Uses of Class
org.orekit.propagation.integration.FieldStateMapper
Packages that use FieldStateMapper
Package
Description
Utilities for integration-based propagators (both numerical and semi-analytical).
Top level package for numerical propagators.
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 FieldStateMapperModifier and TypeMethodDescriptionprotected 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. /** Simple constructor.Constructors in org.orekit.propagation.integration with parameters of type FieldStateMapperModifierConstructorDescriptionFieldIntegratedEphemeris(FieldAbsoluteDate<T> startDate, FieldAbsoluteDate<T> minDate, FieldAbsoluteDate<T> maxDate, FieldStateMapper<T> mapper, AttitudeProvider attitudeProvider, PropagationType type, FieldDenseOutputModel<T> model, FieldDataDictionary<T> unmanaged, List<FieldAdditionalDataProvider<?, 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 FieldStateMapperModifier and TypeMethodDescriptionprotected 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. /** Simple constructor. -
Uses of FieldStateMapper in org.orekit.propagation.semianalytical.dsst
Methods in org.orekit.propagation.semianalytical.dsst that return FieldStateMapperModifier and TypeMethodDescriptionprotected 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. /** Simple constructor.