KozaiIzsakMeanElements Constructor |
Name | Description | |
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KozaiIzsakMeanElements(KeplerianElements, Boolean, Double, Double) |
Initialize a set of Kozai-Izsak mean elements from a set of osculating or mean KeplerianElements.
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KozaiIzsakMeanElements(ModifiedKeplerianElements, Boolean, Double, Double) |
Initialize a set of Kozai-Izsak mean elements from a set of osculating or mean
ModifiedKeplerianElements.
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KozaiIzsakMeanElements(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.
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KozaiIzsakMeanElements(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.
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KozaiIzsakMeanElements(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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