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