Uses of Class
org.orekit.bodies.FieldGeodeticPoint

Packages that use FieldGeodeticPoint

Package	Description
org.orekit.bodies	This package provides interface to represent the position and geometry of space objects such as stars, planets or asteroids.
org.orekit.frames	This package provides classes to handle frames and transforms between them.
org.orekit.models.earth	This package provides models that simulate certain physical phenomena of Earth and the near-Earth environment.
org.orekit.models.earth.ionosphere	This package provides models that simulate the impact of the ionosphere.

Uses of FieldGeodeticPoint in org.orekit.bodies

Methods in org.orekit.bodies that return FieldGeodeticPoint

Modifier and Type	Method and Description
<T extends RealFieldElement<T>> FieldGeodeticPoint<T>	BodyShape.getIntersectionPoint(FieldLine<T> line, FieldVector3D<T> close, Frame frame, FieldAbsoluteDate<T> date) Get the intersection point of a line with the surface of the body.
<T extends RealFieldElement<T>> FieldGeodeticPoint<T>	OneAxisEllipsoid.getIntersectionPoint(FieldLine<T> line, FieldVector3D<T> close, Frame frame, FieldAbsoluteDate<T> date) Get the intersection point of a line with the surface of the body.
<T extends RealFieldElement<T>> FieldGeodeticPoint<T>	BodyShape.transform(FieldVector3D<T> point, Frame frame, FieldAbsoluteDate<T> date) Transform a Cartesian point to a surface-relative point.
<T extends RealFieldElement<T>> FieldGeodeticPoint<T>	OneAxisEllipsoid.transform(FieldVector3D<T> point, Frame frame, FieldAbsoluteDate<T> date) Transform a Cartesian point to a surface-relative point.
FieldGeodeticPoint<DerivativeStructure>	OneAxisEllipsoid.transform(PVCoordinates point, Frame frame, AbsoluteDate date) Transform a Cartesian point to a surface-relative point.

Methods in org.orekit.bodies with parameters of type FieldGeodeticPoint

Modifier and Type	Method and Description
<T extends RealFieldElement<T>> FieldVector3D<T>	BodyShape.transform(FieldGeodeticPoint<T> point) Transform a surface-relative point to a Cartesian point.
<T extends RealFieldElement<T>> FieldVector3D<T>	OneAxisEllipsoid.transform(FieldGeodeticPoint<T> point) Transform a surface-relative point to a Cartesian point.

Uses of FieldGeodeticPoint in org.orekit.frames

Methods in org.orekit.frames that return FieldGeodeticPoint

Modifier and Type	Method and Description
<T extends RealFieldElement<T>> FieldGeodeticPoint<T>	TopocentricFrame.getPoint(Field<T> field) Get the surface point defining the origin of the frame.

Uses of FieldGeodeticPoint in org.orekit.models.earth

Methods in org.orekit.models.earth that return FieldGeodeticPoint

Modifier and Type	Method and Description
<T extends RealFieldElement<T>> FieldGeodeticPoint<T>	Geoid.getIntersectionPoint(FieldLine<T> lineInFrame, FieldVector3D<T> closeInFrame, Frame frame, FieldAbsoluteDate<T> date) Get the intersection point of a line with the surface of the body.
<T extends RealFieldElement<T>> FieldGeodeticPoint<T>	Geoid.transform(FieldVector3D<T> point, Frame frame, FieldAbsoluteDate<T> date) Transform a Cartesian point to a surface-relative point.

Methods in org.orekit.models.earth with parameters of type FieldGeodeticPoint

Modifier and Type	Method and Description
<T extends RealFieldElement<T>> FieldVector3D<T>	Geoid.transform(FieldGeodeticPoint<T> point) Transform a surface-relative point to a Cartesian point.

Uses of FieldGeodeticPoint in org.orekit.models.earth.ionosphere

Methods in org.orekit.models.earth.ionosphere with parameters of type FieldGeodeticPoint

Modifier and Type	Method and Description
<T extends RealFieldElement<T>> T	KlobucharIonoModel.pathDelay(FieldAbsoluteDate<T> date, FieldGeodeticPoint<T> geo, T elevation, T azimuth, double frequency, T[] parameters) Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
<T extends RealFieldElement<T>> T	NeQuickModel.stec(FieldAbsoluteDate<T> date, FieldGeodeticPoint<T> recP, FieldGeodeticPoint<T> satP) This method allows the computation of the Stant Total Electron Content (STEC).
<T extends RealFieldElement<T>> T	NeQuickModel.stec(FieldAbsoluteDate<T> date, FieldGeodeticPoint<T> recP, FieldGeodeticPoint<T> satP) This method allows the computation of the Stant Total Electron Content (STEC).