• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2005년도 춘계학술대회논문집
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• pp.809-812
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• 2005

This paper explains environmental tests of vessel-launched missiles, verifying if a fully assembled missile performs properly from disturbance on delivery by vehicles or naval vessels. We also have operated vibration tests by ground and naval transportation as well as shock tests by naval transportation before firing. The environmental tests have adopted Military Standard Specification and confirmed missile's reliability by performance tests, followed by missile's development. However, this significant testing which have meaning was dong by the missile's body and not with parts.

• 대한전자공학회논문지SD
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• 제45권2호
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• pp.140-149
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• 2008

서비스 기반 아키텍처(Service-Oriented Architecture;SOA) 등장 이후 서비스와 애플리케이션을 상호 연결하는 측면에서 여러 가지 접근 방법들이 개발되고 있다. 모바일과 같은 정보기기는 일반적인 접근법이나 전통적인 접근법과는 달리 메모리와 프로세스 등 단말기 자체의 제약과 스크린 및 입출력 및 사용자 인터페이스의 제약이 많아 여러 가지가 고려되어 설계되어야 한다. 본 연구는 서비스를 기반으로 한 구조에서 많은 제약을 갖는 모바일의 효율성을 높이기 위해 모바일 애플리케이션 요구 사항을 분석하고 명세한 후 설계 방법을 최적화하고, 서비스 유스케이스 테스팅을 위한 확장된 유스케이스 명세를 제공하고, 서비스 명세로부터 서비스간 상호운영 테스트를 한다. 또한 모바일 애플리케이션의 성능을 확장하고, 제약을 최소화 할 수 있는 과정을 제시하며 유스케이스 테스팅을 위한 명세 방법과 서비스 상호간 상호운용성 보장 테스팅을 수행한다. 본 연구는 서비스 지향 아키텍처를 기반으로 모바일 서비스 명세 방법과 애플리케이션 테스팅 방법에 대한 아이디어를 제공한다는데 그 의의가 있다.

• 대한임베디드공학회논문지
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• 제14권1호
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• pp.51-61
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• 2019

There are strict evaluation processes before using new processors to satellites. Engineers evaluate processors from various viewpoints including specification, development environment, and cost. From a viewpoint of computation power, manufacturers provide benchmark results with processors, and engineers decide which processors are adequate to their satellites by comparing the benchmark results with requirements of their satellites. However, the benchmark results depends on a test environment of manufacturers, and it is quite difficult to achieve similar performance in a target environment. Therefore, it is necessary to evaluate the processors in the target environment. This paper compares performance of a processor, AT697F/LEON2, in software testbed (STB) with three development boards of XC2V/LEON3, GR712RC/LEON3, and GR740/LEON4. Seven benchmark functions of Dhrystone, Stanford, Coremark, Whetstone, Flops, NBench, and MiBench are selected. Results are analyzed with hardware and software properties: hardware properties of core architecture, number of cores, cache, and memory; and software properties of build options and compilers. Based on the analysis, this paper describes a guideline for choosing processors for next generation satellites.

• 한국항행학회논문지
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• 제24권3호
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• pp.184-191
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• 2020

항공용 SIL은 항공전자시스템의 통합 및 검증에 사용되는 통합시험환경이다. 항공용 SIL에는 여러 가지 제약으로 인해 항공기에 탑재되는 장비를 직접 연동할 수 없을 때 장비의 소프트웨어 모델이 필요하다. 지금까지 항공기 개발에 적용한 항공용 SIL의 소프트웨어 모델은 표준화된 방법 없이 일반적인 소프트웨어 개발 방법의 적용으로 재사용이 어려워 소프트웨어 모델 재사용을 위한 프레임워크의 필요성이 제기되었다. 이러한 항공용 SIL 모델의 표준화된 모델링 방법을 위해 DEVS (discrete event system specification) 형식론을 채용하였다. DEVS 형식론은 이벤트 구동(event-driven) 알고리즘이며 이는 기존의 항공용 SIL에 적용되는 절차적이고 반복적인 알고리즘과 어울려 동작하기 힘들다. 이에 본 논문에서는 항공용 SIL 모델의 특징과 기존 방식이 가지는 한계를 보완하고 모델의 재사용성을 극대화할 수 있는 이벤트 기반의 모델링 방법과 실시간 시뮬레이션 방법을 제안한다.

• 한국군사과학기술학회지
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• 제25권4호
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• pp.329-338
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• 2022

This paper provides a case study of development testing and evaluation of design goal of Interferometric SAS (Synthetic Aperture Sonar) system that is developing supported by Civil-Military Technology Cooperation Center in offshore fields. For Deep water operating capabilities evaluation, We have surveyed candidate field, bathymetric mapping and target identification over 200 m depth, East Sea. In testing phase, We have provided environmental information of testing field include water column, seabed and weather condition in real time. And to compare excellency of developing InSAS, we have gather commercial imaging sonar system data with same target. This case study will support the Test Readiness Review of future underwater surveillance system developing via investigate marine testing field environment, testing facilities and planning.

• Corrosion Science and Technology
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• 제6권3호
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• pp.120-127
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• 2007

In any developing nation major investment goes for infrastructure and it is not exception in India. Good numbers of buildings, bridges, shopping malls, car parks etc. are coming up with steel for sustainable development. Thus protecting the structures from corrosion are the challenges faced by professionals for all types of steel structures. About 3% of GDP is accounted for loss due to corrosion. To combat this up to date corrosion map is called for as the country has wide variation of climatic zones with vastcoastline. Logically organic paint system can be prescribed based on the corrosion rate on bare steel with respect to environment. Present paper will emphasis on the study conducted on two types of structural steel coated with organic paint located in twomarine environment having been exposed for three years, Test coupons made from steels both bare and coated are deployed at two field stations having marine (Digha) and industrial marine (Channai) environments. Various tests like AC impedance DC corrosion, polarisation, salt spray test, $SO_2$ chamber and Raman spectroscopy were carried out both in laboratory on fresh as well as coupons collected from exposure sites. Rust formed on the bare and scribed coated coupons are investigated. It is found that normal marine environment at Digha exhibits higher corrosion rate than polluted marine environment in Channai. Rust analysis indicates formation of ${\propto}$-FeoOH protects or reduces corrosion rate at Channai and formation of non-protective ${\gamma}$-FeoOH increases corrosion rate at Digha. The slower corrosion rate in Channai than at Digha is attributed due to availability of $SO_2$, in the environment, which converts non‐protective rust ${\gamma}$-FeoOH to protective rust ${\propto}$-FeoOH. While comparing the damage on the coated panels it is found that low alloy structural steel provides less damage than plain carbon steel. From the experimentations a suitable paint system specification is drawn for identical environments for low medium and high durability.

• 항공우주기술
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• 제6권1호
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• pp.157-164
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• 2007

GPS 안테나는 위성발사체의 전 비행 구간에서 GPS 위성 신호를 정상적으로 수신하기 하여 발사체의 외피에 설치되어야 한다. 위성발사체의 표면 온도는 발사체가 대기권을 통과하면서 발생하는 열공력의 영향으로 급격하게 상승하며 발사체 외피에 설치되는 GPS 안테나는 극심한 고온 환경에 직접적으로 노출된다. 따라서 위성발사체의 외피에 설치되는 GPS 안테나에 대한 고온 환경 시험 규격은 발사체 내부 시스템의 고온 환경 시험 규격보다 더 가혹하게 설정되어야 한다. 본 논문에서는 KSLV-I 발사체에 탑재될 GPS 안테나의 고온 환경에서 성능 분석 절차 및 결과를 기술하며, GPS 안테나가 고온 환경에서 물리적인 변형이나 내부 LNA(Low Noise Amplifier)의 성능 저하 없이 정상적으로 동작하였을 보여주고 있다.

• 한국건축시공학회지
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• 제5권3호
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• pp.91-99
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• 2005

It is required to study systematical on the concrete quality management to extend structure life because rebuilding effect is reducing under present condition of large sized and high stories structure. Concrete, which shows its intensity by hydrating action and a big change in quality according to hot weather and temperature, produces a lot of qualify problem under hot and cold weather Because of each specification and construction plan which does not have basic standard on site, concrete's quality is irregular and makes some defect. As a result, Daegu is turned out to be the longest area after investigating application period and days focused on 8 cities weather information about relationship between hot weather circumstance and construction environment. Therefore, we first surveyed the concrete material in the region and found out the problem of quality nanagement. Then figure out the way of solution. Moreover, we integrated concrete material quality management, which is applied differently to each site, to have equal quality and to reduce defect from construction site. And then, based on various test of construction condition and analysis of quality management item, we suggest effective concrete quality management to make concrete material construction standard guide and plan under hot weather.

• 한국군사과학기술학회지
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• 제18권3호
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• pp.267-274
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• 2015

It is necessary to both analyze root-cause of non-conformance of effective illumination time to the specification, and estimate the storage lifetime for 81 mm illuminating projectile stockpiled over 10 years. In this paper, aging mechanism of magnesium flare material due to long-term storage was supposed, and two-stage tests, pre-test and main test based on accelerated degradation tests were performed. Field storage environment of moistureproof was set up, and illumination times in the accelerated degradation tests for temperatures 60 and $70^{\circ}C$ were measured. Then, storage reliability of the projectile was estimated through analyzing the measured data and applying distribution-based degradation models to the data. The $B_{10}$ life by which 10 % of a population of the projectiles will have failed at storage temperature of $25^{\circ}C$ was estimated about 7 years.

• 항공우주기술
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• 제6권1호
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• pp.222-229
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• 2007

환경시험은 개발된 제품이 해당 운용환경에서 설계 성능을 발휘하는가를 운용성과 신뢰성 유지 측면에서 수행하고 있다. 항공전자장비에 대한 환경적합성 시험은 주로 개별 부품 단위로 수행되고 있으며 민간용 규격으로서 RTCA DO-160E이 활용되고 있다. 군용 환경규격은 항공분야 뿐만 아니라 전 군수품에 적용하고 있는 MIL-STD-810F 이외에 전자기 환경분야에는 MIL-STD-461E 등이 적용되고 있다. 항공전자장비에 대한 민간용과 군용 환경시험요건을 분석하여 그 연관성을 검토하였으며 특히 전자기 적합성 요건에 대하여 민간과 군용 규격을 비교 분석하여 민군 겸용화의 방향을 제시하고자 한다.