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@ -116,21 +116,21 @@ All constants defined in `src/test_utilities.h` — use those, do not redefine l
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## Test Refactoring Status |
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### Completed |
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- `test_barkers_equation` ✅ — Barker's equation unit tests + parabolic propagation |
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- `test_cartesian_to_elements_advanced` ✅ — Advanced conversion tests (eccentricity spectrum, inclination, true anomaly, 3D orientation) |
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- `test_cartesian_to_elements_basic` ✅ — Element round-trip conversion (semi-major axis, eccentricity, true anomaly, inclination, radius, velocity) |
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- `test_parabolic_orbit` ✅ — Parabolic orbit energy conservation + escape trajectory + initial conditions |
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- `test_extreme_eccentricity` ✅ — High-eccentricity orbits (single SCENARIO, precalculated values, REL_TOL) |
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- `test_extreme_orientation_mixed` ✅ — Extreme orientation conversions, rotation matrix properties, singularity handling |
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- `test_extreme_timescales` ✅ — 9 TEST_CASEs → 1 SCENARIO with 11 SECTIONs, all WithinAbs use named constants |
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- `test_analytical_propagation` ✅ — 5 SCENARIOs → 1 SCENARIO with 23 SECTIONs, precalculated values, all WithinAbs use named constants |
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- `test_moon_orbits` ✅ — Multi-body hierarchical propagation with local/global coordinate tracking |
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- `test_energy` ✅ — Energy calculations and conservation tests |
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- `test_inclined_orbits` ✅ — 3D inclined orbit conversions, Molniya orbits, rotation matrices |
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- `test_maneuvers` ✅ — Impulsive burn tests with precalculated values |
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- `test_orbital_period` ✅ — Orbital period calculations, SCENARIO/SECTION pattern |
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- `test_true_anomaly_roundtrip` ✅ — True anomaly conversion round-trips, tight tolerances |
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- `test_physics_utilities` ✅ — Vector math, acceleration, matrix ops, rotation matrices, compare_vec3 |
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- `test_barkers_equation` — Barker's equation unit tests + parabolic propagation |
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- `test_cartesian_to_elements_advanced` — Advanced conversion tests (eccentricity spectrum, inclination, true anomaly, 3D orientation) |
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- `test_cartesian_to_elements_basic` — Element round-trip conversion (semi-major axis, eccentricity, true anomaly, inclination, radius, velocity) |
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- `test_parabolic_orbit` — Parabolic orbit energy conservation + escape trajectory + initial conditions |
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- `test_extreme_eccentricity` — High-eccentricity orbits (single SCENARIO, precalculated values, REL_TOL) |
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- `test_extreme_orientation_mixed` — Extreme orientation conversions, rotation matrix properties, singularity handling |
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- `test_extreme_timescales` — 9 TEST_CASEs → 1 SCENARIO with 11 SECTIONs, all WithinAbs use named constants |
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- `test_analytical_propagation` — 5 SCENARIOs → 1 SCENARIO with 23 SECTIONs, precalculated values, all WithinAbs use named constants |
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- `test_moon_orbits` — Multi-body hierarchical propagation with local/global coordinate tracking |
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- `test_energy` — Energy calculations and conservation tests |
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- `test_inclined_orbits` — 3D inclined orbit conversions, Molniya orbits, rotation matrices |
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- `test_maneuvers` — Impulsive burn tests with precalculated values |
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- `test_orbital_period` — Orbital period calculations, SCENARIO/SECTION pattern |
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- `test_true_anomaly_roundtrip` — True anomaly conversion round-trips, tight tolerances |
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- `test_physics_utilities` — Vector math, acceleration, matrix ops, rotation matrices, compare_vec3 |
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- `test_periapsis_burn` — prograde burns |
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### Can Refactor Now (sim_engine.py supports all features needed) |
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