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Descripción
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| In this paper, an analytical solution of the main problem, a satellite only perturbed by the J2 harmonic, is derived with the aid of perturbation theory and by using DROMO variables. The solution, which is valid for circular and elliptic orbits with generic eccentricity and inclination, describes the instantaneous time variation of all orbital elements, that is, the actual values of the osculating elements | |
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Internacional
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Si |
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Nombre congreso
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AIAA/AAS Astrodynamics Specialist Conference 2014 |
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Tipo de participación
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960 |
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Lugar del congreso
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San Diego, CA, USA |
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Revisores
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Si |
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ISBN o ISSN
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9781634394611 |
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DOI
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Fecha inicio congreso
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04/08/2014 |
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Fecha fin congreso
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07/08/2014 |
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Desde la página
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894 |
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Hasta la página
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913 |
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Título de las actas
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American Institute for Aeronautics and Astronautics ( AIAA ) |