Uses of Class
fr.cnes.sirius.patrius.stela.orbits.OrbitNatureConverter

Packages that use OrbitNatureConverter

Package	Description
fr.cnes.sirius.patrius.stela
fr.cnes.sirius.patrius.stela.forces
fr.cnes.sirius.patrius.stela.forces.drag
fr.cnes.sirius.patrius.stela.forces.noninertial
fr.cnes.sirius.patrius.stela.forces.radiation
fr.cnes.sirius.patrius.stela.propagation

Uses of OrbitNatureConverter in fr.cnes.sirius.patrius.stela

Constructors in fr.cnes.sirius.patrius.stela with parameters of type OrbitNatureConverter

Constructor and Description
PerigeeAltitudeDetector(double maxCheck, double threshold, double altitudeIn, double earthRadiusIn, OrbitNatureConverter orbitConverterIn) Build a new altitude detector, with osculating perigee.
PerigeeAltitudeDetector(double maxCheck, double threshold, double altitudeIn, double earthRadiusIn, OrbitNatureConverter orbitConverterIn, EventDetector.Action ascending, EventDetector.Action descending) Build a new altitude detector, with osculating perigee.
PerigeeAltitudeDetector(double maxCheck, double threshold, double altitudeIn, double earthRadiusIn, OrbitNatureConverter orbitConverterIn, EventDetector.Action ascending, EventDetector.Action descending, boolean removeAscending, boolean removeDescending) Build a new altitude detector, with osculating perigee.

Uses of OrbitNatureConverter in fr.cnes.sirius.patrius.stela.forces

Methods in fr.cnes.sirius.patrius.stela.forces with parameters of type OrbitNatureConverter

Modifier and Type	Method and Description
abstract double[]	AbstractStelaGaussContribution.computePerturbation(StelaEquinoctialOrbit orbit, OrbitNatureConverter converter) Compute the dE/dt force derivatives for a given spacecraft state.

Uses of OrbitNatureConverter in fr.cnes.sirius.patrius.stela.forces.drag

Methods in fr.cnes.sirius.patrius.stela.forces.drag with parameters of type OrbitNatureConverter

Modifier and Type	Method and Description
double[]	StelaAtmosphericDrag.computePerturbation(StelaEquinoctialOrbit orbit, OrbitNatureConverter converter) Compute the dE/dt force derivatives for a given spacecraft state.

Uses of OrbitNatureConverter in fr.cnes.sirius.patrius.stela.forces.noninertial

Methods in fr.cnes.sirius.patrius.stela.forces.noninertial with parameters of type OrbitNatureConverter

Modifier and Type	Method and Description
double[]	NonInertialContribution.computePerturbation(StelaEquinoctialOrbit orbit, OrbitNatureConverter converter) Compute the dE/dt force derivatives for a given spacecraft state.

Uses of OrbitNatureConverter in fr.cnes.sirius.patrius.stela.forces.radiation

Methods in fr.cnes.sirius.patrius.stela.forces.radiation with parameters of type OrbitNatureConverter

Modifier and Type	Method and Description
double[]	SRPSquaring.computePerturbation(StelaEquinoctialOrbit orbit, OrbitNatureConverter converter) Compute the dE/dt force derivatives for a given spacecraft state.
double[]	StelaSRPSquaring.computePerturbation(StelaEquinoctialOrbit orbit, OrbitNatureConverter converter) Compute the dE/dt force derivatives for a given spacecraft state.

Uses of OrbitNatureConverter in fr.cnes.sirius.patrius.stela.propagation

Methods in fr.cnes.sirius.patrius.stela.propagation that return OrbitNatureConverter

Modifier and Type	Method and Description
OrbitNatureConverter	StelaGTOPropagator.getOrbitNatureConverter() Get the mean/osculating orbit converter.

Constructors in fr.cnes.sirius.patrius.stela.propagation with parameters of type OrbitNatureConverter

Constructor and Description
ForcesStepHandler(OrbitNatureConverter converterIn, NonInertialContribution nonInertialContributionIn) Constructor.