RotorcraftModel#
- class ansys.stk.core.stkobjects.aviator.RotorcraftModel#
Bases:
IAviatorVehicle
,ICatalogItem
Class defining a rotorcraft in Aviator.
Overview#
Set the maximum safe airspeed and airspeed type. |
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Set the maximum safe translation airspeed and airspeed type. |
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Get the catalog item interface for this object. |
Get or set the maximum altitude at which the rotorcraft is capable of operating. |
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Get or set the rotorcraftβs default cruising altitude. |
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Get or set the descent rate of the rotorcraft as a factor multiplied by the altitude change rate calculated at zero throttle. |
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Get or set the maximum pitch angle of the rotorcraftβs flight path while climbing. |
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Select to define the climbing airspeed of the rotorcraft using the cruise airspeed of the current procedure. |
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Get or set the maximum pitch angle of the rotorcraftβs flight path while descending. |
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Get or set the minimum rate at which the aircraft will descend once established in a steady descent. |
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Get or set the maximum load factor that the aircraft can bear while maneuvering in formation. |
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Get or set the standard roll rate of the rotorcraft in a turn. |
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Get or set the pitch rate when transitioning between attitude modes or procedures. |
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Get or set the yaw rate when transitioning between attitude modes. |
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Get or set the rate of change of the yaw rate. |
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Get or set the maximum pitch angle of the flight path when transitioning between forward flight and hovering. |
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Get or set the maximum pitch angle of the flight path when the rotorcraft is engaged in terrain following flight. |
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Get or set the time interval over which terrain points are sampled when the rotorcraft is engaged in terrain following flight. |
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Get or set the maximum change in altitude in a computed segment before the data is sampled again. |
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Get the maximum cruising airspeed of the rotorcraft. |
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Get the maximum safe airspeed type. |
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Get the maximum translation speed of the rotorcraft. |
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Get the maximum safe translation speed type. |
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Opt to ignore load factor limits when pushing over or pulling up. |
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Get the aircraftβs default configuration as saved in the catalog. |
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Get the aerodynamics interface. |
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Get the propulsion interface. |
Import detail#
from ansys.stk.core.stkobjects.aviator import RotorcraftModel
Property detail#
- property RotorcraftModel.max_altitude: float#
Get or set the maximum altitude at which the rotorcraft is capable of operating.
- property RotorcraftModel.default_cruise_altitude: float#
Get or set the rotorcraftβs default cruising altitude.
- property RotorcraftModel.descent_rate_factor: float#
Get or set the descent rate of the rotorcraft as a factor multiplied by the altitude change rate calculated at zero throttle.
- property RotorcraftModel.max_climb_angle: Any#
Get or set the maximum pitch angle of the rotorcraftβs flight path while climbing.
- property RotorcraftModel.climb_at_cruise_airspeed: bool#
Select to define the climbing airspeed of the rotorcraft using the cruise airspeed of the current procedure.
- property RotorcraftModel.max_descent_angle: Any#
Get or set the maximum pitch angle of the rotorcraftβs flight path while descending.
- property RotorcraftModel.min_descent_rate: float#
Get or set the minimum rate at which the aircraft will descend once established in a steady descent.
- property RotorcraftModel.max_load_factor: float#
Get or set the maximum load factor that the aircraft can bear while maneuvering in formation.
- property RotorcraftModel.roll_rate: Any#
Get or set the standard roll rate of the rotorcraft in a turn.
- property RotorcraftModel.pitch_rate: Any#
Get or set the pitch rate when transitioning between attitude modes or procedures.
- property RotorcraftModel.yaw_rate: Any#
Get or set the yaw rate when transitioning between attitude modes.
- property RotorcraftModel.max_transition_pitch_angle: Any#
Get or set the maximum pitch angle of the flight path when transitioning between forward flight and hovering.
- property RotorcraftModel.tf_max_flight_path_angle: Any#
Get or set the maximum pitch angle of the flight path when the rotorcraft is engaged in terrain following flight.
- property RotorcraftModel.tf_terrain_window: float#
Get or set the time interval over which terrain points are sampled when the rotorcraft is engaged in terrain following flight.
- property RotorcraftModel.compute_delta_altitude: float#
Get or set the maximum change in altitude in a computed segment before the data is sampled again.
- property RotorcraftModel.max_safe_airspeed: float#
Get the maximum cruising airspeed of the rotorcraft.
- property RotorcraftModel.max_safe_airspeed_type: AirspeedType#
Get the maximum safe airspeed type.
- property RotorcraftModel.max_safe_translation_speed: float#
Get the maximum translation speed of the rotorcraft.
- property RotorcraftModel.max_safe_translation_speed_type: AirspeedType#
Get the maximum safe translation speed type.
- property RotorcraftModel.ignore_flight_path_angle_for_climb_descent_transitions: bool#
Opt to ignore load factor limits when pushing over or pulling up.
- property RotorcraftModel.default_configuration: Configuration#
Get the aircraftβs default configuration as saved in the catalog.
- property RotorcraftModel.aerodynamics: RotorcraftAerodynamic#
Get the aerodynamics interface.
- property RotorcraftModel.propulsion: RotorcraftPropulsion#
Get the propulsion interface.
Method detail#
- RotorcraftModel.set_max_safe_airspeed(self, airspeed_type: AirspeedType, airspeed: float) None #
Set the maximum safe airspeed and airspeed type.
- RotorcraftModel.set_max_safe_translation_speed(self, airspeed_type: AirspeedType, airspeed: float) None #
Set the maximum safe translation airspeed and airspeed type.
- RotorcraftModel.get_as_catalog_item(self) ICatalogItem #
Get the catalog item interface for this object.
- Returns:
ICatalogItem