GLONASS-Aided High-Precision Navigation of Space Geodetic Systems


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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).

作者简介

A. Zaliznyuk

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

Email: ivan.skakun@glonass-iac.ru
俄罗斯联邦, Moscow, 119160

S. Karutin

Central Research Institute of Mechanical Engineering (TSNIIMash), FSUE

Email: ivan.skakun@glonass-iac.ru
俄罗斯联邦, Korolev, Moscow Region, 141070

V. Mitrikas

Central Research Institute of Mechanical Engineering (TSNIIMash), FSUE

Email: ivan.skakun@glonass-iac.ru
俄罗斯联邦, Korolev, Moscow Region, 141070

I. Skakun

Central Research Institute of Mechanical Engineering (TSNIIMash), FSUE

编辑信件的主要联系方式.
Email: ivan.skakun@glonass-iac.ru
俄罗斯联邦, Korolev, Moscow Region, 141070

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