Abstract
Since its launching on 21 December 1999, the Korea Multi-Purpose Satellite-I (KOMPSAT-I) has been successfully operated by the Mission Control Element (MCE), which was developed by the ETRI. Most of the major functions of the MCE have been successfully demonstrated and verified during the three years of the mission life of the satellite. This paper presents the operational performances of the various functions in MAPS. We show the performance and analysis of orbit determinations using ground-based tracking data and GPS navigation solutions. We present four instances of the orbit maneuvers that guided the spacecraft from injection orbit into the nominal on-orbit. We include the ground-based attitude determination using telemetry data and the attitude maneuvers for imaging mission. The event prediction, mission scheduling, and command planning functions in MAPS subsequently generate the spacecraft mission operations and command plan. The fuel accounting and the realtime ground track display also support the spacecraft mission operations.
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CITATION STYLE
Lee, B. S., Lee, J. S., Kim, J. H., Lee, S. P., Kim, H. D., Kim, E. K., & Choi, H. J. (2003). Operational report of the mission analysis and planning system for the KOMPSAT-I. ETRI Journal, 25(5), 387–400. https://doi.org/10.4218/etrij.03.0102.0518
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