%L upm33435
%V 150
%J Advances in the Astronautical Sciences
%P 3293-3304
%I Aeronauticos
%X 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
%A Manuel Sanjurjo Rivo
%A D. Scheeres
%A M. Lara
%A Jesús Peláez Álvarez
%T Solution of optimal continuous low-thrust transfer using Lie transforms
%D 2014