fastoad.models.performances.mission.segments.taxi module¶

Classes for Taxi sequences.

class fastoad.models.performances.mission.segments.taxi.TaxiSegment(target: fastoad.model_base.flight_point.FlightPoint, propulsion: fastoad.model_base.propulsion.IPropulsion, polar: Optional[fastoad.models.performances.mission.polar.Polar] = None, reference_area: float = 1.0, time_step: float = 60.0, engine_setting: fastoad.constants.EngineSetting = <EngineSetting.CLIMB: 2>, altitude_bounds: tuple = (-500.0, 40000.0), mach_bounds: tuple = (0.0, 5.0), name: str = '', interrupt_if_getting_further_from_target: bool = True, thrust_rate: float = 1.0)[source]¶

Bases: fastoad.models.performances.mission.segments.base.ManualThrustSegment, fastoad.models.performances.mission.segments.base.FixedDurationSegment

Class for computing Taxi phases.

Taxi phase has a target duration (target.time should be provided) and is at constant altitude, speed and thrust rate.

polar: fastoad.models.performances.mission.polar.Polar = None¶: The Polar instance that will provide drag data.

reference_area: float = 1.0¶: The reference area, in m**2.

time_step: float = 60.0¶: Used time step for computation (actual time step can be lower at some particular times of the flight path).