FIELD: transport.
SUBSTANCE: invention relates to space engineering and is intended for retaining the craft in preset geostationary orbital position. Spacecraft orbital flight parameters are corrected and sent thereto. At the time of tracking the correction engine operation at every step thereof, inertial mass free motion start and end aboard said craft in closed spherical vessel is registered.Control acceleration is defined from equation of uniformly accelerated motion without initial velocity in known path in said vessel by means of high-precision accelerometer of linear accelerating effect at zero-gravity effects. Magneto susceptible ball makes said inertial mass.
EFFECT: higher accuracy of computation of control accelerations and quality of correction.
1 dwg
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