Usage 

FAST-OAD uses a configuration file for defining your OAD problem. You can interact with this problem using command line or Python directly.

You may also use some lower-level features of FAST-OAD to interact with OpenMDAO systems. This part is addressed in the API documentation.

Contents

FAST-OAD configuration file 

FAST-OAD configuration files are in YAML format. A quick tutorial for YAML (among many ones) is available here

title: Sample OAD Process

# List of folder paths where user added custom registered OpenMDAO components
module_folders:

# Input and output files
input_file: ./problem_inputs.xml
output_file: ./problem_outputs.xml

# Definition of problem driver assuming the OpenMDAO convention "import openmdao.api as om"
driver: om.ScipyOptimizeDriver(tol=1e-2, optimizer='COBYLA')

# Definition of OpenMDAO model
# Although "model" is a mandatory name for the top level of the model, its
# sub-components can be freely named by user
model:

  #  Solvers are defined assuming the OpenMDAO convention "import openmdao.api as om"
  nonlinear_solver: om.NonlinearBlockGS(maxiter=100, atol=1e-2)
  linear_solver: om.DirectSolver()


  # Components can be put in sub-groups
  subgroup:

    # A group can be set with its own solvers.

    nonlinear_solver: om.NonlinearBlockGS(maxiter=100, atol=1e-2, iprint=0)
    linear_solver: om.DirectSolver()

    geometry:
      # An OpenMDAO component is identified by its "id"
      id: fastoad.geometry.legacy
    weight:
      id: fastoad.weight.legacy
    mtow:
      id: fastoad.mass_performances.compute_MTOW
    hq_tail_sizing:
      id: fastoad.handling_qualities.tail_sizing
    hq_static_margin:
      id: fastoad.handling_qualities.static_margin
    wing_position:
      id: fastoad.loop.wing_position
    aerodynamics_highspeed:
      id: fastoad.aerodynamics.highspeed.legacy
    aerodynamics_lowspeed:
      id: fastoad.aerodynamics.lowspeed.legacy
    aerodynamics_takeoff:
      id: fastoad.aerodynamics.takeoff.legacy
    aerodynamics_landing:
      id: fastoad.aerodynamics.landing.legacy
      use_xfoil: false
  performance:
    id: fastoad.performances.mission
    propulsion_id: fastoad.wrapper.propulsion.rubber_engine
    # mission_file_path: ::sizing_breguet
    mission_file_path: ::sizing_mission
    out_file: ./flight_points.csv
    adjust_fuel: true
    is_sizing: true
  wing_area:
    id: fastoad.loop.wing_area

optimization: # This section is needed only if optimization process is run
  design_variables:
    - name: data:geometry:wing:aspect_ratio
      lower: 9.0
      upper: 18.0
  constraints:
    - name: data:geometry:wing:span
      upper: 60.0
  objective:
    - name: data:mission:sizing:needed_block_fuel
      scaler: 1.e-4

Now in details:

Custom module path 

module_folders:

Provides the path where user can have his custom OpenMDAO modules. See section How to add custom OpenMDAO modules to FAST-OAD.

Input and output files 

input_file: ./problem_inputs.xml
output_file: ./problem_outputs.xml

Specifies the input and output files of the problem. They are defined in the configuration file and DO NOT APPEAR in the command line interface.

Problem driver 

driver: om.ScipyOptimizeDriver(tol=1e-2, optimizer='COBYLA')

This belongs the domain of the OpenMDAO framework and its utilization. This setting is needed for optimization problems. It is defined as in Python when assuming the OpenMDAO convention import openmdao.api as om.

For more details, please see the OpenMDAO documentation on drivers.

Solvers 

model:
  nonlinear_solver: om.NonlinearBlockGS(maxiter=100, atol=1e-2)
  linear_solver: om.DirectSolver()

This is the starting point for defining the model of the problem. The model is a group of components. If the model involves cycles, which happens for instance when some outputs of A are inputs of B, and vice-versa, it is necessary to specify solvers as done above.

For more details, please see the OpenMDAO documentation on nonlinear solvers and linear solvers.

Problem definition 

model:
  nonlinear_solver: om.NonlinearBlockGS(maxiter=100, atol=1e-2)
  linear_solver: om.DirectSolver()

  # Components can be put in sub-groups
  subgroup:

    # A group can be set with its own solvers.

    nonlinear_solver: om.NonlinearBlockGS(maxiter=100, atol=1e-2, iprint=0)
    linear_solver: om.DirectSolver()

    geometry:
      # An OpenMDAO component is identified by its "id"
      id: fastoad.geometry.legacy
    weight:
      id: fastoad.weight.legacy
    mtow:
      id: fastoad.mass_performances.compute_MTOW
    hq_tail_sizing:
      id: fastoad.handling_qualities.tail_sizing
    hq_static_margin:
      id: fastoad.handling_qualities.static_margin
    wing_position:
      id: fastoad.loop.wing_position
    aerodynamics_highspeed:
      id: fastoad.aerodynamics.highspeed.legacy
    aerodynamics_lowspeed:
      id: fastoad.aerodynamics.lowspeed.legacy
    aerodynamics_takeoff:
      id: fastoad.aerodynamics.takeoff.legacy
    aerodynamics_landing:
      id: fastoad.aerodynamics.landing.legacy
      use_xfoil: false
  performance:
    id: fastoad.performances.mission
    propulsion_id: fastoad.wrapper.propulsion.rubber_engine
    # mission_file_path: ::sizing_breguet
    mission_file_path: ::sizing_mission
    out_file: ./flight_points.csv
    adjust_fuel: true
    is_sizing: true
  wing_area:
    id: fastoad.loop.wing_area

Components of the model can be modules, or sub-groups. They are defined as a sub-section of model:. Sub-sections and sub-components can be freely named by user.

A sub-group gathers several modules and/or other sub-groups and can be set with its own solvers to resolve cycles it may contains, using keys linear_solver and nonlinear_solver, like model (that is merely the root group).

Here above, a sub-group with geometric, weight, handling-qualities and aerodynamic modules is defined and internal solvers are activated. Performance and wing area computation modules are set apart.

A module is defined by its id: key that refers to the module registered name.

Additional keys can be used in model, sub-groups and modules. They are interpreted as option settings:

For model and sub-groups, the OpenMDAO options for Group class apply.
For FAST-OAD modules, the list of available options is available through the list_modules sub-command (see How to get list of registered modules).

Model options 

OpenMDAO 3.27 introduced a new way to set options for any component in the problem, using the model_options attribute of the Problem object (see OpenMDAO documentation here).

This can be controlled from the configuration file, using for instance:

model_options:
  "*":
    propulsion_id: fastoad.wrapper.propulsion.rubber_engine
  "aerodynamics.*":
    use_xfoil: true

With above lines, we set the "propulsion_id" option for all concerned components in the problem, and we set the "use_xfoil" option for all components inside the aerodynamics module (please see OpenMDAO documentation for more examples using wildcards).

Note

Please note that the wildcards have to be (double) quoted.
This feature is especially convenient to set options for sub-components of the declared models, since these options are not directly accessible from the configuration file.

Optimization settings 

This settings are used only when using optimization (see Run Multi-Disciplinary Optimization). They are ignored when doing analysis (see Run Multi-Disciplinary Analysis).

The section is identified by:

optimization:

Design variables 

design_var:
  - name: data:geometry:wing:MAC:at25percent:x
    lower: 16.0
    upper: 18.0

Here are defined design variables (relevant only for optimization). Keys of this section are named after parameters of the OpenMDAO System.add_design_var() method

Several design variables can be defined.

Also, see How to get list of variables.

Objective function 

objective:
  - name: data:mission:sizing:fuel

Here is defined the objective function (relevant only for optimization). Keys of this section are named after parameters of the OpenMDAO System.add_objective() method

Only one objective variable can be defined.

Also, see How to get list of variables.

Constraints 

constraint:
  - name: data:handling_qualities:static_margin
    lower: 0.05
    upper: 0.1

Here are defined constraint variables (relevant only for optimization). Keys of this section are named after parameters of the OpenMDAO System.add_constraint() method

Several constraint variables can be defined.

Also, see How to get list of variables.

Using FAST-OAD through Command line 

FAST-OAD can be used through shell command line or Python. This section deals with the shell command line, but if you prefer using Python, you can skip this part and go to Using FAST-OAD through Python.

The FAST-OAD command is fastoad. Inline help is available with:

$ fastoad -h

fastoad works through sub-commands. Each sub-command provides its own inline help using

$ fastoad <sub-command> -h

How to get information about available plugins 

FAST-OAD is built on a plugin architecture where each plugin can provide FAST-OAD modules, Jupyter notebooks and sample configuration files (see plugin addition),

A list of installed plugins can be obtained with:

$ fastoad plugin_info

How to generate a configuration file 

FAST-OAD can provide a ready-to use configuration.

$ fastoad gen_conf my_conf.yml --from_package my_plugin_package --source sample_configuration_1.yml

This copies the file sample_configuration_1.yml`provided by installed package :code:`my_plugin_package to file my_conf.yml.

See how to get plugin information for listing the values you can put for options --from_package and --source.

If only one package is available, option --from_package may be omitted. If the selected package provides only one configuration file, option --source may be omitted.

Hence with FAST-OAD installed (version below 2.0) without additional plugin, the command can be:

$ fastoad gen_conf my_conf.yml

How to get list of registered modules 

If you want to change the list of components in the model in the configuration file, you need the list of available modules.

List of FAST-OAD modules can be obtained with:

$ fastoad list_modules

If you added custom modules in your configuration file my_conf.yml (see how to add custom OpenMDAO modules to FAST-OAD), they can be listed along FAST-OAD modules with:

$ fastoad list_modules my_conf.yml

You may also use the --verbose option to get detailed information on each module, including the available options, if any.

How to get list of variables 

Once your problem is defined in my_conf.yml, you can get a list of the variables of your problem with:

$ fastoad list_variables my_conf.yml

How to generate an input file 

The name of the input file is defined in your configuration file my_conf.yml. This input file can be generated with:

$ fastoad gen_inputs my_conf.yml

The generated file will be an XML file that contains needed inputs for your problem. Values will be the default values from module definitions, which means several ones will be “nan”. Actual value must be filled before the process is run.

If you already have a file that contains these values, you can use it to populate your new input files with:

$ fastoad gen_inputs my_conf.yml my_ref_values.xml

If you are using the configuration file provided by the gen_conf sub-command (see How to generate a configuration file), you may download our CeRAS01_baseline.xml and use it as source for generating your input file. You may also generate a source data file using the appropriate command (see How to generate a source data file)

How to generate a source data file 

As for the configuration file, FAST-OAD can provide a source data file usable for the generation of your input file.

$ fastoad gen_source_data_file my_source_data_file.xml --from_package my_plugin_package --source sample_source_data_file_1.xml

This copies the file sample_source_data_file_1.xml provided by installed package my_plugin_package to file my_source_data_file.xml.

The remarks made in section how to generate a configuration file on options --from_package and --source remain valid when generating a source data file.

How to view the problem process 

FAST-OAD proposes two graphical ways to look at the problem defined in configuration file. This is especially useful to see how models and variables are connected.

N2 diagram 

FAST-OAD can use OpenMDAO to create a N2 diagram. It provides in-depth information about the whole process.

You can create a n2.html file with:

$ fastoad n2 my_conf.yml

XDSM 

Using WhatsOpt as web service, FAST-OAD can provide a XDSM.

XDSM offers a more synthetic view than N2 diagram.

As it uses a web service, you need an internet access for this command, but you do not need to be a registered user on the WhatsOpt server.

You can create a xdsm.html file with:

$ fastoad xdsm my_conf.yml

Note

It may take a couple of minutes

Also, you may see WhatsOpt developer documentation to run your own server. In such case, you will address your server by using the --server option:

$ fastoad xdsm my_conf.yml --server https://the/address/of/my/WhatsOpt/server

How to run the problem 

Run Multi-Disciplinary Analysis 

Once your problem is defined in my_conf.yml, you can simply run it with:

$ fastoad eval my_conf.yml

Note

This is equivalent to OpenMDAO’s run_model()

Run Multi-Disciplinary Optimization 

You can also run the defined optimization with:

$ fastoad optim my_conf.yml

Note

This is equivalent to OpenMDAO’s run_driver()

Using FAST-OAD through Python 

The command line interface can generate Jupyter notebooks that show how to use the high-level interface of FAST-OAD.

To do so, type this command in your terminal:

$ fastoad notebooks

Then run the Jupyter server as indicated in the obtained message.