Variable-time-domain neighboring optimal guidance applied to space trajectories
Polyhedral representation of invariant manifolds applied to orbit transfers in the Earth–Moon system
Symmetry Properties of Optimal Space Trajectories (IAA-AAS-DyCoSS2-14-14-03 — AAS 14-600)
Symmetry Properties of Optimal Space Trajectories (IAA-AAS-DyCoSS2-14-14-03 - AAS 14-600)
Particle swarm optimization of ascent trajectories of multistage launch vehicles
Low-energy Earth–Moon transfers involving manifolds through isomorphic mapping