diff --git a/docs/conf.py b/docs/conf.py
index 4779e5d5f..ca46e7c33 100644
--- a/docs/conf.py
+++ b/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
diff --git a/docs/notebooks/monte_carlo_analysis/monte_carlo_analysis_outputs/mrs.inputs.txt b/docs/notebooks/monte_carlo_analysis/monte_carlo_analysis_outputs/mrs.inputs.txt
index 0d68c2376..3a9b5454e 100644
--- a/docs/notebooks/monte_carlo_analysis/monte_carlo_analysis_outputs/mrs.inputs.txt
+++ b/docs/notebooks/monte_carlo_analysis/monte_carlo_analysis_outputs/mrs.inputs.txt
@@ -1,116 +1,393 @@
-{"elevation": 113, "gravity": "Function from R1 to R1 : (height (m)) \u2192 (gravity (m/s\u00b2))", "latitude": 39.3897, "longitude": -8.288964, "wind_velocity_x_factor": 1.0, "wind_velocity_y_factor": 1.0, "datum": "SIRGAS2000", "timezone": "UTC", "ensemble_member": 6, "radius": 0.06350803185536065, "mass": 15.321391102645253, "I_11_without_motor": 6.321, "I_22_without_motor": 6.318074651079169, "I_33_without_motor": 0.02231558279750141, "I_12_without_motor": 0, "I_13_without_motor": 0, "I_23_without_motor": 0, "power_off_drag": "Function from R1 to R1 : (Mach Number) \u2192 (Drag Coefficient with Power Off)", "power_on_drag": "Function from R1 to R1 : (Mach Number) \u2192 (Drag Coefficient with Power On)", "power_off_drag_factor": 1.0, "power_on_drag_factor": 1.0, "center_of_mass_without_motor": 0.0, "coordinate_system_orientation": "tail_to_nose", "parachutes": [{"cd_s": 9.796421153818757, "trigger": 800, "sampling_rate": 105, "lag": 1.2889273678634483, "noise": [0, 8.3, 0.5], "name": "Main"}, {"cd_s": 0.9394597068963542, "trigger": "apogee", "sampling_rate": 105, "lag": 1.4863408840421357, "noise": [0, 8.3, 0.5], "name": "Drogue"}], "motors": [{"thrust_source": [[0, 0], [0.055, 100.0], [0.092, 1500.0], [0.1, 2000.0], [0.15, 2200.0], [0.2, 1800.0], [0.5, 1950.0], [1.0, 2034.0], [1.5, 2000.0], [2.0, 1900.0], [2.5, 1760.0], [2.9, 1700.0], [3.0, 1650.0], [3.3, 530.0], [3.4, 350.0], [3.9, 0.0]], "total_impulse": 5051.334409023799, "burn_start_time": 0, "burn_out_time": 3.9, "dry_mass": 1.815, "dry_I_11": 0.125, "dry_I_22": 0.125, "dry_I_33": 0.002, "dry_I_12": 0, "dry_I_13": 0, "dry_I_23": 0, "nozzle_radius": 0.032456100097439426, "grain_number": 5, "grain_density": 1791.4919156464077, "grain_outer_radius": 0.03336766084887191, "grain_initial_inner_radius": 0.015859570445466348, "grain_initial_height": 0.11833708900926163, "grain_separation": 0.005520442830446927, "grains_center_of_mass_position": 0.39720688235605084, "center_of_dry_mass_position": 0.317, "nozzle_position": 0.00044613640497872, "throat_radius": 0.010531081211607219, "interpolate": "linear", "coordinate_system_orientation": "nozzle_to_combustion_chamber", "position": -1.255876687441445}], "aerodynamic_surfaces": [{"length": 0.5575481869662148, "kind": "vonKarman", "base_radius": 0.0635, "bluffness": 0, "rocket_radius": 0.0635, "name": "Nose Cone", "position": [0, 0, 1.133894177473017]}, {"n": 4, "root_chord": 0.11988155918352632, "tip_chord": 0.05955433102562337, "span": 0.11002328692729561, "rocket_radius": 0.0635, "cant_angle": 0.5, "sweep_length": 0.06, "sweep_angle": null, "airfoil": ["../../../data/airfoils/NACA0012-radians.txt", "radians"], "name": "Fins", "position": [0, 0, -1.049681091705158]}, {"top_radius": 0.06350056929758974, "bottom_radius": 0.0431795835697226, "length": 0.061288317308863575, "rocket_radius": 0.0635, "name": "Tail", "position": [0, 0, [0, 0, -1.194656]]}], "rail_buttons": [{"buttons_distance": 0.7011692212916728, "angular_position": 45, "name": "Rail Buttons", "lower_button_position": -0.6163152348259862, "upper_button_position": 0.08485398646568665}], "rail_length": 5, "inclination": 84.47045493851068, "heading": 53.19885912092882}
-{"elevation": 113, "gravity": "Function from R1 to R1 : (height (m)) \u2192 (gravity (m/s\u00b2))", "latitude": 39.3897, "longitude": -8.288964, "wind_velocity_x_factor": 1.0, "wind_velocity_y_factor": 1.0, "datum": "SIRGAS2000", "timezone": "UTC", "ensemble_member": 4, "radius": 0.0634923426395744, "mass": 15.186541205570112, "I_11_without_motor": 6.321, "I_22_without_motor": 6.32969439703265, "I_33_without_motor": 0.031044527733126107, "I_12_without_motor": 0, "I_13_without_motor": 0, "I_23_without_motor": 0, "power_off_drag": "Function from R1 to R1 : (Mach Number) \u2192 (Drag Coefficient with Power Off)", "power_on_drag": "Function from R1 to R1 : (Mach Number) \u2192 (Drag Coefficient with Power On)", "power_off_drag_factor": 1.0, "power_on_drag_factor": 1.0, "center_of_mass_without_motor": 0.0, "coordinate_system_orientation": "tail_to_nose", "parachutes": [{"cd_s": 10.101304635322004, "trigger": 800, "sampling_rate": 105, "lag": 1.449152162843732, "noise": [0, 8.3, 0.5], "name": "Main"}, {"cd_s": 1.0863326011878054, "trigger": "apogee", "sampling_rate": 105, "lag": 1.5807386414953863, "noise": [0, 8.3, 0.5], "name": "Drogue"}], "motors": [{"thrust_source": [[0, 0], [0.055, 100.0], [0.092, 1500.0], [0.1, 2000.0], [0.15, 2200.0], [0.2, 1800.0], [0.5, 1950.0], [1.0, 2034.0], [1.5, 2000.0], [2.0, 1900.0], [2.5, 1760.0], [2.9, 1700.0], [3.0, 1650.0], [3.3, 530.0], [3.4, 350.0], [3.9, 0.0]], "total_impulse": 6334.120250525818, "burn_start_time": 0, "burn_out_time": 3.9, "dry_mass": 1.815, "dry_I_11": 0.125, "dry_I_22": 0.125, "dry_I_33": 0.002, "dry_I_12": 0, "dry_I_13": 0, "dry_I_23": 0, "nozzle_radius": 0.03348962524847486, "grain_number": 5, "grain_density": 1767.1073179570512, "grain_outer_radius": 0.032394751101825256, "grain_initial_inner_radius": 0.01504361534472906, "grain_initial_height": 0.12012668656538848, "grain_separation": 0.00515318449366391, "grains_center_of_mass_position": 0.39673404428016396, "center_of_dry_mass_position": 0.317, "nozzle_position": 0.0016859023790911862, "throat_radius": 0.011074908888687778, "interpolate": "linear", "coordinate_system_orientation": "nozzle_to_combustion_chamber", "position": -1.254658376991242}], "aerodynamic_surfaces": [{"length": 0.5578223347296872, "kind": "vonKarman", "base_radius": 0.0635, "bluffness": 0, "rocket_radius": 0.0635, "name": "Nose Cone", "position": [0, 0, 1.1350307518657035]}, {"n": 4, "root_chord": 0.1203679293308533, "tip_chord": 0.059800875760536006, "span": 0.1091254204553351, "rocket_radius": 0.0635, "cant_angle": 0.5, "sweep_length": 0.06, "sweep_angle": null, "airfoil": ["../../../data/airfoils/NACA0012-radians.txt", "radians"], "name": "Fins", "position": [0, 0, -1.0488985452032389]}, {"top_radius": 0.06453827868465159, "bottom_radius": 0.0431198447535788, "length": 0.05964898322815028, "rocket_radius": 0.0635, "name": "Tail", "position": [0, 0, [0, 0, -1.194656]]}], "rail_buttons": [{"buttons_distance": 0.7012333719890909, "angular_position": 45, "name": "Rail Buttons", "lower_button_position": -0.6173871081166957, "upper_button_position": 0.08384626387239513}], "rail_length": 5, "inclination": 85.13902756092337, "heading": 52.08505981979775}
+{"elevation": 113, "gravity": "Function from R1 to R1 : (height (m)) \u2192 (gravity (m/s\u00b2))", "latitude": 39.3897, "longitude": -8.288964, "wind_velocity_x_factor": 1.0, "wind_velocity_y_factor": 1.0, "datum": "SIRGAS2000", "timezone": "UTC", "ensemble_member": 26, "radius": 0.06350085154042016, "mass": 15.41868602938146, "I_11_without_motor": 6.321, "I_22_without_motor": 6.314009743001999, "I_33_without_motor": 0.042516277850408124, "I_12_without_motor": 0, "I_13_without_motor": 0, "I_23_without_motor": 0, "power_off_drag": "Function from R1 to R1 : (Mach Number) \u2192 (Drag Coefficient with Power Off)", "power_on_drag": "Function from R1 to R1 : (Mach Number) \u2192 (Drag Coefficient with Power On)", "power_off_drag_factor": 1.0, "power_on_drag_factor": 1.0, "center_of_mass_without_motor": 0.0, "coordinate_system_orientation": "tail_to_nose", "parachutes": [{"cd_s": 9.87351827544836, "trigger": 800, "sampling_rate": 105, "lag": 1.5338763231679042, "noise": [0, 8.3, 0.5], "name": "Main"}, {"cd_s": 0.9870787024998243, "trigger": "apogee", "sampling_rate": 105, "lag": 1.4014754896344508, "noise": [0, 8.3, 0.5], "name": "Drogue"}], "motors": [{"thrust_source": [[0, 0], [0.055, 100.0], [0.092, 1500.0], [0.1, 2000.0], [0.15, 2200.0], [0.2, 1800.0], [0.5, 1950.0], [1.0, 2034.0], [1.5, 2000.0], [2.0, 1900.0], [2.5, 1760.0], [2.9, 1700.0], [3.0, 1650.0], [3.3, 530.0], [3.4, 350.0], [3.9, 0.0]], "total_impulse": 4998.800454907017, "burn_start_time": 0, "burn_out_time": 3.9, "dry_mass": 1.815, "dry_I_11": 0.125, "dry_I_22": 0.125, "dry_I_33": 0.002, "dry_I_12": 0, "dry_I_13": 0, "dry_I_23": 0, "nozzle_radius": 0.03223917459521645, "grain_number": 5, "grain_density": 1883.5777764835343, "grain_outer_radius": 0.03390128253364044, "grain_initial_inner_radius": 0.015142918757792974, "grain_initial_height": 0.11886174430852559, "grain_separation": 0.003760153043453114, "grains_center_of_mass_position": 0.3958026817076748, "center_of_dry_mass_position": 0.317, "nozzle_position": -0.0007932754431353338, "throat_radius": 0.011112681197042968, "interpolate": "linear", "coordinate_system_orientation": "nozzle_to_combustion_chamber", "position": -1.2546714035347073}], "aerodynamic_surfaces": [{"length": 0.5590678525392299, "kind": "vonKarman", "base_radius": 0.0635, "bluffness": 0, "rocket_radius": 0.0635, "name": "Nose Cone", "position": [0, 0, 1.1344104201118652]}, {"n": 4, "root_chord": 0.11944031423818127, "tip_chord": 0.06006453824330794, "span": 0.10972808145828339, "rocket_radius": 0.0635, "cant_angle": 0.5, "sweep_length": 0.06, "sweep_angle": null, "airfoil": ["../../../data/airfoils/NACA0012-radians.txt", "radians"], "name": "Fins", "position": [0, 0, -1.049965179010423]}, {"top_radius": 0.06479199126838019, "bottom_radius": 0.04323567648000996, "length": 0.05909791098736002, "rocket_radius": 0.0635, "name": "Tail", "position": [0, 0, [0, 0, -1.194656]]}], "rail_buttons": [{"buttons_distance": 0.6986531598860444, "angular_position": 45, "name": "Rail Buttons", "lower_button_position": -0.6178569783297689, "upper_button_position": 0.08079618155627544}], "rail_length": 5, "inclination": 82.66577730510949, "heading": 54.142713043541164}
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+{"elevation": 113, "gravity": "Function from R1 to R1 : (height (m)) \u2192 (gravity (m/s\u00b2))", "latitude": 39.3897, "longitude": -8.288964, "wind_velocity_x_factor": 1.0, "wind_velocity_y_factor": 1.0, "datum": "SIRGAS2000", "timezone": "UTC", "ensemble_member": 15, "radius": 0.06349927999177071, "mass": 15.62732821456971, "I_11_without_motor": 6.321, "I_22_without_motor": 6.304342109651701, "I_33_without_motor": 0.04760514594921354, "I_12_without_motor": 0, "I_13_without_motor": 0, "I_23_without_motor": 0, "power_off_drag": "Function from R1 to R1 : (Mach Number) \u2192 (Drag Coefficient with Power Off)", "power_on_drag": "Function from R1 to R1 : (Mach Number) \u2192 (Drag Coefficient with Power On)", "power_off_drag_factor": 1.0, "power_on_drag_factor": 1.0, "center_of_mass_without_motor": 0.0, "coordinate_system_orientation": "tail_to_nose", "parachutes": [{"cd_s": 10.075160284366763, "trigger": 800, "sampling_rate": 105, "lag": 1.5126740623331663, "noise": [0, 8.3, 0.5], "name": "Main"}, {"cd_s": 0.9633067377904185, "trigger": "apogee", "sampling_rate": 105, "lag": 1.417239071784473, "noise": [0, 8.3, 0.5], "name": "Drogue"}], "motors": [{"thrust_source": [[0, 0], [0.055, 100.0], [0.092, 1500.0], [0.1, 2000.0], [0.15, 2200.0], [0.2, 1800.0], [0.5, 1950.0], [1.0, 2034.0], [1.5, 2000.0], [2.0, 1900.0], [2.5, 1760.0], [2.9, 1700.0], [3.0, 1650.0], [3.3, 530.0], [3.4, 350.0], [3.9, 0.0]], "total_impulse": 7403.581327796703, "burn_start_time": 0, "burn_out_time": 3.9, "dry_mass": 1.815, "dry_I_11": 0.125, "dry_I_22": 0.125, "dry_I_33": 0.002, "dry_I_12": 0, "dry_I_13": 0, "dry_I_23": 0, "nozzle_radius": 0.03284020180188794, "grain_number": 5, "grain_density": 1809.730692899052, "grain_outer_radius": 0.03338791679405863, "grain_initial_inner_radius": 0.015055942875252058, "grain_initial_height": 0.1203042999308295, "grain_separation": 0.004866751238463473, "grains_center_of_mass_position": 0.39742460414253433, "center_of_dry_mass_position": 0.317, "nozzle_position": -0.0006316590907370708, "throat_radius": 0.010543589499919027, "interpolate": "linear", "coordinate_system_orientation": "nozzle_to_combustion_chamber", "position": -1.255269362996223}], "aerodynamic_surfaces": [{"length": 0.5578298125362579, "kind": "vonKarman", "base_radius": 0.0635, "bluffness": 0, "rocket_radius": 0.0635, "name": "Nose Cone", "position": [0, 0, 1.1336589114438802]}, {"n": 4, "root_chord": 0.12006342194622105, "tip_chord": 0.060468931709032205, "span": 0.10961002478113496, "rocket_radius": 0.0635, "cant_angle": 0.5, "sweep_length": 0.06, "sweep_angle": null, "airfoil": ["../../../data/airfoils/NACA0012-radians.txt", "radians"], "name": "Fins", "position": [0, 0, -1.0498852560599694]}, {"top_radius": 0.0637112975978742, "bottom_radius": 0.04315690776972524, "length": 0.0610625920897514, "rocket_radius": 0.0635, "name": "Tail", "position": [0, 0, [0, 0, -1.194656]]}], "rail_buttons": [{"buttons_distance": 0.6986810839817823, "angular_position": 45, "name": "Rail Buttons", "lower_button_position": -0.6188698733512936, "upper_button_position": 0.07981121063048868}], "rail_length": 5, "inclination": 85.95457831123073, "heading": 55.59499635938657}
diff --git a/docs/notebooks/monte_carlo_analysis/monte_carlo_analysis_outputs/mrs.outputs.txt b/docs/notebooks/monte_carlo_analysis/monte_carlo_analysis_outputs/mrs.outputs.txt
index d299b6c68..648560790 100644
--- a/docs/notebooks/monte_carlo_analysis/monte_carlo_analysis_outputs/mrs.outputs.txt
+++ b/docs/notebooks/monte_carlo_analysis/monte_carlo_analysis_outputs/mrs.outputs.txt
@@ -1,116 +1,393 @@
-{"apogee": 2312.1872472947116, "frontal_surface_wind": -3.0496076096117806, "apogee_y": 792.0643463024578, "lateral_surface_wind": -4.933428593177471, "t_final": 245.8640635159601, "out_of_rail_velocity": 22.602627269750965, "initial_stability_margin": 2.5965475536989793, "out_of_rail_time": 0.3978685698191799, "y_impact": -808.8458905124497, "apogee_x": 473.2474243585599, "impact_velocity": -5.29159675326023, "max_mach_number": 0.6712121311796375, "x_impact": 414.05676153229047, "out_of_rail_stability_margin": 2.676329129911605, "apogee_time": 21.623341277710804}
-{"apogee": 3234.4452475578596, "frontal_surface_wind": -4.337392440631757, "apogee_y": 914.6161005985731, "lateral_surface_wind": -4.330218954821568, "t_final": 308.6136950810929, "out_of_rail_velocity": 25.80568850560873, "initial_stability_margin": 2.5212083871217477, "out_of_rail_time": 0.3566948768302634, "y_impact": -1630.901738601504, "apogee_x": 602.5236652027419, "impact_velocity": -5.1912272264568395, "max_mach_number": 0.861332104930048, "x_impact": 104.54718624691004, "out_of_rail_stability_margin": 2.5904766702124973, "apogee_time": 24.92645235696848}
+{"apogee": 2234.363012975287, "frontal_surface_wind": -4.015500657264189, "apogee_y": 746.9302639391543, "lateral_surface_wind": -4.962994542336395, "t_final": 242.85491410137334, "out_of_rail_velocity": 22.212382995898825, "initial_stability_margin": 2.4408777157767028, "out_of_rail_time": 0.40439552136207935, "y_impact": -997.6272143243594, "apogee_x": 441.46567350420105, "impact_velocity": -5.284647065759667, "max_mach_number": 0.6542024356817283, "x_impact": 195.38461350328657, "out_of_rail_stability_margin": 2.528894112323665, "apogee_time": 21.319685584255506}
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-{"apogee": 2005.5355578422684, "frontal_surface_wind": -4.355137085242682, "apogee_y": 768.6167980634466, "lateral_surface_wind": -5.742328463616666, "t_final": 232.74850709159384, "out_of_rail_velocity": 21.398277969831224, "initial_stability_margin": 2.6161759295091533, "out_of_rail_time": 0.4172765756487621, "y_impact": -980.0914807790709, "apogee_x": 324.1875339535975, "impact_velocity": -5.305869194997984, "max_mach_number": 0.6068006591743482, "x_impact": 332.7869115355111, "out_of_rail_stability_margin": 2.705155629496209, "apogee_time": 20.335146326527934}
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diff --git a/docs/reference/classes/Plate.rst b/docs/reference/classes/Plate.rst
new file mode 100644
index 000000000..3acdcd182
--- /dev/null
+++ b/docs/reference/classes/Plate.rst
@@ -0,0 +1,6 @@
+Plate Class
+------------
+
+.. autoclass:: rocketpy.Plate
+   :members:
+   :exclude-members: from_dict
\ No newline at end of file
diff --git a/docs/reference/classes/Wire.rst b/docs/reference/classes/Wire.rst
new file mode 100644
index 000000000..fdbea4eca
--- /dev/null
+++ b/docs/reference/classes/Wire.rst
@@ -0,0 +1,6 @@
+Wire Class
+------------
+
+.. autoclass:: rocketpy.Wire
+   :members:
+   :exclude-members: from_dict
\ No newline at end of file
diff --git a/docs/reference/classes/sensors/index.rst b/docs/reference/classes/sensors/index.rst
index dd9bb43b5..6674c8388 100644
--- a/docs/reference/classes/sensors/index.rst
+++ b/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>
diff --git a/docs/reference/classes/sensors/magnetometer.rst b/docs/reference/classes/sensors/magnetometer.rst
new file mode 100644
index 000000000..091041fc8
--- /dev/null
+++ b/docs/reference/classes/sensors/magnetometer.rst
@@ -0,0 +1,6 @@
+Magnetometer Class
+------------------
+
+.. autoclass:: rocketpy.sensors.Magnetometer
+    :members:
+    :exclude-members: from_dict
diff --git a/docs/reference/index.rst b/docs/reference/index.rst
index 48d54d989..e1b662326 100644
--- a/docs/reference/index.rst
+++ b/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>
\ No newline at end of file
+   CompareFlights Plots <plots_prints/compare_flights>
diff --git a/docs/reference/plots_prints/Plate/PlatePlots.rst b/docs/reference/plots_prints/Plate/PlatePlots.rst
new file mode 100644
index 000000000..ca872e4ac
--- /dev/null
+++ b/docs/reference/plots_prints/Plate/PlatePlots.rst
@@ -0,0 +1,5 @@
+Plate Plots Class
+-------------------
+
+.. autoclass:: rocketpy.plots.plate_plots._PlatePlots
+   :members:
\ No newline at end of file
diff --git a/docs/reference/plots_prints/Plate/PlatePrints.rst b/docs/reference/plots_prints/Plate/PlatePrints.rst
new file mode 100644
index 000000000..2f56e45e4
--- /dev/null
+++ b/docs/reference/plots_prints/Plate/PlatePrints.rst
@@ -0,0 +1,5 @@
+Plate Prints Class
+-------------------
+
+.. autoclass:: rocketpy.prints.plate_prints._PlatePrints
+   :members:
\ No newline at end of file
diff --git a/docs/reference/plots_prints/Plate/index.rst b/docs/reference/plots_prints/Plate/index.rst
new file mode 100644
index 000000000..5a0a85a53
--- /dev/null
+++ b/docs/reference/plots_prints/Plate/index.rst
@@ -0,0 +1,9 @@
+Plate Plots and Prints Classes
+===============================
+
+.. toctree::
+   :maxdepth: 1
+   :caption: Contents:
+
+   PlatePlots
+   PlatePrints
diff --git a/docs/reference/plots_prints/Wire/WirePlots.rst b/docs/reference/plots_prints/Wire/WirePlots.rst
new file mode 100644
index 000000000..8364b1bb1
--- /dev/null
+++ b/docs/reference/plots_prints/Wire/WirePlots.rst
@@ -0,0 +1,5 @@
+Wire Plots Class
+-------------------
+
+.. autoclass:: rocketpy.plots.wire_plots._WirePlots
+   :members:
\ No newline at end of file
diff --git a/docs/reference/plots_prints/Wire/WirePrints.rst b/docs/reference/plots_prints/Wire/WirePrints.rst
new file mode 100644
index 000000000..77939bfa2
--- /dev/null
+++ b/docs/reference/plots_prints/Wire/WirePrints.rst
@@ -0,0 +1,5 @@
+Wire Prints Class
+-------------------
+
+.. autoclass:: rocketpy.prints.wire_prints._WirePrints
+   :members:
\ No newline at end of file
diff --git a/docs/reference/plots_prints/Wire/index.rst b/docs/reference/plots_prints/Wire/index.rst
new file mode 100644
index 000000000..63ea09ec6
--- /dev/null
+++ b/docs/reference/plots_prints/Wire/index.rst
@@ -0,0 +1,9 @@
+Wire Plots and Prints Classes
+===============================
+
+.. toctree::
+   :maxdepth: 1
+   :caption: Contents:
+
+   WirePlots
+   WirePrints
diff --git a/docs/requirements.txt b/docs/requirements.txt
index 0e9b5ea3d..2c4adc442 100644
--- a/docs/requirements.txt
+++ b/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
diff --git a/requirements.txt b/requirements.txt
index 85fbc96ea..58c03cd34 100644
--- a/requirements.txt
+++ b/requirements.txt
@@ -6,3 +6,4 @@ requests
 pytz
 simplekml
 dill
+pywmm
\ No newline at end of file
diff --git a/rocketpy/__init__.py b/rocketpy/__init__.py
index 27b7c034a..8e346ef14 100644
--- a/rocketpy/__init__.py
+++ b/rocketpy/__init__.py
@@ -46,6 +46,7 @@
     LinearGenericSurface,
     NoseCone,
     Parachute,
+    Plate,
     PointMassRocket,
     RailButtons,
     Rocket,
@@ -53,9 +54,10 @@
     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,
diff --git a/rocketpy/environment/environment.py b/rocketpy/environment/environment.py
index 460f0bc89..0b2e23b1b 100644
--- a/rocketpy/environment/environment.py
+++ b/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
diff --git a/rocketpy/environment/fetchers/__init__.py b/rocketpy/environment/fetchers/__init__.py
index 067208717..4d004c68e 100644
--- a/rocketpy/environment/fetchers/__init__.py
+++ b/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,
diff --git a/rocketpy/exceptions.py b/rocketpy/exceptions.py
index e6bdc4355..875be0ce2 100644
--- a/rocketpy/exceptions.py
+++ b/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):
diff --git a/rocketpy/motors/motor.py b/rocketpy/motors/motor.py
index 9ecb001dd..d83990c8c 100644
--- a/rocketpy/motors/motor.py
+++ b/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,
diff --git a/rocketpy/plots/plate_plots.py b/rocketpy/plots/plate_plots.py
new file mode 100644
index 000000000..ff9fdca3c
--- /dev/null
+++ b/rocketpy/plots/plate_plots.py
@@ -0,0 +1,209 @@
+import matplotlib.pyplot as plt
+import numpy as np
+
+from rocketpy.exceptions import InvalidParameterError
+from rocketpy.plots.plot_helpers import show_or_save_plot
+
+
+class _PlatePlots:
+    """Class that holds plot methods for the Plate class.
+
+    Attributes
+    ----------
+    _PlatePlots.plate : Plate
+        Plate object that will be used for the plots.
+    _PlatePlots.rocket : Rocket, optional
+        Rocket object to which the plate belongs. Default is None.
+    """
+
+    def __init__(self, plate) -> None:
+        """Initializes _PlatePlots class.
+
+        Parameters
+        ----------
+        plate : Plate
+            Plate instance.
+        """
+        self.plate = plate
+        self.rocket = None
+
+    def draw_3d(
+        self,
+        color: str = "teal",
+        marker: str = "h",
+        elev: float | int | None = None,
+        azim: float | int | None = None,
+        filename: str | None = None,
+    ) -> None:
+        """Plots the 3D scatter plot of the discretized points forming the plate
+        surface used to model soft-iron magnetic distortion.
+
+        Parameters
+        ----------
+        color : str, optional
+            Color of the scatter points. A full list of color names can be found
+            at: https://matplotlib.org/stable/gallery/color/named_colors
+            Default is "teal".
+        marker : str, optional
+            Shape of the markers representing the discretization points. A full
+            list of markers can be found at:
+            https://matplotlib.org/stable/api/markers_api.html
+            Default is "h".
+        elev : float, int, optional
+            The elevation angle in degrees rotates the camera above the plane
+            pierced by the vertical axis, with a positive angle corresponding
+            to a location above that plane. If None, the default view is used.
+            Default is None.
+        azim : float, int, optional
+            The azimuthal angle in degrees rotates the camera about the vertical
+            axis. If None, the default view is used. Default is None.
+        filename : str, optional
+            The path the plot should be saved to. If None, the plot will be shown instead
+            of saved. Supported file formats include: eps, jpg, jpeg, pdf, pgf, png, ps,
+            raw, rgba, svg, svgz, tif, tiff, and webp. Default is None.
+        """
+        if self.rocket is None:
+            raise InvalidParameterError(
+                "Plate points list is empty. Add the plate to a rocket before plotting."
+            )
+        # from bacs to ucs
+        x, y, z = zip(*self.plate.points)
+        if self.rocket._csys == -1:
+            x = -np.array(x)
+        else:
+            x = np.array(x)
+        z = self.rocket.center_of_dry_mass_position + (self.rocket._csys * np.array(z))
+        y = np.array(y)
+
+        fig = plt.figure(figsize=(8, 6))
+        ax = fig.add_subplot(111, projection="3d")
+        # plot individual points
+        ax.scatter(x, y, z, color=color, marker=marker, label=self.plate.name)
+        ax.view_init(elev=elev, azim=azim)
+        if self.rocket._csys == 1:
+            ax.invert_xaxis()
+
+        # Labels
+        ax.set_xlabel("X (m)")
+        ax.set_ylabel("Y (m)")
+        ax.set_zlabel("Z (m)")
+        ax.legend()
+
+        print(f"\n{self.plate.name} representation: ")
+        show_or_save_plot(filename)
+
+    def draw(
+        self,
+        vis_args: dict | None = None,
+        plane: str = "xz",
+        color: str = "darkgreen",
+        filename: str | None = None,
+    ) -> None:
+        """Plots the plate along with the 2D cross-sectional outline of the
+        rocket body.
+
+        Parameters
+        ----------
+        vis_args : dict, optional
+            Determines the visual appearance when drawing the rocket body. If
+            None, default parameters are used:
+
+            .. code-block:: python
+
+                {
+                    "background": "#EEEEEE",
+                    "tail": "black",
+                    "nose": "black",
+                    "body": "black",
+                    "fins": "black",
+                    "motor": "black",
+                    "buttons": "black",
+                    "line_width": 1.0,
+                }
+
+            A full list of color names can be found at:
+            https://matplotlib.org/stable/gallery/color/named_colors
+        plane : str, optional
+            Cross-sectional projection plane to represent. Accepted options are
+            "xz" and "yz". Default is "xz".
+        color : str, optional
+            Fill color of the plate. A full list of color names can be found at:
+            https://matplotlib.org/stable/gallery/color/named_colors
+            Default is "darkgreen".
+        filename : str, optional
+            The path the plot should be saved to. If None, the plot is shown
+            interactively. Supported file formats include: eps, jpg, jpeg, pdf,
+            pgf, png, ps, raw, rgba, svg, svgz, tif, tiff, and webp. Default is None.
+        """
+        if self.rocket is None:
+            raise InvalidParameterError(
+                "Plate points list is empty. Add the plate to a rocket before plotting."
+            )
+        if vis_args is None:
+            vis_args = {
+                "background": "#EEEEEE",
+                "tail": "black",
+                "nose": "black",
+                "body": "black",
+                "fins": "black",
+                "motor": "black",
+                "buttons": "black",
+                "line_width": 1.0,
+            }
+
+        ax, _, _ = self.rocket.plots._rocket_shape_plot(vis_args, plane)
+        self._plot_plate_rocket(ax, plane, color)
+
+        plt.ylim([-self.rocket.radius * 4, self.rocket.radius * 6])
+        plt.xlabel("Position (m)")
+        plt.ylabel("Radius (m)")
+        plt.legend(
+            bbox_to_anchor=(1.05, 1),
+            loc="upper left",
+            handlelength=0.8,
+            handleheight=0.6,
+        )
+        plt.tight_layout()
+        show_or_save_plot(filename)
+
+    def _plot_plate_rocket(
+        self, ax, plane: str = "xz", color: str = "darkgreen"
+    ) -> None:
+        """Draws the filled 2D projection of the plate onto the rocket axes.
+
+        Parameters
+        ----------
+        ax : matplotlib.axes.Axes
+            Matplotlib Axes instance where the plate will be drawn.
+        plane : str, optional
+            Cross-sectional projection plane ("xz" or "yz"). Default is "xz".
+        color : str, optional
+            Fill color of the plate projection. Default is "darkgreen".
+        """
+        x, y, z = zip(*self.plate.points)
+
+        x = self.rocket._csys * np.array(x)
+        z = self.rocket.center_of_dry_mass_position + (self.rocket._csys * np.array(z))
+        y = np.array(y)
+
+        if plane == "xz":
+            r = x
+        elif plane == "yz":
+            r = y
+        else:
+            raise InvalidParameterError("Plane value can only be 'xz' or 'yz'.")
+
+        unique_z = np.unique(z)
+        r_min = np.array([r[z == uz].min() for uz in unique_z])
+        r_max = np.array([r[z == uz].max() for uz in unique_z])
+
+        ax.fill_between(
+            unique_z, r_min, r_max, color=color, alpha=0.9, label=self.plate.name
+        )
+
+    def all(self) -> None:
+        """Plots all available graphs for the _PlatePlots instance using default
+        parameters.
+        """
+        self.draw_3d()
+        self.draw()
diff --git a/rocketpy/plots/rocket_plots.py b/rocketpy/plots/rocket_plots.py
index 8e2b35558..dbbcf63f0 100644
--- a/rocketpy/plots/rocket_plots.py
+++ b/rocketpy/plots/rocket_plots.py
@@ -1,6 +1,8 @@
 import matplotlib.pyplot as plt
 import numpy as np
+from matplotlib.pyplot import Axes
 
+from rocketpy.exceptions import InvalidParameterError
 from rocketpy.mathutils.vector_matrix import Vector
 from rocketpy.motors import HybridMotor, LiquidMotor, SolidMotor
 from rocketpy.rocket.aero_surface import Fin, Fins, NoseCone, Tail
@@ -175,8 +177,8 @@ def draw(self, vis_args=None, plane="xz", *, filename=None):
             A full list of color names can be found at: \
             https://matplotlib.org/stable/gallery/color/named_colors
         plane : str, optional
-            Plane in which the rocket will be drawn. Default is 'xz'. Other
-            options is 'yz'. Used only for sensors representation.
+            Plane in which the rocket will be drawn. Default is "xz". Other
+            options is "yz". Used only for sensors representation.
         filename : str | None, optional
             The path the plot should be saved to. By default None, in which case
             the plot will be shown instead of saved. Supported file endings are:
@@ -198,16 +200,7 @@ def draw(self, vis_args=None, plane="xz", *, filename=None):
                 "line_width": 1.0,
             }
 
-        _, ax = plt.subplots(figsize=(8, 6), facecolor=vis_args["background"])
-        ax.set_aspect("equal")
-        ax.grid(True, linestyle="--", linewidth=0.5)
-
-        csys = self.rocket._csys
-        reverse = csys == 1
-        surfaces = self.rocket.aerodynamic_surfaces.sort_by_position(reverse=reverse)
-
-        drawn_surfaces = self._draw_aerodynamic_surfaces(ax, vis_args, plane, surfaces)
-        last_radius, last_x = self._draw_tubes(ax, drawn_surfaces, vis_args)
+        ax, last_radius, last_x = self._rocket_shape_plot(vis_args, plane)
         self._draw_motor(last_radius, last_x, ax, vis_args)
         self._draw_rail_buttons(ax, vis_args)
         self._draw_center_of_mass_and_pressure(ax)
@@ -224,11 +217,13 @@ def draw(self, vis_args=None, plane="xz", *, filename=None):
 
     def __validate_aerodynamic_surfaces(self, plane):
         if not self.rocket.aerodynamic_surfaces:
-            raise ValueError(
+            raise InvalidParameterError(
                 "The rocket must have at least one aerodynamic surface to be drawn."
             )
         if plane not in ("xz", "yz"):
-            raise ValueError("The plane must be 'xz' or 'yz'. The default is 'xz'.")
+            raise InvalidParameterError(
+                "The plane must be 'xz' or 'yz'. The default is 'xz'."
+            )
 
     def _draw_aerodynamic_surfaces(self, ax, vis_args, plane, surfaces):
         """Draws the aerodynamic surfaces and saves the position of the points
@@ -382,7 +377,7 @@ def _draw_fin(self, ax, surface, position, drawn_surfaces, vis_args, plane):
             x_rotated = self.rocket._csys * z_fin_rotated + position.z
             y_rotated = y_fin_rotated + position.y
         else:  # pragma: no cover
-            raise ValueError("Plane must be 'xz' or 'yz'.")
+            raise InvalidParameterError("Plane must be 'xz' or 'yz'.")
 
         ax.plot(
             x_rotated,
@@ -418,7 +413,7 @@ def _draw_generic_surface(
                 # y position of the surface is the y position in the plot
                 y_pos = position[1]
             case _:  # pragma: no cover
-                raise ValueError("Plane must be 'xz' or 'yz'.")
+                raise InvalidParameterError("Plane must be 'xz' or 'yz'.")
 
         ax.scatter(
             x_pos,
@@ -692,7 +687,7 @@ def _draw_sensors(self, ax, sensors, plane):
                     y_pos = pos[1]
                     normal_y = sensor.normal_vector.y
                 case _:  # pragma: no cover
-                    raise ValueError("Plane must be 'xz' or 'yz'.")
+                    raise InvalidParameterError("Plane must be 'xz' or 'yz'.")
 
             # line length is 2/5 of the rocket radius
             line_length = self.rocket.radius / 2.5
@@ -720,6 +715,227 @@ def _draw_sensors(self, ax, sensors, plane):
                     zorder=10,
                 )
 
+    def draw_wires(
+        self,
+        wires: str = "all",
+        vis_args: dict | None = None,
+        plane: str = "xz",
+        color: str | list[str] | tuple[str, ...] = "default",
+        marker: str = "o",
+        linestyle: str = "-",
+        filename: str | None = None,
+    ) -> None:
+        """Plots all the wires that are attached to the rocket.
+
+        Parameters
+        ----------
+        wires : str, optional
+            String that determines which wires will be plotted:
+
+            - "communication_wires": only communication wires will be shown.
+            - "ignition_wires": only ignition wires will be shown.
+            - "all": all wires are shown.
+
+            Default is "all".
+        vis_args : dict, optional
+            Determines the visual aspects when drawing the rocket. If ``None``,
+            default values are used. Default values are:
+
+            .. code-block:: python
+
+                {
+                    "background": "#EEEEEE",
+                    "tail": "black",
+                    "nose": "black",
+                    "body": "black",
+                    "fins": "black",
+                    "motor": "black",
+                    "buttons": "black",
+                    "line_width": 1.0,
+                }
+
+            A full list of color names can be found at:
+            https://matplotlib.org/stable/gallery/color/named_colors
+        plane : str, optional
+            Cross-sectional projection plane to represent. Accepted options are
+            "xz" and "yz". Default is "xz".
+        color : str, list of str, tuple of str, optional
+            Color of the wires. If it is a list or tuple, it must contain one
+            color for each wire. A full list of color names can be found at:
+            https://matplotlib.org/stable/gallery/color/named_colors
+            Default is "default", meaning a distinct color from the default cycle
+            is assigned to each wire.
+        marker : str, optional
+            Shape of the markers representing the wire endpoints. A full list
+            of markers can be found at:
+            https://matplotlib.org/stable/api/markers_api.html
+            Default is "o".
+        linestyle : str, optional
+            Style of the line that represents the wire. A full list of
+            linestyles can be found at:
+            https://matplotlib.org/stable/gallery/lines_bars_and_markers/linestyles.html
+            Default is "-".
+        filename : str, optional
+            The path the plot should be saved to. If None, the plot will be shown instead
+            of saved. Supported file formats include: eps, jpg, jpeg, pdf, pgf, png, ps,
+            raw, rgba, svg, svgz, tif, tiff, and webp. Default is None.
+        """
+        if vis_args is None:
+            vis_args = {
+                "background": "#EEEEEE",
+                "tail": "black",
+                "nose": "black",
+                "body": "black",
+                "fins": "black",
+                "motor": "black",
+                "buttons": "black",
+                "line_width": 1.0,
+            }
+
+        ax, _, _ = self._rocket_shape_plot(vis_args, plane)
+
+        if wires == "all":
+            wires_list = self.rocket._ignition_wires + self.rocket._communication_wires
+        elif wires == "communication_wires":
+            wires_list = self.rocket._communication_wires
+        elif wires == "ignition_wires":
+            wires_list = self.rocket._ignition_wires
+        else:
+            raise InvalidParameterError(
+                "Only 'communication_wires', 'ignition_wires', or 'all' are valid inputs."
+            )
+
+        if isinstance(color, str):
+            if color == "default":
+                color_list = plt.rcParams["axes.prop_cycle"].by_key()["color"]
+            else:
+                color_list = [color] * len(wires_list)
+        elif isinstance(color, (list, tuple)):
+            if len(color) == len(wires_list):
+                color_list = color
+            else:
+                raise InvalidParameterError(
+                    "The length of the list of colors must be the same as the number of wires."
+                )
+        else:
+            raise InvalidParameterError(
+                "The accepted entries for color are str, list, or tuple."
+            )
+
+        for wire, color_wire in zip(wires_list, color_list):
+            wire.plots._draw_wires(
+                ax, plane, color_wire, marker, linestyle, endpoints_names=False
+            )
+
+        plt.title("Wires representation")
+        plt.xlim()
+        plt.ylim([-self.rocket.radius * 4, self.rocket.radius * 6])
+        plt.xlabel("Position (m)")
+        plt.ylabel("Radius (m)")
+        leg = plt.legend(bbox_to_anchor=(1.05, 1), loc="upper left")
+        if leg:
+            for handle in leg.legend_handles:
+                handle.set_linewidth(2.0)
+        plt.tight_layout()
+        show_or_save_plot(filename)
+
+    def draw_plates(
+        self,
+        vis_args: dict | None = None,
+        plane: str = "xz",
+        color: str | list[str] | tuple[str, ...] = "default",
+        filename: str | None = None,
+    ) -> None:
+        """Plots all the plates that are attached to the rocket.
+
+        Parameters
+        ----------
+        vis_args : dict, optional
+            Determines the visual aspects when drawing the rocket. If ``None``,
+            default values are used. Default values are:
+
+            .. code-block:: python
+
+                {
+                    "background": "#EEEEEE",
+                    "tail": "black",
+                    "nose": "black",
+                    "body": "black",
+                    "fins": "black",
+                    "motor": "black",
+                    "buttons": "black",
+                    "line_width": 1.0,
+                }
+
+            A full list of color names can be found at:
+            https://matplotlib.org/stable/gallery/color/named_colors
+        plane : str, optional
+            Cross-sectional projection plane to represent. Accepted options are
+            "xz" and "yz". Default is "xz".
+        color : str, list of str, tuple of str, optional
+            Color of the plates. If it is a list or tuple, it must contain one
+            color for each plate. A full list of color names can be found at:
+            https://matplotlib.org/stable/gallery/color/named_colors
+            Default is "default", meaning a distinct color from the default cycle
+            is applied to each plate.
+        filename : str, optional
+            The path the plot should be saved to. If None, the plot will be shown instead
+            of saved. Supported file formats include: eps, jpg, jpeg, pdf, pgf, png, ps,
+            raw, rgba, svg, svgz, tif, tiff, and webp. Default is None.
+        """
+        if vis_args is None:
+            vis_args = {
+                "background": "#EEEEEE",
+                "tail": "black",
+                "nose": "black",
+                "body": "black",
+                "fins": "black",
+                "motor": "black",
+                "buttons": "black",
+                "line_width": 1.0,
+            }
+        ax, _, _ = self._rocket_shape_plot(vis_args, plane)
+
+        if self.rocket.plates:
+            plates_list, _, _ = zip(*self.rocket.plates)
+        else:
+            plates_list = ()
+
+        if isinstance(color, str):
+            if color == "default":
+                color_list = plt.rcParams["axes.prop_cycle"].by_key()["color"]
+            else:
+                color_list = [color] * len(plates_list)
+        elif isinstance(color, (list, tuple)):
+            if len(color) == len(plates_list):
+                color_list = color
+            else:
+                raise InvalidParameterError(
+                    "The length of the list of colors must be the same as the number of plates."
+                )
+        else:
+            raise InvalidParameterError(
+                "The accepted entries for color are str, list, or tuple."
+            )
+
+        sorted_plates_list = sorted(plates_list, key=lambda p: p.area, reverse=True)
+        for plate, color_plate in zip(sorted_plates_list, color_list):
+            plate.plots._plot_plate_rocket(ax, plane, color_plate)
+
+        plt.title("Plates representation")
+        plt.xlim()
+        plt.ylim([-self.rocket.radius * 4, self.rocket.radius * 6])
+        plt.xlabel("Position (m)")
+        plt.ylabel("Radius (m)")
+        plt.legend(
+            bbox_to_anchor=(1.05, 1),
+            loc="upper left",
+            handlelength=0.8,
+            handleheight=0.6,
+        )
+        plt.tight_layout()
+        show_or_save_plot(filename)
+
     def all(self):
         """Prints out all graphs available about the Rocket. It simply calls
         all the other plotter methods in this class.
@@ -760,3 +976,63 @@ def all(self):
         print("\nThrust-to-Weight Plot")
         print("-" * 40)
         self.thrust_to_weight()
+
+        # Wire and Plate plots
+        print("\n Wire plots")
+        print("-" * 20)
+        self.draw_wires()
+        self.draw_plates()
+
+    def _rocket_shape_plot(
+        self, vis_args: dict | None = None, plane: str = "xz"
+    ) -> tuple[Axes, float, float]:
+        """
+        This is an auxiliary function that plots the outline of the rocket
+        including the aerodynamic surfaces. 
+
+        Parameters
+        ----------
+        vis_args : dict, optional
+            Determines the visual aspects when drawing the rocket. If ``None``,
+            default values are used. Default values are:
+
+            .. code-block:: python
+
+                {
+                    "background": "#EEEEEE",
+                    "tail": "black",
+                    "nose": "black",
+                    "body": "black",
+                    "fins": "black",
+                    "motor": "black",
+                    "line_width": 2.0,
+                }
+
+            A full list of color names can be found at: \
+            https://matplotlib.org/stable/gallery/color/named_colors
+        plane: str, optional
+            Plane that it is wanted to be represented:
+            Accepted options are "xz" and "yz"
+            Default value is "xz"
+
+        Returns
+        -------
+        ax: Axes 
+            Axes instance in which the rocket outline has been displayed.
+        radius: float
+            Last radius of the rocket, (y axis in the plot).
+        last_x: float
+            Last x value of the plot, (z axis value in the rocket frame).
+        """
+        _, ax = plt.subplots(figsize=(8, 6), facecolor=vis_args["background"])
+        ax.set_aspect("equal")
+        ax.grid(True, linestyle="--", linewidth=0.5)
+
+        csys = self.rocket._csys
+        reverse = csys == 1
+        surfaces = self.rocket.aerodynamic_surfaces.sort_by_position(reverse=reverse)
+
+        drawn_surfaces = self._draw_aerodynamic_surfaces(ax, vis_args, plane, surfaces)
+        radius, last_x = self._draw_tubes(ax, drawn_surfaces, vis_args)
+
+        return ax, radius, last_x
diff --git a/rocketpy/plots/wire_plots.py b/rocketpy/plots/wire_plots.py
new file mode 100644
index 000000000..ed22d6268
--- /dev/null
+++ b/rocketpy/plots/wire_plots.py
@@ -0,0 +1,205 @@
+import matplotlib.pyplot as plt
+from matplotlib.pyplot import Axes
+
+from rocketpy.exceptions import InvalidParameterError
+from rocketpy.plots.plot_helpers import show_or_save_plot
+
+
+class _WirePlots:
+    """Class that holds plot methods for the Wire class.
+
+    Attributes
+    ----------
+    _WirePlots.wire : Wire
+        Wire object that will be used for the plots.
+    _WirePlots.rocket : Rocket, optional
+        Rocket object the wire belongs to. Default is None.
+    """
+
+    def __init__(self, wire) -> None:
+        """Initializes _WirePlots class.
+
+        Parameters
+        ----------
+        wire : Wire
+            Wire instance.
+        """
+        self.wire = wire
+        self.rocket = None
+
+    def draw(
+        self,
+        vis_args: dict | None = None,
+        plane: str = "xz",
+        color: str = "salmon",
+        marker: str = "o",
+        linestyle: str = "-",
+        endpoints_names: bool = True,
+        filename: str | None = None,
+    ) -> None:
+        """Plots the wire and the rocket together.
+
+        Parameters
+        ----------
+        vis_args : dict, optional
+            Determines the visual aspects when drawing the rocket. If ``None``,
+            default values are used. Default values are:
+
+            .. code-block:: python
+
+                {
+                    "background": "#EEEEEE",
+                    "tail": "black",
+                    "nose": "black",
+                    "body": "black",
+                    "fins": "black",
+                    "motor": "black",
+                    "buttons": "black",
+                    "line_width": 1.0,
+                }
+
+            A full list of color names can be found at:
+            https://matplotlib.org/stable/gallery/color/named_colors
+        plane : str, optional
+            Plane to represent. Accepted options are "xz" and "yz".
+            Default value is "xz".
+        color : str, optional
+            Color of the wire line and markers. A full list of color names can
+            be found at: https://matplotlib.org/stable/gallery/color/named_colors
+            Default is "salmon".
+        marker : str, optional
+            Shape of the marker representing wire endpoints. A full list of markers
+            can be found at: https://matplotlib.org/stable/api/markers_api.html
+            Default is "o".
+        linestyle : str, optional
+            Line style used to represent the wire. A full list of linestyles
+            can be found at:
+            https://matplotlib.org/stable/gallery/lines_bars_and_markers/linestyles.html
+            Default is "-".
+        endpoints_names : bool, optional
+            Boolean defining whether the endpoint labels are displayed. If False,
+            they will not be displayed. If True, the labels "Endpoint A" and
+            "Endpoint B" will be shown. Default is True.
+        filename : str, optional
+            The path the plot should be saved to. If None, the plot will be shown instead
+            of saved. Supported file formats include: eps, jpg, jpeg, pdf, pgf, png, ps,
+            raw, rgba, svg, svgz, tif, tiff, and webp. Default is None.∫
+        """
+        if self.rocket is None:
+            raise InvalidParameterError("Add the wire to a rocket before plotting.")
+        if vis_args is None:
+            vis_args = {
+                "background": "#EEEEEE",
+                "tail": "black",
+                "nose": "black",
+                "body": "black",
+                "fins": "black",
+                "motor": "black",
+                "buttons": "black",
+                "line_width": 1.0,
+            }
+
+        ax, _, _ = self.rocket.plots._rocket_shape_plot(vis_args, plane)
+        self._draw_wires(ax, plane, color, marker, linestyle, endpoints_names)
+
+        plt.xlim()
+        plt.ylim([-self.rocket.radius * 4, self.rocket.radius * 6])
+        plt.xlabel("Position (m)")
+        plt.ylabel("Radius (m)")
+        plt.legend(bbox_to_anchor=(1.05, 1), loc="upper left")
+        plt.tight_layout()
+        show_or_save_plot(filename)
+
+    def _draw_wires(
+        self,
+        ax: Axes,
+        plane: str = "xz",
+        color: str = "salmon",
+        marker: str = "o",
+        linestyle: str = "-",
+        endpoints_names: bool = True,
+    ) -> None:
+        """Plots the endpoints and the wire on the specified Matplotlib axes.
+
+        Parameters
+        ----------
+        ax : Axes
+            Matplotlib Axes instance on which the wire will be plotted.
+        plane : str, optional
+            Plane to represent. Accepted options are "xz" and "yz".
+            Default is "xz".
+        color : str, optional
+            Color of the wire and endpoint markers. A full list of color names can
+            be found at: https://matplotlib.org/stable/gallery/color/named_colors
+            Default is "salmon".
+        marker : str, optional
+            Shape of the marker representing wire endpoints. A full list of markers
+            can be found at: https://matplotlib.org/stable/api/markers_api.html
+            Default is "o".
+        linestyle : str, optional
+            Line style used to represent the wire. A full list of linestyles
+            can be found at:
+            https://matplotlib.org/stable/gallery/lines_bars_and_markers/linestyles.html
+            Default is "-".
+        endpoints_names : bool, optional
+            Boolean defining whether the endpoint labels are displayed. If False,
+            they will not be displayed. If True, the labels "Endpoint A" and
+            "Endpoint B" will be shown. Default is True.
+        """
+        # change nose to tail with nose origin
+        endpoint_a_x = self.wire._wire_endpoints_bacs[0][0] * self.rocket._csys
+        endpoint_b_x = self.wire._wire_endpoints_bacs[1][0] * self.rocket._csys
+
+        endpoint_a_y = self.wire._wire_endpoints_bacs[0][1]
+        endpoint_b_y = self.wire._wire_endpoints_bacs[1][1]
+
+        endpoint_a_z = self.rocket.center_of_dry_mass_position + (
+            self.wire._wire_endpoints_bacs[0][2] * self.rocket._csys
+        )
+        endpoint_b_z = self.rocket.center_of_dry_mass_position + (
+            self.wire._wire_endpoints_bacs[1][2] * self.rocket._csys
+        )
+        if plane == "xz":
+            r_a = endpoint_a_x
+            r_b = endpoint_b_x
+        elif plane == "yz":
+            r_a = endpoint_a_y
+            r_b = endpoint_b_y
+        else:
+            raise InvalidParameterError("The plane must be 'xz' or 'yz'.")
+
+        z = [endpoint_a_z, endpoint_b_z]
+        r = [r_a, r_b]
+
+        # plot lines connecting endpoints
+        ax.plot(z, r, color=color, linestyle=linestyle, label=self.wire.name)
+
+        if endpoints_names:
+            ax.scatter(
+                z, r, marker=marker, color=color, zorder=5, label="Wire endpoints"
+            )
+
+            ax.annotate(
+                "Endpoint A",
+                xy=(endpoint_a_z, r_a),
+                xytext=(6, 10),
+                textcoords="offset points",
+                fontsize=9,
+            )
+
+            ax.annotate(
+                "Endpoint B",
+                xy=(endpoint_b_z, r_b),
+                xytext=(6, -14),
+                textcoords="offset points",
+                fontsize=9,
+            )
+        else:
+            ax.scatter(z, r, marker=marker, color=color, zorder=5)
+
+    def all(self) -> None:
+        """Plots all available graphs for the _WirePlots instance using default
+        parameters.
+        """
+        print(f"\n{self.wire.name} representation: ")
+        self.draw()
diff --git a/rocketpy/prints/plate_prints.py b/rocketpy/prints/plate_prints.py
new file mode 100644
index 000000000..e5e017d27
--- /dev/null
+++ b/rocketpy/prints/plate_prints.py
@@ -0,0 +1,51 @@
+class _PlatePrints:
+    """Class that holds print methods for the Plate class.
+
+    Attributes
+    ----------
+    _PlatePrints.plate : Plate
+        Plate object that will be used for the prints.
+    """
+
+    def __init__(self, plate) -> None:
+        """Initializes _PlatePrints class.
+
+        Parameters
+        ----------
+        plate: Plate
+            Plate instance.
+        """
+        self.plate = plate
+
+    def len_points_print(self) -> None:
+        """Prints the number of points that form the plate."""
+        len_points = len(self.plate.points)
+        print(f"Number of points that form the plate: {len_points}")
+
+    def properties_material(self) -> None:
+        """Prints material properties including relative magnetic permeability,
+        thickness, area, and volume.
+        """
+        print(
+            f"Relative magnetic permeability of the material: {self.plate.relative_magnetic_permeability}"
+        )
+        print(
+            f"Absolute magnetic permeability: {self.plate.absolute_magnetic_permeability} H/m"
+        )
+        print(f"Thickness: {self.plate.thickness} m")
+        print(f"Area: {self.plate.area} m^2")
+        print(f"Volume: {self.plate.volume} m^3")
+
+    def magnetic_distortion_matrix(self) -> None:
+        """Prints the magnetic distortion matrix at all recorded positions."""
+        for key in self.plate._magnetic_distortion_matrices:
+            print(
+                f"Magnetic distortion matrix at position: {key} is {self.plate._magnetic_distortion_matrices[key]}"
+            )
+
+    def all(self) -> None:
+        """Prints all print methods about the Plate."""
+        print(f"\n{self.plate.name} information: ")
+        self.properties_material()
+        self.len_points_print()
+        self.magnetic_distortion_matrix()
diff --git a/rocketpy/prints/rocket_prints.py b/rocketpy/prints/rocket_prints.py
index 7b768ea2f..602857e9a 100644
--- a/rocketpy/prints/rocket_prints.py
+++ b/rocketpy/prints/rocket_prints.py
@@ -11,27 +11,18 @@ class _RocketPrints:
 
     """
 
-    def __init__(self, rocket):
+    def __init__(self, rocket) -> None:
         """Initializes _EnvironmentPrints class
 
         Parameters
         ----------
         rocket: rocketpy.rocket
             Instance of the rocket class.
-
-        Returns
-        -------
-        None
         """
         self.rocket = rocket
 
-    def inertia_details(self):
-        """Print inertia details.
-
-        Returns
-        -------
-        None
-        """
+    def inertia_details(self) -> None:
+        """Print inertia details."""
         print("\nInertia Details\n")
         print(f"Rocket Mass: {self.rocket.mass:.3f} kg (without motor)")
         print(f"Rocket Dry Mass: {self.rocket.dry_mass:.3f} kg (with unloaded motor)")
@@ -56,13 +47,8 @@ def inertia_details(self):
             f"Rocket Inertia (with unloaded motor) 23: {self.rocket.dry_I_23:.3f} kg*m2"
         )
 
-    def rocket_geometrical_parameters(self):
-        """Print rocket geometrical parameters.
-
-        Returns
-        -------
-        None
-        """
+    def rocket_geometrical_parameters(self) -> None:
+        """Print rocket geometrical parameters."""
         print("\nGeometrical Parameters\n")
         print(f"Rocket Maximum Radius: {self.rocket.radius} m")
         print(f"Rocket Frontal Area: {self.rocket.area:.6f} m2")
@@ -94,13 +80,8 @@ def rocket_geometrical_parameters(self):
             f"Rocket Center of Mass - Rocket Loaded Center of Mass: {distance:.3f} m\n"
         )
 
-    def rocket_aerodynamics_quantities(self):
-        """Print rocket aerodynamics quantities.
-
-        Returns
-        -------
-        None
-        """
+    def rocket_aerodynamics_quantities(self) -> None:
+        """Print rocket aerodynamics quantities."""
         print("\nAerodynamics Lift Coefficient Derivatives\n")
         for surface, _ in self.rocket.aerodynamic_surfaces:
             if isinstance(surface, GenericSurface):
@@ -141,23 +122,13 @@ def rocket_aerodynamics_quantities(self):
             f"{abs(self.rocket.center_of_mass(0) - self.rocket.cp_position(0)):.3f} m\n"
         )
 
-    def parachute_data(self):
-        """Print parachute data.
-
-        Returns
-        -------
-        None
-        """
+    def parachute_data(self) -> None:
+        """Print parachute data."""
         for chute in self.rocket.parachutes:
             chute.all_info()
 
-    def all(self):
-        """Prints all print methods about the Environment.
-
-        Returns
-        -------
-        None
-        """
+    def all(self) -> None:
+        """Prints all print methods about the Environment."""
         self.inertia_details()
         self.rocket_geometrical_parameters()
         self.rocket_aerodynamics_quantities()
diff --git a/rocketpy/prints/wire_prints.py b/rocketpy/prints/wire_prints.py
new file mode 100644
index 000000000..54d4f4677
--- /dev/null
+++ b/rocketpy/prints/wire_prints.py
@@ -0,0 +1,52 @@
+class _WirePrints:
+    """Class that holds print methods for the Wire class.
+
+    Attributes
+    ----------
+    _WirePrints.wire : Wire
+        Wire object that will be used for the prints.
+    """
+
+    def __init__(self, wire) -> None:
+        """Initializes _WirePrints class.
+
+        Parameters
+        ----------
+        wire : Wire
+            Wire instance.
+        """
+        self.wire = wire
+
+    def current(self) -> None:
+        """Prints the current flowing through the wire."""
+        print(f"Current: {self.wire.current} A")
+
+    def endpoints(self) -> None:
+        """Prints the wire endpoints coordinates in the body axis coordinate system."""
+        print(
+            f"Endpoint A is {self.wire._wire_endpoints_bacs[0]}, Endpoint B is {self.wire._wire_endpoints_bacs[1]} in the body axis coordinate system"
+        )
+
+    def wire_type(self) -> None:
+        """Prints the wire type and, if applicable, the ignition wire function."""
+        if self.wire.wire_type == "communications":
+            print("Wire type: communications type")
+        else:
+            print("Wire type: ignition type")
+            print(f"Ignition wire function: {self.wire.ignition_wire_function}")
+
+    def magnetic_field_vectors(self) -> None:
+        """Prints the magnetic field vectors stored in the wire for all recorded positions."""
+        for position, b_field in self.wire.magnetic_field.items():
+            if position is not None:
+                print(
+                    f"Magnetic field vector at position {position} due to the wire is {b_field} T"
+                )
+
+    def all(self) -> None:
+        """Prints all print methods about the Wire."""
+        print(f"\n{self.wire.name} information: ")
+        self.wire_type()
+        self.current()
+        self.magnetic_field_vectors()
+        self.endpoints()
diff --git a/rocketpy/rocket/__init__.py b/rocketpy/rocket/__init__.py
index 3fa907f2d..65968b81b 100644
--- a/rocketpy/rocket/__init__.py
+++ b/rocketpy/rocket/__init__.py
@@ -19,5 +19,7 @@
 )
 from rocketpy.rocket.components import Components
 from rocketpy.rocket.parachute import Parachute
+from rocketpy.rocket.plate import Plate
 from rocketpy.rocket.point_mass_rocket import PointMassRocket
 from rocketpy.rocket.rocket import Rocket
+from rocketpy.rocket.wire import Wire
diff --git a/rocketpy/rocket/aero_surface/nose_cone.py b/rocketpy/rocket/aero_surface/nose_cone.py
index bebe63642..cc7020b78 100644
--- a/rocketpy/rocket/aero_surface/nose_cone.py
+++ b/rocketpy/rocket/aero_surface/nose_cone.py
@@ -71,6 +71,9 @@ class NoseCone(AeroSurface):
         Function which defines the lift coefficient as a function of the angle
         of attack and the Mach number. Takes as input the angle of attack in
         radians and the Mach number. Returns the lift coefficient.
+    Nosecone.radius: Function
+        Function that returns the radius as a function of the z axis
+        based on the local coordinate system.
     NoseCone.clalpha : float
         Lift coefficient slope. Has units of 1/rad.
     NoseCone.plots : plots.aero_surface_plots._NoseConePlots
@@ -137,6 +140,7 @@ def __init__(
         self._rocket_radius = rocket_radius
         self._base_radius = base_radius
         self._length = length
+        self._radius_function = None
         if bluffness is not None:
             if bluffness > 1 or bluffness < 0:  # pragma: no cover
                 raise ValueError(
@@ -217,6 +221,12 @@ def power(self, value):
         self.evaluate_center_of_pressure()
         self.evaluate_nose_shape()
 
+    @property
+    def radius(self):
+        if self._radius_function is None:
+            self._radius_function = self._compute_radius_function()
+        return self._radius_function
+
     @property
     def kind(self):
         return self._kind
@@ -456,6 +466,23 @@ def final_shape(x):
             )
         self.fineness_ratio = self.length / (2 * self.base_radius)
 
+    def _compute_radius_function(self):
+        """Calculates and returns the radius of the nose cone
+        at a certain height z, based on the local
+        coordinate system.
+
+        Local coordinate system:
+            - Origin located at the tip of the nose cone.
+            - Z axis along the longitudinal axis of symmetry, positive downwards (top -> bottom).
+
+        Returns
+        -------
+        nose_radius : Function
+            Function instance mapping axial position z in meters to the corresponding nose cone radius.
+        """
+        data = np.column_stack(self.shape_vec)
+        return Function(data, inputs="z", outputs="nose_radius")
+
     def evaluate_lift_coefficient(self):
         """Calculates and returns nose cone's lift coefficient.
         The lift coefficient is saved and returned. This function
diff --git a/rocketpy/rocket/aero_surface/tail.py b/rocketpy/rocket/aero_surface/tail.py
index 3e738f99c..c2b77df0f 100644
--- a/rocketpy/rocket/aero_surface/tail.py
+++ b/rocketpy/rocket/aero_surface/tail.py
@@ -30,6 +30,9 @@ class Tail(AeroSurface):
     Tail.rocket_radius: int, float
         The reference rocket radius used for lift coefficient normalization in
         meters.
+    Tail.radius : Function
+        Function that returns the radius of the tail at a certain z relative to the
+        local coordinate system.
     Tail.name : str
         Name of the tail. Default is 'Tail'.
     Tail.cpx : int, float
@@ -82,6 +85,7 @@ def __init__(self, top_radius, bottom_radius, length, rocket_radius, name="Tail"
         self._bottom_radius = bottom_radius
         self._length = length
         self._rocket_radius = rocket_radius
+        self._radius_function = None
 
         self.evaluate_geometrical_parameters()
         self.evaluate_lift_coefficient()
@@ -112,6 +116,13 @@ def bottom_radius(self, value):
         self.evaluate_lift_coefficient()
         self.evaluate_center_of_pressure()
 
+    @property
+    def radius(self):
+        if self._radius_function is None:
+            self._radius_function = self._compute_radius_function()
+
+        return self._radius_function
+
     @property
     def length(self):
         return self._length
@@ -153,6 +164,25 @@ def evaluate_shape(self):
             np.array([self.top_radius, self.bottom_radius]),
         ]
 
+    def _compute_radius_function(self):
+        """Calculates and returns the radius of the tail
+        at a certain height z, based on the local
+        coordinate system.
+
+        Local coordinate system:
+            - Z axis along the longitudinal axis of symmetry, positive downwards (top -> bottom).
+            - Origin located at the top of the tail (generally the portion closest to the rocket's nose).
+
+        Returns
+        -------
+        tail_radius : Function
+            Function instance mapping axial position z in meters to the corresponding tail radius.
+        """
+        z = np.linspace(self.shape_vec[0][0], self.shape_vec[0][1], 100)
+        r = np.linspace(self.shape_vec[1][0], self.shape_vec[1][1], 100)
+        data = np.column_stack((z, r))
+        return Function(data, inputs="z", outputs="tail_radius")
+
     def evaluate_lift_coefficient(self):
         """Calculates and returns tail's lift coefficient.
         The lift coefficient is saved and returned. This function
diff --git a/rocketpy/rocket/components.py b/rocketpy/rocket/components.py
index 57e4d12f8..4aeb799cd 100644
--- a/rocketpy/rocket/components.py
+++ b/rocketpy/rocket/components.py
@@ -92,6 +92,29 @@ def get_by_type(self, component_type):
         ]
         return component_type_list
 
+    def get_position_by_type(self, component_type):
+        """Search the list of components and return a list with all the
+        components and their position as a tuple for the given type.
+
+        Parameters
+        ----------
+        component_type : type
+            The type of component to be returned.
+
+        Returns
+        --------
+        list[tuple]
+            A list of components and corresponding positions
+            matching the specified type.
+
+        """
+        component_type_list = [
+            (c.component, c.position)
+            for c in self._components
+            if isinstance(c.component, component_type)
+        ]
+        return component_type_list
+
     def get_tuple_by_type(self, component_type):
         """Search the list of components and return a list with all the components
         of the given type.
diff --git a/rocketpy/rocket/plate.py b/rocketpy/rocket/plate.py
new file mode 100644
index 000000000..bfe7ef9f9
--- /dev/null
+++ b/rocketpy/rocket/plate.py
@@ -0,0 +1,779 @@
+import math as m
+
+import numpy as np
+from matplotlib.path import Path
+
+from rocketpy.exceptions import InvalidParameterError
+from rocketpy.mathutils import Matrix, Vector
+from rocketpy.plots.plate_plots import _PlatePlots
+from rocketpy.prints.plate_prints import _PlatePrints
+
+
+class Plate:
+    """Defines a surface on the rocket fuselage or interior to account for
+    soft-iron magnetic distortion affecting magnetometer readings.
+
+    Attributes
+    ----------
+    Plate.shape : str
+        Shape of the plate ("circular", "rectangular", or "personalized").
+    Plate.dimensions : float, int, tuple or list
+        Dimensions of the plate. For "circular", a float/int representing the
+        radius; for "rectangular", a tuple (width, height); for
+        "personalized", a list of 3D vertices [x, y, z].
+    Plate.material : str
+        Material composing the plate ("iron", "carbon_steel", or "personalized").
+    Plate.absolute_magnetic_permeability : float
+        Absolute magnetic permeability of the ``material`` in H/m (or N/A^2).
+    Plate.relative_magnetic_permeability : float
+        Ratio of absolute magnetic permeability to the magnetic permeability of
+        free space (dimensionless).
+    Plate.thickness : float, int
+        Thickness of the plate in meters.
+    Plate.area : float
+        Surface area of the plate in square meters.
+    Plate.volume : float
+        Volume of the plate in cubic meters.
+    Plate._magnetic_distortion_matrices : dict
+        Dictionary of soft-iron distortion matrices induced by the plate. Keys
+        are position vector tuples (x, y, z) in the Body Axis Coordinate System,
+        and values are the corresponding 3x3 Matrix instances.
+    Plate.points : list[list]
+        Discretized points defining the plate surface in the Body Axis
+        Coordinate System.
+    Plate.grid_spacing : float, optional
+        Spacing between grid points in meters for "personalized" plates.
+    Plate.z_points : int, optional
+        Number of points along the longitudinal axis for "circular" or
+        "rectangular" plates.
+    Plate.angular_points : int, optional
+        Number of angular points for "circular" or "rectangular" plates.
+    Plate.name : str
+        Name of the plate.
+    """
+
+    def __init__(
+        self,
+        shape: str,
+        dimensions: int | float | list | tuple,
+        material: str,
+        thickness: int | float,
+        absolute_magnetic_permeability: int | float | None = None,
+        relative_magnetic_permeability: int | float | None = None,
+        grid_spacing: int | float = 0.001,
+        z_points: int = 40,
+        angular_points: int = 70,
+        name: str = "Plate",
+    ) -> None:
+        """Initializes the Plate.
+
+        Parameters
+        ----------
+        shape : str
+            Shape of the plate. Options are:
+
+            - If "circular": the plate will be built as a circle, and the parameter
+              ``dimensions`` refers to the radius in meters.
+            - If "rectangular": the plate will be built a rectangle, and the parameter
+              ``dimensions`` refers to the sides length in meters.
+            - If "personalized": the plate is created by the
+              vertices defined in ``dimensions``.
+        dimensions : float, int, list, tuple
+            Dimensions defining the plate geometry depending on ``shape``:
+
+            - If "circular": float or int representing radius in meters.
+            - If "rectangular": sequence of [width, height] in meters, or a
+              single float/int for a square.
+            - If "personalized": sequence of at least 3 non-collinear 3D vertices
+              [x, y, z] defined in the User-defined Coordinate System.
+        material : str
+            Material composing the plate. Allowed values are "iron",
+            "carbon_steel", or "personalized".
+        thickness : float, int
+            Thickness of the plate in meters.
+        absolute_magnetic_permeability : float, int, optional
+            Absolute magnetic permeability of the ``material`` in H/m. Default is
+            None.
+        relative_magnetic_permeability : float, int, optional
+            Dimensionless ratio of material permeability to free space
+            permeability. If defined, it overrides
+            ``absolute_magnetic_permeability``. Default is None.
+        grid_spacing : float, optional
+            Distance between points that form the plate in meters when ``shape`` is
+            "personalized". Default is 0.001.
+        z_points : int, optional
+            Number of points along the longitudinal axis for "circular" or
+            "rectangular" plates. Default is 40.
+        angular_points : int, optional
+            Number of angular points for "circular" or
+            "rectangular" plates. Default is 70.
+        name : str, optional
+            Name of the plate. Default is "Plate".
+        """
+        self._magnetic_distortion_matrices = {}
+        self.points = []
+        self.plots = _PlatePlots(self)
+        self.prints = _PlatePrints(self)
+        self._validate_parameters(
+            material,
+            absolute_magnetic_permeability,
+            relative_magnetic_permeability,
+            shape,
+            dimensions,
+            z_points,
+            angular_points,
+            grid_spacing,
+        )
+        self.thickness = thickness
+        self.name = name
+
+    def _validate_parameters(
+        self,
+        material,
+        absolute_magnetic_permeability,
+        relative_magnetic_permeability,
+        shape,
+        dimensions,
+        z_points,
+        angular_points,
+        grid_spacing,
+    ) -> None:
+        """Validates input parameters and defines attributes."""
+        self._validate_material(
+            material, absolute_magnetic_permeability, relative_magnetic_permeability
+        )
+        self._validate_shape(shape, dimensions, z_points, angular_points, grid_spacing)
+
+    def _validate_material(
+        self, material, absolute_magnetic_permeability, relative_magnetic_permeability
+    ) -> None:
+        """Validates and sets material magnetic permeability parameters."""
+        if not isinstance(material, str):
+            raise InvalidParameterError("'material' argument must be a string.")
+
+        mu_0 = 4 * np.pi * 1e-7
+        predefined_materials = {"iron": 1.25e-3, "carbon_steel": 1.2e-4}
+
+        if material in predefined_materials:
+            self.material = material
+            self.absolute_magnetic_permeability = predefined_materials[material]
+            self.relative_magnetic_permeability = (
+                self.absolute_magnetic_permeability / mu_0
+            )
+
+        elif material == "personalized":
+            if not isinstance(absolute_magnetic_permeability, (float, int, type(None))):
+                raise InvalidParameterError(
+                    "The 'absolute_magnetic_permeability' must be None, float, or int."
+                )
+            if (
+                absolute_magnetic_permeability is None
+                and relative_magnetic_permeability is None
+            ):
+                raise InvalidParameterError(
+                    "Either 'absolute_magnetic_permeability' or 'relative_magnetic_permeability' must be specified when 'material' is 'personalized'."
+                )
+
+            self.material = "personalized"
+
+            if relative_magnetic_permeability is None:
+                self.absolute_magnetic_permeability = absolute_magnetic_permeability
+                self.relative_magnetic_permeability = (
+                    absolute_magnetic_permeability / mu_0
+                )
+
+            elif isinstance(relative_magnetic_permeability, (float, int)):
+                self.relative_magnetic_permeability = relative_magnetic_permeability
+                self.absolute_magnetic_permeability = (
+                    relative_magnetic_permeability * mu_0
+                )
+
+            else:
+                raise InvalidParameterError(
+                    "The 'relative_magnetic_permeability' must be None, float, or int."
+                )
+        else:
+            raise InvalidParameterError(
+                "'material' argument must be 'iron', 'carbon_steel', or 'personalized'."
+            )
+
+    def _validate_shape(
+        self, shape, dimensions, z_points, angular_points, grid_spacing
+    ) -> None:
+        """Validates ``shape`` parameters and assigns attributes."""
+        if isinstance(shape, str):
+            if shape in ("circular", "rectangular"):
+                self._validate_not_personalized_shape(
+                    shape, dimensions, z_points, angular_points
+                )
+            elif shape == "personalized":
+                self.shape = shape
+                self.dimensions = dimensions
+                self.grid_spacing = grid_spacing
+                self.z_points = None
+                self.angular_points = None
+            else:
+                raise InvalidParameterError(
+                    "'shape' must be 'circular', 'rectangular', or 'personalized'."
+                )
+        else:
+            raise InvalidParameterError("'shape' must be defined as a string.")
+
+    def _validate_not_personalized_shape(
+        self, shape, dimensions, z_points, angular_points
+    ):
+        """Validates parameters for standard geometric shapes ('circular' or 'rectangular')."""
+        if shape == "circular":
+            if not isinstance(dimensions, (float, int)):
+                raise InvalidParameterError(
+                    "For 'circular' shape, dimensions must be a float or int representing radius in meters."
+                )
+            self.shape = "circular"
+            self.dimensions = dimensions
+            self.z_points = z_points
+            self.angular_points = angular_points
+            self.grid_spacing = None
+
+        elif shape == "rectangular":
+            self.shape = "rectangular"
+            self.z_points = z_points
+            self.angular_points = angular_points
+            self.grid_spacing = None
+
+            if isinstance(dimensions, (float, int)):
+                width = float(dimensions)
+                height = float(dimensions)
+            elif isinstance(dimensions, (list, tuple)) and len(dimensions) == 2:
+                width = float(dimensions[0])
+                height = float(dimensions[1])
+            else:
+                raise InvalidParameterError(
+                    "For 'rectangular' shape, dimensions must be a float/int (square) or a 2-element sequence [width, height]."
+                )
+            self.dimensions = (width, height)
+
+    def define_plate_position(
+        self,
+        rocket,
+        position: float | int | None = None,
+        height: float | int | None = None,
+    ) -> None:
+        """Defines the geometry, area, and volume of the plate when attached
+        to a rocket instance.
+
+        Parameters
+        ----------
+        rocket : Rocket
+            Rocket instance to which the plate is attached.
+        position : float, int, optional
+            Angle between the User-defined Coordinate System y-axis and the
+            geometric center of the plate in degrees. The angle is positive from
+            y to -x. See `Rocket Axes Definition <https://docs.rocketpy.org/en/latest/user/rocket/rocket_axes.html>`_
+            for more information.
+        height : float, int, optional
+            Coordinate of the geometric center along the rocket
+            longitudinal axis in the User-defined Coordinate System in
+            meters.
+        """
+        self.generate_points(rocket, position, height)
+        if self.shape == "rectangular":
+            self.area = self.dimensions[0] * self.dimensions[1]
+        elif self.shape == "circular":
+            self.area = np.pi * (self.dimensions**2)
+        else:  # personalized
+            self.area = len(self.points) * (self.grid_spacing**2)
+        self.volume = self.area * self.thickness
+
+    def generate_points(
+        self,
+        rocket,
+        position: float | int | None = None,
+        height: float | int | None = None,
+    ) -> None:
+        """Generates the points that represent the plate surface in the Body Axis
+        Coordinate System.
+
+        Parameters
+        ----------
+        rocket : Rocket
+            Rocket instance to which the plate is attached.
+        position : float, int, optional
+            Angle between the User-defined Coordinate System y-axis and the
+            geometric center of the plate in degrees. The angle is positive from
+            y to -x. See `Rocket Axes Definition <https://docs.rocketpy.org/en/latest/user/rocket/rocket_axes.html>`_
+            for more information.
+        height : float, int, optional
+            Axial coordinate of the geometric center along the rocket
+            longitudinal axis in the User-defined Coordinate System in
+            meters. Required when the ``shape`` of the plate is "circular" or
+            "rectangular".
+        """
+        self.points = []
+
+        if self.shape == "personalized":
+            self._generate_personalized_internal_plate(rocket)
+        else:
+            if self.shape == "circular":
+                upper_z = height + self.dimensions
+                lower_z = height - self.dimensions
+            else:
+                upper_z = height + self.dimensions[1] / 2
+                lower_z = height - self.dimensions[1] / 2
+            geometric_center_angle = position * (np.pi / 180)
+            for z in np.linspace(lower_z, upper_z, self.z_points):
+                if not rocket.z_bounds_check(z, frame="ucs")[0]:
+                    continue
+
+                r = rocket.general_radius(z, frame="ucs")
+                if r <= 1e-6:
+                    continue
+                alpha, beta = self._define_angles(z, geometric_center_angle, r, height)
+                for theta in np.linspace(alpha, beta, self.angular_points):
+                    x = -r * np.sin(theta)
+                    y = r * np.cos(theta)
+
+                    # Transform to Body Axis Coordinate System (BACS)
+                    z_bacs = (z - self.center_of_dry_mass_position) * self._csys
+                    if self._csys == -1:  # nose_to_tail
+                        self.points.append([-x, y, z_bacs])
+                    else:  # tail_to_nose
+                        self.points.append([x, y, z_bacs])
+
+    def _define_angles(
+        self, z, geometric_center_angle, r, height
+    ) -> tuple[float, float]:
+        """Calculates the angular span for the definition of the points
+        that form the plate at axial position z.
+
+        Parameters
+        ----------
+        z : float
+            Longitudinal coordinate along the rocket axis in meters.
+        geometric_center_angle : float
+            Angle of the geometric center of the plate in radians.
+        r : float
+            Rocket fuselage radius at coordinate z in meters.
+        height : float
+            Longitudinal position of the geometric center of the plate in
+            meters.
+
+        Returns
+        -------
+        alpha : float
+            Starting angular bound in radians.
+        beta : float
+            Ending angular bound in radians.
+        """
+        if self.shape == "circular":
+            alpha, beta = self._circular_angle_calculation(
+                z=z, center_z=height, geometric_center_angle=geometric_center_angle, r=r
+            )
+        else:  # rectangular
+            alpha, beta = self._rectangular_angle_calculation(geometric_center_angle, r)
+        return alpha, beta
+
+    def _circular_angle_calculation(
+        self, z, center_z, geometric_center_angle, r
+    ) -> tuple[float, float]:
+        """Calculates the angular span for the definition of the points
+        that form the plate when it is "circular" at axial position z.
+
+        Parameters
+        ----------
+        z : float
+            Current longitudinal coordinate in meters.
+        center_z : float
+            Longitudinal coordinate of the geometric center in meters.
+        geometric_center_angle : float
+            Angular position of the geometric center in radians.
+        r : float
+            Rocket radius at coordinate z in meters.
+
+        Returns
+        -------
+        alpha : float
+            Starting angular bound in radians.
+        beta : float
+            Ending angular bound in radians.
+        """
+        dz = z - center_z
+        inside_sqrt = max(self.dimensions**2 - dz**2, 0)
+        half_extension_angle = m.sqrt(inside_sqrt) / r
+        alpha = geometric_center_angle - half_extension_angle
+        beta = geometric_center_angle + half_extension_angle
+        return alpha, beta
+
+    def _rectangular_angle_calculation(
+        self, geometric_center_angle, r
+    ) -> tuple[float, float]:
+        """Calculates the angular span for the definition of the points
+        that form the plate when it is "rectangular" at axial position z.
+
+        Parameters
+        ----------
+        geometric_center_angle : float
+            Angular position of the geometric center in radians.
+        r : float
+            Rocket radius at the current coordinate in meters.
+
+        Returns
+        -------
+        alpha : float
+            Starting angular bound in radians.
+        beta : float
+            Ending angular bound in radians.
+        """
+        extension_angle = self.dimensions[0] / r
+        alpha = geometric_center_angle - extension_angle / 2
+        beta = geometric_center_angle + extension_angle / 2
+        return alpha, beta
+
+    def _generate_personalized_internal_plate(
+        self,
+        rocket,
+    ) -> None:
+        """Generates a planar 2D grid of 3D points bounded by arbitrary vertices,
+        constrained within the rocket fuselage.
+
+        Parameters
+        ----------
+        rocket : Rocket
+            Rocket instance to which the plate belongs.
+        """
+        vertices = self._vertices_definition(rocket)
+
+        centroid = [sum(col) / len(vertices) for col in zip(*vertices)]
+        cx, cy, cz = centroid[0], centroid[1], centroid[2]
+
+        ux, uy, uz, vx, vy, vz = self._calculate_uv_frame(vertices)
+
+        uv_vertices = [
+            (
+                (pt[0] - cx) * ux + (pt[1] - cy) * uy + (pt[2] - cz) * uz,
+                (pt[0] - cx) * vx + (pt[1] - cy) * vy + (pt[2] - cz) * vz,
+            )
+            for pt in vertices
+        ]
+
+        u_coords, v_coords = zip(*uv_vertices)
+        plate_path = Path(uv_vertices)
+        final_3d_points = []
+
+        curr_u = min(u_coords)
+        while curr_u <= max(u_coords):
+            curr_v = min(v_coords)
+            while curr_v <= max(v_coords):
+                if plate_path.contains_point((curr_u, curr_v)):
+                    p3d_x = cx + (curr_u * ux) + (curr_v * vx)
+                    p3d_y = cy + (curr_u * uy) + (curr_v * vy)
+                    p3d_z = cz + (curr_u * uz) + (curr_v * vz)
+
+                    if m.hypot(p3d_x, p3d_y) < rocket.general_radius(
+                        p3d_z, frame="bacs"
+                    ):
+                        final_3d_points.append([p3d_x, p3d_y, p3d_z])
+
+                curr_v += self.grid_spacing
+            curr_u += self.grid_spacing
+
+        self.points = final_3d_points
+
+    def _vertices_definition(self, rocket) -> list:
+        """Transforms vertices in user-defined coordinate system into
+        the Body Axis Coordinate System.
+
+        Parameters
+        ----------
+        rocket : Rocket
+            Rocket instance to which the plate belongs.
+
+        Returns
+        -------
+        vertices : list
+            List of 3D vertices transformed into the BACS frame.
+        """
+        vertices = []
+        cdm_user_frame = Vector([0, 0, self.center_of_dry_mass_position])
+        if len(self.dimensions) < 3:
+            raise InvalidParameterError(
+                "At least 3 vertices are required for a personalized plate."
+            )
+        for pt in self.dimensions:
+            self._check_entry_dimensions(pt, rocket)
+
+            # Transform to BACS
+            sensor_vec = Vector(pt) - cdm_user_frame
+            if self._csys == -1:
+                vertices.append([-sensor_vec[0], sensor_vec[1], -sensor_vec[2]])
+            else:
+                vertices.append([sensor_vec[0], sensor_vec[1], sensor_vec[2]])
+        collinear = []
+        for i in range(len(vertices) - 2):
+            e1 = Vector(vertices[i + 1]) - Vector(vertices[i])
+            e2 = Vector(vertices[i + 2]) - Vector(vertices[i + 1])
+            collinear.append(abs(e1 ^ e2) <= 1e-12)
+
+        if all(collinear):
+            raise InvalidParameterError(
+                "All vertices of the personalized plate are collinear."
+            )
+        return vertices
+
+    def _check_entry_dimensions(self, pt, rocket) -> None:
+        """Validates that a vertex lies within the rocket's longitudinal and radial boundaries.
+
+        Parameters
+        ----------
+        pt : list, tuple, Vector
+            Coordinates [x, y, z] in the User-defined Coordinate System.
+        rocket : Rocket
+            Rocket instance in which boundaries are checked.
+        """
+        if not rocket.z_bounds_check(pt[2], frame="ucs")[0]:
+            raise InvalidParameterError(
+                f"The z coordinate {pt[2]} of point {pt} is outside the rocket longitudinal bounds."
+            )
+
+        if m.hypot(pt[0], pt[1]) > rocket.general_radius(pt[2], frame="ucs"):
+            raise InvalidParameterError(
+                f"Point {pt} exceeds the rocket fuselage radius at z = {pt[2]} m."
+            )
+
+    def _calculate_uv_frame(
+        self, vertices
+    ) -> tuple[float, float, float, float, float, float]:
+        """Calculates an orthonormal planar basis (u, v) from polygon vertices.
+
+        Parameters
+        ----------
+        vertices : list
+            List of 3D vertices defining the planar plate.
+
+        Returns
+        -------
+        ux : float
+            X component of the first in-plane basis unit vector.
+        uy : float
+            Y component of the first in-plane basis unit vector.
+        uz : float
+            Z component of the first in-plane basis unit vector.
+        vx : float
+            X component of the second in-plane basis unit vector.
+        vy : float
+            Y component of the second in-plane basis unit vector.
+        vz : float
+            Z component of the second in-plane basis unit vector.
+        """
+        v0, v1, v2 = vertices[:3]
+        nx = (v1[1] - v0[1]) * (v2[2] - v0[2]) - (v1[2] - v0[2]) * (v2[1] - v0[1])
+        ny = (v1[2] - v0[2]) * (v2[0] - v0[0]) - (v1[0] - v0[0]) * (v2[2] - v0[2])
+        nz = (v1[0] - v0[0]) * (v2[1] - v0[1]) - (v1[1] - v0[1]) * (v2[0] - v0[0])
+
+        n_norm = m.hypot(nx, ny, nz)
+        nx, ny, nz = nx / n_norm, ny / n_norm, nz / n_norm
+
+        arb_x, arb_y, arb_z = (
+            (0.0, 0.0, 1.0) if (abs(nx) > 0.5 or abs(ny) > 0.5) else (1.0, 0.0, 0.0)
+        )
+
+        ux = ny * arb_z - nz * arb_y
+        uy = nz * arb_x - nx * arb_z
+        uz = nx * arb_y - ny * arb_x
+        u_norm = m.hypot(ux, uy, uz)
+        if u_norm < 1e-12:
+            raise InvalidParameterError("Invalid plate orientation or geometry.")
+        ux, uy, uz = ux / u_norm, uy / u_norm, uz / u_norm
+
+        vx, vy, vz = ny * uz - nz * uy, nz * ux - nx * uz, nx * uy - ny * ux
+
+        return ux, uy, uz, vx, vy, vz
+
+    def calculate_soft_iron_distortion_matrix(
+        self, position_vector: Vector | list | tuple, frame: str = "ucs"
+    ) -> None:
+        """Calculates and stores the 3x3 soft-iron magnetic distortion matrix
+        induced by the plate at the position indicated by ``position_vector``.
+
+        Parameters
+        ----------
+        position_vector : Vector, list, tuple
+            Coordinates [x, y, z] in meters in the Body Axis Coordinate
+            System where the distortion matrix is evaluated.
+        """
+        if isinstance(self.points, list):
+            if self.points:
+                induced_matrix = Matrix.zeros()
+                diff_magnetic = self.relative_magnetic_permeability - 1.0
+                num_points = len(self.points)
+                dv = self.volume / num_points
+                dipole_scalar = (diff_magnetic * dv) / (4.0 * np.pi)
+                position_vector = self._position_vector_to_bacs(position_vector, frame)
+                for point in self.points:
+                    r_v = position_vector - Vector(point)
+                    r = abs(r_v)
+                    r_unit = r_v / r
+
+                    rx, ry, rz = r_unit[0], r_unit[1], r_unit[2]
+
+                    projection_tensor = Matrix(
+                        [
+                            [rx * rx, rx * ry, rx * rz],
+                            [ry * rx, ry * ry, ry * rz],
+                            [rz * rx, rz * ry, rz * rz],
+                        ]
+                    )
+
+                    dipole_kernel = (3.0 * projection_tensor - Matrix.identity()) / (
+                        r**3
+                    )
+
+                    induced_matrix = induced_matrix + (dipole_scalar * dipole_kernel)
+
+                self._magnetic_distortion_matrices[tuple(position_vector)] = (
+                    induced_matrix
+                )
+            else:
+                raise InvalidParameterError(
+                    "The plate points list is empty. Add the plate to a rocket before calculating the distortion matrix."
+                )
+        else:
+            raise InvalidParameterError("The points attribute must be a list.")
+
+    def _position_vector_to_bacs(
+        self,
+        position_vector: list | tuple | Vector,
+        frame: str = "bacs",
+    ) -> Vector:
+        """Transforms, if necessary, the position_vector to the BACS frame.
+
+        Parameters
+        ----------
+        position_vector : list, tuple, Vector
+            Coordinates [x, y, z] in meters in the specified ``frame``
+            in which we want to calculate the soft iron distortion.
+        frame : str, optional
+            Frame in which the ``position_vector`` is given. It can either be "bacs"
+            (body axis coordinate system) or "ucs" (user defined coordinate
+            system). Default is "ucs".
+
+        Returns
+        -------
+        position_vector_bacs : Vector
+            Vector coordinates [x, y, z] in meters in the BACS frame.
+        """
+        if not isinstance(frame, str):
+            raise InvalidParameterError("'frame' must be a string.")
+
+        frame_lower = frame.lower()
+        if frame_lower not in ("ucs", "bacs"):
+            raise InvalidParameterError(
+                f"Invalid frame '{frame}'. Must be 'ucs' or 'bacs'."
+            )
+        if isinstance(position_vector, (list, tuple, Vector)):
+            pos_v = Vector(position_vector)
+        else:
+            raise InvalidParameterError(
+                "'position_vector' must be a tuple, list, or Vector instance."
+            )
+        if frame_lower == "bacs":
+            position_vector_bacs = pos_v
+        else:
+            cdm_user_frame = Vector([0, 0, self.center_of_dry_mass_position])
+            delta = pos_v - cdm_user_frame
+            if self._csys == -1:  # nose to tail
+                position_vector_bacs = Vector([-delta[0], delta[1], -delta[2]])
+            else:  # tail to nose
+                position_vector_bacs = delta
+
+        return position_vector_bacs
+
+    def draw_3d(
+        self,
+        color: str = "teal",
+        marker: str = "h",
+        elev: float | int | None = None,
+        azim: float | int | None = None,
+        filename: str | None = None,
+    ) -> None:
+        """Plots the 3D scatter plot of the points forming the plate
+        that are used to model soft-iron magnetic distortion.
+
+        Parameters
+        ----------
+        color : str, optional
+            Color of the scatter points. A full list of color names can be found
+            at: https://matplotlib.org/stable/gallery/color/named_colors
+            Default is "teal".
+        marker : str, optional
+            Shape of the markers representing the points. A full
+            list of markers can be found at:
+            https://matplotlib.org/stable/api/markers_api.html
+            Default is "h".
+        elev : float, int, optional
+            The elevation angle in degrees rotates the camera above the plane
+            pierced by the vertical axis, with a positive angle corresponding
+            to a location above that plane. If None, the default view is used.
+            Default is None.
+        azim : float, int, optional
+            The azimuthal angle in degrees rotates the camera about the vertical
+            axis. If None, the default view is used. Default is None.
+        filename : str, optional
+            The path the plot should be saved to. If None, the plot will be shown instead
+            of saved. Supported file formats include: eps, jpg, jpeg, pdf, pgf, png, ps,
+            raw, rgba, svg, svgz, tif, tiff, and webp. Default is None.
+        """
+        self.plots.draw_3d(color, marker, elev, azim, filename)
+
+    def _rocket_belonging(self, rocket) -> None:
+        """Associates the rocket to which the Plate belongs to the
+        _PlatePlots instance.
+
+        Parameters
+        ----------
+        rocket : Rocket
+            Rocket instance to which the plate belongs.
+        """
+        self._csys = rocket._csys
+        self.center_of_dry_mass_position = rocket.center_of_dry_mass_position
+        self.plots.rocket = rocket
+
+    def info(self) -> None:
+        """Prints a summary of the information stored in the plate object."""
+        self.prints.all()
+
+    def all_info(self) -> None:
+        """Prints out all data and graphs available about the Plate."""
+        self.plots.all()
+        self.prints.all()
+
+    @classmethod
+    def from_dict(cls, data: dict) -> "Plate":
+        """Creates a Plate instance from a dictionary containing the initialization
+        parameters.
+
+        Parameters
+        ----------
+        data : dict
+            Dictionary containing plate constructor attributes.
+
+        Returns
+        -------
+        plate : Plate
+            Plate instance initialized with the specified parameters.
+        """
+        return cls(
+            shape=data["shape"],
+            dimensions=data["dimensions"],
+            material=data["material"],
+            thickness=data["thickness"],
+            absolute_magnetic_permeability=data.get(
+                "absolute_magnetic_permeability", None
+            ),
+            relative_magnetic_permeability=data.get(
+                "relative_magnetic_permeability", None
+            ),
+            grid_spacing=data.get("grid_spacing", 0.001),
+            z_points=data.get("z_points", 40),
+            angular_points=data.get("angular_points", 70),
+            name=data.get("name", "Plate"),
+        )
diff --git a/rocketpy/rocket/rocket.py b/rocketpy/rocket/rocket.py
index 68c2d102e..6c288f19d 100644
--- a/rocketpy/rocket/rocket.py
+++ b/rocketpy/rocket/rocket.py
@@ -17,6 +17,7 @@
 from rocketpy.mathutils.function import Function
 from rocketpy.mathutils.vector_matrix import Matrix, Vector
 from rocketpy.motors.empty_motor import EmptyMotor
+from rocketpy.motors.motor import Motor
 from rocketpy.plots.rocket_plots import _RocketPlots
 from rocketpy.prints.rocket_prints import _RocketPrints
 from rocketpy.rocket.aero_surface import (
@@ -36,6 +37,8 @@
 from rocketpy.rocket.aero_surface.generic_surface import GenericSurface
 from rocketpy.rocket.components import Components
 from rocketpy.rocket.parachute import Parachute
+from rocketpy.rocket.plate import Plate
+from rocketpy.rocket.wire import Wire
 from rocketpy.tools import (
     deprecated,
     find_obj_from_hash,
@@ -186,6 +189,11 @@ class Rocket:
         RailButtons object containing the rail buttons information.
     Rocket.motor : Motor
         Rocket's motor. See Motor class for more details.
+    Rocket.wires : Components
+        Collection of all the wires attached to the rocket.
+    Rocket.plates : list
+        Collection of all the plates attached to the rocket, stored as
+        lists of [plate, position, height].
     Rocket.motor_position : float
         Position, in meters, of the motor's coordinate system origin
         relative to the user defined rocket coordinate system.
@@ -359,6 +367,10 @@ def __init__(  # pylint: disable=too-many-statements
         self.radius = radius
         self.area = np.pi * self.radius**2
 
+        # Other attributes
+        self._radius_function = None
+        self._nose_tip_from_ucs = None
+
         # Eccentricity data initialization
         self.cm_eccentricity_x = 0
         self.cm_eccentricity_y = 0
@@ -371,6 +383,10 @@ def __init__(  # pylint: disable=too-many-statements
         self.parachutes = []
         self._controllers = []
         self.air_brakes = []
+        self._communication_wires = []
+        self._ignition_wires = []
+        self.wires = Components()
+        self.plates = []
         self.sensors = Components()
         self.aerodynamic_surfaces = Components()
         self.surfaces_cp_to_cdm = {}
@@ -1195,6 +1211,9 @@ def __add_single_surface(self, surface, position):
             self.rail_buttons.add(surface, position)
         else:
             self.aerodynamic_surfaces.add(surface, position)
+            if isinstance(surface, NoseCone):
+                self.nose_cone = surface
+                self._nose_tip_from_ucs = position[2]
         self.__evaluate_single_surface_cp_to_cdm(surface, position)
 
     def add_surfaces(self, surfaces, positions):
@@ -1375,6 +1394,7 @@ def add_nose(
             name=name,
         )
         self.add_surfaces(nose, position)
+
         return nose
 
     @deprecated(
@@ -1829,6 +1849,7 @@ def add_parachute(
             radius, drag_coefficient, height, porosity and name. Furthermore,
             it stores clean_pressure_signal, noise_signal and
             noisyPressureSignal which are filled in during Flight simulation.
+
         """
         parachute = Parachute(
             name,
@@ -1850,9 +1871,10 @@ def add_sensor(self, sensor, position):
 
         Parameters
         ----------
-        sensor : Sensor
+        sensor: Sensor
             Sensor to be added to the rocket.
-        position : int, float, tuple, list, Vector
+
+        position: int, float, tuple, list, Vector
             Position of the sensor. If a Vector, tuple or list is passed, it
             must be in the format (x, y, z) where x, y, and z are defined in the
             rocket's user defined coordinate system. If a single value is
@@ -1864,14 +1886,183 @@ def add_sensor(self, sensor, position):
         None
         """
         if isinstance(position, (float, int)):
-            position = (0, 0, position)
-        position = Vector(position)
-        self.sensors.add(sensor, position)
+            position_ucs = Vector([0, 0, position])
+        else:
+            position_ucs = Vector(position)
+        self.sensors.add(sensor, position_ucs)
         try:
             sensor._attached_rockets[self] += 1
         except KeyError:
             sensor._attached_rockets[self] = 1
 
+    def add_wire(
+        self,
+        wire: Wire,
+        position_endpoints: list | tuple,
+        parachute_name: str | None = None,
+    ) -> None:
+        """Adds a wire to the rocket. Wires generate magnetic disturbances that
+        affect magnetometer sensor readings during flight simulation.
+
+        Parameters
+        ----------
+        wire : Wire
+            Wire object to be added to the rocket.
+        position_endpoints : list, tuple
+            Sequence of two elements defining Endpoint A and Endpoint B:
+
+            - If numeric scalars: [z_a, z_b] coordinates along the centerline
+              in the User-defined Coordinate System.
+            - If 3D vectors: [[x_a, y_a, z_a], [x_b, y_b, z_b]] coordinates in
+              the User-defined Coordinate System.
+
+            Conventional current flows from Endpoint A to Endpoint B.
+        parachute_name : str, optional
+            Name of the parachute during whose deployment current flows.
+            Mandatory when the wire is an ignition wire with function
+            "parachute_deployment". Default is None.
+        """
+        if not isinstance(wire, Wire):
+            raise InvalidParameterError("The wire parameter must be a Wire instance.")
+
+        endpoints = self._define_3d_endpoints(position_endpoints)
+
+        if wire.ignition_wire_function == "parachute_deployment":
+            if not isinstance(parachute_name, str):
+                raise InvalidParameterError(
+                    "parachute_name must be a string when the wire function is 'parachute_deployment'."
+                )
+            wire.parachute_name = parachute_name
+        else:
+            wire.parachute_name = None
+
+        for endpoint, name in zip(endpoints, ("Endpoint A", "Endpoint B")):
+            x, y, z = endpoint
+            flag, range_z = self.z_bounds_check(z, frame="ucs")
+            if not flag:
+                raise InvalidParameterError(
+                    f"{name} z-coordinate {z} is outside the rocket longitudinal range {range_z}."
+                )
+
+            r_endpoint = math.hypot(x, y)
+            r_rocket = self.general_radius(z, frame="ucs")
+            if r_endpoint > r_rocket:
+                raise InvalidParameterError(
+                    f"{name} with coordinates {endpoint} is outside the rocket radius ({r_endpoint:.4f} m > {r_rocket:.4f} m) at z = {z} m."
+                )
+        wire._rocket_belonging(self)
+        wire._set_wire_endpoints_to_bacs(self, endpoints)
+
+        if wire.wire_type == "communications":
+            self._communication_wires.append(wire)
+        elif wire.wire_type == "ignition":
+            self._ignition_wires.append(wire)
+        self.wires.add(wire, position_endpoints)
+
+    def _define_3d_endpoints(self, position_endpoints: list | tuple) -> list[Vector]:
+        """Creates the 3D position vectors of the wire endpoints from the user inputs.
+
+        Parameters
+        ----------
+        position_endpoints : list, tuple
+            Sequence of two numbers (z-coordinates) or two 3D position vectors
+            ([x, y, z]) relative to the User-defined Coordinate System.
+            Conventional current flows from Endpoint A to Endpoint B.
+
+        Returns
+        -------
+        list of Vector
+            List containing the 3D Vector components of each endpoint [endpoint_a, endpoint_b].
+        """
+        if isinstance(position_endpoints, (list, tuple)):
+            if len(position_endpoints) == 2:
+                if all(isinstance(val, (int, float)) for val in position_endpoints):
+                    endpoint_a = Vector([0, 0, float(position_endpoints[0])])
+                    endpoint_b = Vector([0, 0, float(position_endpoints[1])])
+                    return [endpoint_a, endpoint_b]
+
+                elif all(
+                    isinstance(item, (list, tuple, Vector))
+                    for item in position_endpoints
+                ):
+                    if any(len(item) != 3 for item in position_endpoints):
+                        raise InvalidParameterError(
+                            "The coordinate length for each endpoint must be 3."
+                        )
+
+                    endpoint_a = (
+                        position_endpoints[0]
+                        if isinstance(position_endpoints[0], Vector)
+                        else Vector(position_endpoints[0])
+                    )
+                    endpoint_b = (
+                        position_endpoints[1]
+                        if isinstance(position_endpoints[1], Vector)
+                        else Vector(position_endpoints[1])
+                    )
+
+                    return [endpoint_a, endpoint_b]
+                else:
+                    raise InvalidParameterError(
+                        "position_endpoints must be a sequence of numbers or 3D coordinate vectors."
+                    )
+            else:
+                raise InvalidParameterError(
+                    "position_endpoints must contain exactly 2 endpoint positions."
+                )
+        else:
+            raise InvalidParameterError(
+                "position_endpoints must be a list or tuple of two numbers (z-coordinates) or two 3D position vectors ([x, y, z])."
+            )
+
+    def add_plate(
+        self,
+        plate: Plate,
+        position: float | int | None = None,
+        height: float | int | None = None,
+    ) -> None:
+        """Adds a Plate object to the rocket. Plates are used to measure
+        soft-iron magnetic distortion, that affects magnetometer sensor
+        readings during flight simulation.
+
+        Parameters
+        ----------
+        plate : Plate
+            The Plate instance to be attached to the rocket.
+        position : float, int, optional
+            Angle between the User-defined Coordinate System y-axis and the
+            geometric center of the plate in degrees. The angle is positive from
+            y to -x. See `Rocket Axes Definition <https://docs.rocketpy.org/en/latest/user/rocket/rocket_axes.html>`_
+            for more information.
+        height : float, int, optional
+            Axial coordinate of the geometric center along the rocket
+            longitudinal axis in the User-defined Coordinate System in
+            meters. Required when the ``shape`` of the plate is "circular" or
+            "rectangular".
+        """
+        if not isinstance(plate, Plate):
+            raise InvalidParameterError("The plate parameter must be a Plate instance.")
+
+        if plate.shape in ("circular", "rectangular"):
+            if position is None:
+                raise InvalidParameterError(
+                    f"position must be defined when the shape is '{plate.shape}'."
+                )
+            if not isinstance(position, (float, int)):
+                raise InvalidParameterError("position must be a float or int.")
+            if height is None:
+                raise InvalidParameterError(
+                    f"height must be defined when the shape is '{plate.shape}'."
+                )
+            flag, range_z = self.z_bounds_check(height, frame="ucs")
+            if not flag:
+                raise InvalidParameterError(
+                    f"The defined height {height} m must be within the rocket longitudinal range {range_z} in the user frame."
+                )
+        plate._rocket_belonging(self)
+        plate.define_plate_position(self, position, height)
+        self.plates.append([plate, position, height])
+
     def add_air_brakes(
         self,
         drag_coefficient_curve,
@@ -2207,8 +2398,8 @@ def draw(self, vis_args=None, plane="xz", *, filename=None):
             A full list of color names can be found at:
             https://matplotlib.org/stable/gallery/color/named_colors
         plane : str, optional
-            Plane in which the rocket will be drawn. Default is 'xz'. Other
-            options is 'yz'. Used only for sensors representation.
+            Plane in which the rocket will be drawn. Default is "xz". Other
+            options is "yz". Used only for sensors representation.
         filename : str | None, optional
             The path the plot should be saved to. By default None, in which case
             the plot will be shown instead of saved. Supported file endings are:
@@ -2217,6 +2408,183 @@ def draw(self, vis_args=None, plane="xz", *, filename=None):
         """
         self.plots.draw(vis_args, plane, filename=filename)
 
+    def general_radius(self, z: float, frame: str = "bacs") -> float:
+        """Returns the radius of the rocket, including the
+        nose cone and the radius variations in the body, as a function of
+        the distance along the z axis from the body axes coordinate system
+        or the user defined coordinate system.
+
+        It assumes that the bottom radius of the nose cone is constant until
+        some tail, if defined, is present. Then, the radius of the body will be
+        the top radius of the following tail, or if it is the last tail, the
+        radius will be the radius of the bottom of the tail.
+
+        Parameters
+        ----------
+        z : float, int
+            Position along the z axis relative to the bacs
+            in which we want to calculate the radius.
+        frame : str, optional
+            Frame in which the z component is given. It can either be "bacs"
+            (body axis coordinate sytem) or "ucs" (user defined coordiante
+            system).
+
+        Returns
+        -------
+        r: float
+            Radius for the z value in the whole rocket.
+        """
+        if not isinstance(z, (float, int)):
+            raise InvalidParameterError("Z must be a float or int")
+        if not isinstance(self.nose_cone, NoseCone):
+            raise InvalidParameterError("Define a nose cone first")
+        if not isinstance(frame, str):
+            raise InvalidParameterError("frame parameter must be a string")
+        else:
+            if isinstance(frame, str):
+                if frame.lower() == "ucs":
+                    distance_from_nose = (
+                        self._nose_tip_from_ucs - z
+                    ) * self._csys  # nose cone frame
+                    z_bacs = (z - self.center_of_dry_mass_position) * self._csys
+                elif frame.lower() == "bacs":
+                    nose_tip_bacs = (
+                        self._nose_tip_from_ucs - self.center_of_dry_mass_position
+                    ) * self._csys
+                    distance_from_nose = nose_tip_bacs - z  # nose cone frame
+                    z_bacs = z
+                else:
+                    raise InvalidParameterError(
+                        "Accepted strings for frame are ucs and bacs"
+                    )
+            if 0 <= distance_from_nose <= self.nose_cone.length:
+                r = self.nose_cone.radius(distance_from_nose)
+            else:
+                r = self._calculate_radius_z_intermediate(z_bacs)
+            return r
+
+    def _calculate_radius_z_intermediate(self, z: float) -> float:
+        """This is an auxiliary function returning the radius of the rocket,
+        below the nose cone as a function of the distance along the z
+        axis from the body axes coordinate system.
+
+        Parameters
+        ----------
+        z: float, int
+            Position along the z axis in the body axis coordinate
+            system for which the radius will be returned.
+
+        Returns
+        -------
+        r: float, int
+            Radius for the z value
+        """
+        tails_bacs = []
+        for tail, tail_from_ucs in self.aerodynamic_surfaces.get_position_by_type(Tail):
+            tail_bacs = (
+                tail_from_ucs[2] - self.center_of_dry_mass_position
+            ) * self._csys
+            tails_bacs.append((tail, tail_bacs))
+            distance_from_tail_tip = tail_bacs - z
+            if 0 <= distance_from_tail_tip <= tail.length:
+                r = tail.radius(distance_from_tail_tip)
+                return r
+
+        r = self._calculate_radius_z_tubes(z, tails_bacs)
+        return r
+
+    def _calculate_radius_z_tubes(self, z: float, tails_bacs: list) -> float:
+        """This is an auxiliary function returning the radius of the rocket,
+        when it is not in the nose cone or tails as a function of the
+        distance along the z axis from the body axes coordinate system.
+
+        Parameters
+        ----------
+        z: float, int
+            Position along the z axis in the body axis coordinate
+            system for which the radius will be returned.
+        tails_bacs: list
+            List composed of tuples with the tails of the rocket,
+            and the position in the bacs frame
+
+        Returns
+        -------
+        r: float, int
+            Radius for the z value in the body tubes.
+        """
+        if tails_bacs != []:
+            o_tails_bacs = sorted(tails_bacs, key=lambda x: x[1], reverse=True)
+            for tail, tail_bacs_position in o_tails_bacs:
+                if z > tail_bacs_position:
+                    return tail.top_radius
+
+            last_tail = o_tails_bacs[-1][0]
+            r = last_tail.bottom_radius
+        else:
+            r = self.radius
+        return r
+
+    def z_bounds_check(
+        self, z: float, frame: str = "bacs"
+    ) -> tuple[bool, tuple[float, float]]:
+        """This function is used to check if a given z is inside or outside
+        the defined rocket.
+
+        Parameters
+        ----------
+        z: float, int
+            Position along the z axis for which it will be checked
+            whether it is inside or outside the rocket.
+        frame: str, optional
+            The coordinate system of the input z and the returned bounds.
+            "bacs" for Body Axes Coordinate System (default), or "ucs" for
+            User Coordinate System.
+
+        Returns
+        -------
+        is_inside: bool
+            False if it is outside, True if it is inside.
+        bounds: tuple
+            Tuple formed by the range of the z relative to the specified frame.
+        """
+        if isinstance(z, (float, int)):
+            if not isinstance(self.nose_cone, NoseCone):
+                raise InvalidParameterError("Define a nose cone first")
+            if not isinstance(self.motor, Motor):
+                raise InvalidParameterError("Define a motor first")
+
+            # bounds in the ucs frame
+            nose_tip_ucs = self._nose_tip_from_ucs
+            motor_ucs = self.motor_position
+            if isinstance(frame, str):
+                if frame.lower() == "ucs":
+                    z_min = min(nose_tip_ucs, motor_ucs)
+                    z_max = max(nose_tip_ucs, motor_ucs)
+
+                elif frame.lower() == "bacs":
+                    # change from ucs to bacs
+                    nose_tip_bacs = (
+                        nose_tip_ucs - self.center_of_dry_mass_position
+                    ) * self._csys
+                    motor_bacs = (
+                        motor_ucs - self.center_of_dry_mass_position
+                    ) * self._csys
+
+                    z_min = min(nose_tip_bacs, motor_bacs)
+                    z_max = max(nose_tip_bacs, motor_bacs)
+                else:
+                    raise InvalidParameterError(
+                        "Accepted strings for frame are ucs and bacs"
+                    )
+            else:
+                raise InvalidParameterError("Frame parameter must be a string")
+
+            is_inside = z_min <= z <= z_max
+            return is_inside, (z_min, z_max)
+
+        else:
+            raise InvalidParameterError("The z component must be a float or int")
+
     def info(self):
         """Prints out a summary of the data and graphs available about
         the Rocket.
@@ -2265,6 +2633,8 @@ def to_dict(self, **kwargs):
             "air_brakes": self.air_brakes,
             "_controllers": self._controllers,
             "sensors": self.sensors,
+            "wires": self.wires,
+            "plates": self.plates,
         }
 
         if kwargs.get("include_outputs", False):
@@ -2406,6 +2776,12 @@ def from_dict(cls, data):
                         )
             rocket._add_controllers(controller)
 
+        for wire, position_endpoints in data.get("wires", []):
+            rocket.add_wire(wire, position_endpoints)
+
+        for plate, position, height in data.get("plate", []):
+            rocket.add_plate(plate, position, height)
+
         return rocket
 
     def __process_drag_input(self, input_data, coeff_name):
diff --git a/rocketpy/rocket/wire.py b/rocketpy/rocket/wire.py
new file mode 100644
index 000000000..6a948881e
--- /dev/null
+++ b/rocketpy/rocket/wire.py
@@ -0,0 +1,367 @@
+import math as m
+import warnings
+
+from rocketpy.exceptions import InvalidParameterError
+from rocketpy.mathutils.vector_matrix import Vector
+from rocketpy.plots.wire_plots import _WirePlots
+from rocketpy.prints.wire_prints import _WirePrints
+
+
+class Wire:
+    """Models the physical characteristics and magnetic field generated by an
+    electric wire.
+
+    Calculates the magnetic field generated by a straight, current-carrying
+    wire segment at arbitrary spatial points using the Biot-Savart law. Supports
+    continuous communication wires and event-based ignition wires (e.g., motor
+    ignition, parachute deployment).
+
+    Attributes
+    ----------
+    Wire.current : float, int
+        Intensity of the electric current flowing through the wire in Amperes (A).
+    Wire.magnetic_field : dict
+        Dictionary of calculated magnetic fields. Keys are position coordinate
+        tuples (x, y, z) in the Body Axis Coordinate System, and values
+        are the corresponding magnetic field components in Tesla (T).
+    Wire.wire_length : float
+        Total length of the wire segment in meters.
+    Wire.wire_type : str
+        Type of wire ("communications" or "ignition").
+    Wire.ignition_wire_function : str or None
+        Function sub-type when ``wire_type`` is "ignition" ("motor_ignition" or
+        "parachute_deployment").
+    Wire.extra_ignition_time : float
+        Additional duration in seconds for which the ignition current remains
+        active after the event trigger.
+    Wire.name : str
+        Name identifier of the wire.
+    """
+
+    def __init__(
+        self,
+        current: float | int,
+        wire_type: str,
+        ignition_wire_function: str | None = None,
+        extra_ignition_time: float = 0.0,
+        name: str = "wire",
+    ) -> None:
+        """Initializes the Wire class.
+
+        Parameters
+        ----------
+        current : float, int
+            Intensity of the current flowing through the wire in Amperes (A).
+            Conventional current flows from the first endpoint to the second
+            endpoint defined in the rocket attachment.
+        wire_type : str
+            Type of wire:
+
+            - "communications": Continuous current, represents continuous data
+              or power transmission, generating a steady magnetic field.
+            - "ignition": Current is active only during specific deployment or
+              ignition events.
+        ignition_wire_function : str, optional
+            Function of the ignition wire (mandatory if ``wire_type`` is
+            "ignition"). Valid options are "motor_ignition" or
+            "parachute_deployment". Default is None.
+        extra_ignition_time : float, optional
+            Additional duration in seconds the ignition current persists
+            after event actuation. Default is 0.
+        name : str, optional
+            Name of the wire. Default is "wire".
+        """
+        self._validate_parameters(
+            current, extra_ignition_time, wire_type, ignition_wire_function
+        )
+        self._magnetic_field = {}
+        self.magnetic_field = {}
+        self._wire_endpoints_bacs = []
+        self.wire_length = 0.0
+        self.parachute_name = None
+        self.name = name
+        self._csys = None
+        self.center_of_dry_mass_position = None
+
+        # prints and plots
+        self.prints = _WirePrints(self)
+        self.plots = _WirePlots(self)
+
+    def _validate_parameters(
+        self, current, extra_ignition_time, wire_type, ignition_wire_function
+    ) -> None:
+        """Validates input parameters and initializes corresponding attributes."""
+        self._validate_wire_type(wire_type, ignition_wire_function)
+        self._validate_numbers(current, extra_ignition_time)
+
+    def _validate_wire_type(self, wire_type, ignition_wire_function) -> None:
+        """Validates wire categorization and functional role."""
+        if isinstance(wire_type, str):
+            if wire_type == "communications":
+                self.wire_type = "communications"
+                self.ignition_wire_function = None
+            elif wire_type == "ignition":
+                self.wire_type = "ignition"
+                if ignition_wire_function is None:
+                    raise InvalidParameterError(
+                        "The 'ignition_wire_function' parameter is required when 'wire_type' is 'ignition'."
+                    )
+                if not isinstance(ignition_wire_function, str):
+                    raise InvalidParameterError(
+                        "'ignition_wire_function' must be a string."
+                    )
+                self.ignition_wire_function = ignition_wire_function
+            else:
+                raise InvalidParameterError(
+                    "'wire_type' must be either 'communications' or 'ignition'."
+                )
+        else:
+            raise InvalidParameterError("'wire_type' must be a string.")
+
+    def _validate_numbers(self, current, extra_ignition_time) -> None:
+        """Validates numerical attributes defining wire physical characteristics."""
+        if not isinstance(current, (float, int)):
+            raise InvalidParameterError("Current must be a float or int.")
+        self.current = float(current)
+
+        if not isinstance(extra_ignition_time, (float, int)):
+            raise InvalidParameterError("'extra_ignition_time' must be a float or int.")
+        if extra_ignition_time < 0:
+            raise InvalidParameterError(
+                "'extra_ignition_time' must be greater than or equal to 0."
+            )
+        self.extra_ignition_time = float(extra_ignition_time)
+
+    def measure_magnetic_field(
+        self, position_vector: list | tuple | Vector, frame: str = "ucs"
+    ) -> None:
+        """Calculates and stores the magnetic field vector at the point given by
+        ``position_vector`` in the Body Axis Coordinate System using the finite
+        straight-wire Biot-Savart formula.
+
+        Parameters
+        ----------
+        position_vector : list, tuple, Vector
+            Coordinates [x, y, z] in meters in the specified ``frame``
+            in which we want to calculate the magnetic field.
+        frame : str, optional
+            Frame in which the ``position_vector`` is given. It can either be "bacs"
+            (body axis coordinate sytem) or "ucs" (user defined coordiante
+            system).
+        """
+        r1 = self._wire_endpoints_bacs[0]  # starting endpoint
+        r2 = self._wire_endpoints_bacs[1]  # final end
+        l = r2 - r1  # Vector along the wire pointing in direction of current
+        self.wire_length = abs(l)
+
+        r_v = self._position_vector_to_bacs(position_vector, frame)
+        r_t = tuple(r_v)
+
+        if self.wire_length < 1e-12:
+            self.magnetic_field[r_t] = [0.0, 0.0, 0.0]
+            self._magnetic_field[r_t] = Vector([0.0, 0.0, 0.0])
+            return
+
+        r1_v = r_v - r1
+        r2_v = r_v - r2
+
+        cross_l_r1 = l ^ r1_v
+        cross_norm = abs(cross_l_r1)
+
+        if cross_norm < 1e-12:
+            b_v = Vector([0, 0, 0])
+            warnings.warn(
+                "'position vector' is collinear with the wire segment; magnetic field is zero.",
+                UserWarning,
+            )
+        else:
+            l_unit = l / self.wire_length
+            cos_theta1 = l_unit @ r1_v.unit_vector
+            cos_theta2 = l_unit @ r2_v.unit_vector
+
+            b_v = (
+                (1e-7 * self.current)
+                * (cross_l_r1 / (cross_norm**2))
+                * (cos_theta1 - cos_theta2)
+                * self.wire_length
+            )
+
+        self.magnetic_field[r_t] = list(b_v)
+        self._magnetic_field[r_t] = b_v
+
+    def _position_vector_to_bacs(
+        self,
+        position_vector: list | tuple | Vector,
+        frame: str = "bacs",
+    ) -> Vector:
+        """Transforms, if necessary, the position_vector to the BACS frame.
+
+        Parameters
+        ----------
+        position_vector : list, tuple, Vector
+            Coordinates [x, y, z] in meters in the specified ``frame``
+            in which we want to calculate the magnetic field.
+        frame : str, optional
+            Frame in which the ``position_vector`` is given. It can either be "bacs"
+            (body axis coordinate system) or "ucs" (user defined coordinate
+            system). Default is "ucs".
+
+        Returns
+        -------
+        position_vector_bacs : Vector
+            Vector coordinates [x, y, z] in meters in the BACS frame.
+        """
+        if not isinstance(frame, str):
+            raise InvalidParameterError("'frame' must be a string.")
+
+        frame_lower = frame.lower()
+        if frame_lower not in ("ucs", "bacs"):
+            raise InvalidParameterError(
+                f"Invalid frame '{frame}'. Must be 'ucs' or 'bacs'."
+            )
+        if isinstance(position_vector, (list, tuple, Vector)):
+            pos_v = Vector(position_vector)
+        else:
+            raise InvalidParameterError(
+                "'position_vector' must be a tuple, list, or Vector instance."
+            )
+        if frame_lower == "bacs":
+            position_vector_bacs = pos_v
+        else:
+            cdm_user_frame = Vector([0, 0, self.center_of_dry_mass_position])
+            delta = pos_v - cdm_user_frame
+            if self._csys == -1:  # nose to tail
+                position_vector_bacs = Vector([-delta[0], delta[1], -delta[2]])
+            else:  # tail to nose
+                position_vector_bacs = delta
+
+        return position_vector_bacs
+
+    def define_magnetic_field(
+        self,
+        position_vector: list | tuple | Vector,
+        magnetic_field: float | int | list | tuple | Vector,
+    ) -> None:
+        """Manually sets the magnetic field vector produced by the wire at a
+        specified position coordinate.
+
+        Parameters
+        ----------
+        position_vector : list, tuple, Vector
+            Target position coordinates [x, y, z] in meters defined in the
+            Body Axis Coordinate System.
+        magnetic_field : float, int, list, tuple, Vector
+            Magnetic field vector in Tesla (T):
+
+            - If a scalar (float or int), the same field value is assigned
+              isotropically across all three axes: [B, B, B].
+            - If a 3-element list, tuple, or Vector, sets the directional
+              field components [Bx, By, Bz].
+        """
+        position_vector_t = tuple(position_vector)
+        if isinstance(magnetic_field, (float, int)):
+            magnetic_field = [magnetic_field, magnetic_field, magnetic_field]
+        self._magnetic_field[position_vector_t] = Vector(magnetic_field)
+        self.magnetic_field[position_vector_t] = list(magnetic_field)
+
+    def _set_wire_endpoints_to_bacs(
+        self,
+        rocket,
+        _wire_endpoints_from_user_coordinate_system: list[Vector]
+        | tuple[Vector, Vector],
+    ) -> None:
+        """Transforms wire endpoint coordinates from the User-defined Coordinate
+        System to the Body Axis Coordinate System and stores them.
+
+        Parameters
+        ----------
+        rocket : Rocket
+            Rocket instance to which the wire is attached.
+        _wire_endpoints_from_user_coordinate_system : list[Vector] or tuple[Vector, Vector]
+            Sequence containing the two endpoint position vectors in the
+            User-defined Coordinate System.
+        """
+        self._wire_endpoints_bacs = []
+        cdm_user_frame = Vector([0, 0, self.center_of_dry_mass_position])
+        for endpoint_from_user in _wire_endpoints_from_user_coordinate_system:
+            self._check_entry_dimensions(endpoint_from_user, rocket)
+            endpoint_from_cdm_user_frame = endpoint_from_user - cdm_user_frame
+            if self._csys == -1:  # nose to tail
+                endpoint_position_bacs_frame = Vector(
+                    [
+                        -endpoint_from_cdm_user_frame[0],
+                        endpoint_from_cdm_user_frame[1],
+                        -endpoint_from_cdm_user_frame[2],
+                    ]
+                )
+            else:  # tail to nose
+                endpoint_position_bacs_frame = endpoint_from_cdm_user_frame
+            self._wire_endpoints_bacs.append(endpoint_position_bacs_frame)
+
+    def _check_entry_dimensions(self, pt, rocket) -> None:
+        """Verifies that an endpoint coordinates lie within the physical rocket.
+
+        Parameters
+        ----------
+        pt : list, tuple, Vector
+            Endpoint coordinates [x, y, z] in the User-defined Coordinate System.
+        rocket : Rocket
+            Rocket instance in which geometry bounds are verified.
+        """
+        if not rocket.z_bounds_check(pt[2], frame="ucs")[0]:
+            raise InvalidParameterError(
+                f"The axial coordinate z = {pt[2]} m of endpoint {pt} is outside the rocket longitudinal bounds."
+            )
+
+        if m.hypot(pt[0], pt[1]) > rocket.general_radius(pt[2], frame="ucs"):
+            raise InvalidParameterError(
+                f"Endpoint {pt} exceeds the rocket fuselage radius at z = {pt[2]} m."
+            )
+
+    def _rocket_belonging(self, rocket) -> None:
+        """Associates the rocket to which the Wire belongs to the
+        _WirePlots instance and defines the center of dry mass
+        and the z orientation as a wire attributes.
+
+        Parameters
+        ----------
+        rocket : Rocket
+            Rocket instance to which the wire belongs.
+        """
+        self._csys = rocket._csys
+        self.center_of_dry_mass_position = rocket.center_of_dry_mass_position
+        self.plots.rocket = rocket
+
+    def info(self) -> None:
+        """Print a summary of the information stored in the wire object."""
+        self.prints.all()
+
+    def all_info(self) -> None:
+        """Prints all data and graphs available about the Wire."""
+        self.plots.all()
+        self.prints.all()
+
+    @classmethod
+    def from_dict(cls, data: dict) -> "Wire":
+        """Creates a Wire instance from a dictionary containing the initialization
+        parameters.
+
+        Parameters
+        ----------
+        data : dict
+            Dictionary containing wire constructor attributes.
+
+        Returns
+        -------
+        wire : Wire
+            Wire instance initialized with the specified parameters.
+        """
+        return cls(
+            # Mandatory Parameters
+            current=data["current"],
+            wire_type=data["wire_type"],
+            # Optional Parameters
+            ignition_wire_function=data.get("ignition_wire_function", None),
+            extra_ignition_time=data.get("extra_ignition_time", 0.0),
+            name=data.get("name", "wire"),
+        )
diff --git a/rocketpy/sensors/__init__.py b/rocketpy/sensors/__init__.py
index eb2e20730..0e2a8f1e2 100644
--- a/rocketpy/sensors/__init__.py
+++ b/rocketpy/sensors/__init__.py
@@ -2,4 +2,5 @@
 from .barometer import Barometer
 from .gnss_receiver import GnssReceiver
 from .gyroscope import Gyroscope
+from .magnetometer import Magnetometer
 from .sensor import InertialSensor, ScalarSensor, Sensor
diff --git a/rocketpy/sensors/accelerometer.py b/rocketpy/sensors/accelerometer.py
index 42d6d04d3..c043e3ae0 100644
--- a/rocketpy/sensors/accelerometer.py
+++ b/rocketpy/sensors/accelerometer.py
@@ -241,26 +241,22 @@ def measure(self, time, **kwargs):
         omega = Vector(u[10:13])
         omega_dot = Vector(u_dot[10:13])
 
-        # Measured acceleration at sensor position in inertial frame
-        A = (
-            inertial_acceleration
+        inertial_to_body = Matrix.transformation(u[6:10]).transpose
+        body_acceleration = inertial_to_body @ inertial_acceleration
+
+        a_body = (
+            body_acceleration
             + Vector.cross(omega_dot, r)
             + Vector.cross(omega, Vector.cross(omega, r))
         )
-        # Transform to sensor frame
-        inertial_to_sensor = (
-            self._total_rotation_sensor_to_body
-            @ Matrix.transformation(u[6:10]).transpose
-        )
-        A = inertial_to_sensor @ A
-
+        a_sensor = self._total_rotation_sensor_to_body.transpose @ a_body
         # Apply noise + bias and quantize
-        A = self.apply_noise(A)
-        A = self.apply_temperature_drift(A)
-        A = self.quantize(A)
+        a_sensor = self.apply_noise(a_sensor)
+        a_sensor = self.apply_temperature_drift(a_sensor)
+        a_sensor = self.quantize(a_sensor)
 
-        self.measurement = tuple([*A])
-        self._save_data((time, *A))
+        self.measurement = tuple([*a_sensor])
+        self._save_data((time, *a_sensor))
 
     def export_measured_data(self, filename, file_format="csv"):
         """Export the measured values to a file
diff --git a/rocketpy/sensors/barometer.py b/rocketpy/sensors/barometer.py
index 3320cdc57..2654dfc13 100644
--- a/rocketpy/sensors/barometer.py
+++ b/rocketpy/sensors/barometer.py
@@ -156,7 +156,7 @@ def measure(self, time, **kwargs):
                 State vector of the rocket.
             - u_dot : np.array
                 Derivative of the state vector of the rocket.
-            - relative_position : np.array
+            - relative_position : Vector
                 Position of the sensor relative to the rocket center of mass.
             - environment : Environment
                 Environment object containing the atmospheric conditions.
@@ -166,6 +166,7 @@ def measure(self, time, **kwargs):
         pressure = kwargs["environment"].pressure
 
         # Calculate the altitude of the sensor
+
         relative_altitude = (Matrix.transformation(u[6:10]) @ relative_position).z
 
         # Calculate the pressure at the sensor location and add noise
diff --git a/rocketpy/sensors/magnetometer.py b/rocketpy/sensors/magnetometer.py
new file mode 100644
index 000000000..9b21d3331
--- /dev/null
+++ b/rocketpy/sensors/magnetometer.py
@@ -0,0 +1,946 @@
+import math
+from datetime import datetime
+
+import numpy as np
+from pywmm import WMMv2
+from pywmm.calculator import calculate_geomagnetic
+from pywmm.date_utils import decimal_year
+
+from rocketpy.exceptions import InvalidParameterError
+from rocketpy.mathutils.vector_matrix import Matrix, Vector
+from rocketpy.prints.sensors_prints import _InertialSensorPrints
+from rocketpy.rocket import Rocket
+from rocketpy.sensors.sensor import InertialSensor
+from rocketpy.tools import inverted_haversine
+
+
+class Magnetometer(InertialSensor):
+    """Class for simulating a magnetometer sensor during rocket flight.
+
+    Inherits from the InertialSensor subclass. Models Earth's geomagnetic
+    field using the World Magnetic Model (WMM) and simulates physical sensor
+    distortions, including hard iron, soft iron (via plates), power wire
+    interferences (via communication & ignition wires), thermal drifts, noise, and
+    quantization.
+
+    Attributes
+    ----------
+    sampling_rate : float
+        Sampling rate of the sensor in Hz.
+    orientation : tuple, list
+        Orientation of the sensor in the rocket.
+    magnetic_interference : list
+        Magnetic interference on the magnetometer in Tesla (T), formed by the sum of
+        hard iron distortion, power interference, and soft iron distortion difference.
+    hard_iron_distortion : list
+        Hard iron distortion in Tesla (T).
+    _soft_iron_distortion_matrix : Matrix
+        Soft iron distortion matrix applied to the magnetic reading (dimensionless).
+    soft_iron_distortion_difference : list
+        Difference between the vector after application of soft iron distortion
+        and before in Tesla (T).
+    power_interference : list
+        Total magnetic distortion due to system interference in Tesla (T).
+    communications_interference : list
+        Magnetic distortion due to communication wires in Tesla (T).
+    activation_signal_interference : list
+        Magnetic distortion due to ignition/activation signals in Tesla (T).
+    measurement_range : float or tuple
+        The measurement range of the sensor in Tesla (T).
+    resolution : float
+        The resolution of the sensor in T/LSB.
+    noise_density : float, list
+        The noise density of the sensor in T/√Hz.
+    noise_variance : float, list
+        The variance of the noise of the sensor in T^2.
+    random_walk_density : float, list
+        The random walk density of the sensor in T/√Hz.
+    random_walk_variance : float, list
+        The variance of the random walk of the sensor in T^2.
+    constant_bias : float, list
+        The constant bias of the sensor in Tesla (T).
+    operating_temperature : float
+        The operating temperature of the sensor in Kelvin (K).
+    temperature_bias : float, list
+        The temperature bias of the sensor in T/K.
+    temperature_scale_factor : float, list
+        The temperature scale factor of the sensor in %/K.
+    cross_axis_sensitivity : float
+        The cross axis sensitivity of the sensor in percentage (%).
+    name : str
+        The name of the sensor.
+    _random_walk_drift : Vector
+        The random walk drift of the sensor in Tesla (T).
+    measurement : tuple
+        The measurement of the sensor after quantization, noise, temperature
+        drift, and magnetic interference in Tesla (T).
+    measured_data : list
+        The stored measured data of the sensor after quantization, noise, and
+        temperature drift.
+    wmm : WMMv2
+        WMMv2 object from the pywmm library. Details on its GitHub repository:
+        https://github.com/dougc95/pywmm/tree/main
+    year : float
+        Current decimal year.
+    rotation_sensor_to_body : Matrix
+        The rotation matrix of the sensor from the sensor frame to the rocket
+        frame of reference.
+    normal_vector : Vector
+        The normal vector of the sensor in the rocket frame of reference.
+    """
+
+    units = "T"
+
+    def __init__(  # pylint: disable=too-many-arguments
+        self,
+        sampling_rate,
+        orientation=(0, 0, 0),
+        measurement_range=np.inf,
+        resolution=0,
+        hard_iron_distortion=0,
+        soft_iron_distortion=Matrix.identity(),
+        power_interference=0,
+        activation_signal_interference=None,
+        communications_interference=None,
+        noise_density=0,
+        noise_variance=1,
+        random_walk_density=0,
+        random_walk_variance=1,
+        constant_bias=0,
+        operating_temperature=298,
+        temperature_bias=0,
+        temperature_scale_factor=0,
+        cross_axis_sensitivity=0,
+        name="Magnetometer",
+        seed=None,
+    ) -> None:
+        """Initializes the Magnetometer sensor:
+
+        Parameters
+        ----------
+        sampling_rate : float
+            Sampling rate of the sensor in Hz.
+        orientation : tuple, list, optional
+            Orientation of the sensor in the rocket. The orientation can be
+            given as either:
+
+            - A list of length 3, where the elements are the Euler angles for
+              the rotation yaw (ψ), pitch (θ), and roll (φ) in radians. The
+              standard rotation sequence z-y-x (3-2-1) is used, meaning the
+              sensor is first rotated by ψ around the z axis, then by θ around
+              the new y axis, and finally by φ around the new x axis.
+            - A list of lists (matrix) of shape 3x3, representing the rotation
+              matrix from the sensor frame to the rocket frame. The sensor frame
+              of reference is defined as having the z axis along the sensor's normal
+              vector pointing upwards, with x and y axes perpendicular to the z axis
+              and to each other.
+
+            The rocket frame of reference is defined as having the z axis
+            along the rocket's axis of symmetry pointing upwards, with x and y axes
+            perpendicular to the z axis and to each other. A rotation around the x
+            axis configures a pitch, around the y axis a yaw, and around the z axis a
+            roll. Default is (0, 0, 0), meaning the sensor is aligned with all
+            rocket axes.
+        measurement_range : float, tuple, optional
+            The measurement range of the sensor in T. If a float, the
+            same range is applied both for positive and negative values. If a
+            tuple, the first value is the positive range and the second value is
+            the negative range. Default is np.inf.
+        resolution : float, optional
+            The resolution of the sensor in T/LSB. Default is 0, meaning no
+            quantization is applied.
+        hard_iron_distortion : float, list, optional
+            The hard iron distortion desired for the sensor in T.
+
+            - If a float, the same value is applied to each axis.
+            - If a list, the distortion is applied per axis.
+
+            Default is 0.
+        soft_iron_distortion : Matrix, str, optional
+            Soft iron distortion caused by materials with high permeability on
+            the rocket.
+
+            - If a Matrix, a direct 3x3 transformation matrix applied
+              to the magnetic field.
+            - If the string "plates", computes distortion
+              based on plates attached to the Rocket object.
+
+            Default is Matrix.identity().
+        power_interference : int, float, list, str, optional
+            The power interference is the magnetic distortion due to current
+            flowing through wires in the avionics bay in T:
+
+            - If an int or float, the same magnetic field will be applied to each axis.
+            - If a list, the given vector will be considered as power interference.
+            - If "wires", models total interference using rocket wires.
+            - If "personalized", requires passing activation_signal_interference and
+              communications_interference explicitly.
+
+            Default is 0.
+        activation_signal_interference : int, float, list, str, optional
+            Magnetic field in T generated by ignition wires:
+
+            - If an int or float, applied uniformly to each axis.
+            - If list, the given vector is used.
+            - If "wires", computed from ignition wires attached to the rocket.
+
+            Default is None.
+        communications_interference : int, float, list, str, optional
+            Magnetic field in T generated by communication wires:
+
+            - If an int or float, applied uniformly to each axis.
+            - If list, the given vector is used.
+            - If "wires", computed from communication wires attached to the rocket.
+
+            Default is None.
+        noise_density : float, list, optional
+            The noise density of the sensor for Gaussian white noise in T/√Hz.
+            Default is 0, meaning no noise is applied.
+        noise_variance : float, list, optional
+            The noise variance of the sensor for Gaussian white noise in T^2.
+            Default is 1.
+        random_walk_density : float, list, optional
+            The random walk density of the sensor in T/√Hz. Default is 0.
+        random_walk_variance : float, list, optional
+            The random walk variance of the sensor in T^2. Default is 1.
+        constant_bias : float, list, optional
+            The constant bias of the sensor in T. Default is 0.
+        operating_temperature : float, optional
+            The operating temperature of the sensor in Kelvin. Default is 298.
+        temperature_bias : float, list, optional
+            The temperature bias of the sensor in T/K. Default is 0.
+        temperature_scale_factor : float, list, optional
+            The temperature scale factor of the sensor in %/K. Default is 0.
+        cross_axis_sensitivity : float, optional
+            Skewness of the sensor's axes in percentage. Default is 0.
+        name : str, optional
+            Name of the sensor. Default is "Magnetometer".
+        seed : int, optional
+            Seed for the random number generator. Default is None.
+        """
+        self.magnetic_interference = [0, 0, 0]
+
+        if isinstance(power_interference, str):
+            if power_interference.lower() == "wires":
+                self.initial_power_interference = "wires"
+                self._validate_power_wires_parameters()
+            elif power_interference.lower() == "personalized":
+                self.initial_power_interference = "personalized"
+                self._validate_power_personalized_parameters(
+                    activation_signal_interference, communications_interference
+                )
+            else:
+                raise InvalidParameterError(
+                    "The accepted strings are 'wires' or 'personalized'"
+                )
+        else:
+            self.initial_power_interference = "number"
+            if isinstance(power_interference, (int, float)):
+                power_interference = [power_interference] * 3
+            self.power_interference = list(power_interference)
+            self._power_interference = Vector(self.power_interference)
+
+        self._validate_soft_iron(soft_iron_distortion)
+        self._validate_hard_iron(hard_iron_distortion)
+        self.prints = _InertialSensorPrints(self)
+        self._sensor_from_bacs, self.sensor_from_bacs_t = [None, None]
+
+        # Get current decimal year
+        current_date = datetime.now().strftime("%Y-%m-%d")
+        self.year = decimal_year(current_date)
+
+        # initialize the magnetic model
+        self.wmm = WMMv2()
+
+        # initialize InertialSensor class
+        super().__init__(
+            sampling_rate=sampling_rate,
+            orientation=orientation,
+            measurement_range=measurement_range,
+            resolution=resolution,
+            noise_density=noise_density,
+            noise_variance=noise_variance,
+            random_walk_density=random_walk_density,
+            random_walk_variance=random_walk_variance,
+            constant_bias=constant_bias,
+            operating_temperature=operating_temperature,
+            temperature_bias=temperature_bias,
+            temperature_scale_factor=temperature_scale_factor,
+            cross_axis_sensitivity=cross_axis_sensitivity,
+            name=name,
+            seed=seed,
+        )
+
+    def _validate_soft_iron(self, soft_iron_distortion) -> None:
+        """Checks and defines the soft_iron_distortion parameter."""
+        if isinstance(soft_iron_distortion, Matrix):
+            self._soft_iron_distortion_matrix = soft_iron_distortion
+            self.soft_iron_distortion_difference = []
+            self.initial_soft_iron_distortion_matrix = "matrix"
+        elif isinstance(soft_iron_distortion, str):
+            if soft_iron_distortion == "plates":
+                self._soft_iron_distortion_matrix = Matrix.identity()
+                self.initial_soft_iron_distortion_matrix = "plates"
+                self.total_soft_iron_distortion_matrix_computed = False
+                self.soft_iron_distortion_difference = []
+            else:
+                raise InvalidParameterError("The accepted string must be plates")
+
+    def _validate_hard_iron(self, hard_iron_distortion) -> None:
+        """Checks and defines the hard_iron_distortion parameter."""
+        if isinstance(hard_iron_distortion, (float, int)):
+            hard_iron_distortion = [hard_iron_distortion] * 3
+
+        self.hard_iron_distortion = list(hard_iron_distortion)
+        self._hard_iron_distortion = Vector(self.hard_iron_distortion)
+
+    def _validate_power_personalized_parameters(
+        self, activation_signal_interference, communications_interference
+    ) -> None:
+        """Checks and defines the parameters related to the power interference."""
+        if (
+            activation_signal_interference is None
+            or communications_interference is None
+        ):
+            raise InvalidParameterError(
+                "For 'personalized' interference, you must provide values for both 'activation_signal_interference' and 'communications_interference'."
+            )
+
+        self._validate_activation_signal_interference(activation_signal_interference)
+        self._validate_communications_interference(communications_interference)
+
+    def _validate_activation_signal_interference(
+        self, activation_signal_interference
+    ) -> None:
+        """Checks activation signal interference and defines the related attributes."""
+
+        if isinstance(activation_signal_interference, str):
+            if activation_signal_interference.lower() == "wires":
+                self.activation_signal_interference = [0, 0, 0]
+                self.initial_activation_signal_interference = "wires"
+            else:
+                raise InvalidParameterError("The accepted string is wires")
+        else:
+            if isinstance(activation_signal_interference, (int, float)):
+                activation_signal_interference = [activation_signal_interference] * 3
+            self.initial_activation_signal_interference = "number"
+            self.activation_signal_interference = list(activation_signal_interference)
+        self._activation_signal_interference = Vector(
+            self.activation_signal_interference
+        )
+
+    def _validate_communications_interference(
+        self, communications_interference
+    ) -> None:
+        """Checks communications interference and defines the related attributes."""
+
+        if isinstance(communications_interference, str):
+            if communications_interference.lower() == "wires":
+                self.communications_interference = [0, 0, 0]
+                self.initial_communications_interference = "wires"
+                self.communications_computed = False
+            else:
+                raise InvalidParameterError("The accepted string is wires")
+        else:
+            if isinstance(communications_interference, (int, float)):
+                communications_interference = [communications_interference] * 3
+            self.initial_communications_interference = "number"
+            self.communications_interference = list(communications_interference)
+
+        self._communications_interference = Vector(self.communications_interference)
+
+    def _validate_power_wires_parameters(self):
+        """Defines the power related attributes when the power_interference parmeter is "wires"."""
+        self.power_interference = [0, 0, 0]
+        self.communications_interference = [0, 0, 0]
+        self.communications_computed = False
+        self.activation_signal_interference = [0, 0, 0]
+
+        self.initial_communications_interference = "wires"
+        self.initial_activation_signal_interference = "wires"
+
+    def measure(self, time: float, **kwargs) -> None:
+        """Obtains the simulated reading of the magnetometer for a given time step.
+
+        Parameters
+        ----------
+        time : float
+            Current time in seconds.
+        kwargs : dict
+            Keyword arguments dictionary containing the following keys:
+
+            - u : np.ndarray
+                State vector of the rocket.
+                u = [x, y, z, vx, vy, vz, e0, e1, e2, e3, wx, wy, wz]
+
+            - rocket : Rocket, optional
+                RocketPy Rocket class. It is necessary when the magnetic distortion is modeled
+                using wires or plates. If there is no magnetic distortion, or if it is defined directly,
+                it is not necessary.
+
+            - u_dot : np.ndarray
+                Derivative of the state vector of the rocket.
+
+            - relative_position : Vector
+                Position of the sensor relative to the rocket center of dry mass in m.
+
+            - environment : Environment
+                Environment object containing atmospheric conditions.
+
+            - parachute_events : list, optional
+                List storing parachute events triggered during flight (only required if
+                ``ignition_wire_function`` is "parachute_deployment"). Each element is a list
+                containing the trigger time as the first element and the parachute object
+                as the second.
+        """
+        # initialization of parameters
+        u = kwargs["u"]  # state vector
+        parachute_events = kwargs.get("parachute_events")
+        self._sensor_from_bacs = kwargs[
+            "relative_position"
+        ]  # sensor position from body axis coordinate system
+        self.sensor_from_bacs_t = tuple(self._sensor_from_bacs)
+        current_time = time
+        lat0, lon0, launch_site_elevation = (
+            kwargs["environment"].latitude,
+            kwargs["environment"].longitude,
+            kwargs["environment"].elevation,
+        )
+        earth_radius = kwargs["environment"].earth_radius
+        rocket = kwargs.get(
+            "rocket"
+        )  # if there is no distortion the rocket is not necessary
+
+        # u[6:10]: Quaternion represents the center of dry mass with respect to the inertial frame.
+        rotation_bacs_to_inertial = Matrix.transformation(
+            u[6:10]
+        )  # rotation matrix from cdm to inertial frame
+
+        # --- obtain the current longitude, latitude and elevation ---
+        # obtain the sensor coordinates in the inertial frame, by adding the offset to the position vector
+        x_inertial, y_inertial, z_inertial = (
+            rotation_bacs_to_inertial @ self._sensor_from_bacs
+            + Vector(
+                u[0:3]
+            )  # Vector(u[0:3]) is the coordinates center of dry mass in the inertial frame
+        )
+        b_north, b_east, b_down = self._obtain_magnetic_field(
+            x_inertial,
+            y_inertial,
+            z_inertial,
+            launch_site_elevation,
+            earth_radius,
+            lat0,
+            lon0,
+        )
+
+        # --- Transform from NED to Rocketpy's inertial frame ---
+        b_field_inertial = Vector([b_east, b_north, -b_down])  # T
+
+        # --- from Rocketpy's inertial frame to bacs frame ---
+        b_field_bacs = rotation_bacs_to_inertial.transpose @ b_field_inertial  # T
+
+        # --- Apply magnetic interference ---
+        b_field_bacs = self.apply_magnetic_interference(
+            b_field_bacs, rocket, current_time, parachute_events
+        )  # T
+        # Transform body frame (bacs) to sensor frame, includes the cross-axis sensitivity adjustment
+        b_field_sensor = (
+            self._total_rotation_sensor_to_body.transpose @ b_field_bacs
+        )  # Ts
+        # --- apply noise and quantize ---
+        b_field_sensor = self.apply_temperature_drift(b_field_sensor)  # T
+        b_field_sensor = self.apply_noise(b_field_sensor)  # T
+        b_field_sensor = self.quantize(b_field_sensor)  # T
+
+        self.measurement = (b_field_sensor.x, b_field_sensor.y, b_field_sensor.z)  # T
+        self._save_data((time, *b_field_sensor))
+
+    def _obtain_magnetic_field(
+        self,
+        x_inertial: float,
+        y_inertial: float,
+        z_inertial: float,
+        launch_site_elevation: float,
+        earth_radius: float,
+        lat0: float,
+        lon0: float,
+    ) -> tuple[float, float, float]:
+        """Calculates Earth's magnetic field components in the North-East-Down (NED) frame.
+
+        Parameters
+        ----------
+        x_inertial : float
+            Inertial x-coordinate (East) in meters.
+        y_inertial : float
+            Inertial y-coordinate (North) in meters.
+        z_inertial : float
+            Inertial z-coordinate (Up) in meters.
+        launch_site_elevation : float
+            Launch site elevation above sea level in meters.
+        earth_radius : float
+            Radius of Earth at launch location in meters.
+        lat0 : float
+            Launch site latitude in degrees.
+        lon0 : float
+            Launch site longitude in degrees.
+
+        Returns
+        -------
+        b_north : float
+            Geomagnetic field North component in Tesla (T).
+        b_east : float
+            Geomagnetic field East component in Tesla (T).
+        b_down : float
+            Geomagnetic field Down component in Tesla (T).
+        """
+        altitude_wgs84_km = (z_inertial + launch_site_elevation) / 1000.0
+        drift = math.hypot(x_inertial, y_inertial)
+        bearing = math.atan2(x_inertial, y_inertial) * (180 / math.pi) % 360
+        latitude, longitude = inverted_haversine(
+            lat0, lon0, drift, bearing, earth_radius
+        )
+
+        calculate_geomagnetic(
+            self.wmm, latitude, longitude, self.year, altitude_wgs84_km
+        )
+
+        b_north = self.wmm.bx / 1e9
+        b_east = self.wmm.by / 1e9
+        b_down = self.wmm.bz / 1e9
+
+        return b_north, b_east, b_down
+
+    def apply_magnetic_interference(
+        self,
+        b_field: Vector,
+        rocket: Rocket,
+        current_time: float | int,
+        parachute_events: list | None = None,
+    ) -> Vector:
+        """Applies magnetic distortion due to power interference,
+        hard iron, and soft iron.
+
+        Parameters
+        ----------
+        b_field : Vector
+            Magnetic field Vector.
+        rocket : Rocket
+            RocketPy Rocket class.
+        current_time : float, optional
+            Current time of the simulation (required if ``ignition_wire_function``
+            is "motor_ignition").
+        parachute_events : list, optional
+            List storing parachute events triggered during flight (required if
+            ``ignition_wire_function`` is "parachute_deployment"). Each element is a
+            list containing the trigger time as the first element and the parachute
+            object as the second.
+
+        Returns
+        -------
+        b_field : Vector
+            Magnetic field vector after adjustment for hard iron, soft iron,
+            and power interference.
+        """
+        self.magnetic_interference = [0, 0, 0]
+
+        b_field = self.apply_soft_iron(b_field, rocket)  # T
+        b_field = self.apply_hard_iron(b_field)  # T
+        b_field = self.apply_power_interference(
+            b_field, rocket, current_time, parachute_events
+        )  # T
+
+        self.magnetic_interference = [
+            self.power_interference[0]
+            + self.hard_iron_distortion[0]
+            + self.soft_iron_distortion_difference[0],
+            self.power_interference[1]
+            + self.hard_iron_distortion[1]
+            + self.soft_iron_distortion_difference[1],
+            self.power_interference[2]
+            + self.hard_iron_distortion[2]
+            + self.soft_iron_distortion_difference[2],
+        ]
+        return b_field
+
+    def apply_soft_iron(self, b_field: Vector, rocket: Rocket) -> Vector:
+        """Applies soft iron distortion, which is the distortion of the
+        magnetic field caused by materials with high magnetic permeability relative
+        to the permeability of free space. These materials have lower magnetic resistance,
+        bending magnetic field lines through them.
+
+        Parameters
+        ----------
+        b_field : Vector
+            Vector reading of the Earth's magnetic field.
+        rocket : Rocket
+            RocketPy Rocket class.
+
+        Returns
+        -------
+        b_field_distorted : Vector
+            Magnetic field vector after soft iron distortion.
+        """
+        if self.initial_soft_iron_distortion_matrix == "plates":
+            if not self.total_soft_iron_distortion_matrix_computed:
+                for plate, _, _ in rocket.plates:
+                    if (
+                        self.sensor_from_bacs_t
+                        not in plate._magnetic_distortion_matrices
+                    ):
+                        plate.calculate_soft_iron_distortion_matrix(
+                            self._sensor_from_bacs, frame="bacs"
+                        )
+                        self._soft_iron_distortion_matrix = (
+                            self._soft_iron_distortion_matrix
+                            + plate._magnetic_distortion_matrices[
+                                self.sensor_from_bacs_t
+                            ]
+                        )
+                self.total_soft_iron_distortion_matrix_computed = True
+            b_field_distorted = self._soft_iron_distortion_matrix @ b_field
+        else:
+            b_field_distorted = self._soft_iron_distortion_matrix @ b_field
+
+        self.soft_iron_distortion_difference = list(b_field_distorted - b_field)
+        return b_field_distorted
+
+    def apply_hard_iron(self, b_field: Vector) -> Vector:
+        """Applies hard iron distortion. This magnetic distortion is caused by
+        permanent magnets or magnetized materials on the rocket that move along with
+        the sensor (e.g., steel screws, battery casing, ferromagnetic components),
+        producing a constant offset that shifts the center of the magnetic data.
+
+        Parameters
+        ----------
+        b_field : Vector
+            Magnetic field Vector.
+
+        Returns
+        -------
+        b_field : Vector
+            Magnetic field vector after applying hard iron distortion.
+        """
+        b_field = b_field + self._hard_iron_distortion
+        return b_field
+
+    def apply_power_interference(
+        self,
+        b_field: Vector,
+        rocket: Rocket,
+        current_time: float,
+        parachute_events: list | None = None,
+    ) -> Vector:
+        """Applies electromagnetic interference to the magnetic field vector.
+        Considers current flow when trigger conditions are fulfilled for ignition wires,
+        or continuously for communication wires.
+
+        Parameters
+        ----------
+        b_field : Vector
+            Magnetic field Vector.
+        rocket : Rocket
+            RocketPy Rocket class.
+        current_time : float, optional
+            Current time of the simulation (required if ``ignition_wire_function``
+            is "motor_ignition").
+        parachute_events : list, optional
+            List storing parachute events triggered during flight (required if
+            ``ignition_wire_function`` is "parachute_deployment"). Each element is a
+            list containing the trigger time as the first element and the parachute
+            object as the second.
+
+        Returns
+        -------
+        b_field : Vector
+            Magnetic field vector after adjustment for both activation signal
+            interference and communications interference.
+        """
+        if self.initial_power_interference in ("wires", "personalized"):
+            self.power_interference = [0, 0, 0]
+            b_field = self.apply_communications_interference(b_field, rocket)
+            b_field = self.apply_activation_signal_interference(
+                b_field, rocket, current_time, parachute_events
+            )
+            self.power_interference = [
+                self.activation_signal_interference[0]
+                + self.communications_interference[0],
+                self.activation_signal_interference[1]
+                + self.communications_interference[1],
+                self.activation_signal_interference[2]
+                + self.communications_interference[2],
+            ]
+            self._power_interference = Vector(self.power_interference)
+        else:
+            b_field = b_field + self._power_interference
+
+        return b_field
+
+    def apply_communications_interference(
+        self, b_field: Vector, rocket: Rocket
+    ) -> Vector:
+        """Applies interference caused by current flowing through communication wires.
+
+        Parameters
+        ----------
+        b_field : Vector
+            Magnetic field Vector.
+        rocket : Rocket
+            RocketPy Rocket class.
+
+        Returns
+        -------
+        b_field : Vector
+            Magnetic field vector after adjustment for communications magnetic
+            interference.
+        """
+        if self.initial_communications_interference == "wires":
+            if rocket._communication_wires:
+                if not self.communications_computed:
+                    for communication_wire in rocket._communication_wires:
+                        communication_wire.measure_magnetic_field(
+                            self._sensor_from_bacs, frame="bacs"
+                        )
+                        self.communications_interference = [
+                            self.communications_interference[0]
+                            + communication_wire.magnetic_field[
+                                self.sensor_from_bacs_t
+                            ][0],
+                            self.communications_interference[1]
+                            + communication_wire.magnetic_field[
+                                self.sensor_from_bacs_t
+                            ][1],
+                            self.communications_interference[2]
+                            + communication_wire.magnetic_field[
+                                self.sensor_from_bacs_t
+                            ][2],
+                        ]
+
+                    self._communications_interference = Vector(
+                        self.communications_interference
+                    )
+                    b_field = b_field + self._communications_interference
+                    self.communications_computed = True
+                else:
+                    b_field = b_field + self._communications_interference
+            else:
+                raise InvalidParameterError(
+                    "You must define first some communication wires, to be able to consider the magnetic disturbance created by them"
+                )
+        else:
+            b_field = b_field + self._communications_interference
+
+        return b_field
+
+    def apply_activation_signal_interference(
+        self,
+        b_field: Vector,
+        rocket: Rocket,
+        current_time: float,
+        parachute_events: list | None = None,
+    ) -> Vector:
+        """Applies magnetic interference caused by current flowing through
+        ignition wires during an activation signal.
+
+        Parameters
+        ----------
+        b_field : Vector
+            Magnetic field Vector.
+        rocket : Rocket
+            RocketPy Rocket class.
+        current_time : float, optional
+            Current time of the simulation (required if ``ignition_wire_function``
+            is "motor_ignition").
+        parachute_events : list, optional
+            List storing parachute events triggered during flight (required if
+            ``ignition_wire_function`` is "parachute_deployment"). Each element is a
+            list containing the trigger time as the first element and the parachute
+            object as the second.
+
+        Returns
+        -------
+        b_field : Vector
+            Magnetic field vector after adjustment for activation signal interference.
+        """
+
+        if self.initial_activation_signal_interference == "wires":
+            if rocket._ignition_wires:
+                self.activation_signal_interference = [0, 0, 0]
+                for ignition_wire in rocket._ignition_wires:
+                    if ignition_wire.ignition_wire_function == "parachute_deployment":
+                        b_field = (
+                            self._calculate_activation_signal_interference_parachute(
+                                b_field, current_time, parachute_events, ignition_wire
+                            )
+                        )
+
+                    elif ignition_wire.ignition_wire_function == "motor_ignition":
+                        b_field = self._calculate_activation_signal_interference_motor(
+                            b_field, rocket, current_time, ignition_wire
+                        )
+                    else:
+                        raise InvalidParameterError(
+                            "The accepted strings for the ignition_wire_function are motor_ignition and parachute_deployment"
+                        )
+            else:
+                raise InvalidParameterError(
+                    "You must define some ignition wire to be able to consider its magnetic disturbance."
+                )
+        else:
+            b_field = b_field + self._activation_signal_interference
+
+        return b_field
+
+    def _calculate_activation_signal_interference_parachute(
+        self, b_field, current_time, parachute_events, ignition_wire
+    ):
+        """Applies activation signal interference generated during parachute deployment.
+
+        Parameters
+        ----------
+        b_field : Vector
+            Magnetic field Vector.
+        current_time : float
+            Current time of the simulation.
+        parachute_events : list
+            List storing parachute events triggered during flight.
+        ignition_wire : Wire
+            Wire instance with ``wire_type`` "ignition" and function "parachute_deployment".
+
+        Returns
+        -------
+        b_field : Vector
+            Magnetic field vector after calculating parachute ignition interference.
+        """
+        if parachute_events is not None:
+            for parachute_event in parachute_events:
+                ejection_time = parachute_event[0]
+                parachute = parachute_event[1]
+                if (
+                    parachute.name == ignition_wire.parachute_name
+                    and ejection_time != 0
+                    and current_time
+                    <= ejection_time + ignition_wire.extra_ignition_time
+                ):
+                    if self.sensor_from_bacs_t not in ignition_wire._magnetic_field:
+                        ignition_wire.measure_magnetic_field(
+                            self._sensor_from_bacs, frame="bacs"
+                        )
+                    self.activation_signal_interference = [
+                        self.activation_signal_interference[0]
+                        + ignition_wire.magnetic_field[self.sensor_from_bacs_t][0],
+                        self.activation_signal_interference[1]
+                        + ignition_wire.magnetic_field[self.sensor_from_bacs_t][1],
+                        self.activation_signal_interference[2]
+                        + ignition_wire.magnetic_field[self.sensor_from_bacs_t][2],
+                    ]
+
+                    b_field = (
+                        b_field + ignition_wire._magnetic_field[self.sensor_from_bacs_t]
+                    )
+        else:
+            raise InvalidParameterError(
+                "The parachute events should be passed if a wire has ignition_wire_function == parachute_deployment."
+            )
+
+        return b_field
+
+    def _calculate_activation_signal_interference_motor(
+        self, b_field, rocket, current_time, ignition_wire
+    ):
+        """Applies activation signal interference generated during motor ignition.
+
+        Parameters
+        ----------
+        b_field : Vector
+            Magnetic field Vector.
+        rocket : Rocket
+            RocketPy Rocket class.
+        current_time : float
+            Current time of the simulation.
+        ignition_wire : Wire
+            Wire instance with ``wire_type`` "ignition" and function "motor_ignition".
+
+        Returns
+        -------
+        b_field : Vector
+            Magnetic field vector after calculating motor ignition interference.
+        """
+        if (
+            current_time
+            <= rocket.motor.burn_start_time + ignition_wire.extra_ignition_time
+        ):
+            if self.sensor_from_bacs_t not in ignition_wire._magnetic_field:
+                ignition_wire.measure_magnetic_field(
+                    self._sensor_from_bacs, frame="bacs"
+                )
+            self.activation_signal_interference = [
+                self.activation_signal_interference[0]
+                + ignition_wire.magnetic_field[self.sensor_from_bacs_t][0],
+                self.activation_signal_interference[1]
+                + ignition_wire.magnetic_field[self.sensor_from_bacs_t][1],
+                self.activation_signal_interference[2]
+                + ignition_wire.magnetic_field[self.sensor_from_bacs_t][2],
+            ]
+            b_field = b_field + ignition_wire._magnetic_field[self.sensor_from_bacs_t]
+        return b_field
+
+    def export_measured_data(self, filename, file_format="csv") -> None:
+        """Exports the measured values to a file.
+
+        Parameters
+        ----------
+        filename : str
+            Name of the file to export the values to.
+        file_format : str
+            Format of the file to export the values to. Options are "csv" and
+            "json". Default is "csv".
+        """
+        self._generic_export_measured_data(
+            filename=filename,
+            file_format=file_format,
+            data_labels=("t", "Bx", "By", "Bz"),
+        )
+
+    @classmethod
+    def from_dict(cls, data: dict) -> "Magnetometer":
+        """Creates a Magnetometer instance from a dictionary containing the
+        initialization parameters.
+
+        Parameters
+        ----------
+        data : dict
+            Dictionary containing magnetometer initialization parameters.
+
+        Returns
+        -------
+        magnetometer : Magnetometer
+            Magnetometer instance initialized with the specified parameters.
+        """
+        return cls(
+            # Mandatory Parameter
+            sampling_rate=data["sampling_rate"],
+            # Optional Parameters
+            orientation=data.get("orientation", (0, 0, 0)),
+            measurement_range=data.get("measurement_range", np.inf),
+            resolution=data.get("resolution", 0),
+            hard_iron_distortion=data.get("hard_iron_distortion", 0.0),
+            soft_iron_distortion=data.get("soft_iron_distortion", Matrix.identity()),
+            power_interference=data.get("power_interference", 0),
+            activation_signal_interference=data.get(
+                "activation_signal_interference", None
+            ),
+            communications_interference=data.get("communications_interference", None),
+            # Noise Profiles
+            noise_density=data.get("noise_density", 0),
+            noise_variance=data.get("noise_variance", 1),
+            random_walk_density=data.get("random_walk_density", 0),
+            random_walk_variance=data.get("random_walk_variance", 1),
+            constant_bias=data.get("constant_bias", 0),
+            # Environmental & Structural Shifts
+            operating_temperature=data.get("operating_temperature", 298),
+            temperature_bias=data.get("temperature_bias", 0),
+            temperature_scale_factor=data.get("temperature_scale_factor", 0),
+            cross_axis_sensitivity=data.get("cross_axis_sensitivity", 0),
+            seed=data.get("seed", None),
+        )
diff --git a/rocketpy/sensors/sensor.py b/rocketpy/sensors/sensor.py
index e4dddb162..9901784bf 100644
--- a/rocketpy/sensors/sensor.py
+++ b/rocketpy/sensors/sensor.py
@@ -357,7 +357,7 @@ class InertialSensor(Sensor):
         temperature drift.
     """
 
-    def __init__(  # pylint: disable=too-many-arguments
+    def __init__(
         self,
         sampling_rate,
         orientation=(0, 0, 0),
@@ -511,6 +511,7 @@ def __init__(  # pylint: disable=too-many-arguments
             ).round(12)
         else:
             raise ValueError("Invalid orientation format")
+
         self.normal_vector = Vector(
             [
                 self.rotation_sensor_to_body[0][2],
@@ -527,7 +528,6 @@ def __init__(  # pylint: disable=too-many-arguments
                 [self.cross_axis_sensitivity, self.cross_axis_sensitivity, 100],
             ]
         )
-
         # compute total rotation matrix given cross axis sensitivity
         self._total_rotation_sensor_to_body = (
             self.rotation_sensor_to_body @ cross_axis_matrix
@@ -570,13 +570,13 @@ def apply_noise(self, value):
 
         Parameters
         ----------
-        value : float
-            The value to add noise to
+        value : Vector
+            The Vector value to add noise to
 
         Returns
         -------
-        float
-            The value with added noise
+        value: Vector
+            The Vector value with added noise
         """
         # white noise
         white_noise = Vector(
@@ -599,24 +599,33 @@ def apply_temperature_drift(self, value):
 
         Parameters
         ----------
-        value : float
+        value : float or Vector
             The value to apply temperature drift to
 
         Returns
         -------
-        float
+        Vector
             The value with applied temperature drift
         """
+
+        if isinstance(value, (int, float)):
+            value = Vector([value, value, value])
+
+        elif not isinstance(value, Vector):
+            value = Vector(value)
+
         # temperature drift
-        value += (self.operating_temperature - 298.15) * self.temperature_bias
+        temp_delta = self.operating_temperature - 298.15
+        value = value + (temp_delta * self.temperature_bias)
+
         # temperature scale factor
         scale_factor = (
-            Vector([1, 1, 1])
-            + (self.operating_temperature - 298.15)
-            / 100
-            * self.temperature_scale_factor
+            Vector([1, 1, 1]) + (temp_delta / 100) * self.temperature_scale_factor
         )
-        return value & scale_factor
+
+        res = value & scale_factor
+
+        return res
 
     def to_dict(self, **kwargs):
         data = super().to_dict(**kwargs)
diff --git a/rocketpy/simulation/flight.py b/rocketpy/simulation/flight.py
index 200464ef1..6254e04eb 100644
--- a/rocketpy/simulation/flight.py
+++ b/rocketpy/simulation/flight.py
@@ -884,6 +884,8 @@ def __measure_sensors(self, component_sensors, u_dot, t=None, y_sol=None):
                 pressure=self.env.pressure,
                 earth_radius=self.env.earth_radius,
                 initial_coordinates=(self.env.latitude, self.env.longitude),
+                rocket=self,
+                parachute_events=self.parachute_events,
             )
 
     def __check_and_handle_parachute_triggers(
diff --git a/tests/acceptance/test_defiance_rocket.py b/tests/acceptance/test_defiance_rocket.py
index 9ac574671..d6016ef29 100644
--- a/tests/acceptance/test_defiance_rocket.py
+++ b/tests/acceptance/test_defiance_rocket.py
@@ -6,7 +6,6 @@
 from rocketpy.motors import CylindricalTank, Fluid, HybridMotor
 from rocketpy.motors.tank import MassFlowRateBasedTank
 
-
 MEASURED_APOGEE_AGL = 9308.32
 MAX_RELATIVE_APOGEE_ERROR = 0.01
 REFERENCE_MAX_SPEED = 444.24
diff --git a/tests/conftest.py b/tests/conftest.py
index a12c683e2..dd6d71621 100644
--- a/tests/conftest.py
+++ b/tests/conftest.py
@@ -31,6 +31,8 @@
     "tests.fixtures.sensors.sensors_fixtures",
     "tests.fixtures.generic_surfaces.generic_surfaces_fixtures",
     "tests.fixtures.generic_surfaces.linear_generic_surfaces_fixtures",
+    "tests.fixtures.plates.plate_fixtures",
+    "tests.fixtures.wire.wire_fixtures",
 ]
 
 
diff --git a/tests/fixtures/plates/__init__.py b/tests/fixtures/plates/__init__.py
new file mode 100644
index 000000000..e69de29bb
diff --git a/tests/fixtures/plates/plate_fixtures.py b/tests/fixtures/plates/plate_fixtures.py
new file mode 100644
index 000000000..175a6f814
--- /dev/null
+++ b/tests/fixtures/plates/plate_fixtures.py
@@ -0,0 +1,54 @@
+import pytest
+
+from rocketpy.rocket.plate import Plate
+
+
+@pytest.fixture()
+def test_circular_plate():
+    return Plate(
+        shape="circular",
+        dimensions=0.03,
+        material="carbon_steel",
+        thickness=0.0002,
+        z_points=40,
+        angular_points=40,
+        name="test_circular_plate",
+    )
+
+
+@pytest.fixture()
+def test_squared_plate():
+    return Plate(
+        shape="rectangular",
+        dimensions=0.03,
+        material="carbon_steel",
+        thickness=0.0002,
+        z_points=40,
+        angular_points=40,
+        name="test_squared_plate",
+    )
+
+
+@pytest.fixture()
+def test_rectangular_plate():
+    return Plate(
+        shape="rectangular",
+        dimensions=(0.03, 0.04),
+        material="carbon_steel",
+        thickness=0.0002,
+        z_points=40,
+        angular_points=40,
+        name="test_rectangular_plate",
+    )
+
+
+@pytest.fixture()
+def test_personalized_plate():
+    return Plate(
+        shape="personalized",
+        dimensions=[[0.001, 0.002, 0.3], [-0.001, 0.002, 0.4], [-0.001, -0.002, 0.4]],
+        material="carbon_steel",
+        thickness=0.001,
+        grid_spacing=0.002,
+        name="test_personalized_plate",
+    )
diff --git a/tests/fixtures/rockets/rocket_fixtures.py b/tests/fixtures/rockets/rocket_fixtures.py
index 9cb3caa3c..4c3a7b951 100644
--- a/tests/fixtures/rockets/rocket_fixtures.py
+++ b/tests/fixtures/rockets/rocket_fixtures.py
@@ -281,6 +281,7 @@ def calisto_with_sensors(
     ideal_gyroscope,
     ideal_barometer,
     ideal_gnss,
+    ideal_magnetometer,
 ):
     """Create an object class of the Rocket class to be used in the tests. This
     is the same Calisto rocket that was defined in the calisto fixture, but with
@@ -296,11 +297,12 @@ def calisto_with_sensors(
     calisto.add_surfaces(calisto_tail, -1.313)
     calisto.add_surfaces(calisto_trapezoidal_fins, -1.168)
     # double sensors to test using same instance twice
-    calisto.add_sensor(ideal_accelerometer, -0.1180124376577797)
-    calisto.add_sensor(ideal_accelerometer, -0.1180124376577797)
-    calisto.add_sensor(ideal_gyroscope, -0.1180124376577797)
-    calisto.add_sensor(ideal_barometer, -0.1180124376577797)
-    calisto.add_sensor(ideal_gnss, -0.1180124376577797)
+    calisto.add_sensor(ideal_accelerometer, (0, 0, -0.1180124376577797))
+    calisto.add_sensor(ideal_accelerometer, (0, 0, -0.1180124376577797))
+    calisto.add_sensor(ideal_gyroscope, (0, 0, -0.1180124376577797))
+    calisto.add_sensor(ideal_barometer, (0, 0, -0.1180124376577797))
+    calisto.add_sensor(ideal_gnss, (0, 0, -0.1180124376577797))
+    calisto.add_sensor(ideal_magnetometer, (0, 0, -0.1180124376577797))
     return calisto
 
 
@@ -415,3 +417,36 @@ def prometheus_cd_at_ma(mach):
         trigger=457.2,  # 1500 ft
     )
     return prometheus
+
+
+@pytest.fixture
+def calisto_robust_with_magnetometer_wires_and_plates(
+    noisy_rotated_magnetometer,
+    calisto_robust,
+    test_communications_wire,
+    test_ignition_wire_motor,
+    test_ignition_wire_parachute,
+    test_circular_plate,
+    test_personalized_plate,
+):
+
+    calisto_robust.add_sensor(noisy_rotated_magnetometer, position=[0, 0, 0.5])
+    calisto_robust.add_wire(
+        test_ignition_wire_motor,
+        position_endpoints=[[0.002, 0.004, -0.3], [0.003, 0.001, -1.3]],
+    )
+    calisto_robust.add_wire(
+        test_communications_wire,
+        position_endpoints=[[0.002, 0.004, -0.3], [0.003, 0.001, -1.3]],
+    )
+    calisto_robust.add_wire(
+        test_ignition_wire_parachute,
+        position_endpoints=[[0.002, 0.004, 0.3], [0.003, 0.001, 0.5]],
+        parachute_name="calisto_main_chute",
+    )
+    calisto_robust.add_plate(test_circular_plate, position=30, height=0.2)
+    calisto_robust.add_plate(
+        test_personalized_plate,
+        position=[[0.003, 0.001, -0.4], [0.002, 0.002, -0.4], [-0.002, 0.002, -0.4]],
+    )
+    return calisto_robust
diff --git a/tests/fixtures/sensors/sensors_fixtures.py b/tests/fixtures/sensors/sensors_fixtures.py
index aa515c808..c27e0e2c4 100644
--- a/tests/fixtures/sensors/sensors_fixtures.py
+++ b/tests/fixtures/sensors/sensors_fixtures.py
@@ -3,6 +3,31 @@
 from rocketpy import Accelerometer, Gyroscope
 from rocketpy.sensors.barometer import Barometer
 from rocketpy.sensors.gnss_receiver import GnssReceiver
+from rocketpy.sensors.magnetometer import Magnetometer
+
+
+@pytest.fixture
+def noisy_rotated_magnetometer():
+    """Returns a magnetometer with all parameters set to non-default values,
+    i.e. with noise and rotation."""
+    return Magnetometer(
+        sampling_rate=100,
+        orientation=(60, 60, 60),
+        measurement_range=1300e-6,
+        resolution=1e-6 / 16,
+        hard_iron_distortion=60e-6,
+        soft_iron_distortion="plates",
+        power_interference="wires",
+        noise_density=0.3e-7,
+        random_walk_density=0.02e-7,
+        constant_bias=1e-6,
+        operating_temperature=298.15,
+        temperature_bias=0.005e-6,
+        temperature_scale_factor=0.0001,
+        cross_axis_sensitivity=0.5,
+        name="Magnetometer",
+        seed=42,
+    )
 
 
 @pytest.fixture
@@ -78,6 +103,15 @@ def noisy_gnss():
     )
 
 
+@pytest.fixture
+def quantized_magnetometer():
+    """Returns a magnetometer with all parameters set to non-default values,
+    i.e. with noise and rotation."""
+    return Magnetometer(
+        sampling_rate=100, measurement_range=1300e-6, resolution=1e-6 / 16
+    )
+
+
 @pytest.fixture
 def quantized_accelerometer():
     """Returns an accelerometer with all parameters set to non-default values,
@@ -111,6 +145,11 @@ def quantized_barometer():
     )
 
 
+@pytest.fixture
+def ideal_magnetometer():
+    return Magnetometer(sampling_rate=100)
+
+
 @pytest.fixture
 def ideal_accelerometer():
     return Accelerometer(
diff --git a/tests/fixtures/units/numerical_fixtures.py b/tests/fixtures/units/numerical_fixtures.py
index 8bc6883cf..b9427cc4f 100644
--- a/tests/fixtures/units/numerical_fixtures.py
+++ b/tests/fixtures/units/numerical_fixtures.py
@@ -1,4 +1,4 @@
-import numericalunits
+import numericalunits as nu
 import pytest
 
 
@@ -12,7 +12,7 @@ def m():
     numericalunits.m
         A simple object of the numericalunits.m class
     """
-    return numericalunits.m
+    return nu.m
 
 
 @pytest.fixture
@@ -25,4 +25,4 @@ def kg():
     numericalunits.kg
         A simple object of the numericalunits.kg class
     """
-    return numericalunits.kg
+    return nu.kg
diff --git a/tests/fixtures/wire/__init__.py b/tests/fixtures/wire/__init__.py
new file mode 100644
index 000000000..e69de29bb
diff --git a/tests/fixtures/wire/wire_fixtures.py b/tests/fixtures/wire/wire_fixtures.py
new file mode 100644
index 000000000..4a2f06e4f
--- /dev/null
+++ b/tests/fixtures/wire/wire_fixtures.py
@@ -0,0 +1,32 @@
+import pytest
+
+from rocketpy.rocket import Wire
+
+
+@pytest.fixture
+def test_communications_wire():
+    return Wire(
+        current=0.01, wire_type="communications", name="test_communications_wire"
+    )
+
+
+@pytest.fixture()
+def test_ignition_wire_motor():
+    return Wire(
+        current=3,
+        wire_type="ignition",
+        ignition_wire_function="motor_ignition",
+        extra_ignition_time=0.5,
+        name="test_ignition_wire_motor",
+    )
+
+
+@pytest.fixture()
+def test_ignition_wire_parachute():
+    return Wire(
+        current=3,
+        wire_type="ignition",
+        ignition_wire_function="parachute_deployment",
+        extra_ignition_time=0.5,
+        name="test_ignition_wire_parachute",
+    )
diff --git a/tests/integration/test_sensor.py b/tests/integration/test_sensor.py
index ca9b0c8b9..f932eb696 100644
--- a/tests/integration/test_sensor.py
+++ b/tests/integration/test_sensor.py
@@ -11,6 +11,7 @@
 from rocketpy.sensors.barometer import Barometer
 from rocketpy.sensors.gnss_receiver import GnssReceiver
 from rocketpy.sensors.gyroscope import Gyroscope
+from rocketpy.sensors.magnetometer import Magnetometer
 from rocketpy.simulation import FlightDataExporter
 
 
@@ -32,6 +33,8 @@ def test_sensor_on_rocket(calisto_with_sensors):
     assert isinstance(sensors[3].position, Vector)
     assert isinstance(sensors[4].component, GnssReceiver)
     assert isinstance(sensors[4].position, Vector)
+    assert isinstance(sensors[5].component, Magnetometer)
+    assert isinstance(sensors[5].position, Vector)
 
 
 class TestIdealSensors:
@@ -41,10 +44,11 @@ class TestIdealSensors:
     def setup(self, flight_calisto_with_sensors):
         """Setup an flight fixture for all tests."""
         self.flight = flight_calisto_with_sensors
+        self.rocket = flight_calisto_with_sensors.rocket
 
     def test_accelerometer(self):
         """Test an ideal accelerometer."""
-        accelerometer = self.flight.rocket.sensors[0].component
+        accelerometer = self.rocket.sensors[0].component
         time, ax, ay, az = zip(*accelerometer.measured_data[0])
         sim_ax = self.flight.ax_body_frame(time)
         sim_ay = self.flight.ay_body_frame(time)
@@ -56,13 +60,13 @@ def test_accelerometer(self):
 
         # check if both added accelerometer instances saved the same data
         assert (
-            self.flight.sensors[0].measured_data[0]
-            == self.flight.sensors[0].measured_data[1]
+            self.rocket.sensors[0].component.measured_data[0]
+            == self.rocket.sensors[0].component.measured_data[1]
         )
 
     def test_gyroscope(self):
         """Test an ideal gyroscope."""
-        gyroscope = self.flight.rocket.sensors[2].component
+        gyroscope = self.rocket.sensors[2].component
         time, wx, wy, wz = zip(*gyroscope.measured_data)
         sim_wx = self.flight.w1(time)
         sim_wy = self.flight.w2(time)
@@ -74,7 +78,7 @@ def test_gyroscope(self):
 
     def test_barometer(self):
         """Test an ideal barometer."""
-        barometer = self.flight.rocket.sensors[3].component
+        barometer = self.rocket.sensors[3].component
         time, pressure = zip(*barometer.measured_data)
         pressure = np.array(pressure)
         sim_data = self.flight.pressure(time)
@@ -82,7 +86,7 @@ def test_barometer(self):
 
     def test_gnss_receiver(self):
         """Test an ideal GnssReceiver."""
-        gnss = self.flight.rocket.sensors[4].component
+        gnss = self.rocket.sensors[4].component
         time, latitude, longitude, altitude = zip(*gnss.measured_data)
         sim_latitude = self.flight.latitude(time)
         sim_longitude = self.flight.longitude(time)
@@ -117,39 +121,61 @@ def test_export_all_sensors_data(flight_calisto_with_sensors):
         data = f.read()
         sensor_data = json.loads(data)
     # convert list of tuples into list of lists to compare with the json
-    flight_calisto_with_sensors.sensors[0].measured_data[0] = [
+    flight_calisto_with_sensors.rocket.sensors[0].component.measured_data[0] = [
         list(measurement)
-        for measurement in flight_calisto_with_sensors.sensors[0].measured_data[0]
+        for measurement in flight_calisto_with_sensors.rocket.sensors[
+            0
+        ].component.measured_data[0]
     ]
-    flight_calisto_with_sensors.sensors[1].measured_data[1] = [
+    flight_calisto_with_sensors.rocket.sensors[1].component.measured_data[1] = [
         list(measurement)
-        for measurement in flight_calisto_with_sensors.sensors[1].measured_data[1]
+        for measurement in flight_calisto_with_sensors.rocket.sensors[
+            1
+        ].component.measured_data[1]
     ]
-    flight_calisto_with_sensors.sensors[2].measured_data = [
+    flight_calisto_with_sensors.rocket.sensors[2].component.measured_data = [
         list(measurement)
-        for measurement in flight_calisto_with_sensors.sensors[2].measured_data
+        for measurement in flight_calisto_with_sensors.rocket.sensors[
+            2
+        ].component.measured_data
     ]
-    flight_calisto_with_sensors.sensors[3].measured_data = [
+    flight_calisto_with_sensors.rocket.sensors[3].component.measured_data = [
         list(measurement)
-        for measurement in flight_calisto_with_sensors.sensors[3].measured_data
+        for measurement in flight_calisto_with_sensors.rocket.sensors[
+            3
+        ].component.measured_data
     ]
-    flight_calisto_with_sensors.sensors[4].measured_data = [
+    flight_calisto_with_sensors.rocket.sensors[4].component.measured_data = [
         list(measurement)
-        for measurement in flight_calisto_with_sensors.sensors[4].measured_data
+        for measurement in flight_calisto_with_sensors.rocket.sensors[
+            4
+        ].component.measured_data
+    ]
+    flight_calisto_with_sensors.rocket.sensors[5].component.measured_data = [
+        list(measurement)
+        for measurement in flight_calisto_with_sensors.rocket.sensors[
+            5
+        ].component.measured_data
     ]
     assert (
         sensor_data["Accelerometer"]
-        == flight_calisto_with_sensors.sensors[0].measured_data
+        == flight_calisto_with_sensors.rocket.sensors[0].component.measured_data
     )
     assert (
-        sensor_data["Gyroscope"] == flight_calisto_with_sensors.sensors[2].measured_data
+        sensor_data["Gyroscope"]
+        == flight_calisto_with_sensors.rocket.sensors[2].component.measured_data
     )
     assert (
-        sensor_data["Barometer"] == flight_calisto_with_sensors.sensors[3].measured_data
+        sensor_data["Barometer"]
+        == flight_calisto_with_sensors.rocket.sensors[3].component.measured_data
     )
     assert (
         sensor_data["GnssReceiver"]
-        == flight_calisto_with_sensors.sensors[4].measured_data
+        == flight_calisto_with_sensors.rocket.sensors[4].component.measured_data
+    )
+    assert (
+        sensor_data["Magnetometer"]
+        == flight_calisto_with_sensors.rocket.sensors[5].component.measured_data
     )
     os.remove(filename)
 
@@ -172,11 +198,14 @@ def test_export_single_sensor_data(flight_calisto_with_sensors):
         data = f.read()
         sensor_data = json.loads(data)
     # convert list of tuples into list of lists to compare with the json
-    flight_calisto_with_sensors.sensors[2].measured_data = [
+    flight_calisto_with_sensors.rocket.sensors[2].component.measured_data = [
         list(measurement)
-        for measurement in flight_calisto_with_sensors.sensors[2].measured_data
+        for measurement in flight_calisto_with_sensors.rocket.sensors[
+            2
+        ].component.measured_data
     ]
     assert (
-        sensor_data["Gyroscope"] == flight_calisto_with_sensors.sensors[2].measured_data
+        sensor_data["Gyroscope"]
+        == flight_calisto_with_sensors.rocket.sensors[2].component.measured_data
     )
     os.remove(filename)
diff --git a/tests/unit/environment/test_environment.py b/tests/unit/environment/test_environment.py
index 61d6c3ff4..9755a2a80 100644
--- a/tests/unit/environment/test_environment.py
+++ b/tests/unit/environment/test_environment.py
@@ -2,9 +2,9 @@
 import os
 from datetime import datetime
 
+import netCDF4
 import numpy as np
 import numpy.testing as npt
-import netCDF4
 import pytest
 import pytz
 
diff --git a/tests/unit/plate/test_plate.py b/tests/unit/plate/test_plate.py
new file mode 100644
index 000000000..63adab076
--- /dev/null
+++ b/tests/unit/plate/test_plate.py
@@ -0,0 +1,504 @@
+import numpy as np
+import pytest
+
+from rocketpy.exceptions import InvalidParameterError
+from rocketpy.mathutils import Matrix
+from rocketpy.plots.plate_plots import _PlatePlots
+from rocketpy.rocket.plate import Plate
+
+
+@pytest.mark.parametrize(
+    "shape, dimensions, material, thickness, absolute_magnetic_permeability, grid_spacing, z_points, angular_points, relative_magnetic_permeability, name",
+    [
+        (
+            0,
+            0.05,
+            "personalized",
+            0.002,
+            1e-3,
+            0.0002,
+            40,
+            40,
+            None,
+            "plate_test",
+        ),  # wrong shape: not str
+        (
+            "hi",
+            0.05,
+            "personalized",
+            0.002,
+            1e-3,
+            0.0002,
+            40,
+            40,
+            None,
+            "plate_test",
+        ),  # wrong shape: not allowed str
+        (
+            "rectangular",
+            "0.05",
+            "personalized",
+            0.002,
+            1e-3,
+            0.0002,
+            40,
+            40,
+            None,
+            "plate_test",
+        ),  # wrong dimensions rectangular: string
+        (
+            "rectangular",
+            [0, 9, 10],
+            "personalized",
+            0.002,
+            1e-3,
+            0.0002,
+            40,
+            40,
+            None,
+            "plate_test",
+        ),  # wrong dimensions rectangular: list of not 2 elements
+        (
+            "circular",
+            "0.05",
+            "personalized",
+            0.002,
+            1e-3,
+            0.0002,
+            40,
+            40,
+            None,
+            "plate_test",
+        ),  # wrong dimensions: string
+        (
+            "circular",
+            0.05,
+            0,
+            0.002,
+            1e-3,
+            0.0002,
+            40,
+            40,
+            None,
+            "plate_test",
+        ),  # wrong material: not a string
+        (
+            "circular",
+            0.05,
+            "0",
+            0.002,
+            1e-3,
+            0.0002,
+            40,
+            40,
+            None,
+            "plate_test",
+        ),  # wrong material: not allowed str
+        (
+            "circular",
+            0.05,
+            "personalized",
+            0.002,
+            None,
+            0.0002,
+            40,
+            40,
+            None,
+            "plate_test",
+        ),  # wrong magnetic inputs: neither relative nor absolute defined
+        (
+            "circular",
+            0.05,
+            "personalized",
+            0.002,
+            "None",
+            0.0002,
+            40,
+            40,
+            None,
+            "plate_test",
+        ),  # wrong abs magnetic permeability: str
+        (
+            "circular",
+            0.05,
+            "personalized",
+            0.002,
+            None,
+            0.0002,
+            40,
+            40,
+            "None",
+            "plate_test",
+        ),  # wrong relative magnetic permeability: str
+    ],
+)
+def test_validate_parameters(
+    shape,
+    dimensions,
+    material,
+    thickness,
+    absolute_magnetic_permeability,
+    grid_spacing,
+    z_points,
+    angular_points,
+    relative_magnetic_permeability,
+    name,
+):
+    """Tests that InvalidParameterError are raised with incorrect entry parameters."""
+    with pytest.raises(InvalidParameterError):
+        Plate(
+            shape,
+            dimensions,
+            material,
+            thickness,
+            absolute_magnetic_permeability,
+            relative_magnetic_permeability,
+            grid_spacing,
+            z_points,
+            angular_points,
+            name,
+        )
+
+
+@pytest.mark.parametrize(
+    "vertices",
+    [
+        [
+            [10, 3, 4],
+            [0.03, 0.04, 0.4],
+            [0.03, 0.004, 0],
+        ],  # wrong vertex: z out of bonds
+        [
+            [0.002, 3, 0.4],
+            [0.03, 0.04, -0.04],
+            [0.03, 0.004, 0],
+        ],  # wrong vertex: radius out of bonds
+        [[0.001, 0.003, 0.04], [0.003, -0.004, 0.4]],  # wrong size: at least 3
+    ],
+)
+def test_generate_personalized_points_bounds_out_of_bonds(vertices, calisto_robust):
+    """Tests the raise of InvalidParameterError when the vertices are out of the rocket."""
+    test_plate = Plate(
+        shape="personalized",
+        dimensions=vertices,
+        material="carbon_steel",
+        thickness=0.001,
+        grid_spacing=0.002,
+        name="test_personalized_plate",
+    )
+    with pytest.raises(InvalidParameterError):
+        calisto_robust.add_plate(test_plate)
+
+
+@pytest.mark.parametrize(
+    "vertices",
+    [
+        [
+            [0, 0, 0],
+            [0.001, 0.001, 0.001],
+            [0.002, 0.002, 0.002],
+        ],  # wrong vertices: 1D (line)
+        [
+            [0, 0, 0],
+            [-0.001, -0.001, -0.001],
+            [0.001, 0.001, 0.001],
+        ],  # wrong vertices: 1D (line)
+        [
+            [0, 0, 0],
+            [-0.001, -0.001, -0.001],
+            [0.001, 0.001, 0.001],
+            [-0.002, -0.002, -0.002],
+            [0.002, 0.002, 0.002],
+        ],  # wrong vertices: 1D (line)
+    ],
+)
+def test_generate_personalized_points_bounds_collinear(vertices, calisto_robust):
+    """Tests the raise of InvalidParameterError when the vertices don't form a 2D surface."""
+    test_plate = Plate(
+        shape="personalized",
+        dimensions=vertices,
+        material="carbon_steel",
+        thickness=0.001,
+        grid_spacing=0.002,
+        name="test_personalized_plate",
+    )
+    with pytest.raises(
+        InvalidParameterError,
+        match="All vertices of the personalized plate are collinear.",
+    ):
+        calisto_robust.add_plate(test_plate)
+
+
+@pytest.mark.parametrize(
+    "angle, expected_x",  # considering that calisto's rocket frame is tail to nose, the same as bacs
+    [
+        (0, 0.0),  # Angle = 0°   -> x = 0
+        (90, -0.0635),  # Angle = 90°  -> x = -R
+        (180, 0.0),  # Angle = 180° -> x = 0
+        (270, +0.0635),  # Angle = 270° -> x = +R
+    ],
+)
+def test_generate_angular_plate_position(angle, expected_x, calisto_robust):
+    """Tests proper position vector generation in the BACS frame
+    based on the angular position.
+    """
+    small_plate = Plate(
+        shape="circular",
+        dimensions=0.004,
+        material="carbon_steel",
+        thickness=0.0002,
+        z_points=40,
+        angular_points=70,
+        name="small_circular_plate",
+    )
+    calisto_robust.add_plate(small_plate, position=angle, height=0.2)
+    one_x_true = any(
+        pytest.approx(expected_x, abs=1e-3) == point[0] for point in small_plate.points
+    )
+    assert one_x_true
+
+
+@pytest.mark.parametrize(
+    "plate",
+    [
+        "test_circular_plate",
+        "test_squared_plate",
+        "test_rectangular_plate",
+    ],
+)
+def test_plate_dimensions(request, plate, calisto_robust):
+    """Tests proper position vector generation in the BACS frame
+    based on dimensions.
+    """
+    plate_object = request.getfixturevalue(plate)
+    height = 0.0
+    position_deg = 0.0
+
+    calisto_robust.add_plate(plate_object, position=position_deg, height=height)
+
+    radius = calisto_robust.general_radius(height, frame="ucs")
+
+    # Center position in BACS
+    z_bacs_center = (
+        height - calisto_robust.center_of_dry_mass_position
+    ) * calisto_robust._csys
+
+    if plate_object.shape == "circular":
+        half_height = plate_object.dimensions
+        theta = plate_object.dimensions / radius
+    else:
+        half_height = plate_object.dimensions[1] / 2.0
+        theta = (plate_object.dimensions[0] / 2.0) / radius
+
+    max_expected_x = radius * np.sin(theta)
+    max_expected_y = radius
+    expected_max_z = z_bacs_center + half_height
+    expected_min_z = z_bacs_center - half_height
+
+    points = plate_object.points
+
+    assert any(pytest.approx(max_expected_x, abs=1e-5) == p[0] for p in points)
+    assert any(pytest.approx(max_expected_y, abs=1e-5) == p[1] for p in points)
+    assert any(pytest.approx(expected_max_z, abs=1e-5) == p[2] for p in points)
+    assert any(pytest.approx(expected_min_z, abs=1e-5) == p[2] for p in points)
+
+
+@pytest.mark.parametrize(
+    "height_ucs",
+    [
+        1.15,  # almost out of the rocket(upper bound)
+        -1.2,  # almost out of rocket(lower bound)
+    ],
+)
+def test_less_points_plate(height_ucs, calisto_robust):
+    """Tests that when the dimensions, or the point generated are out of the rocket
+    no error is raised and some points have been dismissed.
+    """
+    z_points = 50
+    angular_points = 70
+    test_plate = Plate(
+        shape="circular",
+        material="carbon_steel",
+        thickness=0.001,
+        dimensions=0.4,
+        z_points=z_points,
+        angular_points=angular_points,
+        name="less_points_than_default_plate",
+    )
+    calisto_robust.add_plate(test_plate, position=30, height=height_ucs)
+    assert 0 < len(test_plate.points) < z_points * angular_points
+
+
+def test_several_positions_soft_iron_distortion_matrix(
+    test_squared_plate, calisto_robust
+):
+    """Ensures proper handling of the soft iron distoriton matrices
+    as a dictionary.
+    """
+    calisto_robust.add_plate(test_squared_plate, position=45, height=0.2)
+    test_squared_plate.calculate_soft_iron_distortion_matrix((0, 0, 0), frame="bacs")
+    test_squared_plate.calculate_soft_iron_distortion_matrix(
+        (0.004, 0.003, 0.5), frame="bacs"
+    )
+    assert len(test_squared_plate._magnetic_distortion_matrices) == 2
+
+    list_keys = list(test_squared_plate._magnetic_distortion_matrices)
+    assert list_keys[0] == (0, 0, 0)
+    assert list_keys[1] == (0.004, 0.003, 0.5)
+
+
+def test_no_soft_iron_distortion_matrix(calisto_robust):
+    """Tests that when the relative magnetic permeability is 1, no distortion is added."""
+    test_plate = Plate(
+        shape="circular",
+        dimensions=0.04,
+        material="personalized",
+        thickness=0.001,
+        absolute_magnetic_permeability=4 * np.pi * 1e-7,
+        name="identity_soft_iron",
+    )
+    calisto_robust.add_plate(test_plate, position=30, height=0.3)
+    test_plate.calculate_soft_iron_distortion_matrix([0, 0, 0], frame="bacs")
+    assert test_plate._magnetic_distortion_matrices[(0, 0, 0)] == Matrix.zeros()
+
+
+@pytest.mark.parametrize(
+    "dimensions_1, material_1, absolute_magnetic_permeability_1, dimensions_2, material_2, absolute_magnetic_permeability_2",
+    [
+        (
+            0.7,
+            "carbon_steel",
+            None,
+            0.007,
+            "carbon_steel",
+            None,
+        ),  # bigger plate -> higher distortion
+        (
+            0.07,
+            "iron",
+            None,
+            0.07,
+            "carbon_steel",
+            None,
+        ),  # bigger absolute magnetic permeability -> higher distortion
+        (
+            0.07,
+            "personalized",
+            1.25e-7,
+            0.07,
+            "personalized",
+            1.25e-6,
+        ),  # lower absolute magnetic permeability (diamagnetic materials) than vacuum -> higher distortion
+    ],
+)
+def test_compare_soft_iron_distortion_matrix(
+    dimensions_1,
+    material_1,
+    absolute_magnetic_permeability_1,
+    dimensions_2,
+    material_2,
+    absolute_magnetic_permeability_2,
+    calisto_robust,
+):
+    """
+    Tests that
+    - The plate class is able to handle wrapped plates, which is also
+      reflected in the magnitude of the distortion of the soft iron
+      distortion matrix.
+    - Bigger magnetic permeability causes bigger magnetic distortion.
+    """
+    z_points = 150
+    angular_points = 200
+    shape = "circular"
+    thickness = 0.003
+    position = 30
+    height = 0.6
+
+    # definition of plates
+    big_plate = Plate(
+        shape=shape,
+        dimensions=dimensions_1,
+        material=material_1,
+        absolute_magnetic_permeability=absolute_magnetic_permeability_1,
+        thickness=thickness,
+        z_points=z_points,
+        angular_points=angular_points,
+    )
+    small_plate = Plate(
+        shape=shape,
+        dimensions=dimensions_2,
+        material=material_2,
+        absolute_magnetic_permeability=absolute_magnetic_permeability_2,
+        thickness=thickness,
+        z_points=z_points,
+        angular_points=angular_points,
+    )
+
+    # big_plate
+    calisto_robust.add_plate(big_plate, position=position, height=height)
+    big_plate.calculate_soft_iron_distortion_matrix((0, 0, 0), frame="bacs")
+    big_plate_matrix = big_plate._magnetic_distortion_matrices[(0, 0, 0)]
+
+    # small_plate
+    calisto_robust.add_plate(small_plate, position=position, height=height)
+    small_plate.calculate_soft_iron_distortion_matrix((0, 0, 0), frame="bacs")
+    small_plate_matrix = small_plate._magnetic_distortion_matrices[(0, 0, 0)]
+
+    for row in range(3):
+        for column in range(3):
+            assert abs(big_plate_matrix[row, column]) > abs(
+                small_plate_matrix[row, column]
+            )
+
+
+def test_rocket_belonging(test_circular_plate, calisto_robust):
+    """Tests if the belonging attribute works as intended"""
+    calisto_robust.add_plate(test_circular_plate, position=-0.3, height=0.3)
+    assert isinstance(test_circular_plate.plots, _PlatePlots)
+    assert not isinstance(test_circular_plate._csys, type(None))
+    assert not isinstance(test_circular_plate.center_of_dry_mass_position, type(None))
+
+
+@pytest.mark.parametrize(
+    "plate, position, height",
+    [
+        ("test_personalized_plate", None, None),
+        ("test_circular_plate", 45, 0.3),
+        ("test_squared_plate", 45, 0.4),
+    ],
+)
+def test_plate_prints_and_plots(request, plate, position, height, calisto_robust):
+    """Test the print methods of the Plate class. Checks if all attributes are
+    printed and plotted correctly.
+    """
+    plate_obj = request.getfixturevalue(plate)
+    with pytest.raises(InvalidParameterError):
+        plate_obj.plots.draw()
+    with pytest.raises(InvalidParameterError):
+        plate_obj.plots.draw_3d()
+    calisto_robust.add_plate(plate_obj, position, height)
+    plate_obj.prints.all()
+    plate_obj.plots.all()
+    assert True
+
+
+def test_from_dict():
+    """Tests if from_dict returns a Plate object."""
+    plate_dict = {
+        "shape": "rectangular",
+        "dimensions": 0.003,
+        "material": "personalized",
+        "thickness": 0.001,
+        "absolute_magnetic_permeability": 1e-5,
+        "relative_magnetic_permeability": None,
+        "z_points": 50,
+        "angular_points": 50,
+        "name": "from_dict_plate",
+    }
+    plate_from_dict = Plate.from_dict(plate_dict)
+    assert isinstance(plate_from_dict, Plate)
+    assert plate_from_dict.dimensions == (0.003, 0.003)
+    assert plate_from_dict.material == "personalized"
+    assert plate_from_dict.thickness == pytest.approx(0.001)
+    assert plate_from_dict.z_points == pytest.approx(50)
+    assert plate_from_dict.angular_points == pytest.approx(50)
diff --git a/tests/unit/rocket/test_rocket.py b/tests/unit/rocket/test_rocket.py
index 2682f5b90..a771dd0b2 100644
--- a/tests/unit/rocket/test_rocket.py
+++ b/tests/unit/rocket/test_rocket.py
@@ -1094,3 +1094,97 @@ def test_evaluate_reduced_mass_with_motor(calisto):
     for t in [0.0, 1.0, 2.0, 3.0]:
         expected = prop_mass(t) * dry_mass / (prop_mass(t) + dry_mass)
         assert reduced_mass(t) == pytest.approx(expected)
+
+
+@pytest.mark.parametrize(
+    "wire, position_endpoints, parachute_name",
+    [
+        (
+            "test_circular_plate",
+            [[0.001, 0.001, 0], [0.001, -0.001, 0]],
+            None,
+        ),  # wrong wire: not Wire
+        (
+            "test_communications_wire",
+            1,
+            None,
+        ),  # wrong dimensions: number
+        (
+            "test_communications_wire",
+            [[0.001, 0.001, 0], [0.001, -0.001, 0], []],
+            None,
+        ),  # wrong dimensions: only 2 position endpoints
+        (
+            "test_communications_wire",
+            [[0.001, 0.001, 0], [0.001, -0.001, 0, 10]],
+            None,
+        ),  # wrong dimensions: only 3 coodinates in endpoint position
+        (
+            "test_communications_wire",
+            [[0.001, 0.001, 0], 9],
+            None,
+        ),  # wrong dimensions: either all are numbers or all list
+        (
+            "test_communications_wire",
+            [[0.001, 0.001, 0], [0.001, -0.001, 10]],
+            None,
+        ),  # wrong endpoint: z out of range
+        (
+            "test_communications_wire",
+            [[0.001, 0.001, 0], [0.001, -1, 0]],
+            None,
+        ),  # wrong endpoint: radius of out range
+        (
+            "test_ignition_wire_parachute",
+            [[0.001, 0.001, 0], [0.001, -0.001, 0]],
+            None,
+        ),  # wrong parachute_name: None
+        (
+            "test_ignition_wire_parachute",
+            [[0.001, 0.001, 0], [0.001, -0.001, 0]],
+            10,
+        ),  # wrong parachute_name: number
+    ],
+)
+def test_add_wire(request, wire, position_endpoints, parachute_name, calisto_robust):
+    """Tests that add_wire raises InvalidParameterError as intended."""
+    wire_object = request.getfixturevalue(wire)
+    with pytest.raises(InvalidParameterError):
+        calisto_robust.add_wire(wire_object, position_endpoints, parachute_name)
+
+
+@pytest.mark.parametrize(
+    "plate, position, height",
+    [
+        ("test_communications_wire", 30, 0.4),  # wrong Plate: not Plate
+        ("test_circular_plate", None, 0.4),  # wrong position: None
+        ("test_circular_plate", "None", 0.4),  # wrong position: str
+        ("test_circular_plate", 30, None),  # wrong height: None
+        ("test_circular_plate", 30, "None"),  # wrong height: str
+        ("test_circular_plate", 30, 40),  # wrong height: out of bounds
+    ],
+)
+def test_add_plate(request, plate, position, height, calisto_robust):
+    """Tests that add_plate raises InvalidParameterError as intended."""
+    plate_obj = request.getfixturevalue(plate)
+    with pytest.raises(InvalidParameterError):
+        calisto_robust.add_plate(plate_obj, position, height)
+
+
+def test_general_radius(calisto_robust):
+    """Tests the general radius funciton as well as the _calculate_radius_z_intermediate,
+    nose cone radius function and the tail radius function."""
+    prev = 0
+    for z in np.linspace(-1.313 - 0.06, 1.16, 100):
+        current_radius = calisto_robust.general_radius(z, frame="ucs")
+        if -1.313 - 0.06 <= z <= -1.313:
+            assert 0.0435 <= current_radius <= 0.0635
+            assert current_radius > prev
+            prev = current_radius
+        elif z <= 1.160 - 0.55829:
+            assert current_radius == 0.0635
+            prev = current_radius
+        else:
+            assert 0 <= current_radius <= calisto_robust.radius
+            assert current_radius < prev
+            prev = current_radius
diff --git a/tests/unit/sensors/test_sensor.py b/tests/unit/sensors/test_sensor.py
index 0813a3638..84ed7f438 100644
--- a/tests/unit/sensors/test_sensor.py
+++ b/tests/unit/sensors/test_sensor.py
@@ -5,7 +5,9 @@
 import pytest
 from pytest import approx
 
+from rocketpy.exceptions import InvalidParameterError
 from rocketpy.mathutils.vector_matrix import Matrix, Vector
+from rocketpy.sensors.magnetometer import Magnetometer
 from rocketpy.tools import euler313_to_quaternions
 
 # calisto standard simulation no wind solution index 200
@@ -46,6 +48,8 @@
 @pytest.mark.parametrize(
     "sensor",
     [
+        "noisy_rotated_magnetometer",
+        "quantized_magnetometer",
         "noisy_rotated_accelerometer",
         "quantized_accelerometer",
         "noisy_rotated_gyroscope",
@@ -152,6 +156,7 @@ def test_quantization(sensor, input_value, expected_output, request):
 @pytest.mark.parametrize(
     "sensor",
     [
+        "ideal_magnetometer",
         "ideal_accelerometer",
         "ideal_gyroscope",
     ],
@@ -265,6 +270,102 @@ def test_scalar_measured_data(sensor, request, example_plain_env):
     assert len(sensor.measured_data[1]) == 3
 
 
+def test_noisy_rotated_magnetometer(
+    noisy_rotated_magnetometer,
+    example_plain_env,
+    calisto_robust_with_magnetometer_wires_and_plates,
+    test_communications_wire,
+    test_circular_plate,
+    test_personalized_plate,
+    calisto_main_chute,
+):
+    """
+    Test the measure method of the Magnetometer class.
+    Verifies coordinate transformations, magnetic field readings,
+    hard/soft iron distortions and power interference.
+    """
+    sensor_from_bacs_list = [
+        0.001,
+        0.002,
+        0.3,
+    ]
+    rotation_bacs_to_inertial = Matrix.transformation(U[6:10])
+
+    x_inertial, y_inertial, z_inertial = rotation_bacs_to_inertial @ Vector(
+        sensor_from_bacs_list
+    ) + Vector(U[0:3])
+    b_north, b_east, b_down = noisy_rotated_magnetometer._obtain_magnetic_field(
+        x_inertial,
+        y_inertial,
+        z_inertial,
+        example_plain_env.elevation,
+        example_plain_env.earth_radius,
+        example_plain_env.latitude,
+        example_plain_env.longitude,
+    )
+    b_field_bacs = rotation_bacs_to_inertial.transpose @ Vector(
+        [b_east, b_north, -b_down]
+    )  # T
+    # apply magnetic interference:
+    # soft iron
+    soft_iron_matrix = Matrix.identity()
+    for plate in [test_circular_plate, test_personalized_plate]:
+        plate.calculate_soft_iron_distortion_matrix(
+            Vector(sensor_from_bacs_list), frame="bacs"
+        )
+        soft_iron_matrix += plate._magnetic_distortion_matrices[
+            tuple(sensor_from_bacs_list)
+        ]
+    b_field_bacs = soft_iron_matrix @ b_field_bacs
+
+    # hard iron
+    b_field_bacs += Vector([60e-6] * 3)
+
+    # communicatons interference
+    test_communications_wire.measure_magnetic_field(
+        Vector(sensor_from_bacs_list), frame="bacs"
+    )
+    b_field_bacs += test_communications_wire._magnetic_field[
+        tuple(sensor_from_bacs_list)
+    ]
+
+    # noise, temperature drift and quantize
+    cross_axis_sensitivity = Matrix(
+        [
+            [1, 0.005, 0.005],
+            [0.005, 1, 0.005],
+            [0.005, 0.005, 1],
+        ]
+    )
+    sensor_rotation = Matrix.transformation(
+        euler313_to_quaternions(*np.deg2rad([60, 60, 60]))
+    )
+    total_rotation = sensor_rotation @ cross_axis_sensitivity
+
+    # expected measurement without noise (and without temperature drift, operating temperature is 298.15)
+    b_field_sensor = total_rotation.transpose @ b_field_bacs
+    # expected measurement with constant bias
+    bx, by, bz = b_field_sensor + Vector([1e-6] * 3)
+
+    # with measure
+    noisy_rotated_magnetometer.measure(
+        time=TIME,
+        u=U,
+        u_dot=U_DOT,
+        relative_position=Vector(sensor_from_bacs_list),
+        environment=example_plain_env,
+        rocket=calisto_robust_with_magnetometer_wires_and_plates,
+        parachute_events=[[6, calisto_main_chute]],
+    )
+    # Assert that the sensor outputs the expected magnetic field
+    assert noisy_rotated_magnetometer.measurement == approx([bx, by, bz], rel=0.1)
+    assert len(noisy_rotated_magnetometer.measurement) == 3
+    assert noisy_rotated_magnetometer.measured_data[0][1:] == approx(
+        [bx, by, bz], rel=0.1
+    )
+    assert noisy_rotated_magnetometer.measured_data[0][0] == TIME
+
+
 def test_noisy_rotated_accelerometer(noisy_rotated_accelerometer, example_plain_env):
     """Test the measure method of the Accelerometer class. Checks if saved
     measurement is (ax,ay,az) and if measured_data is [(t, (ax,ay,az)), ...]
@@ -275,12 +376,12 @@ def test_noisy_rotated_accelerometer(noisy_rotated_accelerometer, example_plain_
     inertial_acceleration = Vector(U_DOT[3:6]) + Vector([0, 0, -GRAVITY])
     omega = Vector(U[10:13])
     omega_dot = Vector(U_DOT[10:13])
-    acceleration = (
-        inertial_acceleration
+    body_acceleration = Matrix.transformation(U[6:10]).transpose @ inertial_acceleration
+    a_body = (
+        body_acceleration
         + Vector.cross(omega_dot, relative_position)
         + Vector.cross(omega, Vector.cross(omega, relative_position))
     )
-
     # calculate total rotation matrix
     cross_axis_sensitivity = Matrix(
         [
@@ -292,15 +393,13 @@ def test_noisy_rotated_accelerometer(noisy_rotated_accelerometer, example_plain_
     sensor_rotation = Matrix.transformation(
         euler313_to_quaternions(*np.deg2rad([60, 60, 60]))
     )
-    total_rotation = sensor_rotation @ cross_axis_sensitivity
-    rocket_rotation = Matrix.transformation(U[6:10]).transpose
-    # expected measurement without noise
-    ax, ay, az = total_rotation @ (rocket_rotation @ acceleration)
+    total_rotation_sensor_to_body = sensor_rotation @ cross_axis_sensitivity
+    # expected measurement without noise in sensor frame
+    ax, ay, az = total_rotation_sensor_to_body.transpose @ a_body
     # expected measurement with constant bias
-    ax += 0.5
-    ay += 0.5
+    ax += 0
+    ay += 0.3
     az += 0.5
-
     # check last measurement considering noise error bounds
     noisy_rotated_accelerometer.measure(
         time=TIME,
@@ -317,6 +416,102 @@ def test_noisy_rotated_accelerometer(noisy_rotated_accelerometer, example_plain_
     assert noisy_rotated_accelerometer.measured_data[0][0] == TIME
 
 
+@pytest.mark.parametrize(
+    "power_interference, hard_iron_distortion, soft_iron_distortion, activation_signal_interference, communications_interference",
+    [
+        (
+            "a",
+            [10, 10, 0],
+            "plates",
+            "wires",
+            "wires",
+        ),  # wrong power_interference: not allowed str
+        (
+            "personalized",
+            [10, 10, 0],
+            "plates",
+            None,
+            None,
+        ),  # wrong personalized inputs: activaiton signal and communications interference cannot be None
+        (
+            "personalized",
+            [10, 10, 0],
+            "plates",
+            "a",
+            None,
+        ),  # wrong activaiton_signal_interference: not allowed str
+        (
+            "personalized",
+            [10, 10, 0],
+            "plates",
+            3,
+            "None",
+        ),  # wrong communications_interference: not allowed str
+        (
+            "personalized",
+            [10, 10, 0],
+            "a",
+            3,
+            "None",
+        ),  # wrong soft_iron_distortion: not allowed str
+    ],
+)
+def test_magnetometer_valid_parameters(
+    power_interference,
+    hard_iron_distortion,
+    soft_iron_distortion,
+    activation_signal_interference,
+    communications_interference,
+):
+    """
+    Validation of the input parameters of the arguments that are
+    unique of the magnetometer (not shared with parent classes).
+    """
+    # common attributes
+    with pytest.raises(InvalidParameterError):
+        Magnetometer(
+            sampling_rate=40,
+            hard_iron_distortion=hard_iron_distortion,
+            soft_iron_distortion=soft_iron_distortion,
+            power_interference=power_interference,
+            activation_signal_interference=activation_signal_interference,
+            communications_interference=communications_interference,
+        )
+
+
+def test_from_dict_magnetometer():
+    all_default_magnetometer_dict = {
+        "sampling_rate": 40,
+    }
+    all_default_magnetometer = Magnetometer.from_dict(all_default_magnetometer_dict)
+    assert isinstance(all_default_magnetometer, Magnetometer)
+
+    nothing_default_magnetometer_dict = {
+        "sampling_rate": 100.0,
+        "orientation": (0.0, 0.0, 0.0),
+        "measurement_range": 16.0,
+        "resolution": 16,
+        "hard_iron_distortion": 0.05,
+        "soft_iron_distortion": 3 * Matrix.identity(),
+        "power_interference": 0.01,
+        "activation_signal_interference": None,
+        "communications_interference": None,
+        "noise_density": 0.001,
+        "noise_variance": 0.05,
+        "random_walk_density": 0.0001,
+        "random_walk_variance": 0.01,
+        "constant_bias": 0.02,
+        "operating_temperature": 298.15,
+        "temperature_bias": 0.005,
+        "temperature_scale_factor": 0.001,
+        "cross_axis_sensitivity": 0.02,
+    }
+    nothing_default_magnetometer = Magnetometer.from_dict(
+        nothing_default_magnetometer_dict
+    )
+    assert isinstance(nothing_default_magnetometer, Magnetometer)
+
+
 def test_noisy_rotated_gyroscope(noisy_rotated_gyroscope, example_plain_env):
     """Test the measure method of the Gyroscope class. Checks if saved
     measurement is (wx,wy,wz) and if measured_data is [(t, (wx,wy,wz)), ...]
@@ -441,6 +636,7 @@ def test_noisy_gnss(noisy_gnss, example_plain_env):
 @pytest.mark.parametrize(
     "sensor, file_format, expected_header",
     [
+        ("ideal_magnetometer", "csv", "t,Bx,By,Bz\n"),
         ("ideal_accelerometer", "csv", "t,ax,ay,az\n"),
         ("ideal_gyroscope", "csv", "t,wx,wy,wz\n"),
         ("ideal_barometer", "csv", "t,pressure\n"),
@@ -482,6 +678,7 @@ def test_export_data_csv(
 @pytest.mark.parametrize(
     "sensor, file_format, expected_keys",
     [
+        ("ideal_magnetometer", "json", ("Bx", "By", "Bz")),
         ("ideal_accelerometer", "json", ("ax", "ay", "az")),
         ("ideal_gyroscope", "json", ("wx", "wy", "wz")),
         ("ideal_barometer", "json", ("pressure",)),
diff --git a/tests/unit/sensors/test_sensor_seeding.py b/tests/unit/sensors/test_sensor_seeding.py
index 73b4c664b..8cb10fca9 100644
--- a/tests/unit/sensors/test_sensor_seeding.py
+++ b/tests/unit/sensors/test_sensor_seeding.py
@@ -22,6 +22,7 @@
 from rocketpy.sensors.barometer import Barometer
 from rocketpy.sensors.gnss_receiver import GnssReceiver
 from rocketpy.sensors.gyroscope import Gyroscope
+from rocketpy.sensors.magnetometer import Magnetometer
 
 
 def _accelerometer(seed):
@@ -125,7 +126,14 @@ def test_seed_survives_serialization_round_trip():
             ),
             44,
         ),
+        (
+            Magnetometer(
+                sampling_rate=10, noise_density=1.0, noise_variance=1.0, seed=55
+            ),
+            55,
+        ),
     ]
+
     for sensor, seed in cases:
         assert sensor.to_dict()["seed"] == seed
         data = json.loads(json.dumps(sensor.to_dict(), cls=RocketPyEncoder))
diff --git a/tests/unit/stochastic/test_stochastic_parachute.py b/tests/unit/stochastic/test_stochastic_parachute.py
index 476384477..82cccf292 100644
--- a/tests/unit/stochastic/test_stochastic_parachute.py
+++ b/tests/unit/stochastic/test_stochastic_parachute.py
@@ -3,8 +3,8 @@
 import numpy as np
 import pytest
 
-from rocketpy.stochastic import StochasticParachute
 from rocketpy.rocket.parachute import Parachute
+from rocketpy.stochastic import StochasticParachute
 from rocketpy.stochastic.stochastic_parachute import _is_a_trigger
 
 
diff --git a/tests/unit/test_tools.py b/tests/unit/test_tools.py
index 3b8df37a3..ed2b13e48 100644
--- a/tests/unit/test_tools.py
+++ b/tests/unit/test_tools.py
@@ -22,7 +22,6 @@
     tuple_handler,
 )
 
-
 WEB_MERCATOR_EARTH_RADIUS = 6378137.0
 
 
diff --git a/tests/unit/wire/test_wire.py b/tests/unit/wire/test_wire.py
new file mode 100644
index 000000000..a8ae4ed47
--- /dev/null
+++ b/tests/unit/wire/test_wire.py
@@ -0,0 +1,184 @@
+import pytest
+
+from rocketpy.exceptions import InvalidParameterError
+from rocketpy.mathutils import Vector
+from rocketpy.plots.wire_plots import _WirePlots
+from rocketpy.rocket import Wire
+
+
+@pytest.mark.parametrize(
+    "wire_type, ignition_wire_funciton, current, extra_ignition_time",
+    [
+        (0, "motor_ignition", 1, 0.4),
+        (  # wrong wire type: number
+            "ignition",
+            None,
+            1,
+            0.4,
+        ),
+        (  # wrong ignition_wire_type: None
+            "ignition",
+            0,
+            1,
+            0.4,
+        ),
+        (  # wrong ignition_wire_type: number
+            "ignition",
+            "motor",
+            "1",
+            0.4,
+        ),
+        (  # wrong current: str
+            "ignition",
+            "motor",
+            1,
+            "0.4",
+        ),
+        (  # wrong extra_igntion_time: str
+            "ignition",
+            "motor",
+            1,
+            -0.4,
+        ),  # wrong extra_igntion_time: -
+    ],
+)
+def validate_wire_type(wire_type, ignition_wire_function, current, extra_ignition_time):
+    """Ensures that InvalidParameterError are raised with incorrect entry parameters."""
+    with pytest.raises(InvalidParameterError):
+        Wire(current, wire_type, ignition_wire_function, extra_ignition_time)
+
+
+def test_define_magnetic_field(test_communications_wire):
+    """Tests proper handling of the magnetic field calculated
+    in the _magnetic_field dictionary."""
+    position_vector = [0.003, 0.002, 1]
+    magnetic_field = [10, 25, 10]
+    test_communications_wire.define_magnetic_field(position_vector, magnetic_field)
+    list_key = list(test_communications_wire._magnetic_field)
+    assert list_key[0] == tuple(position_vector)
+    assert (
+        test_communications_wire._magnetic_field[tuple(position_vector)]
+        == magnetic_field
+    )
+    assert test_communications_wire._magnetic_field[tuple(position_vector)] == Vector(
+        magnetic_field
+    )
+
+
+def test_current_directon(calisto_with_sensors):
+    """Tests that changing direction of the current results in a magnetic field vector
+    of the same magnitude but with opposite components and the magnetic field components
+    have a correct physical meaning."""
+    horizontal_wire_1 = Wire(10, wire_type="communications", name="horizontal_wire")
+    horizontal_wire_2 = Wire(10, wire_type="communications", name="horizontal_wire")
+    calisto_with_sensors.add_wire(
+        horizontal_wire_1, [[0.001, 0.001, 0], [0.001, -0.001, 0]]
+    )
+    calisto_with_sensors.add_wire(
+        horizontal_wire_2, [[0.001, -0.001, 0], [0.001, 0.001, 0]]
+    )
+
+    horizontal_wire_1.measure_magnetic_field([0, 0, 0], frame="bacs")
+    horizontal_wire_2.measure_magnetic_field([0, 0, 0], frame="bacs")
+
+    b_field_1 = horizontal_wire_1._magnetic_field[(0, 0, 0)]
+    b_field_2 = horizontal_wire_2._magnetic_field[(0, 0, 0)]
+
+    # given the calisto_robust frame, [0, 0, 0] is the center of dry mass WITHOUT THE MOTOR,
+    # However the bacs frame in which the magnetic field is calculated is slighlty bellow along the z axis
+    # As a result, following right-hand rule the x component won't be 0, but a really small number, and in opposite directions
+    # In y axis since they are symmetrical component of both field will be 0
+    # In the z axis they will oppose since the direciton is opposite
+    assert b_field_1[0] == pytest.approx(0, abs=1e-6)
+    assert b_field_1[1] == 0
+    assert b_field_2[0] == pytest.approx(0, abs=1e-6)
+    assert b_field_2[1] == 0
+    assert b_field_1[0] == -b_field_2[0]
+    assert b_field_2[2] != 0
+    assert b_field_1[2] != 0
+    assert b_field_2[2] == -b_field_1[2]
+    assert abs(b_field_2) == abs(b_field_1)
+
+
+def test_dimension_increase(calisto_with_sensors):
+    """Tests that if the wire is closer it has a higher magnitude for the magnetic field"""
+    closer_wire = Wire(10, wire_type="communications", name="horizontal_wire")
+    farther_wire = Wire(10, wire_type="communications", name="horizontal_wire")
+    calisto_with_sensors.add_wire(closer_wire, [[0.001, 0.001, 0], [0.001, -0.001, 0]])
+    calisto_with_sensors.add_wire(farther_wire, [[0.001, 0.001, 0], [0.001, -0.001, 0]])
+
+    closer_wire.measure_magnetic_field([0, 0, 0], frame="bacs")
+    farther_wire.measure_magnetic_field([-0.4, 0, 0], frame="bacs")
+
+    b_field_closer = closer_wire._magnetic_field[(0, 0, 0)]
+    b_field_farther = farther_wire._magnetic_field[(-0.4, 0, 0)]
+    assert abs(b_field_closer) > abs(
+        b_field_farther
+    )  # closer wire must have a higher magnetic field
+
+
+@pytest.mark.parametrize(
+    "position_vector",
+    [
+        [0, 0, 0],
+        [0.002, 0.002, 0],
+        [0.001, 0.001, 0],
+        [-0.001, -0.001, 0],
+    ],
+)
+def test_raise_warning(test_communications_wire, calisto_robust, position_vector):
+    """Ensures that a warning is raised when the magnetic field measurement function
+    of the wire has as a parameter a point located along the wire line."""
+    calisto_robust.add_wire(
+        test_communications_wire,
+        position_endpoints=[[-0.003, -0.003, 0], [0.003, 0.003, 0]],
+    )
+    with pytest.warns(UserWarning):
+        test_communications_wire.measure_magnetic_field(
+            position_vector=position_vector, frame="ucs"
+        )
+
+
+def test_from_dict():
+    """Ensures from_dict returns a Wire object, whose attributes
+    are the ones passed in the dict."""
+    wire_dict = {
+        "current": 3,
+        "wire_type": "ignition",
+        "ignition_wire_function": "motor_ignition",
+        "extra_ignition_time": 2,
+    }
+    wire_from_dict = Wire.from_dict(wire_dict)
+
+    assert isinstance(wire_from_dict, Wire)
+    assert wire_from_dict.current == pytest.approx(3)
+    assert wire_from_dict.wire_type == "ignition"
+    assert wire_from_dict.ignition_wire_function == "motor_ignition"
+    assert wire_from_dict.extra_ignition_time == pytest.approx(2)
+
+
+def test_rocket_belonging(test_communications_wire, calisto_robust):
+    """Tests the belonging method of the wire works as intended."""
+    calisto_robust.add_wire(
+        test_communications_wire,
+        position_endpoints=[[0.001, 0.002, -0.3], [0.001, 0.002, 0.3]],
+    )
+    assert isinstance(test_communications_wire.plots, _WirePlots)
+    assert not isinstance(test_communications_wire._csys, type(None))
+    assert not isinstance(
+        test_communications_wire.center_of_dry_mass_position, type(None)
+    )
+
+
+def test_wire_prints_and_plots(test_communications_wire, calisto_robust):
+    """Tests the print methods of the Wire class work properly. Checks if all attributes are
+    printed and plotted correctly.
+    """
+    with pytest.raises(InvalidParameterError):
+        test_communications_wire.plots.draw()
+    calisto_robust.add_wire(
+        test_communications_wire, [[0.001, 0.002, -0.3], [0.001, 0.002, 0.3]]
+    )
+    test_communications_wire.prints.all()
+    test_communications_wire.plots.all()
+    assert True