Uses of Class
fr.cnes.genopus.nonWidget.vehicle.aeroCoeffs.CustomAeroCoeffByOneVarAbstract

Packages that use CustomAeroCoeffByOneVarAbstract

Package	Description
fr.cnes.genopus.nonWidget.vehicle.aeroCoeffs	Package containing some objects related to vehicle aerodynamic coefficients functions intended to be added to PATRIUS.
fr.cnes.genopus.vehicle	Package containing some widgets defining a vehicle.

Uses of CustomAeroCoeffByOneVarAbstract in fr.cnes.genopus.nonWidget.vehicle.aeroCoeffs

Subclasses of CustomAeroCoeffByOneVarAbstract in fr.cnes.genopus.nonWidget.vehicle.aeroCoeffs

Modifier and Type	Class and Description
class	CustomAeroCoeffByAltitude Aerodynamic coefficient function of the spacecraft altitude.
class	CustomAeroCoeffByAoA Aerodynamic coefficient function of the spacecraft angle of attack.
class	CustomAeroCoeffByMach Aerodynamic coefficient as a function of the mach number.

Uses of CustomAeroCoeffByOneVarAbstract in fr.cnes.genopus.vehicle

Methods in fr.cnes.genopus.vehicle with parameters of type CustomAeroCoeffByOneVarAbstract

Modifier and Type	Method and Description
void	GPAeroCoeffByOneVar.setDefaultValue(CustomAeroCoeffByOneVarAbstract dragCoefFunction, CustomAeroCoeffByOneVarAbstract liftCoefFunction) Setter for the default values for abscisas, drag coefficients and lift coefficients.
void	GPAeroCoeffByOneVar.setSavedValue(CustomAeroCoeffByOneVarAbstract dragCoefFunction, CustomAeroCoeffByOneVarAbstract liftCoefFunction) Setter for the saved values for abscisas, drag coefficients and lift coefficients.
void	GPAeroCoeffByOneVar.setValue(CustomAeroCoeffByOneVarAbstract dragCoefFunction, CustomAeroCoeffByOneVarAbstract liftCoefFunction) Setter for the values for abscisas, drag coefficients and lift coefficients.

Constructors in fr.cnes.genopus.vehicle with parameters of type CustomAeroCoeffByOneVarAbstract

Constructor and Description
GPAeroCoeffByOneVar(String widgetId, String label, fr.cnes.genius.highLevel.GEntryRealVector varRealVec, CustomAeroCoeffByOneVarAbstract dragCoefFunction, CustomAeroCoeffByOneVarAbstract liftCoefFunction) Creates a new instance.