Reduced numerical data for: Sliding Patch-Point Multiple Shooting for Low-Impulse Return from Earth-Moon L1 Halo Orbits
Description
This dataset contains the reduced numerical data supporting the tables and figures of the manuscript entitled "Sliding Patch-Point Multiple Shooting for Low-Impulse Return from Earth-Moon L1 Halo Orbits". The dataset includes the final manuscript figures, table-level CSV files, and reduced figure-source CSV files used to reproduce the reported numerical results, comparisons, and diagnostic analyses. The data support the evaluation of four return-design schemes, including full-initial single-shooting correction, sliding patch-point correction, full-initial constrained STM multiple shooting, and sliding patch-point initialization with STM multiple shooting. The complete CR3BP reference-return state database, full implementation files, SPICE kernels, and large intermediate simulation files are not included because they depend on project-specific computational environments, local software configurations, and internal numerical resources. The provided reduced datasets are sufficient to verify the numerical values and trends presented in the manuscript. Additional reduced trajectory data or implementation details may be made available from the corresponding author upon reasonable request, subject to institutional and project-related restrictions.
Files
Steps to reproduce
The reduced numerical data were generated through high-fidelity Earth-Moon trajectory propagation and correction procedures. The dataset was produced using CR3BP-based initial trajectory design, sliding patch-point candidate generation, high-fidelity ephemeris propagation, and constrained STM multiple-shooting refinement. The included CSV files contain reduced numerical results used to generate the manuscript figures and tables.
Institutions
- Nanjing University of Aeronautics and AstronauticsJiangsu, Nanjing