Interface used to access the options for a dyn state launch procedure.
![]() | Get the procedure interface. |
![]() | Set the launch airspeed. |
![]() | The acceleration of the aircraft during the launch. |
![]() | The goal airspeed for the launch. |
![]() | The airspeed type. |
![]() | The attitude mode during the launch. |
![]() | The bearing reference for the dyn state launch procedure. |
![]() | The reference coordinate frame for the dyn state launch procedure. |
![]() | The fuel flow type of the aircraft during the launch. |
![]() | The launch direction bearing. |
![]() | The launch direction elevation. |
![]() | The launch time of the aircraft. |
![]() | The fuel flow value for a fuel flow type set to Override. |
![]() | Opt to specify a minimum launch speed the aircraft will accelerate to. |
![]() | The true course used when the vehicle's direction vector is set to Zenith. |
Implemented Interface |
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IAgAvtrProcedure |