• The Transactions of the Korean Institute of Electrical Engineers
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• v.35 no.6
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• pp.209-216
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• 1986

This paper describes the design of multi channel data acquisiton system for industrial process automation. The prototype hardware assembly consists of Z-80A microprocessor, 10-bit A/D converter with 16-channel analog multiplexor and related interface circuitry. The first order lag filter, which can be implemented without any particular computational problem has implemented in software, and the simulation results are shown. The protype system can communicate with a central processor through RS-232C, and can be used either as an intelligent stand-alone controller or as a satellite controller which can be monitored and controlled by a central processor. The singal conditioners for various temperature and humidity sensors are designed and experimental results are shown.

• Aerospace Engineering and Technology
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• v.2 no.1
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• pp.197-204
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• 2003

General image processing is the production of images of added value with the use of the original and standard images. Generated data and auxiliary data are backed up and this retrieved data is periodically updated to provide images to outside users. To product general images, makes use of EOC Processing System Software. And then added value images is made from the standard images. Standard and added images are possible with internet for search and promptly provides for user. The process of the standard image derived from the original image(received from the satellite) is systematically arranged in this thesis, which also contains a concise explanation of the EOC processing system.

• Proceedings of the KSRS Conference
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• 2009.03a
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• pp.35-38
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• 2009

본 논문은 KOMPSAT-2, KOMPSAT-3 등과 같은 고해상도 위성영상의 정사보정 방법과 그에 따른 시험용 소프트웨어 개발을 목표로 한다. 정사보정은 위성 카메라의 자세나의 지표의 피복인위에 의하여 발생하는 인위를 제거하여 정사투영 된 특성을 갖는 영상을 구하는 과정을 말한다. 정사보정을 위해서는 위성 카메라의 기하학적인 특성과 지표면의 관계식을 나타내는 공선조건 식으로부터 지상기준점 및 수치표고모델을 통하여 구해진다. 본 논문에서는 고해상도 위성영상의 정사보정 방법을 구현하고, 실제 위성영상 데이터에 적용하여 구현된 소프트웨어의 성능을 평가한다.

• Aerospace Engineering and Technology
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• v.12 no.2
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• pp.74-82
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• 2013

This paper deals with a single stage coilgun which is a variety of EML(ElectroMagnetic Launcher) and can be applied to launching a small satellite. We propose a mathematical and physical model in order to design a single stage coilgun and study physical characteristics related to design parameters. A proposed mathematical and physical model is verified by electromagnetic FEM software FEMM 4.2.

• Proceedings of the KSRS Conference
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• 2007.10a
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• pp.317-320
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• 2007

This research focuses on a network based data distribution and visualization system of Multi-functional Tran-port SATellite (MTSAT). Institute of Industrial Science (IIS) and Institute of Earthquake Research Institute (ERI) both at University of Tokyo have been receiving, processing, archiving and distributing of MTSAT imagery with a direct receiving of High Rate Information Transmit (HRIT) since October 2006. A software package, mtsatgeo, is developed including radiometric correction, geometric correction and spatial subset, and they are available on a web-based data distribution and processing service accessed at http://webgms.iis.u-tokyo.ac.jp/.

• Proceedings of the Korean Society of Soil and Groundwater Environment Conference
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• 2000.11a
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• pp.103-106
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• 2000

Geophysical data sets from the Chojeong area in the Chungbuk-Do are compositely studied in terms of multi-attribute interpretation for the subsurface mapping of shallow fracture zones, associated with groundwater reservoir. Utilizing a GIS software, the attribute data are implemented to a database; a lineament from the satellite image, electrical resistivities and its standard deviation, radioactivity, seismic velocity, bedrock depth from exploration data. In an attempt to interpret 1-D electrical sounding data in 2-D and 3-D views, 2-D resistivities structures are firstly made by interpolating 1-D plots. Reconstruction of a resistivity volume is found to be an effective scheme for subsurface mapping of shallow fracture zones. Shallow fracture zones in the southeastern part of the study area are commonly correlated in the various exploration data.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2006.05a
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• pp.258-261
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• 2006

The structure of small launch vehicle can be divided into engine section and payload section. This paper introduces modal test of the payload section of small launch vehicle which is composed to satellite, PLA (Payload Adapter), VEB (Vehicle Equipment Bay), KMS (Kick Motor Support) and KM (Kick Motor). From this test, dynamic properties of the 2nd stage structure of small launch vehicle can be obtained. In this test, to simulate free-free boundary condition, test object was hung by 4 bungee cords and excited by using impact hammer Modal test data are analyzed by using TDAS(Test Data Analysis Software). As the result, modal parameters and mode shapes below 100Hz of the 2nd stage of small launch vehicle were identified.

• International Journal of Aeronautical and Space Sciences
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• v.6 no.1
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• pp.77-88
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• 2005

KOMPSAT-2 is the second Korean earth observation satellite after KOMPSAT-l: the 1 meter GSD cartographic capability and planning to launch at the end of 2005 by ROKOT launch vehicle. The dedicated AOCS operational modes are designed for KOMPSAT-2 based on KOMPSAT-l experience All of AOCS operational modes requires gyro information. To compensate this drawback, Power Safe Mode is designed and implemented. Successfully AOCS on-board software is developed and extensively verified through a nonlinear simulation process. The simulation results of Power Safe Mode and Science Fine Submode are provided to demonstrate its functionality as well as its performance.

• Proceedings of the KIPE Conference
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• 2018.07a
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• pp.470-471
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• 2018

본 논문에서는 소형 큐브위성의 전력시스템 구성품의 용량 및 위성의 운용로직을 설계할 수 있는 소프트웨어 테스트베드 설계 방법을 제시한다. 기존 초소형 인공위성 시스템 설계를 위한 소프트웨어가 개발되어 상용품으로 판매되고 있으나, 주로 자세제어 시스템의 제어기 설계를 위해 소프트웨어가 사용되고있고, 텍스트기반 복잡한 구조로 되어있어 본 논문의 목적인 전력계 구성품 용량 및 운용로직을 설계하는데 이를 활용하기 어려운 측면이 있었다. 따라서 본 논문에서는 전력시스템의 구성품들을 전력 및 에너지 방정식으로 모델링하여 Matlab/Simulink에서 이를 구현함으로써 가독성을 높여 시스템 설계 및 분석 시간을 줄일 수 있는 소프트웨어 테스트베드 설계방법을 제시한다. 제안된 소프트웨어 테스트베드를 이용한 3리터 사이즈의 소형 큐브위성 시스템의 구성품 용량 및 운용로직 설계 결과를 본 논문에서 제시한다.

• Proceedings of the IEEK Conference
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• 2002.06a
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• pp.235-238
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• 2002

In this paper we describe the design and implementation of Electrical Ground Support Equipment(EGSE) for the CBS transponder testing. The main task of EGSE is to check out satellite systems, at system or subsystem level, during integration and validation phases of their life-cycle. Through a combination of hardware and software elements, EGSE supports manual, semi-automatic and fully automated testing. Automation is achieved by offering users simple, yet powerful means to write their own test application programs (test sequences) in high-level, test-oriented language and to run them in a strict real-time environment. The core of this environment is a user-configurable real-time database, containing all the information needed to calibrate acquired data, check them against predefined thresholds, automatically react to out-of-range conditions, display data using animated graphics or synoptic windows, and so on.