FIELD: transport.
SUBSTANCE: invention relates to space engineering and can be used for spacecraft orbital flight correction. Test and correction effects are applied by switching on of engines to make path changes, to define parameters of motion of spacecraft center of gravity, to compute the correction, to generate command-program data with initial conditions of the flight, correction plan and control accelerations, and to transmit said data files to spacecraft.
EFFECT: higher accuracy of determination of control accelerations and geostationary spacecraft retention, prolonged control over center of gravity in automatic mode.
1 dwg
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