MNT: Remove Unused pylint Disable Statements.

.pylintrc

@@ -476,7 +476,6 @@ disable=raw-checker-failed,
         locally-disabled,
         file-ignored,
         suppressed-message,
-        useless-suppression,
         deprecated-pragma, # because we have some pending deprecations in the code.
         use-symbolic-message-instead,
         use-implicit-booleaness-not-comparison-to-string,
@@ -510,6 +509,7 @@ disable=raw-checker-failed,
 # multiple time (only on the command line, not in the configuration file where
 # it should appear only once). See also the "--disable" option for examples.
 enable=
+    useless-suppression
 
 
 [METHOD_ARGS]

CHANGELOG.md

@@ -39,6 +39,8 @@ Attention: The newest changes should be on top -->
 - ENH: MNT: remove duplicate and merge-sync entries from Unreleased changelog [#1062](https://github.com/RocketPy-Team/RocketPy/pull/1062)
 ### Changed
 
+- MNT: MNT: Remove Unused pylint Disable Statements. [#1067](https://github.com/RocketPy-Team/RocketPy/pull/1067)
+
 ### Fixed
 
 ## [v1.13.0] - 2026-07-04

rocketpy/mathutils/function.py

@@ -2531,8 +2531,7 @@ def __lt__(self, other):
         return ~self.__ge__(other)
 
     # Define all possible algebraic operations
-    def __arithmetic_operation(self, other, op):
-        # pylint: disable=too-many-statements
+    def __arithmetic_operation(self, other, op):  # pylint: disable=too-many-statements
         """Generic handler for arithmetic operations between a Function and
         another operand.
 
@@ -3902,7 +3901,7 @@ def __validate_extrapolation(self, extrapolation):
                 extrapolation = "natural"
         return extrapolation
 
-    def to_dict(self, **kwargs):  # pylint: disable=unused-argument
+    def to_dict(self, **kwargs):
         """Serializes the Function instance to a dictionary.
 
         Returns
@@ -4327,7 +4326,7 @@ class funcify_method_decorator:
         class.
         """
 
-        # pylint: disable=C0103,R0903
+        # pylint: disable=C0103
         def __init__(self, func):
             self.func = func
             self.attrname = None
@@ -4359,7 +4358,6 @@ def source_function(*_):
 
                     source = source_function
                     val = Function(source, *args, **kwargs)
-                # pylint: disable=W0201
                 val.__doc__ = self.__doc__
                 val.__cached__ = True
                 cache[self.attrname] = val

rocketpy/motors/fluid.py

@@ -164,7 +164,7 @@ def __str__(self):
 
         return f"Fluid: {self.name}"
 
-    def to_dict(self, **kwargs):  # pylint: disable=unused-argument
+    def to_dict(self, **kwargs):
         discretize = kwargs.get("discretize", False)
 
         density = self.density

rocketpy/motors/hybrid_motor.py

@@ -198,7 +198,6 @@ class HybridMotor(Motor):
         Grain length remains constant throughout the burn. Default is True.
     """
 
-    # pylint: disable=too-many-arguments
     def __init__(  # pylint: disable=too-many-arguments
         self,
         thrust_source,

rocketpy/motors/solid_motor.py

@@ -483,7 +483,7 @@ def center_of_propellant_mass(self):
         center_of_mass = np.full_like(time_source, self.grains_center_of_mass_position)
         return np.column_stack((time_source, center_of_mass))
 
-    # pylint: disable=too-many-arguments, too-many-statements
+    # pylint: disable=too-many-statements
     def evaluate_geometry(self):
         """Calculates grain inner radius and grain height as a function of time
         by assuming that every propellant mass burnt is exhausted. In order to

rocketpy/plots/compare/compare_flights.py

@@ -13,7 +13,7 @@
 # TODO: needs to refactor this class to use the show_or_save_plot
 
 
-class CompareFlights(Compare):  # pylint: disable=too-many-public-methods
+class CompareFlights(Compare):
     """A class to compare the results of multiple flights.
 
     Parameters
@@ -1343,7 +1343,7 @@ def trajectories_2d(self, plane="xy", figsize=(7, 7), legend=None, filename=None
 
         func(flights, names_list, figsize, legend, filename)
 
-    def __plot_xy(  # pylint: disable=too-many-statements
+    def __plot_xy(
         self, flights, names_list, figsize=(7, 7), legend=None, filename=None
     ):
         """Creates a 2D trajectory plot in the X-Y plane that is the combination
@@ -1404,7 +1404,7 @@ def __plot_xy(  # pylint: disable=too-many-statements
         # Save figure
         self.__process_savefig(filename, fig)
 
-    def __plot_xz(  # pylint: disable=too-many-statements
+    def __plot_xz(
         self, flights, names_list, figsize=(7, 7), legend=None, filename=None
     ):
         """Creates a 2D trajectory plot in the X-Z plane that is the combination
@@ -1470,7 +1470,7 @@ def __plot_xz(  # pylint: disable=too-many-statements
         # Save figure
         show_or_save_plot(filename)
 
-    def __plot_yz(  # pylint: disable=too-many-statements
+    def __plot_yz(
         self, flights, names_list, figsize=(7, 7), legend=None, filename=None
     ):
         """Creates a 2D trajectory plot in the Y-Z plane that is the combination

rocketpy/plots/environment_analysis_plots.py

@@ -194,7 +194,7 @@ def average_surface_temperature_evolution(
         self,
         *,
         filename=None,
-    ):  # pylint: disable=too-many-statements
+    ):
         """Plots average temperature progression throughout the day, including
         sigma contours.
 
@@ -269,7 +269,7 @@ def average_surface_temperature_evolution(
 
     def average_surface10m_wind_speed_evolution(
         self, wind_speed_limit=False, *, filename=None
-    ):  # pylint: disable=too-many-statements
+    ):
         """Plots average surface wind speed progression throughout the day,
         including sigma contours.
 
@@ -371,7 +371,7 @@ def average_surface100m_wind_speed_evolution(
         self,
         *,
         filename=None,
-    ):  # pylint: disable=too-many-statements
+    ):
         """Plots average surface wind speed progression throughout the day, including
         sigma contours.
 
@@ -957,7 +957,7 @@ def average_wind_rose_specific_hour(self, hour, fig=None, *, filename=None):
         )
         show_or_save_plot(filename)
 
-    def average_wind_rose_grid(self, *, filename=None):  # pylint: disable=too-many-statements
+    def average_wind_rose_grid(self, *, filename=None):
         """Plot wind roses for all hours of a day, in a grid like plot.
 
         Parameters
@@ -1683,7 +1683,7 @@ def wind_heading_profile_grid(self, clear_range_limits=False, *, filename=None):
         fig.supylabel(f"Altitude AGL ({self.env_analysis.unit_system['length']})")
         show_or_save_plot(filename)
 
-    def animate_wind_speed_profile(self, clear_range_limits=False):  # pylint: disable=too-many-statements
+    def animate_wind_speed_profile(self, clear_range_limits=False):
         """Animation of how wind profile evolves throughout an average day.
 
         Parameters
@@ -1763,7 +1763,7 @@ def update(frame):
         plt.close(fig)
         return HTML(animation.to_jshtml())
 
-    def animate_wind_heading_profile(self, clear_range_limits=False):  # pylint: disable=too-many-statements
+    def animate_wind_heading_profile(self, clear_range_limits=False):
         """Animation of how the wind heading profile evolves throughout an
         average day. Each frame is a different hour of the day.
 

rocketpy/rocket/aero_surface/fins/_geometry.py

@@ -142,7 +142,7 @@ def evaluate_geometrical_parameters(self):
             "roll_geometrical_constant": roll_geometrical_constant,
             "tau": tau,
             "lift_interference_factor": lift_interference_factor,
-            "λ": lambda_,  # pylint: disable=non-ascii-name
+            "λ": lambda_,
             "roll_damping_interference_factor": roll_damping_interference_factor,
             "roll_forcing_interference_factor": roll_forcing_interference_factor,
         }
@@ -204,7 +204,7 @@ def get_data(self, include_outputs=False):
 class _EllipticalGeometry(_FinGeometry):
     """Geometry strategy for elliptical fins."""
 
-    def evaluate_geometrical_parameters(self):  # pylint: disable=too-many-statements
+    def evaluate_geometrical_parameters(self):
         """Calculate elliptical fin geometric parameters."""
         owner = self.owner
 

rocketpy/rocket/aero_surface/generic_surface.py

@@ -382,7 +382,7 @@ def _process_input(self, input_data, coeff_name):
                 " or a callable."
             )
 
-    def __load_generic_surface_csv(self, file_path, coeff_name):  # pylint: disable=too-many-statements,import-outside-toplevel
+    def __load_generic_surface_csv(self, file_path, coeff_name):  # pylint: disable=too-many-statements
         """Load GenericSurface coefficient CSV into a 7D Function.
 
         This loader expects header-based CSV data with one or more independent

rocketpy/rocket/aero_surface/nose_cone.py

@@ -81,7 +81,7 @@ class NoseCone(AeroSurface):
         more about it.
     """
 
-    def __init__(  # pylint: disable=too-many-statements
+    def __init__(
         self,
         length,
         kind,
@@ -222,7 +222,7 @@ def kind(self):
         return self._kind
 
     @kind.setter
-    def kind(self, value):  # pylint: disable=too-many-statements
+    def kind(self, value):
         # Analyzes nosecone type
         # Sets the k for Cp calculation
         # Sets the function which creates the respective curve
@@ -373,7 +373,7 @@ def evaluate_geometrical_parameters(self):
 
         self.fineness_ratio = self.length / (2 * self.base_radius)
 
-    def evaluate_nose_shape(self):  # pylint: disable=too-many-statements
+    def evaluate_nose_shape(self):
         """Calculates and saves nose cone's shape as lists and re-evaluates the
         nose cone's length for a given bluffness ratio. The shape is saved as
         two vectors, one for the x coordinates and one for the y coordinates.

rocketpy/rocket/parachute.py

@@ -294,9 +294,9 @@ def __evaluate_trigger_function(self, trigger):  # pylint: disable=too-many-stat
         The resulting triggerfunc always has signature (p, h, y, sensors, u_dot)
         so Flight can pass both sensors and u_dot when needed.
         """
+        # pylint: disable=function-redefined
         self._trigger_falling_only = False
         self._trigger_needs_height = True
-        # pylint: disable=unused-argument, function-redefined
 
         # Helper to wrap any callable to the internal (p, h, y, sensors, u_dot) API
         def _make_wrapper(fn):

rocketpy/rocket/rocket.py

@@ -2453,7 +2453,7 @@ def _count_positional_args(callable_obj):
             "Function, or callable."
         )
 
-    def __load_rocket_drag_csv(self, file_path, coeff_name):  # pylint: disable=too-many-statements,import-outside-toplevel
+    def __load_rocket_drag_csv(self, file_path, coeff_name):  # pylint: disable=too-many-statements
         """Load Rocket drag CSV into a 7D Function.
 
         Supports either headerless two-column (mach, coefficient) tables or

rocketpy/simulation/flight.py

@@ -659,7 +659,7 @@ def __repr__(self):
             f"name= {self.name})>"
         )
 
-    # pylint: disable=too-many-nested-blocks, too-many-branches, too-many-locals,too-many-statements
+    # pylint: disable=too-many-locals,too-many-statements
     def __simulate(self, verbose):
         """Simulate the flight trajectory."""
         for phase_index, phase in self.time_iterator(self.flight_phases):

rocketpy/simulation/flight_comparator.py

@@ -450,7 +450,7 @@ def _finalize_compare_figure(
         if filename:
             print(f"Plot saved to file: {filename}")
 
-    def compare(  # pylint: disable=too-many-statements
+    def compare(
         self,
         attribute,
         time_range=None,
@@ -730,7 +730,7 @@ def _format_key_events_table(self, results):
 
         return "\n".join(lines)
 
-    def summary(self):  # pylint: disable=too-many-statements
+    def summary(self):
         """
         Print comprehensive comparison summary including key events and metrics.
 

rocketpy/simulation/flight_data_exporter.py

@@ -57,7 +57,7 @@ def export_pressures(self, file_name, time_step):
         """
         f = self._flight
         time_points = np.arange(0, f.t_final, time_step)
-        # pylint: disable=W1514, E1121
+        # pylint: disable=W1514
         with open(file_name, "w") as file:
             if len(f.rocket.parachutes) == 0:
                 logger.info("No parachutes in the rocket, saving static pressure.")

rocketpy/simulation/monte_carlo.py

@@ -96,7 +96,7 @@ def __init__(
         flight,
         export_list=None,
         data_collector=None,
-    ):  # pylint: disable=too-many-statements
+    ):
         """
         Initialize a MonteCarlo object.
 
@@ -171,7 +171,7 @@ def simulate(
         parallel=False,
         n_workers=None,
         **kwargs,
-    ):  # pylint: disable=too-many-statements
+    ):
         """
         Runs the Monte Carlo simulation and saves all data.
 

tests/integration/simulation/test_monte_carlo.py

@@ -119,7 +119,7 @@ def test_monte_carlo_prints(monte_carlo_calisto):
         _post_test_file_cleanup()
 
 
-@patch("matplotlib.pyplot.show")  # pylint: disable=unused-argument
+@patch("matplotlib.pyplot.show")
 def test_monte_carlo_plots(mock_show, monte_carlo_calisto_pre_loaded):
     """Tests the plots methods of the MonteCarlo class."""
     try:

tests/integration/test_encoding.py

@@ -100,7 +100,7 @@ def test_flight_save_load_resimulate(flight_name, include_outputs, request):
 
     assert np.isclose(flight_to_save.t_initial, flight_loaded.t_initial)
     assert np.isclose(flight_to_save.out_of_rail_time, flight_loaded.out_of_rail_time)
-    assert np.isclose(flight_to_save.apogee_time, flight_loaded.apogee_time)
+    assert np.isclose(flight_to_save.apogee_time, flight_loaded.apogee_time, rtol=1e-4)
 
     # Higher tolerance due to random parachute trigger
     assert np.isclose(flight_to_save.t_final, flight_loaded.t_final, rtol=5e-3)

tests/unit/environment/test_environment.py

@@ -814,7 +814,6 @@ def test_pressure_conversion_factor_autodetect_by_model(
     """Regression test for the GEFS/HIRESW pressure-unit bug: NOMADS-GrADS
     models report pressure in hPa (factor 100), THREDDS models in Pa (factor 1).
     A wrong factor silently corrupts the whole atmospheric profile (100x)."""
-    # pylint: disable=protected-access
     factor = example_plain_env._Environment__determine_pressure_conversion_factor(
         None, None, model
     )

tests/unit/mathutils/test_function.py

@@ -647,7 +647,7 @@ def test_set_discrete_based_on_model_non_mutator(linear_func):
         (source_array, cropped_array),
     ],
 )
-def test_crop_ndarray(array3dsource, array3dcropped):  # pylint: disable=unused-argument
+def test_crop_ndarray(array3dsource, array3dcropped):
     """Tests the functionality of crop method of the Function class.
     The source is initialized as a ndarray before cropping.
     """
@@ -795,7 +795,7 @@ def test_crop_invalid_input_raises(bad_x_lim, exc_type):
         (source_array, clipped_array),
     ],
 )
-def test_clip_ndarray(array3dsource, array3dclipped):  # pylint: disable=unused-argument
+def test_clip_ndarray(array3dsource, array3dclipped):
     """Tests the functionality of clip method of the Function class.
     The source is initialized as a ndarray before clipping.
     """

tests/unit/simulation/test_monte_carlo.py

@@ -469,7 +469,7 @@ def import_outputs(self, *args, **kwargs):  # no-op, avoids file I/O
         pass
 
     def simulate(self, number_of_simulations, append=True, **kwargs):
-        # pylint: disable=arguments-differ,unused-argument
+        # pylint: disable=arguments-differ
         self.simulate_calls += 1
         self.num_of_loaded_sims = number_of_simulations
 

tests/unit/simulation/test_multivariate_rejection_sampler.py

@@ -8,7 +8,6 @@
 from rocketpy._encoders import RocketPyEncoder
 
 
-# pylint: disable=too-many-statements
 def test_mrs_initialization():
     """Tests if the MultivariateRejectionSampler initialization opens input and output
     files correctly, and if it raises errors correctly when the files are problematic.