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test-refactor

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6 Commits (31dc42a2c91b9ca7a3759a7082f0fceea5e6657f)

Author	SHA1	Message	Date
cinnaboot	26d7c94767	update testing plan	5 months ago
cinnaboot	47c5975c0a	docs: Update newton_raphson_test_plan with completed work ... - Condensed completed tests to one-line summaries (6 tests → 8 tests) - Added test_cartesian_to_elements_extreme and test_cartesian_to_elements_quadrature to completed section - Removed duplicate test documentation in Phase sections - Removed entire Overlap Analysis section (no longer needed) - Updated Implementation Summary with Barker's equation and recent fixes - Updated test results to reflect 93 tests passing - Reduced document from 379 → 161 lines (57% reduction)	5 months ago
cinnaboot	9f01cc3e3c	Reduce Newton-Raphson test plan from 14 to 11 files after overlap analysis ... - Remove test_energy_conservation_analytical.cpp (covered by hybrid test) - Rename test_extreme_orientation to test_extreme_orientation_mixed - Remove duplicate polar/retrograde tests (covered by test_precision_boundaries) - Document test reduction rationale in planning doc	5 months ago
cinnaboot	5ce0ae0f18	Update test plan: all 80 tests now passing	5 months ago
cinnaboot	986a94e055	Update test plan: document progress on 3 fixed test files	5 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