Interface used to access options for a Relative Bearing Strategy of a Basic Maneuver Procedure.
![]() | Set the method and corresponding value to define the control limits of the aircraft during the maneuver. |
![]() | The option to compensate for the acceleration due to the Coriolis effect. |
![]() | The specified horizontal acceleration for a control limit mode of specify max horiz accel. |
![]() | Get the method to define the control limits of the aircraft during the maneuver. |
![]() | The specified turn radius for a control limit mode of specify min turn radius. |
![]() | The specified turn rate for a control limit mode of specify max turn rate. |
![]() | The range from the target at which the aircraft will stop. |
![]() | The relative bearing angle. |
![]() | The target name. |
![]() | The target position/velocity sampling resolution. |
![]() | Returns the valid target names. |
Implemented Interface |
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IAgAvtrBasicManeuverStrategy |