• Defense and Technology
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• no.3 s.169
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• pp.36-45
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• 1993

유도탄에 의존하는 전투 경향은 향후 계속적으로 증대될 것이며 더구나 유도탄은 지금까지 설명한 것 같이 장거리화, 고속화, 스텔스화, 고고도 또는 저고도 탄도선택, 명중 직전까지 탐지 곤란 및 최종유도 단계에서 고가속도 운동 등 성능은 향상 일로에 있습니다. 함정의 생존성을 제고시키기 위한 각국의 대함유도탄 방어체계 개발 노력은 함정 탑재 무기체계인 근접방어 무기체계, 함대공유도탄, ESM 및 유도탄 기만 장치의 지속적인 성능개량과 함께 지속될 것입니다

• Journal of the Korea Society for Simulation
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• v.31 no.4
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• pp.1-10
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• 2022

This paper describes the development of a modular simulation environment to analyze the performance of guided weapons. For the reusability of the simulation environment, components of the guided weapon simulation are modularized based on MATLAB Simulink. And the module management system is implemented based on Excel and MATLAB GUI for simulation interface and module management. In addition, a method of integration for modules with different interface and a method to set up the guidance and control phase for designing a guided flight scenario are suggested. Finally, to verify the performance of the implemented simulation environment, it was compared with the existing simulation results.

• The KIPS Transactions:PartD
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• v.12D no.5 s.101
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• pp.709-718
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• 2005

To correspond with the unpredictable future tactical environment, Ive expanded the application of M&S(Modeling & Simulation) that is more scientific and more economic in a field of weapon system development process. This paper describes experience in development of ADSF(Air Defense Simulation Framework) that supports not only HLA(High Level Architecture) which is an international standard in M&S but also TCP/IP as well as real-time distributed simulation. ADSF has been applied to the M-SAM(Medium Range Surface to Air Missile) System Simulator, and satisfying test results through GPS(Global Positioning System) timer has been acquired. As a result, an ADSF which is able to support HLA and TCP/IP as veil as precise real-time simulation has been successfully made. we were in need or a real-time simulation engine to support Air Defense System Simulators that were consisted of several subsystems.

• Proceedings of the Korea Information Processing Society Conference
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• 2012.11a
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• pp.1460-1463
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• 2012

본 논문은 대형복합 체계인 국방무기체계를 설계 프로세스에 따라 SysML 을 적용하여 개발하는 방법 및 사례에 대해 다룬다. ISO-IEC 15288 에 제시된 기술 프로세스의 핵심 단계인 요구사항 분석, 기능 분석, 이키텍처 설계를 모델 기반으로 수행하는 것은 이해관계자 사이의 의사소통을 원할히 유지하는 효과적인 방법이다. 더불어 SysML 을 기반으로 작성된 체계 모델은 S/W 설계를 위해 많이 사용되는 UML 과 설계 일관성을 유지하기 용의하다. 본 논문은 SysML 을 통해 체계 개발에 필요한 단계별 모델의 종류와 사용방법을 대공유도무기 사례를 통해 제안하고자 한다.

• Journal of the Korea Institute of Military Science and Technology
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• v.14 no.4
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• pp.556-563
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• 2011

Recently, the development of military system is focused on Network Centric Warfare. But, there is no deployed Command and Control System for Missile System in the country. Therefore, Command and Control System for Missile System was simulated to predict feasibility for the future development in this paper. The contents of the design and implementation for simulated system are described in details. Besides, a method for avoiding collisions in 1:N radio communication environment is proposed as the future work. The simulated system in this paper will be a help to developing Command and Control System for Missile System in the future.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 1998.10a
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• pp.26-26
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• 1998

다련장 로켓과 같이 무유도로서 대량 발사하는 탄을 설계함에 있어서 탄의 성능을 예측하기 위해서는 사거리와 고도 해석을 통해 체계 성능을 분석하고 탄의 특성 및 외부요소의 변화 가능성을 고려하여 탄착 정확도에 대한 해석을 수행하여야 한다. 탄착 정확도는 설계하고자하는 무기체계의 신뢰성을 평가하는 최종단계이므로 매우 중요한 factor이다. 다련장 로켓과 같은 무유도 로켓의 탄착 정확도를 평가하는 가장 좋은 방법은 많은 발수의 시료를 발사하여 획득한 데이터를 바탕으로 평가하는 것이다. 그러나 이 방법은 예비 설계시에는 적용할 수 없으며 제작이 되었다 하더라도 비용이 많이 들기 때문에 적용하기 무척 어렵다.

• The Journal of Korean Institute of Communications and Information Sciences
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• v.35 no.11B
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• pp.1704-1709
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• 2010

A small number of countries are leading the world in the development of advanced weapon systems. In general, the access to the information on the design of advanced systems is limited. As such, when similar weapon systems need to be developed, a special methodology must be considered to catch up with both the technological and information barriers. In this paper, we study a design methodology based on the combination of the reverse engineering and the design structure matrix (DSM) approach. The methodology begins by analyzing the advanced system by reverse engineering and produces a set of design results in the form of physical architecture, functional architecture and system requirements. The design results are further enhanced by applying the DSM clustering. As a result, one can get an improved design result. As a target system, a guided missile system was considered.

• Defense and Technology
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• no.1 s.71
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• pp.6-18
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• 1985

• Defense and Technology
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• no.8 s.222
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• pp.48-59
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• 1997

• Defense and Technology
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• no.2 s.72
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• pp.57-62
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• 1985