public class AeroCoeffByAltitude extends AbstractAeroCoeff1D
Constructor and Description |
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AeroCoeffByAltitude(double[] xVariables,
double[] yVariables,
EllipsoidBodyShape earthShapeIn)
Constructor.
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Modifier and Type | Method and Description |
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protected double |
computeXVariable(SpacecraftState state)
Computes the x variable from the spacecraft state.
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AerodynamicCoefficientType |
getType()
Returns type of aerodynamic coefficient.
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derivativeValue, getFunction, getParameters, getXArray, getYArray, isDifferentiableBy, supportsParameter, toString, value
public AeroCoeffByAltitude(double[] xVariables, double[] yVariables, EllipsoidBodyShape earthShapeIn)
xVariables
- array of x variables (altitude (m))yVariables
- array of y variables (aerodynamic coefficient)earthShapeIn
- Earth shapeprotected double computeXVariable(SpacecraftState state)
computeXVariable
in class AbstractAeroCoeff1D
state
- the spacecraft statepublic AerodynamicCoefficientType getType()
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