Uses of Class
org.orekit.propagation.integration.FieldStateMapper
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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). -
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Uses of FieldStateMapper in org.orekit.propagation.integration
Methods in org.orekit.propagation.integration that return FieldStateMapper Modifier and Type Method Description protected abstract FieldStateMapper<T>
FieldAbstractIntegratedPropagator. createMapper(FieldAbsoluteDate<T> referenceDate, T mu, OrbitType orbitType, PositionAngleType 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 Description FieldIntegratedEphemeris(FieldAbsoluteDate<T> startDate, FieldAbsoluteDate<T> minDate, FieldAbsoluteDate<T> maxDate, FieldStateMapper<T> mapper, PropagationType type, FieldDenseOutputModel<T> model, FieldArrayDictionary<T> unmanaged, List<FieldAdditionalStateProvider<T>> providers, String[] equations, int[] dimensions)
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 Description protected FieldStateMapper<T>
FieldNumericalPropagator. createMapper(FieldAbsoluteDate<T> referenceDate, T mu, OrbitType orbitType, PositionAngleType 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 Description protected FieldStateMapper<T>
FieldDSSTPropagator. createMapper(FieldAbsoluteDate<T> referenceDate, T mu, OrbitType ignoredOrbitType, PositionAngleType ignoredPositionAngleType, AttitudeProvider attitudeProvider, Frame frame)
Create a mapper between raw double components and spacecraft state.
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