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http://dx.doi.org/10.5140/JASS.2006.23.3.245

STATION-KEEPING FOR COMS SATELLITE BY ANALYTIC METHODS  

Kim Young-Rok (Dept. of Astronomy, Yonsei University)
Kim Hae-Yeon (Satellite Ground Control Technology Team, ETRI)
Park Sang-Young (Dept. of Astronomy, Yonsei University)
Lee Byoung-Sun (Satellite Ground Control Technology Team, ETRI)
Park Jae-Woo (Communications Satellite System Research Team, ETRI)
Choi Kyu-Hong (Dept. of Astronomy, Yonsei University)
Publication Information
Journal of Astronomy and Space Sciences / v.23, no.3, 2006 , pp. 245-258 More about this Journal
Abstract
In this paper, an automation algorithm of analyzing and scheduling the station-keeping maneuver is presented for Communication, Ocean and Meteorological Satellite (COMS). The perturbation analysis for keeping the position of the geostationary satellite is performed by analytic methods. The east/west and north/south station-keeping maneuvers we simulated for COMS. Weekly east/west and biweekly north/south station-keeping maneuvers are investigated for a period of one year. Various station-keeping orbital parameters are analyzed. As the position of COMS is not yet decided at either $128.2^{\circ}E\;or\;116.0^{\circ}E$, both cases are simulated. For the case of $128.2^{\circ}E$, east/west station-keeping requires ${\Delta}V$ of 3.50m/s and north/south station-keeping requires ${\Delta}V$ of 52.71m/s for the year 2009. For the case of $116.0^{\circ}E,\;{\Delta}V$ of 3.86m/s and ${\Delta}V$ of 52.71m/s are required for east/west and north/south station-keeping, respectively. The results show that the station-keeping maneuver of COMS is more effective at $128.2^{\circ}E$.
Keywords
station-keeping; geostationary orbit maneuver; COMS;
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