Modifier and Type | Class and Description |
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class |
AbstractStelaGaussContribution
Abstract Class for the computation of Gauss Equations and its derivatives
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class |
AbstractStelaLagrangeContribution
This abstract class represents a force with Lagrange attribute, to be used in a
StelaGTOPropagator . |
Modifier and Type | Class and Description |
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class |
StelaAtmosphericDrag
Class representing the atmospheric drag for the Stela GTO extrapolator.
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Modifier and Type | Class and Description |
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class |
SolidTidesAcc
Class representing the tidal contribution.
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class |
StelaTesseralAttraction
This class represent the tesseral perturbations
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class |
StelaThirdBodyAttraction
Class computing third body attraction perturbations.
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class |
StelaZonalAttraction
Class computing Zonal perturbations
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Modifier and Type | Class and Description |
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class |
NonInertialContribution
Class representing the non-inertial contribution for STELA propagator.
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Modifier and Type | Class and Description |
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class |
SRPPotential
This class represents the PRS Lagrange contribution in the STELA propagator context.
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class |
SRPSquaring
Class representing the srp gauss force model for STELA
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class |
StelaSRPSquaring
This class represents the Stela SRP model, which computes perturbations using the squaring method and the partial
derivatives using the potential approximation.
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Constructor and Description |
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OrbitNatureConverter(List<StelaForceModel> inForceModels)
Default constructor.
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Modifier and Type | Method and Description |
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Map<StelaForceModel,double[][]> |
StelaPartialDerivativesEquations.getDerivatives()
Returns derivatives map
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List<StelaForceModel> |
StelaGTOPropagator.getForceModels()
Get perturbing force models list.
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Modifier and Type | Method and Description |
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void |
StelaGTOPropagator.addForceModel(StelaForceModel forceModel)
Add a force model to the global perturbation model.
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Modifier and Type | Method and Description |
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Set<StelaForceModel> |
TimeDerivativeData.getAvailableForceModels()
Returns available force models.
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Set<StelaForceModel> |
TimeDerivativeData.getAvailableForceModelsSTM()
Returns available force models for state transition matrix.
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Modifier and Type | Method and Description |
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double[] |
TimeDerivativeData.getDerivatives(StelaForceModel force)
Returns derivative dE'/dt (E' = mean orbital parameters) for provided force model.
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double[][] |
TimeDerivativeData.getDerivativesSTM(StelaForceModel force)
Returns derivative dSTM/dt (STM = state transition matrix) for provided force model.
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Constructor and Description |
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TimeDerivativeData(Orbit aOrbit,
double[] aMeanMotion,
double[][] aMeanMotionSTM,
Map<StelaForceModel,double[]> aDerivatives,
Map<StelaForceModel,double[][]> aDerivativesSTM)
Constructor.
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TimeDerivativeData(Orbit aOrbit,
double[] aMeanMotion,
double[][] aMeanMotionSTM,
Map<StelaForceModel,double[]> aDerivatives,
Map<StelaForceModel,double[][]> aDerivativesSTM)
Constructor.
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