• Title/Summary/Keyword: Military Vehicles

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Minimum Weight Design Method for Infantry Fighting Vehicles Hull using Thick Composite Laminate (전투용 차량의 경량화 최적설계 기법 연구)

  • 김건인;조맹효;구만회
    • Journal of the Korea Institute of Military Science and Technology
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    • v.4 no.2
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    • pp.9-16
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    • 2001
  • In this paper, general design process for Tracked Fighting Vehicle has been suggested. Stress analysis and optimal design for ply angle of IFV's composite upper hull has been calculated using KMA CIFV and it is contained exploratory development of design process. In this point, this paper applied composite to IFV's upper hull. Finite element mesh has been made using Matlab program, and we have analyzed stress based on the given material properties and ply arrangement. For each load condition, load distribution in plane and failure index are calculated by using Tasi-Hill criterion, which is composite failure criterion and analyzing change of failure index as change of ply angle. Finally, optimal ply angles of upper hull are calculated using KMA CIFV. We can estimate the decrease of weight for IFV's upper hull.

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Simulation and Analysis of Top-Attack Smart Submunition Descent Motions and Target Searching Footprint (상부공격 지능자탄의 낙하운동 및 탐색경로 시뮬레이션)

  • Kim, Ki-Pyo;Chang, Kwe-Hyun;Choi, Sang-Kyung;Hong, Jong-Tai
    • Journal of the Korea Institute of Military Science and Technology
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    • v.11 no.6
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    • pp.5-13
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    • 2008
  • A smart submunition drops through the expected trajectory to have a appropriate target searching footprint for the armored ground vehicles. Parachutes can be used as a tool to decelerate and spin the submunition. Usually submunition's descent velocity, spin rate, submunition inclination angle against vertical and dynamic stability affect to its target searching footprint. Therefore it is important to design optimal parachute and load configuration for the overall system performance. In this paper we described the dynamic motion of submunition by the mathematical model of parachute and load. Through the computer simulation we can analyze the submunition footprint affected by parachute and load design.

Evaluation of Wartime Domestic Overland Transportation Capability using Simulation (시뮬레이션을 이용한 전시국내 육로 수송 능력평가)

  • Lee, Jin-Seok;Lee, Sang-Jin
    • Journal of the military operations research society of Korea
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    • v.31 no.1
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    • pp.26-41
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    • 2005
  • The ROK TRANSCOM and Army Logistics Command have established wartime overland transportation plans. They have to mobilize several wartime overland transportation troops in order to meet the wartime transportation requirement. But there are some uncertainties in the process of transportation such as the number of vehicles to mobilize, the vehicle utilization factor, and round trip time. Here, we established two models. One is the simulation model to evaluate the transportation capability considering uncertain factors. The simulation model is executed with two scenarios and then the results are analyzed through a sensitivity analysis. The other model is the regression model to analyze the effects of transportation factors toward capability.

Robust Depth and Course Control of AUV Using LMI-based $H_{\infty}$ Servo Control (LMI에 기초한 $H_{\infty}$ 서보제어를 이용한 AUV의 강인한 자동 심도 및 방향제어)

  • 양승윤;김인수;이만형
    • Journal of the Korea Institute of Military Science and Technology
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    • v.3 no.1
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    • pp.38-46
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    • 2000
  • In this paper, robust depth and course controllers of AUV(autonomous underwater vehicles) using LMI-based H$_{\infty}$ servo control are proposed. The $H_{\infty}$ servo problem is modified to an $H_{\infty}$ control problem for the generalized plant that includes a reference input mode, and then a sub-optimal solution that satisfies a given performance criteria is calculated by LMI(Linear Matrix Inequality) approach. The robust depth and course controllers are designed to be satisfied the robust stability about the modeling error generated from the perturbation of the hydrodynamic coefficients and the robust tracking property under sea wave and tide disturbances. The performances of the designed controllers are evaluated by computer simulations, and these simulation results show the applicability of the proposed robust depth and course controller.

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Boundary Layer Analysis in a Hypersonic Flow Field (극초음속 유동장의 경계층 해석)

  • Sohn Chang-Hyun;Choi Seung;Moon Su-Yuon;Kim Jae-Yung;Lee Yul-Hwa
    • Journal of the Korea Institute of Military Science and Technology
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    • v.7 no.3 s.18
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    • pp.165-173
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    • 2004
  • Matching inviscid and boundary layer methods are developed for analysis of hypersonic flow with thick boundary layer. The new equations match all the boundary layer properties with a variation in the inviscid solution near the edge, except for the normal velocity. Computational comparison are peformed for incompressible and compressible flows over a flat plate. Results from the present method are compared with Wavier-Stokes solutions. The present results are in good agreement with Wavier-Stokes solutions. They show that the new technique can provide improved predictions of heating rates and skin friction predictions for preliminary design of vehicles where shear layers and entropy layer swallowing are importantfor for preliminary design.

A Study on the Conceptual Design of an Unmanned Surface Vehicle(USV) for the Korean Navy (한국형 무인 경비정(USV)의 개념설계에 관한 연구)

  • Boo Sung Youn
    • Journal of the Korea Institute of Military Science and Technology
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    • v.7 no.3 s.18
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    • pp.59-68
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    • 2004
  • Unmanned surface vehicles(USVs) have been developed for special operations in foreign navies. These will be employed to conduct critical missions including inspection, coast guard, ISR, fire protection, precision strike, mine interception warfare and antisubmarine warfare. It is also known the USVs will be deployed at the front line of the network-centric warfare to replace the manned naval operations. The unmanned operation can, thus, minimize unnecessary risk to personnel and enhance the success probability for the imposed mission. In this research, the USVs which are under operation and development in foreign navies are investigated. Based on this, an USV with $7\~10m$ of length and 10ton of weight for the Korean Navy which can be deployed near the Northern Limit Line(NLL), is proposed.

A Real-Time NDGPS/INS Navigation System Based on Artificial Vision for Helicopter (인공시계기반 헬기용 3차원 항법시스템 구성)

  • Kim, Jae-Hyung;Lyou, Joon;Kwak, Hwy-Kuen
    • Journal of the Korea Institute of Military Science and Technology
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    • v.11 no.3
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    • pp.30-39
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    • 2008
  • An artificial vision aided NDGPS/INS system has been developed and tested in the dynamic environment of ground and flight vehicles to evaluate the overall system performance. The results show the significant advantages in position accuracy and situation awareness. Accuracy meets the CAT-I precision approach and landing using NDGPS/INS integration. Also we confirm the proposed system is effective enough to improve flight safety by using artificial vision. The system design, software algorithm, and flight test results are presented in details.

Vetronics Design Using Realtime Integrated Control Techniques (실시간 통합제어기법을 이용한 차량전자화 설계)

  • Lee, Seok-Jae;Min, Ji-Hong;Lyou, Joon
    • Journal of the Korea Institute of Military Science and Technology
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    • v.11 no.3
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    • pp.89-98
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    • 2008
  • The vetronics is necessarily required for enhancement of the operational capability and optimization of the system architecture. In this paper, we presents the realtime control methods for the vetronics of the fighting vehicles. We proposed the data distribution based on standard bus and computer resource for realtime and integrated control of the system. Embedded computers are designed considering extensibility and reliability of the system. The integrated display improves the operator's capability. We applied the network centric battle management and digital power control with intelligent switching elements to increase cooperated combat efficiency and reliability. To show the feasibility of the presented design schemes, the vetronics has been implemented and applied to a real fighting vehicle.

A Study on the High Temperature Performance of the Brake Materials Built in Korean Model Combat Vehicle (한국형 기동장비 마찰재의 고온성능 연구)

  • 하상준;정동윤
    • Journal of the Korea Institute of Military Science and Technology
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    • v.3 no.2
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    • pp.53-60
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    • 2000
  • Organic brake materials are installed in the braking system of korean model combat vehicles. Since the binder resin is decomposed in high temperature region, it may possible to drop the friction force which makes the vehicle stop within the desired distance. This study analyses the braking performance of the brake materials in high temperature region by using the pin-on-disk type friction tester. It is observed radical drop of friction coefficients and rapid increase of wear amounts from the transition temperature. It is due to the formation of oxide layer on the friction surface.

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A Study on the Composition of Optimal Supply Route for Follow-on Logistics Support which Considers the Degree of Combat Intensity (전투치열도를 고려한 후속 군수지원의 최적 보급로 구성에 관한 연구)

  • Kim, Ki-Tae;Cho, Sung-Jin
    • Journal of the Korea Institute of Military Science and Technology
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    • v.13 no.6
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    • pp.1091-1098
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    • 2010
  • Victory and defeat of the war depends on follow-on logistics support. The spending time of follow-on logistics support at combat area is greatly influenced by the degree of combat intensity. The main purpose of this study is to compose a optimal supply route for operational sustainability of combat unit at combat area using transport vehicles. This study suggests a composition of optimal supply route for follow-on logistics support which considers the degree of combat intensity. A mathematical programming model and a genetic algorithm suggest to minimize the total spending time of follow-on logistics support. The suggested mathematical programming model is verified by using CPLEX 11.1. This study computes supply route, total spending time, total travel distance, and the number of transport vehicle.