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test-refactor

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9 Commits (6c28eb1560d2b106efbe09e3e70d4aa2d6222f29)

Author	SHA1	Message	Date
cinnaboot	907e47e606	Replace hardcoded tolerances with named constants (REL_TOL, E_TOL)	2 months ago
cinnaboot	0a2c5c671a	Refactor test_hybrid_burns: qualitative→quantitative checks with named tolerances ... - Update precalc script: add after_1_a for multi-burn, three-burn plane change - Convert 17 qualitative checks (> , <, != 0) to quantitative WithinAbs() - Replace hardcoded tolerances: A_TOL, E_TOL, D_TOL, M_TOL, ANG_TOL, R_TOL - Remove unused init_els variable - Keep rel_err thresholds at 0.01 (continuous burn approximation tolerance) - All 932 assertions pass across 25 test cases (no regressions)	2 months ago
cinnaboot	20327a75d1	refactor: test_hybrid_burns - impulse + continuous burn behavior ... - 14 TEST_CASEs consolidated into 1 SCENARIO with 22 SECTIONs - Shared fixture: sim, bodies, all spacecraft, maneuvers - Helper lambdas: init_craft, find_maneuver, exec_by_name - All tolerances precalculated via sim_engine.py - Named tolerance constants (A_TOL, E_TOL, V_TOL) - 112 assertions, all passing - Updated continue.md: no decorative comments, REQUIRE for integers	2 months ago
cinnaboot	2a86e7093a	use old_tests/ while refactoring tests	2 months ago
cinnaboot	2679ec270f	Consolidate rendezvous types into orbital_objects.h ... - Move RendezvousState and RendezvousTarget from rendezvous_types.h to orbital_objects.h - Remove rendezvous_types.h entirely - Simplify rendezvous.h to depend on orbital_objects.h - Delete spacecraft.h and spacecraft.cpp (consolidated into orbital_objects.h) - Update all include paths across codebase - All tests pass (4 pre-existing failures unchanged)	3 months ago
cinnaboot	0e08adbc14	add FIXME to hybrid burn testing	5 months ago
cinnaboot	31f38b9d89	Implement analytical propagation for all orbit types ... - Switch spacecraft and bodies from RK4 to analytical propagation using propagate_orbital_elements() - Fixed three bugs in hyperbolic orbit propagation (formula errors and insufficient Newton-Raphson iterations) - Add orbital element reconstruction after burns and SOI transitions - Zero energy drift for circular, elliptical, parabolic, and hyperbolic orbits - All 132 tests passing (240,294 assertions)	5 months ago
cinnaboot	a68b5e43f0	Move 4 toml config files from tests/configs/ to tests/ ... Moved configs to flatten directory structure: - test_extreme_orientation_mixed.toml - test_extreme_timescales.toml - test_hybrid_burns.toml - test_hybrid_energy_conservation.toml Updated corresponding test files to use new paths: - test_extreme_orientation_mixed.cpp - test_extreme_timescales.cpp - test_hybrid_burns.cpp - test_hybrid_energy_conservation.cpp All 240,294 assertions passing in 132 test cases	5 months ago
cinnaboot	f292fea518	Consolidate hybrid burn tests: merge impulse + continuous into hybrid_burns ... - Combined test_hybrid_impulse_burns.cpp (539 lines) and test_hybrid_continuous_thrust.cpp (566 lines) into test_hybrid_burns.cpp (859 lines, -23% lines saved) - All 15 test cases preserved (7 impulse + 8 continuous) - Merged config with 10 spacecraft and 7 maneuvers - Tests pass: 240,294 assertions in 132 test cases	5 months ago