fr.cnes.genopus.nonWidget.vehicle.aeroCoeffs

Class CustomAeroCoeffByAoAAndMach

java.lang.Object

fr.cnes.genopus.nonWidget.vehicle.aeroCoeffs.CustomAeroCoeffByAoAAndMach

All Implemented Interfaces:

Serializable, org.orekit.parameter.IParamDiffFunction, org.orekit.parameter.IParameterizable, org.orekit.parameter.IParameterizableFunction

public class CustomAeroCoeffByAoAAndMach
extends Object
implements org.orekit.parameter.IParamDiffFunction

Aerodynamic coefficient as a function of two variables: the angle of attack and the mach number.

Author:

sumelzi

See Also:

Serialized Form

Constructor Summary

Constructors

Constructor and Description
CustomAeroCoeffByAoAAndMach(double[] anglesOfAttack, double[] machNumbers, double[][] coeffs, org.orekit.forces.atmospheres.Atmosphere atmosphere, org.orekit.bodies.ExtendedOneAxisEllipsoid earthShape) Creates a new instance.

Method Summary

Methods

Modifier and Type	Method and Description
double	derivativeValue(org.orekit.parameter.Parameter p, org.orekit.propagation.SpacecraftState s)
double[]	getAoAArray() Getter for the Angles of Attack array used for the function definition).
double[][]	getDataArray() Getter for the aerodynamic coefficients array used for the function definition.
org.apache.commons.math3.analysis.interpolation.BiLinearIntervalsFunction	getFunction() Getter for the function.
double[]	getMachArray() Getter for the Mach numbers array used for the function definition.
ArrayList<org.orekit.parameter.Parameter>	getParameters()
boolean	isDifferentiableBy(org.orekit.parameter.Parameter p)
boolean	supportsParameter(org.orekit.parameter.Parameter param)
String	toString()
double	value(org.orekit.propagation.SpacecraftState state)

Methods inherited from class java.lang.Object

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

Constructor Detail

CustomAeroCoeffByAoAAndMach

public CustomAeroCoeffByAoAAndMach(double[] anglesOfAttack,
                           double[] machNumbers,
                           double[][] coeffs,
                           org.orekit.forces.atmospheres.Atmosphere atmosphere,
                           org.orekit.bodies.ExtendedOneAxisEllipsoid earthShape)

Creates a new instance.

Parameters:

anglesOfAttack - array of angles of attack (rad)

machNumbers - array of mach numbers

coeffs - array of arrays of aerodynamic coefficients

atmosphere - atmosphere model

earthShape - earth shape

Method Detail

value

public double value(org.orekit.propagation.SpacecraftState state)

Specified by:

value in interface org.orekit.parameter.IParameterizableFunction

getParameters

public ArrayList<org.orekit.parameter.Parameter> getParameters()

Specified by:

getParameters in interface org.orekit.parameter.IParameterizable

supportsParameter

public boolean supportsParameter(org.orekit.parameter.Parameter param)

Specified by:

supportsParameter in interface org.orekit.parameter.IParameterizable

derivativeValue

public double derivativeValue(org.orekit.parameter.Parameter p,
                     org.orekit.propagation.SpacecraftState s)

Specified by:

derivativeValue in interface org.orekit.parameter.IParamDiffFunction

isDifferentiableBy

public boolean isDifferentiableBy(org.orekit.parameter.Parameter p)

Specified by:

isDifferentiableBy in interface org.orekit.parameter.IParamDiffFunction

getAoAArray

public double[] getAoAArray()

Getter for the Angles of Attack array used for the function definition).

Returns:

the Angles of Attack array

getMachArray

public double[] getMachArray()

Getter for the Mach numbers array used for the function definition.

Returns:

the Mach numbers array

getDataArray

public double[][] getDataArray()

Getter for the aerodynamic coefficients array used for the function definition.

Returns:

the aerodynamic coefficients array

getFunction

public org.apache.commons.math3.analysis.interpolation.BiLinearIntervalsFunction getFunction()

Getter for the function.

Returns:

the function

toString

public String toString()

Overrides:

toString in class Object