fr.cnes.sirius.patrius.assembly.vehicle

Class AerodynamicProperties

java.lang.Object

fr.cnes.sirius.patrius.assembly.vehicle.AerodynamicProperties

All Implemented Interfaces:

Serializable

public class AerodynamicProperties
extends Object
implements Serializable

This class defines an aerodynamic property to be applyied to aerodynamic parts of a vehicle (PATRIUS assembly). It has a dual nature, actually it is either an AeroGlobalProperty or an AeroSphereProperty depending on the constructor used.

Since:

4.1

Version:

$Id$

Author:

Emmanuel Bignon

See Also:

Serialized Form

Constructor Summary

Constructors

Constructor and Description
AerodynamicProperties(Sphere sphere, AerodynamicCoefficient dragCoefIn, AerodynamicCoefficient liftCoefIn) Constructor.
AerodynamicProperties(Sphere sphere, double dragCoefIn) Constructor.
AerodynamicProperties(VehicleSurfaceModel vehicleSurface, double dragCoefIn, double liftCoefIn) Constructor.

Method Summary

Modifier and Type	Method and Description
double	getConstantDragCoef() Get the drag coefficient.
double	getConstantLiftCoef() Get the lift coefficient.
AerodynamicCoefficient	getDragCoef() Get the drag coefficient.
AerodynamicCoefficientType	getFunctionType() Get the type of the aerodynamic coefficients functions among: - Coefficients as a function of altitude, - Coefficients as a function of angle of attack - Coefficients as a function of Mach number - Coefficients as a function of Mach number and angle of attack.
AerodynamicCoefficient	getLiftCoef() Get the lift coefficient.
VehicleSurfaceModel	getVehicleSurfaceModel() Get the surface model.
void	setAerodynamicProperties(AssemblyBuilder builder, String mainPartName, double multiplicativeFactor) Set aerodynamic property to a part (it modifies vehicle surface model as a function of the multplicative factor).
String	toString()

Methods inherited from class java.lang.Object

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

Constructor Detail

AerodynamicProperties

public AerodynamicProperties(Sphere sphere,
                             AerodynamicCoefficient dragCoefIn,
                             AerodynamicCoefficient liftCoefIn)
                      throws PatriusException

Constructor.

Parameters:

sphere - the spherical vehicle shape

dragCoefIn - drag coefficient given as a function of the spacecraftstate

liftCoefIn - lift coefficient given as a function of the spacecraftstate

Throws:

PatriusException - thrown if sphere is null

AerodynamicProperties

public AerodynamicProperties(VehicleSurfaceModel vehicleSurface,
                             double dragCoefIn,
                             double liftCoefIn)
                      throws PatriusException

Constructor.

Parameters:

vehicleSurface - the vehicle surface model

dragCoefIn - constant drag coefficient

liftCoefIn - constant lift coefficient

Throws:

PatriusException - thrown if the vehicle surface model is null

AerodynamicProperties

public AerodynamicProperties(Sphere sphere,
                             double dragCoefIn)
                      throws PatriusException

Constructor.

Parameters:

sphere - the spherical vehicle shape

dragCoefIn - constant drag coefficient

Throws:

PatriusException - thrown if sphere is null

Method Detail

setAerodynamicProperties

public void setAerodynamicProperties(AssemblyBuilder builder,
                                     String mainPartName,
                                     double multiplicativeFactor)

Set aerodynamic property to a part (it modifies vehicle surface model as a function of the multplicative factor).

Parameters:

builder - assembly builder

mainPartName - main part name

multiplicativeFactor - the multiplicative factor (applied to the reference surface)

getFunctionType

public AerodynamicCoefficientType getFunctionType()
                                           throws PatriusException

Get the type of the aerodynamic coefficients functions among:
- Coefficients as a function of altitude,
- Coefficients as a function of angle of attack
- Coefficients as a function of Mach number
- Coefficients as a function of Mach number and angle of attack.

Returns:

the type of function (see AerodynamicCoefficientType enumeration)

Throws:

PatriusException - thrown if drag and lift coefficients are not of the same type

getDragCoef

public AerodynamicCoefficient getDragCoef()

Get the drag coefficient.

Returns:

the drag coefficient

getLiftCoef

public AerodynamicCoefficient getLiftCoef()

Get the lift coefficient.

Returns:

the lift coefficient

getVehicleSurfaceModel

public VehicleSurfaceModel getVehicleSurfaceModel()

Get the surface model.

Returns:

the surface model

getConstantDragCoef

public double getConstantDragCoef()
                           throws PatriusException

Get the drag coefficient.

Returns:

the drag coefficient

Throws:

PatriusException - if the drag coefficient is not constant (use getDragCoef() instead)

getConstantLiftCoef

public double getConstantLiftCoef()
                           throws PatriusException

Get the lift coefficient.

Returns:

the lift coefficient

Throws:

PatriusException - if the lift coefficient is not constant (use getLiftCoef() instead)

toString

public String toString()

Overrides:

toString in class Object