Descripción
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The minimum-time, constant-thrust transfer between two close, coplanar, quasicircular orbits is studied using a novel non-linear formulation of relative motion in curvilinear coordinates. The Optimal Control Problem in the thrust orientation angle is treated from a quantitative and qualitative point of view, using the direct and indirect methods respectively. The former yields numerical solutions for a wide range of thrust parameters, while a better understanding of the physics is achieved seeking for an approximate solution of the latter. Fundamental changes in the structure of the solution with the thrust parameter are identified. | |
Internacional
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Si |
JCR del ISI
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No |
Título de la revista
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ASTRODYNAMICS 2015 |
ISSN
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1081-6003 |
Factor de impacto JCR
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Información de impacto
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Volumen
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DOI
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Número de revista
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Desde la página
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1941 |
Hasta la página
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1958 |
Mes
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SIN MES |
Ranking
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