Package | Description |
---|---|
org.orekit.bodies |
This package provides interface to represent the position and geometry of
space objects such as stars, planets or asteroids.
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org.orekit.frames |
This package provides classes to handle frames and transforms between them.
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org.orekit.models.earth |
This package provides models that simulate certain physical phenomena
of Earth and the near-Earth environment.
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org.orekit.models.earth.ionosphere |
This package provides models that simulate the impact of the ionosphere.
|
org.orekit.models.earth.troposphere |
This package provides models that simulate the impact of the troposphere.
|
Modifier and Type | Method and Description |
---|---|
<T extends org.hipparchus.CalculusFieldElement<T>> |
OneAxisEllipsoid.getIntersectionPoint(org.hipparchus.geometry.euclidean.threed.FieldLine<T> line,
org.hipparchus.geometry.euclidean.threed.FieldVector3D<T> close,
Frame frame,
FieldAbsoluteDate<T> date)
Get the intersection point of a line with the surface of the body.
|
<T extends org.hipparchus.CalculusFieldElement<T>> |
BodyShape.getIntersectionPoint(org.hipparchus.geometry.euclidean.threed.FieldLine<T> line,
org.hipparchus.geometry.euclidean.threed.FieldVector3D<T> close,
Frame frame,
FieldAbsoluteDate<T> date)
Get the intersection point of a line with the surface of the body.
|
<T extends org.hipparchus.CalculusFieldElement<T>> |
OneAxisEllipsoid.lowestAltitudeIntermediate(org.hipparchus.geometry.euclidean.threed.FieldVector3D<T> endpoint1,
org.hipparchus.geometry.euclidean.threed.FieldVector3D<T> endpoint2)
Find intermediate point of lowest altitude along a line between two endpoints.
|
<T extends org.hipparchus.CalculusFieldElement<T>> |
OneAxisEllipsoid.transform(org.hipparchus.geometry.euclidean.threed.FieldVector3D<T> point,
Frame frame,
FieldAbsoluteDate<T> date)
Transform a Cartesian point to a surface-relative point.
|
<T extends org.hipparchus.CalculusFieldElement<T>> |
BodyShape.transform(org.hipparchus.geometry.euclidean.threed.FieldVector3D<T> point,
Frame frame,
FieldAbsoluteDate<T> date)
Transform a Cartesian point to a surface-relative point.
|
FieldGeodeticPoint<org.hipparchus.analysis.differentiation.DerivativeStructure> |
OneAxisEllipsoid.transform(PVCoordinates point,
Frame frame,
AbsoluteDate date)
Transform a Cartesian point to a surface-relative point.
|
Modifier and Type | Method and Description |
---|---|
<T extends org.hipparchus.CalculusFieldElement<T>> |
OneAxisEllipsoid.azimuthBetweenPoints(FieldGeodeticPoint<T> origin,
FieldGeodeticPoint<T> destination)
Compute the azimuth angle from local north between the two points.
|
<T extends org.hipparchus.CalculusFieldElement<T>> |
OneAxisEllipsoid.azimuthBetweenPoints(FieldGeodeticPoint<T> origin,
FieldGeodeticPoint<T> destination)
Compute the azimuth angle from local north between the two points.
|
<T extends org.hipparchus.CalculusFieldElement<T>> |
OneAxisEllipsoid.transform(FieldGeodeticPoint<T> point)
Transform a surface-relative point to a Cartesian point.
|
<T extends org.hipparchus.CalculusFieldElement<T>> |
BodyShape.transform(FieldGeodeticPoint<T> point)
Transform a surface-relative point to a Cartesian point.
|
Modifier and Type | Method and Description |
---|---|
<T extends org.hipparchus.CalculusFieldElement<T>> |
TopocentricFrame.getPoint(org.hipparchus.Field<T> field)
Get the surface point defining the origin of the frame.
|
Modifier and Type | Method and Description |
---|---|
<T extends org.hipparchus.CalculusFieldElement<T>> |
Geoid.getIntersectionPoint(org.hipparchus.geometry.euclidean.threed.FieldLine<T> lineInFrame,
org.hipparchus.geometry.euclidean.threed.FieldVector3D<T> closeInFrame,
Frame frame,
FieldAbsoluteDate<T> date)
Get the intersection point of a line with the surface of the body.
|
<T extends org.hipparchus.CalculusFieldElement<T>> |
Geoid.transform(org.hipparchus.geometry.euclidean.threed.FieldVector3D<T> point,
Frame frame,
FieldAbsoluteDate<T> date)
Transform a Cartesian point to a surface-relative point.
|
Modifier and Type | Method and Description |
---|---|
<T extends org.hipparchus.CalculusFieldElement<T>> |
Geoid.transform(FieldGeodeticPoint<T> point)
Transform a surface-relative point to a Cartesian point.
|
Modifier and Type | Method and Description |
---|---|
<T extends org.hipparchus.CalculusFieldElement<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 org.hipparchus.CalculusFieldElement<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 org.hipparchus.CalculusFieldElement<T>> |
NeQuickModel.stec(FieldAbsoluteDate<T> date,
FieldGeodeticPoint<T> recP,
FieldGeodeticPoint<T> satP)
This method allows the computation of the Stant Total Electron Content (STEC).
|
Modifier and Type | Method and Description |
---|---|
<T extends org.hipparchus.CalculusFieldElement<T>> |
MendesPavlisModel.computeZenithDelay(FieldGeodeticPoint<T> point,
T[] parameters,
FieldAbsoluteDate<T> date)
This method allows the computation of the zenith hydrostatic and
zenith wet delay.
|
<T extends org.hipparchus.CalculusFieldElement<T>> |
ViennaOneModel.computeZenithDelay(FieldGeodeticPoint<T> point,
T[] parameters,
FieldAbsoluteDate<T> date)
This method allows the computation of the zenith hydrostatic and
zenith wet delay.
|
<T extends org.hipparchus.CalculusFieldElement<T>> |
ViennaThreeModel.computeZenithDelay(FieldGeodeticPoint<T> point,
T[] parameters,
FieldAbsoluteDate<T> date)
This method allows the computation of the zenith hydrostatic and
zenith wet delay.
|
<T extends org.hipparchus.CalculusFieldElement<T>> |
MendesPavlisModel.mappingFactors(T elevation,
FieldGeodeticPoint<T> point,
FieldAbsoluteDate<T> date)
With the Mendes Pavlis tropospheric model, the mapping
function is not split into hydrostatic and wet component.
|
<T extends org.hipparchus.CalculusFieldElement<T>> |
ViennaOneModel.mappingFactors(T elevation,
FieldGeodeticPoint<T> point,
FieldAbsoluteDate<T> date)
This method allows the computation of the hydrostatic and
wet mapping functions.
|
<T extends org.hipparchus.CalculusFieldElement<T>> |
GlobalMappingFunctionModel.mappingFactors(T elevation,
FieldGeodeticPoint<T> point,
FieldAbsoluteDate<T> date)
This method allows the computation of the hydrostatic and
wet mapping functions.
|
<T extends org.hipparchus.CalculusFieldElement<T>> |
ViennaThreeModel.mappingFactors(T elevation,
FieldGeodeticPoint<T> point,
FieldAbsoluteDate<T> date)
This method allows the computation of the hydrostatic and
wet mapping functions.
|
<T extends org.hipparchus.CalculusFieldElement<T>> |
NiellMappingFunctionModel.mappingFactors(T elevation,
FieldGeodeticPoint<T> point,
FieldAbsoluteDate<T> date)
This method allows the computation of the hydrostatic and
wet mapping functions.
|
<T extends org.hipparchus.CalculusFieldElement<T>> |
MappingFunction.mappingFactors(T elevation,
FieldGeodeticPoint<T> point,
FieldAbsoluteDate<T> date)
This method allows the computation of the hydrostatic and
wet mapping functions.
|
<T extends org.hipparchus.CalculusFieldElement<T>> |
FixedTroposphericDelay.pathDelay(T elevation,
FieldGeodeticPoint<T> point,
T[] parameters,
FieldAbsoluteDate<T> date)
Calculates the tropospheric path delay for the signal path from a ground
station to a satellite.
|
<T extends org.hipparchus.CalculusFieldElement<T>> |
MendesPavlisModel.pathDelay(T elevation,
FieldGeodeticPoint<T> point,
T[] parameters,
FieldAbsoluteDate<T> date)
Calculates the tropospheric path delay for the signal path from a ground
station to a satellite.
|
<T extends org.hipparchus.CalculusFieldElement<T>> |
DiscreteTroposphericModel.pathDelay(T elevation,
FieldGeodeticPoint<T> point,
T[] parameters,
FieldAbsoluteDate<T> date)
Calculates the tropospheric path delay for the signal path from a ground
station to a satellite.
|
<T extends org.hipparchus.CalculusFieldElement<T>> |
EstimatedTroposphericModel.pathDelay(T elevation,
FieldGeodeticPoint<T> point,
T[] parameters,
FieldAbsoluteDate<T> date)
Calculates the tropospheric path delay for the signal path from a ground
station to a satellite.
|
<T extends org.hipparchus.CalculusFieldElement<T>> |
ViennaOneModel.pathDelay(T elevation,
FieldGeodeticPoint<T> point,
T[] parameters,
FieldAbsoluteDate<T> date)
Calculates the tropospheric path delay for the signal path from a ground
station to a satellite.
|
<T extends org.hipparchus.CalculusFieldElement<T>> |
ViennaThreeModel.pathDelay(T elevation,
FieldGeodeticPoint<T> point,
T[] parameters,
FieldAbsoluteDate<T> date)
Calculates the tropospheric path delay for the signal path from a ground
station to a satellite.
|
<T extends org.hipparchus.CalculusFieldElement<T>> |
MariniMurrayModel.pathDelay(T elevation,
FieldGeodeticPoint<T> point,
T[] parameters,
FieldAbsoluteDate<T> date)
Calculates the tropospheric path delay for the signal path from a ground
station to a satellite.
|
<T extends org.hipparchus.CalculusFieldElement<T>> |
TimeSpanEstimatedTroposphericModel.pathDelay(T elevation,
FieldGeodeticPoint<T> point,
T[] parameters,
FieldAbsoluteDate<T> date)
Calculates the tropospheric path delay for the signal path from a ground
station to a satellite.
|
<T extends org.hipparchus.CalculusFieldElement<T>> |
SaastamoinenModel.pathDelay(T elevation,
FieldGeodeticPoint<T> point,
T[] parameters,
FieldAbsoluteDate<T> date)
Calculates the tropospheric path delay for the signal path from a ground
station to a satellite.
|
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