vibe coding an orbital mechanics simulation to try out claude code

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cinnaboot fff7fa3d49 Replace per-frame propagation probe with analytical mean anomaly delta ... In check_maneuver_trigger() (true-anomaly branch), eliminate the propagate_orbital_elements() look-ahead probe that was called every frame for pending maneuvers. Replace with direct analytical computation of dt_needed from mean anomaly delta. Benefits: - Eliminates ~24k redundant Kepler solves per Hohmann transfer wait period (DT=10s, 244k s wait time) - More precise: no discretization error from single-step propagation - Simpler logic: removed angle_between check, wraparound detection - Removes dead angle_between() helper function Elliptical orbits only — added TODO for parabolic/hyperbolic support. All 154 tests pass (240,445 assertions).		3 months ago
..
planning	Replace per-frame propagation probe with analytical mean anomaly delta	3 months ago
session_summaries	docs: add UI fixes session summary	3 months ago
TODO	add planning doc for improvements to simulation propagation	3 months ago
coding_standards.md	Rewrite technical documentation	5 months ago
config_format.md	Rewrite technical documentation	5 months ago
future_work.md	Update future work doc - reference Newton-Raphson plan and stability findings	5 months ago
periaapsis_burn_test_results.md	Fix periapsis burn execution location and omega calculation	5 months ago
rendering.md	Update rendering.md: UIState and ManeuverDialogState documentation	5 months ago
technical_reference.md	Update technical_reference: add rendezvous module, HohmannTransfer struct, and reset_spacecraft_tracking step	3 months ago