diff --git a/tests/test_flight.py b/tests/test_flight.py index d4ed1e114..fb203b3af 100644 --- a/tests/test_flight.py +++ b/tests/test_flight.py @@ -640,10 +640,10 @@ def test_rail_buttons_forces(flight_calisto_custom_wind): """ test = flight_calisto_custom_wind atol = 5e-3 - assert pytest.approx(3.80358, abs=atol) == test.max_rail_button1_normal_force - assert pytest.approx(1.63602, abs=atol) == test.max_rail_button1_shear_force - assert pytest.approx(1.19353, abs=atol) == test.max_rail_button2_normal_force - assert pytest.approx(0.51337, abs=atol) == test.max_rail_button2_shear_force + assert pytest.approx(3.833613, abs=atol) == test.max_rail_button1_normal_force + assert pytest.approx(1.648938, abs=atol) == test.max_rail_button1_shear_force + assert pytest.approx(1.165307, abs=atol) == test.max_rail_button2_normal_force + assert pytest.approx(0.501229, abs=atol) == test.max_rail_button2_shear_force @pytest.mark.parametrize( @@ -690,7 +690,7 @@ def test_accelerations(flight_calisto_custom_wind, flight_time, expected_values) [ ("t_initial", (0, 0, 0)), ("out_of_rail_time", (0, 2.248727, 25.703072)), - ("apogee_time", (-13.209436, 16.05115, -0.000257)), + ("apogee_time", (-13.204789, 15.990903, -0.000138)), ("t_final", (5, 2, -5.65998)), ], ) @@ -728,7 +728,7 @@ def test_velocities(flight_calisto_custom_wind, flight_time, expected_values): [ ("t_initial", (1.6542528, 0.65918, -0.067107)), ("out_of_rail_time", (5.05334, 2.01364, -1.7541)), - ("apogee_time", (2.35291, -1.8275, -0.87851)), + ("apogee_time", (2.366258, -1.830744, -0.875342)), ("t_final", (0, 0, 159.2212)), ], ) @@ -766,7 +766,7 @@ def test_aerodynamic_forces(flight_calisto_custom_wind, flight_time, expected_va "flight_time, expected_values", [ ("t_initial", (0.17179073815516033, -0.431117, 0)), - ("out_of_rail_time", (0.547026, -1.3727895, 0)), + ("out_of_rail_time", (0.543760, -1.364593, 0)), ("apogee_time", (-0.5874848151271623, -0.7563596, 0)), ("t_final", (0, 0, 0)), ],