AircraftReferenceState.ToMotionInFixedFrame Method

Converts the reference state of the aircraft into motion with respect to the fixed frame of the HeightReferenceSurface.

Namespace: AGI.Foundation.AircraftPropagation
Assembly: AGI.Foundation.AircraftPropagation (in AGI.Foundation.AircraftPropagation.dll) Version: 25.1.421.0 (25.1.421.0)

Syntax

C++

Copy

public Motion<Cartesian> ToMotionInFixedFrame(
	WindModel winds
)

Public Function ToMotionInFixedFrame ( 
	winds As WindModel
) As Motion(Of Cartesian)

public:
Motion<Cartesian> ToMotionInFixedFrame(
	WindModel^ winds
)

member ToMotionInFixedFrame : 
        winds : WindModel -> Motion<Cartesian>

Parameters

winds: Type: AGI.Foundation.Celestial.WindModel
The wind model for the local atmosphere.

Return Value

Type: Motion<Cartesian>
The Motion<T> in the fixed frame of the central body.

Exceptions

Exception	Condition
PropertyInvalidException	Thrown when the HeightReferenceSurface is null.
UnsupportedCaseException	Thrown if the VelocityReferenceAxes is not a ManeuverReferenceAxes.

Reference

AircraftReferenceState Class

AGI.Foundation.AircraftPropagation Namespace

AircraftReferenceState.AddLanguageSpecificTextSet("LST1203CD59_0?cpp=::|nu=.");ToMotionInFixedFrame Method

Parameters

Return Value

Reference

AircraftReferenceState.ToMotionInFixedFrame Method