• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2008년도 International Symposium on Remote Sensing
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• pp.88-91
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• 2008

The COMS IMPS (Communication Ocean and Meteorological Satellite IMage Pre-processing Subsystem) is developed for image pre-processing of COMS. For a test of the COMS IMPS, 7 support software are developed in KARI GS using simulated MI/GOCI WB (Wide-Band) data; COMS Fill Adder, MI (Meteorological Imager) CADU generator, GOCI (Geostationary Ocean Colour Imager) CADU generator, COMS CADU combiner, MI SD (Sensor Data) analyzer, GOCI SD analyzer, and COMS DM (Decomposition Module) test harness. This paper explains functions of developed support software and the COMS IMPS test using those software.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2006년도 Proceedings of ISRS 2006 PORSEC Volume I
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• pp.271-273
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• 2006

In this paper, we describe the MI2U ORB function which is a part of the flight software executed on SCU and controls MI2U/MI which is one of three payloads on COMS. The MI2U ORB function manages MI2U/MI redundancy and reconfiguration, monitors MI2U/MI equipment, performs FDIR, and provides the routing service of commands from Ground/IP (Interpreted Program) through the current used 1553 channel. The MI2U hardware achieves the interface between the SCU and the MI. The MI2U is connected to SCU through MIL-STD-1553B system bus. The MI2U has the internal redundancy but is used in cold redundancy. The MI2U ORB function considers that they are not expected to be simultaneously switched on. The connection combination between MI2U and MI is electrically cross-strapped. However the MI2U ORB function considers only two combinations (MI2U A + MI 1, MI2U B + MI 2). Other combinations can be manually achieved by ground in case of the emergency case.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2006년도 Proceedings of ISRS 2006 PORSEC Volume I
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• pp.159-162
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• 2006

This paper describes the ground system for COMS (Communication, Ocean, and Meteorological Satellite), the first Korean multi-purposed geostationary satellite, at MSC (Meteorological Satellite Center) in Korea. The overview of COMS MI (Meteorological Imager) will be introduced as well. KMA would implement mission planning for COMS MI operation and receive, process, interpret, disseminate, and archive MI data operationally for domestic and foreign user groups. Major missions of COMS MI are mitigation of natural hazard such as typhoon, dust storm, and heavy rain, and short-term warning of severe weather to protect human health and commerce. Moreover, research of climate variability and long-term changes will be supported. In accordance with those missions, the concept and design of COMPASS (COMS operation and meteorological products application service system), the ground system for COMS MI in MSC, have been setting up since 2004. Currently, COMPASS design is being progressed and will have finished the end of 2006. The development of COMPASS has three phases: first phase is development of fundamental COMPASS components in 2007, second phase is to integrate and test all of the COMPASS components in 2008, and the last phase is to operate COMPASS after COMS In-Orbit Tests in 2009.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2006년도 Proceedings of ISRS 2006 PORSEC Volume I
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• pp.71-74
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• 2006

Communication Ocean Meteorological Satellite (COMS) is planned to be launched onto Geostationary Earth Orbit in 2008. The meteorological imager (MI) is one of COMS payloads and has 5 spectral channels to monitor meteorological phenomenon around the Korean peninsular intensively and of Asian-side full Earth disk periodically. The MI has on-board radiometric calibration capabilities called 'blackbody calibration' for infrared channels and 'space look' for infrared/visible channels, and radiometric response stability monitoring device called 'albedo monitor' for visible channel. Additionally the MI has on-board function called 'electrical calibration' for the check of imaging path electronics of both infrared and visible channels. The characterization of MI performance is performed to provide the pre-launch radiometric calibration data which will be used for in-orbit radiometric calibration with the on-board calibration outputs. The radiometric calibration of the COMS MI is introduced in the view point of instrument side in terms of in-orbit calibration devices and capabilities as well as the pre-launch calibration activities and expected outputs.

• 항공우주기술
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• 제6권2호
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• pp.66-72
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• 2007

정지궤도위성은 통신 탑재체와 관측 탑재체를 동시에 장착하는 정지궤도 위성으로, 본 논문에서 언급되는 MI2U는 관측 탑재체의 하나인 기상센스와의 접속 및 전원공급을 위한 유닛이다. 본 논문에서는 기상탑재체 접속장치 ORB의 검증시험 방법을 제안하고 제안된 내용에 따라 시험을 수행하였으며, 결과에 대한 분석하고 향후 시험방향을 제시한다.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2006년도 Proceedings of ISRS 2006 PORSEC Volume I
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• pp.290-293
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• 2006

COMS (Communication, Ocean and Meteorological Satellite) shall be operated with two remote sensing payloads, MI (Meteorological Imager) and GOCI (Geostationary Ocean Color Imager). Since both payloads have rotating mechanisms, the dynamic coupling between two payloads is very important considering the pointing stability during GOCI operation. In addition, COMS adopts a single solar wing to improve the image quality, which leads to the unbalanced solar pressure torque in COMS. As a result, the off-loading of the wheel momentum needs to be performed regularly (2 times per day). Since the frequent off-loading could affect MI/GOCI imaging performance, another suboptimal off-loading time needs to be considered to meet the AOCS design requirements of COMS while having margin enough in the number of thruster actuations. In this paper, preliminary analysis results on the pointing stability and the wheel off-loading time selection with respect to MI/GOCI operations are presented.

• 항공우주기술
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• 제11권2호
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• pp.12-18
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• 2012

이 논문에서는 식기간 동안 미광(stray light)에 의해 천리안 기상 영상이 받게 되는 영향에 대해 분석하였으며 미광의 영향을 제거하기 위한 방법 또한 모색하였다. 기상영상의 경우 식기간 동안 미광의 영향을 받아 영상의 왜곡 (줄무늬 등)문제가 발생한다. 미광의 영향에 대한 정량적 분석이 천리안위성의 궤도상 시험기간 동안에 이루어졌으며, 천리안위성 기상탑재체의 총 4개 적외 채널에 대해 태양과의 거리에 따른 미광의 영향이 분석되었다. 본 연구에서는 계산된 천리안위성의 식기간 자료를 바탕으로 미광의 영향이 매우 강한 사례를 선정하여 적외채널 영상의 미광에 의한 오염 정도를 조사하였다. 또한 영상에 나타난 미광의 영향을 두 개의 열적외 채널을 이용하여 단파적외 채널을 대체하는 방법이 유효함을 확인 하였다.

• 대한원격탐사학회지
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• 제37권6_1호
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• pp.1767-1772
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• 2021

장기간에 걸친 전 지구적인 위성관측 지표면 알베도 자료는 전 지구 기후 및 환경의 변화 감시에 활발히 이용되고 있으며 그 활용도와 중요성이 크다. 우리나라의 경우 정지궤도위성 천리안위성 1호(Communication, Ocean and Meteorological Satellite, COMS) MI(Meteorological Imager) 센서와 천리안위성 2A호(GEO-KOMPSAT-2A, GK-2A) AMI (Advanced Meteorological Imager) 센서의 세대교체를 통해 지속적인 지표면 알베도 산출물의 확보가 가능하다. 그러나 COMS/MI 및 GK-2A/AMI의 지표면 알베도 산출물은 센서 및 알고리즘의 차이로 인해 산출물 간의 차이가 존재한다. 따라서 COMS/MI와 GK-2A/AMI 지표면 알베도 산출 기간을 확장하고 지속적인 기후변화 감시 연계성 확보를 위해 두 위성 산출물 간의 오차 분석이 선행되어야 한다. 본 연구에서는 COMS/MI 및 GK-2A/AMI 지표면 알베도 자료의 중복기간을 대상으로 지상관측자료 AERONET (Aerosol Robotic Network)와 타 위성자료 GLASS (Global Land Surface Satellite)와 함께 비교 분석하였다. 오차 분석 결과 AERONET과의 검증에서 COMS/MI의 평균 제곱근 오차(Root Mean Square Error, RMSE)가 0.043로 GK-2A/AMI의 RMSE인 0.015보다 높게 나타났다. 또한 GLASS와 비교하였을 때 COMS/MI의 RMSE는 0.029로 GK-2A/AMI의 0.038보다 낮게 나타났다. 이러한 오차특성을 이해하고 COMS/MI 및 GK-2A/AMI의 지표면 알베도 자료를 사용할 때 장기간 기후변화 감시에 적극적으로 활용할 수 있을 것이다.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2004년도 Proceedings of ISRS 2004
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• pp.382-385
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• 2004

Communication Ocean Meteorological Satellite (COMS) for the hybrid mission of meteorological observation, ocean monitoring, and telecommunication service is planned to be launched onto Geostationary Earth Orbit in 2008 according to the Korea national space program. A feasibility study on the solar constraint in the operation of the COMS meteorological imager (MI) is performed using the GOES imager hardware operation characteristics. The Earth observation areas of the MI are introduced and the observation time of the MI observation area is calculated. The sun light can enter into the MI optical system around the local midnight and impinge on the performance of the MI. The solar eclipse viewed from the satellite occurs near local midnight around the equinox. This study discusses the restriction of imaging operation time that should be considered in order to avoid the solar intrusion about local midnight and to keep acceptable image quality for the MI observation areas. This study could be useful to build the operation concept of the MI during the development of the MI.

• 항공우주시스템공학회지
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• 제3권2호
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• pp.24-30
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• 2009

MI LV1B images, geometric corrected data of COMS MI, has no time information per each line, but field of weather prediction using the MI LV1B images needs time information on it. This paper explains two calculation methods for receiving time on lines of MI LV1B images and analyzes difference between two calculation methods using simulated data.