Uses of Class
org.orekit.orbits.FieldKeplerianOrbit
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Packages that use FieldKeplerianOrbit Package Description org.orekit.orbits This package provides classes to represent orbits.org.orekit.propagation.analytical Top level package for analytical propagators.org.orekit.propagation.analytical.tle.generation This package provides classes related to TLE generation. -
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Uses of FieldKeplerianOrbit in org.orekit.orbits
Methods in org.orekit.orbits that return FieldKeplerianOrbit Modifier and Type Method Description FieldKeplerianOrbit<T>FieldKeplerianOrbit. inFrame(Frame inertialFrame)Create a new object representing the same physical orbital state, but attached to a different reference frame.FieldKeplerianOrbit<T>FieldKeplerianOrbit. shiftedBy(double dt)Get a time-shifted orbit.FieldKeplerianOrbit<T>FieldKeplerianOrbit. shiftedBy(TimeOffset dt)Get a time-shifted instance.FieldKeplerianOrbit<T>FieldKeplerianOrbit. shiftedBy(T dt)Get a time-shifted orbit.FieldKeplerianOrbit<T>FieldKeplerianOrbit. withCachedPositionAngleType(PositionAngleType positionAngleType)Creates a new instance with the provided type used for caching.FieldKeplerianOrbit<T>FieldKeplerianOrbit. withKeplerianRates()Creates a new instance such thatPositionAngleBased.hasNonKeplerianRates()is false. -
Uses of FieldKeplerianOrbit in org.orekit.propagation.analytical
Methods in org.orekit.propagation.analytical that return FieldKeplerianOrbit 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, double referenceRadius, double mu, double c20, double c30, double c40, double c50, double m2Value, OsculatingToMeanConverter converter)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.FieldKeplerianOrbit<T>FieldBrouwerLyddanePropagator. propagateOrbit(FieldAbsoluteDate<T> date, T[] parameters)Propagate an orbit up to a specific target date. -
Uses of FieldKeplerianOrbit in org.orekit.propagation.analytical.tle.generation
Methods in org.orekit.propagation.analytical.tle.generation with parameters of type FieldKeplerianOrbit Modifier and Type Method Description static <T extends CalculusFieldElement<T>>
FieldTLE<T>TleGenerationUtil. newTLE(FieldKeplerianOrbit<T> keplerianOrbit, FieldTLE<T> templateTLE, T bStar, TimeScale utc)Builds a new TLE from Keplerian parameters and a template for TLE data.
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