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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: 19.1.398.0 (19.1.398.0)
Syntax
public PropagationPointElement ApplyManeuver(
	Maneuver maneuver
)

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.
See Also