STY: Apply ruff format to flight.py

Author: ViniciusCMB

rocketpy/simulation/flight.py

@@ -777,7 +777,8 @@ 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: setattr(
+                            lambda self,
+                            added_mass_coefficient=parachute.added_mass_coefficient: setattr(
                                 self,
                                 "parachute_added_mass_coefficient",
                                 added_mass_coefficient,
@@ -999,7 +1000,8 @@ def __check_and_handle_parachute_triggers(
                 lambda self, parachute_porosity=parachute.porosity: setattr(
                     self, "parachute_porosity", parachute_porosity
                 ),
-                lambda self, added_mass_coefficient=parachute.added_mass_coefficient: setattr(
+                lambda self,
+                added_mass_coefficient=parachute.added_mass_coefficient: setattr(
                     self,
                     "parachute_added_mass_coefficient",
                     added_mass_coefficient,
@@ -1405,7 +1407,8 @@ def __check_overshootable_parachute_triggers(
                 lambda self, parachute_porosity=parachute.porosity: setattr(
                     self, "parachute_porosity", parachute_porosity
                 ),
-                lambda self, added_mass_coefficient=parachute.added_mass_coefficient: setattr(
+                lambda self,
+                added_mass_coefficient=parachute.added_mass_coefficient: setattr(
                     self,
                     "parachute_added_mass_coefficient",
                     added_mass_coefficient,
@@ -1988,9 +1991,7 @@ 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.
@@ -2536,9 +2537,7 @@ 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
@@ -4373,7 +4372,9 @@ 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)