A study of the errors of the averaged models in the restricted three-body problem in a short time scale

DOI10.1007/S40314-014-0148-5zbMath1333.70021OpenAlexW1981743109WikidataQ114842691 ScholiaQ114842691MaRDI QIDQ2516812

Rodolpho Vilhena de Moraes, R. C. Domingos, Antonio Fernando Bertachini De Almeida Prado

Publication date: 4 August 2015

Published in: Computational and Applied Mathematics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s40314-014-0148-5

zbMATH Keywords

celestial mechanicsaveraged modelintegral approach

Mathematics Subject Classification ID

Celestial mechanics (70F15) Dynamical systems in classical and celestial mechanics (37N05) Collisions in celestial mechanics, regularization (70F16)

Related Items (1)

Long-term evaluation of orbital dynamics in the Sun-planet system considering axial-tilt

Cites Work

• Planetary satellite orbiters: applications for the Moon
• A study of single- and double-averaged second-order models to evaluate third-body perturbation considering elliptic orbits for the perturbing body
• Some orbital characteristics of lunar artificial satellites
• Third-body perturbation in the case of elliptic orbits for the disturbing body
• Unnamed Item

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