Abstract
Abstract
Abstract This work introduces the use of normal-form coordinates in the circular restricted three-body problem as local dynamical features for trajectory characterization. In particular, the saddle coordinates of the normal form are leveraged to define admissible-control regions, i.e., subsets of impulsive maneuvers bounded in both magnitude and time, such that trajectories within each subset exhibit dynamically similar behavior. The proposed methodology results in a two-point boundary value problem formulated in mixed Cartesian and normal-form coordinates. To enable rapid maneuver generation, polynomial approximations are constructed for the resulting $$\Delta \textbf{v}$$ Δ v solution surfaces. Additional polynomial approximations are introduced to enforce maneuver-magnitude constraints efficiently within the admissible-control framework. The accuracy and robustness of all approximations are examined extensively across multiple maneuver windows and libration-point regions. The resulting framework provides a computationally efficient approach for generating and characterizing cislunar maneuvers with embedded qualitative dynamical information, without reliance on extensive Monte Carlo simulations or sample-rejection strategies.
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@article{Schwab2026Defining,
title = {Defining Admissible Control Regions Using Hamiltonian Normal Forms of the Circular Restricted Three-Body Problem},
author = {David Schwab and Puneet Singla and Roshan Eapen},
journal = {The Journal of the Astronautical Sciences},
year = {2026},
doi = {10.1007/s40295-026-00605-y},
url = {https://doi.org/10.1007/s40295-026-00605-y}
}
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