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Journal of Automation and Information Sciences
SJR: 0.275 SNIP: 0.59 CiteScore™: 0.8

ISSN Imprimir: 1064-2315
ISSN En Línea: 2163-9337

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Journal of Automation and Information Sciences

DOI: 10.1615/JAutomatInfScien.v29.i1.110
pages 91-99

Satellite Correction Equations for a Strapdown Inertial System

Alexander I. Tkachenko
International Research and Training Center of Information Technologies and Systems of National Academy of Sciences of Ukraine and Ministry of Education and Science of Ukraine, Kyiv


Equations for satellite correction of an aircraft strapdown inertial navigation system are given. Structure of equations that is suitable for estimating the error vector using a triangular Kalman filter (square-root filter) is specified. The possibility of providing the observability and obtaining estimation of the basic elements of the vector of state under the conditions of a horizontal linear flight is considered.

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