def test_check():
plane_parameters = get_plane_parameters()
plane = Plane(plane_parameters)
stability_analisys = FlightStability(plane)
stability_analisys.static_margin()
plane_SMChecker = StaticMarginChecker(plane)
plane_SMChecker.check()
npt.assert_almost_equal(plane_SMChecker.plane.positive_sm_for_positive_alphas, True)
def test_measure():
plane_parameters = get_plane_parameters()
plane = Plane(plane_parameters)
plane_dimensions = Ruler(plane)
plane_dimensions.measure()
dimensions_check = 3.602
npt.assert_almost_equal(plane_dimensions.plane.total_dimensions,
dimensions_check,
decimal=3)
npt.assert_equal(plane_dimensions.plane.dimensions_are_good, True)
def takeoff(plot=True):
plane_parameters = parameters.get_plane_parameters()
performance_data = parameters.get_performance_parameters()
plane = Plane(plane_parameters)
takeoff_analysis = Takeoff(plane, performance_data)
mtow = takeoff_analysis.get_mtow()
print("Final MTOW is {}".format(mtow))
print("V_takeoff : ", plane.V_takeoff)
if plot == True:
plot_takeoff_data(takeoff_analysis, mtow)
plt.show()
def power_curves(mtow, plot=True):
plane_parameters = parameters.get_plane_parameters()
performance_data = parameters.get_performance_parameters()
plane = Plane(plane_parameters)
plane.mtow = mtow
power_analysis = Power(plane, performance_data)
plane.show_plane()
if plot == True:
print("V_max : ", plane.V_max)
print("V_min : ", plane.V_min)
plot_power_curves(power_analysis)
plt.show()
def plane():
plane_parameters = get_plane_parameters()
plane = Plane(plane_parameters)
return plane
import ADR
from ADR import parameters
if __name__ == "__main__":
plane_parameters = parameters.get_plane_parameters()
performance_parameters = parameters.get_performance_parameters()
ADR.analyzer(plane_parameters, performance_parameters, plot=True)