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 adjacent 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 (3С) In after their retransmission by the main S1 and adjacent S2 spacecraft, respectively, radiation of the test radio signal using the GRTS, receiving it after retransmission by the main spacecraft S1 and adjacent S2 spacecraft, respectively, and measuring their frequency , calculation of the radial velocity of the main spacecraft and adjacent spacecraft relative to the GRTS K, calculation of the coordinates of the main x1, y1, z1 and adjacent spacecraft x2, y2, z2, calculation of the coordinates of the main spacecraft The method for determining the coordinates of the main х1, у1, z1 and adjacent spacecraft х2, у2, z2 includes: measuring in the GRTS K for each n-th 3C In the values of the time delays Δtn between the received radio signals after their retransmission by the main S1 and adjacent spacecraft S2, respectively, radiation test radio signals using the GRTS, receiving them after retransmission by the main spacecraft S1 and adjacent spacecraft S2, respectively, and measuring the time delays , calculating the distances from the GRTS to the main and adjacent spacecraft calculating the coordinates of the main spacecraft х1, у1, z1.
EFFECT: increases the accuracy of determining the coordinates and orthogonal components of the velocity vectors of two spacecraft.
4 cl, 7 dwg, 2 ex
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Authors
Dates
2021-07-07—Published
2020-11-06—Filed