발생하였다.