Station-Keeping Maneuver Simulation for the Koreasat Spacecraft Using Mission Analysis Software

Details Station-Keeping Maneuver Simulation for the Koreasat Spacecraft Using Mission Analysis Software Station-Keeping Maneuver Simulation for the Koreasat Spacecraft Using Mission Analysis Software

Jun 1995

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1995jass...12..102l&link_type=abstract

Journal of Astronomy and Space Science, vol. 12, no. 1, p. 101-111.

Astronomy and Astrophysics

Astronomy

1

Scientific paper

A series of east/west and north/south station-keeping maneuvers were simulated for the KOREASAT spacecraft which has to be maintained within +/-0.¢ª05 at the nominal longitude of 116degE. Weekly and biweekly based station-keeping maneuver plannings were used, and weekend maneuvers were avoided. All of the station-keeping maneuver plannings and executions were performed using KOREASAT Mission Analysis Software on VAX/VMS operating system. Fourteen weeks station-keeping maneuvers were performed and various station-keeping orbital parameters were obtained.

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