• 제목/요약/키워드: Test Design

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A Study of the Effects on Applying Test Design to Information Communication Authority Module

  • Jang, Jinwook
    • 한국정보기술학회 영문논문지
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    • 제8권2호
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    • pp.111-118
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    • 2018
  • Information communication authority module software contains various functions and services. A software test is the only acceptance test step. Recently, however, all development steps have become important. In particular, the software acceptance step is very high, and a study of the effective use of limited time and resources on acceptance step is needed. This study examined the efficiency of the Test Design Technique for Software Test. The proposed Test Design process was applied to the domain systems of info-communication and the degree of improvement was measured. This paper establishes Software Test design process Infrastructure based on the developed software.

연속형 시스템의 신뢰성 성장 관리 시험 설계 방안 (A Method of Reliability Growth Management Test Design for Continuous System)

  • 서양우;윤정환;이승상;엄천섭
    • 시스템엔지니어링학술지
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    • 제16권2호
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    • pp.87-96
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    • 2020
  • In this paper we proposed the test design method of reliability growth management. First, we presented the process for establishing the reliability growth management test design considering the number of failures and the termination test time. Reliability growth analysis of continuous system was performed in accordance with the test design process presented. In case the reliability test result is not met with the reliability target value after more than three failures occurred, the required test times were analyzed that 1,725 hrs for one corrective action, 1,950 hrs for two corrective actions. If the number of failures is less than three, design a reliability demonstration test according to confidence level 80% and 90% was performed using RGA 11 Software. As a result, it is possible to establish the reliability growth management test design with sufficient use of available resources. The results of this study can be used when establishing a test design for assessment of reliability growth management of all continuous systems.

Verification for the design limit margin of the power device using the HALT reliability test

  • Chang, YuShin
    • 한국컴퓨터정보학회논문지
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    • 제23권11호
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    • pp.67-74
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    • 2018
  • The verification for the design limit margin of the power device for the information communication and surveillance systems using HALT(Highly Accelerated Life Test) reliability test is described. The HALT reliability test performs with a step stress method which change condition until the marginal step in a design and development phase. The HALT test methods are the low temperature(cold) step stress test, the high temperature(hot) step stress test, the thermal shock cyclic stess test, and the high temperature destruct limit(hot DL) step stress test. The power device is checked the operating performance during the test. In this paper, the HALT was performed to find out the design limit margin of the power device.

Contribution of thermal-hydraulic validation tests to the standard design approval of SMART

  • Park, Hyun-Sik;Kwon, Tae-Soon;Moon, Sang-Ki;Cho, Seok;Euh, Dong-Jin;Yi, Sung-Jae
    • Nuclear Engineering and Technology
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    • 제49권7호
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    • pp.1537-1546
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    • 2017
  • Many thermal-hydraulic tests have been conducted at the Korea Atomic Energy Research Institute for verification of the SMART (System-integrated Modular Advanced ReacTor) design, the standard design approval of which was issued by the Korean regulatory body. In this paper, the contributions of these tests to the standard design approval of SMART are discussed. First, an integral effect test facility named VISTA-ITL (Experimental Verification by Integral Simulation of Transients and Accidents-Integral Test Loop) has been utilized to assess the TASS/SMR-S (Transient and Set-point Simulation/Small and Medium) safety analysis code and confirm its conservatism, to support standard design approval, and to construct a database for the SMART design optimization. In addition, many separate effect tests have been performed. The reactor internal flow test has been conducted using the SCOP (SMART COre flow distribution and Pressure drop test) facility to evaluate the reactor internal flow and pressure distributions. An ECC (Emergency Core Coolant) performance test has been carried out using the SWAT (SMART ECC Water Asymmetric Two-phase choking test) facility to evaluate the safety injection performance and to validate the thermal-hydraulic model used in the safety analysis code. The Freon CHF (Critical Heat Flux) test has been performed using the FTHEL (Freon Thermal Hydraulic Experimental Loop) facility to construct a database from the $5{\times}5$ rod bundle Freon CHF tests and to evaluate the DNBR (Departure from Nucleate Boiling Ratio) model in the safety analysis and core design codes. These test results were used for standard design approval of SMART to verify its design bases, design tools, and analysis methodology.

정보통신 소프트웨어 테스트 설계 효율성에 대한 연구 (A study of The effects on applying test design to Info-communication Software)

  • 장진욱
    • 한국산학기술학회논문지
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    • 제15권7호
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    • pp.4522-4527
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    • 2014
  • 정보통신 소프트웨어는 다양한 기능과 서비스를 포함하고 있다. 소프트웨어 테스트는 인수단계에서 구현을 확인하는 정도로 인식되었으나 최근에는 개발단계별 테스트에 대한 관심이 높아지고 있다. 특히 소프트웨어가 사용자에게 인도되는 인수단계에서의 특히 테스트의 중요성이 높다. 따라서 인수테스트 단계의 제한된 시간과 리소스를 효과적으로 사용하여 테스트하기 위한 기법과 방법에 대한 연구가 많이 이루어지고 있다. 본 논문에서는 테스트 설계기법을 이용하여 전자통신 소프트웨어에 적용하고 테스트 케이스 실행 개수와 시간을 측정하여 테스트 설계의 효율성을 측정하였다. 본 연구는 테스트 설계 및 실행과정에서 최소한의 리소스를 이용한 효과적인 테스트 실행에 기여할 것으로 본다.

비용 효과도 최적화 기반 양산 무기체계 환경 부하 선별 시험 설계 방법 (The Mass Production Weapon System Environmental Stress-Screening Test Design Method based on Cost-effective-Optimization)

  • 김장은
    • 한국신뢰성학회지:신뢰성응용연구
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    • 제18권3호
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    • pp.229-239
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    • 2018
  • Purpose: There is a difficulty in Environmental Stress Screening (ESS) test design for weapon system's electrical/electronic components/products in small and medium-sized enterprises. To overcome this difficulty, I propose an easy ESS test design approach algorithm that is optimized with only one environment tolerance design information parameter (${\Delta}T$). Methods: To propose the mass production weapon system ESS test design for cost-effective optimization, I define an optimum cost-effective mathematical model ESS test algorithm model based on modified MIL-HDBK-344, MIL-HDBK-2164 and DTIC Technical Report 2477. Results: I clearly confirmed and obtained the quantitative data of ESS effectiveness and cost optimization along our ESS test design algorithm through the practical case. I will expect that proposed ESS test method is used for ESS process improvement activity and cost cutting of mass production weapon system manufacturing cost in small and medium-sized enterprises. Conclusion: In order to compare the effectiveness of the proposed algorithm, I compared the effectiveness of the existing ESS test and the proposed algorithm ESS test based on the existing weapon system circuit card assembly for signal processing. As a result of the comparison, it was confirmed that the test time was reduced from 573.0 minutes to 517.2minutes (9.74% less than existing test time).

응력집중 저감을 위한 트랙터용 프론트 로더의 설계개선 및 충격 안전성 평가 (Design Improvement of Front-End Loader for Tractor to Reduce Stress Concentration and Evaluation of Impact Safety)

  • 이부윤
    • 한국기계가공학회지
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    • 제17권3호
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    • pp.109-119
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    • 2018
  • The purpose of this study is to evaluate the structural safety of the front-end loader for the 90 kW class of agricultural tractors in impact test conditions. Deformation and stress on the loader under the impact test conditions are analyzed using the commercial finite element analysis software ANSYS. In previous research dealing with the initial design of the loader, the maximum stress occurred in the mount and exceeded the yield strength of the material. In this paper, an improved design of the mount of the loader was proposed to reduce the stress concentration in the initial design. The safety of the improved design was verified by performing rigid-body dynamics analysis, transient structural analysis, and static structural analysis under three impact test conditions: a drop and catch test, a corner pull test, a corner push test. It was found that the local stress concentration in the mount that appeared in the initial design was greatly reduced in the improved design, and that the maximum stresses occurred in the three impact test conditions are smaller than the yield strength. It is expected that the design improvement of the mount proposed in this study and the method of analysis may be effectively used to enhance structural safety in the development of new model front loaders in the future.

외부장착물지지 주익구조 정적 시험 및 해석 (Static Test and Analysis of Wing Support Structure for External Stores)

  • 엄원섭;윤종민
    • 항공우주시스템공학회지
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    • 제9권1호
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    • pp.28-34
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    • 2015
  • Armed aircraft of a basic trainer class installs external stores under wing box by using pylon and performs an operation such as weapon delivery and jettison, and should be designed to withstand all kinds of loads applied to external stores. The static strength test of pylons and wing box was performed to assess the static strength of pylon and their support structures for substantiation. Based on the test, the structures were verified to fully satisfy a given design requirement. In this paper, methods of test load generation of wing box and pylon, evaluation of test result data and design result of test set-up were presented. Comparing the FEM analysis with the same test data can lead to good match and reasonable deviation between both. Finally, based on the test and the analysis, the static strength of test article was substantiated and the reliability and effectiveness of analysis math model were obtained.

헬리콥터 로터시스템 회전시험설비의 설계 (Design of Whirl Tower Test Facility for Helicopter Rotor System)

  • 김승범;송근웅;최희주;김은종;박병관
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2008년도 추계학술대회A
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    • pp.1136-1141
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    • 2008
  • The helicopter rotor system generates lift, thrust, maneuvering force and moment to the helicopter with the torque and pitch control force transferred from the main rotor hub/control. And the tail rotor system generates the thrust for yaw axis control of the helicopter with the torque and pitch control force transferred from the tail rotor hub/control. Ground whirl test shall be performed to verify the compliance of requirement performance test and dynamic test of rotor blade and hub/control. This paper describes a design of whirl tower test facility for helicopter rotor system test and evaluation. Design results are summarized and compared with design requirements.

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