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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).

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ACKNOWLEDGMENTS

The authors express their gratitude to the International Laser Ranging Service for performing an active campaign of Geo-IK-2 spacecraft observation.

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Authors and Affiliations

  1. Military Survey Directorate of the General Staff of the Russian Federation Armed Forces, 119160, Moscow, Russia

    A. N. Zaliznyuk

  2. Central Research Institute of Mechanical Engineering (TSNIIMash), FSUE, 141070, Korolev, Moscow Region, Russia

    S. N. Karutin, V. V. Mitrikas & I. O. Skakun

Authors
  1. A. N. Zaliznyuk
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  2. S. N. Karutin
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  3. V. V. Mitrikas
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  4. I. O. Skakun
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Correspondence to I. O. Skakun.

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Zaliznyuk, A.N., Karutin, S.N., Mitrikas, V.V. et al. GLONASS-Aided High-Precision Navigation of Space Geodetic Systems. Gyroscopy Navig. 10, 196–205 (2019). https://doi.org/10.1134/S2075108719040163

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  • DOI: https://doi.org/10.1134/S2075108719040163

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