Modifier and Type | Interface and Description |
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interface |
AerodynamicCoefficient
Interface for aerodynamic coefficients.
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Modifier and Type | Class and Description |
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class |
AbstractAeroCoeff1D
Aerodynamic coefficient function of one variable.
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class |
AeroCoeffByAltitude
Aerodynamic coefficient function of the spacecraft altitude.
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class |
AeroCoeffByAoA
Aerodynamic coefficient function of the spacecraft angle of attack.
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class |
AeroCoeffByAoAAndMach
Aerodynamic coefficient function of the spacecraft angle of attack and Mach number.
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class |
AeroCoeffByMach
Aerodynamic coefficient function of the spacecraft Mach number.
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class |
AeroCoeffConstant
Constant aerodynamic coefficient.
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Modifier and Type | Class and Description |
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class |
CnCookModel
This class implements Cook normal coefficient to a facet.
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class |
CtCookModel
This class implements Cook tangential coefficient to a facet.
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Constructor and Description |
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AeroAttitudeLaw(IParameterizableFunction angleofattack,
IParameterizableFunction sideslip,
IParameterizableFunction rollVel,
EllipsoidBodyShape earthShape)
Constructor.
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AeroAttitudeLaw(IParameterizableFunction angleofattack,
IParameterizableFunction sideslip,
IParameterizableFunction rollVel,
EllipsoidBodyShape earthShape,
double dtSpin,
double dtAcc)
Constructor with parameterizable delta-time for spin and acceleration computation.
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Modifier and Type | Interface and Description |
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interface |
IParamDiffFunction
This class is used to define a derivative function parameterizable.
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Modifier and Type | Class and Description |
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class |
ConstantFunction
This class is used to define a constant parameterizable function.
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class |
LinearFunction
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class |
ParamDiffFunction
Abstract class to define generic function of
IParamDiffFunction . |
class |
PiecewiseFunction
This class is used to define parameterizable piecewize function.
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