Uses of Interface
org.orekit.propagation.conversion.averaging.elements.AveragedOrbitalElements
Packages that use AveragedOrbitalElements
Package
Description
This package wraps methods from various (semi)analytical models in Orekit to convert back and
forth between an averaged orbital state and an osculating one.
This package contains data classes representing averaged orbital elements (not time-stamped and
in any theory compatible with this choice of coordinates).
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Uses of AveragedOrbitalElements in org.orekit.propagation.conversion.averaging
Methods in org.orekit.propagation.conversion.averaging that return AveragedOrbitalElementsModifier and TypeMethodDescriptionAveragedOrbitalState.getAveragedElements()Getter for the averaged orbital elements. -
Uses of AveragedOrbitalElements in org.orekit.propagation.conversion.averaging.elements
Classes in org.orekit.propagation.conversion.averaging.elements that implement AveragedOrbitalElementsModifier and TypeClassDescriptionclassImmutable class containing values of averaged circular elements from any applicable theory (with MEAN asPositionAngleType).classImmutable class containing values of averaged equinoctial elements from any applicable theory (with MEAN asPositionAngleType).classImmutable class containing values of averaged Keplerian elements from any applicable theory (with MEAN asPositionAngleType).