MNT: ruff

Author: MateusStano

rocketpy/rocket/aero_surface/fins/trapezoidal_fin.py

@@ -25,7 +25,7 @@ class TrapezoidalFin(_TrapezoidalMixin, Fin):
     Attributes
     ----------
     TrapezoidalFin.angular_position : float
-        Angular position of the fin set with respect to the rocket centerline, 
+        Angular position of the fin set with respect to the rocket centerline,
         in degrees.
     TrapezoidalFin.rocket_radius : float
         The reference rocket radius used for lift coefficient normalization, in

rocketpy/rocket/aero_surface/generic_surface.py

@@ -444,4 +444,4 @@ def wrapper(alpha, beta, mach, reynolds, pitch_rate, yaw_rate, roll_rate):
             interpolation="linear",
             extrapolation="natural",
         )
-        return func
+        return func

rocketpy/rocket/aero_surface/linear_generic_surface.py

@@ -407,4 +407,4 @@ def _compute_from_coefficients(
             alpha, beta, mach, reynolds, pitch_rate, yaw_rate, roll_rate
         )
 
-        return lift, side, drag, pitch, yaw, roll
+        return lift, side, drag, pitch, yaw, roll

rocketpy/rocket/aero_surface/rail_buttons.py

@@ -16,7 +16,7 @@ class RailButtons(AeroSurface):
     RailButtons.angular_position : int, float
         Angular position of the rail buttons in degrees measured
         as the rotation around the symmetry axis of the rocket
-        relative to one of the other principal axis. 
+        relative to one of the other principal axis.
         See :ref:`Angular Position Inputs <angular_position>`
     RailButtons.angular_position_rad : float
         Angular position of the rail buttons in radians.

rocketpy/rocket/components.py

@@ -1,5 +1,5 @@
-from copy import deepcopy
 from collections import namedtuple
+from copy import deepcopy
 
 
 class Components:

rocketpy/rocket/rocket.py

@@ -9,9 +9,15 @@
 from rocketpy.motors.empty_motor import EmptyMotor
 from rocketpy.plots.rocket_plots import _RocketPlots
 from rocketpy.prints.rocket_prints import _RocketPrints
-from rocketpy.rocket.aero_surface import (AirBrakes, EllipticalFins, Fins,
-                                          NoseCone, RailButtons, Tail,
-                                          TrapezoidalFins)
+from rocketpy.rocket.aero_surface import (
+    AirBrakes,
+    EllipticalFins,
+    Fins,
+    NoseCone,
+    RailButtons,
+    Tail,
+    TrapezoidalFins,
+)
 from rocketpy.rocket.aero_surface.fins.elliptical_fin import EllipticalFin
 from rocketpy.rocket.aero_surface.fins.free_form_fin import FreeFormFin
 from rocketpy.rocket.aero_surface.fins.free_form_fins import FreeFormFins
@@ -1029,12 +1035,12 @@ def add_surfaces(self, surfaces, positions):
             AeroSurface if more than one surface is to be added.
         positions : int, float, tuple, list, Vector
             Position(s) of the aerodynamic surface's reference point. Can be:
-            
+
             - a single number (int or float) giving the z-coordinate along
               the rocket axis.
             - a sequence of three numbers (x, y, z) representing the full
               position in the user-defined coordinate system.
-            
+
             If passing multiple surfaces, provide a list of positions matching
             each surface in order.
             For NoseCone type, position is the tip coordinate along the axis.
@@ -1646,9 +1652,9 @@ def add_air_brakes(
             7. `sensors` (list): A list of sensors that are attached to the
                rocket. The most recent measurements of the sensors are provided
                with the ``sensor.measurement`` attribute. The sensors are
-               listed in the same order as they are added to the rocket 
+               listed in the same order as they are added to the rocket
                ``interactive_objects``
-                
+
             This function will be called during the simulation at the specified
             sampling rate. The function should evaluate and change the observed
             objects as needed. The function should return None.