Uses of Interface
fr.cnes.sirius.patrius.math.parameter.IParamDiffFunction

Packages that use IParamDiffFunction

Package	Description
fr.cnes.sirius.patrius.assembly
fr.cnes.sirius.patrius.assembly.models.aerocoeffs
fr.cnes.sirius.patrius.assembly.models.cook
fr.cnes.sirius.patrius.assembly.properties
fr.cnes.sirius.patrius.forces
fr.cnes.sirius.patrius.forces.drag
fr.cnes.sirius.patrius.forces.maneuvers
fr.cnes.sirius.patrius.math.parameter

Uses of IParamDiffFunction in fr.cnes.sirius.patrius.assembly

Methods in fr.cnes.sirius.patrius.assembly that return IParamDiffFunction

Modifier and Type	Method and Description
IParamDiffFunction[]	Vehicle.getAerodynamicsPropertiesFunction() Returns the aero properties : drag and lift coefficients.

Uses of IParamDiffFunction in fr.cnes.sirius.patrius.assembly.models.aerocoeffs

Subinterfaces of IParamDiffFunction in fr.cnes.sirius.patrius.assembly.models.aerocoeffs

Modifier and Type	Interface and Description
interface	AerodynamicCoefficient Interface for aerodynamic coefficients.

Classes in fr.cnes.sirius.patrius.assembly.models.aerocoeffs that implement IParamDiffFunction

Modifier and Type	Class and Description
class	AbstractAeroCoeff1D Aerodynamic coefficient function of one variable.
class	AeroCoeffByAltitude Aerodynamic coefficient function of the spacecraft altitude.
class	AeroCoeffByAoA Aerodynamic coefficient function of the spacecraft angle of attack.
class	AeroCoeffByAoAAndMach Aerodynamic coefficient function of the spacecraft angle of attack and Mach number.
class	AeroCoeffByMach Aerodynamic coefficient function of the spacecraft Mach number.
class	AeroCoeffConstant Constant aerodynamic coefficient.

Uses of IParamDiffFunction in fr.cnes.sirius.patrius.assembly.models.cook

Classes in fr.cnes.sirius.patrius.assembly.models.cook that implement IParamDiffFunction

Modifier and Type	Class and Description
class	CnCookModel This class implements Cook normal coefficient to a facet.
class	CtCookModel This class implements Cook tangential coefficient to a facet.

Uses of IParamDiffFunction in fr.cnes.sirius.patrius.assembly.properties

Methods in fr.cnes.sirius.patrius.assembly.properties that return IParamDiffFunction

Modifier and Type	Method and Description
IParamDiffFunction	AeroGlobalProperty.getDragCoef() Get the drag coefficient.
IParamDiffFunction	AeroCrossSectionProperty.getDragForce() Get the drag force coefficient parametrizable function.
IParamDiffFunction	AeroGlobalProperty.getLiftCoef() Get the lift coefficient.
IParamDiffFunction	AeroFacetProperty.getNormalCoef() Get the normal force parametrizable function.
IParamDiffFunction	AeroFacetProperty.getTangentialCoef() Get the normal force parametrizable function.

Constructors in fr.cnes.sirius.patrius.assembly.properties with parameters of type IParamDiffFunction

Constructor and Description
AeroCrossSectionProperty(CrossSectionProvider shape, IParamDiffFunction dragCoefFct) Constructor of this property defining the drag coef as a IParamDiffFunction.
AeroFacetProperty(Facet inFacet, IParamDiffFunction normalCoefFct, IParamDiffFunction tangentialCoefFct) Constructor of this property.
AeroGlobalProperty(IParamDiffFunction dragCoef, IParamDiffFunction liftCoef, CrossSectionProvider shape) This constructor shall be used for defining the aero coefficients as ParamDiffFunction.
AeroSphereProperty(double inSphereRadius, IParamDiffFunction dragCoefFct) Constructor of this property defining the drag coef as a ParamDiffFunction.

Uses of IParamDiffFunction in fr.cnes.sirius.patrius.forces

Methods in fr.cnes.sirius.patrius.forces that return IParamDiffFunction

Modifier and Type	Method and Description
IParamDiffFunction	EmpiricalForce.getAx() Get the parametereziable function for the Ax coefficient.
IParamDiffFunction	EmpiricalForce.getAy() Get the parametereziable function for the Ay coefficient.
IParamDiffFunction	EmpiricalForce.getAz() Get the parametereziable function for the Az coefficient.
IParamDiffFunction	EmpiricalForce.getBx() Get the parametereziable function for the Bx coefficient.
IParamDiffFunction	EmpiricalForce.getBy() Get the parametereziable function for the By coefficient.
IParamDiffFunction	EmpiricalForce.getBz() Get the parametereziable function for the Bz coefficient.
IParamDiffFunction	EmpiricalForce.getCx() Get the parametereziable function for the Ax coefficient.
IParamDiffFunction	EmpiricalForce.getCy() Get the parametereziable function for the Cy coefficient.
IParamDiffFunction	EmpiricalForce.getCz() Get the parametereziable function for the Cz coefficient.

Constructors in fr.cnes.sirius.patrius.forces with parameters of type IParamDiffFunction

Constructor and Description
EmpiricalForce(int harmonicFactor, Vector3D vectorS, IParamDiffFunction ax, IParamDiffFunction ay, IParamDiffFunction az, IParamDiffFunction bx, IParamDiffFunction by, IParamDiffFunction bz, IParamDiffFunction cx, IParamDiffFunction cy, IParamDiffFunction cz, Frame coeffsFrame) Simple constructor for an empiric force using parameterizable functions for A; B and C coef with a given frame.
EmpiricalForce(int harmonicFactor, Vector3D vectorS, IParamDiffFunction ax, IParamDiffFunction ay, IParamDiffFunction az, IParamDiffFunction bx, IParamDiffFunction by, IParamDiffFunction bz, IParamDiffFunction cx, IParamDiffFunction cy, IParamDiffFunction cz, LOFType coeffsFrameLOFType) Simple constructor for an empiric force using parameterizable functions for A; B and C coef with a given LOF frame.

Uses of IParamDiffFunction in fr.cnes.sirius.patrius.forces.drag

Methods in fr.cnes.sirius.patrius.forces.drag that return IParamDiffFunction

Modifier and Type	Method and Description
IParamDiffFunction	DragForce.getMultiplicativeFactor() Getter for the multiplicative factor.

Constructors in fr.cnes.sirius.patrius.forces.drag with parameters of type IParamDiffFunction

Constructor and Description
DragForce(IParamDiffFunction kIn, Atmosphere atmosphereIn, DragSensitive spacecraftIn) Constructor with multiplicative factor k.
DragForce(IParamDiffFunction kIn, Atmosphere atmosphereIn, DragSensitive spacecraftIn, boolean computePDPos, boolean computePDVel) Constructor with multiplicative factor k.

Uses of IParamDiffFunction in fr.cnes.sirius.patrius.forces.maneuvers

Constructors in fr.cnes.sirius.patrius.forces.maneuvers with parameters of type IParamDiffFunction

Constructor and Description
ConstantThrustError(AbsoluteDate date, double duration, Frame frame, IParamDiffFunction fx, IParamDiffFunction fy, IParamDiffFunction fz) Create a constant thrust error model whose x, y and z components are parameterizable and differentiable function.
ConstantThrustError(AbsoluteDate date, double duration, IParamDiffFunction fx, IParamDiffFunction fy, IParamDiffFunction fz) Create a constant thrust error model whose x, y and z components are parameterizable and differentiable function.
ConstantThrustError(AbsoluteDate date, double duration, LOFType lofType, IParamDiffFunction fx, IParamDiffFunction fy, IParamDiffFunction fz) Create a constant thrust error model whose x, y and z components are parameterizable and differentiable function.
ConstantThrustError(EventDetector startEventDetector, EventDetector stopEventDetector, Frame frame, IParamDiffFunction fx, IParamDiffFunction fy, IParamDiffFunction fz) Create a constant thrust error model whose x, y and z components are constant functions: fx = cx fy = cy fz = cz Errors components are expressed in provided frame.
ConstantThrustError(EventDetector startEventDetector, EventDetector stopEventDetector, IParamDiffFunction fx, IParamDiffFunction fy, IParamDiffFunction fz) Create a constant thrust error model whose x, y and z components are constant functions: fx = cx fy = cy fz = cz Errors components are expressed in spacecraft frame.
ConstantThrustError(EventDetector startEventDetector, EventDetector stopEventDetector, LOFType lofType, IParamDiffFunction fx, IParamDiffFunction fy, IParamDiffFunction fz) Create a constant thrust error model whose x, y and z components are constant functions: fx = cx fy = cy fz = cz Errors components are expressed in provided local orbital frame.

Uses of IParamDiffFunction in fr.cnes.sirius.patrius.math.parameter

Classes in fr.cnes.sirius.patrius.math.parameter that implement IParamDiffFunction

Modifier and Type	Class and Description
class	ConstantFunction This class is used to define a constant parameterizable function.
class	LinearFunction This class is used to define parameterizable linear function a(t -t0) + b.
class	ParamDiffFunction Abstract class to define generic function of IParamDiffFunction.
class	PiecewiseFunction This class is used to define parameterizable piecewize function.

Constructors in fr.cnes.sirius.patrius.math.parameter with parameters of type IParamDiffFunction

Constructor and Description
JacobiansParameterizable(IParamDiffFunction... paramDiffFunctions) Simple constructor.
Parameterizable(IParamDiffFunction... paramDiffFunctions) Simple constructor.

Constructor parameters in fr.cnes.sirius.patrius.math.parameter with type arguments of type IParamDiffFunction

Constructor and Description
PiecewiseFunction(ArrayList<IParamDiffFunction> flist, ArrayList<AbsoluteDate> xlist) Simple constructor with 2 lists (IParamDiffFunction and AbsoluteDate) where dates list represent the connection points between functions.