Third-body perturbation in the case of elliptic orbits for the disturbing body
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Publication:955953
DOI10.1155/2008/763654zbMath1151.70011OpenAlexW1970248228WikidataQ58646264 ScholiaQ58646264MaRDI QIDQ955953
R. C. Domingos, Rodolpho Vilhena de Moraes, Antonio Fernando Bertachini De Almeida Prado
Publication date: 24 November 2008
Published in: Mathematical Problems in Engineering (Search for Journal in Brave)
Full work available at URL: https://eudml.org/doc/54823
Related Items (13)
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Cites Work
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- On analytic modeling of Lunar perturbations of artificial satellites of the Earth
- Lunar-Solar Perturbations of an Earth Satellite
- On the long-period lunisolar effect in the motion of the artificial satellite
- On the double averaged three-body problem
- Orbits near critical inclination, including lunisolar perturbations
- Lunar perturbations of artificial satellites of the earth
- Solar System Dynamics
- An Approximation to the Re-Entry Trajectory
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