Interface used to access options for the Relative Flight Path Angle Strategy of a Basic Maneuver Procedure.
![]() | Set the method and corresponding value to define the control limits of the aircraft during the maneuver. |
![]() | Set whether to enable and a value for the maximum absolute altitude. |
![]() | Set whether to enable and a value for the maximum altitude offset from the target. |
![]() | Set whether to enable and a value for the minimum absolute altitude. |
![]() | Set whether to enable and a value for the minimum altitude offset from the target. |
![]() | Get the airspeed options. |
![]() | Gets or sets the goal height above or below the target. |
![]() | Gets or sets the option to compensate for the acceleration due to the Coriolis effect. |
![]() | Get the method to define the control limits of the aircraft during the maneuver. |
![]() | Get the specified pitch rate for a control limit mode of specify max pitch rate. |
![]() | Gets or sets the flight path angle for the maneuver. |
![]() | Gets or sets the maneuver factor, a dimensionless factor that determines how tightly or gently the aircraft will maneuver. |
![]() | Get the maximum absolute altitude. |
![]() | Get the maximum altitude offset from the target. |
![]() | Get the minimum absolute altitude. |
![]() | Get the minimum altitude offset from the target. |
![]() | Get the option to specify a maximum absolute altitude. |
![]() | Get the option to specify a maximum altitude offset from the target. |
![]() | Get the option to specify a minimum absolute altitude. |
![]() | Get the option to specify a minimum altitude offset from the target. |
Implemented Interface |
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IAgAvtrBasicManeuverStrategy |