TY - JOUR
EP - 3304
VL - 150
Y1 - 2014///
SN - 0065-3438
N2 - 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
SP - 3293
TI - Solution of optimal continuous low-thrust transfer using Lie transforms
ID - upm33435
JF - Advances in the Astronautical Sciences
AV - public
UR - https://oa.upm.es/33435/
A1 - Sanjurjo Rivo, Manuel
A1 - Scheeres, D.
A1 - Lara, M.
A1 - Peláez Álvarez, Jesús
ER -