#include #include #include "../src/physics.h" #include "../src/orbital_mechanics.h" #include using Catch::Matchers::WithinAbs; SCENARIO("True anomaly round-trip conversion and radius sanity checks", "[orbital_elements][true_anomaly][sanity]") { const double parent_mass = 5.972e24; const double a = 7000e3; const double e = 0.3; OrbitalElements elements = {0}; elements.semi_major_axis = a; elements.eccentricity = e; Vec3 pos, vel; // Precomputed analytical values const double expected_r_peri = a * (1.0 - e); // 4900000.0 const double expected_r_apo = a * (1.0 + e); // 9100000.0 auto check_roundtrip = [&](double expected_nu) { elements.true_anomaly = expected_nu; orbital_elements_to_cartesian(elements, parent_mass, &pos, &vel); OrbitalElements reconstructed = cartesian_to_orbital_elements(pos, vel, parent_mass); INFO("Expected nu: " << expected_nu); INFO("Reconstructed: " << reconstructed.true_anomaly); REQUIRE_THAT(reconstructed.true_anomaly, WithinAbs(expected_nu, 1e-12)); }; SECTION("at periapsis (nu = 0)") { check_roundtrip(0.0); } SECTION("at apoapsis (nu = pi)") { check_roundtrip(M_PI); } SECTION("at 90 degrees (nu = pi/2)") { check_roundtrip(M_PI / 2.0); } SECTION("at 270 degrees (nu = 3*pi/2)") { check_roundtrip(3.0 * M_PI / 2.0); } SECTION("periapsis radius = a*(1-e)") { orbital_elements_to_cartesian(elements, parent_mass, &pos, &vel); const double r_peri = vec3_magnitude(pos); INFO("Expected r: " << expected_r_peri); INFO("Calculated r: " << r_peri); REQUIRE_THAT(r_peri, WithinAbs(expected_r_peri, 1e-6)); } SECTION("apoapsis radius = a*(1+e)") { elements.true_anomaly = M_PI; orbital_elements_to_cartesian(elements, parent_mass, &pos, &vel); const double r_apo = vec3_magnitude(pos); INFO("Expected r: " << expected_r_apo); INFO("Calculated r: " << r_apo); REQUIRE_THAT(r_apo, WithinAbs(expected_r_apo, 1e-6)); } }