• Title/Summary/Keyword: 다목적실용위성2호(KOMPSAT-2)

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A Conceptual Design of Integrated Receiving end for Multi-Satellite Mission Data Processing (다중위성 운영을 위한 통합 자료처리 시스템의 개념적 설계)

  • Bae, Hee-Jin;Chae, Tae-Byeong;Oh, Seung-Hyeub
    • Journal of Korea Society of Industrial Information Systems
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    • v.15 no.2
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    • pp.17-22
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    • 2010
  • Establishment of systematic platform is needed for technological progress of receiving of satellite image data with high quality and processing system for product generation and operation related with direct receiving system for satellite from abroad. Besides, it's necessary to develop the integrated data processing system to prohibit similar functions on developing (or being developed) for KOMPSAT-3, KOMPSAT-5 and to operate system efficiently. Therefore, conceptual design of the integrated data processing system is performed considering commercialization of KOMPSAT(Korea Multi-Purpose Satellite) series based on KOMPSAT-2 IRPE on operation in this paper.

Design of Numerical Functions for KOMPSAT-2 Coprocessor (다목적실용위성 2호 코프로세서를 위한 수치연산프로그램 설계)

  • 최종욱;천이진;이재승
    • Proceedings of the Korean Information Science Society Conference
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    • 2003.10a
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    • pp.235-237
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    • 2003
  • 다목적실용위성 2호(KOMPSAT-2)에서는 위성자세 제어를 담당하고 있는 RDU(Remote Drive Unit)의 성능 향상를 위하여 80386 CPU와 함께 80387 Coprocessor를 장착하여 임무수행을 담당한다. 다목적실용위성 1호(KOMPSAT-1)에서는 수치연산을 위하여 상용소프트웨어인 PACLIB를 사용하여 수치연산을 80C186을 이용한 에뮬레이션 방식으로 수행하였지만, 2호기에서는 실질적인 코프로세서를 이용한 수치연산을 수행하게 된다. 본 논문에서는 다목적실용위성 2호에서 사용되는 80387 코프로세서의 초기화 과정과 예외사항 발생시 처리 방법, 80387 코프로세서를 이용한 수치연산 함수 구현 및 libtary 구성 방법에 대하여 설명한다.

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The construction of KOMPSAT-2 User Support System (다목적실용위성 2호 영상자료 사용자 지원체계 구축)

  • Jeon, Gap-Ho;Jeon, Jeong-Nam;Lee, Seon-Gu;Kim, Yun-Su
    • Proceedings of the KSRS Conference
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    • 2007.03a
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    • pp.120-125
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    • 2007
  • 다목적실용위성 2호(KOMPSAT-2)는 2006년 7월 28일 러시아 플레세츠크(Plesetsk) 발사장에서 성공적으로 발사되어 현재 초기운영 및 영상 검증과정을 거치며 영상자료를 실제 사용자들에게 배포하기위한 최종 준비 작업이 진행되고 있다. 다목적실용위성 2호는 1m급 의 고해상도 영상을 촬영할 수 있기 때문에 국내외 많은 사용자들의 관심과 요청을 받고 있다. 항우연 우주웅용센터에서는 이상의 요구사항에 대응하기 위하여 영상자료 주문접수 및 배포업무를 담당하는 전담팀 (KOCUST)을 구성하였으며, 국내외 상용배포 대행업체를 선정하는 등 사용자지원 체계구축 업무를 수행하고 있다. 본 연구의 목적은 영상자료 요청에서부터 촬영,데이터 생성 그리고 전달까지의 일련의 과정을 체계적으로 정리함으로써 운성운영 과정에 대한 사용자들의 이해를 증진시 키는데 도움이 되고자 한다. 나아가 사용자들이 쉽게 다목적실용위성 2호 영상자료를 검색 및 획득할 수 있는 방법에 대해 논하고자 한다.

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The Construction and Development of Support System for Satellite image Commercialization (위성영상 상용화 지원시스템 구축 및 개발)

  • Bae, Hee-Jin;Jeon, Gab-Ho;Jun, Jung-Nam;Kim, Min-A;Chae, Tae-Byeong
    • Current Industrial and Technological Trends in Aerospace
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    • v.8 no.1
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    • pp.25-32
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    • 2010
  • Utilization of KOMPSAT-2 satellite image is growing, because the resolution of KOMPSAT -2 is improved 43.5 times than that of KOMPSAT-1. To support for satellite image commercialization, KOCUST(KOMPSAT Customer & User Support Team) was composed, operation process was established and defined and support system for satellite image Commercialization was constructed. Also the support system constantly is improved for various user. In this paper, organization and function of support system developed so far these days for commercial user and operations related with it were described. In addition, direction of development was discussed

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다목적 실용위성 2호 기계 시스템 개념설계

  • Kim, Gyu-Seon
    • Aerospace Engineering and Technology
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    • v.1 no.1
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    • pp.42-54
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    • 2002
  • In December of 1997, Korea Aerospace Research Institute begin to develope the conceptual design of Kompsat2 as the Kompsat1 design is nearly completed. Basic direction of this design was set up to utilized the heritage of Kompsat1 and modify the payload module to accommodate the new high resolution space borne camera. And in the early stage of this design, total system configuration design study was conducted based on 1st level payload information. In this paper, mechanical system design at various stage is documented and this will be used as a path finder or guidelines in the future feasibility study or conceptual design.

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Characterizing Overlap Area of KOMPSAT-3 (다목적실용위성 3호 Overlap 영역의 특성분석)

  • Seo, Doo-Chun;Kim, Hee-Seob
    • Aerospace Engineering and Technology
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    • v.10 no.2
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    • pp.154-162
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    • 2011
  • The KOrea Multi-Purpose Satellite-3 (KOMPSAT-3) provides 0.7 m Ground Sample Distance (GSD) panchromatic image and 2.8 m GSD multi-spectral image data for various applications. The KOMPSAT-3 system data will be applied in the field of earth observations, covering land, sea, coastal zones, and Geographic Information Systems (GIS). In order to keep the swath width of 15km at nadir view of KOMPSAT-3, CCD consist of approximately 24,020 pixels excluding 20 dark pixels at both sides and has overlap region. Because there are no CCD-line sensors with a pixel size of $7{\mu}m$, the field of view is separated into 2 parts and imaged on 2 detectors, each with 12,080 pixels. Therefore, 2 detectors have different geometric characteristic. This paper provides image simulation for geometric characteristics analysis of overlapping area of KOMPSAT-3 using KOMPSAT-2 image data.

Study of the Post Mission Disposal Maneuver for KOMPSAT-2 (다목적실용위성 2호의 폐기기동 연구)

  • Seong, Jaedong;Jung, Okchul;Chung, Daewon
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.46 no.12
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    • pp.1037-1048
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    • 2018
  • In this paper, we investigated the international guidelines and actual disposal maneuver cases to prepare KOMPSAT-2 post mission disposal. And then, disposal maneuver plan was established using current propellant of KOMPSAT-2 and verification was also performed to find out whether the international guidelines are satisfied. As a result, the lifetime of KOMPSAT-2 was 3.6 years when 45kg propellant was used to decrease perigee altitude to 300km. And if more than 14.5kg propellant consumed for same strategy, KOMPSAT-2 can satisfy the international guidelines. Finally, re-entry survivability analysis was performed and it represented that heat resistant objects, such as propellant tank and reaction wheel, could be survived but total ground casualty probability was less than international guidelines.

Characteristics of Location Accuracy in KOMPSAT-2 (다목적실용위성2호 위치정확도 특성)

  • Seo, Doo-Chun;Park, Ji-Yong;Choi, Hea-Sun;Jung, Jae-Heon;Hong, Ki-Byung;Lee, Sun-Gu
    • Aerospace Engineering and Technology
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    • v.12 no.1
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    • pp.144-151
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    • 2013
  • The KOrea Multi-Purpose SATellite-2 (KOMPSAT-2) is to provide 1.0 m Ground Sample Distance (GSD) panchromatic image and 4.0 m GSD multi-spectral image data for various applications. The KOMPSAT-2 system performs mission applications in the field of earth observations, covering land, sea, coastal zones, and Geographic Information Systems (GIS). The purpose of this document is to compute ground coordinate using satellite position, velocity and attitude data in KOMPSAT-2 and document for work-flow of location accuracy correction in KOMPSAT-2.

Current Status of Application of KOMPSAT Series (최근 다목적실용위성 시리즈 활용 현황)

  • Lee, Kwang-Jae;Oh, Kwan-Young;Lee, Won-Jin
    • Korean Journal of Remote Sensing
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    • v.36 no.6_2
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    • pp.1485-1492
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    • 2020
  • It has been more than 20 years since the launch of KOMPSAT-1, and so far, a total of 5 satellites have been successfully launched. Until now, KOMPSAT has been used in various fields, including the production of various thematic maps, land change, environmental analysis, and marine monitoring. Many researchers have conducted research to process, analyze, and utilize KOMPSAT images. According to the national space development plan, the KOMPSAT series will be continuously developed to meet the demand for satellite images at the national level. If the ultimate purpose of satellite development is to utilize acquired images, systematic research to effectively utilize the developed satellites should be followed. This special issue introduces the recently conducted research on the use of KOMPSAT images.

Flight Software Development for KOMPSAT-2 On-Board Computers (다목적실용위성 2호 탑재소프트웨어 개발)

  • 강수연;이재승;최종욱;이종인
    • Proceedings of the Korean Information Science Society Conference
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    • 2003.10b
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    • pp.346-348
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    • 2003
  • 본 논문에서는 2004년 12월 발사 예정인 다목적실용위성 2호의 탑재소프트웨어의 구성과 전반적인 개발 과정 및 개발 환경에 관련된 내용을 서술한다. 다목적실용위성 2호 탑재소프트웨어 개발은 다목적실용 위성 1호 탑재소프트웨어를 근간으로 2호기 요구사양에 따라 요구사양 분석, 설계. 코딩 및 단위 테스트, 통합 테스트와 검증 시험 등을 거쳐 진행되었으며 일련의 모든 개발과정은 국내 연구진에 의해 수행되었다.

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