Solution of optimal continuous low-thrust transfer using Lie transforms
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 | |
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 |