Uses of Class
org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements

Packages that use FieldAuxiliaryElements

Package	Description
org.orekit.propagation.semianalytical.dsst.forces	This package provides force models for Draper Semi-analytical Satellite Theory (DSST).

Uses of FieldAuxiliaryElements in org.orekit.propagation.semianalytical.dsst.forces

Methods in org.orekit.propagation.semianalytical.dsst.forces that return FieldAuxiliaryElements

Modifier and Type	Method and Description
FieldAuxiliaryElements<T>	FieldForceModelContext.getFieldAuxiliaryElements() Method to get the auxiliary elementsrelated to the ForceModelContext.

Methods in org.orekit.propagation.semianalytical.dsst.forces with parameters of type FieldAuxiliaryElements

Modifier and Type	Method and Description
protected abstract <T extends org.hipparchus.CalculusFieldElement<T>> T[]	AbstractGaussianContribution.getLLimits(FieldSpacecraftState<T> state, FieldAuxiliaryElements<T> auxiliaryElements) Compute the limits in L, the true longitude, for integration.
protected <T extends org.hipparchus.CalculusFieldElement<T>> T[]	DSSTSolarRadiationPressure.getLLimits(FieldSpacecraftState<T> state, FieldAuxiliaryElements<T> auxiliaryElements) Compute the limits in L, the true longitude, for integration.
protected <T extends org.hipparchus.CalculusFieldElement<T>> T[]	DSSTAtmosphericDrag.getLLimits(FieldSpacecraftState<T> state, FieldAuxiliaryElements<T> auxiliaryElements) Compute the limits in L, the true longitude, for integration.
<T extends org.hipparchus.CalculusFieldElement<T>> T[]	DSSTZonal.getMeanElementRate(FieldSpacecraftState<T> spacecraftState, FieldAuxiliaryElements<T> auxiliaryElements, T[] parameters) Computes the mean equinoctial elements rates dai / dt.
<T extends org.hipparchus.CalculusFieldElement<T>> T[]	DSSTForceModel.getMeanElementRate(FieldSpacecraftState<T> state, FieldAuxiliaryElements<T> auxiliaryElements, T[] parameters) Computes the mean equinoctial elements rates dai / dt.
<T extends org.hipparchus.CalculusFieldElement<T>> T[]	DSSTTesseral.getMeanElementRate(FieldSpacecraftState<T> spacecraftState, FieldAuxiliaryElements<T> auxiliaryElements, T[] parameters) Computes the mean equinoctial elements rates dai / dt.
<T extends org.hipparchus.CalculusFieldElement<T>> T[]	DSSTJ2SquaredClosedForm.getMeanElementRate(FieldSpacecraftState<T> state, FieldAuxiliaryElements<T> auxiliaryElements, T[] parameters) Computes the mean equinoctial elements rates dai / dt.
<T extends org.hipparchus.CalculusFieldElement<T>> T[]	AbstractGaussianContribution.getMeanElementRate(FieldSpacecraftState<T> state, FieldAuxiliaryElements<T> auxiliaryElements, T[] parameters) Computes the mean equinoctial elements rates dai / dt.
<T extends org.hipparchus.CalculusFieldElement<T>> T[]	DSSTThirdBody.getMeanElementRate(FieldSpacecraftState<T> currentState, FieldAuxiliaryElements<T> auxiliaryElements, T[] parameters) Computes the mean equinoctial elements rates dai / dt.
<T extends org.hipparchus.CalculusFieldElement<T>> T[]	DSSTNewtonianAttraction.getMeanElementRate(FieldSpacecraftState<T> state, FieldAuxiliaryElements<T> auxiliaryElements, T[] parameters) Computes the mean equinoctial elements rates dai / dt.
<T extends org.hipparchus.CalculusFieldElement<T>> List<FieldShortPeriodTerms<T>>	DSSTZonal.initializeShortPeriodTerms(FieldAuxiliaryElements<T> auxiliaryElements, PropagationType type, T[] parameters) Performs initialization prior to propagation for the current force model.
<T extends org.hipparchus.CalculusFieldElement<T>> List<FieldShortPeriodTerms<T>>	DSSTForceModel.initializeShortPeriodTerms(FieldAuxiliaryElements<T> auxiliaryElements, PropagationType type, T[] parameters) Performs initialization prior to propagation for the current force model.
<T extends org.hipparchus.CalculusFieldElement<T>> List<FieldShortPeriodTerms<T>>	DSSTTesseral.initializeShortPeriodTerms(FieldAuxiliaryElements<T> auxiliaryElements, PropagationType type, T[] parameters) Performs initialization prior to propagation for the current force model.
<T extends org.hipparchus.CalculusFieldElement<T>> List<FieldShortPeriodTerms<T>>	DSSTJ2SquaredClosedForm.initializeShortPeriodTerms(FieldAuxiliaryElements<T> auxiliaryElements, PropagationType type, T[] parameters) Performs initialization prior to propagation for the current force model.
<T extends org.hipparchus.CalculusFieldElement<T>> List<FieldShortPeriodTerms<T>>	AbstractGaussianContribution.initializeShortPeriodTerms(FieldAuxiliaryElements<T> auxiliaryElements, PropagationType type, T[] parameters) Performs initialization prior to propagation for the current force model.
<T extends org.hipparchus.CalculusFieldElement<T>> List<FieldShortPeriodTerms<T>>	DSSTThirdBody.initializeShortPeriodTerms(FieldAuxiliaryElements<T> auxiliaryElements, PropagationType type, T[] parameters) Performs initialization prior to propagation for the current force model.
<T extends org.hipparchus.CalculusFieldElement<T>> List<FieldShortPeriodTerms<T>>	DSSTNewtonianAttraction.initializeShortPeriodTerms(FieldAuxiliaryElements<T> auxiliaryElements, PropagationType type, T[] parameters) Performs initialization prior to propagation for the current force model.

Constructors in org.orekit.propagation.semianalytical.dsst.forces with parameters of type FieldAuxiliaryElements

Constructor and Description
FieldDSSTJ2SquaredClosedFormContext(FieldAuxiliaryElements<T> auxiliaryElements, UnnormalizedSphericalHarmonicsProvider provider) Simple constructor.
FieldDSSTThirdBodyDynamicContext(FieldAuxiliaryElements<T> aux, CelestialBody body, T[] parameters) Constructor.
FieldForceModelContext(FieldAuxiliaryElements<T> auxiliaryElements) Simple constructor.