• 한국산학기술학회논문지
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• 제20권9호
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• pp.397-404
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• 2019

무기체계 연구개발 시, 실제 환경에서의 기간, 안전, 비용 등의 사유로 시험평가가 제한되는 항목에 대해 M&S(Modeling and Simulation)를 활용하여 시험평가를 실시할 수 있다. 이때 시험평가용 M&S의 신뢰성(credibility) 확보를 위해 VV&A(Verification, Validation and Accreditation) 활동이 요구된다. 최근 무기체계의 연구개발 경향이 첨단화됨에 따라 M&S 활용과 이에 따른 VV&A 활동도 증가되고 있다. VV&A 활동이란 시험평가용 M&S가 실체계의 모습대로 구현되고, 사용 목적과 의도에 대한 신뢰성이 보장되었는지 검증(verification), 확인(validation)하여, 인정(accreditation)하는 것이다. VV&A 활동은 V&V(Verification & Validation)와 인정 활동으로 나뉜다. 국방과학연구소(이하, 국과연)에서 시험평가용 M&S의 VV&A를 수행할 시, V&V 활동을 수행하는 V&V에이전트는 국과연의 별도부서가 수행하고 인정 활동을 수행하는 인정(A)에이전트는 기품원이 수행한다. 본 논문은 현재까지 국과연에서 V&V에이전트로 수행한 시험평가용 M&S VV&A에 적용된 V&V 활동 프로세스 적립 결과를 소개한다. 이는 시험평가용 M&S의 개발과정에서 산출되는 각종 문서 및 개발 자료 등을 인정평가 항목의 관점에 따라 검증 및 확인을 하여, 인정판정 및 수락기준 충족여부를 판단할 수 있는 객관적인 근거 자료를 만들기 위해 수행한 프로세스이다.

• 한국컴퓨터정보학회논문지
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• 제28권9호
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• pp.177-188
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• 2023

본 연구의 목적은 디지털 리터러시의 구성요인을 확인하고 요인별 문항들을 추출하여 디지털 리터러시 측정을 위한 척도를 개발, 타당화하는 것이다. 선행연구 분석과 연구진의 숙의을 통하여 예비문항들을 개발하여 2차례에 걸쳐 전문가 델파이 조사를 실시한 결과, 본조사를 위한 65개의 문항이 선정되었다. 문항의 타당화 작업은 본조사로 수집된 데이터에 대한 탐색적, 확인적 요인분석과 신뢰도 검사 및 준거타당도 검증의 과정으로 진행되었다. 그 결과, 31문항으로 구성된 4요인 구조(1요인: 디지털 테크놀로지 & 데이터 리터러시-9문항, 2요인: 디지털 콘텐츠 & 미디어 리터러시-8문항, 3요인: 디지털 커뮤니케이션 & 공동체(Community) 리터러시-9문항, 4요인: 디지털 웰니스 리터러시-5문항)를 확인하였으며, 모델의 적합도 지수들이 양호한 것으로 나타났고, 척도의 신뢰도 Cronbach's alpha도 .956으로 매우 적절한 수준으로 평가되었다. 또한, 기존 근거에서 디지털 리터러시와 상관관계에 있을 것으로 예측되었던 인터넷자기효능감과 자기주도학습능력이 통계적으로 유의미한 정적 상관관계(p<.001)로 나타나 개발된 척도의 준거타당도가 확보되었다. 마지막으로, 연구의 실천적, 학문적 함의와 후속연구에 대한 제언 및 한계점이 제공되었다.

• Structural Engineering and Mechanics
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• 제11권3호
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• pp.325-340
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• 2001

This paper addresses an efficient modification method that eliminates the undesirable effects of strains due to various non-conforming modes so that the non-conforming element can pass the patch test unconditionally. The scheme is incorporated in the element formulation to establish new types of non-conforming hexahedral elements designated as NHx and NVHx for the regular element and variable node element, respectively. Non-conforming displacement modes are selectively added to the ordinary (conforming) element displacement assumptions to improve the bending behavior of the distorted solid element. To verify the validation of proposed direct modification method and the improvement of element behavior, several numerical tests are carried out. Test results show that the proposed method is effective and its applications to non-conforming solid elements guarantee for the element to pass the patch test.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2004년도 추계학술대회
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• pp.1564-1568
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• 2004

The requirements of internal balance were studied that should be considered on performing force & moment transonic wind tunnel testing to develop combat aircraft. In many insecure factors of test condition, uncertainty analysis was conducted to verify one drag count measurements. The analysis result was applied to T-50 aircraft model and compared for data verifaction. In conclusion, the aerodynamicist should estimate the validation and accuracy of test data by having an overall grasp of system components including internal balance. It will help him get high productivity of testing and effective validated data at tunnel.

• 한국자동차공학회논문집
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• 제18권5호
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• pp.56-61
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• 2010

This paper presents dynamic clearance verification considering engine movement for vehicle engine room package and validates through physical vehicle test. Traditionally, static clearance guide has been used for engine room package, but it's only 2-dimension criteria that results in requiring unnecessary space and it's not possible to conduct engine movement with real driving conditions. Thus, the dynamic DMU considers engine movement based on 28 load cases that are Roll Data analyzed by CAE for maximum engine movement and visualizes part-to-part dynamic clearance into virtual space. The dynamic DMU enables to develop compact engine room package without unnecessary space. The result of comparison between simulation and physical test has 0.892 correlation coefficient.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2007년도 추계학술대회논문집
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• pp.92-96
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• 2007

Microphone array beamforming method has been recognized as an important aeroacoustic research field and become a standard technique in localizing sound sources. This method also used in flight acoustic measurement, and especially, it is very useful when measure sounds inside the wind tunnel. In measuring sound which is inside the wind tunnel by traditional beamforming method, there are some errors caused by airstream. The speed and the propagation path of the sound changes as it travel through the airstream. This makes the error which the position of sound is changed a little bit to the down stream direction. In this paper, validation test has made about the correction equation for this wind effects of previous researches. And beamforming including shear layer correction was performed about a sound source in the anechoic open-jet windtunnel.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2007년도 춘계학술대회A
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• pp.855-860
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• 2007

This paper describes a human driver model developed based on finite preview optimal control method. The human driver steering model is constructed to minimize a performance index which is a quadratic form of lateral position error, yaw angle error and steering input. Simulation studies are conducted using a vehicle simulation software, Carsim. The Carsim vehicle model is validated using vehicle test data. In order to validate the human driving steering model, the human driver steering model is compared to the driving data on a virtual test track(VTT) and the actual vehicle test data. It is shown that human driver steering behaviors can be well represented by the human driver steering model presented in this paper

• 한국위성정보통신학회논문지
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• 제2권2호
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• pp.36-40
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• 2007

EGSE is used to check out satellite payload during the development prior to launch. The EGSE represented in this paper is a test system for Ka band communication transponder of COMS. The EGSE consist of two subsystems as CTS subsystem and PCTS subsystem. Communication Test subsystem (CTS) performs satellite transponder RF performance testing, data analysis and trending. Most of transponder RF performances are automatically tested by the CTS subsystem. Power, Command & Telemetry subsystem (PCTS) monitor telemetry messages from the transponder and send tele-commands to satellite transponder for the configuration change. PCTS also provide simulated S/C power to the transponder during the ground validation testing. The EGSE test functions are verified by the transponder simulator testing and will be used for the flight model transponders testing.

• 대한전기학회:학술대회논문집
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• 대한전기학회 2006년도 추계학술대회 논문집 전력기술부문
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• pp.237-239
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• 2006

The residual flux(${\psi}_r$) in transformer's iron cores cause the distortion of short-circuit current occasionally. And some considerable distortion effect on the validation of test results. To prevent this situation, there needs some suitable control of residual flux through the pretest. This paper deals with the how to control the residual flux in pretest and the comparison between the two test results which were obtained by different test method.

• 한국소음진동공학회논문집
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• 제16권7호
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• pp.677-682
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• 2006

In the case of aeroacoustic test in windtunnel, measurement accuracy is reduced by not only Doppler effects but also by the microphone self noise due to airflow and high turbulence in the wall boundary layer. Microphone array measurements can be easily utilized for the solutions of these problems. In this paper, geometrical optics approach and diagonal term elimination of cross spectral matrix was introduced to the de-dopplerization and self noise reduction methods for the microphone array measurement. For the validation, beamforming tests for sinusoidal point source were performed in the closed type test section of windtunnel, and their performances of beam width and sidelobe rejection were significantly improved.