Creation of the magnetometer sensor

docs/conf.py

@@ -85,7 +85,7 @@
 # Napoleon settings
 napoleon_numpy_docstring = True
 napoleon_include_init_with_doc = True
-napoleon_include_private_with_doc = True
+napoleon_include_private_with_doc = False
 napoleon_include_special_with_doc = True
 napoleon_use_admonition_for_examples = True
 napoleon_use_admonition_for_notes = True

docs/reference/classes/Plate.rst

@@ -0,0 +1,6 @@
+Plate Class
+------------
+
+.. autoclass:: rocketpy.Plate
+   :members:
+   :exclude-members: from_dict

docs/reference/classes/Wire.rst

@@ -0,0 +1,6 @@
+Wire Class
+------------
+
+.. autoclass:: rocketpy.Wire
+   :members:
+   :exclude-members: from_dict

docs/reference/classes/sensors/index.rst

@@ -10,3 +10,4 @@ Sensor Classes
    Barometer Class <barometer>
    Gyroscope Class <gyroscope>
    GNSS Receiver Class <gnss_receiver>
+   Magnetometer Class <magnetometer>

docs/reference/classes/sensors/magnetometer.rst

@@ -0,0 +1,6 @@
+Magnetometer Class
+------------------
+
+.. autoclass:: rocketpy.sensors.Magnetometer
+    :members:
+    :exclude-members: from_dict

docs/reference/index.rst

@@ -14,8 +14,10 @@ This reference manual details functions, modules, methods and attributes include
    classes/Components
    classes/Rocket
    classes/Parachute
-   classes/sensors/index.rst
+   Sensor Classes <classes/sensors/index>
    classes/Flight
+   classes/Wire
+   classes/Plate
    Utilities <classes/utils/index>
    classes/EnvironmentAnalysis
    Monte Carlo Analysis <classes/monte_carlo/index>
@@ -31,6 +33,8 @@ This reference manual details functions, modules, methods and attributes include
    Motor Classes Plots and Prints <plots_prints/motors/index>
    AeroSurface Classes Plots and Prints <plots_prints/aero_surfaces/index>
    Rocket Plots and Prints <plots_prints/Rocket/index>
+   Wire Plots and Prints <plots_prints/Wire/index>
+   Plate Plots and Prints <plots_prints/Plate/index>
    Flight Plots and Prints <plots_prints/Flight/index>
    EnvironmentAnalysis Plots and Prints <plots_prints/EnvironmentAnalysis/index>
-   CompareFlights Plots <plots_prints/compare_flights>
+   CompareFlights Plots <plots_prints/compare_flights>

docs/reference/plots_prints/Plate/PlatePlots.rst

@@ -0,0 +1,5 @@
+Plate Plots Class
+-------------------
+
+.. autoclass:: rocketpy.plots.plate_plots._PlatePlots
+   :members:

docs/reference/plots_prints/Plate/PlatePrints.rst

@@ -0,0 +1,5 @@
+Plate Prints Class
+-------------------
+
+.. autoclass:: rocketpy.prints.plate_prints._PlatePrints
+   :members:

docs/reference/plots_prints/Plate/index.rst

@@ -0,0 +1,9 @@
+Plate Plots and Prints Classes
+===============================
+
+.. toctree::
+   :maxdepth: 1
+   :caption: Contents:
+
+   PlatePlots
+   PlatePrints

docs/reference/plots_prints/Wire/WirePlots.rst

@@ -0,0 +1,5 @@
+Wire Plots Class
+-------------------
+
+.. autoclass:: rocketpy.plots.wire_plots._WirePlots
+   :members:

docs/reference/plots_prints/Wire/WirePrints.rst

@@ -0,0 +1,5 @@
+Wire Prints Class
+-------------------
+
+.. autoclass:: rocketpy.prints.wire_prints._WirePrints
+   :members:

docs/reference/plots_prints/Wire/index.rst

@@ -0,0 +1,9 @@
+Wire Plots and Prints Classes
+===============================
+
+.. toctree::
+   :maxdepth: 1
+   :caption: Contents:
+
+   WirePlots
+   WirePrints

docs/requirements.txt

@@ -244,7 +244,7 @@ tzdata==2025.2
     # via pandas
 urllib3==2.5.0
     # via requests
-wcwidth==0.2.13
+wcwidth>=0.8.0
     # via prompt-toolkit
 webencodings==0.5.1
     # via

requirements.txt

@@ -6,3 +6,4 @@ requests
 pytz
 simplekml
 dill
+pywmm

rocketpy/__init__.py

@@ -46,16 +46,18 @@
     LinearGenericSurface,
     NoseCone,
     Parachute,
+    Plate,
     PointMassRocket,
     RailButtons,
     Rocket,
     Tail,
     TrapezoidalFin,
     TrapezoidalFins,
     TubeFins,
+    Wire,
 )
 from .sensitivity import SensitivityModel
-from .sensors import Accelerometer, Barometer, GnssReceiver, Gyroscope
+from .sensors import Accelerometer, Barometer, GnssReceiver, Gyroscope, Magnetometer
 from .simulation import Flight, MonteCarlo, MultivariateRejectionSampler
 from .stochastic import (
     CustomSampler,

rocketpy/environment/environment.py

@@ -5,8 +5,8 @@
 import os
 import re
 import warnings
-from collections.abc import Mapping
 from collections import namedtuple
+from collections.abc import Mapping
 from datetime import datetime
 
 import netCDF4

rocketpy/environment/fetchers/__init__.py

@@ -20,18 +20,6 @@
     fetch_atmospheric_data_from_meteomatics,
     fetch_meteomatics_token,
 )
-from rocketpy.environment.fetchers.open_meteo_fetcher import (
-    OPEN_METEO_ENSEMBLE_MODELS,
-    OPEN_METEO_ENSEMBLE_URL,
-    OPEN_METEO_FORECAST_URL,
-    OPEN_METEO_HISTORICAL_START_DATE,
-    OPEN_METEO_HISTORICAL_URL,
-    OPEN_METEO_PRESSURE_LEVELS,
-    OPEN_METEO_TIMEOUT_SECONDS,
-    build_hourly_variables,
-    fetch_open_meteo_ensemble,
-    fetch_open_meteo_forecast,
-)
 from rocketpy.environment.fetchers.noaa_catalog import (
     FORECAST_MODELS_CATALOG_URL,
     NOAA_MODEL_COLLECTIONS,
@@ -45,6 +33,18 @@
     list_noaa_dataset_identifiers,
     resolve_noaa_collection_path,
 )
+from rocketpy.environment.fetchers.open_meteo_fetcher import (
+    OPEN_METEO_ENSEMBLE_MODELS,
+    OPEN_METEO_ENSEMBLE_URL,
+    OPEN_METEO_FORECAST_URL,
+    OPEN_METEO_HISTORICAL_START_DATE,
+    OPEN_METEO_HISTORICAL_URL,
+    OPEN_METEO_PRESSURE_LEVELS,
+    OPEN_METEO_TIMEOUT_SECONDS,
+    build_hourly_variables,
+    fetch_open_meteo_ensemble,
+    fetch_open_meteo_forecast,
+)
 from rocketpy.environment.fetchers.opendap_fetchers import (
     fetch_aigfs_file_return_dataset,
     fetch_cmc_ensemble,

rocketpy/exceptions.py

@@ -11,8 +11,9 @@ class RocketPyError(Exception):
 
 
 class InvalidParameterError(RocketPyError, ValueError):
-    """Raised when a constructor parameter has an invalid value (e.g. negative
-    radius or mass)."""
+    """Raised when a function, method, or constructor parameter receives an
+    invalid value or violates geometric/physical constraints (e.g., negative
+    mass, out-of-bounds coordinates, or unsupported options)."""
 
 
 class InvalidInertiaError(RocketPyError, ValueError):

rocketpy/motors/motor.py

@@ -168,7 +168,6 @@ class Motor(ABC):
         It will allow to obtain the net thrust in the Flight class.
     """
 
-    # pylint: disable=too-many-statements
     def __init__(
         self,
         thrust_source,