Interface used to access options for a Push/Pull Strategy of a Basic Maneuver Procedure.
![]() | Set whether to enable the airspeed stopping condition and the corresponding value. |
![]() | Set whether to enable the altitude stopping condition and the corresponding value. |
![]() | Set whether to enable the altitude rate stopping condition and the corresponding value. |
![]() | Gets or sets the specific G force rate to accelerate/decelerate at. |
![]() | Gets or sets the option to accelerate, decelerate, or maintain the current airspeed. |
![]() | Gets or sets the option to compensate for the acceleration due to the Coriolis effect. |
![]() | Get the airspeed to maintain. |
![]() | Gets or sets the airspeed type for the maintain airspeed. |
![]() | Gets or sets the option to push over or pull up. |
![]() | Gets or sets the G force of the maneuver. |
![]() | Gets or sets the reference frame the aircraft will use. |
![]() | Get the airspeed stopping condition. |
![]() | Get the airspeed type for the airspeed stopping condition. |
![]() | Get the altitude stopping condition. |
![]() | Get the altitude rate stopping condition. |
![]() | Gets or sets the flight path angle the maneuver will stop at if achieved. |
![]() | Get the option to stop the maneuver if a specified airspeed is achieved. |
![]() | Get the option to stop the maneuver if a specified altitude is achieved. |
![]() | Get the option to stop the maneuver if a specified altitude rate is achieved. |
Implemented Interface |
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IAgAvtrBasicManeuverStrategy |