• Proceedings of the Korean Society of Broadcast Engineers Conference
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• 2017.06a
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• pp.155-157
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• 2017

본 논문에서는 ATSC(Avanced Television Systems Committee) 3.0 물리계층에서 다양한 서비스 시나리오별 가능한 프로파일을 도출하기 위한 MATLAB GUI(graphical user interface)기반의 ATSC 3.0 시뮬레이터를 구현한다. 개발된 시뮬레이터는 ATSC 3.0 에서 지원하는 다양한 종류의 BICM(bit interleaved and coded modulation) 및 OFDM(orthogonal frequency division multiplexing) 파라미터 조합과 다중화 방식을 지원할 수 있고, 그에 따른 프레임 길이와 전송률을 계산할 수 있다. 개발된 시뮬레이터에서는 4 개의 PLP(physical layer pipe)까지 지원할 수 있고, 최대 4 개의 부프레임(subframe)까지 구성이 가능하다.

• Proceedings of the Korean Society of Disaster Information Conference
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• 2015.11a
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• pp.186-188
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• 2015

본 연구에서는 Matlab GUI언어로 개발한 수질관리모형(water quality model)을 소개한다. Matlab GUI언어는 사용자 편의에 중점을 둔 프로그램으로 다양한 계산용 함수의 포함 및 데이터의 입출력이 쉽고 조작이 용이하다. 본 모형은 기존의 복잡한 수질관리모형을 단순화 및 간소화하여 비전문가들 또한 사용이 가능하도록 데이터의 입력 과정과 변수 지정이 쉽도록 제작하였으며 서울특별시 수질오염총량관리 단위유역 내 한강수계에 적용하여 분석하였다. 이는 기존의 사용법이 어려운 수질관리모형의 한계를 깨고 사용가능 계층의 확대 및 예측 모형의 단순화에 새로운 패러다임을 제시할 것으로 기대된다.

• Journal of Positioning, Navigation, and Timing
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• v.8 no.2
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• pp.69-77
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• 2019

This study introduces MATLAB Graphical User Interface (GUI)-based software to monitor ionospheric disturbances. This software detects ionospheric disturbances using Global Positioning System (GPS) and Global Navigation Satellite System (GLONASS) measurements, and estimates a location of the disturbance source through the detected disturbance. In addition, this software includes a sky plot making function and frequency analysis function through wavelet transform. To evaluate the performance of the developed software, data of 2011 Tohoku earthquake in Japan were analyzed by using the software. The analysis results verified that the ionospheric disturbances were detected through GPS and GLONASS measurements, and the location of the disturbance source was estimated through the detected disturbance.

• Journal of Advanced Navigation Technology
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• v.4 no.2
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• pp.132-142
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• 2000

This paper includes a study on the performance analysis of SDINS by a simulator using Matlab/Simulink. The performance model is considered gravity and Coriolis force, and a barometer is included to damp down diversity of a perpendicular axis error. Using the simulator, the performance included gyro sensor errors was analyzed in various maneuvering patterns. Also, the performance is virtually presented for the variation of error parameters of gyro and accelerometer under GUI.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.43 no.9
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• pp.787-798
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• 2015

The emergence of mid-to-small satellites has created a need for rapid development with a relatively low cost. However, the development of mid-to-small satellites requires considerable time and cost in early phase, in particular, during the development of mission and system requirements through iterations of conceptual design and mission design. In this research, Spacecraft Conceptual Design Tool(SCDT) which is based on Graphical User Interface(GUI) was developed to reduce the time and cost for early phase development. Furthermore, GUI-based software can make the input values to be editable easily and show users design results in various way. In this paper, the development results of MATLAB GUI-based SCDT are introduced.

• Proceedings of the KIPE Conference
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• 2007.11a
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• pp.145-147
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• 2007

This paper presents an implementation of vector control for SMPMSM using model based controller design in MATLAB/SIMULINK. The model based controller design enables fast development of control system for motor by designing controllers and performing simulation on the GUI (Graphic User Interface) platform, converting program code directly into real-time programs, and then performing tests for the responses from controllers. The controller is designed as PI controller for speed and decoupling PI controller for current. And PWM used space vector modulation method using offset voltage and system stability is also secured by close magnitude overmodulation method, maintaining dynamics of load when it overmodulation. The validity of vector control implemented is verified through simulations and experiments.

• Proceedings of the KIEE Conference
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• 2004.07d
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• pp.2568-2570
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• 2004

CEMTool is a command style design and analyzing package for scientific and technological algorithm and a matrix based computation language. In this paper, we present new FEM (Finite Element Method) package in CEMTool environment. In contrast to the existing MATLAB PDE Toolbox, our proposed FEM package can deal with the combination of the reserved words. Also, we can control the mesh in a very effective way With the introduction of new mesh generation algorithm and NDM (Hosted Dissection Method), our FEM package can guarantee the shorter computational time than MATLAB PDE Toolbox. In addition, using the advanced electromagnetics library of CEMTool FEM package, we can analyze the practical problems such as the motor field analysis. Consequently, with our new FEM package, we can overcome some disadvantages of the existing MATLAB PDE Toolbox.

• Proceedings of the KIEE Conference
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• 2006.07d
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• pp.2109-2110
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• 2006

유한요소법은 전자기, 기계, 또는 다른 공학 분야에서 다루는 풀기 어려운 복잡한 문제들을 해석하는데 널리 사용되고 있는 수치해석기법이다. CEMTool은 MATLAB과 유사한 과학기술 범용 패키지로서, 간편한 명령어 방식의 문법과 블록 다이어그램 설계, 이공학 전반의 함수 등의 다양한 기능들을 제공한다. 본 논문에서는 범용 공학 소프트웨어인 CEMTool 환경에서 실행되는 GUI 3D FEM 패키지에 대해 기술한다. FEM 해석의 일반적 단계인 전처리, 솔버, 후처리 단계별로 나누어 각 단계의 구조와 특징 등을 기존의 CEMTool 2D FEM 패키지, MATLAB PDE Toolbox, FEMLAB2.2와 비교하여 자세히 살펴보기로 한다.

• Journal of Advanced Navigation Technology
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• v.22 no.5
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• pp.384-390
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• 2018

This paper introduces a MATLAB graphical user interface (GUI) based software for analysis of korea augmentation satellite system (KASS) availability performance. This software uses minimum variance (MV) estimator and Kriging algorithm to generate integrity information such as user differential range error (UDRE) and grid ionospheric vertical error (GIVE). The information is offered to ground and aviation users in Korean region. The software also gives accuracy data, protection level data and availability map about each user position by using the integrity information. In particular the software calculates the protection level along a path of aircraft. We verified the result of protection level of aviation user by comparing them with the results of SBASimulator#2, which is a simulation tool of european geostationary navigation overlay service (EGNOS). As a result, the protection level error between the result of our software and the SBASimulator#2 was about 2% which means that the result of our software is accurate.

• Journal of the Korea Society for Simulation
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• v.31 no.4
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• pp.1-10
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• 2022

This paper describes the development of a modular simulation environment to analyze the performance of guided weapons. For the reusability of the simulation environment, components of the guided weapon simulation are modularized based on MATLAB Simulink. And the module management system is implemented based on Excel and MATLAB GUI for simulation interface and module management. In addition, a method of integration for modules with different interface and a method to set up the guidance and control phase for designing a guided flight scenario are suggested. Finally, to verify the performance of the implemented simulation environment, it was compared with the existing simulation results.