Improving satellite orbit solution using double-differenced GPS carrier phase in kinematic mode.
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Publication:1862615
DOI10.1007/S001900100205zbMATH Open1049.86507OpenAlexW1997968206MaRDI QIDQ1862615
Publication date: 2001
Published in: Journal of Geodesy (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1007/s001900100205
Related Items (2)
Improved Direct Solution of the Global Positioning System Equation ⋮ Determination of high-precision GPS orbits using triple differencing technique
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