Integrated navigation system for a space vehicle on a geostationary or highly elliptic orbit operating in the presence of active jam

DOI10.1134/S1064230713030106zbMath1278.93233OpenAlexW2006816929MaRDI QIDQ393688

M. N. Krasil'shchikov, D. M. Kruzhkov, D. A. Kozorez, K. I. Sypalo

Publication date: 23 January 2014

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

Full work available at URL: https://doi.org/10.1134/s1064230713030106

zbMATH Keywords

Kalman filter global positioning system artificial jam deeply integrated system instrument sensor errors multichannel global navigation satellite system receiver navigation signals receiver navigation system optoelectronic earth space vehicle star trackers

Mathematics Subject Classification ID

Filtering in stochastic control theory (93E11) Stochastic systems in control theory (general) (93E03) Geodesy, mapping problems (86A30)

Related Items (5)

An optimal discrete nonlinear logical-dynamical filter-predictor ⋮ On the properties of the limit control sets for a class of unstable linear systems with discrete time and \(l_1\)-restrictions ⋮ Autonomous navigation during the final ascent of a spacecraft into the geostationary orbit. Autonomous integrated navigation system concept ⋮ Optimal injection of a satellite into geostationary orbit using a limited number of thruster firings ⋮ A solution of the navigation problem for autonomous insertion of payload into a geostationary orbit using a low-thrust engine

Cites Work

Study of observability of motion of an orbital group of navigation space system using intersatellite range measurements. Part I

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