Package | Description |
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org.orekit.attitudes |
This package provides classes to represent simple attitudes.
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org.orekit.propagation |
This package provides tools to propagate orbital states with different methods.
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Modifier and Type | Method and Description |
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Attitude |
GroundPointing.getAttitude(PVCoordinatesProvider pvProv,
AbsoluteDate date,
Frame frame)
Compute the attitude corresponding to an orbital state.
|
Attitude |
GroundPointingWrapper.getAttitude(PVCoordinatesProvider pvProv,
AbsoluteDate date,
Frame frame)
Compute the attitude corresponding to an orbital state.
|
Attitude |
AttitudeProvider.getAttitude(PVCoordinatesProvider pvProv,
AbsoluteDate date,
Frame frame)
Compute the attitude corresponding to an orbital state.
|
Attitude |
LofOffset.getAttitude(PVCoordinatesProvider pvProv,
AbsoluteDate date,
Frame frame)
Compute the attitude corresponding to an orbital state.
|
Attitude |
FixedRate.getAttitude(PVCoordinatesProvider pvProv,
AbsoluteDate date,
Frame frame)
Compute the attitude corresponding to an orbital state.
|
Attitude |
AttitudesSequence.getAttitude(PVCoordinatesProvider pvProv,
AbsoluteDate date,
Frame frame)
Compute the attitude corresponding to an orbital state.
|
Attitude |
TabulatedProvider.getAttitude(PVCoordinatesProvider pvProv,
AbsoluteDate date,
Frame frame)
Compute the attitude corresponding to an orbital state.
|
Attitude |
CelestialBodyPointed.getAttitude(PVCoordinatesProvider pvProv,
AbsoluteDate date,
Frame frame)
Compute the attitude corresponding to an orbital state.
|
Attitude |
InertialProvider.getAttitude(PVCoordinatesProvider pvProv,
AbsoluteDate date,
Frame frame)
Compute the attitude corresponding to an orbital state.
|
Attitude |
SpinStabilized.getAttitude(PVCoordinatesProvider pvProv,
AbsoluteDate date,
Frame frame)
Compute the attitude corresponding to an orbital state.
|
Attitude |
LofOffsetPointing.getAttitude(PVCoordinatesProvider pvProv,
AbsoluteDate date,
Frame frame)
Compute the attitude corresponding to an orbital state.
|
Attitude |
GroundPointingWrapper.getBaseState(PVCoordinatesProvider pvProv,
AbsoluteDate date,
Frame frame)
Compute the base system state at given date, without compensation.
|
Attitude |
FixedRate.getReferenceAttitude()
Get the reference attitude.
|
Attitude |
Attitude.interpolate(AbsoluteDate interpolationDate,
Collection<Attitude> sample)
Get an interpolated instance.
|
Attitude |
Attitude.shiftedBy(double dt)
Get a time-shifted attitude.
|
Attitude |
Attitude.withReferenceFrame(Frame newReferenceFrame)
Get a similar attitude with a specific reference frame.
|
Modifier and Type | Method and Description |
---|---|
abstract Rotation |
GroundPointingWrapper.getCompensation(PVCoordinatesProvider pvProv,
AbsoluteDate date,
Frame frame,
Attitude base)
Compute the compensation rotation at given date.
|
Rotation |
YawSteering.getCompensation(PVCoordinatesProvider pvProv,
AbsoluteDate date,
Frame orbitFrame,
Attitude base)
Compute the compensation rotation at given date.
|
Rotation |
YawCompensation.getCompensation(PVCoordinatesProvider pvProv,
AbsoluteDate date,
Frame orbitFrame,
Attitude base)
Compute the compensation rotation at given date.
|
Modifier and Type | Method and Description |
---|---|
Attitude |
Attitude.interpolate(AbsoluteDate interpolationDate,
Collection<Attitude> sample)
Get an interpolated instance.
|
Constructor and Description |
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FixedRate(Attitude referenceAttitude)
Creates a new instance.
|
Constructor and Description |
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TabulatedProvider(List<Attitude> table,
int n,
boolean useRotationRate)
Creates new instance.
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Modifier and Type | Method and Description |
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Attitude |
SpacecraftState.getAttitude()
Get the attitude.
|
Constructor and Description |
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SpacecraftState(Orbit orbit,
Attitude attitude)
Build a spacecraft state from orbit and attitude provider.
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SpacecraftState(Orbit orbit,
Attitude attitude,
double mass)
Build a spacecraft state from orbit, attitude provider and mass.
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SpacecraftState(Orbit orbit,
Attitude attitude,
double mass,
Map<String,double[]> additional)
Build a spacecraft state from orbit, attitude provider and mass.
|
SpacecraftState(Orbit orbit,
Attitude attitude,
Map<String,double[]> additional)
Build a spacecraft state from orbit and attitude provider.
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