Package | Description |
---|---|
org.orekit.files.ccsds.definitions |
This package contains definitions for CCSDS objects (frames, time systems...).
|
org.orekit.files.ccsds.ndm |
This package contains the base hierarchy for CCSDS ADM, ODM and TDM.
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org.orekit.files.ccsds.ndm.adm |
This package contains class managing CCSDS Attitude Data Message.
|
org.orekit.files.ccsds.ndm.adm.acm |
This package contains class managing CCSDS Attitude Comprehensive Message.
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org.orekit.files.ccsds.ndm.adm.aem |
This package contains class managing CCSDS Attitude Ephemeris Message.
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org.orekit.files.ccsds.ndm.adm.apm |
This package contains class managing CCSDS Attitude Parameter Message.
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org.orekit.files.ccsds.ndm.cdm |
This package contains class managing CCSDS Conjunction Data Message.
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org.orekit.files.ccsds.ndm.odm |
This package contains class managing CCSDS Orbit Data Message.
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org.orekit.files.ccsds.ndm.odm.ocm |
This package contains class managing CCSDS Orbit Comprehensive Message.
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org.orekit.files.ccsds.ndm.odm.opm |
This package contains class managing CCSDS Orbit Parameter Message.
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org.orekit.files.ccsds.ndm.tdm |
This package contains class managing CCSDS Tracking Data Message.
|
org.orekit.files.ccsds.utils.lexical |
This package contains utilities for CCSDS messages lexical analysis.
|
Modifier and Type | Method and Description |
---|---|
static FrameFacade |
FrameFacade.map(Frame frame)
Map an Orekit frame to a CCSDS frame facade.
|
static FrameFacade |
FrameFacade.parse(String name,
IERSConventions conventions,
boolean simpleEOP,
DataContext dataContext,
boolean allowCelestial,
boolean allowOrbit,
boolean allowSpacecraft)
Simple constructor.
|
Modifier and Type | Method and Description |
---|---|
static Transform |
FrameFacade.getTransform(FrameFacade frameIn,
FrameFacade frameOut,
Frame inertialPivotFrame,
AbsoluteDate date,
PVCoordinatesProvider pv)
Get the transform between
CCSDS frames . |
Modifier and Type | Method and Description |
---|---|
FrameFacade |
CommonPhysicalProperties.getOebParentFrame()
Get the Optimally Enclosing Box parent reference frame.
|
Modifier and Type | Method and Description |
---|---|
void |
CommonPhysicalProperties.setOebParentFrame(FrameFacade oebParentFrame)
Set the Optimally Enclosing Box parent reference frame.
|
Modifier and Type | Method and Description |
---|---|
FrameFacade |
AttitudeEndpoints.getExternalFrame()
Get the external frame.
|
FrameFacade |
AttitudeEndpoints.getFrameA()
Get frame A.
|
FrameFacade |
AttitudeEndpoints.getFrameB()
Get frame B.
|
FrameFacade |
AttitudeEndpoints.getSpacecraftBodyFrame()
Get the spacecraft body frame.
|
Modifier and Type | Method and Description |
---|---|
void |
AttitudeEndpoints.setFrameA(FrameFacade frameA)
Set frame A.
|
void |
AttitudeEndpoints.setFrameB(FrameFacade frameB)
Set frame B.
|
Modifier and Type | Method and Description |
---|---|
FrameFacade |
AttitudePhysicalProperties.getCenterOfPressureReferenceFrame()
Get reference frame for center of pressure.
|
FrameFacade |
AttitudeCovarianceHistoryMetadata.getCovReferenceFrame()
Get reference frame of the covariance.
|
FrameFacade |
AttitudePhysicalProperties.getInertiaReferenceFrame()
Get reference frame for inertia.
|
FrameFacade |
AttitudeManeuver.getTargetMomFrame()
Get reference frame for
AttitudeManeuver.getTargetMomentum() . |
Modifier and Type | Method and Description |
---|---|
void |
AttitudePhysicalProperties.setCenterOfPressureReferenceFrame(FrameFacade centerOfPressureReferenceFrame)
Set reference frame for center of pressure.
|
void |
AttitudeCovarianceHistoryMetadata.setCovReferenceFrame(FrameFacade covReferenceFrame)
Set reference frame of the covariance.
|
void |
AttitudePhysicalProperties.setInertiaReferenceFrame(FrameFacade inertiaReferenceFrame)
Set reference frame for inertia.
|
void |
AttitudeManeuver.setTargetMomFrame(FrameFacade targetMomFrame)
Set reference frame for
AttitudeManeuver.getTargetMomentum() . |
Modifier and Type | Method and Description |
---|---|
FrameFacade |
AemMetadata.getFrameAngvelFrame()
Get frame in which angular velocities are specified.
|
Modifier and Type | Method and Description |
---|---|
void |
AemMetadata.setAngvelFrame(FrameFacade angvelFrame)
Set frame in which angular velocities are specified.
|
Modifier and Type | Method and Description |
---|---|
FrameFacade |
Maneuver.getFrame()
Get Coordinate system for the torque vector.
|
FrameFacade |
Inertia.getFrame()
Get frame in which inertia is specified.
|
FrameFacade |
AngularVelocity.getFrame()
Get frame in which angular velocities are specified.
|
Modifier and Type | Method and Description |
---|---|
void |
Maneuver.setFrame(FrameFacade frame)
Set Coordinate system for the torque vector.
|
void |
Inertia.setFrame(FrameFacade frame)
Set frame in which inertia is specified.
|
void |
AngularVelocity.setFrame(FrameFacade frame)
Set frame in which angular velocities are specified.
|
Modifier and Type | Method and Description |
---|---|
FrameFacade |
CdmMetadata.getAltCovRefFrame()
Get the value of
ALT_COV_REF_FRAME as an Orekit Frame . |
FrameFacade |
CdmMetadata.getRefFrame()
Get the value of
REF_FRAME as an Orekit Frame . |
Modifier and Type | Method and Description |
---|---|
void |
CdmMetadata.setAltCovRefFrame(FrameFacade altCovRefFrame)
Set the name of the reference frame in which the alternate covariance data are given.
|
void |
CdmMetadata.setRefFrame(FrameFacade refFrame)
Set the name of the reference frame in which the state vector data are given.
|
Modifier and Type | Method and Description |
---|---|
FrameFacade |
CartesianCovariance.getReferenceFrame()
Get the reference frame.
|
FrameFacade |
OdmCommonMetadata.getReferenceFrame()
Get the value of
REF_FRAME as an Orekit Frame . |
Modifier and Type | Method and Description |
---|---|
void |
CartesianCovariance.setReferenceFrame(FrameFacade referenceFrame)
Set the reference frame in which data are given.
|
void |
OdmCommonMetadata.setReferenceFrame(FrameFacade referenceFrame)
Set the reference frame in which data are given: used for state vector
and Keplerian elements data (and for the covariance reference frame if none is given).
|
Constructor and Description |
---|
CartesianCovariance(Supplier<FrameFacade> defaultFrameSupplier)
Create an empty data set.
|
Modifier and Type | Method and Description |
---|---|
FrameFacade |
OrbitCovarianceHistoryMetadata.getCovReferenceFrame()
Get reference frame of the covariance.
|
FrameFacade |
OrbitManeuverHistoryMetadata.getManReferenceFrame()
Get reference frame of the maneuver.
|
FrameFacade |
TrajectoryStateHistoryMetadata.getTrajReferenceFrame()
Get reference frame of the trajectory.
|
Modifier and Type | Method and Description |
---|---|
void |
OrbitCovarianceHistoryMetadata.setCovReferenceFrame(FrameFacade covReferenceFrame)
Set reference frame of the covariance.
|
void |
OrbitManeuverHistoryMetadata.setManReferenceFrame(FrameFacade manReferenceFrame)
Set reference frame of the maneuver.
|
void |
TrajectoryStateHistoryMetadata.setTrajReferenceFrame(FrameFacade trajReferenceFrame)
Set reference frame of the trajectory.
|
Modifier and Type | Method and Description |
---|---|
FrameFacade |
Maneuver.getReferenceFrame()
Get Coordinate system for velocity increment vector.
|
Modifier and Type | Method and Description |
---|---|
void |
Maneuver.setReferenceFrame(FrameFacade referenceFrame)
Set Coordinate system for velocity increment vector.
|
Modifier and Type | Method and Description |
---|---|
FrameFacade |
TdmMetadata.getReferenceFrame()
Get the the value of
REFERENCE_FRAME as an Orekit Frame . |
Modifier and Type | Method and Description |
---|---|
void |
TdmMetadata.setReferenceFrame(FrameFacade referenceFrame)
Set the reference frame in which data are given: used for RADEC tracking data.
|
Modifier and Type | Method and Description |
---|---|
void |
ParseToken.FrameConsumer.accept(FrameFacade frameFacade)
Consume a frame.
|
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