Uses of Class
agi.foundation.coordinates.DelaunayElements

Packages that use DelaunayElements

Package	Description
agi.foundation.coordinates	Contains types for quantifying and converting between various coordinate representations.
agi.foundation.geometry	Contains types for expressing the motion of fundamental geometric objects such as points, axes, and reference frames; the manner in which they are related; and transformations between representations.
agi.foundation.propagators	Contains types used in producing the state of an object from a known element set.

Uses of DelaunayElements in agi.foundation.coordinates

Constructors in agi.foundation.coordinates with parameters of type DelaunayElements

Constructor and Description
EquinoctialElements(DelaunayElements elements) Initialize a set of equinoctial elements from a set of DelaunayElements.
KeplerianElements(DelaunayElements elements) Initialize a set of classical Keplerian elements from a set of DelaunayElements.
KeplerianElements(DelaunayElements elements, double eccentricityTolerance, double inclinationTolerance) Initialize a set of classical Keplerian elements from a set of DelaunayElements.
ModifiedKeplerianElements(DelaunayElements elements) Initializes a new instance for the specified DelaunayElements.
ModifiedKeplerianElements(DelaunayElements elements, double eccentricityTolerance, double inclinationTolerance) Initializes a new instance for the specified DelaunayElements.

Uses of DelaunayElements in agi.foundation.geometry

Methods in agi.foundation.geometry that return types with arguments of type DelaunayElements

Modifier and Type	Method and Description
Evaluator<DelaunayElements>	DynamicDelaunayElements.getEvaluator() Gets an evaluator that can be used to compute the DelaunayElements of the OrbitalPoint (get / set) at a given date.
Evaluator<DelaunayElements>	DynamicDelaunayElements.getEvaluator(EvaluatorGroup group) Gets an evaluator that can be used to compute the DelaunayElements of the OrbitalPoint (get / set) at a given date.

Uses of DelaunayElements in agi.foundation.propagators

Constructors in agi.foundation.propagators with parameters of type DelaunayElements

Constructor and Description
J2Propagator(JulianDate orbitEpoch, ReferenceFrame referenceFrame, DelaunayElements initialConditions, double j2UnnormalizedValue, double referenceDistance) Initializes a new instance.
J4Propagator(JulianDate orbitEpoch, ReferenceFrame referenceFrame, DelaunayElements initialConditions, double j2UnnormalizedValue, double j4UnnormalizedValue, double referenceDistance) Initializes a new instance.
TwoBodyPropagator(JulianDate orbitEpoch, ReferenceFrame referenceFrame, DelaunayElements elements) Initializes a new instance.