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Descripción
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| Based on the Lambert's problem, once identified the one-parameter family of orbits that verify the geometric constraints of the problem, we must express the orbits based on a single parameter that allows to select those that satisfy the kinematic condition. The aim of this paper is to reformulate the problem choosing as parameter the true anomaly of the bisector defined by the directions of the two position vectors. The algorithm applied is the SDG-code, developed by the Space Dynamics Group at UPM, which has already been assessed on the resolution of the Kepler equation proving its stability and reliability. | |
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Internacional
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Si |
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Nombre congreso
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27th AAS/AIAA Space Flight Mechanics Meeting |
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Tipo de participación
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960 |
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Lugar del congreso
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San Antonio (Texas) |
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Revisores
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Si |
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ISBN o ISSN
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DOI
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Fecha inicio congreso
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05/02/2017 |
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Fecha fin congreso
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09/02/2017 |
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Título de las actas
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