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test-refactor

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2 Commits (3c884445c77628c8c12a4bcb88a18c20414e7576)

Author	SHA1	Message	Date
cinnaboot	c4c06d4cd3	Phase 7: Implement parabolic orbit support with union ... - Added union in OrbitalElements (semi_major_axis | semi_latus_rectum) - Updated config_loader to parse and validate semi_latus_rectum for parabolic orbits - Validation ensures correct parameter (semi_latus_rectum for e≈1, semi_major_axis for other) - Updated orbital_mechanics.cpp parabolic case: r = p / (1 + cos(ν)) - Updated parabolic_comet.toml to use semi_latus_rectum = 1.496e11 - Tolerance for parabolic detection: |e - 1.0| < 0.005 Note: Parabolic test still fails velocity tolerance check due to floating-point precision at r=0.5 AU, E ≈ -200 J/kg (not exactly 0)	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