• Title/Summary/Keyword: Military Modeling

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Full Dynamic Model in the Loop Simulation for Path Tracking Control of a 6$\times$6 Mobile Robot (6$\times$6 이동로봇의 경로추종을 위한 동역학 시뮬레이션)

  • Huh, Jin-Wook
    • Journal of the Korea Institute of Military Science and Technology
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    • v.11 no.4
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    • pp.141-148
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    • 2008
  • In this paper, we develop a detailed full dynamic model which includes various rough terrains for 6-wheel skid-steering mobile robot based on the real experimental autonomous vehicle called Dog-Horse Robot. We also design a co-simulation for performance comparison of path tracking algorithms. The control architecture in the co-simulation can be divided into two levels. The high level control is the closed-loop control of path tracking to follow a given path, and the low level is concerned about torque control of wheel motion. The simulation using the mechanical data of the Dog-Horse Robot is performed under the Matlab/Simulink environment. We also simulate and evaluate the performance of the model based adaptive controller.

Improving Adaptability of the DEVS Based Simulator with AOP (AOP 기술을 이용한 DEVS 기반 시뮬레이터의 적응성 향상 기법)

  • Kim, Cheol-Ho
    • Journal of the Korea Institute of Military Science and Technology
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    • v.10 no.3
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    • pp.90-99
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    • 2007
  • The DEVS formalism has the well-defined relationship between its model and simulator. However, it does not define the connection between its model and experimental frame needed when a simulator's implemented with it. So, in most DEVS based simulators, the modules of the two parts are tangled, so that changing and reusing them is not easy. This paper proposes a method to improve the changeability of the experimental frame and the reusability of the model by modularizing the two parts using the AOP technology. I applied the new method to a real project, and the result shows that it improves the two qualities effectively than before.

The Development of Torpedo Defense Experimental Technique based on M&S (M&S 기반 어뢰방어전 모의실험 기술 구현)

  • Nah, Young-In;Lee, Sim-Yong;Yoon, Han-Saem
    • Journal of the Korea Institute of Military Science and Technology
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    • v.13 no.5
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    • pp.818-823
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    • 2010
  • Exploiting models and simulations are encouraged among the defense acquisition society, as now enforced by the Defense Aquisition Program Administration's regulations. They are useful and, sometimes, inevitable especially in an earlier phase of system development. Computer-simulation-based experimentation technique for the system operational performance analysis for a torpedo defense system is introduced in this paper. Problem definition for the torpedo defense system analysis and engineering efforts for models and simulations development are presented here, including defining measures of performance and effectiveness for the torpedo defense system, conceptual modeling for torpedo engagement and defense simulation, design of experimentation, design of simulator and experimentor, and hardware and software implementation of an analysis support tool - a system operations demonstration and experimentation simulator.

Stochastic Combat Simulation with Variable Hit Probabilities (명중확률의 변화를 고려한 확률과정 전투 시뮬레이션)

  • 홍윤기
    • Journal of the military operations research society of Korea
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    • v.27 no.2
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    • pp.76-87
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    • 2001
  • The effect of variable hit probabilities in the stochastic duel are examined. The objective of this study is to evaluate the outcomes of combat under the situations which we assume either round dependent hit probabilities or time dependent hit probabilities. Due to the complexity of an analytic approach to large-sized battles, a simulation modeling technique has been introduced. several specific examples are demonstrated fire allocation strategies. Output measures are compared among cases each with its own type of hit probability fashion such as constant, round to round, or time dependent manners. For these specific cases, the advantages of round to round improvement or increasing function of time for the hit probability are displayed.

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Distributed Air Defense Simulation Model and its Applications (방공교전모델(DADSim) 개발 및 활용사례)

  • 최상영;김의환
    • Journal of the military operations research society of Korea
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    • v.27 no.2
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    • pp.134-148
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    • 2001
  • In this paper, air-defense simulation model, called "DADSim", will be introduced. DADSim(Distributed Air Defense Simulation Model) was developed by Modeling&Simulation Lab of K.N.D.U.(Korea National Defence Univ) Weapon Systems Department. This model is an analysis-purpose model in the engagement-level. DADSim can simulate not only the global air-defense or Korean Peninsula but also the local air-defense or a battle field. DADSim uses the DTED(digital terrain elevation data) LeveII it for the representation of peninsula terrain characteristics. The weapon systems cooperated in the model are low/medium-range missile systems such as HAWK, NIKE, SAM. DADSim was designed in the way of object-oriented development method, implemented by C++ language. The simulation view is an event-sequenced object-orientation. For the convenience of input, output analysis, GUI(Graphic User Interface) of menu, window, dialog box, etc. are provided to the user, For the execution of DADSim, Silicon Graphic IRIX 6.3 or high version is required. DADSim can be used for the effectiveness analysis of­defence systems. Some illustrative examples will be shown in this paper.

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Finite strip analysis of a box girder simulating the hull of a ship

  • Akhras, G.;Tremblay, J.P.;Graham, T.;Cheung, M.S.;Li, W.C.
    • Structural Engineering and Mechanics
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    • v.15 no.2
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    • pp.225-238
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    • 2003
  • In the present study, the finite strip analysis of a box girder to simulate a ship's hull model is carried out to investigate its inelastic post-buckling behavior and to predict its ultimate flexural strength. Residual stresses and initial geometrical imperfections are both considered in the combined material and geometrical nonlinear analysis. The von-Mises yield criterion and the Prandtl-Reuss flow theory of plasticity are applied in modeling the elasto-plastic behavior of material. The Newton-Raphson iterative process is also employed in the analysis to achieve convergence. The numerical results agree well with the experimental data. The effects of some material and geometrical parameters on the ultimate strength of the structure are also investigated.

Analysis of Acceleration Characteristics of a Railgun (레일건 가속특성 분석)

  • Lee, Young-Hyun;Kim, Seong-Ho;Lee, Byung-Ha
    • Journal of the Korea Institute of Military Science and Technology
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    • v.24 no.5
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    • pp.511-518
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    • 2021
  • To accelerate a launch mass with a low level of pressure as possible in a railgun, it is required to hold supplied current nearly constant during launch phase. We obtained the discharging conditions for required current shaping by modeling and analysis of circuit equations coupled to acceleration equation of the launch mass. The acceleration characteristics of the railgun in the conditions were analyzed by comparing experimental and theoretical results.

A Mechanism Study of a HyperSpectral Image Sensor for Nadir and Slant Range Operation (직하방과 빗각 촬영 운용을 위한 초분광 영상센서 구동방식에 관한 연구)

  • Lee, Kyeongyeon
    • Journal of the Korea Institute of Military Science and Technology
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    • v.22 no.4
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    • pp.484-491
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    • 2019
  • General Hyperspectral Image Sensor acquires an image of line form such as a thin rectangle shape because of using 1D array Push Broom or Whisk Broom scanning method. A special mechanism is required for a Hyperspectral Image Sensor to operate for nadir and slant range. To design the mechanism, the characteristics of the flight motion and the overlap rate between consecutive frames were analyzed. Also, system requirements were proposed through modeling and simulation.

Stabilization Converter Design and Modeling of LEO Satellite Power Systems (저궤도 위성의 전력 시스템 안정화를 위한 모델링 및 제어)

  • Yun, Seok-Teak;Won, Young-Jin;Lee, Jin-Ho
    • Journal of Satellite, Information and Communications
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    • v.5 no.2
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    • pp.29-33
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    • 2010
  • Satellites industry has been developing with the commercial and military needs. Because power system of satellite is very important to survival operation and hard to test, increasing reliability is very critical. Due to LEO small satellites are very sensitive to power system, effective stabilization control is important. Therefore, this paper introduce methods for general modeling of power converting system which it can be used design of controller and analysis of external disturbance influences. In conclusion, a modeling of LEO small satellites power converting system and a possible guide line to design reliable controller which optimizing power converters of LEO small satellite are generated.

Modeling Combat Entity with POMDP and DEVS (POMDP-DEVS를 활용한 전투 개체 모델링)

  • Bae, Jang Won;Lee, Kanghoon;Kim, Hyeoneun;Lee, Jun Seok;Goh, Bongseok;Nam, Bowon;Moon, Il-Chul;Kim, Kee-Eung;Park, Jaehyun
    • Journal of Korean Institute of Industrial Engineers
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    • v.39 no.6
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    • pp.498-516
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    • 2013
  • Combat Modeling and Simulation (M&S) is significant to decision makers who predict the next direction of wars. Classical methodologies for combat M&S aimed to describe the exact behaviors of combat entities from military doctrines, yet they had a limitation of describing reasonable behaviors of combat entities that did not appear in the doctrines. Hence, this paper proposed a synthesizing modeling methodology for combat entity models considering both 1) the exact behaviors using descriptive modeling and 2) the reasonable behaviors using prescriptive modeling. With the proposed methodology, combat entities can represent a reality for combat actions rather than the classical methodologies. Moreover, the experiment results using the proposed methodology were significantly different from the results using the classical methodologies. Through the analyses of the experiment results, we showed that the reasonable behaviors of combat entities, which are not specified in the doctrines, should be considered in combat M&S.