AircraftStateElementConverterConvertState Method (Double)

Convert the raw state into a Cartesian and its derivatives.

Namespace: AGI.Foundation.AircraftPropagation
Assembly: AGI.Foundation.AircraftPropagation (in AGI.Foundation.AircraftPropagation.dll) Version: 24.2.419.0 (24.2.419.0)

Syntax

C++

Copy

public Motion<Cartesian> ConvertState(
	double[] overallState
)

Public Function ConvertState ( 
	overallState As Double()
) As Motion(Of Cartesian)

public:
Motion<Cartesian> ConvertState(
	array<double>^ overallState
)

member ConvertState : 
        overallState : float[] -> Motion<Cartesian>

Parameters

overallState: Type: SystemDouble
The raw state to convert.

Return Value

Type: MotionCartesian
The value and its derivatives corresponding to the state.

Reference

AircraftStateElementConverter Class

ConvertState Overload

AGI.Foundation.AircraftPropagation Namespace

AircraftStateElementConverterAddLanguageSpecificTextSet("LST2356117C_0?cpp=::|nu=.");ConvertState Method (AddLanguageSpecificTextSet("LST2356117C_1?cpp=array&lt;");DoubleAddLanguageSpecificTextSet("LST2356117C_2?cpp=&gt;|vb=()|nu=[]");)

Parameters

Return Value

Reference

AircraftStateElementConverterConvertState Method (Double)