Determination of thrusts to generate artificial equilibrium points in binary systems with applications to a planar solar sail

DOI10.1007/s11071-018-4605-3zbMath1439.70016OpenAlexW2898228237WikidataQ114842659 ScholiaQ114842659MaRDI QIDQ784027

Tadashi Yokoyama, A. K. jun. de Almeida, Antonio Fernando Bertachini De Almeida Prado

Publication date: 5 August 2020

Published in: Nonlinear Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s11071-018-4605-3

zbMATH Keywords

nonlinear systemsrestricted three-body problemsolar sailastrodynamicsartificial equilibrium point

Mathematics Subject Classification ID

Three-body problems (70F07) Two-body problems (70F05) Dynamical systems in classical and celestial mechanics (37N05)

Cites Work

• Dynamics, geometry and solar sails
• On the stability of artificial equilibrium points in the circular restricted three-body problem
• The IAU 2009 system of astronomical constants: the report of the IAU working group on numerical standards for fundamental astronomy
• Artificial equilibrium points for a generalized sail in the circular restricted three-body problem
• Non-Keplerian orbits for electric sails
• Solar sail halo orbits at the Sun-Earth artificial \(L_1\) point
• Artificial halo orbits for low-thrust propulsion spacecraft
• Solar sail parking in restricted three-body systems
• The restricted 3-body problem with radiation pressure
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