Identifies discontinuous TOF behavior in three-body Earth-Moon transfers and augments grid search with a diffusion model, reporting 47-56% better convergence and 39-40% time savings for different orbital altitudes.
Sun-Perturbed Earth-to-Moon Transfers with Ballistic Capture,
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A graph-based framework using sequences of lobe dynamics constructs low-energy transfer trajectories in the Earth-Moon CR3BP, refines them via multiple shooting in the bicircular four-body problem, and demonstrates effectiveness against existing solutions.
The paper defines reflective-sail weak stability boundary structures and uses them with a locally optimal energy-rate control law to construct Earth-escape trajectories in the Sun-Earth PCR3BP that show shorter flight times and higher hyperbolic excess velocity than ballistic escapes.
citing papers explorer
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Three-Body Earth-Moon Transfers with Different Departure/Arrival Orbital Altitudes: New Phenomenon and Diffusion Model-Augmented Construction
Identifies discontinuous TOF behavior in three-body Earth-Moon transfers and augments grid search with a diffusion model, reporting 47-56% better convergence and 39-40% time savings for different orbital altitudes.
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Design of low-energy transfers in cislunar space using sequences of lobe dynamics
A graph-based framework using sequences of lobe dynamics constructs low-energy transfer trajectories in the Earth-Moon CR3BP, refines them via multiple shooting in the bicircular four-body problem, and demonstrates effectiveness against existing solutions.
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Reflective-Sail Weak Stability Boundary Structure with the Locally Optimal Control Law
The paper defines reflective-sail weak stability boundary structures and uses them with a locally optimal energy-rate control law to construct Earth-escape trajectories in the Sun-Earth PCR3BP that show shorter flight times and higher hyperbolic excess velocity than ballistic escapes.