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IAgAvtrRotorcraft Interface

Description

Interface used to access the rotorcraft options in the Aviator catalog.

Public Methods

Public Method GetAsCatalogItemGet the catalog item interface for this object.
Public Method SetMaxSafeAirspeedSet the maximum safe airspeed and airspeed type.
Public Method SetMaxSafeTranslationSpeedSet the maximum safe translation airspeed and airspeed type.

Public Properties

Public Property AerodynamicsGet the aerodynamics interface.
Public Property ClimbAtCruiseAirspeedSelect to define the climbing airspeed of the rotorcraft using the cruise airspeed of the current procedure.
Public Property ComputeDeltaAltThe maximum change in altitude in a computed segment before the data is sampled again.
Public Property DefaultConfigurationThe aircraft's default configuration as saved in the catalog.
Public Property DefaultCruiseAltitudeThe rotorcraft's default cruising altitude.
Public Property DescentRateFactorThe descent rate of the rotorcraft as a factor multiplied by the altitude change rate calculated at zero throttle.
Public Property IgnoreFPAForClimbDescentTransitionsOpt to ignore load factor limits when pushing over or pulling up.
Public Property MaxAltitudeThe maximum altitude at which the rotorcraft is capable of operating.
Public Property MaxClimbAngleThe maximum pitch angle of the rotorcraft's flight path while climbing.
Public Property MaxDescentAngleThe maximum pitch angle of the rotorcraft's flight path while descending.
Public Property MaxLoadFactorThe maximum load factor that the aircraft can bear while maneuvering in formation.
Public Property MaxSafeAirspeedThe maximum cruising airspeed of the rotorcraft.
Public Property MaxSafeAirspeedTypeThe maximum safe airspeed type.
Public Property MaxSafeTranslationSpeedThe maximum translation speed of the rotorcraft.
Public Property MaxSafeTranslationSpeedTypeThe maximum safe translation speed type.
Public Property MaxTransitionPitchAngleThe maximum pitch angle of the flight path when transitioning between forward flight and hovering.
Public Property MinDescentRateThe minimum rate at which the aircraft will descend once established in a steady descent.
Public Property PitchRateThe pitch rate when transitioning between attitude modes or procedures.
Public Property PropulsionGet the propulsion interface.
Public Property RollRateThe standard roll rate of the rotorcraft in a turn.
Public Property TFMaxFlightPathAngleThe maximum pitch angle of the flight path when the rotorcraft is engaged in terrain following flight.
Public Property TFTerrainWindowThe time interval over which terrain points are sampled when the rotorcraft is engaged in terrain following flight.
Public Property YawRateThe yaw rate when transitioning between attitude modes.
Public Property YawRateDotThe rate of change of the yaw rate.

Interfaces

CoClasses that Implement IAgAvtrRotorcraft

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