fr.cnes.sirius.patrius.progmission

Class KeplerianParamUtils

java.lang.Object

fr.cnes.sirius.patrius.progmission.KeplerianParamUtils

public final class KeplerianParamUtils
extends Object

Utility class describing keplerian characteristics features imported from CelestLab.

Since:

4.17

Author:

vermeulenp, guillemettem

Nested Class Summary

Nested Classes

Modifier and Type	Class and Description
static class	KeplerianParamUtils.ApsParamType Enumerate containing the existing parameter types that can be provided for conversion

Method Summary

Modifier and Type	Method and Description
static double[][]	computeAllApsParam(KeplerianParamUtils.ApsParamType typeIn1, double[] param1, KeplerianParamUtils.ApsParamType typeIn2, double[] param2) Compute all orbit parameter types for each entry of the provided inputs.
static double[][]	computeAllApsParam(KeplerianParamUtils.ApsParamType typeIn1, double[] param1, KeplerianParamUtils.ApsParamType typeIn2, double[] param2, double mu) Compute all orbit parameter types for each entry of the provided inputs.
static double[]	computeAllApsParam(KeplerianParamUtils.ApsParamType typeIn1, double param1, KeplerianParamUtils.ApsParamType typeIn2, double param2) Compute all orbit parameter types based on the provided inputs.
static double[]	computeAllApsParam(KeplerianParamUtils.ApsParamType typeIn1, double param1, KeplerianParamUtils.ApsParamType typeIn2, double param2, double mu) Compute all orbit parameter types based on the provided inputs.
static double[]	computeApsParam(KeplerianParamUtils.ApsParamType typeIn1, double[] param1, KeplerianParamUtils.ApsParamType typeIn2, double[] param2, KeplerianParamUtils.ApsParamType typeOut) Compute the desired orbit parameter type based on the provided inputs.
static double[]	computeApsParam(KeplerianParamUtils.ApsParamType typeIn1, double[] param1, KeplerianParamUtils.ApsParamType typeIn2, double[] param2, KeplerianParamUtils.ApsParamType typeOut, double mu) Compute the desired orbit parameter type based on the provided inputs.
static double	computeApsParam(KeplerianParamUtils.ApsParamType typeIn1, double param1, KeplerianParamUtils.ApsParamType typeIn2, double param2, KeplerianParamUtils.ApsParamType typeOut) Compute the desired orbit parameter type based on the provided inputs.
static double	computeApsParam(KeplerianParamUtils.ApsParamType typeIn1, double param1, KeplerianParamUtils.ApsParamType typeIn2, double param2, KeplerianParamUtils.ApsParamType typeOut, double mu) Compute the desired orbit parameter type based on the provided inputs.

Methods inherited from class java.lang.Object

clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait

Method Detail

computeAllApsParam

public static double[][] computeAllApsParam(KeplerianParamUtils.ApsParamType typeIn1,
                                            double[] param1,
                                            KeplerianParamUtils.ApsParamType typeIn2,
                                            double[] param2)
                                     throws PatriusException

Compute all orbit parameter types for each entry of the provided inputs.
Constants.EGM96_EARTH_MU will be used as the gravitational parameter.

Inspired by the Celestlab method CL_kp_apsConvert.

Parameters:

typeIn1 - Parameter type of param1

param1 - Array of values of the first parameter

typeIn2 - Parameter type of param2

param2 - Array of values of the second parameter

Returns:

the array containing all parameter types for each entry.

Throws:

PatriusException - if param1 and param2 don't have the same length

computeAllApsParam

public static double[][] computeAllApsParam(KeplerianParamUtils.ApsParamType typeIn1,
                                            double[] param1,
                                            KeplerianParamUtils.ApsParamType typeIn2,
                                            double[] param2,
                                            double mu)
                                     throws PatriusException

Compute all orbit parameter types for each entry of the provided inputs.

Inspired by the Celestlab method CL_kp_apsConvert.

Parameters:

typeIn1 - Parameter type of param1

param1 - Array of values of the first parameter

typeIn2 - Parameter type of param2

param2 - Array of values of the second parameter

mu - Gravitational parameter of the central first body (m^3/s^2)

Returns:

the array containing all parameter types for each entry.

Throws:

PatriusException - if param1 and param2 don't have the same length

computeAllApsParam

public static double[] computeAllApsParam(KeplerianParamUtils.ApsParamType typeIn1,
                                          double param1,
                                          KeplerianParamUtils.ApsParamType typeIn2,
                                          double param2)
                                   throws PatriusException

Compute all orbit parameter types based on the provided inputs.
Constants.EGM96_EARTH_MU will be used as the gravitational parameter.

Inspired by the Celestlab method CL_kp_apsConvert.

Parameters:

typeIn1 - Parameter type of param1

param1 - Value of the first parameter

typeIn2 - Parameter type of param2

param2 - Value of the second parameter

Returns:

the corresponding parameter type

Throws:

PatriusException - if incompatible or unhandled types are provided

computeAllApsParam

public static double[] computeAllApsParam(KeplerianParamUtils.ApsParamType typeIn1,
                                          double param1,
                                          KeplerianParamUtils.ApsParamType typeIn2,
                                          double param2,
                                          double mu)
                                   throws PatriusException

Compute all orbit parameter types based on the provided inputs.

Inspired by the Celestlab method CL_kp_apsConvert.

Parameters:

typeIn1 - Parameter type of param1

param1 - Value of the first parameter

typeIn2 - Parameter type of param2

param2 - Value of the second parameter

mu - Gravitational parameter of the central first body (m^3/s^2)

Returns:

the corresponding parameter type

Throws:

PatriusException - if incompatible or unhandled types are provided

computeApsParam

public static double[] computeApsParam(KeplerianParamUtils.ApsParamType typeIn1,
                                       double[] param1,
                                       KeplerianParamUtils.ApsParamType typeIn2,
                                       double[] param2,
                                       KeplerianParamUtils.ApsParamType typeOut)
                                throws PatriusException

Compute the desired orbit parameter type based on the provided inputs.
Constants.EGM96_EARTH_MU will be used as the gravitational parameter.

Inspired by the Celestlab method CL_kp_apsConvert.

Parameters:

typeIn1 - Parameter type of param1

param1 - Array of values of the first parameter

typeIn2 - Parameter type of param2

param2 - Array of values of the second parameter

typeOut - Orbit parameter type to compute

Returns:

the corresponding array of desired parameter type

Throws:

PatriusException - if param1 and param2 don't have the same length

computeApsParam

public static double[] computeApsParam(KeplerianParamUtils.ApsParamType typeIn1,
                                       double[] param1,
                                       KeplerianParamUtils.ApsParamType typeIn2,
                                       double[] param2,
                                       KeplerianParamUtils.ApsParamType typeOut,
                                       double mu)
                                throws PatriusException

Compute the desired orbit parameter type based on the provided inputs.

Inspired by the Celestlab method CL_kp_apsConvert.

Parameters:

typeIn1 - Parameter type of param1

param1 - Array of values of the first parameter

typeIn2 - Parameter type of param2

param2 - Array of values of the second parameter

typeOut - Orbit parameter type to compute

mu - Gravitational parameter of the central first body (m^3/s^2)

Returns:

the corresponding array of desired parameter type

Throws:

PatriusException - if param1 and param2 don't have the same length

computeApsParam

public static double computeApsParam(KeplerianParamUtils.ApsParamType typeIn1,
                                     double param1,
                                     KeplerianParamUtils.ApsParamType typeIn2,
                                     double param2,
                                     KeplerianParamUtils.ApsParamType typeOut)
                              throws PatriusException

Compute the desired orbit parameter type based on the provided inputs.
Constants.EGM96_EARTH_MU will be used as the gravitational parameter.

Inspired by the Celestlab method CL_kp_apsConvert.

Parameters:

typeIn1 - Parameter type of param1

param1 - Value of the first parameter

typeIn2 - Parameter type of param2

param2 - Value of the second parameter

typeOut - Orbit parameter type to compute

Returns:

the corresponding parameter type

Throws:

PatriusException - if incompatible or unhandled types are provided

computeApsParam

public static double computeApsParam(KeplerianParamUtils.ApsParamType typeIn1,
                                     double param1,
                                     KeplerianParamUtils.ApsParamType typeIn2,
                                     double param2,
                                     KeplerianParamUtils.ApsParamType typeOut,
                                     double mu)
                              throws PatriusException

Compute the desired orbit parameter type based on the provided inputs.

Inspired by the Celestlab method CL_kp_apsConvert.

Parameters:

typeIn1 - Parameter type of param1

param1 - Value of the first parameter

typeIn2 - Parameter type of param2

param2 - Value of the second parameter

typeOut - Orbit parameter type to compute

mu - Gravitational parameter of the central first body (m^3/s^2)

Returns:

the corresponding parameter type

Throws:

PatriusException - if incompatible or unhandled types are provided