Uses of Class
org.orekit.orbits.FieldOrbit
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Packages that use FieldOrbit Package Description org.orekit.orbits This package provides classes to represent orbits.org.orekit.propagation Propagationorg.orekit.propagation.analytical Top level package for analytical propagators.org.orekit.propagation.analytical.intelsat This package provides classes to propagate Intelsat's 11 elements.org.orekit.propagation.analytical.tle This package provides classes to read and extrapolate tle's.org.orekit.propagation.conversion This package provides tools to convert a given propagator or a set ofSpacecraftState
into another propagator.org.orekit.propagation.events This package provides interfaces and classes dealing with events occurring during propagation.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).org.orekit.propagation.semianalytical.dsst.forces This package provides force models for Draper Semi-analytical Satellite Theory (DSST).org.orekit.propagation.semianalytical.dsst.utilities This package provides utilities for Draper Semi-analytical Satellite Theory (DSST).org.orekit.ssa.collision.shorttermencounter.probability.twod Package specific to calculus assuming a 2D short-term encounter model.org.orekit.utils This package provides useful objects. -
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Uses of FieldOrbit in org.orekit.orbits
Subclasses of FieldOrbit in org.orekit.orbits Modifier and Type Class Description class
FieldCartesianOrbit<T extends CalculusFieldElement<T>>
This class holds Cartesian orbital parameters.class
FieldCircularOrbit<T extends CalculusFieldElement<T>>
This class handles circular orbital parameters.class
FieldEquinoctialOrbit<T extends CalculusFieldElement<T>>
This class handles equinoctial orbital parameters, which can support both circular and equatorial orbits.class
FieldKeplerianOrbit<T extends CalculusFieldElement<T>>
This class handles traditional Keplerian orbital parameters.Methods in org.orekit.orbits that return FieldOrbit Modifier and Type Method Description abstract <T extends CalculusFieldElement<T>>
FieldOrbit<T>OrbitType. convertToFieldOrbit(Field<T> field, Orbit orbit)
Convert an orbit to the "Fielded" instance type.abstract <T extends CalculusFieldElement<T>>
FieldOrbit<T>OrbitType. convertType(FieldOrbit<T> orbit)
Convert an orbit to the instance type.FieldOrbit<KK>
AbstractFieldOrbitInterpolator. interpolate(FieldAbsoluteDate<KK> interpolationDate, Collection<FieldOrbit<KK>> sample)
Get an interpolated instance.FieldOrbit<KK>
FieldOrbitBlender. interpolate(AbstractFieldTimeInterpolator.InterpolationData interpolationData)
Interpolate instance from given interpolation data.protected FieldOrbit<KK>
FieldOrbitHermiteInterpolator. interpolate(AbstractFieldTimeInterpolator.InterpolationData interpolationData)
Interpolate instance from given interpolation data.abstract <T extends CalculusFieldElement<T>>
FieldOrbit<T>OrbitType. mapArrayToOrbit(T[] array, T[] arrayDot, PositionAngleType type, FieldAbsoluteDate<T> date, T mu, Frame frame)
Convert state array to orbital parameters.abstract <T extends CalculusFieldElement<T>>
FieldOrbit<T>OrbitType. normalize(FieldOrbit<T> orbit, FieldOrbit<T> reference)
Normalize one orbit with respect to a reference one.abstract FieldOrbit<T>
FieldOrbit. shiftedBy(T dt)
Get a time-shifted orbit.Methods in org.orekit.orbits with parameters of type FieldOrbit Modifier and Type Method Description abstract <T extends CalculusFieldElement<T>>
FieldOrbit<T>OrbitType. convertType(FieldOrbit<T> orbit)
Convert an orbit to the instance type.abstract <T extends CalculusFieldElement<T>>
voidOrbitType. mapOrbitToArray(FieldOrbit<T> orbit, PositionAngleType type, T[] stateVector, T[] stateVectorDot)
Convert orbit to state array.abstract <T extends CalculusFieldElement<T>>
FieldOrbit<T>OrbitType. normalize(FieldOrbit<T> orbit, FieldOrbit<T> reference)
Normalize one orbit with respect to a reference one.Method parameters in org.orekit.orbits with type arguments of type FieldOrbit Modifier and Type Method Description FieldOrbit<KK>
AbstractFieldOrbitInterpolator. interpolate(FieldAbsoluteDate<KK> interpolationDate, Collection<FieldOrbit<KK>> sample)
Get an interpolated instance.Constructors in org.orekit.orbits with parameters of type FieldOrbit Constructor Description FieldCartesianOrbit(FieldOrbit<T> op)
Constructor from any kind of orbital parameters.FieldCircularOrbit(FieldOrbit<T> op)
Constructor from any kind of orbital parameters.FieldEquinoctialOrbit(FieldOrbit<T> op)
Constructor from any kind of orbital parameters.FieldKeplerianOrbit(FieldOrbit<T> op)
Constructor from any kind of orbital parameters. -
Uses of FieldOrbit in org.orekit.propagation
Methods in org.orekit.propagation that return FieldOrbit Modifier and Type Method Description FieldOrbit<T>
FieldSpacecraftState. getOrbit()
Get the current orbit.Methods in org.orekit.propagation that return types with arguments of type FieldOrbit Modifier and Type Method Description Optional<FieldTimeInterpolator<FieldOrbit<KK>,KK>>
FieldSpacecraftStateInterpolator. getOrbitInterpolator()
Get orbit interpolator.Methods in org.orekit.propagation with parameters of type FieldOrbit Modifier and Type Method Description FieldStateCovariance<T>
FieldStateCovariance. changeCovarianceFrame(FieldOrbit<T> orbit, Frame frameOut)
Get the covariance in the output frame.FieldStateCovariance<T>
FieldStateCovariance. changeCovarianceFrame(FieldOrbit<T> orbit, LOF lofOut)
Get the covariance in a given local orbital frame.FieldStateCovariance<T>
FieldStateCovariance. changeCovarianceType(FieldOrbit<T> orbit, OrbitType outOrbitType, PositionAngleType outAngleType)
Get the covariance matrix in another orbit type.FieldStateCovariance<T>
FieldStateCovariance. shiftedBy(Field<T> field, FieldOrbit<T> orbit, T dt)
Get a time-shifted covariance matrix.Constructors in org.orekit.propagation with parameters of type FieldOrbit Constructor Description FieldSpacecraftState(FieldOrbit<T> orbit)
Build a spacecraft state from orbit only.FieldSpacecraftState(FieldOrbit<T> orbit, FieldAttitude<T> attitude)
Build a spacecraft state from orbit and attitude.FieldSpacecraftState(FieldOrbit<T> orbit, FieldAttitude<T> attitude, FieldArrayDictionary<T> additional)
Build a spacecraft state from orbit attitude and additional states.FieldSpacecraftState(FieldOrbit<T> orbit, FieldAttitude<T> attitude, T mass)
Build a spacecraft state from orbit, attitude and mass.FieldSpacecraftState(FieldOrbit<T> orbit, FieldAttitude<T> attitude, T mass, FieldArrayDictionary<T> additional)
Build a spacecraft state from orbit, attitude, mass and additional states.FieldSpacecraftState(FieldOrbit<T> orbit, FieldAttitude<T> attitude, T mass, FieldArrayDictionary<T> additional, FieldArrayDictionary<T> additionalDot)
Build a spacecraft state from orbit, attitude, mass, additional states and derivatives.FieldSpacecraftState(FieldOrbit<T> orbit, FieldArrayDictionary<T> additional)
Build a spacecraft state from orbit and additional states.FieldSpacecraftState(FieldOrbit<T> orbit, T mass)
Create a new instance from orbit and mass.FieldSpacecraftState(FieldOrbit<T> orbit, T mass, FieldArrayDictionary<T> additional)
Create a new instance from orbit, mass and additional states. -
Uses of FieldOrbit in org.orekit.propagation.analytical
Methods in org.orekit.propagation.analytical that return FieldOrbit Modifier and Type Method Description protected abstract FieldOrbit<T>
FieldAbstractAnalyticalPropagator. propagateOrbit(FieldAbsoluteDate<T> date, T[] parameters)
Extrapolate an orbit up to a specific target date.protected FieldOrbit<T>
FieldKeplerianPropagator. propagateOrbit(FieldAbsoluteDate<T> date, T[] parameters)
Extrapolate an orbit up to a specific target date.Methods in org.orekit.propagation.analytical with parameters of type FieldOrbit Modifier and Type Method Description static <T extends CalculusFieldElement<T>>
FieldKeplerianOrbit<T>FieldBrouwerLyddanePropagator. computeMeanOrbit(FieldOrbit<T> osculating, double referenceRadius, double mu, double c20, double c30, double c40, double c50, double M2Value, double epsilon, int maxIterations)
Conversion from osculating to mean orbit.static <T extends CalculusFieldElement<T>>
FieldKeplerianOrbit<T>FieldBrouwerLyddanePropagator. computeMeanOrbit(FieldOrbit<T> osculating, UnnormalizedSphericalHarmonicsProvider provider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics harmonics, double M2Value)
Conversion from osculating to mean orbit.static <T extends CalculusFieldElement<T>>
FieldKeplerianOrbit<T>FieldBrouwerLyddanePropagator. computeMeanOrbit(FieldOrbit<T> osculating, UnnormalizedSphericalHarmonicsProvider provider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics harmonics, double M2Value, double epsilon, int maxIterations)
Conversion from osculating to mean orbit.static <T extends CalculusFieldElement<T>>
FieldCircularOrbit<T>FieldEcksteinHechlerPropagator. computeMeanOrbit(FieldOrbit<T> osculating, double referenceRadius, double mu, double c20, double c30, double c40, double c50, double c60, double epsilon, int maxIterations)
Conversion from osculating to mean orbit.static <T extends CalculusFieldElement<T>>
FieldCircularOrbit<T>FieldEcksteinHechlerPropagator. computeMeanOrbit(FieldOrbit<T> osculating, UnnormalizedSphericalHarmonicsProvider provider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics harmonics)
Conversion from osculating to mean orbit.static <T extends CalculusFieldElement<T>>
FieldCircularOrbit<T>FieldEcksteinHechlerPropagator. computeMeanOrbit(FieldOrbit<T> osculating, UnnormalizedSphericalHarmonicsProvider provider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics harmonics, double epsilon, int maxIterations)
Conversion from osculating to mean orbit.Constructors in org.orekit.propagation.analytical with parameters of type FieldOrbit Constructor Description FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, double referenceRadius, T mu, double c20, double c30, double c40, double c50, double M2)
Build a propagator from orbit and potential.FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, double referenceRadius, T mu, double c20, double c30, double c40, double c50, double M2)
Build a propagator from orbit, attitude provider and potential.FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, UnnormalizedSphericalHarmonicsProvider provider, double M2)
Build a propagator from orbit, attitude provider and potential provider.FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, double referenceRadius, T mu, double c20, double c30, double c40, double c50, double M2)
Build a propagator from orbit, attitude provider, mass and potential.FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, double referenceRadius, T mu, double c20, double c30, double c40, double c50, PropagationType initialType, double M2)
Build a propagator from orbit, attitude provider, mass and potential.FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, double referenceRadius, T mu, double c20, double c30, double c40, double c50, PropagationType initialType, double M2, double epsilon, int maxIterations)
Build a propagator from orbit, attitude provider, mass and potential.FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, UnnormalizedSphericalHarmonicsProvider provider, double M2)
Build a propagator from orbit, attitude provider, mass and potential provider.FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitude, T mass, UnnormalizedSphericalHarmonicsProvider provider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics harmonics, double M2)
Private helper constructor.FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitude, T mass, UnnormalizedSphericalHarmonicsProvider provider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics harmonics, PropagationType initialType, double M2)
Private helper constructor.FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, UnnormalizedSphericalHarmonicsProvider provider, PropagationType initialType, double M2)
Build a propagator from orbit, attitude provider, mass and potential provider.FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, UnnormalizedSphericalHarmonicsProvider provider, double M2)
Build a propagator from orbit and potential provider.FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, UnnormalizedSphericalHarmonicsProvider provider, PropagationType initialType, double M2)
Build a propagator from orbit and potential provider.FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, T mass, double referenceRadius, T mu, double c20, double c30, double c40, double c50, double M2)
Build a propagator from orbit, mass and potential.FieldBrouwerLyddanePropagator(FieldOrbit<T> initialOrbit, T mass, UnnormalizedSphericalHarmonicsProvider provider, double M2)
Build a propagator from orbit, mass and potential provider.FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, double referenceRadius, T mu, double c20, double c30, double c40, double c50, double c60)
Build a propagator from FieldOrbit and potential.FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, double referenceRadius, T mu, double c20, double c30, double c40, double c50, double c60)
Build a propagator from FieldOrbit, attitude provider and potential.FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, UnnormalizedSphericalHarmonicsProvider provider)
Build a propagator from FieldOrbit, attitude provider and potential provider.FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, double referenceRadius, T mu, double c20, double c30, double c40, double c50, double c60)
Build a propagator from FieldOrbit, attitude provider, mass and potential.FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, double referenceRadius, T mu, double c20, double c30, double c40, double c50, double c60, PropagationType initialType)
Build a propagator from FieldOrbit, attitude provider, mass and potential.FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, double referenceRadius, T mu, double c20, double c30, double c40, double c50, double c60, PropagationType initialType, double epsilon, int maxIterations)
Build a propagator from FieldOrbit, attitude provider, mass and potential.FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, UnnormalizedSphericalHarmonicsProvider provider)
Build a propagator from FieldOrbit, attitude provider, mass and potential provider.FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitude, T mass, UnnormalizedSphericalHarmonicsProvider provider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics harmonics)
Private helper constructor.FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitude, T mass, UnnormalizedSphericalHarmonicsProvider provider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics harmonics, PropagationType initialType)
Private helper constructor.FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mass, UnnormalizedSphericalHarmonicsProvider provider, PropagationType initialType)
Build a propagator from orbit, attitude provider, mass and potential provider.FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, UnnormalizedSphericalHarmonicsProvider provider)
Build a propagator from FieldOrbit and potential provider.FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, UnnormalizedSphericalHarmonicsProvider provider, PropagationType initialType)
Build a propagator from orbit and potential provider.FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, T mass, double referenceRadius, T mu, double c20, double c30, double c40, double c50, double c60)
Build a propagator from FieldOrbit, mass and potential.FieldEcksteinHechlerPropagator(FieldOrbit<T> initialOrbit, T mass, UnnormalizedSphericalHarmonicsProvider provider)
Build a propagator from FieldOrbit, mass and potential provider.FieldKeplerianPropagator(FieldOrbit<T> initialFieldOrbit)
Build a propagator from orbit only.FieldKeplerianPropagator(FieldOrbit<T> initialFieldOrbit, AttitudeProvider attitudeProv)
Build a propagator from orbit and attitude provider.FieldKeplerianPropagator(FieldOrbit<T> initialFieldOrbit, AttitudeProvider attitudeProv, T mu)
Build a propagator from orbit, attitude provider and central attraction coefficient μ.FieldKeplerianPropagator(FieldOrbit<T> initialOrbit, AttitudeProvider attitudeProv, T mu, T mass)
Build propagator from orbit, attitude provider, central attraction coefficient μ and mass.FieldKeplerianPropagator(FieldOrbit<T> initialFieldOrbit, T mu)
Build a propagator from orbit and central attraction coefficient μ. -
Uses of FieldOrbit in org.orekit.propagation.analytical.intelsat
Methods in org.orekit.propagation.analytical.intelsat that return FieldOrbit Modifier and Type Method Description protected FieldOrbit<T>
FieldIntelsatElevenElementsPropagator. propagateOrbit(FieldAbsoluteDate<T> date, T[] parameters)
Extrapolate an orbit up to a specific target date. -
Uses of FieldOrbit in org.orekit.propagation.analytical.tle
Methods in org.orekit.propagation.analytical.tle that return FieldOrbit Modifier and Type Method Description FieldOrbit<T>
FieldTLEPropagator. propagateOrbit(FieldAbsoluteDate<T> date, T[] parameters)
Extrapolate an orbit up to a specific target date. -
Uses of FieldOrbit in org.orekit.propagation.conversion
Methods in org.orekit.propagation.conversion with parameters of type FieldOrbit Modifier and Type Method Description AbstractFieldIntegrator<T>
AbstractFieldIntegratorBuilder. buildIntegrator(FieldOrbit<T> orbit, OrbitType orbitType)
Build a first order integrator.AbstractFieldIntegrator<T>
FieldODEIntegratorBuilder. buildIntegrator(FieldOrbit<T> orbit, OrbitType orbitType)
Build a first order integrator. -
Uses of FieldOrbit in org.orekit.propagation.events
Constructors in org.orekit.propagation.events with parameters of type FieldOrbit Constructor Description FieldApsideDetector(FieldOrbit<T> orbit)
Build a new instance.FieldApsideDetector(T threshold, FieldOrbit<T> orbit)
Build a new instance.FieldNodeDetector(FieldOrbit<T> orbit, Frame frame)
Build a new instance.FieldNodeDetector(T threshold, FieldOrbit<T> orbit, Frame frame)
Build a new instance. -
Uses of FieldOrbit in org.orekit.propagation.integration
Methods in org.orekit.propagation.integration that return FieldOrbit Modifier and Type Method Description protected FieldOrbit<T>
FieldIntegratedEphemeris. propagateOrbit(FieldAbsoluteDate<T> date, T[] parameters)
Extrapolate an orbit up to a specific target date. -
Uses of FieldOrbit in org.orekit.propagation.numerical
Methods in org.orekit.propagation.numerical with parameters of type FieldOrbit Modifier and Type Method Description static <T extends CalculusFieldElement<T>>
double[][]FieldNumericalPropagator. tolerances(T dP, FieldOrbit<T> orbit, OrbitType type)
Estimate tolerance vectors for integrators.static <T extends CalculusFieldElement<T>>
double[][]FieldNumericalPropagator. tolerances(T dP, T dV, FieldOrbit<T> orbit, OrbitType type)
Estimate tolerance vectors for integrators when propagating in orbits. -
Uses of FieldOrbit in org.orekit.propagation.semianalytical.dsst
Methods in org.orekit.propagation.semianalytical.dsst with parameters of type FieldOrbit Modifier and Type Method Description static <T extends CalculusFieldElement<T>>
double[][]FieldDSSTPropagator. tolerances(T dP, FieldOrbit<T> orbit)
Estimate tolerance vectors for an AdaptativeStepsizeIntegrator.static <T extends CalculusFieldElement<T>>
double[][]FieldDSSTPropagator. tolerances(T dP, T dV, FieldOrbit<T> orbit)
Estimate tolerance vectors for an AdaptativeStepsizeIntegrator. -
Uses of FieldOrbit in org.orekit.propagation.semianalytical.dsst.forces
Methods in org.orekit.propagation.semianalytical.dsst.forces with parameters of type FieldOrbit Modifier and Type Method Description T[]
AbstractGaussianContribution.FieldGaussianShortPeriodicCoefficients. value(FieldOrbit<T> meanOrbit)
Evaluate the contributions of the short period terms.T[]
FieldShortPeriodTerms. value(FieldOrbit<T> meanOrbit)
Evaluate the contributions of the short period terms. -
Uses of FieldOrbit in org.orekit.propagation.semianalytical.dsst.utilities
Methods in org.orekit.propagation.semianalytical.dsst.utilities that return FieldOrbit Modifier and Type Method Description FieldOrbit<T>
FieldAuxiliaryElements. getOrbit()
Get the orbit.Constructors in org.orekit.propagation.semianalytical.dsst.utilities with parameters of type FieldOrbit Constructor Description FieldAuxiliaryElements(FieldOrbit<T> orbit, int retrogradeFactor)
Simple constructor. -
Uses of FieldOrbit in org.orekit.ssa.collision.shorttermencounter.probability.twod
Methods in org.orekit.ssa.collision.shorttermencounter.probability.twod that return FieldOrbit Modifier and Type Method Description FieldOrbit<T>
FieldShortTermEncounter2DDefinition. getOtherAtTCA()
Get other's orbit at time of closest approach.FieldOrbit<T>
FieldShortTermEncounter2DDefinition. getReferenceAtTCA()
Get reference's orbit at time of closest approach.Methods in org.orekit.ssa.collision.shorttermencounter.probability.twod with parameters of type FieldOrbit Modifier and Type Method Description <T extends CalculusFieldElement<T>>
FieldProbabilityOfCollision<T>AbstractShortTermEncounter1DNumerical2DPOCMethod. compute(FieldOrbit<T> primaryAtTCA, FieldStateCovariance<T> primaryCovariance, T primaryRadius, FieldOrbit<T> secondaryAtTCA, FieldStateCovariance<T> secondaryCovariance, T secondaryRadius, FieldUnivariateIntegrator<T> customIntegrator, int customMaxNbOfEval, double zeroThreshold)
Compute the probability of collision using parameters necessary for creating acollision definition
instance.<T extends CalculusFieldElement<T>>
FieldProbabilityOfCollision<T>AbstractShortTermEncounter2DPOCMethod. compute(FieldOrbit<T> primaryAtTCA, FieldStateCovariance<T> primaryCovariance, FieldOrbit<T> secondaryAtTCA, FieldStateCovariance<T> secondaryCovariance, T combinedRadius, double zeroThreshold)
Compute the probability of collision using parameters necessary for creating acollision definition
instance.default <T extends CalculusFieldElement<T>>
FieldProbabilityOfCollision<T>ShortTermEncounter2DPOCMethod. compute(FieldOrbit<T> primaryAtTCA, FieldStateCovariance<T> primaryCovariance, FieldOrbit<T> secondaryAtTCA, FieldStateCovariance<T> secondaryCovariance, T combinedRadius)
Compute the probability of collision using parameters necessary for creating acollision definition
instance.<T extends CalculusFieldElement<T>>
FieldProbabilityOfCollision<T>ShortTermEncounter2DPOCMethod. compute(FieldOrbit<T> primaryAtTCA, FieldStateCovariance<T> primaryCovariance, FieldOrbit<T> secondaryAtTCA, FieldStateCovariance<T> secondaryCovariance, T combinedRadius, double zeroThreshold)
Compute the probability of collision using parameters necessary for creating acollision definition
instance.default <T extends CalculusFieldElement<T>>
FieldProbabilityOfCollision<T>ShortTermEncounter2DPOCMethod. compute(FieldOrbit<T> primaryAtTCA, FieldStateCovariance<T> primaryCovariance, T primaryRadius, FieldOrbit<T> secondaryAtTCA, FieldStateCovariance<T> secondaryCovariance, T secondaryRadius)
Compute the probability of collision using parameters necessary for creating acollision definition
instance.Constructors in org.orekit.ssa.collision.shorttermencounter.probability.twod with parameters of type FieldOrbit Constructor Description FieldShortTermEncounter2DDefinition(FieldOrbit<T> referenceAtTCA, FieldStateCovariance<T> referenceCovariance, FieldOrbit<T> otherAtTCA, FieldStateCovariance<T> otherCovariance, T combinedRadius)
Constructor.FieldShortTermEncounter2DDefinition(FieldOrbit<T> referenceAtTCA, FieldStateCovariance<T> referenceCovariance, FieldOrbit<T> otherAtTCA, FieldStateCovariance<T> otherCovariance, T combinedRadius, EncounterLOFType encounterFrameType, double tcaTolerance)
Constructor.FieldShortTermEncounter2DDefinition(FieldOrbit<T> referenceAtTCA, FieldStateCovariance<T> referenceCovariance, T referenceRadius, FieldOrbit<T> otherAtTCA, FieldStateCovariance<T> otherCovariance, T otherRadius)
Constructor.FieldShortTermEncounter2DDefinition(FieldOrbit<T> referenceAtTCA, FieldStateCovariance<T> referenceCovariance, T referenceRadius, FieldOrbit<T> otherAtTCA, FieldStateCovariance<T> otherCovariance, T otherRadius, EncounterLOFType encounterFrameType, double tcaTolerance)
Constructor. -
Uses of FieldOrbit in org.orekit.utils
Methods in org.orekit.utils that return FieldOrbit Modifier and Type Method Description static <T extends CalculusFieldElement<T>>
FieldOrbit<T>Fieldifier. fieldify(Field<T> field, Orbit orbit)
Deprecated.
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