ModifiedKeplerianElementsToCartesian Method

Returns a cartesian representation of these orbital elements.

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

Syntax

public Motion<Cartesian> ToCartesian()

Public Function ToCartesian As Motion(Of Cartesian)

public:
Motion<Cartesian> ToCartesian()

member ToCartesian : unit -> Motion<Cartesian>

Type: MotionCartesian
Cartesian elements that are equivalent to these ModifiedKeplerianElements.

Exceptions

Exception	Condition
InvalidOperationException	Throws an exception in the case where the values become singular, namely when the true anomaly is π in the case of a parabolic orbit.

ModifiedKeplerianElementsAddLanguageSpecificTextSet("LSTE93CB88F_0?cpp=::|nu=.");ToCartesian Method