Autonomous navigation during the final ascent of a spacecraft into the geostationary orbit. Autonomous integrated navigation system concept

DOI10.1134/S106423071505007XzbMath1383.93052OpenAlexW2267559301MaRDI QIDQ1742394

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

Publication date: 11 April 2018

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

Full work available at URL: https://doi.org/10.1134/s106423071505007x

zbMATH Keywords

spacecraftgeostationary orbitautonomous navigation systemdynamic Bayesian measurements filteringinterval estimation algorithms

Mathematics Subject Classification ID

Filtering in stochastic control theory (93E11) Reliability, availability, maintenance, inspection in operations research (90B25) Estimation and detection in stochastic control theory (93E10) Automated systems (robots, etc.) in control theory (93C85) Variable mass, rockets (70P05)

Related Items (2)

On the properties of the limit control sets for a class of unstable linear systems with discrete time and \(l_1\)-restrictions ⋮ Autonomous implementation of dynamic operations in a geostationary orbit. I: Formalization of control problem

Cites Work

• Integrated navigation system for a space vehicle on a geostationary or highly elliptic orbit operating in the presence of active jam
• A solution of the navigation problem for autonomous insertion of payload into a geostationary orbit using a low-thrust engine
• Unnamed Item
• Unnamed Item

This page was built for publication: Autonomous navigation during the final ascent of a spacecraft into the geostationary orbit. Autonomous integrated navigation system concept