fastoad.models.performances.mission.openmdao.flight module

class fastoad.models.performances.mission.openmdao.flight.SizingFlight(**kwargs)

Bases: openmdao.core.explicitcomponent.ExplicitComponent

Simulates a complete flight mission with diversion.

Computes thrust, SFC and thrust rate by direct call to engine model.

Options:

• propulsion_id: (mandatory) the identifier of the propulsion wrapper.

• out_file: if provided, a csv file will be written at provided path with all computed

  flight points. If path is relative, it will be resolved from working directory

compute(inputs, outputs, discrete_inputs=None, discrete_outputs=None)

Compute outputs given inputs. The model is assumed to be in an unscaled state.

Parameters

• inputs (Vector) – unscaled, dimensional input variables read via inputs[key]

• outputs (Vector) – unscaled, dimensional output variables read via outputs[key]

• discrete_inputs (dict or None) – If not None, dict containing discrete input values.

• discrete_outputs (dict or None) – If not None, dict containing discrete output values.

compute_breguet(inputs, outputs)

compute_mission(inputs, outputs)

initialize()

Perform any one-time initialization run at instantiation.

setup()

Declare inputs and outputs.

Available attributes:

name pathname comm options