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. | |
Internacional
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Si |
JCR del ISI
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No |
Título de la revista
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Advances in the Astronautical Sciences |
ISSN
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1081-6003 |
Factor de impacto JCR
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Información de impacto
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SPACEFLIGHT MECHANICS 2017 |
Volumen
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160 |
DOI
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Número de revista
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Part-IV |
Desde la página
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4125 |
Hasta la página
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4142 |
Mes
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SIN MES |
Ranking
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