• Title/Summary/Keyword: Ballistic-Missile Defense

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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.

An Effectiveness Analysis of Anti-Ballisitic Missile Launcher Arrangement for the Lower Tier Defense against the Ballistic Missile (탄도미사일 하층 방어 수행을 위한 발사대 배치 효과도 분석)

  • Kwon, Hyuck-Hoon;Lee, Bum-Seok;Kim, Yoon-Hwan;Choi, Kwan-Bum
    • Journal of the Korea Institute of Military Science and Technology
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    • v.16 no.5
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    • pp.590-597
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    • 2013
  • For a lower tier defense, the distance between a launcher and an engagement control station is quite important to estimate the proper defense area and to effectively arrange missile launchers. In this paper, we have analyzed an effectiveness of anti-ballistic missile launcher arrangement for the lower tier defense against the ballistic missile. The operation concept, specific configuration and aerodynamic characteristics of the ballistic missile such as SCUD-B/C, Nodong are considered in order to develop a realistic engagement simulation. The diverse engagement results through numerical simulations are provided to conduct the effectiveness analysis of anti-ballistic missiles.

U.S. Ballistic Missile Defense System and THAAD (미국의 탄도미사일 방어체계와 THAAD)

  • Park, Young-Chul;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.455-457
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    • 2015
  • Since V-2, the first ballistic missile was developed during world war II, ballistic missile threat is increasing consistently due to science technology progress. United States is constructing and operating BMDS(Ballistic Missile Defense System) to defend homeland and allies. Various Interceptors will try intercept ballistic missile detected by sensors at boost phase, midcourse phase or terminal phase. THAAD(Terminal High Altitude Area Defense) is intercept system that intercept ballistic missile at high altitude of terminal phase. In this paper, concept of U.S. BMDS, and operational and technical characteristics of THAAD is surveyed and described.

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Homeland Defense Radar-Hawaii(HDR-H) for Anti-Ballistic Missile (하와이 배치 탄도미사일 방어용 레이더)

  • Park, Tae-yong
    • Proceedings of the Korean Institute of Information and Commucation Sciences Conference
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    • 2018.10a
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    • pp.258-259
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    • 2018
  • The United States has deployed and operates a ballistic missile defense system to defend the homeland from ballistic missile attacks launched from direct and potential threats. The Missile Defense Agency has deployed the Aegis BMDs, Sea-based X-band radars(SBX), Ground-Based Interceptors(GBI), Early Warning Radars and THAADs. In addition, the Homeland Defense Radar-Hawaii(HDR-H) will be deployed in Hawaii. The HDR-H is expected to improve defensive ability to ballistic missile threats in the Asia-Pacific region.

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The U.S. Navy Aegis Ballistic Missile Defense (미 해군의 이지스 탄도미사일 방어)

  • Park, Tae-yong
    • Proceedings of the Korean Institute of Information and Commucation Sciences Conference
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    • 2015.05a
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    • pp.359-362
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    • 2015
  • The United States is constructing Missile Defense System to defend from elevated ballistic missile threat of Russia, China and North Korea. U.S. MD system is consists of IAMD concept by MDA centralized, and U.S. Navy takes charge detection, tracking and intercepting on the sea. In this paper, it is reported that concept, current state and plan of U.S. Navy Aegis Ballistic Missile Defense.

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The Optimal Deployment Problem of Air Defense Artillery for Missile Defense (미사일 방어를 위한 방공포대 최적 배치 문제)

  • Kim, Jae-Kwon;Seol, Hyeonju
    • Journal of Korean Society of Industrial and Systems Engineering
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    • v.39 no.1
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    • pp.98-104
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    • 2016
  • With the development of modern science and technology, weapon systems such as tanks, submarines, combat planes, radar are also dramatically advanced. Among these weapon systems, the ballistic missile, one of the asymmetric forces, could be considered as a very economical means to attack the core facilities of the other country in order to achieve the strategic goals of the country during the war. Because of the current ballistic missile threat from the North Korea, establishing a missile defense (MD) system becomes one of the major national defense issues. This study focused on the optimization of air defense artillery units' deployment for effective ballistic missile defense. To optimize the deployment of the units, firstly this study examined the possibility of defense, according to the presence of orbital coordinates of ballistic missiles in the limited defense range of air defense artillery units. This constraint on the defense range is originated from the characteristics of anti-ballistic missiles (ABMs) such as PATRIOT. Secondly, this study proposed the optimized mathematical model considering the total covering problem of binary integer programming, as an optimal deployment of air defense artillery units for defending every core defense facility with the least number of such units. Finally, numerical experiments were conducted to show how the suggested approach works. Assuming the current state of the Korean peninsula, the study arbitrarily set ballistic missile bases of the North Korea and core defense facilities of the South Korea. Under these conditions, numerical experiments were executed by utilizing MATLAB R2010a of the MathWorks, Inc.

Ballistic Missile Tracking using Unscented Kalman Filter (Unscented Kalman Filter를 이용한 탄도 미사일 추적)

  • Park, Sang-Hyuk;Yun, Joong-Sup;Ryoo, Chang-Kyung
    • Journal of Institute of Control, Robotics and Systems
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    • v.14 no.9
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    • pp.898-903
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    • 2008
  • In most cases, the trajectory of a ballistic missile is well explained by the Kepler's laws. It implies that the remaining trajectory of the ballistic missile including its final destination can be easily predicted if the position and velocity vector of the ballistic missile at any point on its path can be exactly known. Hence, an effective tracking algorithm based on an exact radar measurement model is very important for developing Ballistic Missile Defense(BMD) system. In this paper, we address to design a nonlinear filter, Unscented Kalman Filter(UKF), to track the ballistic missile.

Threat Assessment of Anti-Ship Ballistic Missile (ASBM) of North Korea (북한 대함탄도미사일 위협 분석)

  • Park, Younghan;Oh, Kyungwon;Kim, Jiwon
    • Journal of Aerospace System Engineering
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    • v.10 no.3
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    • pp.1-8
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    • 2016
  • This paper provides an empirical assessment of the development of North Korea's Anti-Ship Ballistic Missile (ASBM), and its influence on South Korea's maritime strategy. While research studies on North Korea's ballistic-missile capabilities and South Korea's ballistic-missile defense systems are proliferating, less analytical attention has been given to the way that the strengthening of North Korea's ballistic-missile capacities presents a critical threat to the ROK's navy and lines of communication. The authors of this paper identify the continuing development of unique ASBM capabilities by China and Iran, and determine that such processes are mutually interactive and in accordance with threat perceptions; furthermore, North Korea can enact the same process by learning lessons from these nations. The findings of this paper provide an implication for the formulation of South Korea's maritime strategy and the related assets in consideration of the ASBM as a future threat.

A Study on the Optimal Allocation of Korea Air and Missile Defense System using a Genetic Algorithm (유전자 알고리즘을 이용한 한국형 미사일 방어체계 최적 배치에 관한 연구)

  • Yunn, Seunghwan;Kim, Suhwan
    • Journal of the Korea Institute of Military Science and Technology
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    • v.18 no.6
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    • pp.797-807
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    • 2015
  • The low-altitude PAC-2 Patriot missile system is the backbone of ROK air defense for intercepting enemy aircraft. Currently there is no missile interceptor which can defend against the relatively high velocity ballistic missile from North Korea which may carry nuclear, biological or chemical warheads. For ballistic missile defense, Korea's air defense systems are being evaluated. In attempting to intercept ballistic missiles at high altitude the most effective means is through a multi-layered missile defense system. The missile defense problem has been studied considering a single interception system or any additional capability. In this study, we seek to establish a mathematical model that's available for multi-layered missile defense and minimize total interception fail probability and proposes a solution based on genetic algorithms. We perform computational tests to evaluate the relative speed and solution of our GA algorithm in comparison with the commercial optimization tool GAMS.

Analysis of Flight Trajectory Characteristics of the MRBM by Adjusting the Angle of a Flight Path (비행경로각 조정에 의한 중거리 탄도미사일의 비행궤적 특성 해석)

  • Kim, Jiwon;Kwon, Yong Soo
    • Journal of the Korea Institute of Military Science and Technology
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    • v.18 no.2
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    • pp.173-180
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    • 2015
  • North Korea has developed ballistic missiles over the past 30 years. It is believed that they have a variety of ballistic missiles more than 1,000. Because these ballistic missiles threaten South Korea directly, accurate analysis of them is essential. Flight trajectories of the ballistic missiles are generally changed by means of adjusting payload weight, Isp, flight path angle, and cut-off time. The flight path angle is widely used to control the missile range. However it is difficult to predict the missile trajectory exactly in real operational environment because the missile could be launched according to its intention and purpose. This work analyzed the 1,000 km range MRBM's trajectory characteristics from adjusting flight path angle which is depressed as well as lofted method. The analysis of missile trajectory characteristics is based on the simulation of the missile trajectory model developed by KNDU research team.