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@ -21,6 +21,8 @@ TEST_CASE("Propagation through perigee (velocity maximum)", "[analytical][propag
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Vec3 pos_before; |
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Vec3 vel_before; |
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craft->orbit.true_anomaly = M_PI / 4.0; |
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orbital_elements_to_cartesian(craft->orbit, earth->mass, &pos_before, &vel_before); |
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double v_before = vec3_magnitude(vel_before); |
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