Strapdown inertial navigation systems for high precision near-earth navigation and satellite geodesy: analysis of operation and errors

DOI10.1134/S1064230708030180zbMath1178.93102OpenAlexW2036421540MaRDI QIDQ733999

L. A. Fokin, A. G. Shchipitsin

Publication date: 19 October 2009

Published in: Journal of Computer and Systems Sciences International (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1134/s1064230708030180

zbMATH Keywords

mathematical modelsatellite geodesynear-Earth inertial navigation

Mathematics Subject Classification ID

Cites Work

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• Unified approach to inertial navigation system error modeling
• Flight experience on CHAMP and GRACE with ultra-sensitive accelerometers and return for LISA
• SINS/ANS integration for augmented performance navigation solution using unscented Kalman filtering
• Non-linear mathematical model for integrated global positioning/inertial navigation systems

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