Uses of Interface
fr.cnes.sirius.patrius.assembly.IPart

Packages that use IPart

Package	Description
fr.cnes.sirius.patrius.assembly
fr.cnes.sirius.patrius.assembly.models

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

Classes in fr.cnes.sirius.patrius.assembly that implement IPart

Modifier and Type	Class and Description
class	MainPart -Class to manage the assembly's main part.
class	Part -Class to manage the assembly's part (the main part is excluded).

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

Modifier and Type	Method and Description
IPart	MainPart.getParent() Returns null : this part has no parent.
IPart	Part.getParent()
IPart	IPart.getParent()
IPart	AssemblyBuilder.getPart(String name) This method returns the part whose name is given in parameter.
IPart	Assembly.getPart(String name) Returns the part whose name is specified.

Methods in fr.cnes.sirius.patrius.assembly that return types with arguments of type IPart

Modifier and Type	Method and Description
Map<String,IPart>	Assembly.getParts() Returns all the parts of the assembly.

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

Modifier and Type	Method and Description
void	Assembly.addPart(IPart part) Adds a part to the assembly.

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

Constructor and Description
Part(String inName, IPart inParentPart, Transform inTransform) Constructor of a part with a transformation.

Uses of IPart in fr.cnes.sirius.patrius.assembly.models

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

Modifier and Type	Method and Description
protected static Vector3D	AeroModel.forceOnFacet(SpacecraftState state, IPart part, Assembly assembly, double density, Vector3D relativeVelocity) Method to compute the force for a plane model.
protected static Vector3D	DirectRadiativeModel.forceOnFacet(SpacecraftState state, IPart part, Vector3D flux) Method to compute the force for a plane model.
protected static Vector3D	AeroModel.forceOnSphere(SpacecraftState state, IPart part, double density, Vector3D relativeVelocity, Frame mainPartFrame) Method to compute the force for the part model (cylinder, parallelepiped, sphere).
protected static Vector3D	DirectRadiativeModel.forceOnSphere(SpacecraftState state, IPart part, Vector3D flux, Frame mainPartFrame) Method to compute the force for a spherical model.