Low-Energy Sub-Optimal Low-Thrust Trajectories to Libration Points and Halo-Orbits the
problem is proposed. It consists of calculating stable manifolds of libration
points or halo
Equilibrium dynamics of the restricted 3-body problem with prolate primaries-collinear libration
points takes place. Compared to the classical circular restricted three-body
problem, our
Continuous Dependence of Coincidence Points on a ParameterThe coincidence
points existence
problem with a parameter is considered. Sufficient conditions
Deployment and Retrieval Missions from Quasi-Periodic and Chaotic States under a Non-Linear Control Law positions, which are center and
saddle points, respectively. However, when out-of-plane motion is initially
Three-Body problem for the earth-moon system under photo-gravitational influence of the sun in the neighborhood of the triangular libration
points of the Earth-Moon system. More than 60 years after the first