FIELD: astronautics.
SUBSTANCE: invention relates to spacecraft (SC) motion control, spacecraft retention at preset longitude of geostationary orbit. Performing holding cycles of orbital parameters containing measurements, calculation and performance of corrections. Based on the measurement data, the corrections are calculated not only for the current holding cycle, but also for the group of subsequent cycles on the autonomous operation interval based on the same data.
EFFECT: reduced spacecraft deviations from preset longitude at standalone operation interval.
1 cl, 1 dwg
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