• Title/Summary/Keyword: 미사일

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한국 방위산업의 육성 패러다임과 지원정책 방향

  • Kim, Deok-Yeong
    • Defense and Technology
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    • no.10 s.260
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    • pp.28-43
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    • 2000
  • 기술진보와 불확실성이 방산 시장의 두드러진 특징이다. 군이 요구되는 무기와 장비는 신속히 변화하는 고가의 첨단기술에 의존함으로써 방위산업은 지속적인 대규모 기술개발투자를 요구하며 비용 및 성능요건 등에 관한 불확실성에 의해 지배된다. 예컨대 제트엔진, 미사일, 전자, 헬기 등 새로운 생산물을 탄생시킨 방산 분야의 기술진보는 민수품 생산기술을 크게 진보시켰으며 기업들에게 R&D를 강조하면서 새로운 개발 및 생산시설 투자를 요구하였다.

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Soil Properties of Reclaimed Tidel Lands and Tidelands of Western Sea Coast in Korea (우리나라 서해안 간척지 및 간석지 토양의 이화학적 특성)

  • Koo, Ja-Woong;Choi, Jin-Kyu;Son, Jae-Gwon
    • Korean Journal of Soil Science and Fertilizer
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    • v.31 no.2
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    • pp.120-127
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    • 1998
  • This study was performed to produce basic data for developing prediction techniques of desalinization through analyzing soil properties of reclaimed tidal lands, using soil samples collected in 11 units of tidal land reclamation projects. The average apparent specific gravity (bulk density), real specific gravity (particle density), porosity, and saturation percentage were measured to be 1.33, 2.64, 49.6%, and 56.3%, respectively. It was estimated that the soil texture class of reclaimed tidal lands would be silt or silt loam. The electrical conductivity and exchangeable sodium percentage were estimated to be $20{\sim}40dS\;m^{-1}$ and 30~50% in the beginning of tidal land reclamation, and the value of pH was measured to be 6.5~7.9. In conclusion, the soil properties of reclaimed tidal lands could be descrived to be saline-sodic soils with the high electrical conductivity and exchangeable sodium percentage.

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The Countermeasures of North Korea's Nuclear Weapon Terror (북한의 핵테러와 대응방안)

  • Kim, Sung Woo
    • Convergence Security Journal
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    • v.14 no.6_1
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    • pp.129-138
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    • 2014
  • South Korea should correspond to the primary threat to North Korea's nuclear weapons. It is necessary to have countermeasures to solve the realistic problems of North Korea's nuclear weapons. We can intensify military pact between the United States and Korea and at the same time strengthening the current military power. Currently, we take note the threat North Korea's missile. We can not control the development of a nuclear weapon and there are possibilities that North Korea have successfully miniaturized nuclear enough to carry by the missile. We should overview and check the Korea's missile defenses system. While the direction of the overall missile defense system deployment with a focus on lower and upper air defense network. And discuss defense research should be to build a system that can be protected with a key strategic facilities and cities. While North Korea have nuclear weapon, the main issues related to North Korea's nuclear threat. The six party talks countries try to solve the problem by the international and diplomatic approach. At the same time we should make somewhat to defend measures such as military defenses of Kill chain system to protect our country. Kill Chain is on of the effective defense system. We know that North Korea do not abandon to develop nuclear weapons by diplomatic efforts. We should performed in fact by a variety of military suppression method.

The Adsorption and Movement Characteristics of Pendimethalin in Soils (토양중 Pendimethalin의 흡착 및 이동특성)

  • 라덕관;김영규
    • Journal of Korea Soil Environment Society
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    • v.5 no.3
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    • pp.17-23
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    • 2001
  • The adsorption and movement characteristics of herbicide pendimethalin was studied in three kinds of soil, sandy loam, silty clay and loam. The results of the batch test and columnexperimentweresummarizedasfollows. The shaking time reached to the adsorption equilibrium of pendimethalin in soils was 6 hours. The adsorption rates of pendimethalin for sandy loam, silty clay and loam were 59.6%, 77.3% and 64.0%, respectively. The adsorption isotherms with the Freundlich equation showed better consistency than that with the Langmuir one. The adsorption coefficients of pendimethalin for soils were 8.0. 16.1 and 9.5. respectively. When breakthrough point was 0.05Co, the breakthrough times reached for soils were 256 minutes, 810 minutes and 420 minutes. respectively.

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Study on the countermeasures of the runway bombing using the mobile runway (이동식 활주로를 이용한 활주로 폭격 대응 방안에 관한 연구)

  • Seong, Min Cheol;Kim, Yongchul
    • Convergence Security Journal
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    • v.19 no.4
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    • pp.35-41
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    • 2019
  • Considering North Korea's strategy, North Korea's top hitting target in the event of a war is likely to be the main goal of the air force runway to neutralize the air force. As a countermeasure, there are emergency runway construction and runway emergency recovery operations. However, emergency runway construction is mainly intended for emergency landing and fueling and rearmament. The emergency runway restoration operation has also several limitations considering North Korea's threatening missile level, recovery time, and so on, so it cannot respond quickly to the North's runway bombing. In this study, we first describe the threat of North Korea's missiles and their air defense capabilities. Then the concept and limitations of the mobile runway, which is the next generation countermeasure, are presented.

Performance Analysis of Missile/Rocket Defense System for RPG-7 Defense of Main Battle Tank (미사일/로켓 방어체계의 RPG-7에 대한 전차방호 성능분석)

  • Ha, Jong-Soo;Lee, Eui-Hyuk;Lee, Hyun-Ah;Park, Gyu-Churl;Cho, Kyu-Gong
    • Journal of the Korea Institute of Military Science and Technology
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    • v.17 no.3
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    • pp.350-357
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    • 2014
  • MRDS is a short range missile/rocket defense system which protects a main battle tank(MBT) from threats at a short range. It is composed of 2 radars, 2 infrared trackers(IRT)s, 1 fire control computer(FCC), 2 launchers and countermeasures. In this paper, the radar and the IRT models based on sensing errors, the FCC model based on filtering errors, the launcher model based on driving errors and the countermeasure model based on flying errors are proposed to analyze the defense performance with the approaching RPG-7 and the moving MBT. The simulation results are presented to evaluate and verify the effectiveness of the proposed method.

Model Establishment of a Deployable Missile Control Fin Using Substructure Synthesis Method (부구조물 합성법을 이용한 접는 미사일 조종날개 모델 수립)

  • Kim, Dae-Kwan;Bae, Jae-Sung;Lee, In;Han, Jae-Hung
    • Transactions of the Korean Society for Noise and Vibration Engineering
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    • v.15 no.7 s.100
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    • pp.813-820
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    • 2005
  • A deployable missile control fin has some structural nonlinearities because of the worn or loose hinges and the manufacturing tolerance. The structural nonlinearity cannot be eliminated completely, and exerts significant effects on the static and dynamic characteristics of the control fin. Thus, It is important to establish the accurate deployable missile control fin model. In the present study, the nonlinear dynamic model of 4he deployable missile control fin is developed using a substructure synthesis method. The deployable missile control fin can be subdivided Into two substructures represented by linear dynamic models and a nonlinear hinge with structural nonlinearities. The nonlinear hinge model is established by using a system identification method, and the substructure modes are improved using the Frequency Response Method. A substructure synthesis method Is expanded to couple the substructure models and the nonlinear hinge model, and the nonlinear dynamic model of the fin is developed. Finally, the established nonlinear dynamic model of the deployable missile control fin is verified by dynamic tests. The established model is In good agreement with test results, showing that the present approach is useful in aeroelastic stability analyses such as time-domain nonlinear flutter analysis.

Design of a Missile Guidance Law via Backstepping and Disturbance Observer Techniques Considering Missile Control System Dynamics (백스텝핑 방법과 외란관측기법에 의한 미사일 제어시스템의 동역학을 고려한 미사일 유도법칙의 설계)

  • Song, Seong-Ho
    • Journal of Institute of Control, Robotics and Systems
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    • v.14 no.1
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    • pp.88-94
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    • 2008
  • In this paper, a design method of a missile guidance command is presented considering the dynamics of missile control systems. The design of a new guidance command is based on the well-known PNG(propotional navigation guidance) laws. The missile control system dynamics cause the time-delays of the PN guidance command and degrade the performance of original guidance laws which are designed under the assumption of the ideal missile control systems. Using a backstepping method, these time-delay effects can be compensated. In order to implement the guidance command developed by the backstepping procedure, it is required to measure or calculate the successive time-derivatives of the original guidance command, PNG and other kinematic variables such as the relative distance. Instead of directly using the measurements of these variables and their successive derivatives, a simple disturbance observer technique is employed to estimate a guidance command described by them. Using Lyapunov method, the performance of a newly developed guidance command is analyzed against a target maneuvering with a bounded and time-varying acceleration.

Design of Simulator for Missile Warning Radar of GVWS (지상 기동 무기 체계 탑재 미사일 경고 레이더 시뮬레이터 설계)

  • Ha, Jong-Soo;Park, Gyu-Churl
    • The Journal of Korean Institute of Electromagnetic Engineering and Science
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    • v.21 no.4
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    • pp.331-339
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    • 2010
  • To analyze and verify the performance of a MWR(Missile Warning Radar) of a GVWS(Ground Vehicle Weapon System), there is a need to make a simulator which can conduct the linked and engaged test virtually using the simulated signals. In this paper, a method of the simulator design for MWR is proposed to solve the above need. The SP(Signal Processor) part which generates the simulated signals and analyzes the algorithms is explained. The RF(Radio Frequency) part which transforms IF(Intermediate Frequency) signals into RF signals, radiates RF signals, and controls the linked equipments is also explained. The utility of the proposed design is proved by presenting the results of the contributions to the development of MWR.

The Effect Analysis of Missile Warning Radar Using Probability Model (확률 모델을 이용한 미사일 경고 레이다의 효과도 분석)

  • Park, Gyu-Churl;Hong, Sung-Yong
    • The Journal of Korean Institute of Electromagnetic Engineering and Science
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    • v.20 no.6
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    • pp.544-550
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    • 2009
  • To analyze the threat decision performance of MWR(Missile Warning Radar) give analysis on condition that we decide the effective threat using the POC(Probability of Over Countermeasure)/PUC(Probability of Under Countermeasure). Thus, we execute the simulation using the Monte-Carlo method to analyze effect, but the execution time of simulation took longer than we expected. In this paper, the effect analysis is proposed using the probability model to reduce the execution time of simulation. We present the setting method of parameter for probability model and the effect analysis result of MWR using the simulation. Also, we present the comparison result of simulation execution time for Monte-Carlo and probability model.