Correction of a strapdown inertial navigation system during descent in the atmosphere

DOI10.3103/S0025654422600830OpenAlexW4320485201MaRDI QIDQ2699167

O. E. Korolev

Publication date: 26 April 2023

Published in: Mechanics of Solids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.3103/s0025654422600830

zbMATH Keywords

quaternionsleast squares methodsatellite navigationstrapdown inertial navigation system (SINS)

Mathematics Subject Classification ID

Mechanics of deformable solids (74-XX)

Cites Work

• Control of angular motion of a landing module of ``Soyuz type upon satellite returning from the orbit
• On the rapid orbital attitude control of manned and cargo spacecraft \textit{Soyuz MS} and \textit{Progress MS}
• Method for analyzing the influence of the errors induced by the gyroscopic channel of a strapdown INS in the autonomous mode

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