• Title/Summary/Keyword: Satellite System

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Ground Receiving System for KOMPSAT-2

  • Kim, Moon-Gyu;Kim, Tae-Jung;Choi, Hae-Jin;Park, Sung-Og;Lee, Dong-Han;Im, Yong-Jo;Shin, Ji-Hyun;Choi, Myung-Jin;Park, Seung-Ran;Lee, Jong-Ju
    • Korean Journal of Remote Sensing
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    • v.19 no.3
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    • pp.191-200
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    • 2003
  • Remote sensing division of satellite technology research center (SaTReC) , Korea advanced institute of science and technology (KAIST) has developed a ground receiving and processing system for high resolution satellite images. The developed system will be adapted and operated to receive, process and distributes images acquired from of the second Korean Multi-purpose Satellite (KOMPSAT-2), which will be launched in 2004. This project had initiated to develop and Koreanize the state-of-the-art technologies for the ground receiving system for high resolution remote sensing images, which range from direct ingestion of image data to the distribution of products through precise image correction. During four years development from Dec. 1998 until Aug. 2002, the system had been verified in various ways including real operation of custom-made systems such as a prototype system for SPOT and a commercialized system for KOMPSAT-1. Currently the system is under customization for installation at KOMPSAT-2 ground station. In this paper, we present accomplished work and future work.

Thermal Analysis for Design of Propulsion System Employed in LEO Earth Observation Satellite

  • Han C.Y.;Kim J.S.;Lee K.H.;Rhee S.W.
    • 한국전산유체공학회:학술대회논문집
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    • 2003.10a
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    • pp.248-250
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    • 2003
  • Thermal analysis is performed to protect the propulsion system of low-earth-orbit earth observation satellite from unwanted thermal disaster like propellant freezing. To implement thermal design adequately, heater powers for the propulsion system estimated through the thermal analysis are decided. Based on those values anticipated herein, the average power for propulsion system becomes 22.02 watts when the only one redundant catalyst bed heater is turned on. When for the preparation of thruster firing, 25.93 watts of the average power is required. All heaters selected for propulsion components operate to prevent propellant freezing meeting the thermal requirements for the propulsion system with the worst-case average voltage, i.e. 25 volts.

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GROUND RECEIVING SYSTEM FOR KOMPSAT-2

  • Kim, Moon-Gyu;Kim, Tae-Jung;Park, Sung-Og;Im, Yong-Jo;Shin, Ji-Hyun;Choi, Myung-Jin;Park, Seung-Ran;Lee, Jong-Ju
    • Proceedings of the KSRS Conference
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    • 2002.10a
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    • pp.804-809
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    • 2002
  • Remote sensing division of satellite technology research center (SaTReC), Korea advanced institute of science and technology (KAIST) has developed a ground receiving and processing system for high resolution satellite images. Developed system will be adapted and operated to receive, process and distributes images acquired from of the second Korean Multi-purpose Satellite (KOMPSAT-2), which will be launched in 2004. This project had initiated to develop and Koreanize the state-of-the-art technologies related to the ground receiving system fur high resolution remote sensing images, which range from direct ingestion of image data to the distribution of products through precise image correction. During four years development, the system has been verified in various ways including real operation of custom-made systems such as a prototype system for SPOT and a commercialised system for KOMPSAT-1. Currently the system is under customisation for installation at KOMPSAT-2 ground station. In this paper, we present accomplished work and future work.

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DEVELOPMENT OF THE KOMPSAT-2 SATELLITE MISSION CONTROL SYSTEM

  • Lee Byoung-Sun;Lee Sanguk;Mo Hee-Sook;Cho Sungki;Jung Won Chan;Kim Myungja;Kim In-Jun;Kim Tae-Hee;Joo Inone;Hwang Yoola;Kim Jaehoon
    • Bulletin of the Korean Space Science Society
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    • 2004.10b
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    • pp.300-303
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    • 2004
  • KOMPSAT-2 satellite mission operations and control system has been developed by ETRI. The system functional architecture, analysis and design, implementation, and tests are presented in this paper.

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HIGH FIDELITY MODELING AND SIMULATION OF A SATELLITE SYSTEM

  • Sungki Cho;Lee, Sanguk;Kim, Jae-Hoon;Lee, Seong-Pal
    • Proceedings of the Korea Society for Simulation Conference
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    • 2001.10a
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    • pp.131-135
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    • 2001
  • A method for modeling and simulation of a satellite system is presented. The characteristics of a typical satellite system is discussed. for high fidelity modeling and simulator development of a satellite, the object-oriented analysis and design methodology is discussed and applied.

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COMMUNICATIONS SATELLITE SYSTEM BY USING MOON ORBIT SATELLITE CONSTELLATION

  • Lee, Sang-Uk;Kim, Jae-Hoon;Lee, Seong-Pal
    • Journal of Astronomy and Space Sciences
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    • v.20 no.4
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    • pp.313-318
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    • 2003
  • A communications satellite system placed in three-Lagrange points, $L_3$, $L_4$ and $L_5$, of the restricted three-body problem in Earth-Moon system is proposed in this paper. LEO satellite constellation has been another choice of communications system. The proposed system which is alternatives of limited geostationary orbit resources, has some weak points such as long distance from the Earth, relatively expensive launch cost, long delay time, more required power, and so on. It has good points like less efforts (fuel) for station keeping, less eclipses, etc. This system has limitations for applications to provide commercial services but it is still some attractive points.

INTRODUCTION OF THE SIMC PROJECT

  • Chae, Gee-Ju;Cho, Seong-Ik;Park, Jong-Hyun;Jo, Kwan-Bok
    • Proceedings of the KSRS Conference
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    • v.1
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    • pp.356-359
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    • 2006
  • The high prices and lack of information for satellite images prevent researchers from studying remote sensing and most non-professional people can't have the simple and easy solutions for the manipulation of satellite images. 'Satellite Imagery Information Management Center'(SIMC) project which is promoted by ETRI (Electronics and Telecommunications Research Institute) from 2002 to 2005 in Korea have the purpose to provide the satellite images freely to the public domain and the solutions for the above mentioned problems. Our project have the following five systems; Data Acquisition System, Data Preservation System, Integrated Solution System, Technology Development System, Operation Plan System. Data Acquisition System collects the satellite images such as LANDSAT, IKONOS, etc. Data Preservation System consists of database which registers the diverse satellite images. Integrated Solution System gives the user of public domain for the web service which search, order and transfer the satellite images. Technology Development System has the many processing technologies for the satellite images. Finally, the Operation Plan system has the role to plan the future of our SIMC project. In this paper, we will give the result of SIMC Project for each five systems during the fast four years from 2002 to 2005.

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