FIELD: transport.
SUBSTANCE: invention relates to aerospace engineering and may be used for retaining spacecraft in preset range of altitudes and longitudes at working position in orbit. Error in controlling displacement of spacecraft center of gravity is eliminated by using the coefficient of converting voltage and current in plasma engines into engine thrust and displacing spacecraft period check plane into center of orbit active section center. Nominal line (paradigm) of retaining in pane is selected while stable centripetal effect of spacecraft evolution at orbital position is triggered and maintained by correction for long time interval.
EFFECT: higher accuracy, ruled out longitude period correction, reduced power consumption.
1 dwg
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