Solution of optimal continuous low-thrust transfer using Lie transforms


Autoria(s): Sanjurjo Rivo, Manuel; Scheeres, D.; Lara, M.; Peláez Álvarez, Jesús
Data(s)

2014

Resumo

This paper addresses the problem of optimal constant continuous low-thrust transfer in the context of the restricted two-body problem (R2BP). Using the Pontryagin’s principle, the problem is formulated as a two point boundary value problem (TPBVP) for a Hamiltonian system. Lie transforms obtained through the Deprit method allow us to obtain the canonical mapping of the phase flow as a series in terms of the order of magnitude of the thrust applied. The reachable set of states starting from a given initial condition using optimal control policy is obtained analytically. In addition, a particular optimal transfer can be computed as the solution of a non-linear algebraic equation. Se investiga el uso de series y transformadas de Lie en problemas de optimización de trayectorias de satélites impulsados por motores de bajo empuje

Formato

application/pdf

Identificador

http://oa.upm.es/33435/

Idioma(s)

eng

Publicador

E.T.S.I. Aeronáuticos (UPM)

Relação

http://oa.upm.es/33435/1/INVE_MEM_2014_182531.pdf

Direitos

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

info:eu-repo/semantics/openAccess

Fonte

Advances in the Astronautical Sciences, ISSN 0065-3438, 2014, Vol. 150

Palavras-Chave #Astronomía #Aeronáutica
Tipo

info:eu-repo/semantics/article

Artículo

PeerReviewed