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ModifiedKeplerianElementsToCartesian Method

Returns a cartesian representation of these orbital elements.

Namespace:  AGI.Foundation.Coordinates
Assembly:  AGI.Foundation.Core (in AGI.Foundation.Core.dll) Version: 19.1.398.0 (19.1.398.0)
Syntax
public Motion<Cartesian> ToCartesian()

Return Value

Type: MotionCartesian
Cartesian elements that are equivalent to these ModifiedKeplerianElements (distance and distance per time).
Exceptions
ExceptionCondition
InvalidOperationException Throws an exception in the case where the values become singular, namely when the true anomaly is Pi in the case of a parabolic orbit.
See Also