BUG: Parachute Pressures not being Set before All Info.

.pylintrc

@@ -435,6 +435,7 @@ disable=raw-checker-failed,
         use-implicit-booleaness-not-comparison-to-zero,
         no-else-return,
         inconsistent-return-statements,
+        unspecified-encoding,
 
 # Enable the message, report, category or checker with the given id(s). You can
 # either give multiple identifier separated by comma (,) or put this option

CHANGELOG.md

@@ -40,6 +40,7 @@ straightforward as possible.
 
 ### Fixed
 
+- BUG: Parachute Pressures not being Set before All Info. [#534](https://github.com/RocketPy-Team/RocketPy/pull/534)
 - BUG: Invalid Arguments on Two Dimensional Discretize. [#521](https://github.com/RocketPy-Team/RocketPy/pull/521)
 
 ## [v1.1.4] - 2023-12-07

rocketpy/plots/flight_plots.py

@@ -817,7 +817,6 @@ def pressure_signals(self):
         if len(self.flight.parachute_events) > 0:
             for parachute in self.flight.rocket.parachutes:
                 print("\nParachute: ", parachute.name)
-                self.flight._calculate_pressure_signal()
                 parachute.noise_signal_function()
                 parachute.noisy_pressure_signal_function()
                 parachute.clean_pressure_signal_function()

rocketpy/simulation/flight.py

@@ -1065,6 +1065,7 @@ def __init__(
                                         )
 
         self.t_final = self.t
+        self._calculate_pressure_signal()
         if verbose:
             print("Simulation Completed at Time: {:3.4f} s".format(self.t))
 
@@ -3089,8 +3090,8 @@ def export_pressures(self, file_name, time_step):
             else:
                 for parachute in self.rocket.parachutes:
                     for t in time_points:
-                        p_cl = parachute.clean_pressure_signal(t)
-                        p_ns = parachute.noisy_pressure_signal(t)
+                        p_cl = parachute.clean_pressure_signal_function(t)
+                        p_ns = parachute.noisy_pressure_signal_function(t)
                         file.write(f"{t:f}, {p_cl:.5f}, {p_ns:.5f}\n")
                     # We need to save only 1 parachute data
                     break

tests/test_flight.py

@@ -949,3 +949,31 @@ def test_aerodynamic_moments(flight_calisto_custom_wind, flight_time, expected_v
         test.M2(t),
         test.M3(t),
     ), f"Assertion error for moment vector at {expected_attr}."
+
+
+def test_export_pressures(flight_calisto_robust):
+    """Tests if the method Flight.export_pressures is working as intended.
+
+    Parameters
+    ----------
+    flight_calisto_robust : Flight
+        Flight object to be tested. See the conftest.py file for more info
+        regarding this pytest fixture.
+    """
+    file_name = "pressures.csv"
+    time_step = 0.5
+    parachute = flight_calisto_robust.rocket.parachutes[0]
+
+    flight_calisto_robust.export_pressures(file_name, time_step)
+
+    with open(file_name, "r") as file:
+        contents = file.read()
+
+    expected_data = ""
+    for t in np.arange(0, flight_calisto_robust.t_final, time_step):
+        p_cl = parachute.clean_pressure_signal_function(t)
+        p_ns = parachute.noisy_pressure_signal_function(t)
+        expected_data += f"{t:f}, {p_cl:.5f}, {p_ns:.5f}\n"
+
+    assert contents == expected_data
+    os.remove(file_name)