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      KCI등재 SCI SCIE SCOPUS

      Orbit Determination Accuracy Improvement for Geostationary Satellite with Single Station Antenna Tracking Data

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      https://www.riss.kr/link?id=A103381131

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      다국어 초록 (Multilingual Abstract) kakao i 다국어 번역

      An operational orbit determination (OD) and prediction system for the geostationary Communication, Ocean, and Meteorological Satellite (COMS) mission requires accurate satellite positioning knowledge to accomplish image navigation registration on the ground. Ranging and tracking data from a single ground station is used for COMS OD in normal operation. However, the orbital longitude of the COMS is so close to that of satellite tracking sites that geometric singularity affects observability. A method to solve the azimuth bias of a single station in singularity is to periodically apply an estimated azimuth bias using the ranging and tracking data of two stations. Velocity increments of a wheel off-loading maneuver which is performed twice a day are fixed by planned values without considering maneuver efficiency during OD. Using only single-station data with the correction of the azimuth bias, OD can achieve three-sigma position accuracy on the order of 1.5 km root-sum-square.
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      An operational orbit determination (OD) and prediction system for the geostationary Communication, Ocean, and Meteorological Satellite (COMS) mission requires accurate satellite positioning knowledge to accomplish image navigation registration on the ...

      An operational orbit determination (OD) and prediction system for the geostationary Communication, Ocean, and Meteorological Satellite (COMS) mission requires accurate satellite positioning knowledge to accomplish image navigation registration on the ground. Ranging and tracking data from a single ground station is used for COMS OD in normal operation. However, the orbital longitude of the COMS is so close to that of satellite tracking sites that geometric singularity affects observability. A method to solve the azimuth bias of a single station in singularity is to periodically apply an estimated azimuth bias using the ranging and tracking data of two stations. Velocity increments of a wheel off-loading maneuver which is performed twice a day are fixed by planned values without considering maneuver efficiency during OD. Using only single-station data with the correction of the azimuth bias, OD can achieve three-sigma position accuracy on the order of 1.5 km root-sum-square.

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      참고문헌 (Reference)

      1 J.L. Cooley, "“Error Studies for Ground Tracking of Synchronous Satellites,” GSFC Report X-551-72-30, 1972"

      2 "“Electrical and Mechanical Characteristics of Earth Station Antenna for Satellite Communications,” EIA-411-A, Electronic Industries Association"

      3 W.M. Kaula, "Theory of Satellite Geodesy" Blaisdell Publishing Co. 1966

      4 F.G. Lemoine, "The Development of the Joint NASA GSFC and the National Imagery and Mapping Agency (NIMA) Geopotential Model EGM96, NASA, Goddard Space Flight Center, July 1998"

      5 B.D. Tapley, "Statistical Orbit Determination, 1st ed" Elsevier Academic Press 2004

      6 J.R. Wertz, "Space Mission Analysis and Design" Kluwer Academic Publisher 1991

      7 O. Montenbruck, "Satellite Orbits Models Methods Applications, 1st ed" Springer-Verlag 2000

      8 E.M. Soop, "Handbook of Geostationary Orbits, 1st ed" Kluwer Academic Publishers 1994

      9 S. Kawase, "Ground Antenna Pointing Performance for Geostationary Orbit Determination" 10 : 71-83, 1986

      10 Y. Hwang, "Communication, Ocean, and Meteorological Satellite Orbit Determination Analysis Considering Maneuver Scheme" 2006

      1 J.L. Cooley, "“Error Studies for Ground Tracking of Synchronous Satellites,” GSFC Report X-551-72-30, 1972"

      2 "“Electrical and Mechanical Characteristics of Earth Station Antenna for Satellite Communications,” EIA-411-A, Electronic Industries Association"

      3 W.M. Kaula, "Theory of Satellite Geodesy" Blaisdell Publishing Co. 1966

      4 F.G. Lemoine, "The Development of the Joint NASA GSFC and the National Imagery and Mapping Agency (NIMA) Geopotential Model EGM96, NASA, Goddard Space Flight Center, July 1998"

      5 B.D. Tapley, "Statistical Orbit Determination, 1st ed" Elsevier Academic Press 2004

      6 J.R. Wertz, "Space Mission Analysis and Design" Kluwer Academic Publisher 1991

      7 O. Montenbruck, "Satellite Orbits Models Methods Applications, 1st ed" Springer-Verlag 2000

      8 E.M. Soop, "Handbook of Geostationary Orbits, 1st ed" Kluwer Academic Publishers 1994

      9 S. Kawase, "Ground Antenna Pointing Performance for Geostationary Orbit Determination" 10 : 71-83, 1986

      10 Y. Hwang, "Communication, Ocean, and Meteorological Satellite Orbit Determination Analysis Considering Maneuver Scheme" 2006

      11 H.Y. Kimet, "Analysis of Wheel Off-Loading Strategy of COMS" 2006

      12 J.J. Pocha, "An Introduction to Mission Design for Geostationary Satellites, 1st ed" D. Reidel Publishing Company 1987

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      연월일 이력구분 이력상세 등재구분
      2023 평가예정 해외DB학술지평가 신청대상 (해외등재 학술지 평가)
      2020-01-01 평가 등재학술지 유지 (해외등재 학술지 평가) KCI등재
      2005-09-27 학술지등록 한글명 : ETRI Journal
      외국어명 : ETRI Journal
      KCI등재
      2003-01-01 평가 SCI 등재 (신규평가) KCI등재
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      2016 0.78 0.28 0.57
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