#include #include #include "../src/physics.h" #include "../src/simulation.h" #include "../src/config_loader.h" #include "../src/test_utilities.h" #include using Catch::Matchers::WithinAbs; SCENARIO("Orbital period measurement with analytical propagation", "[period][analytical]") { const double TIME_STEP = 60.0; const double SECONDS_PER_DAY = 86400.0; SimulationState* sim = create_simulation(10, 0, 0, TIME_STEP); REQUIRE(load_system_config(sim, "tests/test_orbital_period.toml")); auto propagate_and_check = [&](OrbitTracker* tracker, CelestialBody* body, CelestialBody* parent, double max_time, double expected_days) { while (sim->time < max_time && !tracker->orbit_completed) { update_simulation(sim); update_orbit_tracker(tracker, body, parent, sim->time); } REQUIRE(tracker->orbit_completed); const double measured_days = tracker->time_at_completion / SECONDS_PER_DAY; INFO("Measured period: " << measured_days << " days"); REQUIRE_THAT(measured_days, WithinAbs(expected_days, 0.1)); destroy_orbit_tracker(tracker); }; SECTION("Earth completes one orbit in ~365 days") { CelestialBody* earth = &sim->bodies[1]; CelestialBody* sun = &sim->bodies[0]; OrbitTracker* tracker = create_orbit_tracker(1); const double max_time = 400.0 * SECONDS_PER_DAY; propagate_and_check(tracker, earth, sun, max_time, 365.2105); } SECTION("Mars completes one orbit in ~671 days") { CelestialBody* mars = &sim->bodies[2]; CelestialBody* sun = &sim->bodies[0]; OrbitTracker* tracker = create_orbit_tracker(2); const double max_time = 750.0 * SECONDS_PER_DAY; propagate_and_check(tracker, mars, sun, max_time, 670.9345); } }