A Special Perturbation Method in Orbital Dynamics


Autoria(s): Hedo Rodríguez, José Manuel; Peláez Álvarez, Jesús; Rodriguez de Andrés, Pedro
Data(s)

2005

Resumo

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.

Formato

application/pdf

Identificador

http://oa.upm.es/35120/

Idioma(s)

eng

Publicador

E.T.S.I. Aeronáuticos (UPM)

Relação

http://oa.upm.es/35120/1/INVE_MEM_2005_188746.pdf

BFM2001-3663

info:eu-repo/semantics/altIdentifier/doi/10.1007/s10569-006-9056-3

Direitos

http://creativecommons.org/licenses/by-nc-nd/3.0/es/

info:eu-repo/semantics/openAccess

Fonte

15th AAS/AIAA Space Flight Mechanics Conference | 15th AAS/AIAA Space Flight Mechanics Conference | 23/01/2005 - 27/01/2005 | Copper Mountain, Colorado, USA

Palavras-Chave #Aeronáutica
Tipo

info:eu-repo/semantics/conferenceObject

Ponencia en Congreso o Jornada

PeerReviewed