AircraftAdvancedClimbModel

class ansys.stk.core.stkobjects.aviator.AircraftAdvancedClimbModel

Bases: IPerformanceModel, ICatalogItem

Class defining the advanced climb performance model for an Aviator aircraft.

Overview

Methods

get_as_catalog_item	Get the catalog item interface for this object.
set_airspeed_limit	Set the airspeed limit and airspeed type below the altitude threshold.
set_climb_override_airspeed	Set the override airspeed and airspeed type.
set_flight_path_angle	Enable the flight path angle limit an set the flight path angle value.

Properties

airspeed_limit	Get the airsepeed limit below the altitude threshold.
airspeed_limit_type	Get the airspeed limit type.
altitude_limit	Get or set the altitude threshold, below which the airspeed limit will be applied.
climb_override_airspeed	Get the override airsepeed.
climb_override_airspeed_type	Get the override airspeed type.
climb_speed_type	Get or set the mode to calculate the aircraft’s airspeed while climbing.
compute_delta_altitude	Get or set the maximum change in altitude in a computed segment before the data is sampled again.
flight_path_angle	Get the flight path angle limit.
use_afterburner	Opt to use the engine’s afterburner when climbing if available.
use_airspeed_limit	Opt to limit the airspeed below a specified altitude.
use_flight_path_angle_limit	Opt to limit the flight path angle.

Import detail

from ansys.stk.core.stkobjects.aviator import AircraftAdvancedClimbModel

Property detail

property AircraftAdvancedClimbModel.airspeed_limit: float

Get the airsepeed limit below the altitude threshold.

property AircraftAdvancedClimbModel.airspeed_limit_type: AirspeedType

Get the airspeed limit type.

property AircraftAdvancedClimbModel.altitude_limit: float

Get or set the altitude threshold, below which the airspeed limit will be applied.

property AircraftAdvancedClimbModel.climb_override_airspeed: float

Get the override airsepeed.

property AircraftAdvancedClimbModel.climb_override_airspeed_type: AirspeedType

Get the override airspeed type.

property AircraftAdvancedClimbModel.climb_speed_type: ClimbSpeedType

Get or set the mode to calculate the aircraft’s airspeed while climbing.

property AircraftAdvancedClimbModel.compute_delta_altitude: float

Get or set the maximum change in altitude in a computed segment before the data is sampled again.

property AircraftAdvancedClimbModel.flight_path_angle: Any

Get the flight path angle limit.

property AircraftAdvancedClimbModel.use_afterburner: bool

Opt to use the engine’s afterburner when climbing if available.

property AircraftAdvancedClimbModel.use_airspeed_limit: bool

Opt to limit the airspeed below a specified altitude.

property AircraftAdvancedClimbModel.use_flight_path_angle_limit: bool

Opt to limit the flight path angle.

Method detail

AircraftAdvancedClimbModel.get_as_catalog_item(self) → ICatalogItem

Get the catalog item interface for this object.

Returns:

ICatalogItem

AircraftAdvancedClimbModel.set_airspeed_limit(self, airspeed_type: AirspeedType, airspeed: float) → None

Set the airspeed limit and airspeed type below the altitude threshold.

Parameters:

airspeed_type : AirspeedType

airspeed : float

Returns:

None

AircraftAdvancedClimbModel.set_climb_override_airspeed(self, airspeed_type: AirspeedType, airspeed: float) → None

Set the override airspeed and airspeed type.

Parameters:

airspeed_type : AirspeedType

airspeed : float

Returns:

None

AircraftAdvancedClimbModel.set_flight_path_angle(self, angle: Any) → None

Enable the flight path angle limit an set the flight path angle value.

Parameters:

angle : Any

Returns:

None