Memorias de investigación
Ponencias en congresos:
EDROMO: An Accurate Propagator for Elliptical Orbits in the Perturbed Two-Body Problem
Año:2014
Áreas de investigación
  • Tecnología espacial,
  • Ingeniería aeronaútica
Datos
Descripción
EDromo is a special perturbation method for the propagation of elliptical orbits in the perturbed two-body problem. The state vector consists of a time-element and seven spatial elements, and the independent variable is a generalized eccentric anomaly introduced through a Sundman time transformation. The key role in the derivation of the method is played by an intermediate reference frame which enjoys the property of remaining fixed in space as long as perturbations are absent. Three elements of EDromo characterize the dynamics in the orbital frame and its orientation with respect to the intermediate frame, and the Euler parameters associated to the intermediate frame represent the other four spatial elements. The performance of EDromo has been analyzed by considering some typical problems in astrodynamics. In almost all our tests the method is the best among other popular formulations based on elements.
Internacional
Si
Nombre congreso
24th AAS/AIAA Space Flight Mechanics Meeting
Tipo de participación
960
Lugar del congreso
Santa Fe, New Mexico (EEUU)
Revisores
Si
ISBN o ISSN
978-0-87703-611-1
DOI
Fecha inicio congreso
26/01/2014
Fecha fin congreso
30/01/2014
Desde la página
1117
Hasta la página
1136
Título de las actas
Advances in the Astronautical Sciences
Esta actividad pertenece a memorias de investigación
Participantes
Grupos de investigación, Departamentos, Centros e Institutos de I+D+i relacionados
  • Creador: Grupo de Investigación: Dinámica Espacial (SDG-UPM)
  • Departamento: Física Aplicada a Las Ingenierías Aeronáutica y Naval