StochasticNoseCone does not support "powerseries" nose cones

[cazzopardi]

Describe the bug

The StochasticNoseCone class does not support nose cones of kind 'powerseries' as the constructor does not accept a power parameter.

To Reproduce

Attempt to call simulate() on any Monte Carlo simulation object that was initialised with a nose cone of kind "powerseries". The following is an example modified from the documentation:

import datetime

from rocketpy import Environment, Flight, Function, MonteCarlo, Rocket, SolidMotor
from rocketpy.stochastic import (
    StochasticEnvironment,
    StochasticFlight,
    StochasticNoseCone,
    StochasticParachute,
    StochasticRailButtons,
    StochasticRocket,
    StochasticSolidMotor,
    StochasticTail,
    StochasticTrapezoidalFins,
)
# Environment
env = Environment(latitude=39.389700, longitude=-8.288964, elevation=113)
tomorrow = datetime.date.today() + datetime.timedelta(days=1)
env.set_date((tomorrow.year, tomorrow.month, tomorrow.day, 12))
env.set_atmospheric_model(type="Ensemble", file="GEFS")

# Motor
motor = SolidMotor(
    thrust_source="Data/K1102.eng",
    dry_mass=1.815,
    dry_inertia=(0.125, 0.125, 0.002),
    nozzle_radius=33 / 1000,
    grain_number=5,
    grain_density=1815,
    grain_outer_radius=33 / 1000,
    grain_initial_inner_radius=15 / 1000,
    grain_initial_height=120 / 1000,
    grain_separation=5 / 1000,
    grains_center_of_mass_position=0.397,
    center_of_dry_mass_position=0.317,
    nozzle_position=0,
    burn_time=3.9,
    throat_radius=11 / 1000,
    coordinate_system_orientation="nozzle_to_combustion_chamber",
)
print(f"Total Impulse of the Solid Motor: {motor.total_impulse} Ns")

drag_curve = Function("Data/cleaned_drag.csv")
# Rocket
rocket = Rocket(
    radius=127 / 2000,
    mass=14.426,
    inertia=(6.321, 6.321, 0.034),
    power_off_drag=drag_curve,
    power_on_drag=drag_curve,
    center_of_mass_without_motor=0,
    coordinate_system_orientation="tail_to_nose",
)

rail_buttons = rocket.set_rail_buttons(
    upper_button_position=0.0818,
    lower_button_position=-0.618,
    angular_position=45,
)

rocket.add_motor(motor, position=-1.255)

nose_cone = rocket.add_nose(length=0.55829, kind="powerseries", power=0.7, position=1.278)

fin_set = rocket.add_trapezoidal_fins(
    n=4,
    root_chord=0.120,
    tip_chord=0.060,
    span=0.110,
    position=-1.04956,
    cant_angle=0.5,
)

tail = rocket.add_tail(
    top_radius=0.0635, bottom_radius=0.0435, length=0.060, position=-1.194656
)
Main = rocket.add_parachute(
    "Main",
    cd_s=10.0,
    trigger=800,
    sampling_rate=105,
    lag=1.5,
    noise=(0, 8.3, 0.5),
)

Drogue = rocket.add_parachute(
    "Drogue",
    cd_s=1.0,
    trigger="apogee",
    sampling_rate=105,
    lag=1.5,
    noise=(0, 8.3, 0.5),
)

# Flight
test_flight = Flight(
    rocket=rocket,
    environment=env,
    rail_length=5,
    inclination=84,
    heading=133,
)
stochastic_env = StochasticEnvironment(
    environment=env,
    ensemble_member=list(range(env.num_ensemble_members)),
)

stochastic_env.visualize_attributes()
wind_speed_at_1000m = []
for i in range(5):
    rnd_env = stochastic_env.create_object()
    wind_speed_at_1000m.append(rnd_env.wind_velocity_x(1000))

print(wind_speed_at_1000m)
stochastic_motor = StochasticSolidMotor(
    solid_motor=motor,
    burn_start_time=(0, 0.1, "binomial"),
    grains_center_of_mass_position=0.001,
    grain_density=50,
    grain_separation=1 / 1000,
    grain_initial_height=1 / 1000,
    grain_initial_inner_radius=0.375 / 1000,
    grain_outer_radius=0.375 / 1000,
    total_impulse=(6500, 1000),
    throat_radius=0.5 / 1000,
    nozzle_radius=0.5 / 1000,
    nozzle_position=0.001,
)
stochastic_motor.visualize_attributes()
total_impulse = []
for i in range(5):
    rnd_motor = stochastic_motor.create_object()
    total_impulse.append(rnd_motor.total_impulse)

print(total_impulse)
stochastic_rocket = StochasticRocket(
    rocket=rocket,
    radius=0.0127 / 2000,
    mass=(15.426, 0.5, "normal"),
    inertia_11=(6.321, 0),
    inertia_22=0.01,
    inertia_33=0.01,
    center_of_mass_without_motor=0,
)
stochastic_rocket.visualize_attributes()

stochastic_nose_cone = StochasticNoseCone(
    nosecone=nose_cone,
    length=0.001,
)

stochastic_fin_set = StochasticTrapezoidalFins(
    trapezoidal_fins=fin_set,
    root_chord=0.0005,
    tip_chord=0.0005,
    span=0.0005,
)

stochastic_tail = StochasticTail(
    tail=tail,
    top_radius=0.001,
    bottom_radius=0.001,
    length=0.001,
)

stochastic_rail_buttons = StochasticRailButtons(
    rail_buttons=rail_buttons, buttons_distance=0.001
)

stochastic_main = StochasticParachute(
    parachute=Main,
    cd_s=0.1,
    lag=0.1,
)

stochastic_drogue = StochasticParachute(
    parachute=Drogue,
    cd_s=0.07,
    lag=0.2,
)
stochastic_rocket.add_motor(stochastic_motor, position=0.001)
stochastic_rocket.add_nose(stochastic_nose_cone, position=(1.134, 0.001))
stochastic_rocket.add_trapezoidal_fins(stochastic_fin_set, position=(0.001, "normal"))
stochastic_rocket.add_tail(stochastic_tail)
stochastic_rocket.set_rail_buttons(
    stochastic_rail_buttons, lower_button_position=(0.001, "normal")
)
stochastic_rocket.add_parachute(stochastic_main)
stochastic_rocket.add_parachute(stochastic_drogue)

stochastic_flight = StochasticFlight(
    flight=test_flight,
    inclination=(84.7, 1),  # mean= 84.7, std=1
    heading=(53, 2),  # mean= 53, std=2
)
test_dispersion = MonteCarlo(
    filename="monte_carlo_analysis_outputs/monte_carlo_class_example",
    environment=stochastic_env,
    rocket=stochastic_rocket,
    flight=stochastic_flight,
)
test_dispersion.simulate(
    number_of_simulations=10,
    append=False,
    include_function_data=False,
    parallel=False,
    n_workers=4,
)

Expected behavior

Simulation should run normally. Currently, this results in:

ValueError: Parameter 'power' cannot be None when using a nose cone kind 'powerseries'.