fr.cnes.sirius.patrius.assembly.models.aerocoeffs

Class AeroCoeffConstant

java.lang.Object

fr.cnes.sirius.patrius.math.parameter.Parameterizable

fr.cnes.sirius.patrius.math.parameter.ParamDiffFunction

fr.cnes.sirius.patrius.assembly.models.aerocoeffs.AeroCoeffConstant

All Implemented Interfaces:

AerodynamicCoefficient, IParamDiffFunction, IParameterizable, IParameterizableFunction, Serializable

public class AeroCoeffConstant
extends ParamDiffFunction
implements AerodynamicCoefficient

Constant aerodynamic coefficient.

Since:

4.1

Version:

$Id$

Author:

Emmanuel Bignon

See Also:

Serialized Form

Constructor Summary

Constructors

Constructor and Description
AeroCoeffConstant(Parameter aeroCoeffIn) Constructor.

Method Summary

Modifier and Type	Method and Description
double	derivativeValue(Parameter p, SpacecraftState s) Compute the derivative value with respect to the input parameter.
double	getAerodynamicCoefficient() Getter for the aerodynamic coefficient.
ArrayList<Parameter>	getParameters() Get the supported parameters.
AerodynamicCoefficientType	getType() Returns type of aerodynamic coefficient.
double	value(SpacecraftState state) Getting the value of the function.

Methods inherited from class fr.cnes.sirius.patrius.math.parameter.ParamDiffFunction

isDifferentiableBy, supportsParameter

Methods inherited from class fr.cnes.sirius.patrius.math.parameter.Parameterizable

addParameter

Methods inherited from class java.lang.Object

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

Methods inherited from interface fr.cnes.sirius.patrius.math.parameter.IParamDiffFunction

isDifferentiableBy

Methods inherited from interface fr.cnes.sirius.patrius.math.parameter.IParameterizable

supportsParameter

Constructor Detail

AeroCoeffConstant

public AeroCoeffConstant(Parameter aeroCoeffIn)

Constructor.

Parameters:

aeroCoeffIn - aerodynamic coefficient

Method Detail

value

public double value(SpacecraftState state)

Getting the value of the function.

Specified by:

value in interface IParameterizableFunction

Parameters:

state - the spacecraft state

Returns:

the value of the function.

getAerodynamicCoefficient

public double getAerodynamicCoefficient()

Getter for the aerodynamic coefficient.

Returns:

the aerodynamic coefficient

derivativeValue

public double derivativeValue(Parameter p,
                              SpacecraftState s)

Compute the derivative value with respect to the input parameter.

Specified by:

derivativeValue in interface IParamDiffFunction

Parameters:

p - parameter

s - current state

Returns:

the derivative value

getParameters

public ArrayList<Parameter> getParameters()

Get the supported parameters.

Specified by:

getParameters in interface IParameterizable

Overrides:

getParameters in class Parameterizable

Returns:

list of supported parameters

getType

public AerodynamicCoefficientType getType()

Returns type of aerodynamic coefficient.

Specified by:

getType in interface AerodynamicCoefficient

Returns:

type of aerodynamic coefficient