• Title/Summary/Keyword: COMS (Communication, Ocean and Meteorological Satellite)

검색결과 198건 처리시간 0.029초

Structural Design Development of GOCI

  • Yeon Jeoung-Heum;Kang Song-Doug;Kim Jongah;Kang Gurrl.sil;Myung Hwan-Chun;Youn Heong-Sik
    • 대한원격탐사학회:학술대회논문집
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    • 대한원격탐사학회 2005년도 Proceedings of ISRS 2005
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    • pp.104-107
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    • 2005
  • COMS(Communication, Ocean, and Meteorological Satellite) is the geostationary satellite for the mission of satellite communication, ocean monitoring, and meteorological service. It is scheduled to be launched at the end of 2008. Ocean payload of COMS named as GOCI(Geostationary Ocean Color Imager) observes ocean color and derives the chlorophyll concentrlition, the concentration of dissolved organic material and so on. In operational oceanography, satellite derived data products are used to provide forecasting and now casting of the ocean and coastal water state. In this work, conceptual design of structural part of GOCI is carried out and two baseline concepts are proposed. The one is dioptric module that uses lens system and the other is TMA(Three Mirror Anastigmat) module that uses mirror system. Trade-off studies between two concepts are investigated by considering optical and mechanical performances. Finally, on-going tasks and future development plan are briefly discussed.

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COMPONENT TEST STRATEGY FOR COMS ON-BOARD SOFTWARE USING ATTOL

  • Park, Su-Hyun;Kang, Soo-Yeon;Yang, Koon-Ho;Choi, Seong-Bong
    • 대한원격탐사학회:학술대회논문집
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    • 대한원격탐사학회 2007년도 Proceedings of ISRS 2007
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    • pp.175-178
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    • 2007
  • COMS (Communication Ocean Meteorological Satellite) is the geostationary satellite being developed by Korea Aerospace Research Institute for multi-mission: experimental communication, ocean monitoring and meteorological observations. The COMS operation is controlled by the on-board software running on the spacecraft central computer. The software is written in ADA language and developed under the software life cycle: Requirement analysis, Design, Implementation, Component test and Integration test. Most functional requirements are tested at component level on a software component testing tool, ATTOL. ATTOL provides a simple way to define the test cases and automates the test program generation, test execution and test analysis. When two or more verified components are put together, the integration test starts to check the non-functional requirements: real-time aspect, performance, the HW/SW compatibility and etc. This paper introduces the COMS on-board software and explains what to test and how to test the on-board software at component level using ATTOL.

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COMPONENT TEST STRATEGY FOR COMS ON-BOARD SOFTWARE USING ATTOL

  • Park, Su-Hyun;Kang, Soo-Yeon;Yang, Koon-Ho;Choi, Seong-Bong
    • 대한원격탐사학회:학술대회논문집
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    • 대한원격탐사학회 2007년도 Proceedings of ISRS 2007
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    • pp.460-463
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    • 2007
  • COMS (Communication Ocean Meteorological Satellite) is the geostationary satellite being developed by Korea Aerospace Research Institute for multi-mission: experimental communication, ocean monitoring and meteorological observations. The COMS operation is controlled by the on-board software running on the spacecraft central computer. The software is written in ADA language and developed under the software life cycle: Requirement analysis, Design, Implementation, Component test and Integration test. Most functional requirements are tested at component level on a software component testing tool, ATTOL. ATTOL provides a simple way to define the test cases and automates the test program generation, test execution and test analysis. When two or more verified components are put together, the integration test starts to check the non-functional requirements: real-time aspect, performance, the HW/SW compatibility and etc. This paper introduces the COMS on-board software and explains what to test and how to test the on-board software at component level using ATTOL.

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천리안 위성을 사용한 방출장파복사량 검증 : 청미천, 설마천 (Assessment of Outgoing Longwave Radiation using COMS : Cheongmi and Sulma Catchments)

  • 백종진;서찬양;최민하
    • 한국수자원학회논문집
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    • 제46권5호
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    • pp.465-476
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    • 2013
  • 방출장파복사량은 수치예보모형, 수문모형, 증발산 등에 사용되는 인자로 지구의 에너지 균형을 이해하는데 필수적이다. 현재 국내외에서는 이를 정확하게 관측하기가 어려우며, 또한 공간적인 제약이 따른다. 따라서, 본 연구에서는 원격탐사 기술을 적용함으로써 지상관측의 단점을 보완하기 위해 정지궤도 위성인 Communication, Ocean and Meteorological Satellite (COMS)를 사용하여 방출장파복사량(Outgoing Longwave Radiation, $R_{lu}$ )를 계산하였다. 이 자료의 검증을 위해 유량조사사업단에서운영 관리하는 청미천/설마천 Flux Tower의 자료를 사용하여 계산된 $R_{lu}$ 와 MODIS 위성자료를 사용하여 계산된 $R_{lu}$ 를 비교 및 검증하였다. 전반적으로 COMS의 자료가 높은 상관계수를 나타내어 COMS의 사용가능성을 보여주었다. 이러한 결과를 바탕으로 향후 COMS를 이용한 증발산 산정 연구를 할 계획이다.

정지궤도 위성의 열해석 모델 보정 (THERMAL MODEL CORRELATION OF A GEOSTATIONARY SATELLITE)

  • 전형열;김정훈
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2011년 춘계학술대회논문집
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    • pp.230-235
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    • 2011
  • COMS (Communication, Ocean and Meteorological Satellite) is a geostationary satellite and was developed by KARI for communication, ocean and meteorological observations. COMS was tested under vacuum and very law temperature conditions in order to correlate thermal model and to verify thermal design. The test was performed by using KARI large thermal vacuum chamber. The COMS S/C thermal model was successfully correlated versus the 2 thermal balance test phases. After model correlation, temperatures deviation of all individual unit were less than $5^{\circ}C$ and global deviation and standard deviation also satisfied the requirements, less than $2^{\circ}C$ and $3^{\circ}C$. The final flight prediction was performed by using the correlated thermal model.

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지구 정지궤도 위성의 열해석 모델 보정 (THERMAL MODEL CORRELATION OF A GEOSTATIONARY SATELLITE)

  • 전형열;김정훈
    • 한국전산유체공학회지
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    • 제16권3호
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    • pp.59-65
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    • 2011
  • COMS (Communication, Ocean and Meteorological Satellite) is a geostationary satellite and was developed by KARI for communication, ocean and meteorological observations. COMS was tested under vacuum and very low temperature conditions in order to correlate thermal model and to verify thermal design. The test was performed by using KARI large thermal vacuum chamber. The COMS S/C thermal model was successfully correlated versus the 2 thermal balance test phases. After model correlation, temperatures deviation of all individual units were less than $5^{\circ}C$ and global deviation and standard deviation also satisfied the requirements, less than $2^{\circ}C$ and $3^{\circ}C$. The final flight prediction was performed by using the correlated thermal model.

천리안위성 기상탑재체의 스캔미러 방사율 보정 (Scan Mirror Emissivity Compensation for the COMS MI)

  • 서석배;진경욱;안상일
    • 항공우주기술
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    • 제10권1호
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    • pp.156-166
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    • 2011
  • 천리안위성은 대한민국 최초의 정지궤도 지구관측위성으로써 기상탑재체와 해양탑재체를 이용하여 24시간 지구관측 임무를 수행한다. 위성은 궤도상 시험을 성공적으로 완료하고 2011년 4월부터 정상운영 중이다. 본 논문에서는 천리안위성 기상탑재체의 스캔미러 방사율 보정 알고리즘 및 이의 소프트웨어 구현에 대해서 설명한다.

Implementation and Validation of Earth Acquisition Algorithm for Communication, Ocean and Meteorological Satellite

  • Park, Sang-Wook;Lee, Young-Ran;Lee, Byoung-Sun;Hwang, Yoo-La;Lee, Un-Seob
    • Journal of Astronomy and Space Sciences
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    • 제28권4호
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    • pp.345-354
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    • 2011
  • Earth acquisition is to solve when earth can be visible from satellite after Sun acquisition during launch and early operation period or on-station satellite anomaly. In this paper, the algorithm and test result of the Communication, Ocean and Meteorological Satellite (COMS) Earth acquisition are presented in case of on-station satellite anomaly status. The algorithms for the calculation of Earth-pointing attitude control parameters including those attitude direction vector, rotation matrix, and maneuver time and duration are based on COMS configuration (Eurostar 3000 bus). The coordinate system uses the reference initial frame. The constraint calculating available time-slot to perform the earth acquisition considers eclipse, angular separation, solar local time, and infra-red earth sensor blinding conditions. The results of Electronics and Telecommunications Research Institute (ETRI) are compared with that of the Astrium software to validate the implemented ETRI software.

천리안 위성 적외 영상 자료를 이용한 태풍의 최대풍속반경 산출 및 통계적 특성 (Estimation and Statistical Characteristics of the Radius of Maximum Wind of Tropical Cyclones using COMS IR Imagery)

  • 권민호
    • 대기
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    • 제22권4호
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    • pp.473-481
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    • 2012
  • The objective methods estimating the radius of maximum wind (RMW) of tropical cyclones (TCs) are discussed using infraed (IR) imagery of geostationary satellite, and an alternative method is suggested that can estimate RMW in the TCs having eyes using IR imagery. The RMW-estimating methods are based on the characteristic structure of the eyewall of a tropical cyclone. RMW is dependent upon the radius of the eye and the distance from the center to the top of the most developed convective cloud. In order to test these methods, blackbody brightness temperature of Korean geostationary satellite, COMS (Communication, Ocean, and Meteorological Satellite) IR imagery are utilized in this study. The estimated RMWs are compared with surface winds of ASCAT (Advanced Scatterometer) of a polar orbiting satellite.

천리안위성 기상자료처리를 위한 컴포넌트 기반의 시스템 아키텍처 설계 (A Design of Component-based System Architecture for COMS Meteorological Data Processing)

  • 조상규;김병길;사공영보
    • 한국위성정보통신학회논문지
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    • 제9권1호
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    • pp.65-69
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    • 2014
  • 통신해양기상위성 자료처리시스템(CMDPS)은 기상 관측과 기상 예측을 지원하기 위해서 국가기상위성센터에 의해서 개발되었고, 16종 기상자료(Level 2)를 생성하고 있다. 현재 CMDPS는 후속 기상위성자료처리를 위한 시스템 확장이나 통합 S/W에 대한 효율성, 유지관리 관점에서 다소 문제가 있다. 이러한 문제를 해결하기 위해서, 본 논문에서는 확장성을 갖는 통신해양기상위성 기상자료처리를 위한 컴포넌트 기반 시스템 아키텍처를 제안하였다. 제안된 시스템은 확장 가능한 아키텍처를 갖는 컴포넌트 기반의 프레임워크를 채택하고 있으며, 신규 위성자료처리 알고리즘 개발과 시스템 유지관리를 위해 손쉬운 방법을 제공할 것으로 기대된다.