• 천문학회보
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• 제42권2호
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• pp.58.1-58.1
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• 2017

The NISS (Near-infrared Imaging Spectrometer for Star formation history) is the near-infrared spectro-photometric instrument optimized to the first Next Generation of small satellite (NEXTSat-1). The off-axis optics was developed to cover a wide field of view with 2 deg. ${\times}$ 2 deg. as well as a wide wavelength range from 0.95 to $2.5{\mu}m$. Considering the simple alignment scheme, afocal system was adapted in the optical components. The mechanical structures were tested under the space environment. We have obtained the accurate calibration data using our test facilities under the operational condition. After the final integration of flight model into the satellite, the communication with the satellite and the functional test were passed. The NISS will be launched in early 2018. During around 2-year operation, the spectro-photometric survey covering more than 100 square degree will be performed. To achieve the major scientific objectives for the study of the cosmic star formation in local and distant universe, the main observational targets will be nearby galaxies, galaxy clusters, star-forming regions and low background regions. Here, we report the final performance of the flight model of the NISS.

• 한국위성정보통신학회논문지
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• 제9권3호
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• pp.22-26
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• 2014

본 연구에서는 액정의 수직배향을 달성하기 위해서 특별히 제조된 폴리스타일렌 박막에 다양한 이온빔을 조사하는 방법을 사용하였다. 일반적으로 폴리스타일렌 수지는 통상의 폴리이미드 계열의 수지에 비해서 박막코팅을 하였을 때 보다 우수한 투과율을 나타내므로, 투과형 디스플레이로 사용되는 LCD의 배향막 재료로 더 적합하다고 생각되었다. 특히 고휘도이면서 저전력 사양을 달성하여야 하는 휴대용 디스플레이에서의 응용가능성이 기대되었다. 그러나, 일반적인 러빙법에 의한 배향처리에 대해서는 액정분자의 배향성이 폴리이미드 계열의 재료에 비해서 열등하여 사용되지 못하였다. 본 연구에서는 폴리스타일렌 계열의 박막재료를 배향막으로 가공함에 있어서 새로운 이온빔 조사법에 의한 비접촉식 배향법을 사용하였으며, 배향성과 액정분자의 프리틸트각 특성에 대해서 정량적인 결과를 얻을 수 있었다. 실험에서는 폴리스타일렌 수지에 이온빔의 조사시간을 15초까지 변화시키면서 액정분자의 배향성 및 프리틸트각의 특성을 측정하였다. 측정결과 스마트폰 및 휴대용 정보단말기 등의 디스플레이에 적합한 고투과율 액정표시소자의 구현이 가능하였다.

• Korean Journal of Geomatics
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• 제3권1호
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• pp.15-22
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• 2003

This study aims to construct a management system of road position information as part of the build-up to a maintenance and management system of highways. First, information on the positions of the roads were obtained by a real-time kinematic satellite surveying, and then the degree of accuracy was analyzed in comparison with the data of the existing design drawings. The linear coordinates of road center line obtained by using RTK GPS showed about 7.6-13.2cm errors in X and Y directions in the case of the national road No.2 section, and about 8.4-9.2cm errors in the case of local road No.1045 section. These errors were within the tolerance scope regulated by the TS survey, and could be practically used. In the case of vertical alignment, there were about 6.2cm errors in the Z direction in local road No.1045 section. Aerial photographs are normally used in producing numerical maps, and it can be practically used because the tolerance scope of the elevation control point is l0cm when the scale of aerial photographs is 1/1000. The management system of road position information, utilizing Object-Oriented Programming(OOP), was built having the data acquired in this way as the attribute data. The system developed in this way can enable us to spot the positions of road facilities, the target of management with ease, to easily update the data in case of changes in the positions of roads and road facilities, and to manage the positions of roads and road facilities more effectively.

• 한국동물생명공학회지
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• 제36권4호
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• pp.314-322
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• 2021

Paired box protein, PAX7, is a key molecule for the specification, maintenance and skeletal muscle regeneration of muscle satellite cells. In this study, we identified and characterized the cDNA and amino acid sequences of PAX7 from black sea bream (Acanthopagrus schlegelii) via molecular cloning and sequence analysis. A. schlegelii PAX7 cDNA was comprised of 1,524 bp encoding 507 amino acids and multiple sequence alignment analysis of the translated amino acids showed that it contained three domains including paired DNA-binding domain, homeobox domain and OAR domain which were well conserved across various animal species investigated. Pairwise Sequence Alignment indicated that A. schlegelii PAX7 had the same amino acid sequences with that of yellowfin seabream (A. latus) and 99.8% identity and similarity with that of gilt-head bream (Sparus aurata). Molecular phylogenetic analysis confirmed that A. schlegelii PAX7 formed a monophyletic group with those of teleost and most closely related with those of the fish that belong to Sparidae family including A. latus and S. aurata. In the investigation of its tissue specific mRNA expression, the expression was specifically identified in skeletal muscle tissue and a weak expression was also shown in gonad tissue. The cultured cells derived from skeletal muscle tissues expressed PAX7 mRNA at early passage but the expression was not observed after several times of subculture.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2005년도 Proceedings of ISRS 2005
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• pp.182-185
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• 2005

Satellite cameras are calibrated before launch in detail and in general, but it cannot be guaranteed that the geometry is not changing during launch and caused by thermal influence of the sun in the orbit. Modem satellite imaging systems are based on CCD-line sensors. Because of the required high sampling rate the length of used CCD-lines is limited. For reaching a sufficient swath width, some CCD-lines are combined to a longer virtual CCD-line. The images generated by the individual CCD-lines do overlap slightly and so they can be shifted in x- and y-direction in relation to a chosen reference image just based on tie points. For the alignment and difference in scale, control points are required. The resulting virtual image has only negligible errors in areas with very large difference in height caused by the difference in the location of the projection centers. Color images can be related to the joint panchromatic scenes just based on tie points. Pan-sharpened images may show only small color shifts in very mountainous areas and for moving objects. The direct sensor orientation has to be calibrated based on control points. Discrepancies in horizontal shift can only be separated from attitude discrepancies with a good three-dimensional control point distribution. For such a calibration a program based on geometric reconstruction of the sensor orientation is required. The approximations by 3D-affine transformation or direct linear transformation (DL n cannot be used. These methods do have also disadvantages for standard sensor orientation. The image orientation by geometric reconstruction can be improved by self calibration with additional parameters for the analysis and compensation of remaining systematic effects for example caused by a not linear CCD-line. The determined sensor geometry can be used for the generation? of rational polynomial coefficients, describing the sensor geometry by relations of polynomials of the ground coordinates X, Y and Z.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2006년도 춘계학술대회논문집
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• pp.376-379
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• 2006

Reaction Wheel Assembly (RWA) is one of the major disturbance sources that have influence upon the Line of Sight (LOS) of payload. A micro-vibration induced by RWA is propagated through the satellite structure and decrease the LOS stability performance of payload. This effect shall be analyzed through the jitter analysis. If a requirement or specification of payload jitter level is found to be not satisfied according to the jitter analysis campaign, some modification or redesign should be done on the satellite structure or a couple of isolator should be attached on the RWA interface in order to reduce the transmitted vibration level of RWA. The purpose of ???RWA isolator test? is to roughly evaluate the performance of vibration suppression level with a passive RWA isolator made of rubber. For this test, actual RWA is used as a vibration source and a couple of cube-shaped rubber mount designed for satellite is used as a passive isolator. There may be several considerations in order to accommodate RWA isolator to spacecraft such as not only vibration reduction performance but also thermal conduction problem, mechanical size, RWA alignment problem, etc. But in this report the feasibility of RWA isolator is analyzed only in a vibration suppression point of view. As a result, high frequency vibration of RWA above 50Hz is perfectly attenuated with isolators, however, first harmonic components below 50Hz became larger due to the additional low frequency resonance modes of roll, pitch, yaw rigid body motion of RWA+bracket.

• 한국산학기술학회논문지
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• 제21권2호
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• pp.1-7
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• 2020

현대 사회에서는 기술의 고도화와 인간의 생활 영역이 확대됨에 따라 시간과 장소의 제약 없이 고품질 음성, 영상 등의 통신 서비스를 제공 받고자하는 요구가 증가하고 있다. 이러한 요구에 대응하여 지역적인 거리에 영향을 받지 않고 광범위한 통신 반경을 제공하고 다중접근이 가능한 위성 통신 시스템이 나날이 발전하고 있으며 DVB-RCS, WIN-T 등의 위성 통신 체계에서는 효율적인 자원 할당을 위해 복수의 주파수 대역에서 시간을 분할하여 할당하는 기법인 MF-TDMA DAMA 다중접속 방식을 사용하고 있다. 이 방식의 경우, 망제어기에 위성 단말들이 주기적으로 자원을 요청하고 이에 따라 망제어기는 동적으로 자원을 할당하게 되므로 수시로 자원할당 정보의 정렬이 필요하다. 이런 정렬 시간의 단축은 원거리 송수신에 의해 긴 전송지연 시간이 발생하는 위성 통신 시스템에서는 더욱더 중요한 요소로 작용한다. 본 논문은 MF-TDMA DAMA 위성통신 시스템에서 자원할당 정보 정렬 시 최대 프레임 개수를 임계값으로 두고 임계값을 기준으로 정렬 알고리즘을 교차 선택하여 정렬 시간을 단축하는 정렬 알고리즘 가변 선택 기법을 제안한다.

• 한국항행학회논문지
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• 제16권5호
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• pp.738-743
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• 2012

INS/GPS 통합 항법 필터는 주로 칼만 필터를 이용하여 구성되고 있다. 그러나 낮은 성능의 관성 센서를 이용한 INS/GPS 통합 항법 필터의 경우 센서 오차 레벨 등의 문제로 인해 정확한 방위각 정보의 제공이 곤란하며, 이로 인해 통합 필터를 구성하는 칼만 필터의 추정 성능이나 안정성을 보장할 수 없게 된다. 본 논문에서는 칼만 필터와 파티클 필터의 결합된 형태의 국지선형 파티클 필터를 이용하여 초기 방위각 오차를 극복할 수 있는 방법을 제시하였다.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2005년도 Proceedings of ISRS 2005
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• pp.601-603
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• 2005

Refocusing methods are used to compensate optical performance degradation of high resolution satellite camera during on-orbit operation. Due to mechanical vibration during launch and thermal vacuum environment of space where camera is exposed, the alignment of optical system may have error. The focusing error is dominant of misalignment and caused by the de-space error of secondary mirror of catoptric camera, which is most sensitive to vibration and space environment. The high resolution camera of SPOT, Pleiades and KOMPSAT2 have refocusing device to adjust focusing during orbital operation while QuickBird of US does not use on orbit refocusing method. For the Korsch type optical configuration which is preferred for large aperture space remote sensing camera, secondary mirror and folding mirror are available as refocusing element.

• 항공우주시스템공학회지
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• 제12권4호
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• pp.64-74
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• 2018

고해상도 지구관측 위성의 성공적인 임무 수행을 위하여 궤도 진입 후 리포커싱 과정은 필수적으로 요구된다. 마이크론 단위의 정밀한 광학 정렬을 요하는 광학 위성카메라는 발사 전 충분한 정렬 과정을 거치지만 발사 및 운용 과정에서 외부 환경에 의한 광부품의 정렬오차가 발생하게 된다. 기존의 지구관측위성들은 지상과의 통신을 통한 오프라인 방식의 리포커싱을 수행해왔으며 이는 비용 시간적 측면에서 비효율적이다. 따라서 본 논문에서는 궤도 상에서 자동초점 정렬과정이 수행되는 온라인 리포커싱 알고리즘을 제안하였다. 또한 부경의 틸팅에 따른 광학적 효과를 리포커싱 알고리즘에 적용하여 디스페이스 외 틸팅이 발생한 위성카메라에도 적용되도록 개발하였다. 리포커싱 알고리즘의 개발 및 성능평가를 위하여 실험실 수준의 광학계를 설계하였으며, 이를 기반으로 데이터를 추출하여 부경 정렬오차에 따른 MTF(Modulation Transfer Function) 경향성을 파악하였다. MTF 경향성을 바탕으로 궤도상에서의 De-space VS MTF 함수를 추정하여 알고리즘을 개발하였다. 리포커싱 알고리즘의 성능 평가는 MATLAB과 CODE V의 연동 시뮬레이션을 통하여 수행되었다.