Observatorio de I+D+i UPM

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

Esta actividad pertenece a memorias de investigación

• Autor: Juan Luis Gonzalo Gomez (UPM)
• Autor: Claudio Bombardelli (UPM)

• Creador: Grupo de Investigación: Dinámica Espacial (SDG-UPM)