Minimum fuel-consumption stabilization of a spacecraft at the Lagrangian points

DOI10.1134/S0005117919120105zbMath1441.49039OpenAlexW2994734181WikidataQ126556164 ScholiaQ126556164MaRDI QIDQ2190359

L. A. Shalby, Boris T. Polyak

Publication date: 18 June 2020

Published in: Automation and Remote Control (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1134/s0005117919120105

zbMATH Keywords

optimal controlstabilizationrestricted three-body problemLagrangian pointsunstable equilibrium points\(l_1\)-minimization

Mathematics Subject Classification ID

Variational inequalities (49J40) Three-body problems (70F07) Variational principles of physics (49S05)

Related Items (1)

The behavior of a satellite trajectory near the equilibrium points of sun-earth system and its control

Cites Work

• Celestial mechanics and astrodynamics: theory and practice
• Simulation of control processes, stability and stabilization of systems with program constraints
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