• Title/Summary/Keyword: 미사일방어

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A Study on Effectiveness Analysis of K2 system with Weapon's unit cost (무기체계 단위비용을 고려한 K2 체계의 효과분석 방법 연구)

  • Jung, Byungki
    • Journal of the Korea Society for Simulation
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    • v.26 no.2
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    • pp.31-39
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    • 2017
  • This paper analyses the effectiveness of Kill Chain (KC) and Korea Air and Missile Defense (KAMD), also known as the K2 systems, using monte carlo simulation. It is assumed that the K2 systems are consisted with unitary KC and multi-layered (upper-tier and lower-tier) KAMD. And each system has two or three arbitrary weapon systems and its combination makes 12 scenarios. Measures of effectiveness (MOE) of the K2 systems were defined as ratio of eliminated ballistic missiles from total threats. And total cost was calculated by number of weapon launched and its unit cost. MOE and total cost of the K2 systems were estimated using monte carlo simulation with a thousand iteration for each scenario. Cost-effectiveness analysis was performed and the best candidate was selected using fixed effectiveness approach. As a result, the performances of KC are prime factor that affects both effectiveness and total cost of the K2 systems. It is also, acquired proper level of lower-tier KAMD to achieve desired defense effectiveness. For future work, it needs to be performed cost-effectiveness analysis based on practical specification and life cycle cost of weapon systems.

Effective Response Time Verify of Active Decoy Against Anti-Ship Missile Using DEVS Simulation (DEVS 시뮬레이션을 사용한 능동기만기의 대함미사일에 대한 효과적인 대응시간 검증)

  • Choi, Soon-Ho;Cho, Tae-Ho
    • Journal of the Korean Institute of Intelligent Systems
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    • v.25 no.5
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    • pp.495-501
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    • 2015
  • Abroad warships are confronted with various menaces. The most critical threat of the warship is an Anti-Ship Missile (ASM). The ASM is able to be launched at a variety of environments and platforms. The ASM can evades conventional naval radar systems and electronic countermeasure techniques for providing a fatal damage to the warship. To cope with the ASM, an active decoy is an effective method to minimize the direct damage to the warship. The active decoy increases survivability of the warship because the ASM can lure pursuit of the active decoy instead of the warship. In this paper, our proposed method verifies an available response time of the active decoy to deal with the ASM using the active decoy of the warship in marine environments. We defined models of the warship, the ASM, and the active decoy, and executed simulation by combining the models. By the simulation result, the proposed method demonstrated the superiority of the mobile active decoy of the response time decoy among various active decoys, and estimated a protection area to prevent the ASM according the response time of the mobile active decoy against the ASM.

A Requirement Assessment Algorithm for Anti-Ballistic Missile Considering Ballistic Missile's Flight Characteristics (탄도미사일의 비행특성을 고려한 요격미사일 소요 알고리즘)

  • Kim, Heung-Seob;Kim, Ki-Tae;Jeon, Geon-Wook
    • Journal of the Korea Institute of Military Science and Technology
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    • v.14 no.6
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    • pp.1009-1017
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    • 2011
  • A Ballistic Missile(BM) is a missile that follows a sub-orbital ballistic flightpath with the objective of delivering one or more wardheads to a predetermined target and An Anti-Ballistic Missile(ABM) is a missile designed to destroy a ballistic missile before reaching its target. The main objective of this study is to assess the requirement of ABM by considering both flight characteristic of the SCUD-B/C, Nodong missiles and intercept performance of ABM in the Lower tier Ballistic Missile Defense(BMD). The Ballistic Missile's flight characteristics, such as trajectory, velocity etc., are estimated by simulation using the physical motion equations. The requirement of ABM is calculated by evaluating whether the BMD forces can defend those when the ballistic missiles attack prime facilities.

함정용 대공방어 시스템 이지스

  • Korea Defense Industry Association
    • Defense and Technology
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    • no.6 s.208
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    • pp.40-45
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    • 1996
  • 이지스 시스템은 미국이 고성능 대함 미사일을 함정에서 요격하기 위하여 개발한 함정용 대공 방어 시스템이다. 이지스(Aegis)는 그리스 신화에 나오는 방패(모든 사악한 것으로부터 몸을 지킨다는 방패)로, 중앙에 괴물 고르곤(Gorgon)의 머리 모양이 그려져 있다. 고르곤은 머리털이 뱀이며 그 눈을 본 사람은 무서운 나머지 돌로 변했다고 전해지는 스테노(Stheno), 에우리알레(Euryale), 메두사(medusa) 등 3자매중 하나를 말한다. 이 방패는 처음에 제우스(Zeus)가 소유하였으나, 뒤에 자신의 딸인 지혜.예술.전쟁의 여신 아테나(Athena)에게 주었다. 이지스 시스템은 요격용 대공 미사일인 Standard Missile SM-MR(RIM-66시리즈)과 위상 배열 레이다 SPY-1을 중심으로 하여, 그 외의 함내 센서(탐지 장치), 전술 정보처리장치 등 많은 무기 체계의 기능을 통합시킨 집합체이며, 이 위상 배열 안테나는 이지스 시스템의 상징으로 되어 있다. 현재 미국 해군의 Ticonderogal(CG-47)급 순양함, Arleigh Burke(DDG-51)급 구축함, 그리고 일본 해상 자위대 Kongo(DD-173)급 구축함에 탑재되어 작전의 효율성을 높이고 있다.

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2010년 우리 국군의 첨단병기

  • Yun, Jae-Seok
    • The Science & Technology
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    • no.7 s.410
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    • pp.44-47
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    • 2003
  • 한마디로 막강한 위용을자랑하는 최강의 군으로 변모해 있을 것이라는 낙관적 전망이 지배적이다. 자주국방에 대한 우리 군의 비전은 동아시아 긴장의 핵이자 일촉즉발의 전운이 감도는 한반도를 전쟁의 위험으로부터 차단하는 사전 억지력을 확보하기 위한 독자적인 첨단 정예군 육성으로요약된다. 중장기적으로 주한미군을 대신할 수 있는 첨단장비를 다수 배치해 유사시 미군에 의존하지 않는 자주방위를 실현하겠다는 것이다. 아울러 미국이 추진하고 있는 미사일방어체제의 일환인 전역미사일방어 참여를 위한 무기체제의 수립도 병행해 나갈 예정이다. 지난 5월 6일 조영길 국방장관이 노무현 대통령에게 분야별 전력증강 목록과 달성시기, 소요 예산 등을 요약해보고한 '자주국방 비전'과 이전에 각군별로 발표한 군전력강화방안, 지난 6월 27일 미국 워싱턴D.C. 에서 열린 한 · 미 국방장관 회담에서의 논의사항 등을 중심으로 향후 도입될 첨단 무기 시스템을 살펴본다.

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Concept and Employment Status of EPAA(European Phased Adaptive Approach) (EPAA(European Phased Adaptive Approach) 개념과 구축 현황)

  • Moon, Suk-hyun;Kim, Young-deuk;Park, Tae-yong
    • Proceedings of the Korean Institute of Information and Commucation Sciences Conference
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    • 2015.10a
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    • pp.586-588
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    • 2015
  • U.S. is constructing EPAA(European Phased Adaptive Approach) as a part of BMDS(Ballistic Missile System). The purpose of EPAA is to protect European NATO territory from Iranian ballistic missile threats. EPAA project consists of three phase, $1^{st}$ phase is completed as deploying transportable forces such as aegis BMD ships at the mediterranean, and $2^{nd}$ phase is on going. In this paper, the concept, characteristics, current status and future works of EPAA are surveyed and described.

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Analysis of the Flight Trajectory Characteristics of North Korea SLBM (북한 SLBM의 비행특성 해석)

  • Lee, Kyoung-Haing;Seo, Hyeong-Pil;Kwon, Yong-Soo;Kim, Jiwon
    • Journal of the Korea Society for Simulation
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    • v.24 no.3
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    • pp.9-16
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    • 2015
  • This research focuses on analysis of the flight trajectory characteristics of SLBM (Submarine Launched Ballistic Missile) of North Korea. Recently, North Korea tested launching of SLBM which is threatening international security. Also it is known that North Korea had possessed the technologies about SLBM since they disassembled submarines out of commission of the former Soviet Union. If the development of the SLBM of North Korea is completed, it should be affected as asymmetric threat to South Korea. Therefore, for active respondence to these threat, it is essential to analyze the SLBM systematically. In this point of view, this work made a SLBM flight model and simulated. In addition, we controled flight trajectories according to adjusting loft angle and described their characteristics. The sea-based ballistic missile defense system is required for an effective response to the flight trajectory of the SLBM from mid-course to terminal phase.

Analysis of Flight Trajectory Characteristics of Ballistic Missiles Considering Effects of Drag Forces (항력을 고려한 탄도미사일 비행궤적 특성 해석)

  • Kim, Jiwon;Kwon, Yong Soo
    • Journal of Advanced Navigation Technology
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    • v.20 no.2
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    • pp.134-140
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    • 2016
  • This paper analyzed flight trajectory characteristics of ballistic missiles considering effects of drag forces. It is difficult to intercept ballistic missiles which fly over atmosphere with supersonic speeds and small radar cross section (RCS). In particular, the velocities in the phases of boost and terminal are changed significantly due to the steep variation of the drag force. Therefore, in order to build up a successful ballistic missile defense systems, the effects of the drag forces should be considered in the analysis of ballistic missile trajectory characteristics. In this point of view, this work analyzed the effects of drag forces and derived the flight trajectory characteristics of Scud B, C and Nodong missiles. Model of the ballistic missile flight trajectory is considered the effects of Coriolis and centrifugal forces, and specifications of the missiles are open sources.

Study on Military Policy of North Korea (북한군사정책 특징 연구)

  • Kim, Sung Woo
    • Convergence Security Journal
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    • v.16 no.3_1
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    • pp.107-114
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    • 2016
  • The North Korean regime, Kim Jungun's foreign policy is changed frequently. And their military policy has no gravity. North Korea has developed nuclear weapons and long range missile. Now they have Inter-Continental Ballistic Missile. These activities redound a great threat in Korean peninsula. There are a no possibilities to give up its nuclear weapons and missile development. For the peace in Korean peninsula, we should make North Korea to abandon its nuclear himself through effective sanctions. Now China should effort to control North Korea. To reduce the threat we should coordinate the strategic interests of China and US. This study is to predict the North Korea military activities to analyze "military policies."

Development of Simulator for Analyzing Intercept Performance of Surface-to-air Missile (지대공미사일 요격 성능 분석 시뮬레이터 개발)

  • Kim, Ki-Hwan;Seo, Yoon-Ho
    • Journal of the Korea Society for Simulation
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    • v.19 no.1
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    • pp.63-71
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    • 2010
  • In modern war, Intercept Performance of SAM(Surface to Air Missile) is gaining importance as range and precision of Missile and Guided Weapon on information warfare have been improved. An aerial defence system using Surface-to-air Radar and Guided Missile is needed to be built for prediction and defense from threatening aerial attack. When developing SAM, M&S is used to free from a time limit and a space restriction. M&S is widely applied to education, training, and design of newest Weapon System. This study was conducted to develop simulator for evaluation of Intercept Performance of SAM. In this study, architecture of Intercept Performance of SAM analysis simulator for estimation of Intercept Performance of various SAM was suggested and developed. The developed Intercept Performance of SAM analysis simulator was developed by C++ and Direct3D, and through 3D visualization using the Direct3D, it shows procedures of the simulation on a user animation window. Information about design and operation of Fighting model is entered through input window of the simulator, and simulation engine consisted of Object Manager, Operation Manager, and Integrated Manager conducts modeling and simulation automatically using the information, so the simulator gives user feedback in a short time.