GLONASS-Aided High-Precision Navigation of Space Geodetic Systems


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Abstract

The paper considers the methods of high-precision navigation of space geodetic systems. A technology of determining the orbit parameters by kinematic and dynamic methods using GLONASS signals is proposed. It is for the first time that experimental estimates of position errors have been obtained in a study case of Geo-IK-2 spacecraft, with the measurement residuals of the global quantum-optical network being at the level of 0.06 m (RMS).

About the authors

A. N. Zaliznyuk

Military Survey Directorate of the General Staff of the Russian Federation Armed Forces

Email: ivan.skakun@glonass-iac.ru
Russian Federation, Moscow, 119160

S. N. Karutin

Central Research Institute of Mechanical Engineering (TSNIIMash), FSUE

Email: ivan.skakun@glonass-iac.ru
Russian Federation, Korolev, Moscow Region, 141070

V. V. Mitrikas

Central Research Institute of Mechanical Engineering (TSNIIMash), FSUE

Email: ivan.skakun@glonass-iac.ru
Russian Federation, Korolev, Moscow Region, 141070

I. O. Skakun

Central Research Institute of Mechanical Engineering (TSNIIMash), FSUE

Author for correspondence.
Email: ivan.skakun@glonass-iac.ru
Russian Federation, Korolev, Moscow Region, 141070

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