fr.cnes.genopus.nonWidget.vehicle.aeroCoeffs

Class CustomAeroCoeffByAltitude

java.lang.Object

fr.cnes.genopus.nonWidget.vehicle.aeroCoeffs.CustomAeroCoeffByOneVarAbstract

fr.cnes.genopus.nonWidget.vehicle.aeroCoeffs.CustomAeroCoeffByAltitude

All Implemented Interfaces:

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

public class CustomAeroCoeffByAltitude
extends CustomAeroCoeffByOneVarAbstract

Aerodynamic coefficient function of the spacecraft altitude.

Author:

sumelzi

See Also:

Serialized Form

Constructor Summary

Constructors

Constructor and Description
CustomAeroCoeffByAltitude(Double[] xVariable, Double[] yVariable, org.orekit.bodies.ExtendedOneAxisEllipsoid earthShape) Creates a new instance entering the x and y variables as doubles.

Method Summary

Methods

Modifier and Type	Method and Description
protected double	computeXVariable(org.orekit.propagation.SpacecraftState state) Computes the x variable from the spacecraft state.

Methods inherited from class fr.cnes.genopus.nonWidget.vehicle.aeroCoeffs.CustomAeroCoeffByOneVarAbstract

derivativeValue, extendedVectorY, getFunction, getParameters, getXArray, getYArray, isDifferentiableBy, supportsParameter, toString, value

Methods inherited from class java.lang.Object

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

Constructor Detail

CustomAeroCoeffByAltitude

public CustomAeroCoeffByAltitude(Double[] xVariable,
                         Double[] yVariable,
                         org.orekit.bodies.ExtendedOneAxisEllipsoid earthShape)

Creates a new instance entering the x and y variables as doubles.

Parameters:

xVariable - array of x variables (altitude (m))

yVariable - array of y variables (aerodynamic coefficient)

earthShape - Earth shape

Method Detail

computeXVariable

protected double computeXVariable(org.orekit.propagation.SpacecraftState state)
                           throws NonWidgetException

Computes the x variable from the spacecraft state.

Specified by:

computeXVariable in class CustomAeroCoeffByOneVarAbstract

Parameters:

state - the spacecraft state

Returns:

the x variable

Throws:

NonWidgetException - if the orbit in state is not valid.