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vol 64 / October, 2021
Article

DOI 10.17586/0021-3454-2016-59-1-25-31

UDC 551.510.535+621.396.967

COMPENSATION FOR ATMOSPHERE-INDUCED ERRORS IN EVALUATION OF SPACE OBJECT TRAJECTORY ON THE BASE OF DATA FROM FUNCTIONAL APPLICATIONS TO GLONASS/GPS

A. P. Aleoshkin
Mozhaisky Military Space Academy, Department of Aerial-Feeder Transmitting Devices, St. Petersburg; Professor


T. O. Myslivtsev
A. F. Mozhaysky Military Space Academy, Department of Antenna Feeder and Transmitting Devices, St. Petersburg;


S. V. Nikiforov
A. F. Mozhaysky Military Space Academy, Department of Transmission, Antenna-Feeder Devices and Means for SEV; Adjunct


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Abstract. An algorithm is developed for compensation of atmospheric errors in trajectory information processing based of data from wide-area differential satellite navigation systems. The proposed method is demonstrated to improve accuracy of the state vector of the object evaluation in accordance with the degree of compensation of atmosphere-induced errors.
Keywords: atmospheric errors, radar long-range detection, trajectory processing, model of the ionosphere

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