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3 Commits (a7ecc46f1508c38376b3dbfbf86e748987eab492)

Author	SHA1	Message	Date
cinnaboot	9fd1e29947	refactor: cartesian_to_elements_basic — SCENARIO pattern, named tolerances, TOML 1.0 ... - Consolidate 5 TEST_CASEs into 1 SCENARIO with 6 SECTIONs - Add tolerance constants (A_TOL, E_TOL, ANG_TOL, R_TOL, V_TOL) - Convert TOML to inline table syntax - Add precalc script for expected values - Update continue.md with tolerance reference table and strict widen policy	2 months ago
cinnaboot	2a86e7093a	use old_tests/ while refactoring tests	2 months ago
cinnaboot	13ebe5d0aa	Add Newton-Raphson analytical propagation tests ... Added 6 test files for Newton-Raphson solver and analytical propagation: - test_cartesian_to_elements_basic.cpp: Tests state vector ↔ orbital elements conversion - test_newton_raphson_convergence.cpp: Tests Newton-Raphson solver convergence behavior - test_analytical_propagation_apsides.cpp: Tests propagation through orbital apsides - test_analytical_propagation_timesteps.cpp: Tests propagation with various timesteps - test_extreme_eccentricity.cpp: Tests near-parabolic and hyperbolic orbits - test_precision_boundaries.cpp: Tests exact boundary value handling Implemented core orbital mechanics functions: - solve_kepler_equation(): Newton-Raphson solver with 1e-10 tolerance - get_initial_trial_value(): Series expansion initial guess - cartesian_to_orbital_elements(): State vectors to orbital elements conversion - propagate_orbital_elements(): Analytical propagation using Kepler's equation Updated test plan document with current progress and remaining tests. Test status: 66 passed, 14 failed (out of 80 test cases) - Failing tests are expected: implementation needs debugging - Config validation issues fixed by adjusting orbital parameters	5 months ago