muttimarcello/msc_thesis_indirect_lt_trajectory_optimization

This is a thesis research codebase for indirect low-thrust SEP trajectory optimization, organized as three validation case studies: variable-parameter and constant-parameter two-body asteroid rendezvous, and constant-parameter CR3BP Earth–Moon transfer. The documented workflow is to run optimal-control case studies and use their numerical results to validate the formulation; the README also describes energy-to-fuel continuation and post-processing. No source excerpts were provided, so implementation-level calls are not verifiable; dashed, uncited edges indicate only the documented or strongly implied workflow.