make lint

Author: Gui-FernandesBR

rocketpy/rocket/aero_surface/fins/fin.py

@@ -336,7 +336,7 @@ def compute_forces_and_moments(
         cp,
         omega,
         *args,
-    ):  # pylint: disable=arguments-differ
+    ):  # pylint: disable=arguments-differ,unused-argument
         """Computes the forces and moments acting on the aerodynamic surface.
 
         Parameters

rocketpy/utilities.py

@@ -5,6 +5,7 @@
 from datetime import date
 from importlib.metadata import version
 from pathlib import Path
+from typing import TYPE_CHECKING
 
 import matplotlib.pyplot as plt
 import numpy as np
@@ -16,7 +17,9 @@
 from .mathutils.function import Function
 from .plots.plot_helpers import show_or_save_plot
 from .rocket.aero_surface import TrapezoidalFins
-from .simulation.flight import Flight
+
+if TYPE_CHECKING:  # pragma: no cover
+    from .simulation.flight import Flight
 
 
 def compute_cd_s_from_drop_test(
@@ -524,6 +527,9 @@ def apogee_by_mass(flight, min_mass, max_mass, points=10, plot=True):
         Function object containing the estimated apogee as a function of the
         rocket's mass (without motor nor propellant).
     """
+    # Imported lazily to avoid a circular import (Flight imports utilities).
+    from .simulation.flight import Flight  # pylint: disable=import-outside-toplevel
+
     rocket = flight.rocket
 
     def apogee(mass):
@@ -594,6 +600,9 @@ def liftoff_speed_by_mass(flight, min_mass, max_mass, points=10, plot=True):
         Function object containing the estimated liftoff speed as a function of
         the rocket's mass (without motor nor propellant).
     """
+    # Imported lazily to avoid a circular import (Flight imports utilities).
+    from .simulation.flight import Flight  # pylint: disable=import-outside-toplevel
+
     rocket = flight.rocket
 
     def liftoff_speed(mass):
@@ -652,7 +661,7 @@ def get_instance_attributes(instance):
     return attributes_dict
 
 
-def save_to_rpy(flight: Flight, filename: str, include_outputs=False):
+def save_to_rpy(flight: "Flight", filename: str, include_outputs=False):
     """Saves a .rpy file into the given path, containing key simulation
     informations to reproduce the results.
 

tests/unit/test_parachute_triggers.py

@@ -122,7 +122,9 @@ def derivative_func(_t, _y):
 
     recorded = {}
 
-    def user_trigger(pressure, altitude, state, sensor_list, state_derivative):
+    def user_trigger(  # pylint: disable=unused-argument
+        pressure, altitude, state, sensor_list, state_derivative
+    ):
         recorded["u_dot"] = (
             None if state_derivative is None else np.array(state_derivative)
         )