STY: apply ruff format fixes to flight.py

Author: ViniciusCMB

rocketpy/simulation/flight.py

@@ -764,8 +764,7 @@ 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",
@@ -1887,7 +1886,9 @@ 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.
@@ -2453,7 +2454,9 @@ 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
@@ -4438,9 +4441,7 @@ 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)