Uses of Class
org.orekit.frames.Transform

Packages that use Transform

Package	Description
org.orekit.estimation.measurements	The measurements package defines everything that is related to orbit determination measurements.
org.orekit.frames	This package provides classes to handle frames and transforms between them.
org.orekit.geometry.fov
org.orekit.propagation	Propagation

Uses of Transform in org.orekit.estimation.measurements

Methods in org.orekit.estimation.measurements that return Transform

Modifier and Type	Method and Description
Transform	GroundStation.getOffsetToInertial(Frame inertial, AbsoluteDate clockDate) Get the transform between offset frame and inertial frame.
Transform	EstimatedEarthFrameProvider.getTransform(AbsoluteDate date) Get the Transform corresponding to specified date.

Uses of Transform in org.orekit.frames

Fields in org.orekit.frames declared as Transform

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

Methods in org.orekit.frames that return Transform

Modifier and Type	Method and Description
Transform	Transform.freeze() Get a frozen transform.
Transform	Transform.getInverse() Get the inverse transform of the instance.
static Transform	FramesFactory.getNonInterpolatingTransform(Frame from, Frame to, AbsoluteDate date) Get the transform between two frames, suppressing all interpolation.
Transform	InterpolatingTransformProvider.getTransform(AbsoluteDate date) Get the Transform corresponding to specified date.
Transform	FixedTransformProvider.getTransform(AbsoluteDate date) Get the Transform corresponding to specified date.
Transform	L1TransformProvider.getTransform(AbsoluteDate date) Get the Transform corresponding to specified date.
Transform	GTODProvider.getTransform(AbsoluteDate date) Get the Transform corresponding to specified date.
Transform	TransformProvider.getTransform(AbsoluteDate date) Get the Transform corresponding to specified date.
Transform	ShiftingTransformProvider.getTransform(AbsoluteDate date) Get the Transform corresponding to specified date.
Transform	EclipticProvider.getTransform(AbsoluteDate date)
Transform	ITRFVersion.Converter.getTransform(AbsoluteDate date) Get the Transform corresponding to specified date.
Transform	HelmertTransformation.getTransform(AbsoluteDate date) Get the Transform corresponding to specified date.
Transform	Frame.getTransformTo(Frame destination, AbsoluteDate date) Get the transform from the instance to another frame.
static Transform	Transform.interpolate(AbsoluteDate date, CartesianDerivativesFilter cFilter, AngularDerivativesFilter aFilter, Collection<Transform> sample) Interpolate a transform from a sample set of existing transforms.
Transform	Transform.interpolate(AbsoluteDate interpolationDate, Stream<Transform> sample) Get an interpolated instance.
Transform	Transform.shiftedBy(double dt) Get a time-shifted instance.
Transform	LOFType.transformFromInertial(AbsoluteDate date, PVCoordinates pv) Get the transform from an inertial frame defining position-velocity and the local orbital frame.

Methods in org.orekit.frames that return types with arguments of type Transform

Modifier and Type	Method and Description
List<Transform>	TransformGenerator.generate(AbsoluteDate existingDate, AbsoluteDate date) Generate a chronologically sorted list of entries to be cached.

Methods in org.orekit.frames with parameters of type Transform

Modifier and Type	Method and Description
void	OrphanFrame.addChild(OrphanFrame child, Transform transform, boolean isPseudoInertial) Add a child.
void	OrphanFrame.attachTo(Frame parent, Transform transform, boolean isPseudoInertial) Attach the instance (and all its children down to leafs) to the main tree.
void	UpdatableFrame.updateTransform(Frame f1, Frame f2, Transform f1Tof2, AbsoluteDate date) Update the transform from parent frame implicitly according to two other frames.

Method parameters in org.orekit.frames with type arguments of type Transform

Modifier and Type	Method and Description
static Transform	Transform.interpolate(AbsoluteDate date, CartesianDerivativesFilter cFilter, AngularDerivativesFilter aFilter, Collection<Transform> sample) Interpolate a transform from a sample set of existing transforms.
Transform	Transform.interpolate(AbsoluteDate interpolationDate, Stream<Transform> sample) Get an interpolated instance.

Constructors in org.orekit.frames with parameters of type Transform

Constructor and Description
FieldTransform(Field<T> field, Transform transform) Build a transform from a regular transform.
FixedTransformProvider(Transform transform) Simple constructor.
Frame(Frame parent, Transform transform, String name) Build a non-inertial frame from its transform with respect to its parent.
Frame(Frame parent, Transform transform, String name, boolean pseudoInertial) Build a frame from its transform with respect to its parent.
Transform(AbsoluteDate date, Transform first, Transform second) Build a transform by combining two existing ones.
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 org.orekit.geometry.fov

Methods in org.orekit.geometry.fov with parameters of type Transform

Modifier and Type	Method and Description
List<List<GeodeticPoint>>	SmoothFieldOfView.getFootprint(Transform fovToBody, OneAxisEllipsoid body, double angularStep) Get the footprint of the Field Of View on ground.
List<List<GeodeticPoint>>	PolygonalFieldOfView.getFootprint(Transform fovToBody, OneAxisEllipsoid body, double angularStep) Get the footprint of the Field Of View on ground.
List<List<GeodeticPoint>>	FieldOfView.getFootprint(Transform fovToBody, OneAxisEllipsoid body, double angularStep) Get the footprint of the Field Of View on ground.

Uses of Transform in org.orekit.propagation

Methods in org.orekit.propagation that return Transform

Modifier and Type	Method and Description
Transform	SpacecraftState.toTransform() Compute the transform from state defining frame to spacecraft frame.