Kc. Howell et al., APPLICATION OF DYNAMICAL-SYSTEMS THEORY TO TRAJECTORY DESIGN FOR A LIBRATION POINT MISSION, The Journal of the astronautical sciences, 45(2), 1997, pp. 161-178
Recently, there has been accelerated interest in missions utilizing tr
ajectories near libration points. The trajectory design issues involve
d in missions of such complexity go beyond the lack of preliminary bas
eline trajectories (since conic analysis fails in this region of the s
olution space). Successful and efficient design of mission options wil
l require new persepectives; a more complete understanding of the solu
tion space is imperative. In this investigation, dynamical systems the
ory is applied to better understand the geometry of the phase space in
the three-body problem via stable and unstable manifolds. Then, the m
anifolds are used to generate various solution arcs and establish traj
ectory options that are then utilized in preliminary design for the pr
oposed Suess-Urey mission.