Tree: c4c06d4cd3

main

test-refactor

Branches Tags

${ item.name }

Create tag ${ searchTerm }

Create branch ${ searchTerm }

from 'c4c06d4cd3'

${ noResults }

Commit Graph

6 Commits (c4c06d4cd39f8c58702e1782b3161870f9feb40d)

Author	SHA1	Message	Date
cinnaboot	64f20ef309	Phase 5: Update all test configs to new orbit table format	6 months ago
cinnaboot	dade860e89	Phase 4: Update initialization to use orbital mechanics module	6 months ago
cinnaboot	ec1d115676	Phase 3: Update config parser to use orbital elements ... - Replace position/velocity with orbit table parsing - Parse all orbital element fields with defaults - Support altitude convenience field for semi_major_axis - Add validation for orbital elements - Remove manual position/velocity calculation from loader - Build succeeds (expected unused function warning)	6 months ago
cinnaboot	121f1b9d29	Phase 2: Update data structures with global_position/global_velocity ... - Rename CelestialBody/Spacecraft position/velocity to global_* - Add OrbitalElements struct to both bodies and spacecraft - Rename old OrbitalElements to OrbitalMetrics (for output/analysis) - Update all references throughout codebase - Preserve parent_index in outer structs (not in OrbitalElements) - Build succeeds with only unused variable warning	6 months ago
cinnaboot	dc1f9f4e58	Phase 1: Create orbital mechanics module ... - Add OrbitalElements struct with Keplerian elements - Implement orbital_elements_to_cartesian() for all orbit types - Handle circular, elliptical, parabolic, and hyperbolic orbits - Support planar orbits (3D orientation deferred) - Update planning document	6 months ago
cinnaboot	9b88825046	add breaking orbital elements update planning doc	6 months ago