public class AeroCoeffByAltitude extends AbstractAeroCoeff1D
| Constructor and Description |
|---|
AeroCoeffByAltitude(double[] xVariables,
double[] yVariables,
OneAxisEllipsoid earthShapeIn)
Constructor.
|
| Modifier and Type | Method and Description |
|---|---|
protected double |
computeXVariable(SpacecraftState state)
Computes the x variable from the spacecraft state.
|
AerodynamicCoefficientType |
getType()
Returns type of aerodynamic coefficient.
|
derivativeValue, getFunction, getParameters, getXArray, getYArray, isDifferentiableBy, supportsParameter, toString, valuepublic AeroCoeffByAltitude(double[] xVariables,
double[] yVariables,
OneAxisEllipsoid 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 AbstractAeroCoeff1Dstate - the spacecraft statepublic AerodynamicCoefficientType getType()
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