A Special Perturbation Method in Orbital Dynamics

Hedo Rodríguez, José Manuel ORCID: https://orcid.org/0000-0003-3599-9486, Peláez Álvarez, Jesús ORCID: https://orcid.org/0000-0001-9755-1674 and Rodriguez de Andrés, Pedro (2005). A Special Perturbation Method in Orbital Dynamics. En: "15th AAS/AIAA Space Flight Mechanics Conference", 23/01/2005 - 27/01/2005, Copper Mountain, Colorado, USA. pp. 1061-1078.

Descripción

Título: A Special Perturbation Method in Orbital Dynamics
Autor/es:
Tipo de Documento: Ponencia en Congreso o Jornada (Artículo)
Título del Evento: 15th AAS/AIAA Space Flight Mechanics Conference
Fechas del Evento: 23/01/2005 - 27/01/2005
Lugar del Evento: Copper Mountain, Colorado, USA
Título del Libro: 15th AAS/AIAA Space Flight Mechanics Conference
Fecha: 2005
Materias:
ODS:
Escuela: E.T.S.I. Aeronáuticos (UPM) [antigua denominación]
Departamento: Otro
Licencias Creative Commons: Reconocimiento - Sin obra derivada - No comercial

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Resumen

Bead models are used in dynamical simulation of tethers. These models discretize a cable using beads distributed along its length. The time evolution is obtained nu- merically. Typically the number of particles ranges between 5 and 50, depending on the required accuracy. Sometimes the simulation is extended over long periods (several years). The complex interactions between the cable and its spatial environment require to optimize the propagators —both in runtime and precisión that constitute the central core of the process. The special perturbation method treated on this article conjugates simpleness of computer implementation, speediness and precision, and is capable to propagate the orbit of whichever material particle. The paper describes the evolution of some orbital elements, which are constants in a non-perturbed problem, but which evolve in the time scale imposed by the perturbation. It can be used with any kind of orbit and it is free of sin- gularities related to small inclination and/or small eccentricity. The use of Euler parameters makes it robust.

Proyectos asociados

Tipo
Código
Acrónimo
Responsable
Título
Gobierno de España
BFM2001-3663
Sin especificar
Spanish Ministry of Science and Technology
Estabilidad y Simulación Dinámica de Tethers

Más información

ID de Registro: 35120
Identificador DC: https://oa.upm.es/35120/
Identificador OAI: oai:oa.upm.es:35120
Depositado por: Memoria Investigacion
Depositado el: 08 Feb 2016 19:33
Ultima Modificación: 27 Feb 2024 11:14