• Title/Summary/Keyword: space center

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Science Goal of the Diagnostic Coronagraph on the International Space Station

  • Bong, Su-Chan;Kim, Yeon-Han;Cho, Kyung-Suk;Lee, Jae-Ok;Seough, Jungjoon;Park, Young-Deuk;Newmark, Jeffrey S.;Gopalswamy, Natchimuthuk;Viall, Nicholeen M.;Antiochos, Spiro;Arge, Charles N.;Yashiro, Seiji;Reginald, Nelson L.;Fineschi, Silvano;Strachan, Leonard
    • The Bulletin of The Korean Astronomical Society
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    • v.43 no.2
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    • pp.47.3-47.3
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    • 2018
  • The Korea Astronomy and Space Science Institute (KASI) plans to develop a coronagraph in collaboration with the National Aeronautics and Space Administration (NASA), to be installed on the International Space Station (ISS). It uses multiple filters to obtain simultaneous measurements of electron density, temperature, and velocity within a single instrument. The primary science goal is to understand the physical conditions in the solar wind acceleration region, and the secondary goal is to enable and validate the next generation of space weather science models. The planned launch in 2022 provides great potential for synergy with other solar space missions such as Solar Orbiter and Parker Solar Probe.

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A Study on the Strategies of the Positioning of a Satellite on Observed Images by the Astronomical Telescope and the Observation and Initial Orbit Determination of Unidentified Space Objects

  • Choi, Jin;Jo, Jung-Hyun;Choi, Young-Jun;Cho, Gi-In;Kim, Jae-Hyuk;Bae, Young-Ho;Yim, Hong-Suh;Moon, Hong-Kyu;Park, Jang-Hyun
    • Journal of Astronomy and Space Sciences
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    • v.28 no.4
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    • pp.333-344
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    • 2011
  • An optical tracking system has advantages for observing geostationary earth orbit (GEO) satellites relatively over other types of observation system. Regular surveying for unidentified space objects with the optical tracking system can be an early warning tool for the safety of five Korean active GEO satellites. Two strategies of positioning on the observed image of Communication, Ocean and Meteorological Satellite 1 are tested and compared. Photometric method has a half root mean square error against streak method. Also eccentricity method for initial orbit determination (IOD) is tested with simulation data and real observation data. Under 10 minutes observation time interval, eccentricity method shows relatively better IOD results than the other time interval. For follow-up observation of unidentified space objects, at least two consecutive observations are needed in 5 minutes to determine orbit for geosynchronous orbit space objects.

BITSE Instrument

  • Choi, Seonghwan;Park, Jongyeob;Yang, Heesu;Baek, Ji-Hye;Kim, Jihun;Kim, Jinhyun;Kim, Yeon-Han;Cho, Kyung-Suk;Newmark, Jeffrey S.;Gong, Qian;Nguyen, Hanson;Chang, William S.;Swinski, Joseph-Paul A.;Gopalswamy, Natchumuthuk
    • The Bulletin of The Korean Astronomical Society
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    • v.44 no.2
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    • pp.57.2-57.2
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    • 2019
  • BITSE is a balloon mission, which is a solar coronagraph to measure speed and temperature of the solar wind using 4 different wavelength filters and an pixelated polarization camera. KASI and NASA jointly designed, developed, and tested the solar coronagraph. Mainly KASI developed an imaging system and a control system, and NASA developed an optical system and mechanical structures. We mount the BITSE on Wallops Arc-Second Pointer (WASP) of Wallops Flight Facility, and launch it with a 39 mcf balloon of Columbia Scientific Ballon Facility. We will introduce the overall system of the BITSE.

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Development of a Data Reduction algorithm for Optical Wide Field Patrol

  • Park, Sun-Youp;Keum, Kang-Hoon;Lee, Seong-Whan;Jin, Ho;Park, Yung-Sik;Yim, Hong-Suh;Jo, Jung Hyun;Moon, Hong-Kyu;Bae, Young-Ho;Choi, Jin;Choi, Young-Jun;Park, Jang-Hyun;Lee, Jung-Ho
    • Journal of Astronomy and Space Sciences
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    • v.30 no.3
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    • pp.193-206
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    • 2013
  • The detector subsystem of the Optical Wide-field Patrol (OWL) network efficiently acquires the position and time information of moving objects such as artificial satellites through its chopper system, which consists of 4 blades in front of the CCD camera. Using this system, it is possible to get more position data with the same exposure time by changing the streaks of the moving objects into many pieces with the fast rotating blades during sidereal tracking. At the same time, the time data from the rotating chopper can be acquired by the time tagger connected to the photo diode. To analyze the orbits of the targets detected in the image data of such a system, a sequential procedure of determining the positions of separated streak lines was developed that involved calculating the World Coordinate System (WCS) solution to transform the positions into equatorial coordinate systems, and finally combining the time log records from the time tagger with the transformed position data. We introduce this procedure and the preliminary results of the application of this procedure to the test observation images.