• Journal of the Korea Society for Simulation
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• v.21 no.1
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• pp.89-96
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• 2012

Recent modeling and simulation technologies are being used in various fields, especially in the field of military simulation-based acquisition (Simulation Based Acquisition) is recognized as an essential policy. In test and evaluation phase of the SBA process, to build a simulation-based T&E(test and evaluation) environment is needed when T&E cannot be carried by real weapon system. To improve efficiency and reliability for T&E, interoperability, reusability and reliability for T&E equipments and systems are important. In this study, we propose applying simulation framework for efficienct test and applying VV&A process for reliable evaluation. We describes the characteristics of the development process, the actual test cases and the results of evaluation. Finally utilization plan and the future direction of research is described.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.43 no.6
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• pp.540-547
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• 2015

This paper describes development contents and flight tests of an ACMI simulator based on LVC integrating architecture. ACMI is the system that provides air combat training and ground bombing training for improving fighting efficiency, that is the live simulation involving real people to operate real systems. ACMI simulator was developed for technic acquisition of LVC interoperability by using data link communication. ACMI simulator simulated maneuvering of a fighter by operating an UAV, a fighter can be distinguished from an UAV by maneuvering characteristics. This study proposes maneuvering simulation method by using flight data of the UAV, and performed its flight test for verifying similarity of fighter maneuvering.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.40 no.5
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• pp.446-453
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• 2012

As part of the integration phases in developing a UAV, a System Integration Laboratory (SIL) has been developed to provide integrated test capability for the verification of avionics system requirements. The SIL has realized primary functions that are common in manned aircraft SIL's, and specialized laying stress on test data visualization and test automation under the closed-loop structure of the ground control simulation, aircraft simulation and flight simulation components. Those design results have led to easy and sure verification of lots of complex requirements of the UAV avionics system. The functions and performances of the SIL have been proved in four gradational test steps and checked to operate successfully in aircraft System Integration Test Environment for the integration of UAV ground station and aircraft.

• Proceedings of the Korean Nuclear Society Conference
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• 1996.05d
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• pp.543-548
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• 1996

국내 가압 경수형 원자력 발전소 주제이실의 바닥에 가장 적합한 화재 감지기 선정을 위하여 원전 심사, 검사시 적용한 국내·외 화재감지기 설계 및 설치에 관한 법규와 규제요건의 종합적인 검토를 수행하고 원전의 주제이실 바닥 환경을 최대로 모의한 시험장치를 이용하여 선형열감지기와 공기 표본 추출형 연기감지기의 동작 성능을 비교 시험하였다. 시험 결과 케이블 화재시 공기 표본 추출형 연기감지기가 감도 및 응답특성이 정온식 선형 감지기 보다 우수한 것으로 확인되었다.

• The Journal of the Korea Contents Association
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• v.15 no.12
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• pp.1-7
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• 2015

These anti-jamming GPS systems are verified using large anechoic chamber or field-test until now. When using a large anechoic chamber, Independent verification from external enviroments like noise is an advantage but high cost and availability of chamber are disadvantages. And in case of field test, verification under real propagation enviroment is an advantage but security problem of military equipments and problem of making same test condition are disadvantages. This paper presents an newly developed anti-jamming GPS test system. This test system mainly consists of small anechoic chamber, jamming divider, jamming signal generator and satellite simulator. The small anechoic chamber is installed many jamming antennas to transmit multi jamming signals and the jamming divider is newly developed to control multi jamming signals. According to self performance test and combined test with Anti-jamming GPS receiver, we verified our system's reliability.

• Proceedings of the KIEE Conference
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• 2011.07a
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• pp.1554-1555
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• 2011

안정적인 전력공급을 위해 전력설비 진단이 중요시 되고 있고 이를 위해 변전기기인 변압기의 초기고장 검출을 통한 예방진단 기술을 필요로 하고 있다. 변압기 예방진단 기술 중에서도 유중가스진단은 가장 오래되고 신뢰성이 입증된 기술이다. 기존의 유중가스진단법들은 가스비분석법을 이용하고 있는데 대상 가스들이 절연유에의 열화에 의해 발생하는 가스들이고 주위 운전환경에 대한 고려가 부족하여 진단이 불가능하거나 진단오류가 발생한다. 본 연구에서는 절연유뿐만 아니라 고체절연물에 대한 열화를 고려하기 위하여 변압기 내부 결함 모의 시험 쳄버를 제작하고 시험 결과를 바탕으로 진단 알고리즘을 개발하고자 한다.

• Proceedings of the KSR Conference
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• 2007.05a
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• pp.980-986
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• 2007

본 연구는 매우 짧은 차간 간격을 요구하면서 차량 간의 충돌을 피하기 위해서 매우 정확한 속도제어를 필요로 하는 개인 고속 이동 시스템의 운행제어 알고리즘의 검증을 위한 검증 시스템의 설계에 대해서 다룬다. 검증시스템은 모의 차량, 중앙제어 시스템, 모의지상설비, 모니터링 장치로 구성된다. 모의차량은 총 4EA의 서버(노트북)로 구성 하며, 중앙(지역)제어시스템은 산업용 Motorola사(社)의 PowerPC기반 프로세서 모듈 및 I/O 보드 장치로 구성한다. 모의지상설비는 National Instruments社의 PXI 산업용 제어기를 사용하여 구현한다. 설계된 검증시스템의 시험을 위해서 Labview Simulation Interface Toolkit 과 Matlab/Simulink 가 결합된 환경하에서 모의시험을 거친 시험용 알고리즘을 이용한다.

• The Journal of Korean Institute of Electromagnetic Engineering and Science
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• v.23 no.1
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• pp.47-55
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• 2012

This paper describes the developed HILS and test equipment in order to test the performances of MMW(Millimeter-Wave) seeker which can detect and track a high speed of short-range ballistic missile and aircraft. This system is used to 141 horn antenna array, array switching, and gain and phase control algorithm to simulate various kind of targets and trajectory of high speed and maneuver moving target. In addition, it simulates not only velocity and range for these targets but also clutter and jamming environments. System configuration and implementation and the measurement results of major subsystems such as target motion simulator, simulation signal generator, high speed data aquisition unit, and central control unit are presented. These systems could verify the detection and tracking performance of MMW seeker through dynamic real-time test based on simulation flight scenario.

• Transactions of the Korean Society of Automotive Engineers
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• v.14 no.4
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• pp.192-198
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• 2006

The real-time simulator of a turning-type sluice gate actuated by the hydraulic cylinders is developed using a PC and a visual C++ program language. The real-time simulator receives the directional control valve signal selected by the operator using the mouse, updates the state variables of the turning-type sluice gate system responding to the control signal, and draws the moving figures of the sluice gate, cylinder, reserved water every drawing time on the PC monitor. Also, the operator can observe the sluice gate angle, cylinder force, cylinder pressures, and hydraulic power representing the operation of sluice gate system through the PC monitor every drawing time. The simulator can be a very useful tool to design and improve the turning-type sluice gate system.

• 제어로봇시스템학회:학술대회논문집
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• 1986.10a
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• pp.619-622
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• 1986

컴퓨터 기술의 발달에 따라 디지탈 전산기는 연산처리 능력이 더욱 빨라지고, 더욱 큰 기억용량을 갖게 되었다. 따라서 산업공정, 화학프랜트, 원자력발전 및 항공분야 등의 복잡한 연속 동특성계에 대한 실시간 시뮬레이션이 가능하게 되었다. 특히 복잡한 연속 동특성계의 시뮬레이션 목적으로 Multiprocessor 형태의 전산기가 개발되었다. 이 Multiprocessor형태의 전산기는 D/A 변환기와 A/D 변환기를 갖추므로써 실시간 실물 모의시험(A real time hardware-in-the-loop simulation) 시의 컴퓨터와 외부장비와의 데이타 전달이 용이하여 졌다. 본 연구에서는 비행체의 비행자세를 제어하기 위한 조종장치의 설계해석 및 성능시험을 위하여 Multiprocessor를 이용하여 실시간 실물 모의실험이 가능함을 보였다. 본 시뮬레이션에 사용된 전산기는 AD10 전산기이다.