def setUp(self):
self.airplane = get_airplane_data('b734')
import matplotlib.pyplot as plt
from toa.data import get_airplane_data
from toa.runway import Runway
from toa.traj.aeo_non_optimized import run_takeoff
from toa.utils.plotting_non import plot_results
from toa.utils.validation import validate_result
runway = Runway(2500, 0.0, 0.0, 0.0, 0.00)
airplane = get_airplane_data('b734')
flap_angle = 5
p, sim = run_takeoff(airplane, runway, flap_angle=flap_angle, wind_speed=0.0)
validate_result(p, airplane, runway, flap_angle)
plot_results(p, sim)
def setUp(self) -> None:
self.airplane_744 = get_airplane_data('b744')
self.airplane_734 = get_airplane_data('b734')
