• Journal of Astronomy and Space Sciences
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• 제25권3호
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• pp.321-328
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• 2008

위성 온-보드 소프트웨어 중 새로 개발되거나 일부분이 변경된 소프트웨어의 성능을 검증하기 위해서 요구되는 소프트웨어 테스트 벤치는 실제 구동환경을 가능한 가깝게 묘사하여야 하며 특히 결함 검출 및 복구 성능 검증에 대한 시험 환경을 충분히 제공하여야 한다. 실시간적인 성능 시험을 제외하면 프로세서 에뮬레이터 기반의 시뮬레이션 소프트웨어 테스트 벤치는 매우 매력적인 소프트웨어 성능 검증 환경을 하드웨어 소프트웨어 테스트 벤치보다 앞서 제공하는 것이 가능하다. 이 논문에서는 시뮬레이션 소프트웨어 테스트 벤치를 개발하기 위한 개념 연구 결과를 제시하고 있다.

• Journal of Astronomy and Space Sciences
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• 제28권3호
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• pp.241-252
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• 2011

A simulated network protocol provides the capability of distributed simulation to a generic simulator. Through this, full coverage of management of data and service handling among separated simulators is achieved. The distributed simulation environment is much more conducive to handling simulation load balancing and hazard treatment than a standalone computer. According to the simulated network protocol, one simulator takes on the role of server and the other simulators take on the role of client, and client is controlled by server. The purpose of the simulated network protocol is to seamlessly connect multiple simulator instances into a single simulation environment. This paper presents the development of a simulated network (simNetwork) that provides the capability of distributed simulation to a generic simulator (GenSim), which is a software simulator of satellites that has been developed by the Korea Aerospace Research Institute since 2010, to use as a flight software validation bench for future satellite development.

• Journal of Astronomy and Space Sciences
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• 제27권4호
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• pp.407-412
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• 2010

Software reusability is one of key factors which impacts cost and schedule on a software development project. It is very crucial also in satellite simulator development since there are many commercial simulator models related to satellite and dynamics. If these models can be used in another simulator platform, great deal of confidence and cost/schedule reduction would be achieved. Simulation model portability (SMP) is maintained by European Space Agency and many models compatible with SMP/simulation model interface (SMI) are available. Korea Aerospace Research Institute (KARI) is developing hardware abstraction layer (HAL) supported satellite simulator to verify on-board software of satellite. From above reasons, KARI wants to port these SMI compatible models to the HAL supported satellite simulator. To port these SMI compatible models to the HAL supported satellite simulator, simulation scheduler is preliminary designed according to the SMI standard.

• 열처리공학회지
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• 제9권3호
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• pp.169-176
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• 1996

Effect of retained austenite on rolling contact fatigue of nitrocarburized high-carbon chromium bearing steel has been investigated to develop surface-hardened bearing steel with imprved resistance to rolling contact fatigue. Fatigue tests were conducted in elesto-hydrodynamic lubricating conditions at a shaft speed of 5,000rpm, under max, hertzian stress of $492kg/mm^2$. Volume fraction of retained austenite in austenitic nitrocarburized STB2 steel was controlled by tempering at various temperature, $200{\sim}250^{\circ}C$. It was observed using TEM that decomposition of retained austenite during tempering at $250^{\circ}C$ was the highest in quantity, resulted in formation of lower bainite. Rolling contact fatigue life of the specimens with lower bainite, formed by decomposition of retained austenite, was improved in comparison with there of specimens with more amount of retained austenite.

• 한국자기학회지
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• 제17권4호
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• pp.166-171
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• 2007

단결정 Bi단일 나노선의 정상 자기 저항(ordinary magnetoresistance) 특성을 $2{\sim}300K$에서 4 단자법으로 측정하였다. I-V 측정을 통해 전기적 오믹 형성을 확인하였고, 2 K과 300 K에서 비저항이 각각 $1.0{\times}10^{-4}$와 $8.2{\times}10^{-5}{\Omega}{\cdot}cm$으로 측정되었다. 수직(transverse) 및 수평(longitudinal) 자기저항비(MR ratio)가 110 K와 2 K에서 각각 현재까지 보고된 MR 중 가장 큰 2496%와 -38%으로 관찰되었으며, 이 결과는 자발 성장법으로 성장된 Bi 나노선의 결정성이 매우 우수한 단결정임을 증명한다. simple two band(STB) 모델을 통해 Bi 나노선의 수직 및 수평 정상 자기 저항(OMR) 거동이 온도에 따른 페르미 준위(Fermi level)와 밴드 겹침(band overlap)등의 전자 구조 변화 및 운반자 농도 변화로 잘 설명된다.