Python CPACSInOut Examples

Example #1

File: __specs__.py Project: cfsengineering/CEASIOMpy

#!/usr/bin/env python3
# -*- coding: utf-8 -*-

from ceasiompy.utils.moduleinterfaces import CPACSInOut
from ceasiompy.utils.xpath import FUSELAGES_XPATH

# ===== CPACS inputs and outputs =====

cpacs_inout = CPACSInOut()

include_gui = False

# ----- Input -----

# * In the following example we add three (!) new entries to 'cpacs_inout'
# * Try to use (readable) loops instead of copy-pasting three almost same entries :)
for direction in ["x", "y", "z"]:
    cpacs_inout.add_input(
        var_name=direction,
        var_type=float,
        default_value=None,
        unit="1",
        descr=f"Fuselage scaling on {direction} axis",
        xpath=FUSELAGES_XPATH +
        f"/fuselage/transformation/scaling/{direction}",
        gui=include_gui,
        gui_name=f"{direction.capitalize()} scaling",
        gui_group="Fuselage scaling",
    )

cpacs_inout.add_input(

Example #2

File: __specs__.py Project: sowhatwchen/CEASIOMpy

    "name": "Range",
    "description": "Module to calculate the rage of an aircraft",
    "exec": "pwd\npython rangemain.py",
    "author": "Stefano Piccini",
    "email": "*****@*****.**",
}

CEASIOMPY_XPATH = '/cpacs/toolspecific/CEASIOMpy'
WEIGHT_XPATH = '/cpacs/toolspecific/CEASIOMpy/weight'
RANGE_XPATH = '/cpacs/toolspecific/CEASIOMpy/ranges'
FUEL_CONSUMPTION_XPATH = '/cpacs/toolspecific/CEASIOMpy/fuelConsumption'
MASSBREAKDOWN_XPATH = '/cpacs/vehicles/aircraft/model/analyses/massBreakdown'

# ===== CPACS inputs and outputs =====

cpacs_inout = CPACSInOut()

# ----- Input -----

### Masses

cpacs_inout.add_input(
    var_name='maximum_take_off_mass',
    var_type=float,
    default_value=None,
    unit='kg',
    descr='Maximum take off mass (MTOM)',
    xpath=MASSBREAKDOWN_XPATH + '/designMasses/mTOM/mass',
    gui=False,
    gui_name=None,
    gui_group=None,

Example #3

File: __specs__.py Project: cfsengineering/CEASIOMpy

# -*- coding: utf-8 -*-

from pathlib import Path

from ceasiompy.utils.moduleinterfaces import CPACSInOut
from ceasiompy.utils.xpath import REF_XPATH, WINGS_XPATH, PYTORNADO_XPATH, AEROPERFORMANCE_XPATH


# ===== Results directory path =====

RESULTS_DIR = Path("Results", "PyTornado")


# ===== CPACS inputs and outputs =====

cpacs_inout = CPACSInOut()

# ===== Input =====

cpacs_inout.add_input(
    var_name="",
    var_type=list,
    default_value=None,
    unit=None,
    descr="Name of the aero map to evaluate",
    xpath=PYTORNADO_XPATH + "/aeroMapUID",
    gui=True,
    gui_name="__AEROMAP_SELECTION",
    gui_group=None,
)

Example #4

from ceasiompy.utils.moduleinterfaces import CPACSInOut, AIRCRAFT_XPATH, CEASIOM_XPATH

# ===== RCE integration =====

RCE = {
    "name": "Optimisation module",
    "description":
    "This module implements the optimization routine for a workflow",
    "exec": "pwd\npython optimisation.py",
    "author": "Vivien Riolo",
    "email": "*****@*****.**",
}

# ===== CPACS inputs and outputs =====

cpacs_inout = CPACSInOut()

include_gui = True

# ----- Input -----

cpacs_inout.add_input(
    var_name='Objective function',
    var_type=str,
    default_value='cl',
    unit='-',
    descr="""Objective function of the optimisation problem. \n Warning !
    The parameters name must match the ones in the CSV file !""",
    xpath=CEASIOM_XPATH + '/Optimisation/objective',
    gui=include_gui,
    gui_name='Objective',

Example #5

File: __specs__.py Project: sowhatwchen/CEASIOMpy

from ceasiompy.utils.moduleinterfaces import CPACSInOut, CEASIOM_XPATH, AIRCRAFT_XPATH

# ===== RCE integration =====

RCE = {
    "name": "CLCalculator",
    "description": "Calculate required Lift coefficient to fly",
    "exec": "pwd\npython clcalculator.py",
    "author": "Aidan Jungo",
    "email": "*****@*****.**",
}

# ===== CPACS inputs and outputs =====

cpacs_inout = CPACSInOut()

# ===== Input =====

cpacs_inout.add_input(
    var_name='mtom',
    var_type=float,
    default_value=None,
    unit='kg',
    descr='Maximum take off mass (MTOM)',
    xpath=AIRCRAFT_XPATH + '/model/analyses/massBreakdown/designMasses/mTOM/mass',
    gui=False,
    gui_name=None,
    gui_group=None,
)

Example #6

File: __specs__.py Project: cfsengineering/CEASIOMpy

#!/usr/bin/env python3
# -*- coding: utf-8 -*-

from ceasiompy.utils.moduleinterfaces import CPACSInOut
from ceasiompy.utils.xpath import REF_XPATH, CLCALC_XPATH, SU2_XPATH


# ===== CPACS inputs and outputs =====

cpacs_inout = CPACSInOut()

# ===== Input =====

cpacs_inout.add_input(
    var_name="mass_type",
    var_type=list,
    default_value=["mTOM", "mZFM", "Custom", "% fuel mass"],
    unit=None,
    descr="Type of mass to use for CL calculation",
    xpath=CLCALC_XPATH + "/massType",
    gui=True,
    gui_name="Type",
    gui_group="Mass",
)

cpacs_inout.add_input(
    var_name="custom_mass",
    var_type=float,
    default_value=0.0,
    unit="kg",
    descr="Mass value if Custom is selected",

Example #7

#!/usr/bin/env python3
# -*- coding: utf-8 -*-
from pathlib import Path
from ceasiompy.utils.moduleinterfaces import CPACSInOut
from ceasiompy.utils.xpath import OPTIM_XPATH

# ===== Results directory path =====

RESULTS_DIR = Path("Results", "Optimisation")

# ===== CPACS inputs and outputs =====

cpacs_inout = CPACSInOut()

include_gui = True

# ----- Input -----

cpacs_inout.add_input(
    var_name="Objective function",
    var_type=str,
    default_value="cl",
    unit="-",
    descr="""Objective function of the optimisation problem. \n Warning !
    The parameters name must match the ones in the CSV file !""",
    xpath=OPTIM_XPATH + "/objective",
    gui=include_gui,
    gui_name="Objective",
    gui_group="Global settings",
)

Example #8

from ceasiompy.utils.moduleinterfaces import CPACSInOut, AIRCRAFT_XPATH, CEASIOM_XPATH

# ===== RCE integration =====

RCE = {
    "name": "SMUse module",
    "description":
    "This module uses a surrogate model to make predictions on data",
    "exec": "pwd\npython smuse.py",
    "author": "Vivien Riolo",
    "email": "*****@*****.**",
}

# ===== CPACS inputs and outputs =====

cpacs_inout = CPACSInOut()

include_gui = True

# ----- Input -----

cpacs_inout.add_input(var_name='model_file',
                      var_type='pathtype',
                      default_value='-',
                      descr='File that contains a trained model',
                      xpath=CEASIOM_XPATH + '/surrogateModelUse/modelFile',
                      gui=include_gui,
                      gui_name='Model to use',
                      gui_group='Prediction options')

cpacs_inout.add_input(

Example #9

File: __specs__.py Project: AlejandroRios/CEASIOMpy

from ceasiompy.utils.moduleinterfaces import CPACSInOut, AIRCRAFT_XPATH, CEASIOM_XPATH

# ===== RCE integration =====

RCE = {
    "name": "SMTrain module",
    "description": "This module generates a surrogate model",
    "exec": "pwd\npython smtrain.py",
    "author": "Vivien Riolo",
    "email": "*****@*****.**",
}

# ===== CPACS inputs and outputs =====

cpacs_inout = CPACSInOut()

include_gui = True

# ----- Input -----

cpacs_inout.add_input(
    var_name='Objectives',
    var_type=str,
    default_value='cl',
    unit='-',
    descr="""Objective function list for the surrogate model to predict \n Warning !
    The parameters name must match the ones in the CSV file !""",
    xpath=CEASIOM_XPATH+'/surrogateModel/objective',
    gui=include_gui,
    gui_name='Objective',

Example #10

File: __specs__.py Project: cfsengineering/CEASIOMpy

#!/usr/bin/env python3
# -*- coding: utf-8 -*-
from pathlib import Path

from ceasiompy.utils.moduleinterfaces import CPACSInOut
from ceasiompy.utils.xpath import SMTRAIN_XPATH

# ===== Results directory path =====

RESULTS_DIR = Path("Results", "SurrogateModels")

# ===== CPACS inputs and outputs =====

cpacs_inout = CPACSInOut()

include_gui = True

# ----- Input -----

cpacs_inout.add_input(
    var_name="Objectives",
    var_type=str,
    default_value="cl",
    unit="-",
    descr=
    """Objective function list for the surrogate model to predict \n Warning !
    The parameters name must match the ones in the CSV file !""",
    xpath=SMTRAIN_XPATH + "/objective",
    gui=include_gui,
    gui_name="Objective",
    gui_group="Global settings",

Example #11

File: __specs__.py Project: mldmnn/CEASIOMpy

from ceasiompy.utils.moduleinterfaces import CPACSInOut, AIRCRAFT_XPATH

# ===== RCE integration =====

RCE = {
    "name": "ModuleTemplate",
    "description": "This is a template module",
    "exec": "pwd\npython moduletemplate.py",
    "author": "Neil Armstrong",
    "email": "*****@*****.**",
}

# ===== CPACS inputs and outputs =====

cpacs_inout = CPACSInOut()

include_gui = False

# ----- Input -----

# * In the following example we add three (!) new entries to 'cpacs_inout'
# * Try to use (readable) loops instead of copy-pasting three almost same entries :)
for direction in ['x', 'y', 'z']:
    cpacs_inout.add_input(
        var_name=direction,
        var_type=float,
        default_value=None,
        unit='1',
        descr=f"Fuselage scaling on {direction} axis",
        xpath=AIRCRAFT_XPATH + f'/model/fuselages/fuselage/transformation/scaling/{direction}',

Example #12

File: __specs__.py Project: mldmnn/CEASIOMpy

PLOT_XPATH = '/cpacs/toolspecific/CEASIOMpy/aerodynamics/plotAeroCoefficient'

# ===== RCE integration =====

RCE = {
    "name": "PlotAeroCoef",
    "description": "Plot aerodynamic coefficient from a CPACS file",
    "exec": "pwd\npython plotaerocoef.py",
    "author": "Aidan Jungo",
    "email": "*****@*****.**",
}

# ===== CPACS inputs and outputs =====

cpacs_inout = CPACSInOut()

#===== Input =====

cpacs_inout.add_input(
    var_name='',
    var_type=list,
    default_value=None,
    descr='List of aeroMap to plot',
    xpath=PLOT_XPATH + '/aeroMapToPlot',
    gui=True,
    gui_name='__AEROMAP_CHECHBOX',
    # gui_group='Multipe aeromap'
)

cpacs_inout.add_input(var_name='alt_crit',

Example #13

#!/usr/bin/env python3
# -*- coding: utf-8 -*-
from pathlib import Path

from ceasiompy.utils.moduleinterfaces import CPACSInOut
from ceasiompy.utils.xpath import CEASIOMPY_XPATH, GEOM_XPATH, RANGE_XPATH, REF_XPATH, SU2_XPATH

# ===== Results directory path =====

RESULTS_DIR = Path("Results", "SU2")

# ===== CPACS inputs and outputs =====

cpacs_inout = CPACSInOut()

# ----- Input -----

cpacs_inout.add_input(
    var_name="aeromap_uid",
    var_type=list,
    default_value=None,
    unit=None,
    descr="Name of the aero map to calculate",
    xpath=SU2_XPATH + "/aeroMapUID",
    gui=True,
    gui_name="__AEROMAP_SELECTION",
    gui_group=None,
)

cpacs_inout.add_input(
    var_name="ref_len",

Example #14

File: __specs__.py Project: cfsengineering/CEASIOMpy

from ceasiompy.utils.moduleinterfaces import CPACSInOut
from ceasiompy.utils.xpath import (
    CAB_CREW_XPATH,
    FUEL_XPATH,
    GEOM_XPATH,
    MASSBREAKDOWN_XPATH,
    ML_XPATH,
    PASS_XPATH,
    PILOTS_XPATH,
    PROP_XPATH,
)


# ===== CPACS inputs and outputs =====

cpacs_inout = CPACSInOut()


# ----- Input -----

# User inputs ----
cpacs_inout.add_input(
    var_name="IS_DOUBLE_FLOOR",
    var_type=list,
    default_value=[0, 1, 2],
    unit=None,
    descr="0: no 2nd floor, 1: full 2nd floor (A380), 2: half 2nd floor (B747)",
    xpath=GEOM_XPATH + "/isDoubleFloor",
    gui=True,
    gui_name="Double deck",
    gui_group="User inputs",

Example #15

from ceasiompy.utils.moduleinterfaces import CPACSInOut, AIRCRAFT_XPATH

# ===== RCE integration =====

RCE = {
    "name": "PlotAeroCoef",
    "description": "Plot aerodynamic coefficient from a CPACS file",
    "exec": "pwd\npython plotaerocoef.py",
    "author": "Aidan Jungo",
    "email": "*****@*****.**",
}


# ===== CPACS inputs and outputs =====

cpacs_inout = CPACSInOut()


#===== Input =====

cpacs_inout.add_input(
    var_name='',
    var_type=list,
    default_value=None,
    descr='To which aeroMap the skin priction coef shoud be added',
    xpath='/cpacs/toolspecific/CEASIOMpy/aerodynamics/plotAeroCoefficient/aeroMapToPlot',
    gui=True,
    gui_name='__AEROMAP_CHECHBOX',
)

Example #16

File: __specs__.py Project: lverdier1/CEASIOMpy

# ===== RCE integration =====

RCE = {
    "name": "StabilityStatic",
    "description": "Determine if a vehicle is statically stable or not  ",
    "exec": "pwd\npython staticstability.py",
    "author": "Loïc Verdier",
    "email": "*****@*****.**",
}


# ===== CPACS inputs and outputs =====

cpacs_inout = CPACSInOut()


# ===== Input =====

cpacs_inout.add_input(
    var_name='',
    var_type=list,
    default_value=None,
    unit=None,
    descr="Name of the aero map to evaluate",
    xpath=STABILITY_STATIC_XPATH + '/aeroMapUid',
    gui=True,
    gui_name='__AEROMAP_SELECTION',
    gui_group='Inputs',
)

Example #17

#!/usr/bin/env python3
# -*- coding: utf-8 -*-

from ceasiompy.utils.moduleinterfaces import CPACSInOut, AIRCRAFT_XPATH

cpacs_inout = CPACSInOut()

#===== Input =====

cpacs_inout.add_input(
    var_name='x',
    default_value=None,
    unit='1',
    descr='Fuselage scalingo on x axis',
    cpacs_path=AIRCRAFT_XPATH + '/model/fuselages/fuselage/transformation   \
                                /scaling/x',
)

cpacs_inout.add_input(
    var_name='y',
    default_value=None,
    unit='1',
    descr='Fuselage scalingo on x axis',
    cpacs_path=AIRCRAFT_XPATH + '/model/fuselages/fuselage/transformation   \
                                /scaling/y',
)

cpacs_inout.add_input(
    var_name='z',
    default_value=None,
    unit='1',

Example #18

File: __specs__.py Project: mldmnn/CEASIOMpy

from ceasiompy.utils.moduleinterfaces import CPACSInOut, CEASIOM_XPATH

SKINFRICTION_PATH = CEASIOM_XPATH + '/aerodynamics/skinFriction'

# ===== RCE =====

RCE = {
    "name": "SkinFriction",
    "description": "Calculate skin friction drag coefficent",
    "exec": "pwd\npython skinfriction.py",
    "author": "Aidan Jungo",
    "email": "*****@*****.**",
}


cpacs_inout = CPACSInOut()

# ===== Input =====

cpacs_inout.add_input(
    var_name='',
    var_type=list,
    default_value=None,
    descr='To which aeroMap the skin priction coef shoud be added',
    xpath=SKINFRICTION_PATH + '/aeroMapToCalculate',
    gui=True,
    gui_name='__AEROMAP_CHECHBOX',
)

cpacs_inout.add_input(
    var_name='wetted_area',

Example #19

SU2_XPATH = '/cpacs/toolspecific/CEASIOMpy/aerodynamics/su2'

# ===== RCE integration =====

RCE = {
    "name": "SU2Run",
    "description": "Moudule to run SU2 calculation",
    "exec": "pwd\npython su2run.py",
    "author": "Aidan Jungo",
    "email": "*****@*****.**",
}

# ===== CPACS inputs and outputs =====

cpacs_inout = CPACSInOut()

# ----- Input -----

cpacs_inout.add_input(
    var_name='aeromap_uid',
    var_type=list,
    default_value=None,
    unit=None,
    descr="Name of the aero map to calculate",
    xpath=CEASIOM_XPATH + '/aerodynamics/su2/aeroMapUID',
    gui=True,
    gui_name='__AEROMAP_SELECTION',
    gui_group=None,
)

Example #20

#!/usr/bin/env python3
# -*- coding: utf-8 -*-

from ceasiompy.utils.moduleinterfaces import CPACSInOut, AIRCRAFT_XPATH, CEASIOM_XPATH

cpacs_inout = CPACSInOut()

#===== Input =====

cpacs_inout.add_input(
    var_name='ref_len',
    default_value=None,
    unit='m',
    descr='Reference length of the aircraft',
    cpacs_path=AIRCRAFT_XPATH + '/model/reference/length',
)

cpacs_inout.add_input(
    var_name='ref_area',
    default_value=None,
    unit='m^2',
    descr='Reference area of the aircraft',
    cpacs_path=AIRCRAFT_XPATH + '/model/reference/area',
)

cpacs_inout.add_input(
    var_name='cruise_alt',
    default_value=12000,
    unit='m',
    descr='Aircraft cruise altitude',
    cpacs_path=CEASIOM_XPATH + '/aerodynamics/su2/cruise_alt',

Example #21

#!/usr/bin/env python3
# -*- coding: utf-8 -*-

from pathlib import Path
from ceasiompy.utils.moduleinterfaces import CPACSInOut
from ceasiompy.utils.xpath import EXPORT_XPATH

# ===== Results directory path =====

RESULTS_DIR = Path("Results", "Aeromaps")

# ===== CPACS inputs and outputs =====

cpacs_inout = CPACSInOut()

include_gui = False

# ----- Input -----

cpacs_inout.add_input(
    var_name="",
    var_type=list,
    default_value=None,
    descr="List of aeroMap to plot",
    xpath=EXPORT_XPATH + "/aeroMapToExport",
    gui=True,
    gui_name="__AEROMAP_CHECHBOX",
    # gui_group='Multipe aeromap'
)

# ----- Output -----

Example #22

File: __specs__.py Project: mldmnn/CEASIOMpy

from ceasiompy.utils.moduleinterfaces import CPACSInOut, CEASIOM_XPATH

# ===== RCE integration =====

RCE = {
    "name": "CPACS2SUMO",
    "description": "Convert CPACS .xml file into SUMO .smx file",
    "exec": "pwd\npython cpacs2sumo.py",
    "author": "Aidan Jungo",
    "email": "*****@*****.**",
}

# ===== CPACS inputs and outputs =====

cpacs_inout = CPACSInOut()

# ----- Input -----

cpacs_inout.add_input(
    var_name='include_engine',
    var_type=bool,
    default_value=False,
    unit='1',
    descr='Convert engine from CEASIOMpy',
    xpath=CEASIOM_XPATH + '/engine/includeEngine',
    gui=True,
    gui_name='Include engine',
    gui_group='Option',
)

Example #23

File: __specs__.py Project: sowhatwchen/CEASIOMpy

from ceasiompy.utils.moduleinterfaces import CPACSInOut, AIRCRAFT_XPATH, CEASIOM_XPATH

# ===== RCE integration =====

RCE = {
    "name": "WeightUnconventional",
    "description": "Estimate weights of unconventional aircraft",
    "exec": "pwd\npython weightuncmain.py",  #Change this name
    "author": "Stefano Piccini",
    "email": "*****@*****.**",
}

# ===== CPACS inputs and outputs =====

cpacs_inout = CPACSInOut()

# ----- Input -----

# User inputs
cpacs_inout.add_input(
    var_name='IS_DOUBLE_FLOOR',
    var_type=list,
    default_value=[0, 1, 2],
    unit=None,
    descr='0: no 2nd floor, 1: full 2nd floor (A380), 2: half 2nd floor (B747)',
    xpath=CEASIOM_XPATH + '/geometry/isDoubleFloor',
    gui=True,
    gui_name='Double deck',
    gui_group='Cabin',
)

Example #24

#!/usr/bin/env python3
# -*- coding: utf-8 -*-

from ceasiompy.utils.moduleinterfaces import CPACSInOut
from ceasiompy.utils.xpath import STABILITY_STATIC_XPATH


# ===== CPACS inputs and outputs =====

cpacs_inout = CPACSInOut()


# ===== Input =====

cpacs_inout.add_input(
    var_name="",
    var_type=list,
    default_value=None,
    unit=None,
    descr="Name of the aero map to evaluate",
    xpath=STABILITY_STATIC_XPATH + "/aeroMapUid",
    gui=True,
    gui_name="__AEROMAP_SELECTION",
    gui_group="Inputs",
)

cpacs_inout.add_input(
    var_name="MassConfig",
    var_type=list,
    default_value=["mMLM", "mMRM", "mTOM", "mZFM"],
    unit="[unit]",

Example #25

File: __specs__.py Project: mldmnn/CEASIOMpy

from ceasiompy.utils.moduleinterfaces import CPACSInOut, AIRCRAFT_XPATH, CEASIOM_XPATH

# ===== RCE integration =====

RCE = {
    "name": "WeightConventional",
    "description": "Estimate weights of conventional aircraft",
    "exec": "pwd\npython weightconventional.py",
    "author": "Stefano Piccini",
    "email": "*****@*****.**",
}

# ===== CPACS inputs and outputs =====

cpacs_inout = CPACSInOut()

# ----- Input -----

# User inputs ----
cpacs_inout.add_input(
    var_name='IS_DOUBLE_FLOOR',
    var_type=list,
    default_value=[0, 1, 2],
    unit=None,
    descr='0: no 2nd floor, 1: full 2nd floor (A380), 2: half 2nd floor (B747)',
    xpath=CEASIOM_XPATH + '/geometry/isDoubleFloor',
    gui=True,
    gui_name='Double deck',
    gui_group='User inputs',
)

Example #26

# -*- coding: utf-8 -*-

from ceasiompy.utils.moduleinterfaces import CPACSInOut, AIRCRAFT_XPATH

# ===== RCE integration =====

RCE = {
    "name": "PlotAeroCoef",
    "description": "Plot aerodynamic coefficient from a CPACS file",
    "exec": "pwd\npython plotaerocoef.py",
    "author": "Aidan Jungo",
    "email": "*****@*****.**",
}

# ===== CPACS inputs and outputs =====

cpacs_inout = CPACSInOut()

#===== Input =====

cpacs_inout.add_input(
    var_name='',
    var_type=list,
    default_value=None,
    descr='List of aeroMap to plot',
    xpath=
    '/cpacs/toolspecific/CEASIOMpy/aerodynamics/plotAeroCoefficient/aeroMapToPlot',
    gui=True,
    gui_name='__AEROMAP_CHECHBOX',
)

Example #27

#!/usr/bin/env python3
# -*- coding: utf-8 -*-

from ceasiompy.utils.moduleinterfaces import CPACSInOut

cpacs_inout = CPACSInOut()

# There is are no strictly required CPACS nodes, so do not add anything to 'CPACSInOut'

Example #28

#!/usr/bin/env python3
# -*- coding: utf-8 -*-
from pathlib import Path

from ceasiompy.utils.moduleinterfaces import CPACSInOut
from ceasiompy.utils.xpath import SMUSE_XPATH

# ===== Results directory path =====

RESULTS_DIR = Path("Results", "SurrogateModels")

# ===== CPACS inputs and outputs =====

cpacs_inout = CPACSInOut()

include_gui = True

# ----- Input -----

cpacs_inout.add_input(
    var_name="model_file",
    var_type="pathtype",
    default_value="-",
    descr="File that contains a trained model",
    xpath=SMUSE_XPATH + "/modelFile",
    gui=include_gui,
    gui_name="Model to use",
    gui_group="Prediction options",
)

cpacs_inout.add_input(

Example #29

from ceasiompy.utils.moduleinterfaces import CPACSInOut, CEASIOM_XPATH

# ===== RCE integration =====

RCE = {
    "name": "SUMOAutoMesh",
    "description": "Module to generate a SUMO mesh automatically",
    "exec": "pwd\npython sumoautomesh.py",
    "author": "Aidan Jungo",
    "email": "*****@*****.**",
}


# ===== CPACS inputs and outputs =====

cpacs_inout = CPACSInOut()


# ----- Input -----

cpacs_inout.add_input(
    var_name='sumo_file_path',
    var_type='pathtype',
    default_value='-',
    unit='1',
    descr='Absolute path to the SUMO file',
    xpath=CEASIOM_XPATH + '/filesPath/sumoFilePath',
    gui=True,
    gui_name='SUMO File path',
    gui_group='Inputs',
)

Example #30

File: __specs__.py Project: nuaalht/CEASIOMpy

from ceasiompy.utils.moduleinterfaces import CPACSInOut, AIRCRAFT_XPATH, CEASIOM_XPATH

# ===== RCE integration =====

RCE = {
    "name": "Predictive tool module",
    "description":
    "This module builds a surrogate model to make predictions on data",
    "exec": "pwd\npython prediction.py",
    "author": "Vivien Riolo",
    "email": "-",
}

# ===== CPACS inputs and outputs =====

cpacs_inout = CPACSInOut()

include_gui = True

# ----- Input -----

cpacs_inout.add_input(
    var_name='Objectives',
    var_type=str,
    default_value='cl/cd,cl',
    unit='-',
    descr=
    """Objective function list for the surrogate model to predict \n Warning ! 
    The parameters name must match the ones in the CSV file !""",
    xpath=CEASIOM_XPATH + '/SurrogateModel/objective',
    gui=include_gui,