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
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Constructor Summary |
CustomAeroCoeffByAltitude(Double[] xVariable,
Double[] yVariable,
org.orekit.bodies.ExtendedOneAxisEllipsoid earthShape)
Creates a new instance entering the x and y variables as doubles. |
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Method Summary |
protected double |
computeXVariable(org.orekit.propagation.SpacecraftState state)
Computes the x variable from the spacecraft state. |
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
computeXVariable
protected double computeXVariable(org.orekit.propagation.SpacecraftState state)
- Computes the x variable from the spacecraft state.
- Specified by:
computeXVariable in class CustomAeroCoeffByOneVarAbstract
- Parameters:
state - the spacecraft state
- Returns:
- the x variable
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