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KozaiIzsakMeanElements Constructor

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  NameDescription
Public methodKozaiIzsakMeanElements(KeplerianElements, Boolean, Double, Double)
Initialize a set of Kozai-Izsak mean elements from a set of osculating or mean KeplerianElements.
Public methodKozaiIzsakMeanElements(ModifiedKeplerianElements, Boolean, Double, Double)
Initialize a set of Kozai-Izsak mean elements from a set of osculating or mean ModifiedKeplerianElements.
Public methodKozaiIzsakMeanElements(MotionCartesian, Double, Double, Double)
Initializes a set of Kozai-Izsak mean elements from the specified Cartesian motion. Please note that there must be a correspondence between the inertial and fixed frames used for the input motion. Specifically, the XY plane of the input motion should correspond to the equatorial plane.
Public methodKozaiIzsakMeanElements(Cartesian, Cartesian, Double, Double, Double)
Initialize a set of Kozai-Izsak mean elements from a Cartesian position and velocity. Please note that there must be a correspondence between the inertial and fixed frames used for the input position and velocity. Specifically, the XY plane of the input motion should correspond to the equatorial plane.
Public methodKozaiIzsakMeanElements(Double, Double, Double, Double, Double, Double, Double, Double, Double)
Initialize a set of Kozai-Izsak mean orbital elements. Inputs are assumed to be mean elements.
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