Description
Interface used to access the advanced climb model options for a climb model of an aircraft in the Aviator catalog.
Public Methods
 GetAsCatalogItem | Get the catalog item interface for this object. |
| SetAirspeedLimit | Set the airspeed limit and airspeed type below the altitude threshold. |
| SetClimbOverrideAirspeed | Set the override airspeed and airspeed type. |
| SetFlightPathAngle | Enable the flight path angle limit an set the flight path angle value. |
Public Properties
 AirspeedLimit | Get the airsepeed limit below the altitude threshold. |
| AirspeedLimitType | Get the airspeed limit type. |
| AltitudeLimit | The altitude threshold, below which the airspeed limit will be applied. |
| ClimbOverrideAirspeed | Get the override airsepeed. |
| ClimbOverrideAirspeedType | Get the override airspeed type. |
| ClimbSpeedType | The mode to calculate the aircraft's airspeed while climbing. |
| ComputeDeltaAltitude | The maximum change in altitude in a computed segment before the data is sampled again. |
| FlightPathAngle | Get the flight path angle limit. |
| UseAfterburner | Opt to use the engine's afterburner when climbing if available. |
| UseAirspeedLimit | Opt to limit the airspeed below a specified altitude. |
| UseFlightPathAngleLimit | Opt to limit the flight path angle. |
Interfaces
| Implemented Interface |
|---|
| IAgAvtrPerformanceModel |
| IAgAvtrCatalogItem |