• Proceedings of the Korea Contents Association Conference
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• 2004.11a
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• pp.417-420
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• 2004

As a lot of components are developed by CBD methodology, COTS are activated along with fast technology change of software. In this paper, implemented a view that show class diagram and specification of component in web. For this, we classified components in database and each information is used to retrieve through the view.

• Journal of Korea Society of Industrial Information Systems
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• v.5 no.3
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• pp.18-29
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• 2000

This study presents a cost of efforts estimation model under the environment of developing a software using component software package tools. The approach taken was to drive from variety of sources in an attempt to identify the most significant factors. These sources ranged from already existing cost models like COTS integration cost and COCOMO models to information gathered in a data collection survey. Once the candidate drivers had been identified, the next step was to interview with the experts who had been experienced more than 5 years in component development area to identify the most significant driving factors. From those selected drivers, I established the Cost Estimation Model which is suitable for the developing a software using component software package tools by applying the general from of the well-know COCOMO software cost estimation model. To established the best fit in Korean Software industry, I used Regression statistical analysis with 31 data collections.

• Journal of Aerospace System Engineering
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• v.18 no.2
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• pp.21-28
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• 2024

In light of the rapid development of the space industry, there has been increased attention on small satellites. These satellites rely on components that are considered to have lower reliability compared to larger-scale satellites. As a result, predicting reliability becomes even more crucial in this context. Therefore, this study aims to compare three reliability prediction techniques: MIL-HDBK-217F, RiAC-HDBK-217Plus, and FIDES. The goal is to determine a suitable reliability standard specifically for nano-satellites. Furthermore, we have refined the quality assurance factors of the manufacturing company. These factors have been adjusted to be applicable across various industrial sectors, with a particular focus on the selected FIDES prediction standard. This approach ensures that the scoring system accurately reflects the suitability for the aerospace industry. Finally, by implementing this refined system, we confirm the impact of the manufacturer's quality assurance level on the total failure rate.

• Proceedings of the Korean Nuclear Society Conference
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• 1997.10a
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• pp.239-243
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• 1997

상용기기(Commercial Grade Item CGI)란 구조물, 시스템, 콤포넌트 또는 그것들의 일부분을 구성하는 것으로써 안전기능(safety function)에 영향을 미치지만 basic component로써 설계되거나 제작되지 아니한 것을 의미한다 즉, ASME/NQA-1 Appendix B의 엄격한 품질보증 프로그램 하에서 설계되고 제작되지 아니한 것으로써 원전 이외의 분야에서 상용적으로 널리 사용되고 있는 기기들을 의미한다. 본 논문에서는 이러한 원전 안전등급 분류기준 Non-Nuclear System(NNS) Simple에 해당되는 Non-Safety CGI를 Safety Application의 Nuclear Grade Item으로 사용하기 위한 CGI 평가 및 승인 절차를 제안하고 새로운 CGI 생명주기 모델을 제시하였다. 본 논문에서 제시한 CGI Dedication 절차 및 CGI 생명주기 모델은 우리나라 원전 계측제어계통의 디지털 upgrade plan 및 교체, 신규원전 상용기기 평가방법론에 적용할 수 있을 것이다. CGI Dedication은 10여년전부터 원자력계가 고민해온 분야로써 원전 계측제어계통의 디지털화에 따라 상용 (Commercial Off The Shelf : COTS) 소프트웨어의 승인과 함께 전세계적으로 hot issue가 될 만큼 활발한 연구와 논의가 현재 진행되고 있는 분야이다.

• Journal of the Korea Society of Computer and Information
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• v.11 no.5 s.43
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• pp.149-156
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• 2006

The demands for the development of large scale software systems are being increased. Various software development methods have been introduced to meet these demands. The unit size of the codes that are reused is increasing in the development methods. These units reflect the concept of software reusability and can be identified as the object, component, and module. Recent trend in the development or a large scale software systems treats a commercial program as a unit to be reused. This approach lies along the same line as the identification of above three types of units. This paper shows how the above four types of units for enhancing the software reusability can be applied to the development of automatic graphic drawing System for a metal production.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2004.03a
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• pp.369-375
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• 2004

Gas turbine engine simulation in terms of transient, steady state performance and operational characteristics is complex work at the various engineering functions of aero engine manufacturers. Especially, efficiency of control system design and development in terms of cost, development period and technical relevance implies controlling diverse simulation and identification activities. The previous engine simulation has been accomplished within a limited analysis area such as fan, compressor, combustor, turbine, controller, etc. and this has resulted in improper engine performance and control characteristics because of limited interaction between analysis areas. In this paper, we propose a new simulation methodology for gas turbine engine performance analysis as well as its digital controller to solve difficulties as mentioned above. The novel method has particularities of (ⅰ) resulting in the integrated control simulation using almost every component/module analysis, (ⅱ) providing automated math model generation process of engine itself, various engine subsystems and control compensators/regulators, (ⅲ) presenting total sophisticated output results and easy understandable graphic display for a final user. We call this simulation system GT3GS (Gas Turbine 3D Graphic Simulator). GT3GS was built on both software and hardware technology for total simulation capable of high calculation flexibility as well as interface with real engine controller. All components in the simulator were implemented using COTS (Commercial Off the Shelf) modules. In addition, described here includes GT3GS main features and future works for better gas turbine engine simulation.