• Title/Summary/Keyword: Defence Science and Technology

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A Concept Study on Efficiently Improving Performance for Korean MBT (한국형 전차의 효율적인 성능개량 개념)

  • Kim, Seok;Son, Seung-Hyun
    • Journal of the Korea Institute of Military Science and Technology
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    • v.11 no.6
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    • pp.14-20
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    • 2008
  • A battle management system should be introduced to improve mission success capabilities and accommodate integrated combat capabilities through increasing SA(Situation Awareness), or spatiotemporal synchronization of military operation in battle field environment. Conventional Korean Main Battle Tanks(Korean MBTs), which have been operated without digital network, were developed for 1980s. Korean new MBTs, which are mounted the battle management system, will be fielded soon. Therefore, old Korean MBT is needed to improve performances for co-operation with new one. This paper is reviewed each improved MBTs of world countries and domestic maintenance facilities. And this study suggests some processing methods which might be applicable to improve information network performance of old Korean MBTs.

A Study on Hydrogel-Based CK Agent Detecting Gel Using Konig Reaction (Konig 반응을 이용한 CK 작용제 탐지젤 개발에 관한 연구)

  • Kim, Kyungmin;Kim, Kyung-pil
    • Journal of the Korea Institute of Military Science and Technology
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    • v.18 no.6
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    • pp.829-834
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    • 2015
  • A simple and sensitive hydrogel-based detecting gel has been presented for the qualitative determination of cyanogen chloride(CK) using Konig reaction. To optimize Konig reaction conditions, the effects of pyridine and barbituric acid concentration were investigated. Under the optimized conditions, CK gas concentration was directly related with absorbance change at 567 nm. Based on aqueous solution test results, we finally prepared CK detecting hydrogel by absorbing pyridine and barbituric acid solution. Color change of the prepared CK detecting hydrogel was clearly observed when the detecting gel was exposed to 10 ppm CK gas.

A Study of the Design for the Korean Wheeled Armored Command Post Vehicle Using AHP (AHP 기법을 이용한 한국형 차륜형 지휘소차량 디자인에 관한 연구)

  • Kim, Gunkook;Kim, Seokhwan;Lee, Jeongyeob;Kim, Jeongwoo;Choi, Insuk;Lee, Jaewoo;Kim, Uiwhan
    • Journal of the Korea Institute of Military Science and Technology
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    • v.20 no.5
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    • pp.717-725
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    • 2017
  • Traditionally, a design has been applied on a various defense area for the improvement of the mobility, reducing the radar detection area and other reasons. In case of Korean Wheeled Armored Vehicle(WAV), a design has been also applied for retaining the agility and threatening feature in the battlefield. However some figures has been changed because of constraints such as assembling and manufacturing in the development stage. Today, the government has planned to develop the Wheeled Armored Command Post Vehicle(CPV), a variant of WAV, and it is necessary to apply the latest design trend, which is suitable for the concept of the CPV, on it.

Simulation of Meshing for the Spur Gear Drive with Modified Tooth Surfaces

  • Seol, In-Hwan;Chung, Soon-Bae
    • Journal of Mechanical Science and Technology
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    • v.14 no.5
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    • pp.490-498
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    • 2000
  • The authors have proposed methods (lead crowning and profile modification) for modifying the geometry of spur gears and investigated the contact pattern as well as the transmission errors to recommend the appropriate amount of modification. Based on the investigation, dynamic load of the modified spur gear drive has been calculated, which is helpful to predict the life of the designed gear drive. Computer programs for simulation of meshing, contact and dynamics of the modified spur gears have been developed. The developed theory is illustrated with numerical examples.

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Vision-based Navigation for VTOL Unmanned Aerial Vehicle Landing (수직이착륙 무인항공기 자동 착륙을 위한 영상기반 항법)

  • Lee, Sang-Hoon;Song, Jin-Mo;Bae, Jong-Sue
    • Journal of the Korea Institute of Military Science and Technology
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    • v.18 no.3
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    • pp.226-233
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    • 2015
  • Pose estimation is an important operation for many vision tasks. This paper presents a method of estimating the camera pose, using a known landmark for the purpose of autonomous vertical takeoff and landing(VTOL) unmanned aerial vehicle(UAV) landing. The proposed method uses a distinctive methodology to solve the pose estimation problem. We propose to combine extrinsic parameters from known and unknown 3-D(three-dimensional) feature points, and inertial estimation of camera 6-DOF(Degree Of Freedom) into one linear inhomogeneous equation. This allows us to use singular value decomposition(SVD) to neatly solve the given optimization problem. We present experimental results that demonstrate the ability of the proposed method to estimate camera 6DOF with the ease of implementation.

Study on the Management of Mix Proportioning for the Military Hardtack by Nutritional Components Analysis (일반성분분석을 통한 군납 건빵의 배합비 관리 연구)

  • Lee, Donghun;Jeong, Minhong;Byun, Ji Eun;Lee, Kwang-Geun
    • Food Engineering Progress
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    • v.23 no.1
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    • pp.16-21
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    • 2019
  • In this study, the nutritional components (moisture, fat, protein, ash) value of military hardtack was collected and analyzed to control the mixing ratio of rice and flour. Hardtack from 4 factories was analyzed by 3 testing organizations certified by the Korean Ministry Food and Drug Safety. In addition, the accuracy and collaborative study possibility of each organization were evaluated in Q-test and HorRat. Also, other hardtack groups with different mixing ratios were compared to quality control of hardtack by I-MR charts. As a result, the HorRat and Q-test values of test organizations were 0.5-6.2 and 0.08-0.91, respectively. The quality of hardtack by the factories was similar. However, for accurate management of the mixing ratio, suggesting both upper and lower limit requirements of the nutritional components is necessary.

Efficient Detection of Small Unmanned Aerial Vehicles in Cluttered Environment (클러터 환경을 고려한 효과적 소형 무인기 탐지에 관한 연구)

  • Choi, Jae-Ho;Kang, Ki-Bong;Sun, Sun-Gu;Lee, Jung-Soo;Cho, Byung-Lae;Kim, Kyung-Tae
    • The Journal of Korean Institute of Electromagnetic Engineering and Science
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    • v.30 no.5
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    • pp.389-398
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    • 2019
  • In this paper, we propose a method to detect small unmanned aerial vehicles(UAVs) flying in a real-world environment. Small UAV signals are frequently obscured by clutter signals because UAVs usually fly at low altitudes over urban or mountainous terrain. Therefore, to obtain a desirable detection performance, clutter signals must be considered in addition to noise, and thus, a performance analysis of each clutter removal technique is required. The proposed detection process uses clutter removal and pulse integration methods to suppress clutter and noise signals, and then detects small UAVs by utilizing a constant false alarm rate detector. After applying three clutter removal techniques, we analyzed the performance of each technique in detecting small UAVs. Based on experimental data acquired in a real-world outdoor environment, we found it was possible to derive a clutter removal method suitable for the detection of small UAVs.

A Study on the Risk Management of Core Technology R&D Project using Degree of Difficulty and Technology Readiness Level (기술난이도와 기술성숙도를 이용한 핵심기술 연구개발 위험도 관리에 관한 연구)

  • Lee, Taehyung
    • Journal of the Korea Institute of Military Science and Technology
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    • v.19 no.6
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    • pp.789-796
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    • 2016
  • In the Core Technology R&D of the defence area, the development of the related core element technology could be the foundation to develop advanced weapon system in the future. But it might make various problems if you can not accurately define the TRL of the element technology. In other words, if the technology is not sufficiently mature and then the project starts, it might require an increase in the development period and additional cost. Finally the system will be in an incomplete state and result in user dissatisfaction and the project failure. Therefore it is a very important task to properly assess the TRL for a successful project. In this study, We propose the method for risk management of core technology R&D project of the defence area using the QFD process with degree of difficulty and technology readiness level. It is also presented the process to determine the risk level using TRL and Degree of difficulty. Finally We apply this method to UGV system for verifying the result of this study.

Fabrication and Properties of Reactively Hot Pressed HfB2-HfC Ultra-High Temperature Ceramics

  • Lee, Seung-Jun;Seong, Young-Hoon;Baek, Seung-Su;Kang, Eul-Son;Kim, Do-Kyung
    • Journal of the Korean Ceramic Society
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    • v.47 no.6
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    • pp.534-539
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    • 2010
  • $HfB_2$-HfC composites were prepared by reactive hot pressing using Hf and $B_4C$ at temperatures of 1800 and $1900^{\circ}C$ for 60 min under 32 MPa in an Ar atmosphere. The reaction sequences of the $HfB_2$-HfC composite were studied through series of pressureless heat treatments ranging from 800 to $1600^{\circ}C$. The effect of size reduction of the starting powders on densification was investigated by vibration milling. Fully dense $HfB_2$-HfC composites were obtained by size reduction of the starting powders via vibration milling. The oxidation behaviour of the $HfB_2$-HfC composites at $1500^{\circ}C$ in air showed formation of a non-protective $HfO_2$ scale with linear mass gain. Examination of the mechanical properties showed that particle size reduction via vibration milling also led to improved flexural strength, hardness and fracture toughness.

Earliest Intercept Geometry Guidance to Improve Mid-Course Guidance in Area Air-Defence

  • Shin, Hyo-Sang;Tahk, Min-Jea;Tsourdos, A.;White, B.A.
    • International Journal of Aeronautical and Space Sciences
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    • v.11 no.2
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    • pp.118-125
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    • 2010
  • This paper describes a mid-course guidance strategy based on the earliest intercept geometry (EIG) guidance. An analytical solution and performance validation will be addressed for generalized mid-course guidance problems in area air-defence in order to improve reachability and performance. The EIG is generated for a wide range of possible manoeuvres of the challenging missile based on the guidance algorithm using differential geometry concepts. The main idea is that a mid-course guidance law can defend the area as long as it assures that the depending area and objects are always within the defended area defined by EIG. The velocity of Intercept Point in EIG is analytically derived to control the Intercept Geometry and the defended area. The proposed method can be applied in deciding a missile launch window and launch point for the launch phase.