• Proceedings of the Korean Information Science Society Conference
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• 2008.06b
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• pp.96-100
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• 2008

본 논문에서는 워크스페이스 기반 소프트웨어 형상관리 (Software Configuration Management, SCM) 시스템의 설계와 그 구현 방법에 대하여 논한다. 워크스페이스는 팀 단위의 협업 개발을 지원하기 위한 통합 환경으로, 형상항목(configuration item)에 대한 버전관리와 병렬 개발 프로세스를 제공한다. 본 연구는 이러한 워크스페이스 기반의 협업 개발 환경과 함께 프로젝트 관리 변경 프로세스 관리 기능을 결합한 통합 소프트웨어 형상관리 시스템 구축을 목표로 한다.

• Journal of the Korea Institute of Military Science and Technology
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• v.16 no.4
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• pp.435-440
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• 2013

In this paper, a design method of the simulation program for HILS(Hardware-In-the-Loop Simulation) system is proposed. The present method consists of definition of requirements for HILS, development of specifications, and implementation of the program to satisfy the specifications. In the implementation of the program, the application of hardware interface and the concept of structural modularization are proposed to satisfy the specifications. The concepts of CSCI(Computer Software Configuration Item) and encapsulation are used for structural modularization. The proposed method was practically applied to the development of the simulation program for the efficient operation in HILS of an anti-ship missile system.

• Journal of the Korea Institute of Military Science and Technology
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• v.2 no.2
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• pp.173-185
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• 1999

고품질의 소프트웨어를 개발하는 사업의 중요성이 나날이 증대되고 있는 시점에서 소프트웨어를 종합군수지원 관점에서 해석하려고 하는 연구가 최근에 진행되고 있다. 즉, 소프트웨어 설계자의 입장은 소프트웨어 개발도 중요한 문제이지만 소프트웨어를 얼마나 가용성 있게 유지하는가에 더 많은 관심을 갖게 된다. 하드웨어는 개발 시부터 종합군수지원이라는 기법을 적용하여 체계 배치 시 체계 장비가 최상의 가용도를 가질 수 있도록 하는 노력이 이루어지고 있으며, 그 결과도 현실화되고 있다. 본 논문에서는 하드웨어에서만 적용하고 있는 종합군수지원 개발 기법을 소프트웨어에 적용하여 소프트웨어에 대한 종합군수지원 적용방안을 제시하고, 향후 소프트웨어 개발/배치 시에 경제적이고 가용도가 높은 소프트웨어의 개발/활용이 가능하도록 군수지원 분석을 통한 종합군수지원 활용 방안을 제안한다.

• Journal of the Korea Society of Computer and Information
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• v.29 no.8
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• pp.67-75
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• 2024

Frequently changeable functional requirements in System Management CSCI Software make it difficult to reuse an overall application, but only the partial class codes repeatedly as a new version of Naval Combat Management System is developed. This structural environment leads to increasing development time and expenses. This is why modularization for System Management CSCI Software is proposed as a solution, leveraging the advantages of proper standardization and functional expandability offered by Standard Interface Architecture. This paper outlines the comparisons of modified class ratios as well as software reliability test runtime results between before and after implementing the modularization for System Management CSCI Software. The findings demonstrate there is sufficient improvement in areas, such as higher maintenance and reusability, supporting the application of modularization for System Management CSCI Software with the implementation of Standard Interface Architecture.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.33 no.9
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• pp.104-112
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• 2005

This paper presents the technique to develop an operational flight program(OFP) of avionic system computer(ASC) which integrates the avionics control, navigation and fire control and provides informations for flight, navigation and weapon aiming missions. For the development of the OFP of ASC, two i960KB chips are used as central processing units board and standard computer interface library(SCIL) which is built in house is used. The Irvine compiler corporation(ICC) integrated development environment(IDE) and the programming language Ada95 are used for the OFP development. We designed the OFP to a computer software configuration item(CSCI) which consists of to three parts for independency of software modules. The OFP has been verified through a series of flight tests. The relevant tests also have been rigorously conducted on the OFP such as software integrated test, and ground functional test.