Optimal injection of a satellite into geostationary orbit using a limited number of thruster firings

DOI10.1134/S1064230713060051zbMath1311.49099MaRDI QIDQ2017634

A. S. Bortakovskii, A. A. Konovalova

Publication date: 23 March 2015

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

zbMATH Keywords

satellitenecessary optimality conditionsgeostationary orbitcontinuous-discrete systemoptimal injection

Mathematics Subject Classification ID

Applications of optimal control and differential games (49N90) Variable mass, rockets (70P05) Control/observation systems governed by ordinary differential equations (93C15) Optimality conditions for problems involving ordinary differential equations (49K15)

Related Items (3)

Synthesis of optimal switched systems ⋮ Synthesis of optimal discrete automaton-type systems in the case of multiple instantaneous switchings ⋮ The Synthesis of the Proportional-Differential Regulators for the Systems with Fixed Ends of Trajectories Under Two-Sided Constraints on Control Values

Cites Work

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• Integrated navigation system for a space vehicle on a geostationary or highly elliptic orbit operating in the presence of active jam
• Sufficient optimality conditions for discrete automaton-type systems
• Sufficient conditions of optimality of the automaton part of the logical-dynamical system

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