FIELD: transport.
SUBSTANCE: method for spacecraft flight path correction and device for its implementation relate to space engineering, specifically to satellite systems navigation. Reconfiguring sequence is used: single-sideband signal reception and single-sideband reception with compensation of parasitic phase signal displacement from doppler displacement.
EFFECT: improving navigation accuracy by complexing errors of determined origin in counts of diagonal matrix used in optimisation of modified dynamic filter of Kalman in control loop during path integration.
3 cl, 22 dwg
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