• Korean Journal of Remote Sensing
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• v.14 no.3
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• pp.223-231
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• 1998

Ocean Scanning Multispectral Imager (OSMI) is a payload on the Korean Multi-Purpose SATellite (KOMPSAT) to perform worldwide ocean color monitoring for the study of biological oceanography. The instrument images the ocean surface using a whisk-broom motion with a swath width of 800 km and a ground sample distance (GSD) of less than 1 km over the entire field-of-view (FOV). The instrument is designed to have an on-orbit operation duty cycle of 20% over the mission lifetime of 3 years with the functions of programmable gain/offset and on-orbit image data storage. The instrument also performs sun calibration and dark calibration for on-orbit instalment calibration. The OSMI instrument is a multi-spectral imager covering the spectral range from 400 nm to 900 nm using a Charge Coupled Device (CCD) Focal Plane Array (FPA). The ocean colors are monitored using 6 spectral channels that can be selected via ground commands after launch. The instrument performances are fully measured for 8 basic spectral bands centered at 412, 443, 490, 510, 555, 670, 765 and 865 nm during ground characterization of instalment. In addition to the ground calibration, the on-orbit calibration will also be used for the on-orbit band selection. The on-orbit band selection capability can provide great flexibility in ocean color monitoring.

• The Journal of the Convergence on Culture Technology
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• v.9 no.6
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• pp.1057-1063
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• 2023

The urban railway sleeper floating track, the subject of this study, is an anti-vibration track to reduce vibration transmitted to the structure. currently, the replacement cycle of resilience pad for sleeper floating tracks is set and operated based on load. however, most previous studies were conducted on load-based structural safety aspects, such as fatigue life evaluation of sleeper anti-vibration pads and increase in track impact coefficient and track support stiffness due to increase in spring stiffness. therefore, in this study, we measure the vibration acceleration of the ballast for each analysis section and use the results of 7 million fatigue tests to calculate the spring stiffness of the resilience pad for each section. the spring stiffness of the resilience pad calculated for each section was set as the analysis data and the concrete vibration acceleration was derived analytically. the adequacy of analysis modeling was verified as the analyzed concrete bed vibration acceleration for each section was within the field-measured concrete bed vibration acceleration range. using the vibration acceleration curve according to the derived spring stiffness change, the spring stiffness of the resilience pad is estimated from the measured vibration acceleration. therefore, we would like to present a technique that can estimate the spring stiffness of resilience pad of a running track using the vibration acceleration of the measured concrete bed.

• The Journal of Korean Institute of Communications and Information Sciences
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• v.32 no.5A
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• pp.441-450
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• 2007

In this paper, it is proposed the link performance analysis results using SNRAT(Satellite Network Resource Allocation & Analysis Tool) and verified the anticipated results by satellite communication network simulator. A communication satellite cannot be corrected or fixed for the error in orbit operation after launching unlike the ground operation equipment and has a restricted operation life. So, it is important to make possible to use satellite communications in the proper time. It is expected the link BER(Bit Error Rate), throughput and AJ(Anti-Jamming) performance using SNRAT tool before launching. And it is verified the performance of the repeaters and ground equipment specification using the satellite network simulator and is extracted the optimum operational scenarios through the tests of various network operational plans.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.40 no.3
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• pp.237-242
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• 2012

Spaceborne pulse tube-type cryogenic compressors are widely used for space applications. To guarantee cooling performance of the compressor, mission life time and micor-vibration stability, suitable thermal control of compressor is required. Micro-vibration of the compressor is the one of the sources to degrade the pointing performance of observation satellite. In the present work, on-orbit thermal design of compressor in order not to degrade the performance of micro-vibration isolation system keeping the thermal control performance has been proposed and investigated through thermo-mechanical analysis.

• 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.

• Transactions of the Korean Society of Automotive Engineers
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• v.13 no.3
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• pp.154-161
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• 2005

The durability of a vehicle is a very important performance which can be evaluated from endurance test. This study developed a procedure for determination of a duty cycle theoretically. Vehicle load data is classified and rearranged using standard test road profile. A load pattern and a duty cycles are extracted from classified vehicle data using genetic algorithm. A duty cycle could be utilized in dynamo test to meet required test mileage. The derived duty cycles have been verified by fatigue test through the dynamometer test.

• Bulletin of the Korean Space Science Society
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• 2003.10a
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• pp.97-97
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• 2003

아리랑위성 1호는 1999년 12월 21일 발사되어 3년의 설계 임무 수명을 성공적으로 완료하였으며 현재 위성체의 특이한 이상 상태 없이 안정적으로 연장 운영되고 있다. 위성이 성공적으로 임무를 수행하기 위해서는 태양전지 및 배터리 등의 기능이 적절하게 유지되어야 한다. 위성의 전력을 생산하는 태양 전지는 여러 가지 복사 및 운영중의 온도차와 같은 우주환경 등에 의해서 서서히 성능이 감소하게 되고, 배터리 또한 온도상승 등으로 인해서 성능이 감소하게 된다. 또한 위성의 궤도평면과 태양 벡터 사이의 각으로 정의되는 베타각($\beta$)에 의해서 식기간의 변화 및 온도 변화로 인해서 전력계에도 변화가 발생한다. 본 논문에서는 정상운영 초기부터 현재까지 실제 운영 궤도상에서 얻어진 원격계측자료(Telemetry)를 이용하여 전력계의 주요 부분 변화를 살펴보았다.

• Proceedings of the KIPE Conference
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• 2008.06a
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• pp.167-168
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• 2008

인공위성에서 궤도 변경에 사용되는 추진계를 제외한 인공위성 본체와 탑재체의 모든 기능은 전기에너지를 이용하여 임무를 수행한다. 이러한 전기에너지가 태양전지 배열기에 의해 생성되는 만큼, 태양전지 배열기의 설계는 인공위성 개발에서 매우 중요하다. 인공위성을 위한 태양전지 배열기는 발사시의 충격과 우주환경에서의 방사능에 대한 노출을 직접적으로 받으므로 견고하게 제작되어야 하며, 인공위성의 수명 말기까지 위성 운용을 위한 충분한 전력을 생산하도록 설계되어야 한다. 본 논문에서는 저궤도 인공위성을 위한 태양전지 배열기의 제작 및 설계에 관하여 기술한다.

• Journal of the Korean Society for Railway
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• v.4 no.4
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• pp.138-146
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• 2001

For the purpose of the effective maintenance of surface irregularities of rail, this paper investigates the rail service life to a bending fatigue failure of welding parts of rail on the slab track by the structures laboratory testing to derive S-N curves, a GTDAP(General Track Dynamic Analysis Program) to calculate the stresses and a modified Miner's rule to predict a fatigue life. The useful guides for maintenance of rail welded parts on the slab track are proposed in terms of a grinding period and the depth of rail surface irregularities. This study also proposed the guides for maintenance of rail welded part on the ballast track. The effects of fatigue service lives are compared one another.

• Proceedings of the Korean Vacuum Society Conference
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• 2014.02a
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• pp.140.1-140.1
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• 2014

인공위성은 지상에서 발사된 후 로켓에 의해 임무궤도에 안착을 한 뒤 위성 내부에 탑재된 추진시스템에 의하여 자세 및 궤도제어를 수행한다. 특히, 저궤도 관측위성의 경우 정확한 이미지 촬영을 위해서는 자세제어가 매우 중요하고, 추진체의 잔여량에 따라 인공위성의 수명이 결정되기도 하므로 추진시스템의 역할이 매우 중요하다. 특히, 추진체의 무게에 따라 위성 전체 중량이 좌우되어 발사중량에도 영향을 미치게 되므로 고성능, 저질량의 추진계가 요구되며, 추진계는 극히 미세한 누설도 허용되지 않는다. 개발된 인공위성 추진계 내부의 누설 여부 확인을 위하여 우주환경을 모사한 진공챔버 내부에서 고압으로 충진된 추진 탱크의 누설탐지 시험을 수행하게 된다. 본 논문에서는 지상에서 모사된 우주환경 하에서 인공위성 추진계의 누설 탐지 기법에 대해 알아보고자 한다.