A Simplified Method to Determine Gravity Vector Through Aerodynamic Coefficients and its Applications in Attitude Determination

DOI10.1007/978-3-030-11292-9_28zbMath1504.93271OpenAlexW2941438301MaRDI QIDQ5053640

Raúl de Celis, Luis Cadarso

Publication date: 6 December 2022

Published in: Informatics in Control, Automation and Robotics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/978-3-030-11292-9_28

zbMATH Keywords

aircraftGNSSattitude determinationIMUterminal guidancesensor model

Mathematics Subject Classification ID

Application models in control theory (93C95)

Cites Work

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