fr.cnes.genopus.orbits

Enum MeanOrbitPropagationModel

java.lang.Object

java.lang.Enum<MeanOrbitPropagationModel>

fr.cnes.genopus.orbits.MeanOrbitPropagationModel

All Implemented Interfaces:

Serializable, Comparable<MeanOrbitPropagationModel>

public enum MeanOrbitPropagationModel
extends Enum<MeanOrbitPropagationModel>

Enumeration about the available mean orbit propagation models.

Author:

Alex Nardi HISTORIQUE VERSION:2.4:DM:DM-1578:06/04/2023:[GENOPUS] Montee de niveau GENIUS V1.12 et de PATRIUS ainsi que de PATRIUS_DATASET FIN-HISTORIQUE

Enum Constant Summary

Enum Constants

Enum Constant and Description
ECKSTEIN_HECHLER Eckstein-Hechler.
LYDDANE_LONG_PERIOD Lyddane long period.
LYDDANE_SECULAR Lyddane secular.

Method Summary

Modifier and Type	Method and Description
abstract fr.cnes.sirius.patrius.propagation.MeanOsculatingElementsProvider	buildModel(fr.cnes.sirius.patrius.orbits.Orbit meanOrbit, double req, double mu, double j2, double j3, double j4, double j5, double j6, fr.cnes.sirius.patrius.propagation.ParametersType parametersType) Build PATRIUS mean orbit propagation model.
static MeanOrbitPropagationModel	valueOf(String name) Returns the enum constant of this type with the specified name.
static MeanOrbitPropagationModel[]	values() Returns an array containing the constants of this enum type, in the order they are declared.

Methods inherited from class java.lang.Enum

clone, compareTo, equals, finalize, getDeclaringClass, hashCode, name, ordinal, toString, valueOf

Methods inherited from class java.lang.Object

getClass, notify, notifyAll, wait, wait, wait

Enum Constant Detail

LYDDANE_SECULAR

public static final MeanOrbitPropagationModel LYDDANE_SECULAR

Lyddane secular.

LYDDANE_LONG_PERIOD

public static final MeanOrbitPropagationModel LYDDANE_LONG_PERIOD

Lyddane long period.

ECKSTEIN_HECHLER

public static final MeanOrbitPropagationModel ECKSTEIN_HECHLER

Eckstein-Hechler.

Method Detail

values

public static MeanOrbitPropagationModel[] values()

Returns an array containing the constants of this enum type, in the order they are declared. This method may be used to iterate over the constants as follows:

for (MeanOrbitPropagationModel c : MeanOrbitPropagationModel.values())
    System.out.println(c);

Returns:

an array containing the constants of this enum type, in the order they are declared

valueOf

public static MeanOrbitPropagationModel valueOf(String name)

Returns the enum constant of this type with the specified name. The string must match exactly an identifier used to declare an enum constant in this type. (Extraneous whitespace characters are not permitted.)

Parameters:

name - the name of the enum constant to be returned.

Returns:

the enum constant with the specified name

Throws:

IllegalArgumentException - if this enum type has no constant with the specified name

NullPointerException - if the argument is null

buildModel

public abstract fr.cnes.sirius.patrius.propagation.MeanOsculatingElementsProvider buildModel(fr.cnes.sirius.patrius.orbits.Orbit meanOrbit,
                                                                                             double req,
                                                                                             double mu,
                                                                                             double j2,
                                                                                             double j3,
                                                                                             double j4,
                                                                                             double j5,
                                                                                             double j6,
                                                                                             fr.cnes.sirius.patrius.propagation.ParametersType parametersType)
                                                                                      throws fr.cnes.sirius.patrius.utils.exception.PatriusException

Build PATRIUS mean orbit propagation model.

Parameters:

meanOrbit - mean orbit

req - Earth equatorial radius

mu - Earth mu

j2 - Earth potential J2

j3 - Earth potential J3

j4 - Earth potential J4

j5 - Earth potential J5

j6 - Earth potential J6

parametersType - parameters type

Returns:

osculating orbit

Throws:

fr.cnes.sirius.patrius.utils.exception.PatriusException - thrown if conversion failed