Observatorio de I+D+i UPM

Descripción
The minimum-time, constant-thrust orbit correction between two close non-coplanar circular orbits is studied using a relative motion formulation in curvilinear coordinates. The associated optimal control problem in the thrust orientation is tackled using the direct method to numerically solve a diverse set of problems for varying orbital radius and inclination. Additionally, an analytical estimate for the minimum-time inclination change maneuver is obtained. Fundamental changes in the structure of the solution and objective function are highlighted depending on the relation between the required radial displacement, inclination change and available thrust.
Internacional	Si
Nombre congreso	26th AAS/AIAA Space Flight Mechanics Meeting
Tipo de participación	960
Lugar del congreso	Napa, California (EEUU)
Revisores	Si
ISBN o ISSN	1081-6003
DOI
Fecha inicio congreso	14/02/2016
Fecha fin congreso	18/02/2016
Desde la página	397
Hasta la página	414
Título de las actas	Advances in the Astronautical Sciences Volume 158, Spaceflight Mechanics 2016

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)
• Departamento: Física Aplicada a Las Ingenierías Aeronáutica y Naval