Package | Description |
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org.orekit.files.ccsds.definitions |
This package contains definitions for CCSDS objects (frames, time systems...).
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org.orekit.files.ccsds.ndm.adm |
This package contains class managing CCSDS Attitude Data 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.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.
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org.orekit.files.ccsds.utils.lexical |
This package contains utilities for CCSDS messages lexical analysis.
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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 |
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FrameFacade |
AttitudeEndoints.getExternalFrame()
Get the external frame.
|
FrameFacade |
AttitudeEndoints.getFrameA()
Get frame A.
|
FrameFacade |
AttitudeEndoints.getFrameB()
Get frame B.
|
FrameFacade |
AttitudeEndoints.getSpacecraftBodyFrame()
Get the spacecraft body frame.
|
Modifier and Type | Method and Description |
---|---|
void |
AttitudeEndoints.setFrameA(FrameFacade frameA)
Set frame A.
|
void |
AttitudeEndoints.setFrameB(FrameFacade frameB)
Set frame B.
|
Modifier and Type | Method and Description |
---|---|
FrameFacade |
SpacecraftParameters.getInertiaReferenceFrame()
Get the coordinate system for the inertia tensor.
|
Modifier and Type | Method and Description |
---|---|
void |
SpacecraftParameters.setInertiaReferenceFrame(FrameFacade inertiaReferenceFrame)
Set the coordinate system for the inertia tensor.
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Modifier and Type | Method and Description |
---|---|
FrameFacade |
CartesianCovariance.getReferenceFrame()
Get the reference frame.
|
FrameFacade |
CommonMetadata.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 |
CommonMetadata.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 |
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CartesianCovariance(Supplier<FrameFacade> defaultFrameSupplier)
Create an empty data set.
|
Modifier and Type | Method and Description |
---|---|
FrameFacade |
CovarianceHistoryMetadata.getCovReferenceFrame()
Get reference frame of the covariance.
|
FrameFacade |
ManeuverHistoryMetadata.getManReferenceFrame()
Get reference frame of the maneuver.
|
FrameFacade |
PhysicalProperties.getOebParentFrame()
Get the Optimally Enclosing Box parent reference frame.
|
FrameFacade |
TrajectoryStateHistoryMetadata.getTrajReferenceFrame()
Get reference frame of the trajectory.
|
Modifier and Type | Method and Description |
---|---|
void |
CovarianceHistoryMetadata.setCovReferenceFrame(FrameFacade covReferenceFrame)
Set reference frame of the covariance.
|
void |
ManeuverHistoryMetadata.setManReferenceFrame(FrameFacade manReferenceFrame)
Set reference frame of the maneuver.
|
void |
PhysicalProperties.setOebParentFrame(FrameFacade oebParentFrame)
Set the Optimally Enclosing Box parent reference frame.
|
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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