FIELD: cosmonautics.
SUBSTANCE: inventions group relates to the field of cosmonautics, namely to the technique of performing trajectory measurements, determining the coordinates and orthogonal components of the spacecraft velocity vector, and can be used on ground and onboard spacecraft flight control systems to accurately determine the current parameters of the spacecraft movement. The method for determining the velocity vector of the main spacecraft includes: measuring in the ground radio technical station (GRTS) K values of the nominal frequencies of the received radio signals of n-th earth stations (3C) In after their retransmission by the main S1 and adjacent S1 spacecraft, respectively, calculation of the coordinates of the main spacecraft х1, у1, z1, calculation of the orthogonal components of the velocity vector of the main spacecraft The method for determining the coordinates of the main spacecraft х1, у1, z1 includes: measuring in the GRTS K for each n-th 3C In values of the time delays Δtn between the received radio signals after their retransmission by the main S1and adjacent spacecraft S2, respectively, calculating the coordinates of the main spacecraft x1, y1, z1.
EFFECT: increases accuracy of determining the coordinates and orthogonal components of the spacecraft velocity vector.
4 cl, 7 dwg, 2 ex
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Authors
Dates
2021-06-24—Published
2020-11-06—Filed