Compare Flights example

%load_ext autoreload
%autoreload 2

%matplotlib inline

Importing libraries

from rocketpy.plots.compare import CompareFlights
from rocketpy import Environment, Flight, Rocket, SolidMotor
from datetime import datetime, timedelta

Creating the Flight objects

First, let’s create the environment, motor and rocket objects.

after_tomorrow = datetime.now() + timedelta(days=2)
env = Environment(latitude=-23, longitude=-49, date=after_tomorrow)
env.set_atmospheric_model(type="Forecast", file="GFS")

Pro75M1670 =  SolidMotor(
    thrust_source="../../data/motors/Cesaroni_M1670.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",
)

calisto = Rocket(
    radius=127 / 2000,
    mass=14.426,
    inertia=(6.321, 6.321, 0.034),
    power_off_drag="../../data/calisto/powerOffDragCurve.csv",
    power_on_drag="../../data/calisto/powerOnDragCurve.csv",
    center_of_mass_without_motor=0,
    coordinate_system_orientation="tail_to_nose",
)

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

calisto.add_motor(Pro75M1670, position=-1.255)

nosecone = calisto.add_nose(
    length=0.55829, kind="vonKarman", position=1.278
)

fin_set = calisto.add_trapezoidal_fins(
    n=4,
    root_chord=0.120,
    tip_chord=0.060,
    span=0.110,
    position=-1.04956,
    cant_angle=0.5,
    airfoil=("../../data/calisto/NACA0012-radians.csv","radians"),
)

tail = calisto.add_tail(
    top_radius=0.0635, bottom_radius=0.0435, length=0.060, position=-1.194656
)


def drogue_trigger(p, h, y):
    # p = pressure considering parachute noise signal
    # h = height above ground level considering parachute noise signal
    # y = [x, y, z, vx, vy, vz, e0, e1, e2, e3, w1, w2, w3]

    # activate drogue when vz < 0 m/s.
    return True if y[5] < 0 else False


def main_trigger(p, h, y):
    # p = pressure considering parachute noise signal
    # h = height above ground level considering parachute noise signal
    # y = [x, y, z, vx, vy, vz, e0, e1, e2, e3, w1, w2, w3]

    # activate main when vz < 0 m/s and z < 800 m
    return True if y[5] < 0 and h < 800 else False


Main = calisto.add_parachute(
    "Main",
    cd_s=10.0,
    trigger=main_trigger,
    sampling_rate=105,
    lag=1.5,
    noise=(0, 8.3, 0.5),
)

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

Now we can create different flights varying the launch angle and the rail inclination:

inclinations = [85, 75, 60]
headings = [90, 135]
flights = []

for heading in headings:
    for inclination in inclinations:
        flight = Flight(
            environment=env,
            rocket=calisto,
            rail_length=5.2,
            inclination=inclination,
            heading=heading,
            name=f"Incl {inclination} Head {heading}",
        )
        flights.append(flight)

print("Number of flights: ", len(flights))

Number of flights:  6

Start the comparison

comparison = CompareFlights(flights)

Linear Kinematics

comparison.trajectories_3d(legend=True)

comparison.positions()

comparison.trajectories_2d(plane="xy", legend=True)

comparison.velocities()

comparison.stream_velocities()

comparison.accelerations()

Angular kinematics

comparison.angular_velocities()

comparison.angular_accelerations()

Attitudes

comparison.attitude_angles()

comparison.euler_angles()

comparison.quaternions()

comparison.angles_of_attack()

Forces and Moments

comparison.aerodynamic_forces()

comparison.aerodynamic_moments()

# comparison.rail_buttons_forces() # Currently not working!

Energies and Power

comparison.fluid_mechanics()

comparison.energies()

comparison.powers()

Plotting everything together

Alternatively, we can plot all the results together by calling one simple method:

comparison.all()

This method is not implemented yet

This method is not implemented yet