AircraftMotionElementApplyManeuver Method

Produces a point PropagationStateElement that uses the provided maneuver definition to compute the derivatives for integration.

Namespace: AGI.Foundation.AircraftPropagation
Assembly: AGI.Foundation.AircraftPropagation (in AGI.Foundation.AircraftPropagation.dll) Version: 24.3.420.0 (24.3.420.0)

Syntax

C++

Copy

public PropagationPointElement ApplyManeuver(
	Maneuver maneuver
)

Public Function ApplyManeuver ( 
	maneuver As Maneuver
) As PropagationPointElement

public:
PropagationPointElement^ ApplyManeuver(
	Maneuver^ maneuver
)

member ApplyManeuver : 
        maneuver : Maneuver -> PropagationPointElement

Parameters

maneuver: Type: AGI.Foundation.AircraftPropagationManeuver
The maneuver definition which will define the derivatives for integration.

Return Value

Type: PropagationPointElement
The point propagation state element.

Reference

AircraftMotionElement Class

AGI.Foundation.AircraftPropagation Namespace

AircraftMotionElementAddLanguageSpecificTextSet("LST770D8A7C_0?cpp=::|nu=.");ApplyManeuver Method

Parameters

Return Value

Reference

AircraftMotionElementApplyManeuver Method