|
Descripción
|
|
|---|---|
| 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
|
Si |
|
JCR del ISI
|
No |
|
Título de la revista
|
ASTRODYNAMICS 2015 |
|
ISSN
|
1081-6003 |
|
Factor de impacto JCR
|
|
|
Información de impacto
|
|
|
Volumen
|
|
|
DOI
|
|
|
Número de revista
|
|
|
Desde la página
|
1941 |
|
Hasta la página
|
1958 |
|
Mes
|
SIN MES |
|
Ranking
|
|