Third-body perturbation using a single averaged model: application in nonsingular variables
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Publication:936231
DOI10.1155/2007/40475zbMath1190.70006OpenAlexW1980948390WikidataQ114842731 ScholiaQ114842731MaRDI QIDQ936231
Antonio Fernando Bertachini De Almeida Prado, Carlos Renato Huaura Solórzano
Publication date: 13 August 2008
Published in: Mathematical Problems in Engineering (Search for Journal in Brave)
Full work available at URL: https://eudml.org/doc/45231
Related Items (3)
Searching less perturbed circular orbits for a spacecraft travelling around Europa ⋮ Searching for orbits with minimum fuel consumption for station-keeping maneuvers: an application to lunisolar perturbations ⋮ Inner third-body perturbations
Cites Work
- Unnamed Item
- Omne quod movetur necesse est ab aliquo moveri: A Refutation of Galen by Alexander of Aphrodisias and the Theory of Motion
- A set modified equinoctial orbit elements
- Nonsingular elements in description of the motion of small eccentricity and inclination satellites
- The problem of the critical inclination revisited
- The geopotential in nonsingular orbital elements
- The equations of motion of an artificial satellite in nonsingular variables
- On the equinoctial orbit elements
- The critical inclination problem with small eccentricity
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