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')