Uses of Class
fr.cnes.sirius.patrius.frames.transformations.Transform

Packages that use Transform

Package	Description
fr.cnes.sirius.patrius.assembly
fr.cnes.sirius.patrius.attitudes
fr.cnes.sirius.patrius.attitudes.orientations
fr.cnes.sirius.patrius.bodies.mesh
fr.cnes.sirius.patrius.forces.gravity
fr.cnes.sirius.patrius.forces.radiation
fr.cnes.sirius.patrius.frames
fr.cnes.sirius.patrius.frames.transformations
fr.cnes.sirius.patrius.propagation

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

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

Modifier and Type	Method and Description
Transform	Part.getTransform() Returns the transform linking the part to its parent part.

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

Modifier and Type	Method and Description
void	AssemblyBuilder.addPart(String partName, String parentPartName, Transform transform) This method adds a new part to the currently built assembly, defining its new frame by a Transform object.
void	Part.updateFrame(Transform t)
void	MobilePart.updateFrame(Transform t)
void	MainPart.updateFrame(Transform transform)
void	IPart.updateFrame(Transform t)
void	Assembly.updateMainPartFrame(Transform transform) Updates the main part frame's transformation to its parent frame using a Transform as an input argument.

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

Constructor and Description
Part(String name, IPart parentPart, Transform transform) Constructor.

Uses of Transform in fr.cnes.sirius.patrius.attitudes

Methods in fr.cnes.sirius.patrius.attitudes that return Transform

Modifier and Type	Method and Description
Transform	OrientationTransformProvider.getTransform(AbsoluteDate date) Get the Transform corresponding to specified date.
Transform	AttitudeTransformProvider.getTransform(AbsoluteDate date) Get the Transform corresponding to specified date.
Transform	OrientationTransformProvider.getTransform(AbsoluteDate date, boolean computeSpinDerivatives) Get the Transform corresponding to specified date.
Transform	AttitudeTransformProvider.getTransform(AbsoluteDate date, boolean computeSpinDerivatives) Get the Transform corresponding to specified date.
Transform	OrientationTransformProvider.getTransform(AbsoluteDate date, FramesConfiguration config) Get the Transform corresponding to specified date.
Transform	AttitudeTransformProvider.getTransform(AbsoluteDate date, FramesConfiguration config) Get the Transform corresponding to specified date.
Transform	OrientationTransformProvider.getTransform(AbsoluteDate date, FramesConfiguration config, boolean computeSpinDerivatives) Get the Transform corresponding to specified date.
Transform	AttitudeTransformProvider.getTransform(AbsoluteDate date, FramesConfiguration config, boolean computeSpinDerivatives) Get the Transform corresponding to specified date.

Uses of Transform in fr.cnes.sirius.patrius.attitudes.orientations

Methods in fr.cnes.sirius.patrius.attitudes.orientations that return Transform

Modifier and Type	Method and Description
Transform	OrientationAngleTransform.getReference() Returns the reference transform.
Transform	OrientationAngleTransform.getTransform(SpacecraftState state) Get the Transform corresponding to specified state.

Constructors in fr.cnes.sirius.patrius.attitudes.orientations with parameters of type Transform

Constructor and Description
OrientationAngleTransform(Transform reference, Vector3D axis, OrientationAngleProvider orientationAngleProvider) Constructor.

Uses of Transform in fr.cnes.sirius.patrius.bodies.mesh

Methods in fr.cnes.sirius.patrius.bodies.mesh with parameters of type Transform

Modifier and Type	Method and Description
boolean	FacetBodyShape.isVisible(Triangle triangle, Vector3D pos, IFieldOfView fieldOfView, Transform t) Returns true if the triangle is visible from the field of view, i.e.: Is oriented toward the field of view All points of the triangle are in the field of view Triangle not masked by another facet

Uses of Transform in fr.cnes.sirius.patrius.forces.gravity

Methods in fr.cnes.sirius.patrius.forces.gravity with parameters of type Transform

Modifier and Type	Method and Description
protected Vector3D	ThirdBodyAttraction.computeAcceleration(Vector3D positionInBodyFrame, AbsoluteDate date, Transform scFrameToBodyFrame) Abstract method to compute the acceleration of the implementation
protected Vector3D	DirectBodyAttraction.computeAcceleration(Vector3D positionInBodyFrame, AbsoluteDate date, Transform scFrameToBodyFrame) Abstract method to compute the acceleration of the implementation
protected abstract Vector3D	AbstractBodyAttraction.computeAcceleration(Vector3D positionInBodyFrame, AbsoluteDate date, Transform scFrameToBodyFrame) Abstract method to compute the acceleration of the implementation

Uses of Transform in fr.cnes.sirius.patrius.forces.radiation

Methods in fr.cnes.sirius.patrius.forces.radiation with parameters of type Transform

Modifier and Type	Method and Description
ElementaryFlux[]	RediffusedFlux.getFlux(Transform t) Getter for all elementary rediffused fluxes.

Uses of Transform in fr.cnes.sirius.patrius.frames

Methods in fr.cnes.sirius.patrius.frames that return Transform

Modifier and Type	Method and Description
Transform	Frame.getTransformTo(Frame destination, AbsoluteDate date) Get the transform from the instance to another frame.
Transform	Frame.getTransformTo(Frame destination, AbsoluteDate date, boolean computeSpinDerivatives) Get the transform from the instance to another frame.
Transform	Frame.getTransformTo(Frame destination, AbsoluteDate date, FramesConfiguration config) Get the transform from the instance to another frame.
Transform	Frame.getTransformTo(Frame destination, AbsoluteDate date, FramesConfiguration config, boolean computeSpinDerivatives) Get the transform from the instance to another frame.
Transform	LOFType.transformFromInertial(AbsoluteDate date, PVCoordinates pv) Get the transform from an inertial frame defining position-velocity and the local orbital frame.
Transform	LOFType.transformFromInertial(AbsoluteDate date, PVCoordinates pv, boolean computeSpinDerivatives) Get the transform from an inertial frame defining position-velocity and the local orbital frame.

Methods in fr.cnes.sirius.patrius.frames with parameters of type Transform

Modifier and Type	Method and Description
void	UpdatableFrame.setTransform(Transform transform) Update the transform from the parent frame to the instance.
void	UpdatableFrame.updateTransform(Frame f1, Frame f2, Transform f1Tof2, AbsoluteDate date) Update the transform from parent frame implicitly according to two other frames.

Constructors in fr.cnes.sirius.patrius.frames with parameters of type Transform

Constructor and Description
CelestialBodyFrame(Frame parent, Transform transform, String name, boolean pseudoInertial, CelestialPoint celestialPoint) Constructor.
CelestialBodyFrame(Frame parent, Transform transform, String name, CelestialPoint celestialPoint) Constructor.
Frame(Frame parentIn, Transform transformIn, String nameIn) Build a non-inertial frame from its transform with respect to its parent.
Frame(Frame parentIn, Transform transformIn, String nameIn, boolean pseudoInertialIn) Build a frame from its transform with respect to its parent.
UpdatableFrame(Frame parent, Transform transform, String name) Build a non-inertial frame from its transform with respect to its parent.
UpdatableFrame(Frame parent, Transform transform, String name, boolean pseudoInertial) Build a frame from its transform with respect to its parent.

Uses of Transform in fr.cnes.sirius.patrius.frames.transformations

Fields in fr.cnes.sirius.patrius.frames.transformations declared as Transform

Modifier and Type	Field and Description
static Transform	Transform.IDENTITY Identity transform.

Methods in fr.cnes.sirius.patrius.frames.transformations that return Transform

Modifier and Type	Method and Description
Transform	Transform.freeze() Get a freezed transform.
Transform	Transform.getInverse() Get the inverse transform of the instance.
Transform	Transform.getInverse(boolean computeSpinDerivatives) Get the inverse transform of the instance.
Transform	TransformProvider.getTransform(AbsoluteDate date) Get the Transform corresponding to specified date.
Transform	TODProvider.getTransform(AbsoluteDate date) Get the transform from Mean Of Date at specified date.
Transform	TIRFProvider.getTransform(AbsoluteDate date) Get the transform from CIRF 2000 at specified date.
Transform	TEMEProvider.getTransform(AbsoluteDate date) Get the transform from True Of Date date.
Transform	MODProvider.getTransform(AbsoluteDate date) Get the transfrom from parent frame.
Transform	ITRFProvider.getTransform(AbsoluteDate date) Get the transform from TIRF 2000 at specified date.
Transform	ITRFEquinoxProvider.getTransform(AbsoluteDate date) Get the transform from GTOD at specified date.
Transform	InterpolatingTransformProvider.getTransform(AbsoluteDate date) Get the Transform corresponding to specified date.
Transform	HelmertTransformation.getTransform(AbsoluteDate date) Compute the transform at some date.
Transform	GTODProvider.getTransform(AbsoluteDate date) Get the transform from TOD at specified date.
Transform	GCRFProvider.getTransform(AbsoluteDate date) Get the transform from GCRF to Earth-Moon barycenter frame at the specified date.
Transform	FixedTransformProvider.getTransform(AbsoluteDate date) Get the Transform corresponding to specified date.
Transform	EMBProvider.getTransform(AbsoluteDate date) Get the transform from Earth-Moon barycenter frame to Solar System barycenter frame (ICRF) at the specified date.
Transform	EclipticMODProvider.getTransform(AbsoluteDate date) Get the Transform corresponding to specified date.
Transform	CIRFProvider.getTransform(AbsoluteDate date) Get the transform from GCRF to CIRF2000 at the specified date.
Transform	AbstractVeisProvider.getTransform(AbsoluteDate date) Get the transform from GTOD at specified date.
Transform	TransformProvider.getTransform(AbsoluteDate date, boolean computeSpinDerivatives) Get the Transform corresponding to specified date.
Transform	TODProvider.getTransform(AbsoluteDate date, boolean computeSpinDerivatives) Get the transform from Mean Of Date at specified date.
Transform	TIRFProvider.getTransform(AbsoluteDate date, boolean computeSpinDerivatives) Get the transform from CIRF 2000 at specified date.
Transform	TEMEProvider.getTransform(AbsoluteDate date, boolean computeSpinDerivatives) Get the transform from True Of Date date.
Transform	MODProvider.getTransform(AbsoluteDate date, boolean computeSpinDerivatives) Get the transfrom from parent frame.
Transform	ITRFProvider.getTransform(AbsoluteDate date, boolean computeSpinDerivatives) Get the transform from TIRF 2000 at specified date.
Transform	ITRFEquinoxProvider.getTransform(AbsoluteDate date, boolean computeSpinDerivatives) Get the transform from GTOD at specified date.
Transform	InterpolatingTransformProvider.getTransform(AbsoluteDate date, boolean computeSpinDerivatives) Get the Transform corresponding to specified date.
Transform	HelmertTransformation.getTransform(AbsoluteDate date, boolean computeSpinDerivatives) Compute the transform at some date.
Transform	GTODProvider.getTransform(AbsoluteDate date, boolean computeSpinDerivatives) Get the transform from TOD at specified date.
Transform	GCRFProvider.getTransform(AbsoluteDate date, boolean computeSpinDerivatives) Get the transform from GCRF to Earth-Moon barycenter frame at the specified date.
Transform	FixedTransformProvider.getTransform(AbsoluteDate date, boolean computeSpinDerivatives) Get the Transform corresponding to specified date.
Transform	EMBProvider.getTransform(AbsoluteDate date, boolean computeSpinDerivatives) Get the transform from Earth-Moon barycenter frame to Solar System barycenter frame (ICRF) at the specified date.
Transform	EclipticMODProvider.getTransform(AbsoluteDate date, boolean computeSpinDerivatives) Get the Transform corresponding to specified date.
Transform	CIRFProvider.getTransform(AbsoluteDate date, boolean computeSpinDerivatives) Get the transform from GCRF to CIRF2000 at the specified date.
Transform	AbstractVeisProvider.getTransform(AbsoluteDate date, boolean computeSpinDerivatives) Get the transform from GTOD at specified date.
Transform	TransformProvider.getTransform(AbsoluteDate date, FramesConfiguration config) Get the Transform corresponding to specified date.
Transform	TODProvider.getTransform(AbsoluteDate date, FramesConfiguration config) Get the transform from Mean Of Date at specified date.
Transform	TIRFProvider.getTransform(AbsoluteDate date, FramesConfiguration config) Get the transform from CIRF 2000 at specified date.
Transform	TEMEProvider.getTransform(AbsoluteDate date, FramesConfiguration config) Get the transform from True Of Date date.
Transform	MODProvider.getTransform(AbsoluteDate date, FramesConfiguration config) Get the transfrom from parent frame.
Transform	ITRFProvider.getTransform(AbsoluteDate date, FramesConfiguration config) Get the transform from TIRF 2000 at specified date.
Transform	ITRFEquinoxProvider.getTransform(AbsoluteDate date, FramesConfiguration config) Get the transform from GTOD at specified date.
Transform	InterpolatingTransformProvider.getTransform(AbsoluteDate date, FramesConfiguration config) Get the Transform corresponding to specified date.
Transform	HelmertTransformation.getTransform(AbsoluteDate date, FramesConfiguration config) Compute the transform at some date.
Transform	GTODProvider.getTransform(AbsoluteDate date, FramesConfiguration config) Get the transform from TOD at specified date.
Transform	GCRFProvider.getTransform(AbsoluteDate date, FramesConfiguration config) Get the transform from GCRF to Earth-Moon barycenter frame at the specified date.
Transform	FixedTransformProvider.getTransform(AbsoluteDate date, FramesConfiguration config) Get the Transform corresponding to specified date.
Transform	EMBProvider.getTransform(AbsoluteDate date, FramesConfiguration config) Get the transform from Earth-Moon barycenter frame to Solar System barycenter frame (ICRF) at the specified date.
Transform	EclipticMODProvider.getTransform(AbsoluteDate date, FramesConfiguration config) Get the Transform corresponding to specified date.
Transform	CIRFProvider.getTransform(AbsoluteDate date, FramesConfiguration config) Get the transform from GCRF to CIRF2000 at the specified date.
Transform	AbstractVeisProvider.getTransform(AbsoluteDate date, FramesConfiguration config) Get the Transform corresponding to specified date.
Transform	TransformProvider.getTransform(AbsoluteDate date, FramesConfiguration config, boolean computeSpinDerivatives) Get the Transform corresponding to specified date.
Transform	TODProvider.getTransform(AbsoluteDate date, FramesConfiguration config, boolean computeSpinDerivatives) Get the transform from Mean Of Date at specified date.
Transform	TIRFProvider.getTransform(AbsoluteDate date, FramesConfiguration config, boolean computeSpinDerivatives) Get the transform from CIRF 2000 at specified date.
Transform	TEMEProvider.getTransform(AbsoluteDate date, FramesConfiguration config, boolean computeSpinDerivatives) Get the transform from True Of Date date.
Transform	MODProvider.getTransform(AbsoluteDate date, FramesConfiguration config, boolean computeSpinDerivatives) Get the transfrom from parent frame.
Transform	ITRFProvider.getTransform(AbsoluteDate date, FramesConfiguration config, boolean computeSpinDerivatives) Get the transform from TIRF 2000 at specified date.
Transform	ITRFEquinoxProvider.getTransform(AbsoluteDate date, FramesConfiguration config, boolean computeSpinDerivatives) Get the transform from GTOD at specified date.
Transform	InterpolatingTransformProvider.getTransform(AbsoluteDate date, FramesConfiguration config, boolean computeSpinDerivatives) Get the Transform corresponding to specified date.
Transform	HelmertTransformation.getTransform(AbsoluteDate date, FramesConfiguration config, boolean computeSpinDerivatives) Compute the transform at some date.
Transform	GTODProvider.getTransform(AbsoluteDate date, FramesConfiguration config, boolean computeSpinDerivatives) Get the transform from TOD at specified date.
Transform	GCRFProvider.getTransform(AbsoluteDate date, FramesConfiguration config, boolean computeSpinDerivatives) Get the transform from GCRF to Earth-Moon barycenter frame at the specified date.
Transform	FixedTransformProvider.getTransform(AbsoluteDate date, FramesConfiguration config, boolean computeSpinDerivatives) Get the Transform corresponding to specified date.
Transform	EMBProvider.getTransform(AbsoluteDate date, FramesConfiguration config, boolean computeSpinDerivatives) Get the transform from Earth-Moon barycenter frame to Solar System barycenter frame (ICRF) at the specified date.
Transform	EclipticMODProvider.getTransform(AbsoluteDate date, FramesConfiguration config, boolean computeSpinDerivatives) Get the Transform corresponding to specified date.
Transform	CIRFProvider.getTransform(AbsoluteDate date, FramesConfiguration config, boolean computeSpinDerivatives) Get the transform from GCRF to CIRF2000 at the specified date.
Transform	AbstractVeisProvider.getTransform(AbsoluteDate date, FramesConfiguration config, boolean computeSpinDerivatives) Get the Transform corresponding to specified date.
Transform	TransformStateProvider.getTransform(SpacecraftState state) Get the Transform corresponding to specified state.
static Transform	Transform.interpolate(AbsoluteDate date, boolean useVelocities, boolean useRotationRates, Collection<Transform> sample) Interpolate a transform from a sample set of existing transforms.
static Transform	Transform.interpolate(AbsoluteDate date, boolean useVelocities, boolean useRotationRates, Collection<Transform> sample, boolean computeSpinDerivative) Interpolate a transform from a sample set of existing transforms.
Transform	Transform.interpolate(AbsoluteDate interpolationDate, Collection<Transform> sample) Get an interpolated instance.
Transform	Transform.interpolate(AbsoluteDate interpolationDate, Collection<Transform> sample, boolean computeSpinDerivative) Get an interpolated instance.
Transform	Transform.shiftedBy(double dt) Get a time-shifted instance.
Transform	Transform.shiftedBy(double dt, boolean computeSpinDerivative) Get a time-shifted instance.

Method parameters in fr.cnes.sirius.patrius.frames.transformations with type arguments of type Transform

Modifier and Type	Method and Description
static Transform	Transform.interpolate(AbsoluteDate date, boolean useVelocities, boolean useRotationRates, Collection<Transform> sample) Interpolate a transform from a sample set of existing transforms.
static Transform	Transform.interpolate(AbsoluteDate date, boolean useVelocities, boolean useRotationRates, Collection<Transform> sample, boolean computeSpinDerivative) Interpolate a transform from a sample set of existing transforms.
Transform	Transform.interpolate(AbsoluteDate interpolationDate, Collection<Transform> sample) Get an interpolated instance.
Transform	Transform.interpolate(AbsoluteDate interpolationDate, Collection<Transform> sample, boolean computeSpinDerivative) Get an interpolated instance.

Constructors in fr.cnes.sirius.patrius.frames.transformations with parameters of type Transform

Constructor and Description
FixedTransformProvider(Transform transformIn) Simple constructor.
Transform(AbsoluteDate dateIn, Transform first, Transform second) Build a transform by combining two existing ones without computing spin derivatives.
Transform(AbsoluteDate dateIn, Transform first, Transform second, boolean computeSpinDerivatives) Build a transform by combining two existing ones, while not simply projecting velocity and acceleration.
Transform(AbsoluteDate dateIn, Transform first, Transform second, boolean computeSpinDerivatives, boolean projectVelocityAndAcceleration) Deprecated. since 4.16, the concept of projectVelocityAndAcceleration has been introduced to answer the needs of referential frame whereas this concept is erroneous. All methods using it should be avoided.

Uses of Transform in fr.cnes.sirius.patrius.propagation

Methods in fr.cnes.sirius.patrius.propagation that return Transform

Modifier and Type	Method and Description
Transform	SpacecraftState.toTransform() Compute the transform from orbit/attitude reference frame to spacecraft frame.
Transform	SpacecraftState.toTransform(Frame frame) Compute the transform from specified frame to spacecraft frame.
Transform	SpacecraftState.toTransform(Frame frame, LOFType lofType) Compute the transform from specified frame to local orbital frame.
Transform	SpacecraftState.toTransform(LOFType lofType) Compute the transform from orbit/attitude reference frame to local orbital frame.
Transform	SpacecraftState.toTransformEvents() Compute the transform from orbit/attitude (for events computation) reference frame to spacecraft frame.
Transform	SpacecraftState.toTransformEvents(Frame frame) Compute the transform from specified reference frame to spacecraft frame.
Transform	SpacecraftState.toTransformForces() Compute the transform from orbit/attitude (for forces computation) reference frame to spacecraft frame.
Transform	SpacecraftState.toTransformForces(Frame frame) Compute the transform from specified frame to spacecraft frame.