Mass-optimal forced periodic trajectories in the Earth-Moon CR3BP can be generated by warm-starting from energy-optimal solutions, and the thrust-limited reachable set appears to contain the linearized energy-limited set in the xy-plane.
Artificial Three-Body Equilibria for Hybrid Low-Thrust Propulsion,
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Mass-Optimal Low-Thrust Forced Periodic Trajectories in the Earth-Moon CR3BP
Mass-optimal forced periodic trajectories in the Earth-Moon CR3BP can be generated by warm-starting from energy-optimal solutions, and the thrust-limited reachable set appears to contain the linearized energy-limited set in the xy-plane.