Uses of Class
org.orekit.propagation.integration.FieldStateMapper

Packages that use FieldStateMapper

Package	Description
org.orekit.propagation.integration	Utilities for integration-based propagators (both numerical and semi-analytical).
org.orekit.propagation.numerical	Top level package for numerical propagators.
org.orekit.propagation.semianalytical.dsst	This package provides an implementation of the Draper Semi-analytical Satellite Theory (DSST).

Uses of FieldStateMapper in org.orekit.propagation.integration

Methods in org.orekit.propagation.integration that return FieldStateMapper

Modifier and Type	Method and Description
protected abstract FieldStateMapper<T>	FieldAbstractIntegratedPropagator.createMapper(FieldAbsoluteDate<T> referenceDate, T mu, OrbitType orbitType, PositionAngle positionAngleType, AttitudeProvider attitudeProvider, Frame frame) Create a mapper between raw double components and spacecraft state.

Constructors in org.orekit.propagation.integration with parameters of type FieldStateMapper

Constructor and Description
FieldIntegratedEphemeris(FieldAbsoluteDate<T> startDate, FieldAbsoluteDate<T> minDate, FieldAbsoluteDate<T> maxDate, FieldStateMapper<T> mapper, PropagationType type, FieldDenseOutputModel<T> model, Map<String,T[]> unmanaged, List<FieldAdditionalStateProvider<T>> providers, String[] equations) Creates a new instance of IntegratedEphemeris.

Uses of FieldStateMapper in org.orekit.propagation.numerical

Methods in org.orekit.propagation.numerical that return FieldStateMapper

Modifier and Type	Method and Description
protected FieldStateMapper<T>	FieldNumericalPropagator.createMapper(FieldAbsoluteDate<T> referenceDate, T mu, OrbitType orbitType, PositionAngle positionAngleType, AttitudeProvider attitudeProvider, Frame frame) Create a mapper between raw double components and spacecraft state.

Uses of FieldStateMapper in org.orekit.propagation.semianalytical.dsst

Methods in org.orekit.propagation.semianalytical.dsst that return FieldStateMapper

Modifier and Type	Method and Description
protected FieldStateMapper<T>	FieldDSSTPropagator.createMapper(FieldAbsoluteDate<T> referenceDate, T mu, OrbitType ignoredOrbitType, PositionAngle ignoredPositionAngleType, AttitudeProvider attitudeProvider, Frame frame) Create a mapper between raw double components and spacecraft state.