def set_mass_of_payload(value=0.0):
data = database.read_structures_specifications()
try:
data[mass_of_payload] = value
database.write_structures_specification(data)
except Exception as e:
logging.error(e)
data.update({mass_of_payload: value})
database.write_structures_specification(data)
def set_maximum_takeoff_weight(value=0.0):
data = database.read_structures_specifications()
try:
data[maximum_takeoff_weight] = value
database.write_aircraft_specification(data)
except Exception as e:
logging.error(e)
data.update({maximum_takeoff_weight: value})
database.write_structures_specification(data)
def set_mass_of_fuselage(value=0.0):
data = database.read_structures_specifications()
try:
data[mass_of_fuselage] = value
database.write_aircraft_specification(data)
except Exception as e:
logging.error(e)
data.update({mass_of_fuselage: value})
database.write_structures_specification(data)
def get_moments_of_inertia():
try:
value = database.read_structures_specifications()[moments_of_inertia]
return value
except Exception as e:
dialog = QMessageBox()
dialog.setIcon(QMessageBox.Warning)
dialog.setText(f"{e.__str__()}")
dialog.addButton(QMessageBox.Ok)
dialog.exec()
def get_center_of_mass():
try:
value = database.read_structures_specifications()[center_of_gravity]
return value
except:
dialog = QMessageBox()
dialog.setIcon(QMessageBox.Warning)
dialog.setText(f"{e.__str__()}")
dialog.addButton(QMessageBox.Ok)
dialog.exec()
def set_moments_of_inertia(value=None):
if value is None:
value = {}
data = database.read_structures_specifications()
try:
data[moments_of_inertia].update(value)
database.write_structures_specification(data)
except Exception as e:
logging.error(e)
data.update({moments_of_inertia: value})
database.write_structures_specification(data)
def set_center_of_mass(value=None):
if value is None:
value = {}
data = database.read_structures_specifications()
try:
data[center_of_gravity].update(value)
database.write_structures_specification(data)
except Exception as e:
logging.error(e)
data.update({center_of_gravity: value})
database.write_structures_specification(data)
def set_mass_of_engine_or_motor(value=None):
if value is None:
value = {}
data = database.read_structures_specifications()
try:
data[mass_of_engine_or_motor].update(value)
database.write_structures_specification(data)
except Exception as e:
logging.error(e)
data.update({mass_of_battery_or_fuel: value})
database.write_structures_specification(
{mass_of_engine_or_motor: value})
def get_structures_specifications():
value = database.read_structures_specifications()
mass_of_battery_or_fuel_ = value[mass_of_battery_or_fuel]
maximum_takeoff_weight_ = value[maximum_takeoff_weight]
mass_of_payload_ = value[mass_of_payload]
mass_of_engine_or_motor_ = value[mass_of_engine_or_motor]
return mass_of_battery_or_fuel_,\
mass_of_engine_or_motor_,\
maximum_takeoff_weight_, \
mass_of_payload_, \
def exportValues():
output = ""
for major_key in database.read_datcom_stability_specifications().keys():
for key in database.read_datcom_stability_specifications(
)[major_key].keys():
alpha_, velocity_, y = read_datcom_table_data(type_=datcom_data,
major_key=major_key,
key=key)
try:
value = y[alpha_.index(0)]
except:
value = 0
output = output + f"{key}:{value},"
for key, value in database.read_propulsion_specifications(
)["propulsion_dialogs"].items():
output = output + f"{key}:{value},"
for key, value in database.read_structures_specifications().items():
try:
for k, v in value.items():
output = output + f"{k}:{v},"
except:
output = output + f"{key}:{value},"
writeTxt(sim_export_txt_dir, output)
def get_mass_of_engine_or_motor():
return database.read_structures_specifications()[mass_of_engine_or_motor]
def get_mass_of_battery_or_fuel():
return database.read_structures_specifications()[mass_of_battery_or_fuel]
def get_maximum_takeoff_weight():
return database.read_structures_specifications()[maximum_takeoff_weight]
def get_mass_of_fuselage():
return database.read_structures_specifications()[mass_of_fuselage]
def get_mass_of_wing():
return database.read_structures_specifications()[mass_of_wing]
def get_mass_of_payload():
return database.read_structures_specifications()[mass_of_payload]
