Descripción
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In this article, an approximate analytical solution for the two body problem perturbed by a radial, low acceleration is obtained, using a regularized formulation of the orbital motion and the method of multiple scales. The results reveal that the physics of the problem evolve in two fundamental scales of the true anomaly. The first one drives the oscillations of the orbital parameters along each orbit. The second one is responsible of the long-term variations in the amplitude and mean values of these oscillations. A good agreement is found with high precision numerical solutions. | |
Internacional
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Si |
Nombre congreso
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24th AAS/AIAA Space Flight Mechanics Meeting |
Tipo de participación
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960 |
Lugar del congreso
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Santa Fe, New Mexico (EEUU) |
Revisores
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Si |
ISBN o ISSN
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978-0-87703-611-1 |
DOI
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Fecha inicio congreso
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26/01/2014 |
Fecha fin congreso
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30/01/2014 |
Desde la página
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359 |
Hasta la página
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377 |
Título de las actas
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SpaceFlight Mechanics 2014 (Volume 152 in the Advances in the Astronautical Sciences Series) |