STY: apply ruff format fixes

RocketPy-Team · ViniciusCMB · Dec 4, 2025 · Dec 7, 2025 · Dec 8, 2025 · Dec 8, 2025
commit 02d344d3c0b0635fde3fca50b127c285bfbeadcb
@@ -300,9 +300,7 @@ def __init_noise(self, noise):
             + beta * np.random.normal(noise[0], noise[1])
         )
 
-    def __evaluate_trigger_function(
-        self, trigger
-    ):  # pylint: disable=too-many-statements
+    def __evaluate_trigger_function(self, trigger):  # pylint: disable=too-many-statements
         """This is used to set the triggerfunc attribute that will be used to
         interact with the Flight class.
 

@@ -764,7 +764,8 @@ def __simulate(self, verbose):
                             lambda self, parachute_porosity=parachute.porosity: setattr(
                                 self, "parachute_porosity", parachute_porosity
                             ),
-                            lambda self, added_mass_coefficient=parachute.added_mass_coefficient: (
+                            lambda self,
+                            added_mass_coefficient=parachute.added_mass_coefficient: (
                                 setattr(
                                     self,
                                     "parachute_added_mass_coefficient",
@@ -1886,9 +1887,7 @@ def udot_rail2(self, t, u, post_processing=False):  # pragma: no cover
         # Hey! We will finish this function later, now we just can use u_dot
         return self.u_dot_generalized(t, u, post_processing=post_processing)
 
-    def u_dot(
-        self, t, u, post_processing=False
-    ):  # pylint: disable=too-many-locals,too-many-statements
+    def u_dot(self, t, u, post_processing=False):  # pylint: disable=too-many-locals,too-many-statements
         """Calculates derivative of u state vector with respect to time
         when rocket is flying in 6 DOF motion during ascent out of rail
         and descent without parachute.
@@ -2454,9 +2453,7 @@ def u_dot_generalized_3dof(self, t, u, post_processing=False):
 
         return u_dot
 
-    def u_dot_generalized(
-        self, t, u, post_processing=False
-    ):  # pylint: disable=too-many-locals,too-many-statements
+    def u_dot_generalized(self, t, u, post_processing=False):  # pylint: disable=too-many-locals,too-many-statements
         """Calculates derivative of u state vector with respect to time when the
         rocket is flying in 6 DOF motion in space and significant mass variation
         effects exist. Typical flight phases include powered ascent after launch
@@ -4441,7 +4438,9 @@ def add(self, flight_phase, index=None):  # TODO: quite complex method
             new_index = (
                 index - 1
                 if flight_phase.t < previous_phase.t
-                else index + 1 if flight_phase.t > next_phase.t else index
+                else index + 1
+                if flight_phase.t > next_phase.t
+                else index
             )
             flight_phase.t += adjust
             self.add(flight_phase, new_index)

diff --git a/tests/unit/simulation/test_monte_carlo_plots_background.py b/tests/unit/simulation/test_monte_carlo_plots_background.py
@@ -386,8 +386,8 @@ def mock_import_optional_dependency(name):
 
         error_message = str(exc_info.value)
         for expected_msg in expected_messages:
-            assert (
-                expected_msg in error_message
-            ), f"Expected message '{expected_msg}' not found in error: {error_message}"
+            assert expected_msg in error_message, (
+                f"Expected message '{expected_msg}' not found in error: {error_message}"
+            )
 
         assert "Esri.WorldImagery" in error_message