Uses of Interface
org.orekit.parameter.IParamDiffFunction

Packages that use IParamDiffFunction

fr.cnes.sirius.patrius.assembly
fr.cnes.sirius.patrius.assembly.models.cook
fr.cnes.sirius.patrius.assembly.properties
fr.cnes.sirius.patrius.forces
org.orekit.forces.drag
org.orekit.forces.maneuvers	This package provides models of simple maneuvers.
org.orekit.parameter

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

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

IParamDiffFunction[]

Vehicle.getAerodynamicsProperties() Returns the aero properties : drag and lift coefficients.

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

void	Vehicle.setAerodynamicsProperties(IParamDiffFunction cx, IParamDiffFunction cz) Set aerodynamics properties as functions IParamDiffFunction only if possible : main shape must be a sphere or there must be no solar panels.

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

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

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

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

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

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

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 org.orekit.forces.drag

Constructors in org.orekit.forces.drag with parameters of type IParamDiffFunction

DragForce(IParamDiffFunction k, Atmosphere atmosphere, DragSensitive spacecraft)
Constructor with multiplicative factor k.

DragForce(IParamDiffFunction k, Atmosphere atmosphere, DragSensitive spacecraft, boolean computePDPos, boolean computePDVel)
Constructor with multiplicative factor k.

Uses of IParamDiffFunction in org.orekit.forces.maneuvers

Constructors in org.orekit.forces.maneuvers with parameters of type IParamDiffFunction

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

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

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

Uses of IParamDiffFunction in org.orekit.parameter

Classes in org.orekit.parameter that implement IParamDiffFunction

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 org.orekit.parameter with parameters of type IParamDiffFunction

JacobiansParameterizable(IParamDiffFunction... paramDiffFunctions)
Simple constructor.

Parameterizable(IParamDiffFunction... paramDiffFunctions)
Simple constructor.

Constructor parameters in org.orekit.parameter with type arguments of type IParamDiffFunction

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