def wipe_design():
value = {}
try:
database.write_aircraft_specification(value)
except:
pass
try:
database.write_datcom_stability_specification(value)
except:
pass
try:
database.write_structures_specification(value)
except:
pass
try:
database.write_aerodynamic_results(value)
except:
pass
try:
database.write_control_specifications(value)
except:
pass
try:
database.write_stability_specification(value)
except:
pass
def init_action(self):
self.accept_inputs()
self.parameters = {
lifting_surface: {
str(self.text): {
design_type: self.design_type_,
surface_type: self.surface_type_,
root_le_position_x: float(self.Wing_postion_x_text.text()),
root_le_position_y: float(self.Wing_postion_y_text.text()),
root_le_position_z: float(self.Wing_postion_z_text.text()),
span: float(self.span_text.text()),
profile: str(self.wing_profile_selection),
chord: float(self.chord_length_text.text()),
taper_ratio: float(self.taper_ratio_text.text()),
sweep: float(self.sweep_angle_text.text()),
dihedral: float(self.dihedral_angle_text.text()),
twist: float(self.twist_angle_text.text()),
}
}
}
try:
print(self.parameters)
database.update_aircraft_specifications(
key=lifting_surface, value=self.parameters[lifting_surface])
except:
database.write_aircraft_specification(self.parameters)
return self.parameters
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 write_control_surface_to_objects(surface_name="",parent__=""):
data = database.read_aircraft_specifications()
try:
val = data[objects]
val[surface_name] = {surface_name: {parent_:parent__}}
except Exception as e:
logging.error(e)
data.update({objects: {surface_name: {parent_:parent__}}})
database.write_aircraft_specification(data)
def delete_control_surface_from_objects(surface_name=""):
data = database.read_aircraft_specifications()
try:
array = data[objects]
array.pop(surface_name)
data[objects] = array
except:
pass
database.write_aircraft_specification(data)
def delete_control_surface_objects(value=""):
data = database.read_aircraft_specifications()
try:
array = data[control_surface_objects]
array.remove(value)
data[control_surface_objects] = array
except:
pass
database.write_aircraft_specification(data)
def write_boom_objects(value=""):
data = database.read_aircraft_specifications()
try:
array = data[boom_objects]
if not array.__contains__(value):
array.append(value)
data[boom_objects] = array
except:
data.update({boom_objects: [value]})
database.write_aircraft_specification(data)
def write_control_surface_objects(value=""):
data = database.read_aircraft_specifications()
try:
array = data[control_surface_objects]
if not array.__contains__(value):
array.append(value)
data[control_surface_objects] = array
except Exception as e:
data.update({control_surface_objects: [value]})
database.write_aircraft_specification(data)
def write_boom_to_objects(boom_name="", boom_type_="", design_type_=""):
data = database.read_aircraft_specifications()
try:
val = data[objects]
val[boom_name] = {boom_type: boom_type_, design_type: design_type_}
except Exception as e:
logging.error(e)
data.update({
objects: {
boom_name: {
boom_type: boom_type_,
design_type: design_type_
}
}
})
database.write_aircraft_specification(data)
def write_lifting_surface_to_objects(surface_name="",
surface_type_="",
design_type_=""):
data = database.read_aircraft_specifications()
try:
val = data[objects]
val[surface_name] = {
surface_type: surface_type_,
design_type: design_type_
}
except Exception as e:
logging.error(e)
data.update({
objects: {
surface_name: {
surface_type: surface_type_,
design_type: design_type_
}
}
})
database.write_aircraft_specification(data)
def init_action(self):
self.parameters = {
control_surface: {
self.name: {
root_le_position_x:
float(self.vtp_position_x_text.text()),
root_le_position_y:
float(self.vtp_position_y_text.text()),
root_le_position_z:
float(self.Wing_postion_z_text.text()),
parent_:
self.selection_ if self.selection_ is not None else
read_lifting_surface_objects()[
self.itemsComboBox.currentIndex()],
span:
float(self.span_text.text()),
rotation_x:
float(self.rotation_x_text.text()),
rotation_y:
float(self.rotation_y_text.text()),
rotation_z:
float(self.rotation_z_text.text()),
chord:
float(self.chord_length_text.text()),
}
}
}
try:
database.update_aircraft_specifications(
key=control_surface, value=self.parameters[control_surface])
except:
database.write_aircraft_specification(self.parameters)
write_control_surface_objects(value=self.name)
write_control_surface_to_objects(
surface_name=self.name,
parent__=self.selection_ if self.selection_ is not None else
read_lifting_surface_objects()[self.itemsComboBox.currentIndex()])
return self.parameters
def init_action(self):
if self.landing_gear_type.text() == "c" or self.landing_gear_type.text(
) == "t":
self.parameters = {
landing_gear: {
landing_gear_type:
self.landing_gear_type.text(),
struct_length_main_gear:
float(self.struct_length_main_gear.text()),
struct_length_aux:
float(self.struct_length_aux.text()),
tire_diameter:
float(self.tire_diameter_text.text()),
wheel_diameter:
float(self.wheel_diameter_text.text()),
aux_gear_position_x:
float(self.aux_gear_position_x_text.text()),
aux_gear_position_y:
float(self.aux_gear_position_y_text.text()),
aux_gear_position_z:
float(self.aux_gear_position_z_text.text()),
rol_gear_position_x:
float(self.rol_gear_position_x_text.text()),
rol_gear_position_y:
float(self.rol_gear_position_y_text.text()),
rol_gear_position_z:
float(self.rol_gear_position_z_text.text())
}
}
try:
database.update_aircraft_specifications(
key=landing_gear, value=self.parameters[landing_gear])
except:
database.write_aircraft_specification(self.parameters)
return self.parameters
else:
raise AttributeError("You cannot add instance attributes to %s" %
self)
def init_action(self):
self.accept_inputs()
self.parameters = {
boom: {
self._name: {
design_type:
self.design_type_,
boom_type:
self.boom_type_,
boom_length:
float(
get_fuselage_length([
float(self.nose_length_text.text()),
float(self.section_1_length_text.text()),
float(self.section_2_length_text.text()),
float(self.section_3_length_text.text()),
float(self.tail_length_text.text())
])),
boom_diameter:
float(
get_diameter([
float(self.nose_width_text.text()),
float(self.section_1_width_text.text()),
float(self.section_2_width_text.text()),
float(self.section_3_width_text.text()),
float(self.tail_width_text.text()),
float(self.tip_width_text.text())
])),
nose_width:
float(self.nose_width_text.text()),
nose_height:
float(self.nose_height_text.text()),
nose_profile:
str(self.nose_profile_selection),
nose_length:
float(self.nose_length_text.text()),
nose_position_z:
float(self.nose_position_z_text.text()),
nose_tip_position:
float(self.nose_tip_position_text.text()),
design_cockpit:
self.cockpitCheckMark,
xy_mirror:
self.xy_mirror_,
xz_mirror:
self.xz_mirror_,
yz_mirror:
self.yz_mirror_,
root_position_x:
float(self.root_le_position_x_text.text()),
root_position_y:
float(self.root_le_position_y_text.text()),
root_position_z:
float(self.root_le_position_z_text.text()),
section_1_length:
float(self.section_1_length_text.text()),
section_1_width:
float(self.section_1_width_text.text()),
section_1_height:
float(self.section_1_height_text.text()),
section_1_profile:
str(self.section_1_profile_selection),
section_1_position_z:
float(self.section_1_position_z_text.text()),
section_2_length:
float(self.section_2_length_text.text()),
section_2_width:
float(self.section_2_width_text.text()),
section_2_height:
float(self.section_2_height_text.text()),
section_2_profile:
str(self.section_2_profile_selection),
section_2_position_z:
float(self.section_2_position_z_text.text()),
section_3_length:
float(self.section_3_length_text.text()),
section_3_width:
float(self.section_3_width_text.text()),
section_3_height:
float(self.section_3_height_text.text()),
section_3_profile:
str(self.section_3_profile_selection),
section_3_position_z:
float(self.section_3_position_z_text.text()),
tip_width:
float(self.tip_width_text.text()),
tip_height:
float(self.tip_height_text.text()),
tail_profile:
str(self.tail_profile_selection),
tail_tip_position:
float(self.tail_tip_position_text.text()),
tail_length:
float(self.tail_length_text.text()),
tail_width:
float(self.tail_width_text.text()),
tail_height:
float(self.tail_height_text.text()),
tail_position_z:
float(self.tail_position_z_text.text()),
}
}
}
if self.cockpitCheckMark == True:
self.parameters[boom][self._name].update({
cockpit_height:
float(self.cockpit_height_text.text()),
cockpit_width:
float(self.cockpit_width_text.text()),
cockpit_length:
float(self.cockpit_length_text.text()),
cockpit_position_x:
float(self.cockpit_position_x_text.text()),
cockpit_position_y:
float(self.cockpit_position_y_text.text()),
cockpit_position_z:
float(self.cockpit_position_z_text.text()),
})
else:
self.parameters[boom][self._name].update({
cockpit_height:
float(0),
cockpit_width:
float(0),
cockpit_length:
float(0),
cockpit_position_x:
float(0),
cockpit_position_y:
float(0),
cockpit_position_z:
float(0),
})
try:
database.update_aircraft_specifications(
key=boom, value=self.parameters[boom])
except:
database.write_aircraft_specification(self.parameters)
return self.parameters
def init_action(self):
self.parameters = {
boom: {
self.text: {
design_type:
self.design_type_,
boom_type:
self.boom_type_,
fuselage_length:
float(
get_fuselage_length([
float(self.nose_length_text.text()),
float(self.section_1_length_text.text()),
float(self.section_2_length_text.text()),
float(self.section_3_length_text.text()),
float(self.tail_length_text.text())
])),
fuselage_diameter:
float(
get_diameter([
float(self.nose_radius_text.text()),
float(self.section_1_radius_text.text()),
float(self.section_2_radius_text.text()),
float(self.section_3_radius_text.text()),
float(self.tail_radius_text.text()),
float(self.tip_radius_text.text())
])),
nose_width:
float(self.nose_radius_text.text()),
nose_length:
float(self.nose_length_text.text()),
nose_position_z:
float(self.nose_position_z_text.text()),
nose_tip_position:
float(self.nose_tip_position_text.text()),
design_cockpit:
self.cockpitCheckMark,
section_1_length:
float(self.section_1_length_text.text()),
section_1_width:
float(self.section_1_radius_text.text()),
section_1_position_z:
float(self.section_1_position_z_text.text()),
section_2_length:
float(self.section_2_length_text.text()),
section_2_width:
float(self.section_2_radius_text.text()),
section_2_position_z:
float(self.section_2_position_z_text.text()),
section_3_length:
float(self.section_3_length_text.text()),
section_3_width:
float(self.section_3_radius_text.text()),
section_3_position_z:
float(self.section_3_position_z_text.text()),
tip_width:
float(self.tip_radius_text.text()),
tail_tip_position:
float(self.tail_tip_position_text.text()),
tail_length:
float(self.tail_length_text.text()),
tail_width:
float(self.tail_radius_text.text()),
tail_position_z:
float(self.tail_position_z_text.text()),
}
}
}
if self.cockpitCheckMark == True:
self.parameters[boom][self.text].update({
cockpit_height:
float(self.cockpit_height_text.text()),
cockpit_width:
float(self.cockpit_width_text.text()),
cockpit_length:
float(self.cockpit_length_text.text()),
cockpit_position_x:
float(self.cockpit_position_x_text.text()),
cockpit_position_y:
float(self.cockpit_position_y_text.text()),
cockpit_position_z:
float(self.cockpit_position_z_text.text()),
})
else:
self.parameters[boom][self.text].update({
cockpit_height:
float(0),
cockpit_width:
float(0),
cockpit_length:
float(0),
cockpit_position_x:
float(0),
cockpit_position_y:
float(0),
cockpit_position_z:
float(0),
})
try:
database.update_aircraft_specifications(
key=boom, value=self.parameters[boom])
except:
database.write_aircraft_specification(self.parameters)
return self.parameters
def init_action(self):
self.accept_inputs()
self.parameters = {
lifting_surface: {
str(self._name): {
design_type:
self.design_type_,
surface_type:
self.surface_type_,
root_le_position_x:
float(self.root_le_position_x_text.text()),
root_le_position_y:
float(self.root_le_position_y_text.text()),
root_le_position_z:
float(self.root_le_position_z_text.text()),
xy_mirror:
self.xy_mirror_,
xz_mirror:
self.xz_mirror_,
yz_mirror:
self.yz_mirror_,
profile:
str(self.wing_profile_selection),
surface_curve_type:
self.surface_curve_type_,
rotation_x:
float(self.rotation_x_text.text()),
rotation_y:
float(self.rotation_y_text.text()),
rotation_z:
float(self.rotation_z_text.text()),
section_1_x:
float(self.section_1_x_text.text()),
section_1_y:
float(self.section_1_y_text.text()),
section_1_z:
float(self.section_1_z_text.text()),
section_1_chord:
float(self.section_1_chord_text.text()),
section_1_twist_angle:
float(self.section_1_twist_angle_text.text()),
section_2_x:
float(self.section_2_x_text.text()),
section_2_y:
float(self.section_2_y_text.text()),
section_2_z:
float(self.section_2_z_text.text()),
section_2_chord:
float(self.section_2_chord_text.text()),
section_2_twist_angle:
float(self.section_2_twist_angle_text.text()),
section_3_x:
float(self.section_3_x_text.text()),
section_3_y:
float(self.section_3_y_text.text()),
section_3_z:
float(self.section_3_z_text.text()),
section_3_chord:
float(self.section_3_chord_text.text()),
section_3_twist_angle:
float(self.section_3_twist_angle_text.text()),
section_4_x:
float(self.section_4_x_text.text()),
section_4_y:
float(self.section_4_y_text.text()),
section_4_z:
float(self.section_4_z_text.text()),
section_4_chord:
float(self.section_4_chord_text.text()),
section_4_twist_angle:
float(self.section_4_twist_angle_text.text()),
section_5_x:
float(self.section_5_x_text.text()),
section_5_y:
float(self.section_5_y_text.text()),
section_5_z:
float(self.section_5_z_text.text()),
section_5_chord:
float(self.section_5_chord_text.text()),
section_5_twist_angle:
float(self.section_5_twist_angle_text.text()),
}
}
}
try:
database.update_aircraft_specifications(
key=lifting_surface, value=self.parameters[lifting_surface])
except:
database.write_aircraft_specification(self.parameters)
return self.parameters
