Interface used to access options for a Glide Profile Strategy of a Basic Maneuver Procedure.
![]() | Set the airspeed and airspeed type that the aircraft will attempt to achieve and maintain if the hold initial airspeed option is not enabled. |
![]() | Set the glide speed control mode and altitude |
![]() | Get the airspeed the aircraft will attempt to achieve and maintain if the hold initial airspeed option is not enabled. |
![]() | Get the airspeed type. |
![]() | The option to compensate for the acceleration due to the Coriolis effect. |
![]() | The glide speed altitude when using the altitude control mode |
![]() | The glide speed control mode |
![]() | Select whether to maintain the airspeed of the aircraft at the beginning of the procedure throughout the maneuver. |
![]() | The maximum load factor the aircraft can withstand. |
![]() | The options of what the procedure will do if the aircraft has exceeded the maximum speed limits. |
![]() | The minimum load factor the aircraft can withstand. |
![]() | The powered cruise mode |
![]() | The powered cruise throttle |
![]() | The powered cruise thrust model |
Implemented Interface |
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IAgAvtrBasicManeuverStrategy |