• Title/Summary/Keyword: K-space

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Introduction of Space Weather Monitoring Lab at KASI

  • Moon, Yong-Jae;Choi, Seong-Hwan;Baek, Ji-Hye;Park, Young-Deuk;Cho, Kyung-Suk;Kim, Khan-Hyuk;Park, Hyung-Min;Kim, Yeon-Han;Bong, Su-Chan;Kim, Su-Jin;Park, Jin-Young;Hwang, Jung-A
    • Bulletin of the Korean Space Science Society
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    • 2007.04a
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    • pp.36-36
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    • 2007
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Construction of Korean Space Weather Prediction Center: Introduction

  • Cho, Kyung-Suk;Bong, Su-Chan;Kim, Yeon-Han;Kim, Khan-Hyuk;Hwang, Jung-A;Kwak, Young-Sil;Kim, Rok-Soon;Lee, Jae-Jin;Choi, Seong-Hwan;Baek, Ji-Hye;Park, Young-Deuk
    • Bulletin of the Korean Space Science Society
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    • 2008.10a
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    • pp.32.1-32.1
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    • 2008
  • It is well known that solar and space weather activities can influence the performance and reliability of modern technological system and can endanger human life. Since 2007, the Korea Astronomy and Space Science Institute (KASI) has initiated a research project for the construction of Korean Space Weather Prediction Center (K-SWPC) to make preparations for the next solar cycle maximum (~2012). In this talk, we briefly introduce the current progress of KASI activities for K-SWPC; extension of ground observation system, construction of space weather database and network, development of prediction models, and space weather effects. In addition, future plans for KSWPC will be discussed.

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Thermal Analysis of MIRIS Space Observation Camera for Verification of Passive Cooling

  • Lee, Duk-Hang;Han, Won-Yong;Moon, Bong-Kon;Park, Young-Sik;Jeong, Woong-Seob;Park, Kwi-Jong;Lee, Dae-Hee;Pyo, Jeong-Hyun;Kim, Il-Joong;Kim, Min-Gyu;Matsumoto, Toshio
    • Journal of Astronomy and Space Sciences
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    • v.29 no.3
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    • pp.305-313
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    • 2012
  • We conducted thermal analyses and cooling tests of the space observation camera (SOC) of the multi-purpose infrared imaging system (MIRIS) to verify passive cooling. The thermal analyses were conducted with NX 7.0 TMG for two cases of attitude of the MIRIS: for the worst hot case and normal case. Through the thermal analyses of the flight model, it was found that even in the worst case the telescope could be cooled to less than $206^{\circ}K$. This is similar to the results of the passive cooling test (${\sim}200.2^{\circ}K$). For the normal attitude case of the analysis, on the other hand, the SOC telescope was cooled to about $160^{\circ}K$ in 10 days. Based on the results of these analyses and the test, it was determined that the telescope of the MIRIS SOC could be successfully cooled to below $200^{\circ}K$ with passive cooling. The SOC is, therefore, expected to have optimal performance under cooled conditions in orbit.

Status of Korean Large Telescope Project

  • Kim, Young-Soo;Ahn, Sang-Hyeon;Lee, Dong-Wook;Chun, Moo-Young;Kim, Sang-Chul;Kim, Ho-Il;Park, Byeong-Gon;Sung, Hyun-Il;Han, Jeong-Yeol
    • Bulletin of the Korean Space Science Society
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    • 2008.04a
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    • pp.28.3-28.3
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    • 2008
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Magnitude Standardization Procedure for OWL-Net Optical Observations of LEO Satellites

  • Roh, Dong-Goo;Choi, Jin;Jo, Jung Hyun;Yim, Hong-Suh;Park, Sun-Youp;Park, Maru;Choi, Young-Jun;Bae, Young-Ho;Park, Young-Sik;Jang, Hyun-Jung;Cho, Sungki;Kim, Ji-Hye;Park, Jang-Hyun
    • Journal of Astronomy and Space Sciences
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    • v.32 no.4
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    • pp.349-355
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    • 2015
  • As a governmentally approved domestic entity for Space Situational Awareness, Korea Astronomy and Space Science Institute (KASI) is developing and operating an optical telescopes system, Optical Wide-field PatroL (OWL) Network. During the test phase of this system, it is necessary to determine the range of brightness of the observable satellites. We have defined standard magnitude for Low Earth Orbit (LEO) satellites to calibrate their luminosity in terms of standard parameters such as distance, phase angle, and angular rate. In this work, we report the optical brightness range of five LEO Satellites using OWL-Net.

AN EXISTENCE OF LINEAR SYSTEMS WITH GIVEN TRANSFER FUNCTION

  • Yang, Meehyea
    • Bulletin of the Korean Mathematical Society
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    • v.30 no.1
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    • pp.99-107
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    • 1993
  • A vector space K with scalar product <.,.> is called a Krein space if it can be decomposed as a northogonal sum of a Hilbert space and an anti-space of a Hilbert space. The space K induces a Hilbert space $K_{J}$ in the inner product <.,.> $K_{J}$=<.,.>K, where $J^{2}$=I. the eigenspaces of J are denoted by $K^{+}$$_{J}$, which is a Hilbert space and $K^{-}$$_{J}$, which is an anti-space of a Hilbert space. Then the Krein space K is the orthogonal sum of $K^{+}$$_{J}$ and $K^{-}$$_{J}$. Such a decomposition of K is called a fundamental decomposition. In general, fundamental decompositions are not unique. The norm of the Hilbert space depends on the choice of a fundamental decomposion, but such norms are equivalent. The topology generated by these norms is called the strong or Mackey topology of K. It is used to define all topological notions on the Krein space K with respect to this topology. The Pontryagin index of a Krein space is the dimension of the antispace of a Hilbert space in any such decomposition. the dimension does not depend on the choice of orthogonal decomposition. A Krein space is called a Pontryagin space if it has finite Pontryagin index.dex.yagin index.dex.

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