Memorias de investigación
Ponencias en congresos:
The Elliptic Rendezvous Problem in DROMO Formulation
Año:2014
Áreas de investigación
  • Tecnología espacial,
  • Ingeniería aeronaútica
Datos
Descripción
The extension of DROMO formulation to relative motion is evaluated. The orbit of the follower spacecraft can be constructed through differences on the elements defining the orbit of the leader spacecraft. Assuming that the differences are small, the problemis linearized. Typical linearized solutions to relativemotion determine the relative state of the follower spacecraft at a certain time step. Because of the form of DROMO formulation, the performance of a frozen-anomaly transformation is explored. In this case, the relative state is computed for a certain value of the anomaly, equal for leader and follower. Since the time for leader and follower do not coincide, the implicit time delay needs to be corrected to recover the physical sense of the solution. When determining the relative orbit, numerical testing shows significant error reductions compared to previous linearized solutions.
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
2531
Hasta la página
2546
Título de las actas
SpaceFlight Mechanics 2014 (Volume 152 in the Advances in the Astronautical Sciences Series)
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