• 한국군사과학기술학회지
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• 제10권3호
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• pp.181-188
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• 2007

This paper presents a torque control method of a hydraulic actuation system for measuring the dynamic stiffness of missile fin actuators. We propose a new control technique called Dual Dynamic Torque Feedback Control(DDTFC), which improves the stability of the torque control system and enables fast tracking of torque command. The developed control scheme is derived from the physical understanding based on mathematical modelling and analysis. The dynamics of hydraulic torque control servo-system is unravelled via physics-based modelling and nonparametric system identification. In order to verify the effectiveness of the method, the experiment is carried out with a test equipment for measuring the dynamic stiffness. The experiment and simulation results show that DDTFC gives stability improvement.

• Journal of the Korean Society for Industrial and Applied Mathematics
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• 제19권3호
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• pp.253-270
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• 2015

Two major simultaneous attack strategies have been introduced, as one of cooperative attack of multiple missiles. One strategy is an undesignated time attack, in which the missiles communicate among themselves to synchronize the arrival times by reducing the mutual differences of times-to-go of multiple missiles during the homing. The other is a designated time attack, in which a common impact time is commanded to all members in advance, and thereafter each missile tries to home on the target on time independently. For this individual homing, Impact-Time-Control Guidance (ITCG) law is required. After introducing cooperative proportional navigation (CPN) for the first strategy, this article presents a new closed-form ITCG guidance solution for the second strategy. It is based on the linear formulation, employing base trajectories driven by PNG with various navigation constants. Nonlinear simulation of several engagement situations demonstrates the performance and feasibility of the proposed ITCG law.

• 한국멀티미디어학회논문지
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• 제22권7호
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• pp.815-821
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• 2019

This paper presents the design and implementation of a Mission Planning System(MPS) for multiple ballistic missiles. MPSs are also a kind of M&S systems in defense domain, and these provide important computations on the ground before flights of flying objects. The proposed MPS in this paper has a new concept which is far from generating a set of waypoints of a flying object and proving the set. In this paper, we firstly discuss the research motivation of our own MPS; then, we introduce the design of our MPS and its functionalities. In order to prove the practicality of our MPS, we have conducted a case study.

• 한국군사과학기술학회지
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• 제16권4호
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• pp.435-440
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• 2013

In this paper, a design method of the simulation program for HILS(Hardware-In-the-Loop Simulation) system is proposed. The present method consists of definition of requirements for HILS, development of specifications, and implementation of the program to satisfy the specifications. In the implementation of the program, the application of hardware interface and the concept of structural modularization are proposed to satisfy the specifications. The concepts of CSCI(Computer Software Configuration Item) and encapsulation are used for structural modularization. The proposed method was practically applied to the development of the simulation program for the efficient operation in HILS of an anti-ship missile system.

• 한국항공우주학회지
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• 제35권5호
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• pp.381-389
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• 2007

외부장착물의 효율적인 분리해석을 위해 6-DOF 시뮬레이션 프로그램을 개발하였다. 이 S/W는 장착물에 작용하는 공기력을 미리 작성된 공력 데이터베이스를 이용하여 간단한 보간으로 얻기에 전산유체역학에 기초한 방법에 비해 매우 빠른 계산시간을 가지며, 고정된 형상의 무장 뿐 아니라 분리 중 날개를 전개하는 무장에 대해서도 해석이 가능하다. 본 논문에서는 날개전개 무장의 공력 데이터베이스를 MSAP(Multi-body Separation Analysis Program)을 이용하여 작성하고, 비정상 감쇠계수를 Missile Datcom을 이용하여 예측하였다. 이 데이터베이스와 6-DOF 시뮬레이션 프로그램으로 무장의 고정된 날개 뿐 아니라, 날개전개에 따른 무장의 분리 안전성을 판단하였다

• 한국시뮬레이션학회논문지
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• 제26권2호
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• pp.31-39
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• 2017

본 연구는 무기체계의 단위비용을 고려한 K2(KC와 KAMD) 체계의 효과분석을 수행하였다. 단일 KC와 다중(고층 및 저층) KAMD를 가정하고, 각 체계에 임의의 무기체계를 설정하여 각각의 조합에 따라 총 12개의 시나리오를 작성하였다. 효과도는 전체 탄도미사일 위협 수량 대비 감소된 탄도미사일 위협의 비율로 정의하였으며, 비용은 발사된 무장의 수량과 단위비용으로 계산하였다. K2 체계의 효과도와 총비용은 몬테카를로 시뮬레이션을 1,000번 반복하여 추정하였다. 각각의 시나리오를 대안으로 하여 비용대 효과분석을 실시하였고, 효과고정법을 사용하여 최적 대안을 선정하였다. 연구 결과 KC 능력이 K2 체계의 방어 효과와 총비용을 결정하는 가장 중요한 요소였으며, 적정 수준의 저층방어체계를 갖춰야 요구되는 방어 효과를 달성할 수 있음을 확인하였다. 향후 연구에서 실질적인 무기체계 제원과 수명주기비용을 고려한 비용대 효과분석이 이루진다면 더욱 현실적인 분석이 가능할 것이다.

• 한국국방경영분석학회지
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• 제27권2호
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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.

• 한국군사과학기술학회지
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• 제19권2호
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• pp.244-251
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• 2016

In defense domain, mission level and engagement level simulation tools exist. In order to experiment a simulation scenario for obtaining results of both mission level and engagement level simulations, we should write a same simulation scenario in a mission level simulation tool as well as an engagement level simulation tool, and we have to operate these tools for analysis of each purpose. Moreover, we could not guarantee that these scenarios are completely same since each scenario is composed of different fidelities of simulation models, although the scenarios are written by a same experimenter and with same simulation purpose. To deal with the difficulties, I propose an approach to analysis of both mission level and engagement level simulations from one simulation result. For this, I have built Composite Combat Mission Planning Simulation Environment (CCMPSE). In this paper, the HLA/RTI based simulation composition technology and my experiences for the designed Composite Combat Mission Planning Simulation Control System (CCMPSCS) are explained. Moreover, This paper also conducts a case study with EADSIM, SADM, and the CCMPSCS. Finally, this paper provides lesson learned from the case study.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2010년 춘계학술대회논문집
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• pp.17-20
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• 2010

An aerial target system is used for the purpose of experimental test and fire training of missile that newly developed and in mass production. Since the target drones of aerial target systems are monopolized by several major countries so that they are selling at a high price. In this paper, we present the CFD simulation results on a new target drone that Kyungan co. ltd is developing with their own technologies. The presented CFD simulation was conducted in the same conditions of a wind tunnel tests and we could obtain the simulation results of the lift and drag values were in errors by less than 15 percent compared to the experiment. The simulation results were used to determine the modified shapes of new prototype target drone that could fly safely.

• 한국항공우주학회지
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• 제41권5호
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• pp.373-382
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• 2013

본 논문에서는 적외선 영상탐색기가 탑재된 대함유도탄에 대한 함정 방어용 기만 체계의 성능 분석을 위한 교전모의 프로그램을 소개한다. 대함유도탄에 탑재된 적외선 영상탐색기는 함정의 적외선 신호를 탐지하는 거리로부터, 비례항법 유도법칙 또는 입사각 제어유도법칙에 기반하여 접근한다. 그러므로 대함유도탄의 유도 수행 능력은 기본적으로 탐색기의 표적 추적 알고리듬뿐만 아니라 함정의 적외선 신호에 의존한다. 개발한 프로그램을 사용하여, 대함유도탄 적외선 영상탐색기의 다양한 추적 알고리듬으로 flare와 함정 표면을 냉각하기 위한 Counter-Measures Wash-Down System(CMWDS) 같은 함정 기만 체계의 영향을 살펴볼 수 있다.